BOMBARDIERN213TS STATUS REPORT
with relations
General Categories: RVSM,FAR 91,FAA,Standard Cost:
740.5+Man Hrs:
3,315+
Owner:
Operator:
DuPage Aerospace Corporation
DuPage Aerospace Corporation
7859 APUS7859 Hrs15-Dec-2015P-107CGTCP36-100APU 1
6728 Enc12020.4 Hrs10-Feb-2016350107CF34-3AEng 2
6769 Enc12137.4 Hrs10-Feb-2016350101CF34-3AEng 1
6326 Ldg12041.2 Hrs10-Feb-20163013Challenger 601Airframe
Analyst: Jeffrey Ivy [email protected]
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
▼ 5 - TIME LIMITS/MAINTENANCE CHECKS
Unscheduled Maintenance CheckRE (A/R)05-50-01 Hard/Overweight Landing Checks
Mos
Hrs
Ldg
5 A/F
Unscheduled Maintenance CheckRE (A/R)05-50-02 Extreme Turbulence Or Maneuver Checks
Mos
Hrs
Ldg
5 A/F
Unscheduled Maintenance CheckRE (A/R)05-50-03 Lightning Strike Check
Mos
Hrs
Ldg
5 A/F
Unscheduled Maintenance CheckRE (A/R)05-50-04 Engine Checks
Mos
Hrs
Enc
5 ENG1
Unscheduled Maintenance CheckRE (A/R)05-50-04 Engine Checks
Mos
Hrs
Enc
5 ENG2
Unscheduled Maintenance CheckRE (A/R)05-50-05 Main Wheel Fusible Plug Release
Mos
Hrs
Ldg
5 A/F
Unscheduled Maintenance CheckRE (A/R)05-50-06 APU Enclosure Fire
Mos
Hrs
Ldg
5 A/F
Unscheduled Maintenance CheckRE (A/R)05-50-07 Hydraulic System Overheat
Mos
Hrs
Ldg
5 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM1/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Unscheduled Maintenance CheckRE (A/R)05-50-08 Wing Leading Edge Overheat
Mos
Hrs
Ldg
5 A/F
Unscheduled Maintenance CheckRE (A/R)05-50-09 Air Driven Generator In - Flight Deployment - Inspection/Check
Mos
Hrs
Ldg
5 A/F
Unscheduled Maintenance CheckRE (A/R)05-50-10 Hydraulic Pump Shock Mount Contamination
Mos
Hrs
Ldg
5 A/F
Unscheduled Maintenance CheckRE (A/R)05-50-11 Cabin Overpressurization
Mos
Hrs
Ldg
5 A/F
Unscheduled Maintenance CheckRE (A/R)05-50-12 Landing Gear Overspeed Check
Mos
Hrs
Ldg
5 A/F
Unscheduled Maintenance CheckRE (A/R)05-50-13 Wing Flap System Overspeed Check
Mos
Hrs
Ldg
5 A/F
Unscheduled Maintenance CheckRE (A/R)05-50-14 Hydraulic Harrison “H” Fittings
Mos
Hrs
Ldg
5 A/F
Unscheduled Maintenance CheckRE (A/R)05-50-15 Aircraft Tire Limitations
Mos
Hrs
Ldg
5 A/F
Unscheduled Maintenance CheckRE (A/R)05-50-16 CF 34 - Compressor Cleaning
Mos
Hrs
Enc
5 ENG1
Unscheduled Maintenance CheckRE (A/R)05-50-16 CF 34 - Compressor Cleaning
Mos
Hrs
Enc
5 ENG2
Unscheduled Maintenance CheckRE (A/R)05-50-17 Inspection Of Engine Driven Pump (EDP) After Dry Operation Due To Hydraulic Fluid Loss
Mos
Hrs
Enc
5 ENG1
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM2/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Unscheduled Maintenance CheckRE (A/R)05-50-17 Inspection Of Engine Driven Pump (EDP) After Dry Operation Due To Hydraulic Fluid Loss
Mos
Hrs
Enc
5 ENG2
Unscheduled Maintenance CheckRE (A/R)05-50-18 High Energy Stop/Rejected Takeoff (RTO) Damage
Mos
Hrs
Ldg
5 A/F
Unscheduled Maintenance CheckRE (A/R)05-50-19 Inspection After The Aircraft Is Parked In Strong Winds Or Windgusts
Mos
Hrs
Ldg
5 A/F
Unscheduled Maintenance CheckRE (A/R)05-50-20 Inspection After A Bird Strike
Mos
Hrs
Ldg
5 A/F
Unscheduled Maintenance CheckRE (A/R)05-50-21 Inspection After A Tire Burst
Mos
Hrs
Ldg
5 A/F
MandatoryRE (-)2006-25-16 Corrosion Prevention and Control Program (CPCP)
12-Sep-2008Mos
11,455.7Hrs
5,898Ldg
5 A/FINSPECTEDEff: 19-Jan-2007 Complied
With
MandatoryRE (-)2013-03-08 Periodic Inspections
10-May-2013Mos
11,786Hrs
6,141Ldg
5 A/FREVISED MAINT DOCSEff: 19-Mar-2013 Complied
With
Nextdue Share EarliestDUE:1. T 60 Days | 2. RE -Periodic Inspections - Time Limits/Maintenance Checks (TLMC)...2013-03-08 Paragraph (g)A/F5
Nextdue Share EarliestDUE:1. T 12 Mos, 7800 Ldg (later) | 2. RE -Periodic Inspections - Initial Compliance Times for Inspect...2013-03-08 Paragraph (h)A/F5
MandatoryRE (-)2013-03-08 Paragraph (g) Periodic Inspections - Time Limits/Maintenance Checks (TLMC) Manual Revision
10-May-2013Days
11,786Hrs
6,141Ldg
5 A/FREVISED MAINT DOCSEff: 19-Mar-2013 Complied
With
MandatoryRE (-)2013-03-08 Paragraph (h) Periodic Inspections - Initial Compliance Times for Inspections
10-May-2013Mos
11,786Hrs
6,141Ldg
5 A/FREVISED MAINT DOCSEff: 19-Mar-2013 Complied
With
OptionalT (A/R)601-0590 Scheduled Maintenance Instructions (MSG-3 Derived) – Qualification
Mos
Hrs
Ldg
5 A/FEff: 17-Dec-2007
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM3/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
FAA, FAAREFAA 14 CFR Part 47 FAA - Aircraft Registration
4.9 Months (+181
Days)01-Sep-2016+63628-Feb-2014Mos
Hrs
Ldg
5 A/FExpiration Date 28-Feb-2017
FAA, FAA ≈20-May-2017REFAA RVSM FAA - RVSM Height Monitoring
-1.6 Year27-Aug-20142427-Aug-2012Mos
612.3 Hrs12,653.51,00011,653.5Hrs
Ldg
5 A/F
REPKG 12 Month 12 Monthly Tasks
6.6 Months (+31
Days)21-Oct-2016-/+11221-Oct-2015Mos
Hrs
Ldg
5 A/F
In PackageDUE: 21-Oct-20161. RE 12 MosScheduled Servicing - Lubricate throttle control inner eleme...12-20-00-309A/F12
In PackageDUE: 21-Oct-20161. RE 12 MosScheduled Servicing - Lubricate air driven generator (ADG)12-20-00-312A/F12
In PackageDUE: 21-Oct-20161. RE 12 MosScheduled Servicing - Lubricate flap actuator12-20-00-313A/F12
In PackageDUE: 21-Oct-20161. RE 12 MosWire Cables - Flight Controls Visual Check (using a borescop...20-40-00-203A/F20
In PackageDUE: 21-Oct-20161. RE 12 MosBattery System - Operational Test (Cycling) of the Thermal C...24-00-00-301A/F24
In PackageDUE: 21-Oct-20161. RE 12 MosADG Auto-Deploy Control Unit Operational Test - ADG Auto-De...24-23-46-210A/F24
In PackageDUE: 21-Oct-20161. RE 12 MosBattery System Functional Test - Main Battery Charger Therm...24-33-00-213A/F24
In PackageDUE: 21-Oct-20161. RE 12 MosAuxiliary Power Unit Firex Container - Check APU Firex Conta...26-21-11-206A/F26
In PackageDUE: 21-Oct-20161. RE 12 MosAuxiliary Power Unit Firex Discharge Line Visual Check26-21-21-205A/F26
In PackageDUE: 21-Oct-20161. RE 12 MosPower Plant Firex Container - Check Power Plant Firex Contai...26-23-11-210A/F26
In PackageDUE: 21-Oct-20161. RE 12 MosPower Plant Firex Container - Check Power Plant Firex Contai...26-23-11-210A/F26
In PackageDUE: 21-Oct-20161. RE 12 MosPortable Fire Extinguisher - Check weight26-25-00-213A/F26
In PackageDUE: 21-Oct-20161. RE 12 MosPortable Fire Extinguisher - Check weight26-25-00-213A/F26
In PackageDUE: 21-Oct-20161. RE 12 MosMain Gear Trailing Arm Check transverse shear bolt32-10-36-204A/F32
In PackageDUE: 21-Oct-20161. RE 12 MosEmergency Lighting Inspect Power Supplies per Check section ...33-50-00-203A/F33
In PackageDUE: 21-Oct-20161. RE 12 MosEmergency Lighting Inspect Power Supplies per Check section ...33-50-00-203A/F33
In PackageDUE: 21-Oct-20161. RE 12 MosPitot Static System and Temperature Sensing System Pitot sta...34-11-00-202A/F34
In PackageDUE: 21-Oct-20161. RE 12 MosStandby Magnetic Compass - Compass Swing34-27-00-206A/F34
In PackageDUE: 21-Oct-20161. RE 12 MosAPU Starting and Ignition (Post SB 601-0099 and A/C 3045 to ...49-40-00-211A/F49
In PackageDUE: 21-Oct-20161. RE 12 MosFloor Structure Under Toilet and Galley (without removal) ca...53-10-11-228A/F53
In PackageDUE: 21-Oct-20161. RE 12 MosAttachment Fittings (Nose Gear Trunnion Assembly) Visual Che...53-40-00-225A/F53
In PackageDUE: 21-Oct-20161. RE 12 MosWing Structure Visual Check of the following areas: (1) Wing...57-00-00-203A/F57
In PackageDUE: 21-Oct-20161. RE 12 MosPlates/Skins (Wing Box Lower Skin BL0.00 to WS148.00) Visual...57-30-00-213A/F57
≈20-Oct-2017REPKG 1200 Eng Hour 1200 Engine Hourly Task
29-Oct-2012Mos
812.3 Hrs (+40)12,949.7-/+401,20011,749.7Hrs
Enc
5 ENG1
In PackageDUE: 12,949.7 Hrs1. RE 1200 HrsEngine - General - Borescope inspection of combustion liner ...72-00-00-210ENG172
In PackageDUE: 12,949.7 Hrs1. RE 1200 HrsEngine - General - Borescope inspection of turbine section, ...72-00-00-211ENG172
In PackageDUE: 12,949.7 Hrs1. RE 1200 HrsEngine - General (Pre G.E. SB (CF34) 72-11) - Borescope insp...72-00-00-212ENG172
In PackageDUE: 12,949.7 Hrs1. RE 1200 HrsEngine - General (Pre SB 75-2) - B-Sump pressure measurement...72-00-00-220ENG172
In PackageDUE: 12,949.7 Hrs1. RE 1200 HrsOil/Fuel Heat Exchanger Assembly - Visual Check, paying part...79-20-26-208ENG179
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM4/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
≈20-Oct-2017REPKG 1200 Eng Hour 1200 Engine Hourly Task
29-Oct-2012Mos
812.3 Hrs (+40)12,832.7-/+401,20011,632.7Hrs
Enc
5 ENG2
In PackageDUE: 12,832.7 Hrs1. RE 1200 HrsEngine - General - Borescope inspection of combustion liner ...72-00-00-210ENG272
In PackageDUE: 12,832.7 Hrs1. RE 1200 HrsEngine - General - Borescope inspection of turbine section, ...72-00-00-211ENG272
In PackageDUE: 12,832.7 Hrs1. RE 1200 HrsEngine - General (Pre G.E. SB (CF34) 72-11) - Borescope insp...72-00-00-212ENG272
In PackageDUE: 12,832.7 Hrs1. RE 1200 HrsEngine - General (Pre SB 75-2) - B-Sump pressure measurement...72-00-00-220ENG272
In PackageDUE: 12,832.7 Hrs1. RE 1200 HrsOil/Fuel Heat Exchanger Assembly - Visual Check, paying part...79-20-26-208ENG279
≈20-Oct-2017REPKG 1200 Hour 1200 Hourly Tasks
29-Oct-2012Mos
812.3 Hrs (+40)12,853.5-/+401,20011,653.5Hrs
Ldg
5 A/F
Also ConsiderDUE: 12,632 Hrs1. RE 600 Hrs600 Hourly TasksPKG 600 HourA/F5
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsScheduled Servicing - Lubricate wing-fuselage pick-up link12-20-00-311A/F12
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsOutflow Valves Outflow valve Functional Test (Using Pressure...21-30-11-208A/F21
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsStatic Dischargers Visual Check - Static Dischargers Functio...23-60-00-201A/F23
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsMain Landing Gear Bay Overheat Detection System Functional T...26-10-21-203A/F26
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsAnti-Float Mechanism Operational Test - Anti-Float Mechanis...27-13-11-204A/F27
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsElevator Control (Pre SB 601-0304) Visual Check of elevator ...27-31-00-214A/F27
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsPitch Trim Actuator - Lubricate horizontal stabilizer pitch ...27-40-00-238A/F27
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsMain Systems Functional Test of Reservoir-Mounted Return Lin...29-10-00-204A/F29
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsCase Drain Filter Check Filter Elements in No. 1, No. 2 and ...29-11-31-208A/F29
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsPressure Manifold Check Filter Elements in No. 1, No. 2 and ...29-11-36-209A/F29
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsReturn Manifold Check Filter Elements in No. 1, No. 2 and No...29-11-41-210A/F29
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsElectrical Anti-Icing Functional Test of Heating Element - F...30-41-00-210A/F30
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsVaristor Suppressor Nominal varistor voltage test - DC stand...30-41-16-211A/F30
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsExtension and Retraction Landing gear control unit - check f...32-30-00-208A/F32
In PackageDUE: 12,853.5 Hrs1. RE N/ADownward Opening Door (Pre SB 601-0451) Internally Lubricate...52-12-00-204A/F52
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsDownward Opening Passenger/Crew Entrance Door Visual Check o...52-12-00-205A/F52
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsDownward Opening Passenger/Crew Entrance Door Functional Tes...52-12-00-206A/F52
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsDoor Warning Functional Test - Baggage Door Switches- Funct...52-70-00-211A/F52
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsFuselage Visual Check of the external skin, paying particula...53-00-00-202A/F53
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsExhaust Nozzle Assembly Remove exhaust nozzle fairing and ca...78-10-00-211 (Left)A/F78
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsExhaust Nozzle Assembly Remove exhaust nozzle fairing and ca...78-10-00-211 (Right)A/F78
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsThrust Reverser Functional Test of auto stow system78-30-00-202 (Left)A/F78
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsThrust Reverser Functional Test of auto stow system78-30-00-202 (Right)A/F78
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsThrust Reverser Thrust Reverser Unlocked Light Functional Te...78-30-00-216 (Left)A/F78
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsThrust Reverser Thrust Reverser Unlocked Light Functional Te...78-30-00-216 (Right)A/F78
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsMain and Pylon Track Slider Blocks Detailed Inspection of sl...78-30-41-201 (Left)A/F78
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsMain and Pylon Track Slider Blocks Detailed Inspection of sl...78-30-41-201 (Right)A/F78
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsAuto-Throttle Retarder Control Functional Test of Auto-Throt...78-30-61-213 (Left)A/F78
In PackageDUE: 12,853.5 Hrs1. RE 1200 HrsAuto-Throttle Retarder Control Functional Test of Auto-Throt...78-30-61-213 (Right)A/F78
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM5/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
REPKG 24 Month 24 Monthly Tasks
10 Months (+29
Days)30-Jan-2017-/+12430-Jan-2015Mos
Hrs
Ldg
5 A/F
Also ConsiderDUE: 21-Oct-20161. RE 12 Mos12 Monthly TasksPKG 12 MonthA/F5
In PackageDUE: 30-Jan-20171. RE 24 MosAir Driven Generator System Operational Test - ADG24-23-00-209A/F24
In PackageDUE: 30-Jan-20171. RE 24 MosHydraulic Power - Hydraulic fluid acidity check29-00-00-301A/F29
In PackageDUE: 30-Jan-20171. RE 24 MosAural Warning System Functional Test of: (1) Overspeed warni...31-51-00-202A/F31
In PackageDUE: 30-Jan-20171. RE 24 MosPitot Static System and Temperature Sensing System Pressure ...34-11-00-203A/F34
In PackageDUE: 30-Jan-20171. RE 24 MosPitot Static System and Temperature Sensing System Altimeter...34-11-00-205A/F34
In PackageDUE: 30-Jan-20171. RE 24 MosPitot Static System and Temperature Sensing System Altimeter...34-11-00-205A/F34
In PackageDUE: 30-Jan-20171. RE 24 MosPitot Static System and Temperature Sensing System Altimeter...34-11-00-205A/F34
In PackageDUE: 30-Jan-20171. RE 24 MosATC Transponder System - Functional Test34-54-00-207A/F34
In PackageDUE: 30-Jan-20171. RE 24 MosATC Transponder System - Functional Test34-54-00-207A/F34
In PackageDUE: 30-Jan-20171. RE 24 MosDigital Clocks - Remove and install new batteries34-62-00-303A/F34
In PackageDUE: 30-Jan-20171. RE 24 MosDigital Clocks - Remove and install new batteries34-62-00-303A/F34
In PackageDUE: 30-Jan-20171. RE 24 MosOverwing Emergency Exit Operational Test52-20-00-207A/F52
In PackageDUE: 30-Jan-20171. RE 24 MosOverwing Emergency Exit Betalight brightness check52-20-00-208A/F52
In PackageDUE: 30-Jan-20171. RE 24 MosOverwing Emergency Exit Lubricate the Overwing Emergency Exi...52-20-00-216A/F52
In PackageDUE: 30-Jan-20171. RE 24 MosNacelles/Pylons, External - CPCP CheckC54-00-801A/F54
In PackageDUE: 30-Jan-20171. RE 24 MosHorizontal Stabilizer Visual Check of the following items pa...55-10-00-202A/F55
In PackageDUE: 30-Jan-20171. RE 24 MosHorizontal Stabilizer Visual Check (Upon removal of the inne...55-10-11-206A/F55
In PackageDUE: 30-Jan-20171. RE 24 MosVertical Stabilizer Visual Check of the Canted Top Rib for c...55-30-00-209A/F55
In PackageDUE: 30-Jan-20171. RE 24 MosAttachment Fittings Visual Check of Horizontal Stabilizer Pi...55-50-00-211A/F55
In PackageDUE: 30-Jan-20171. RE 24 MosAttachment Fittings Visual Check of the vertical stabilizer ...55-50-00-212A/F55
In PackageDUE: 30-Jan-20171. RE 24 MosAttachment Fittings Visual Check of Horizontal Stabilizer - ...55-50-00-213A/F55
In PackageDUE: 30-Jan-20171. RE 24 MosWing Lower External Surface, BL0.00 to WS353.00 - CPCP Check...C57-00-802A/F57
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM6/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
≈13-Jul-2017REPKG 2400 Hour 2400 Hourly Tasks
04-May-2004Mos
684 Hrs (+30)12,725.2-/+302,40010,325.2Hrs
Ldg
5 A/F
Also ConsiderDUE: 12,853.5 Hrs1. RE 1200 Hrs1200 Hourly TasksPKG 1200 HourA/F5
In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsCheck Valves Check Valve inspection21-20-11-202A/F21
In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsPressurization Control Cabin Low Pressure Warning System Ope...21-30-00-206A/F21
In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsPressurization Control Operational Test of Manual Pressuriza...21-30-00-207A/F21
In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsIDG Oil-in Filter Assembly Remove, inspect and install new f...24-21-16-204A/F24
In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsIDG Oil-out Filter Assembly Remove, inspect and install new ...24-21-21-205A/F24
In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsRudder Control Rudder Anti-Jam Mechanism Functional Test27-21-00-211A/F27
In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsPitch Control System Pitch Trim Suppressor Unit - Bench Chec...27-30-00-235A/F27
In PackageDUE: 12,859 Hrs1. RE 2400 HrsElevator Control Elevator load limiters test27-31-00-215A/F27
In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsStall Protection System Functional Test27-39-00-221A/F27
In PackageDUE: 12,208.2 Hrs1. RE 2400 HrsFlap Actuator - Outboard flap actuator backlash check27-50-16-224A/F27
In PackageDUE: 12,859 Hrs1. RE 2400 HrsFlap Actuator Torque and Side Play Check27-50-16-237A/F27
In PackageDUE: 13,259.8 Hrs1. RE 2400 HrsFlexible Drive Shaft - Check flexible drive shaft casing / C...27-50-41-301A/F27
In PackageDUE: 12,366.7 Hrs1. RE 2400 HrsSpoiler Control (Pre SB 601-0113) Ground Spoiler/Thrust Reve...27-61-00-233A/F27
In PackageDUE: 12,467.3 Hrs1. RE 2400 HrsFuel Tanks Check Fuel Tanks for Leaks- Visual Check (externa...28-10-11-204A/F28
In PackageDUE: 12,366.7 Hrs1. RE 2400 HrsFirewall Fuel Shutoff Valve Internal leakage check28-21-16-213A/F28
In PackageDUE: 12,859 Hrs1. RE 2400 HrsWing Anti-Icing Check valve condition check30-11-00-201A/F30
In PackageDUE: 12,208.2 Hrs1. RE 2400 HrsExtension and Retraction Priority Valves Functional Test32-30-00-209A/F32
In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsParking Brake Shutoff Valve Functional Test - Parking Brake...32-45-31-224A/F32
In PackageDUE: 12,467.3 Hrs1. RE 2400 HrsWing Structure Visual Check of leading edge external surface57-00-00-202A/F57
In PackageDUE: 12,467.3 Hrs1. RE 2400 HrsPlates/Skins (Upper Wing Box) Visual Check - External57-30-00-212A/F57
In PackageDUE: 12,467.3 Hrs1. RE 2400 HrsAttachment Fittings - Main Gear Side Brace (MLG Actuator Pic...57-40-00-214A/F57
In PackageDUE: 12,467.3 Hrs1. RE 2400 HrsFlaps (Inboard Flap Vane Assembly) Visual Check (Upon remova...57-53-00-224A/F57
In PackageDUE: 13,118 Hrs1. RE 2400 HrsThrust Reverser General Visual Check of the torque box, torq...78-30-00-212A/F78
In PackageDUE: 12,725.2 Hrs1. RE 2400 HrsThrust Reverser Thrust Reverser Warning Circuit Functional T...78-30-00-215A/F78
In PackageDUE: 13,118 Hrs1. RE 2400 HrsBlocker Doors Special Detailed Inspection of Blocker Door Bu...78-30-26-204A/F78
In PackageDUE: 13,118 Hrs1. RE 2400 HrsFlexshafts Special Detailed Inspection of Flexshaft78-30-51-217A/F78
In PackageDUE: 13,118 Hrs1. RE 2400 HrsBallscrew Actuators Inspection Detailed Inspection of Ballsc...78-30-56-214A/F78
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM7/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
≈25-Sep-2016REPKG 300 Eng Hour 300 Engine Hourly Task
10-Feb-2016Mos
300 Hrs (+40)12,437.4-/+4030012,137.4Hrs
6,769Enc
5 ENG1
In PackageDUE: 12,437.4 Hrs1. RE 300 HrsScheduled Servicing - Lubricate variable geometry actuator12-20-00-314ENG112
In PackageDUE: 12,437.4 Hrs1. RE 300 HrsEngine - General - Visual Check of Fan Stator for the follow...72-00-00-201ENG172
In PackageDUE: 12,437.4 Hrs1. RE 300 HrsEngine - General - Carry out a visual check of the following...72-00-00-203ENG172
In PackageDUE: 12,437.4 Hrs1. RE 300 HrsEngine - General - Visual Check of engine external lines, po...72-00-00-206ENG172
In PackageDUE: 12,437.4 Hrs1. RE 300 HrsEngine - General - Visual check of high pressure turbine sec...72-00-00-208ENG172
In PackageDUE: 12,437.4 Hrs1. RE 300 HrsEngine - General - Compressor Waterwash72-00-00-301ENG172
In PackageDUE: 12,437.4 Hrs1. RE 300 HrsEngine - General (Engine model CF34-1A/-3A/-3A2 only) - Powe...72-00-00-302ENG172
In PackageDUE: 12,437.4 Hrs1. RE 300 HrsFuel Heater Assembly - Check for evidence of leakage from fu...73-10-16-208ENG173
In PackageDUE: 12,437.4 Hrs1. RE 300 HrsFuel Filter Assembly - Check bypass indicator and carry out ...73-10-21-202ENG173
In PackageDUE: 12,437.4 Hrs1. RE 300 HrsN1 Speed Control Amplifier - Visual Check of control amplifi...73-20-16-210ENG173
In PackageDUE: 12,437.4 Hrs1. RE 300 HrsIgnition Exciter - Visual Check74-10-11-203ENG174
In PackageDUE: 12,437.4 Hrs1. RE 300 HrsIgniter Plug - Inspect Igniter plugs74-10-16-202ENG174
In PackageDUE: 12,437.4 Hrs1. RE 300 HrsVariable Geometry Control - Visual Check of VG system, payin...75-30-00-201ENG175
≈25-Sep-2016REPKG 300 Eng Hour 300 Engine Hourly Task
10-Feb-2016Mos
300 Hrs (+40)12,320.4-/+4030012,020.4Hrs
6,728Enc
5 ENG2
In PackageDUE: 12,320.4 Hrs1. RE 300 HrsScheduled Servicing - Lubricate variable geometry actuator12-20-00-314ENG212
In PackageDUE: 12,320.4 Hrs1. RE 300 HrsEngine - General - Visual Check of Fan Stator for the follow...72-00-00-201ENG272
In PackageDUE: 12,320.4 Hrs1. RE 300 HrsEngine - General - Carry out a visual check of the following...72-00-00-203ENG272
In PackageDUE: 12,320.4 Hrs1. RE 300 HrsEngine - General - Visual Check of engine external lines, po...72-00-00-206ENG272
In PackageDUE: 12,320.4 Hrs1. RE 300 HrsEngine - General - Visual check of high pressure turbine sec...72-00-00-208ENG272
In PackageDUE: 12,320.4 Hrs1. RE 300 HrsEngine - General - Compressor Waterwash72-00-00-301ENG272
In PackageDUE: 12,320.4 Hrs1. RE 300 HrsEngine - General (Engine model CF34-1A/-3A/-3A2 only) - Powe...72-00-00-302ENG272
In PackageDUE: 12,320.4 Hrs1. RE 300 HrsFuel Heater Assembly - Check for evidence of leakage from fu...73-10-16-208ENG273
In PackageDUE: 12,320.4 Hrs1. RE 300 HrsFuel Filter Assembly - Check bypass indicator and carry out ...73-10-21-202ENG273
In PackageDUE: 12,320.4 Hrs1. RE 300 HrsN1 Speed Control Amplifier - Visual Check of control amplifi...73-20-16-210ENG273
In PackageDUE: 12,320.4 Hrs1. RE 300 HrsIgnition Exciter - Visual Check74-10-11-203ENG274
In PackageDUE: 12,320.4 Hrs1. RE 300 HrsIgniter Plug - Inspect Igniter plugs74-10-16-202ENG274
In PackageDUE: 12,320.4 Hrs1. RE 300 HrsVariable Geometry Control - Visual Check of VG system, payin...75-30-00-201ENG275
≈18-Sep-2016REPKG 300 Hour 300 Hourly Task
10-Feb-2016Mos
290.8 Hrs (+40)12,332-/+4030012,041.2Hrs
6,326Ldg
5 A/F
(Tol. Adjustment: -9.2 Hrs)
In PackageDUE: 12,332 Hrs1. RE 300 HrsHydraulic System Replenishing (No.1, No.2, and No.3 Systems)...12-10-29-301A/F12
In PackageDUE: 12,332 Hrs1. RE 300 HrsHydraulic System Replenishing (No.1, No.2, and No.3 Systems)...12-10-29-318A/F12
In PackageDUE: 12,332 Hrs1. RE 300 HrsLanding Gear Replenishing - Check main gear shock strut exte...12-10-32-316A/F12
In PackageDUE: 12,332 Hrs1. RE 300 HrsLanding Gear Replenishing - Check nose gear shock strut exte...12-10-32-317A/F12
In PackageDUE: 12,332 Hrs1. RE 300 HrsScheduled Servicing - Lubricate landing gear doors12-20-00-302A/F12
In PackageDUE: 12,332 Hrs1. RE 300 HrsScheduled Servicing - Lubricate dual brake control valve pus...12-20-00-303A/F12
In PackageDUE: 12,332 Hrs1. RE 300 HrsScheduled Servicing - Lubricate servicing doors / Lubricate ...12-20-00-304A/F12
In PackageDUE: 12,332 Hrs1. RE 300 HrsScheduled Servicing - Lubricate main tracks12-20-00-305A/F12
In PackageDUE: 12,332 Hrs1. RE 300 HrsScheduled Servicing - Lubricate pylon tracks12-20-00-306A/F12
In PackageDUE: 12,332 Hrs1. RE 300 HrsScheduled Servicing - Lubricate inboard flap vane mechanism12-20-00-307A/F12
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM8/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
In PackageDUE: 12,332 Hrs1. RE 300 HrsIntegrated Drive Generator System Differential Pressure Chec...24-21-00-202A/F24
In PackageDUE: 12,332 Hrs1. RE 300 HrsIntegrated Drive Generator Oil System Replenishing - Repleni...24-21-00-301A/F24
In PackageDUE: 12,332 Hrs1. RE 300 HrsPower Plant and APU Fire Sensing Cables Visual Check all vis...26-10-11-201A/F26
In PackageDUE: 12,332 Hrs1. RE 300 HrsAuxiliary Power Unit (APU) Fire Extinguishing Functional Tes...26-21-00-204A/F26
In PackageDUE: 12,332 Hrs1. RE 300 HrsPortable Fire Extinguisher - Check pressure26-25-00-212A/F26
In PackageDUE: 12,332 Hrs1. RE 300 HrsAileron, Flap Actuators and Attachments Visual Check27-11-00-201A/F27
In PackageDUE: 12,332 Hrs1. RE 300 HrsAileron Power Control Unit Operational Test27-17-00-208A/F27
In PackageDUE: 12,332 Hrs1. RE 300 HrsRudder Power Control Units Operational Test27-25-00-212A/F27
In PackageDUE: 12,332 Hrs1. RE 300 HrsElevator Power Control Units Operational Test27-37-00-219A/F27
In PackageDUE: 12,332 Hrs1. RE 300 HrsSpoiler Control/Scheduled Servicing Lubricate Flight Spoiler...27-61-00-231A/F27
In PackageDUE: 12,332 Hrs1. RE 300 HrsGround Spoiler Actuators and Manifold Assembly (Pre SB 601-0...27-69-00-228A/F27
In PackageDUE: 12,332 Hrs1. RE 300 HrsFuel and Vent Line Shrouds Visual Check of the Vent and Dist...28-10-31-211A/F28
In PackageDUE: 12,332 Hrs1. RE 300 HrsHydraulic Power Check Filter Differential Pressure Indicator...29-00-00-201A/F29
In PackageDUE: 12,332 Hrs1. RE 300 HrsNose Cowl Anti-Ice/Thrust Reverser Ducting Visual Check, pay...30-20-21-206A/F30
In PackageDUE: 12,332 Hrs1. RE 300 HrsMain Gear and Doors / Main Landing Gear Uplock /Emergency Ex...32-10-00-210A/F32
In PackageDUE: 12,332 Hrs1. RE 300 HrsMain Landing Gear Lubricate Landing Gear32-10-00-241A/F32
In PackageDUE: 12,332 Hrs1. RE 300 HrsNose Gear and Doors Visual Check32-20-00-205A/F32
In PackageDUE: 12,332 Hrs1. RE 300 HrsNose Landing Gear Lubricate Nose Landing Gear32-20-00-242A/F32
In PackageDUE: 12,332 Hrs1. RE 300 HrsNose Landing Gear Uplock Visual Check, paying particular att...32-30-51-211A/F32
In PackageDUE: 12,332 Hrs1. RE 300 HrsAccumulator/Hydraulic System - Replenishing Check accumulato...32-43-16-222A/F32
In PackageDUE: 12,332 Hrs1. RE 300 HrsDual Brake Control Valve Assembly Visual Check visible porti...32-43-21-216A/F32
In PackageDUE: 12,332 Hrs1. RE 300 HrsFunctional Test of Nose Wheel Steering Selector Valve32-47-00-226A/F32
In PackageDUE: 12,332 Hrs1. RE 300 HrsNosewheel Steering Nosewheel Steering Selector and arming va...32-50-00-226A/F32
In PackageDUE: 12,332 Hrs1. RE 300 HrsMain Landing Gear - CPCP CheckC32-10-801A/F32
In PackageDUE: 12,332 Hrs1. RE 300 HrsNose Landing Gear - CPCP CheckC32-20-801A/F32
In PackageDUE: 12,332 Hrs1. RE 300 HrsEmergency Lighting Visual Check- Operational Test33-50-00-202A/F33
In PackageDUE: 12,332 Hrs1. RE 300 HrsPitot Static System and Temperature Sensing System Visual Ch...34-11-00-201A/F34
In PackageDUE: 12,332 Hrs1. RE 300 HrsPitot Static Heads Clean pitot drain holes34-11-11-208A/F34
In PackageDUE: 12,332 Hrs1. RE 300 HrsDoors Visual Check of passenger/crew entrance door seal52-00-00-201A/F52
In PackageDUE: 12,332 Hrs1. RE 300 HrsPassenger/Crew Entrance Door Visual Check that water drains ...52-10-00-202A/F52
In PackageDUE: 12,332 Hrs1. RE 300 HrsDownward Opening Passenger/Crew Entrance Door Scheduled Serv...52-12-00-212A/F52
In PackageDUE: 12,332 Hrs1. RE 300 HrsDownward Opening Passenger/Crew Entrance Door Cam Latch Mech...52-12-00-213A/F52
In PackageDUE: 12,332 Hrs1. RE 300 HrsDoor Warning - Passenger/Crew Entrance Door Switches Operati...52-70-00-214A/F52
In PackageDUE: 12,332 Hrs1. RE 300 HrsFuselage Visual Check (External)53-00-00-201A/F53
In PackageDUE: 12,332 Hrs1. RE 300 HrsNacelles/Pylons Visual Check - External54-00-00-201A/F54
In PackageDUE: 12,332 Hrs1. RE 300 HrsStabilizers Visual Check - External55-00-00-201A/F55
In PackageDUE: 12,332 Hrs1. RE 300 HrsElevators and Rudder Visual Check - External55-20-00-207A/F55
In PackageDUE: 12,332 Hrs1. RE 300 HrsFlight Compartment Windows Visual Check - Internal and Exter...56-10-00-201A/F56
In PackageDUE: 12,332 Hrs1. RE 300 HrsNose Cowl Assembly Visual Check71-10-11-209A/F71
In PackageDUE: 12,332 Hrs1. RE 300 HrsTranslating Cowl Doors Visual Check, paying particular atten...71-10-16-201A/F71
In PackageDUE: 12,332 Hrs1. RE 300 HrsCore Cowl Doors Check Core Cowl71-12-01-202A/F71
In PackageDUE: 12,332 Hrs1. RE 300 HrsThrust Reverser With thrust reversers manually deployed, vis...78-30-00-208A/F78
In PackageDUE: 12,332 Hrs1. RE 300 HrsThrust Reverser (Pre SB 601-1084) Detailed Inspection of the...78-30-16-219A/F78
In PackageDUE: 12,332 Hrs1. RE 300 HrsAir Turbine Starter/Air Turbine Starter Replenishing Visual ...80-10-11-201A/F80
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM9/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
≈22-Feb-2021REPKG 3000 Eng Hour 3000 Engine Hourly Task
05-Jun-2009Mos
2,417.4 Hrs (+40)14,554.8-/+403,00011,554.8Hrs
Enc
5 ENG1
In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Mid point inspection72-00-00-213ENG172
In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Borescope Compressor / Visual Check of vi...72-00-00-215ENG172
In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Detailed Inspection of engine accessory g...72-00-00-218ENG172
In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Visual Check of 6 o’clock c-sump scavenge...72-00-00-221ENG172
In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Visual Check of LPT stator assembly P/N 6...72-00-00-222ENG172
In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Visual Check of HPT stage 1 and stage 2 s...72-00-00-223ENG172
In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Inspect/Check turbine thermocouple harnes...72-00-00-224ENG172
In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Visual Check of turbine nozzles72-00-00-225ENG172
In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Detailed visual inspection of the swirler...72-00-00-226ENG172
In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Visual Check of primary swirlers, paying ...72-00-00-227ENG172
In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Visual Check of stage 1 and stage 2 nozzl...72-00-00-228ENG172
In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Visual Check of combustion liner after di...72-00-00-229ENG172
In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Check combustion section fuel injector he...72-00-00-230ENG172
In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsEngine - General - Visual Check of fan disk to ensure bushin...72-00-00-231ENG172
In PackageDUE: 13,956 Hrs1. RE 3000 HrsFuel Pump Assembly - General Visual Inspection of the engine...73-10-11-204ENG173
In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsFuel Control Unit - General Visual Inspection of main fuel c...73-20-11-206ENG173
In PackageDUE: 14,554.8 Hrs1. RE 3000 HrsC-Sump Scavenge Screens - Detailed Inspection79-21-01-202ENG179
≈24-Nov-2019REPKG 3000 Eng Hour 3000 Engine Hourly Task
28-Jul-2005Mos
1,818.6 Hrs (+40)13,839-/+403,00010,839Hrs
Enc
5 ENG2
In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Mid point inspection72-00-00-213ENG272
In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Borescope Compressor / Visual Check of vi...72-00-00-215ENG272
In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Detailed Inspection of engine accessory g...72-00-00-218ENG272
In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Visual Check of 6 o’clock c-sump scavenge...72-00-00-221ENG272
In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Visual Check of LPT stator assembly P/N 6...72-00-00-222ENG272
In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Visual Check of HPT stage 1 and stage 2 s...72-00-00-223ENG272
In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Inspect/Check turbine thermocouple harnes...72-00-00-224ENG272
In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Visual Check of turbine nozzles72-00-00-225ENG272
In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Detailed visual inspection of the swirler...72-00-00-226ENG272
In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Visual Check of primary swirlers, paying ...72-00-00-227ENG272
In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Visual Check of stage 1 and stage 2 nozzl...72-00-00-228ENG272
In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Visual Check of combustion liner after di...72-00-00-229ENG272
In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Check combustion section fuel injector he...72-00-00-230ENG272
In PackageDUE: 13,839 Hrs1. RE 3000 HrsEngine - General - Visual Check of fan disk to ensure bushin...72-00-00-231ENG272
In PackageDUE: 13,839 Hrs1. RE 3000 HrsFuel Pump Assembly - General Visual Inspection of the engine...73-10-11-204ENG273
In PackageDUE: 13,839 Hrs1. RE 3000 HrsFuel Control Unit - General Visual Inspection of main fuel c...73-20-11-206ENG273
In PackageDUE: 13,839 Hrs1. RE 3000 HrsC-Sump Scavenge Screens - Detailed Inspection79-21-01-202ENG279
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM10/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
REPKG 36 Month 36 Monthly Tasks
11.9 Months (+31
Days)28-Mar-2017-/+13628-Mar-2014Mos
Hrs
Ldg
5 A/F
Also ConsiderDUE: 21-Oct-20161. RE 12 Mos12 Monthly TasksPKG 12 MonthA/F5
In PackageDUE: 28-Mar-20171. RE 36 MosAttachment Fittings Visual Check of the vertical stabilizer ...55-50-00-214A/F55
In PackageDUE: 28-Mar-20171. RE 36 MosAttachment Fittings Visual Check of the rudder actuator/hing...55-50-00-215A/F55
In PackageDUE: 28-Mar-20171. RE 36 MosAttachment Fittings Visual Check of the rudder attachment fi...55-50-00-216A/F55
In PackageDUE: 28-Mar-20171. RE 36 MosAttachment Fittings Visual Check of Hinge Fitting on Horizon...55-50-00-217A/F55
In PackageDUE: 28-Mar-20171. RE 36 MosAttachment Fittings Visual Check of PCU Fittings, Horizontal...55-50-00-218A/F55
In PackageDUE: 28-Mar-20171. RE 36 MosAttachment Fittings Visual Check of PCU and Elevator, paying...55-50-00-219A/F55
In PackageDUE: 28-Mar-20171. RE 36 MosVertical Stabilizer Rear Spar Structure - CPCP Check includi...C55-00-805A/F55
In PackageDUE: 28-Mar-20171. RE 36 MosRudder External Skin, Structure and Attachments - CPCP Check...C55-00-812A/F55
In PackageDUE: 28-Mar-20171. RE 36 MosElevator External Skin, Structure and Attachments - CPCP Che...C55-00-813A/F55
REPKG 48 Month 48 Monthly Tasks
2.5 Years (+30 Days)26-Sep-2018-/+14826-Sep-2014Mos
Hrs
Ldg
5 A/F
Also ConsiderDUE: 30-Jan-20171. RE 24 Mos24 Monthly TasksPKG 24 MonthA/F5
In PackageDUE: 26-Sep-20181. RE 48 MosNose-Radome Lightning Strips Functional Test23-60-00-203A/F23
In PackageDUE: 26-Sep-20181. RE 48 MosPassenger/Crew Entrance Door Structure (External) - CPCP Che...C52-00-803A/F52
In PackageDUE: 26-Sep-20181. RE 48 MosFuselage External Skin Panels, FS621.00 to VS67.5% - CPCP Ch...C53-00-814A/F53
In PackageDUE: 26-Sep-20181. RE 48 MosNose Landing Gear Wheel Well Structure - CPCP Check includin...C53-00-815A/F53
In PackageDUE: 26-Sep-20181. RE 48 MosVertical Stabilizer External Surfaces - CPCP Check including...C55-00-801A/F55
In PackageDUE: 26-Sep-20181. RE 48 MosVertical Stabilizer, Pitch Trim Actuator Attachment Structur...C55-00-804A/F55
In PackageDUE: 26-Sep-20181. RE 48 MosHorizontal Stabilizer Front Spar - CPCP Check including the ...C55-00-806A/F55
In PackageDUE: 26-Sep-20181. RE 48 MosHorizontal and Vertical Stabilizer - CPCP Check including th...C55-00-809A/F55
In PackageDUE: 26-Sep-20181. RE 48 MosHorizontal Stabilizer, Pitch Trim Actuator Attachment - CPCP...C55-00-810A/F55
In PackageDUE: 26-Sep-20181. RE 48 MosHorizontal Stabilizer, External Surfaces - CPCP Check includ...C55-00-811A/F55
In PackageDUE: 26-Sep-20181. RE 48 MosMain Landing Gear Actuator Fitting at Wing Box FS513.00 and ...C57-00-810A/F57
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM11/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
≈24-Aug-2023REPKG 4800 Hour 4800 Hourly Tasks
08-Aug-2005Mos
3,618.6 Hrs (+40)15,659.8-/+404,80010,859.8Hrs
Ldg
5 A/F
Also ConsiderDUE: 12,725.2 Hrs1. RE 2400 Hrs2400 Hourly TasksPKG 2400 HourA/F5
In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsAileron Flutter Dampers - Remove, carry out “Testing and Fau...27-13-21-206A/F27
In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsAileron Flutter Dampers - Remove, carry out “Testing and Fau...27-13-21-206A/F27
In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsElevator Flutter Dampers - Remove, carry out “Testing and Fa...27-33-11-217A/F27
In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsElevator Flutter Dampers - Remove, carry out “Testing and Fa...27-33-11-217A/F27
In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsElevator Flutter Dampers - Remove, carry out “Testing and Fa...27-33-11-217A/F27
In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsElevator Flutter Dampers - Remove, carry out “Testing and Fa...27-33-11-217A/F27
In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsAPU Return Line Check Valve Remove Check Valve and Perform I...28-25-21-223A/F28
In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsMain Systems Remove No.1 and No.2 system hydraulic reservoir...29-10-00-205A/F29
In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsMain Systems Remove No.3 system hydraulic reservoir in-line ...29-10-00-206A/F29
In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsStabilizers Structure NDT Check of the vertical stabilizer t...55-50-00-220A/F55
In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsStabilizers Structure NDT Check of the horizontal stabilizer...55-50-00-221A/F55
In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsWing Structure NDT Check of wing to aileron hinge bolts for ...57-40-00-215A/F57
In PackageDUE: 15,659.8 Hrs1. RE 4800 HrsWing to Flap Hinge Bolts NDT Check57-40-00-216A/F57
REPKG 60 Month 60 Monthly Task
5.8 Months (+30
Days)26-Sep-2016-/+16026-Sep-2011Mos
Hrs
Ldg
5 A/F
In PackageDUE: 26-Sep-20161. RE 60 MosWire Cables - Flight Controls Wire Cable Inspection (straigh...20-40-00-202A/F20
In PackageDUE: 26-Sep-20161. RE 60 MosForward and Aft Auxiliary Fuel Tanks External Check28-10-21-206A/F28
In PackageDUE: 26-Sep-20161. RE 60 MosFuel and Vent Line Shrouds Fuselage tank wall interspace and...28-10-31-205A/F28
In PackageDUE: 26-Sep-20161. RE 60 MosFuel and Vent Line Shrouds Pressure test of the following sh...28-10-31-208A/F28
In PackageDUE: 26-Sep-20161. RE 60 MosFuel and Vent Line Shrouds (Post SB 601-0262) Tail tank fuel...28-10-31-209A/F28
In PackageDUE: 26-Sep-20161. RE 60 MosScavenge Fuel Ejector Visual Check of pump screen28-21-26-215A/F28
In PackageDUE: 26-Sep-20161. RE 60 MosWing Anti-Icing Ducting Visual Check of ducts, brackets, cla...30-11-06-204A/F30
In PackageDUE: 22-Mar-20171. RE 60 MosMain Landing Gear Assembly - Detailed Inspection32-10-00-237A/F32
In PackageDUE: 22-Mar-20171. RE 60 MosMain Landing Gear Assembly - Detailed Inspection32-10-00-237A/F32
In PackageDUE: 26-Sep-20161. RE 60 MosNose Landing Gear Assembly - Detailed Inspection32-20-00-239A/F32
In PackageDUE: 26-Sep-20161. RE 60 MosEmergency Extension Visual Check of the control path (straig...32-35-00-244A/F32
In PackageDUE: 26-Sep-20161. RE 60 MosAccumulator Visual Check of No. 2 and No. 3 System Brake Acc...32-43-16-223A/F32
In PackageDUE: 26-Sep-20161. RE 60 MosOverwing Emergency Exit Visual Check of all structure, payin...52-20-00-209A/F52
In PackageDUE: 26-Sep-20161. RE 60 MosBaggage Compartment Door Visual Check of all structure, payi...52-30-00-210A/F52
In PackageDUE: 26-Sep-20161. RE 60 MosOverwing Emergency Exit Door, External - CPCP Check includin...C52-00-801A/F52
In PackageDUE: 26-Sep-20161. RE 60 MosBaggage Compartment Door Structure - CPCP Check including th...C52-00-802A/F52
In PackageDUE: 26-Sep-20161. RE 60 MosMain Landing Gear Doors - CPCP Check including the following...C52-00-804A/F52
In PackageDUE: 26-Sep-20161. RE 60 MosPassenger/Crew Entrance Door Structure (Internal) - CPCP Che...C52-00-805A/F52
In PackageDUE: 26-Sep-20161. RE 60 MosOverwing Emergency Exit Door (Internal) - CPCP Check includi...C52-00-806A/F52
In PackageDUE: 26-Sep-20161. RE 60 MosFuselage Visual Check - External - along rivet lines, paying...53-00-00-204A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Pressure Bulkhead FS202.75) Visual Check of the ...53-10-00-205A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (FS625.30 and Engine Support Beam Attachment) Vis...53-10-00-206A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Keel Longerons) Visual Check of the following it...53-10-00-207A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (FS755.00) Visual Check, paying particular attent...53-10-00-208A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Floor Beam End Fittings at FS621.00) Visual Chec...53-10-00-209A/F53
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM12/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Passenger Door Surround Structure) Visual Check ...53-10-00-210A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Overwing Emergency Exit Surround Structure) Visu...53-10-00-211A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Baggage Door Surround Structure) Visual Check of...53-10-00-212A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Equipment Bay Door Surround Structure) Visual Ch...53-10-00-213A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame - Fuselage Floor Beam Splices Visual Check53-10-00-214A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Frame Assembly FS424.00) Visual Check, paying pa...53-10-00-215A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Frame Assembly FS473.15) Visual Check, paying pa...53-10-00-216A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Frame Assembly FS513.00) Visual Check, paying pa...53-10-00-217A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Frame Assembly FS640.00 and Engine Support Beam ...53-10-00-218A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Frame Assembly FS654.50) Visual Check - Internal53-10-00-219A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (FS672.20 and FS682.20) Visual Check - Internal53-10-00-220A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosFloor Structure (Pre or Post SB 601-0372) - Remove Toilet, G...53-10-11-230A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosCabin Window Cut-Outs NDT Check53-30-00-221A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosPlates/Skins (Side Skin Panel FS409.00 and WL73.50) Visual C...53-30-00-222A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosNose Radome Visual Check, paying particular attention to int...53-50-11-227A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosFuselage Upper External Skin, FS169.00 to FS621.00, above WL...C53-00-801A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosFuselage Lower External Skin, FS169.00 to FS621.00 - CPCP Ch...C53-00-802A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosKeel Longerons and Surround Structure - CPCP Check including...C53-00-804A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosFuselage Frame Attachment at FS755.00 and Skin at FS710.00 t...C53-00-805A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosPassenger Door Surround Structure - CPCP Check including the...C53-00-806A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosOverwing Emergency Exit Door Structure - CPCP Check includin...C53-00-807A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosBaggage Door Surround Structure - CPCP Check including the f...C53-00-808A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Equipment Bay Door Surround Structure) - CPCP Ch...C53-00-809A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosWing to Fuselage Integral Attachment at FS424.00 and BL45.00...C53-00-810A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosWing to Fuselage Integral Attachment at FS473.15 and BL45.00...C53-00-811A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosWing to Fuselage Integral Attachment at FS513.00 and BL13.00...C53-00-812A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosCabin Window Cut-Outs and Surround Structure FS364.00 to FS5...C53-00-813A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosTail Cone Assembly (Pre SB 601-0262) - CPCP Check including ...C53-00-816A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosNose Radome - CPCP Check including the following items: (1) ...C53-00-817A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosFloor Structure, FS589.00 to FS621.00 - CPCP Check including...C53-00-818A/F53
In PackageDUE: 26-Sep-20161. T 120 Mos | 2. RE 60 MosTail Cone (Post SB 601-0262) - CPCP Check including the foll...C53-00-822A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosFloor Structure, FS169.00 to FS280.00 - CPCP Check including...C53-00-823A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosFloor Structure, FS280.00 to FS424.00 - CPCP Check including...C53-00-824A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosFloor Structure, FS424.00 to FS589.00 - CPCP Check including...C53-00-825A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosStructure Adjacent to Overboard Lavatory Services (External)...C53-00-826A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosFuselage Frame FS409.00, Aft Face, External - CPCP Check inc...C53-00-827A/F53
In PackageDUE: 26-Sep-20161. RE 60 MosNacelles/Pylons (Pylon Structure) Visual Check - Internal54-00-00-202A/F54
In PackageDUE: 26-Sep-20161. RE 60 MosNacelles/Pylons, Internal (Pylon Structure) - CPCP CheckC54-00-802A/F54
In PackageDUE: 26-Sep-20161. RE 60 MosHorizontal Stabilizer Visual Check of the following items, p...55-10-00-203A/F55
In PackageDUE: 26-Sep-20161. RE 60 MosHorizontal Stabilizer Visual Check - Internal - Structure at...55-10-00-204A/F55
In PackageDUE: 26-Sep-20161. RE 60 MosVertical Stabilizer Visual Check of the following items, pay...55-30-00-210A/F55
In PackageDUE: 26-Sep-20161. RE 60 MosVertical Stabilizer Front Spar - CPCP Check including the fo...C55-00-802A/F55
In PackageDUE: 26-Sep-20161. RE 60 MosVertical Stabilizer Internal Structure - CPCP Check includin...C55-00-803A/F55
In PackageDUE: 26-Sep-20161. RE 60 MosHorizontal Stabilizer Rear Spar - CPCP Check including the f...C55-00-807A/F55
In PackageDUE: 26-Sep-20161. RE 60 MosHorizontal Stabilizer Internal Structure - CPCP Check includ...C55-00-808A/F55
In PackageDUE: 26-Sep-20161. RE 60 MosWing Structure - Wing Box Visual Check of the following item...57-00-00-204A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Wing Center Section Internal Structure) Visual C...57-10-00-205A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Front Spar Splice WS29.42) Visual Check (Interna...57-10-00-206A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Wing Inboard Box Internal Structure WS45.00 to W...57-10-00-207A/F57
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM13/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Wing Outboard Box Internal Structure WS148.00 to...57-10-00-208A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosMain Frame (Rear Spar Splice at WS45.00) Visual Check (Inter...57-10-00-209A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosAuxiliary Structure (Winglet) Visual Check (Internal and Ext...57-20-00-210A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosAuxiliary Structure Visual Check of Wing Trailing Edge and W...57-20-00-211A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosAttachment Fittings (Main Gear Trunnion) Visual Check (as ex...57-40-00-217A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosAttachment Fittings (Wing to Fuselage Attach Assembly FS424....57-40-00-218A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosAttachment Fittings (Wing to Fuselage Attachment Fitting FS4...57-40-00-219A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosAttachment Fittings (Hinge/Actuator Aileron) Visual Check (U...57-40-00-220A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosAttachment Fittings (Flap Hinges) Visual Check (Upon extensi...57-40-00-221A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosFlight Control Surfaces (Ailerons, Spoilers and Flaps) Visua...57-50-00-222A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosWing Front Spar and Leading Edge WS50.00 to WS353.00 - CPCP ...C57-00-801A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosWing Upper Surface, BL0.00 to BL50.00 - CPCP Check: (1) Wing...C57-00-803A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosWing Structure Between the Front Spar and Rear Spar, BL0.00 ...C57-00-804A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosWing Front Spar, BL0.00 to WS50.00 - CPCP Check of the follo...C57-00-805A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosWing Structure Between the Front Spar and Rear Spar, WS45.00...C57-00-806A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosWing Rear Spar, BL0.00 to WS66.00 (External) - CPCP Check in...C57-00-807A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosWingtip/Winglet Assembly (Internal/External) - CPCP Check in...C57-00-808A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosWing Rear Spar and Auxiliary Spar, WS50.00 to WS353.00 - CPC...C57-00-809A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosWing Rear Spar and Auxiliary Spar, WS66.00 to WS148.00 - CPC...C57-00-811A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosWing to Fuselage Attachment Fitting, FS424.00 and BL45.00 - ...C57-00-812A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosWing to Fuselage Attachment Fitting, FS473.15 and BL45.00 - ...C57-00-813A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosOutboard Flap (External) - CPCP Check including the followin...C57-00-814A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosInboard Flap (External) - CPCP Check including the following...C57-00-815A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosInboard Flap Vane Actuating Assemblies - CPCP Check includin...C57-00-816A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosAileron (External) - CPCP Check including the following item...C57-00-817A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosFlight Spoiler (External) - CPCP Check including the followi...C57-00-818A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosWing Upper External Surface, WS50.00 to WS353.00 - CPCP Chec...C57-00-819A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosWing to Fuselage Attachment Fitting, WS513.00 and BL45.00 - ...C57-00-820A/F57
In PackageDUE: 26-Sep-20161. RE 60 MosForward Engine Mount - CPCP Check including the following it...C71-00-801A/F71
In PackageDUE: 26-Sep-20161. RE 60 MosAft Engine Mount - CPCP Check including the following items:...C71-00-802A/F71
In PackageDUE: 26-Sep-20161. RE 60 MosForward Nacelle and Nose Cowl Actuator Support Fitting - CPC...C71-00-803A/F71
In PackageDUE: 26-Sep-20161. RE 60 MosThrust Reverser - CPCP Check including the following items: ...C78-00-801A/F78
≈10-May-2017REPKG 600 Eng Hour 600 Engine Hourly Task
10-Feb-2016Mos
600 Hrs (+40)12,737.4-/+4060012,137.4Hrs
6,769Enc
5 ENG1
In PackageDUE: 12,737.4 Hrs1. RE 600 HrsEngine - General - Carry out a visual check of the following...72-00-00-209ENG172
In PackageDUE: 12,737.4 Hrs1. RE 600 HrsEngine - General - Oil Sample Check72-00-00-219ENG172
In PackageDUE: 12,737.4 Hrs1. RE 600 HrsFuel Filter Assembly - Check Fuel filter element73-10-21-203ENG173
In PackageDUE: 12,728.2 Hrs1. RE 600 HrsPneumatic Drive/Flexshaft Lock Unit (Pre Allied Signal SB 12...78-30-46-206ENG178
In PackageDUE: 12,737.4 Hrs1. RE 600 HrsOil Filter Assembly - Inspect and install new filter element79-20-21-203ENG179
In PackageDUE: 12,737.4 Hrs1. RE 600 HrsOil Filter Impending Bypass Sensor - Functional Test79-30-26-204ENG179
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM14/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
≈03-May-2017REPKG 600 Eng Hour 600 Engine Hourly Task
10-Feb-2016Mos
590.8 Hrs (+40)12,611.2-/+4060012,020.4Hrs
6,728Enc
5 ENG2
(Tol. Adjustment: -9.2 Hrs)
In PackageDUE: 12,611.2 Hrs1. RE 600 HrsEngine - General - Carry out a visual check of the following...72-00-00-209ENG272
In PackageDUE: 12,611.2 Hrs1. RE 600 HrsEngine - General - Oil Sample Check72-00-00-219ENG272
In PackageDUE: 12,611.2 Hrs1. RE 600 HrsFuel Filter Assembly - Check Fuel filter element73-10-21-203ENG273
In PackageDUE: 12,611.2 Hrs1. RE 600 HrsPneumatic Drive/Flexshaft Lock Unit (Pre Allied Signal SB 12...78-30-46-206ENG278
In PackageDUE: 12,611.2 Hrs1. RE 600 HrsOil Filter Assembly - Inspect and install new filter element79-20-21-203ENG279
In PackageDUE: 12,611.2 Hrs1. RE 600 HrsOil Filter Impending Bypass Sensor - Functional Test79-30-26-204ENG279
≈03-May-2017REPKG 600 Hour 600 Hourly Tasks
10-Feb-2016Mos
590.8 Hrs (+40)12,632-/+4060012,041.2Hrs
6,326Ldg
5 A/F
(Tol. Adjustment: -9.2 Hrs)
In PackageDUE: 12,632 Hrs1. RE 600 HrsScheduled Servicing - Lubricate BUTE door hinge / Lubricate ...12-20-00-308A/F12
In PackageDUE: 12,632 Hrs1. RE 600 HrsWire Cables - Flight Controls Wire Cable Inspection (except ...20-40-00-201A/F20
In PackageDUE: 12,632 Hrs1. RE 600 HrsDistribution Visual Check of accessible Air Conditioning Plu...21-20-00-201A/F21
In PackageDUE: 12,632 Hrs1. RE 600 HrsPressurization Control Operational Test of Emergency Pressur...21-30-00-204A/F21
In PackageDUE: 12,632 Hrs1. RE 600 HrsPressurization Control Operational Test of Emergency Depress...21-30-00-205A/F21
In PackageDUE: 12,632 Hrs1. RE 600 HrsOutflow Valves - Remove and install new filter element21-30-11-301A/F21
In PackageDUE: 12,632 Hrs1. RE 600 HrsEmergency Ram Air Shutoff Valve Functional Test Emergency Ra...21-53-11-210A/F21
In PackageDUE: 12,632 Hrs1. RE 600 HrsWater Separator - Clean coalescer bag21-70-11-302A/F21
In PackageDUE: 12,632 Hrs1. RE 600 HrsAC Generation Functional Test - Complete Generator System24-20-00-201A/F24
In PackageDUE: 12,632 Hrs1. RE 600 HrsDC Static Conversion System Functional Test24-31-00-211A/F24
In PackageDUE: 12,632 Hrs1. RE 600 HrsCrew Seats/Safety Harness and Inertial Reel Visual Check, pa...25-11-00-201A/F25
In PackageDUE: 12,632 Hrs1. RE 600 HrsPower Plant Firex Discharge Lines Visual Check, paying parti...26-23-21-215A/F26
In PackageDUE: 12,632 Hrs1. RE 600 HrsAileron Control Check aileron backlash27-11-00-202A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsTension Regulator Operational Test - Tension Regulator27-11-11-203A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsAileron Flutter Dampers - Check aileron flutter damper / Che...27-13-21-205A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsAileron Flutter Dampers - Check aileron flutter damper / Che...27-13-21-205A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsRoll Disconnect Mechanism Functional Test27-15-00-207A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsAileron Power Control Unit Visual Check, paying particular a...27-17-00-209A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsRudder Control Check Rudder Backlash- Check PCU Input Load L...27-21-00-210A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsElevator Control Check elevator backlash - Check PCU Input J...27-31-00-213A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsElevator Flutter Dampers - Check elevator flutter damper27-33-11-216A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsElevator Flutter Dampers - Check elevator flutter damper27-33-11-216A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsElevator Flutter Dampers - Check elevator flutter damper27-33-11-216A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsElevator Flutter Dampers - Check elevator flutter damper27-33-11-216A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsPitch Disconnect Mechanism Operational Test27-35-00-218A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsStall Protection System Operational Test27-39-00-220A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsHorizontal Stabilizer Trim Control Pitch trim actuator backl...27-40-00-222A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsPitch Trim Actuator - Inspect pitch trim actuator27-40-16-223A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsFlap Actuator Detailed Inspection27-50-16-236A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsPower Drive Unit (PDU) Operational Test of flap PDU motor br...27-50-21-225A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsAsymmetry/Overspeed Detector and Brake Brake drag torque tes...27-50-26-226A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsFlexible Drive Shaft Check flexible drive shaft casing27-50-41-227A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsSpoiler Control Visual Check of Flight Spoiler and Ground Sp...27-61-00-229A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsSpoiler Control (A/C 3001 to 3059 with SB 601-0113 NOT incor...27-61-00-230A/F27
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM15/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
In PackageDUE: 12,632 Hrs1. RE 600 HrsFlight Spoiler Power Control Units Operational Test27-65-00-234A/F27
In PackageDUE: 12,632 Hrs1. RE 600 HrsFuel Tank Gravity Filler Cap Remove, inspect for condition a...28-10-00-225A/F28
In PackageDUE: 12,632 Hrs1. RE 600 HrsHydraulic Power Internal leakage Check29-00-00-202A/F29
In PackageDUE: 12,632 Hrs1. RE 600 HrsHeat Exchanger Visual Check, paying particular attention to ...29-11-51-211A/F29
In PackageDUE: 12,632 Hrs1. RE 600 HrsNo. 3 Main System Visual Check pump installation areas for c...29-13-00-212A/F29
In PackageDUE: 12,632 Hrs1. RE 600 HrsWing Anti-Ice Coupling (Pre SB 601-0433) Detailed inspection...30-11-06-212A/F30
In PackageDUE: 12,632 Hrs1. RE 600 HrsAural Warning System Operational Test of Fire Detection Warn...31-51-00-201A/F31
In PackageDUE: 12,632 Hrs1. RE 600 HrsWeight on Wheels Functional Test32-05-11-201A/F32
In PackageDUE: 12,632 Hrs1. RE 600 HrsExtension and Retraction Functional Test - Landing Gear Retr...32-30-00-207A/F32
In PackageDUE: 12,632 Hrs1. RE 600 HrsNose Gear Drag Brace Visual Check, paying particular attenti...32-30-26-206A/F32
In PackageDUE: 12,632 Hrs1. RE 600 HrsEmergency Extension Functional Test32-35-00-212A/F32
In PackageDUE: 12,632 Hrs1. RE 600 HrsEmergency Extension Visual Check of the control path (except...32-35-00-243A/F32
In PackageDUE: 12,632 Hrs1. RE 600 HrsDual Brake Control Valve Assembly Brake pressure decay check32-43-21-221A/F32
In PackageDUE: 12,632 Hrs1. RE 600 HrsParking Brake Control Cable Assembly / Pilots and Co-Pilots ...32-45-11-217A/F32
In PackageDUE: 12,632 Hrs1. RE 600 HrsAnti-Skid System Anti-skid system operational test32-47-00-225A/F32
In PackageDUE: 12,632 Hrs1. RE 600 HrsNosewheel Steering - Functional test of Electronic Control M...32-50-00-236A/F32
In PackageDUE: 12,632 Hrs1. RE 600 HrsCrew Oxygen System Functional Test35-10-00-201A/F35
In PackageDUE: 12,632 Hrs1. RE 600 HrsBleed Air Distribution Visual Check - Ducting36-10-00-201A/F36
In PackageDUE: 12,632 Hrs1. RE 600 HrsDownward Opening Passenger/Crew Entrance Door Visual Check o...52-12-00-203A/F52
In PackageDUE: 12,632 Hrs1. RE 600 HrsIgnition System Operational Test - Ignition System74-00-00-204 (Left)A/F74
In PackageDUE: 12,632 Hrs1. RE 600 HrsIgnition System Operational Test - Ignition System74-00-00-204 (Right)A/F74
In PackageDUE: 12,632 Hrs1. RE 600 HrsBallscrew Actuators Lubrication of Ballscrew Actuators and M...78-30-00-218A/F78
In PackageDUE: 12,632 Hrs1. RE 600 HrsCascades/Pylon Tracks Visual Check78-30-11-209A/F78
In PackageDUE: 12,632 Hrs1. RE 600 HrsMain Tracks Visual Check of the main track and attachments78-30-31-210A/F78
In PackageDUE: 12,641.2 Hrs1. RE 600 HrsAir Turbine Starter Air Turbine Starter (ATS) Oil change80-10-11-202 (Left)A/F80
In PackageDUE: 12,641.2 Hrs1. RE 600 HrsAir Turbine Starter Air Turbine Starter (ATS) Oil change80-10-11-202 (Right)A/F80
In PackageDUE: 12,632 Hrs1. RE 600 HrsAir Turbine Starter (Part No. 3505188-9 and Subs) - Detailed...80-10-11-203A/F80
REPKG 96 Month 96 Monthly Tasks
OVD11-Dec-2015-/+19611-Dec-2007Mos
Hrs
Ldg
5 A/F
Also ConsiderDUE: 26-Sep-20181. RE 48 Mos48 Monthly TasksPKG 48 MonthA/F5
In PackageDUE: 11-Dec-20151. RE 96 MosLower Fuselage Skins (External) NDT Check53-30-00-224A/F53
≈29-Dec-2030REPKG 9600 Hour 9600 Hourly Task
05-Aug-2003Mos
7,144.4 Hrs (+40)19,185.6-/+409,6009,585.6Hrs
Ldg
5 A/F
In PackageDUE: 19,185.6 Hrs1. RE 9600 HrsCheck Valves Visual Check of Conditioned Air and Cold Air Ch...21-20-11-203A/F21
In PackageDUE: 19,185.6 Hrs1. RE 9600 HrsCollector Tanks Collector Tank Flapper Check Valves Check28-21-11-212A/F28
In PackageDUE: 19,185.6 Hrs1. RE 9600 HrsWing Anti-Icing Functional Test Wing Anti-Icing30-11-00-202A/F30
In PackageDUE: 19,185.6 Hrs1. RE 9600 HrsTail Cone Visual Check of interior surface, frames, access d...53-50-00-226A/F53
▼ 8 - LEVELING AND WEIGHING.
AMMRE08-10-01-001 Aircraft Weighing and Balancing
1.4 Years18-Aug-20173618-Aug-2014Mos
Hrs
Ldg
8 A/FInspected Date 18-Aug-2014
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM16/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
▼ 11 - PLACARDS AND MARKINGS
RecommendedRE (-)601-0032 Modification - Tires and Airspeed Limitation Placards - 43,100 Pounds Take-off Weight
01-Sep-1983Mos
0Hrs
0Ldg
11 A/FEff: 15-Mar-1984 Complied With
OptionalT (A/R)601-0205 Modification - Flight Compartment Tire Pressure "Caution" Placard - Special Operating Conditions Only
Mos
Hrs
Ldg
11 A/FEff: 05-Oct-1988
OptionalRE (-)601-0280 Modification - Increased MTOW - 44,600 LBS
Mos
Hrs
Ldg
11 A/F
OptionalRE (-)601-0280 Rev 1 Modification - Increased MTOW - 44,600 LBS
Mos
Hrs
Ldg
11 A/F
OptionalRE (-)601-0280 Rev 2 Modification - Increased MTOW - 44,600 LBS
12-Jun-1999Mos
5,934.4Hrs
2,605Ldg
11 A/FEff: 24-Sep-1990 Complied With
OptionalRE (-)601-0360 Modification - Increased MTOW - 45,100 Lbs
Mos
Hrs
Ldg
11 A/F
OptionalRE (-)601-0360 Rev 1 Modification - Increased MTOW - 45,100 Lbs
12-Jun-1999Mos
5,934.4Hrs
2,605Ldg
11 A/FEff: 12-Dec-1990 Complied With
OptionalRE (-)601-0385 Brazilian Registration Requirements - Servicing and Emergency Placards/Cabin Pressure Indication/Overspeed Warning
Mos
Hrs
Ldg
11 A/F
OptionalT (A/R)601-0385 Rev 1 Brazilian Registration Requirements - Servicing and Emergency Placards/Cabin Pressure Indication/Overspeed Warning
Mos
Hrs
Ldg
11 A/FEff: 30-Oct-1998
OptionalT (A/R)601-0467 Modification - Remove MLG Wheel Discs and Add Placard in Flight Compartment
Mos
Hrs
Ldg
11 A/FEff: 30-Nov-1995
OptionalRE (-)601-0511 Modification - Argentinian Certification Requirements
Mos
Hrs
Ldg
11 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM17/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalT (A/R)601-0511 Rev 1 Modification - Argentinian Certification Requirements
Mos
Hrs
Ldg
11 A/FEff: 24-Mar-2008
RecommendedRE (-)601-0551 Modification - Fuselage Placards and Markings - Addition of Stow Rod Warning Decal on Upper Core Cowl Door
25-Jul-2008Mos
11,432Hrs
5,881Ldg
11 A/FEff: 30-Aug-2002 Complied With
RecommendedRE (-)601-0552 Special Check/Modification - Wing Placards and Markings - Painted Overwing Anti-Slip Walkway
Mos
Hrs
Ldg
11 A/F
RecommendedT (A/R)601-0552 Rev 1 Special Check/Modification - Wing Placards and Markings - Painted Overwing Anti-Slip Walkway
Mos
Hrs
Ldg
11 A/FEff: 15-Dec-2003
OptionalT (-)601-0638 Stage 4 Noise Levels Standards - Certification
Mos
Hrs
Ldg
11 A/FEff: 29-May-2014
OptionalT (A/R)601-0638 Rev 1 Stage 4 Noise Levels Standards - Certification
Mos
Hrs
Ldg
11 A/FEff: 21-Oct-2015
(AVG MAN HRS: 1) (NOTE: Controlled Effectivity)
RecommendedT (A/R)601-1025 Modification - Engine Cowling - Warning Placard
Mos
Hrs
Ldg
11 A/FEff: 12-Dec-1983
RecommendedRE (-)601-1037 Special Check/Modification - Engine Cowling - Warning Placards
Mos
Hrs
Ldg
11 A/F
RecommendedRE (-)601-1037 Rev 1 Special Check/Modification - Engine Cowling - Warning Placards
26-Jan-1987Mos
1,267Hrs
480Ldg
11 A/FEff: 26-Mar-1986 Complied With
MandatoryRE (-)85-14-04 Lightning Protection
13-Nov-1992Mos
Hrs
Ldg
11 A/FSB A601-0069Eff: 12-Aug-1985 Complied
With
AlertRE (-)A601-0052 Special Check/Modification - APU - Removal of Restriction
Mos
Hrs
Ldg
11 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM18/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AlertRE (-)A601-0052 Rev 1 Special Check/Modification - APU - Removal of Restriction
23-Jan-1985Mos
Hrs
Ldg
11 A/FEff: 02-Nov-1984 Complied With
IsModSumRE (-)IS600-11-0001 REV A Kit - Registration Plate Instl. Pax Door Surround
Mos
Hrs
Ldg
11 A/FEff: 08-Aug-2011
IsModSumT (A/R)IS600-11-0001 REV B Kit - Registration Plate Instl. Pax Door Surround
Mos
Hrs
Ldg
11 A/F
▼ 12 - SERVICING - ROUTINE MAINTENANCE
Servicing - Recommended ≈18-Sep-2016RE12-10-29-301 Hydraulic System Replenishing (No.1, No.2, and No.3 Systems) - Check accumulator charge pressures / Service hydraulic overspill containers
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
12 A/F
(ZONE: 140, 190, 310) (ACCESS: 144-DZ, 311-BB) (SOURCE: MPD 3.2)
Servicing - Optional ≈18-Sep-2016RE12-10-29-318 Hydraulic System Replenishing (No.1, No.2, and No.3 Systems) - Check reservoir for fluid level
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
12 A/F
(ZONE: 140, 190, 310) (ACCESS: 144-DZ, 311-BB) (SOURCE: MPD 3.3)
Servicing - Recommended ≈18-Sep-2016RE12-10-32-316 Landing Gear Replenishing - Check main gear shock strut extension
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
12 A/F
(ZONE: 721, 731) (SOURCE: MPD 3.2)
Servicing - Recommended ≈18-Sep-2016RE12-10-32-317 Landing Gear Replenishing - Check nose gear shock strut extension
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
12 A/F
(ZONE: 710) (SOURCE: MPD 3.2)
Servicing - Recommended ≈18-Sep-2016RE12-20-00-302 Scheduled Servicing - Lubricate landing gear doors
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
12 A/F
(ZONE: 700) (SOURCE: MPD 3.2)
Servicing - Recommended ≈18-Sep-2016RE12-20-00-303 Scheduled Servicing - Lubricate dual brake control valve push rods
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
12 A/F
(SOURCE: MPD 3.2)
Servicing - Optional ≈18-Sep-2016RE12-20-00-304 Scheduled Servicing - Lubricate servicing doors / Lubricate baggage compartment door
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
12 A/F
(ZONE: 100, 200, 812, 815, 824) (ACCESS: 112-BR, 140-FR, 190-DR, 211-AL, 212-AR -BR,) (SOURCE: MPD 3.3) (NOTE: more zone (continued);
311-AL, 312-AR, 815-BL)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM19/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Servicing - Recommended ≈18-Sep-2016RE12-20-00-305 Scheduled Servicing - Lubricate main tracks
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
12 A/F
(ZONE: 410, 420) (ACCESS: 413-AB -AT, 423-AB -AT) (SOURCE: MPD 3.2)
Servicing - Recommended ≈18-Sep-2016RE12-20-00-306 Scheduled Servicing - Lubricate pylon tracks
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
12 A/F
(ZONE: 410, 420) (ACCESS: 413-AB -AT, 423-AB -AT) (SOURCE: MPD 3.2)
Servicing - Recommended ≈18-Sep-2016RE12-20-00-307 Scheduled Servicing - Lubricate inboard flap vane mechanism
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
12 A/F
(ZONE: 500, 600) (SOURCE: MPD 3.2)
Servicing - Recommended ≈03-May-2017RE12-20-00-308 Scheduled Servicing - Lubricate BUTE door hinge / Lubricate BUTE door rollers
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
12 A/F
(ZONE: 500, 600) (Tol. Adjustment: -9.2 Hrs) (SOURCE: MPD 3.2)
Servicing - RecommendedRE12-20-00-309 Scheduled Servicing - Lubricate throttle control inner element and pressure seal
6.6 Months (+31
Days)21-Oct-2016-/+11221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
12 A/F
(ZONE: 200) (ACCESS: 222CZ-DZ) (SOURCE: MPD 3.2)
Servicing - Recommended ≈20-Oct-2017RE12-20-00-311 Scheduled Servicing - Lubricate wing-fuselage pick-up link
29-Oct-2012Mos
812.3 Hrs12,853.51,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
12 A/F
(ZONE: 140, 240) (ACCESS: 140-CL-CR) (SOURCE: MPD 3.2)
Servicing - RecommendedRE12-20-00-312 Scheduled Servicing - Lubricate air driven generator (ADG)
6.6 Months (+31
Days)21-Oct-2016-/+11221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
12 A/F
(ZONE: 112) (ACCESS: 112-AR, 116-AZ) (SOURCE: MPD 3.2)
Servicing - RecommendedRE12-20-00-313 Scheduled Servicing - Lubricate flap actuator
6.6 Months (+31
Days)21-Oct-2016-/+11221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
12 A/F
(ZONE: 500, 600) (SOURCE: MPD 3.2)
Servicing - Recommended ≈25-Sep-2016RE12-20-00-314 Scheduled Servicing - Lubricate variable geometry actuator
10-Feb-2016Mos
300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs
6,769Enc
(PKG 300 Eng Hour)
12 ENG1
(ZONE: 410, 420) (ACCESS: 412-AB-AT, 414-AB-AT, 422-AB-AT, 424-AB-AT) (SOURCE: MPD 3.2)
Servicing - Recommended ≈25-Sep-2016RE12-20-00-314 Scheduled Servicing - Lubricate variable geometry actuator
10-Feb-2016Mos
300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs
6,728Enc
(PKG 300 Eng Hour)
12 ENG2
(ZONE: 410, 420) (ACCESS: 412-AB-AT, 414-AB-AT, 422-AB-AT, 424-AB-AT) (SOURCE: MPD 3.2)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM20/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Servicing - OptionalRE12-20-00-320 Scheduled Servicing - Lubrication of the Service Door Locks
35 Days11-May-2016611-Nov-2015Mos
Hrs
Ldg
12 A/F
(ZONE: 100, 200, 812, 815) (ACCESS: 112-BR, 140-FR, 190-DR, 211-AL, 212-AR -BR,) (SOURCE: MPD 3.3) (NOTE: more zone (continued); 311-AL,
312-AR, 815-BL)
OptionalT (A/R)601-0147 Modification - Fuel System Replenishing - Level Attitude Indicators
Mos
Hrs
Ldg
12 A/FEff: 08-Jul-1985
OptionalT (A/R)601-0623 Modification – System and Components Replenishing and Hydraulic Power – Introduction of Hydraulic Servicing Placards with Values at Different Ambient
Temperatures
Mos
Hrs
Ldg
12 A/FEff: 04-Mar-2013
▼ 20 - STANDARD PRACTICES – AIRFRAME
MRB ≈03-May-2017RE20-40-00-201 Wire Cables - Flight Controls Wire Cable Inspection (except for straight runs under cabin floor and in vertical stabilizer), paying particular attention to safetying of
turnbuckles and pulleys for freedom of rotation
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
20 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRBRE20-40-00-202 Wire Cables - Flight Controls Wire Cable Inspection (straight runs under cabin floor and invertical stabilizer), paying particular attention to safetying of turnbuckles and
pulleys for freedom of rotation - Check Cable Tensions
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
20 A/F
(SOURCE: TLMC 05-20-15)
MRBRE20-40-00-203 Wire Cables - Flight Controls Visual Check (using a borescope) of Flight Control Cables located below Toilet/Galley areas (without removal), paying particular attention
to corrosion of cables
6.6 Months (+31
Days)(21-Oct-2016)-/+11221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
20 A/F
(SOURCE: TLMC 05-20-15)
RecommendedT (A/R)601-0561 Special Check/Rework - Wiring - Possible Chafing on Electrical Harness Located on the APU Support Structure
Mos
Hrs
Ldg
20 A/FEff: 31-Oct-2003
▼ 21 - AIR CONDITIONING AND PRESSURIZATION
RE (O/C)2 Inch Check Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Left21 A/FNew3202062-1-1
UNKNOWN
RE (O/C)2 Inch Check Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Right21 A/FNew3202062-1-1
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM21/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)3 Inch Backup Valve
20-Sep-1983Mos
0Hrs
0Ldg
Left21 A/FUnknownUnknown
RE (O/C)3 Inch Shutoff (Emerg Ram Air) Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
21 A/FNew398724-1-1
UNKNOWN
RE (O/C)AC (LIRS) Blower
20-Sep-1983Mos
0Hrs
0Ldg
No.121 A/FUnknownUnknown
RE (O/C)AC (LIRS) Blower
20-Sep-1983Mos
0Hrs
0Ldg
No.221 A/FUnknownUnknown
RE (O/C)Air Pressure Regulator
20-Sep-1983Mos
0Hrs0
0Ldg0
21 A/FNew131402-2
UNKNOWN
RE (O/C)Balancing - 4 Inch Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Left21 A/FNew600-95278-1
UNKNOWN
RE (O/C)Balancing - 4 Inch Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Right21 A/FNew600-95278-1
UNKNOWN
RE (O/C)Cabin Pressure Controller
20-Sep-1983Mos
0Hrs0
0Ldg0
21 A/FNew2117804-2
UNKNOWN
RE (O/C)Cabin Pressure Indicator
20-Sep-1983Mos
0Hrs0
0Ldg0
21 A/FNew600-59117-7
UNKNOWN
RE (O/C)Cabin Pressure Selector
20-Sep-1983Mos
0Hrs0
0Ldg0
21 A/FNew2117598-3
UNKNOWN
RE (O/C)Cabin Temperature Indicator
20-Sep-1983Mos
0Hrs0
0Ldg0
21 A/FNew115-079
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM22/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Check Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
No.121 A/FNew123790-1-1
UNKNOWN
RE (O/C)Check Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
No.221 A/FNew3202062-1-1
UNKNOWN
RE (O/C)Check Valve
20-Sep-1983Mos
0Hrs
0Ldg
No.321 A/FUnknownUnknown
RE (O/C)Control Unit Air Conditioning ECU
20-Sep-1983Mos
0Hrs0
0Ldg0
No.121 A/FNew2201600-4
UNKNOWN
RE (O/C)Control Unit Air Conditioning ECU
20-Sep-1983Mos
0Hrs0
0Ldg0
No.221 A/FNew2201600-4
UNKNOWN
RE (O/C)Cooling Turbine
20-Sep-1983Mos
0Hrs0
0Ldg0
Left21 A/FNew586110-3
UNKNOWN
RE (O/C)Cooling Turbine
09-Jul-2003Mos
9,566.9Hrs
4,786Ldg
Right21 A/F586110-374-2703
RE (O/C)Diverter Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
21 A/FNew228565-1
UNKNOWN
RE (O/C)Duct Temperature Sensor
20-Sep-1983Mos
0Hrs
0Ldg
No.121 A/FUnknownUnknown
RE (O/C)Duct Temperature Sensor
20-Sep-1983Mos
0Hrs
0Ldg
No.221 A/FUnknownUnknown
RE (O/C)Duct Temperature Sensor
20-Sep-1983Mos
0Hrs
0Ldg
No.321 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM23/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Duct Temperature Sensor
20-Sep-1983Mos
0Hrs
0Ldg
No.421 A/FUnknownUnknown
RE (O/C)Ejector Shutoff Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Left21 A/FNew979142-1-1
UNKNOWN
RE (O/C)Ejector Shutoff Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Right21 A/FNew979142-1-1
UNKNOWN
RE (O/C)Fan Sensor
10-Nov-2004Mos
10,467.3Hrs
5,311Ldg
Cabin21 A/F625692-20470-483
RE (O/C)Fan Sensor
20-Sep-1983Mos
0Hrs0
0Ldg0
Cockpit21 A/FNew625692-2
UNKNOWN
RE (O/C)Low Limit Temperature Control Unit
20-Sep-1983Mos
0Hrs0
0Ldg0
Left21 A/FNew625520-2
UNKNOWN
RE (O/C)Low Limit Temperature Control Unit
20-Sep-1983Mos
0Hrs0
0Ldg0
Right21 A/FNew625520-2
UNKNOWN
RE (O/C)Modulating/Shutoff Valve
21-Feb-2002Mos
8,126.5Hrs
3,910Ldg
Left21 A/F979558-8976
RE (O/C)Modulating/Shutoff Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Right21 A/FNew979558-8
UNKNOWN
RE (O/C)Motor Driven Fan
20-Sep-1983Mos
0Hrs0
0Ldg0
21 A/FNew605385-6-1
UNKNOWN
RE (O/C)Pressure Regulating Primary Valve
29-Jul-2004Mos
10,458.3Hrs
5,306Ldg
21 A/F103632-2102-362
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM24/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Pressure Regulating Secondary Valve
29-Jul-2004Mos
10,458.3Hrs
5,306Ldg
21 A/F103664-136-446
RE (O/C)Pressure Regulating Shutoff Valve
25-Jul-2008Mos
11,432Hrs
5,881Ldg
Left21 A/F228845UNKNOWN
RE (O/C)Pressure Regulating Shutoff Valve
20-Sep-1983Mos
0Hrs
0Ldg
Right21 A/FUnknownUnknown
RE (O/C)Pressure Regulating Valve
20-Sep-1983Mos
0Hrs
0Ldg
Left21 A/FUnknownUnknown
RE (O/C)Pressure Regulating Valve
20-Sep-1983Mos
0Hrs
0Ldg
Right21 A/FUnknownUnknown
RE (O/C)Regulating Valve
20-Sep-1983Mos
0Hrs
0Ldg
21 A/FUnknownUnknown
RE (O/C)Temperature Control
20-Sep-1983Mos
0Hrs
0Ldg
21 A/FUnknownUnknown
RE (O/C)Temperature Control
20-Sep-1983Mos
0Hrs0
0Ldg0
No.121 A/FNew625514-2-1
UNKNOWN
RE (O/C)Temperature Control
20-Sep-1983Mos
0Hrs0
0Ldg0
No.221 A/FNew625514-2-1
UNKNOWN
RE (O/C)Temperature Limiter Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
No.121 A/FNew129580-6
UNKNOWN
RE (O/C)Temperature Limiter Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
No.221 A/FNew129580-6
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM25/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Torque Motor
20-Sep-1983Mos
0Hrs0
0Ldg0
No.121 A/FNew124904-1-1
UNKNOWN
RE (O/C)Torque Motor
20-Sep-1983Mos
0Hrs0
0Ldg0
No.221 A/FNew124904-1-1
UNKNOWN
RE (O/C)Upper ACU Thermal Switch
20-Sep-1983Mos
0Hrs0
0Ldg0
Left21 A/FNew641119-2
UNKNOWN
RE (O/C)Upper ACU Thermal Switch
20-Sep-1983Mos
0Hrs0
0Ldg0
Right21 A/FNew641119-2
UNKNOWN
MRB ≈03-May-2017RE21-20-00-201 Distribution Visual Check of accessible Air Conditioning Plumbing and Ducting, paying particular attention to: (1) Discoloration of insulation tubes and condensation in
the tube area which may indicate leakage / (2) The ram air intake and exhausts for F.O.D. and cracks / (3) Air Conditioning ducts and connections under the cockpit
floor
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
21 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈13-Jul-2017RE21-20-11-202 Check Valves Check Valve inspection
04-May-2004Mos
684 Hrs (+30)(12,725.2)-/+402,40010,325.2Hrs
Ldg
(PKG 2400 Hour)
21 A/F
(SOURCE: TLMC 05-20-15) (NOTE: (Footwarmer/Demist Manifold Check Valve Only))
MRB ≈29-Dec-2030RE21-20-11-203 Check Valves Visual Check of Conditioned Air and Cold Air Check Valves forinternal condition
05-Aug-2003Mos
7,144.4 Hrs (+40)(19,185.6)-/+409,6009,585.6Hrs
Ldg
(PKG 9600 Hour)
21 A/F
(SOURCE: TLMC 05-20-15) (NOTE: The inspection criteria for the “Check Valve Inspection” in the Maintenance Manual are equally applicable to
these valves.)
MRB ≈03-May-2017RE21-30-00-204 Pressurization Control Operational Test of Emergency Pressurization System
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
21 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE21-30-00-205 Pressurization Control Operational Test of Emergency Depressurization Control System
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
21 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈13-Jul-2017RE21-30-00-206 Pressurization Control Cabin Low Pressure Warning System Operational Check
24-Feb-2005Mos
684 Hrs (+30)(12,725.2)-/+402,40010,601.2Hrs
Ldg
(PKG 2400 Hour)
21 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM26/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈13-Jul-2017RE21-30-00-207 Pressurization Control Operational Test of Manual Pressurization Control System - Operational Test of Jet Pump Right Bleed Air Check Valve - Operational Test of Jet
Pump Left Bleed Air Check Valve
04-May-2004Mos
684 Hrs (+30)(12,725.2)-/+402,40010,325.2Hrs
Ldg
(PKG 2400 Hour)
21 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE21-30-11-208 Outflow Valves Outflow valve Functional Test (Using Pressure Test Kit) - Visual Check, paying particular attention to valve seat; (1) Alt Limit Control Poppet Mechanism
/ (2) Overpressure Limiter / (3) Negative Pressure Relief
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
21 A/F
(SOURCE: TLMC 05-20-15)
Servicing - Recommended ≈03-May-2017RE21-30-11-301 Outflow Valves - Remove and install new filter element
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
21 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: MPD 3.2)
MRBRE (N/A)21-51-31-209 Air Conditioning Overheat Switch (A/C 3001 to 3059 Post SB 601-0141, A/C 3060 to 3990) - Functional Test of overheat warning
Mos
Hrs
Ldg
21 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE21-53-11-210 Emergency Ram Air Shutoff Valve Functional Test Emergency Ram Air Shutoff Valve
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
21 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
Servicing - Optional ≈03-May-2017RE21-70-11-302 Water Separator - Clean coalescer bag
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
21 A/F
(ZONE: 311, 312) (ACCESS: 311-BB) (Tol. Adjustment: -9.2 Hrs) (SOURCE: MPD 3.3)
OptionalT (A/R)601-0141 Modification - Conditioned Air Ducting - Thermoswitch Addition
Mos
Hrs
Ldg
21 A/FEff: 29-Jan-1987
RecommendedRE (-)601-0151 Modification - Cabin Air and Anti-Ice Ducts - Connections
Mos
Hrs
Ldg
21 A/F
RecommendedRE (-)601-0151 Rev 1 Modification - Cabin Air and Anti-Ice Ducts - Connections
Mos
Hrs
Ldg
21 A/F
RecommendedRE (-)601-0151 Rev 2 Modification - Cabin Air and Anti-Ice Ducts - Connections
27-Jan-1987Mos
0Hrs
Ldg
21 A/FEff: 03-Mar-1989 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM27/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0197 Emergency Pressurization Shut-Off Valve - Wire Protection
01-Dec-1990Mos
3,058.6Hrs
1,212Ldg
21 A/FEff: 23-Mar-1987 Complied With
RecommendedRE (-)601-0241 Modification - RAM Air Duct - Insulation Addition
Mos
Hrs
Ldg
21 A/F
RecommendedRE (-)601-0241 Rev 1 Modification - RAM Air Duct - Insulation Addition
28-Mar-1989Mos
2,373Hrs
910Ldg
21 A/FEff: 04-May-1988 Complied With
OptionalT (A/R)601-0282 Modification - Ground Cooling Fan - Addition of Spacer
Mos
Hrs
Ldg
21 A/FEff: 21-Feb-1989
RecommendedRE (-)601-0310 Modification - Air Conditioning Unit (ACU) - Introduction of Water Extractor
Mos
Hrs
Ldg
21 A/F
RecommendedRE (-)601-0310 Rev 1 Modification - Air Conditioning Unit (ACU) - Introduction of Water Extractor
Mos
Hrs
Ldg
21 A/F
RecommendedRE (-)601-0310 Rev 2 Modification - Air Conditioning Unit (ACU) - Introduction of Water Extractor
14-Oct-1992Mos
Hrs
Ldg
21 A/FEff: 10-Jan-1992 Complied With
OptionalRE (-)601-0323 Modification - Temperature Control - Duct Temperature Sensors
Mos
Hrs
Ldg
21 A/F
OptionalT (A/R)601-0323 Rev 1 Modification - Temperature Control - Duct Temperature Sensors
Mos
Hrs
Ldg
21 A/FEff: 30-Aug-1990
RecommendedT (A/R)601-0369 Modification - Water Extractor Drain Hoses - Addition of Clamps and Inline Restrictors
Mos
Hrs
Ldg
21 A/FEff: 10-Jan-1992
RecommendedRE (-)601-0375 Modification - Air Conditioning Unit (ACU) Ducts - Prevention of Connector Separation
Mos
Hrs
Ldg
21 A/FEff: 20-Mar-1992
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM28/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0442 Special Check/Rework - Pressurization - Outflow Valve - Diaphragm
28-Apr-1995Mos
4,555Hrs
1,824Ldg
21 A/FEff: 15-Feb-1995 Complied With
OptionalT (A/R)601-0448 Modification - Cockpit Air Conditioned - Ducts Replacement Below the Side Consoles
Mos
Hrs
Ldg
21 A/FEff: 29-Feb-1996
OptionalRE (-)601-0450 Modification - Air Conditioning Units (ACU) - ACUs Inhibit During Either Engine Start
12-Nov-1997Mos
5,395Hrs
2,274Ldg
21 A/FComplied With
OptionalT (A/R)601-0450 Rev 1 Modification - Air Conditioning Units (ACU) - ACUs Inhibit During Either Engine Start
Mos
Hrs
Ldg
21 A/FEff: 28-Mar-2002
RecommendedT (A/R)601-0505 Special Check/Rework - Pressurization Control - Check Valves, Part No. 2770080-102 Installation
Mos
Hrs
Ldg
21 A/FEff: 29-May-1998
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Pressurization Control - Check Valves...601-0505 Part AA/F21
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Pressurization Control - Check Valves...601-0505 Part BA/F21
RecommendedRE (-)601-0505 Part A Special Check/Rework - Pressurization Control - Check Valves, Part No. 2770080-102 Installation - Special Check
05-Nov-1998Mos
5,824Hrs
2,521Ldg
21 A/FEff: 29-May-1998 Complied With
RecommendedT (A/R)601-0505 Part B Special Check/Rework - Pressurization Control - Check Valves, Part No. 2770080-102 Installation - Rework
Mos
Hrs
Ldg
21 A/FEff: 29-May-1998
OptionalT (A/R)601-0518 Modification - Temperature Control - Prevention of Ice Formation Downstream of Air Conditioning Units (ACU)
Mos
Hrs
Ldg
21 A/FEff: 31-Jan-2001
RecommendedT (A/R)601-0533 Modification - Air Conditioning Units - Replacement of Existing Relays K2000HG and K2001HG With 5 Second Delay Relays
Mos
Hrs
Ldg
21 A/FEff: 28-Feb-2002
RecommendedRE (-)601-0607 Special Check/Rework – Corrosion Prevention – ACU Exhaust Duct Flange & Fuselage Skin Mating Surfaces
Mos
Hrs
Ldg
21 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM29/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0607 Rev 1 Special Check/Rework – Corrosion Prevention – ACU Exhaust Duct Flange & Fuselage Skin Mating Surfaces
Mos
Hrs
Ldg
21 A/F
RecommendedT (A/R)601-0607 Rev 2 Special Check/Rework – Corrosion Prevention – ACU Exhaust Duct Flange & Fuselage Skin Mating Surfaces
Mos
Hrs
Ldg
21 A/FEff: 24-Jul-2015
AlertRE (-)A601-0016 Modification - Cabin Air Duct - Support Clamps
Mos
Hrs
Ldg
21 A/FEff: 25-Jul-1983
▼ 22 - AUTOFLIGHT
RE (O/C)Autopilot Computer
15-May-2004Mos
10,352.6Hrs
5,241Ldg
22 A/F4029377-91184080661
RE (O/C)Autopilot Controller
16-Nov-2001Mos
7,861.9Hrs
3,759Ldg
22 A/F4018639-904C80030161
RE (O/C)Autopilot-Status Controller
26-Mar-2007Mos
11,045.9Hrs
5,659Ldg
22 A/F4031474-90385020542
RE (O/C)Duplex Aileron Servo
25-Jul-2008Mos
11,432Hrs
5,881Ldg
22 A/F4015373-71381070567
RE (O/C)Duplex Elevator Servo
25-Jul-2008Mos
11,432Hrs
5,881Ldg
22 A/F4015373-71680090415
RE (O/C)Linear Yaw Damper Actuator
20-Sep-1983Mos
0Hrs
0Ldg
Left22 A/FUnknownUnknown
RE (O/C)Linear Yaw Damper Actuator
20-Sep-1983Mos
0Hrs
0Ldg
Right22 A/FUnknownUnknown
RE (O/C)Roll Rate Monitor
20-Sep-1983Mos
0Hrs0
0Ldg0
Left22 A/FNew4015901-921
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM30/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Roll Rate Monitor
20-Sep-1983Mos
0Hrs0
0Ldg0
Right22 A/FNew4015901-921
UNKNOWN
RE (O/C)Stability Augmentation Computer
18-Dec-2014Mos
11,854.6Hrs
Ldg
22 A/F4031475-80585040359
MRB ≈03-May-2017RE22-10-00-201 Autopilot System (Post SB 601-0048 and A/C 3022 to 3066) - Roll Rate Monitors Operational Test
10-Feb-2016Mos
590.8 Hrs (+40)12,632-/+4060012,041.2Hrs
6,326Ldg
22 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
RecommendedRE (-)601-0048 Modification - Autopilot System - Aileron Channel
Mos
Hrs
Ldg
22 A/F
RecommendedRE (-)601-0048 Rev 1 Modification - Autopilot System - Aileron Channel
30-Jan-1987Mos
Hrs
Ldg
22 A/FEff: 10-Jun-1984 Complied With
RecommendedRE (-)601-0125 Modification - Auto Pilot System - A.F.C.S. Light
28-Mar-1989Mos
2,373Hrs
910Ldg
22 A/FEff: 03-Jul-1986 Complied With
OptionalRE (-)601-0143 Modification - Automatic Flight Control System - Improvements
Mos
Hrs
Ldg
22 A/F
OptionalRE (-)601-0143 Rev 1 Modification - Automatic Flight Control System - Improvements
26-Jan-1987Mos
1,267Hrs
480Ldg
22 A/FEff: 18-Aug-1986 Complied With
OptionalT (A/R)601-0166 Modification - Autopilot/Vert Nav Valid Lines - Protection
Mos
Hrs
Ldg
22 A/FEff: 24-Mar-1986
RecommendedRE (-)601-0276 Modification - Flight Guidance Computers - Replacement
Mos
Hrs
Ldg
22 A/F
OptionalT (A/R)601-0403 Modification - Dual-Channel Synchro-Transmitter - Replacement
Mos
Hrs
Ldg
22 A/FEff: 15-Jan-1997
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM31/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0411 Special Check/Rework/Modification - Autopilot System - Wire Splices, Ground Studs and Flight Guidance Computer
Mos
Hrs
Ldg
22 A/F
RecommendedRE (-)601-0570 Modification - General - Conversion of Servo Drive Assemblies from Part No. 4015373-813 and -816 to Part No. 4015373-713 and -716 to Ensure Retention of Clutch
Screws
25-Jul-2008Mos
11,432Hrs
5,881Ldg
22 A/FEff: 16-Feb-2005 Complied With
▼ 23 - COMMUNICATIONS
RE (O/C)Audio Amplifier
20-Sep-1983Mos
0Hrs
0Ldg
23 A/FUnknownUnknown
RE (O/C)Audio Amplifier Filter
20-Sep-1983Mos
0Hrs
0Ldg
23 A/FUnknownUnknown
RE (O/C)Audio Panel
20-Sep-1983Mos
0Hrs
0Ldg
Copilot23 A/FUnknownUnknown
RE (O/C)Audio Panel
04-Mar-2015Mos
11,879.4Hrs
6,207Ldg
Pilot23 A/FM1045-MLAL-GFE7840355 REPAIR
RE (O/C)Audio Unit
16-Nov-2001Mos
7,861.9Hrs
3,759Ldg
23 A/F990-6800-00100120010799
RE (O/C)Cockpit Voice recorder (CVR)
20-Sep-1983Mos
0Hrs0
0Ldg0
23 A/FNewUNKNOWN
UNKNOWN
Assembly SubDUE: 04-Mar-20211. RE DueCockpit Voice Recorder (CVR) Underwater Locating DeviceDK120 / SD40876A/F23
Life LimitRE (Due)Cockpit Voice Recorder (CVR) Underwater Locating Device
4.9 Years04-Mar-202104-Mar-2015Mos
Hrs
Ldg
23 A/F
Expiration Date 04-Mar-2021
DK120SD40876
RE (O/C)Com-2/Nav-2 Controller
20-Sep-1983Mos
0Hrs
0Ldg
23 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM32/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)CVR Inertia Switch
20-Sep-1983Mos
0Hrs
0Ldg
23 A/FUnknownUnknown
RE (O/C)Handset
20-Sep-1983Mos
0Hrs
0Ldg
23 A/FUnknownUnknown
RE (O/C)HF Coupler/PWR Amplifier
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
No.123 A/F064-1017-0211990
RE (O/C)HF Coupler/PWR Amplifier
19-Dec-2003Mos
9,982.2Hrs
5,021Ldg
No.223 A/F064-1017-0210725
RE (O/C)HF Receiver/Transmitter
26-Sep-2006Mos
10,897.5Hrs1,622.8
5,558Ldg941
No.123 A/FOverhauled064-1015-01
32389
RE (O/C)HF Receiver/Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.223 A/FUnknownUnknown
RE (O/C)VHF Antenna
20-Sep-1983Mos
0Hrs0
0Ldg0
No.123 A/FNewS65-8280
UNKNOWN
RE (O/C)VHF Antenna
25-Jul-2008Mos
11,432Hrs
5,881Ldg
No.223 A/FS65-8280-102799
RE (O/C)VHF Communications Control
15-Apr-2003Mos
9,393.4Hrs
4,682Ldg
No.123 A/F822-1120-0056540
RE (O/C)VHF Communications Control
06-Aug-2002Mos
8,695.2Hrs
4,260Ldg
No.223 A/F822-1120-00518010
RE (O/C)VHF Communications Control
20-Sep-1983Mos
0Hrs
0Ldg
No.323 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM33/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)VHF Transceiver
08-Nov-2003Mos
9,866.8Hrs
4,961Ldg
No.123 A/F822-1113-00135906
RE (O/C)VHF Transceiver
30-Oct-2003Mos
9,838.7Hrs
4,941Ldg
No.223 A/F822-1113-001UNKNOWN
RE (O/C)VHF Transceiver
20-Sep-1983Mos
0Hrs
0Ldg
No.323 A/FUnknownUnknown
MandatoryRE (-)2005-11-04 Microphone jack assemblies.
25-Jul-2008Mos
11,432Hrs
5,881Ldg
23 A/FEff: 27-May-2005 Not Applicable
MRB ≈20-Oct-2017RE23-60-00-201 Static Dischargers Visual Check - Static Dischargers Functional Test
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
23 A/F
(SOURCE: TLMC 05-20-15)
MRBRE23-60-00-203 Nose-Radome Lightning Strips Functional Test
2.5 Years (+30 Days)(26-Sep-2018)-/+14826-Sep-2014Mos
Hrs
Ldg
(PKG 48 Month)
23 A/F
(SOURCE: TLMC 05-20-15)
Custom TaskRE23-CUS-003 Cockpit Voice Recorder ULB Battery - Check
11.1 Months04-Mar-20172404-Mar-2015Mos
11,879.4Hrs
6,207Ldg
23 A/F
RecommendedRE (-)601-0281 Modification - Audio Electronic Unit (AEU) - Cockpit Voice Recorder (CVR) Audio Levels
Mos
Hrs
Ldg
23 A/F
RecommendedRE (-)601-0281 Rev 1 Modification - Audio Electronic Unit (AEU) - Cockpit Voice Recorder (CVR) Audio Levels
Mos
Hrs
Ldg
23 A/F
RecommendedRE (-)601-0383 Modification - HF Communications System - Introduction of Improved Fiber-Optic Cables
Mos
Hrs
Ldg
23 A/F
OptionalT (A/R)601-0390 Modification - Audio Electronic Unit (AEU) - Cockpit Voice Recorder (CVR) Continuous Recording (”Hot Mic") Capability
Mos
Hrs
Ldg
23 A/FEff: 06-Sep-1991
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM34/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0405 Modification - Fuel Tank Water Drains - Improved Protective Finish
Mos
Hrs
Ldg
23 A/F
RecommendedRE (-)601-0405 Rev 1 Modification - Fuel Tank Water Drains - Improved Protective Finish
26-Jan-1996Mos
4,785Hrs
1,932Ldg
23 A/FEff: 31-Mar-1995 Complied With
OptionalT (A/R)601-0486 Modification - Interphone - Addition of Shock Mounts to Ground Crew Interphone Unit
Mos
Hrs
Ldg
23 A/FEff: 15-Nov-1996
▼ 24 - ELECTRICAL POWER
AWL - Life LimitREADG Uplock Actuator Assy (Squib)
2.6 Years01-Nov-20186001-Nov-2013Mos
11,854.6Hrs
Ldg
24 A/F
Manufactured Date 01-Nov-2013
055046B575 11/2013
(NOTE: NOTE:Life limit is 60 months from date of manufacture or 42 months from date of installation whichever comes first.)
Component Inspection SimpleDUE: 18-Jun-20181. RE 42 MosADG Uplock Actuator Assy (Squib) - In Service Limit05-10-20A/F24
RE (O/C)Air Driven Gen Auto Deploy Controller
20-Sep-1983Mos
0Hrs
0Ldg
24 A/FUnknownUnknown
RE (O/C)Air Driven Generator (ADG)
23-Feb-2003Mos
9,253.9Hrs
4,606Ldg
24 A/F720848-A0552
RE (O/C)Air Driven Generator Control
19-Apr-2002Mos
8,358.5Hrs
4,045Ldg
24 A/F72831081113
RE (O/C)Air Driven Generator Eject Jack
20-Sep-1983Mos
0Hrs0
0Ldg0
24 A/FNew728431B
UNKNOWN
RE (O/C)Air Driven Turbine Assy
20-Sep-1983Mos
0Hrs
0Ldg
24 A/FUnknownUnknown
RE (O/C)AMPS-500 Battery
21-Nov-2004Mos
10,477.5Hrs
5,321Ldg
No.124 A/F171BS101-1079
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM35/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)AMPS-500 Battery
20-Sep-1983Mos
0Hrs
0Ldg
No.224 A/FUnknownUnknown
RE (O/C)AMPS-500 Battery
20-Sep-1983Mos
0Hrs
0Ldg
No.324 A/FUnknownUnknown
RE (O/C)APU Generator Control Unit (GCU)
20-Sep-1983Mos
0Hrs0
0Ldg0
24 A/FNew720846B
UNKNOWN
RE (O/C)Battery Charger
20-Sep-1983Mos
0Hrs
0Ldg
24 A/FUnknownUnknown
RE (O/C)Fan Cooled (TRU) Converter
20-Sep-1983Mos
0Hrs0
0Ldg0
No.124 A/FNewMS17976-2
UNKNOWN
RE (O/C)Fan Cooled (TRU) Converter
20-Sep-1983Mos
0Hrs0
0Ldg0
No.224 A/FNewMS17976-2
UNKNOWN
RE (O/C)Fan Cooled (TRU) Converter
21-Nov-2002Mos
9,021.9Hrs
4,466Ldg
No.324 A/F28V550Y3573A
RE (O/C)Frequency/Voltage Sensor
20-Sep-1983Mos
0Hrs
0Ldg
24 A/FUnknownUnknown
RE (O/C)Generator Contactor
20-Sep-1983Mos
0Hrs
0Ldg
24 A/FUnknownUnknown
RE (O/C)Generator Control Unit (GCU)
16-Nov-2003Mos
9,901.1Hrs
4,981Ldg
No.124 A/F720846B0884
RE (O/C)Generator Control Unit (GCU)
20-Sep-1983Mos
0Hrs0
0Ldg0
No.224 A/FNew720846B
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM36/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Hand Air Driven Generator Pump
20-Sep-1983Mos
0Hrs
0Ldg
24 A/FUnknownUnknown
RE (O/C)Heat IDG Exchanger
20-Sep-1983Mos
0Hrs0
0Ldg0
No.124 A/FNew24E26-1
UNKNOWN
RE (O/C)Heat IDG Exchanger
20-Sep-1983Mos
0Hrs0
0Ldg0
No.224 A/FNew24E26-1
UNKNOWN
RE (O/C)IDG Generator
15-Sep-2007Mos
11,184.3Hrs
5,748Ldg
No.124 A/F720845E537
RE (O/C)IDG Generator
15-Sep-2007Mos
11,184.3Hrs
5,748Ldg
No.224 A/F720845E0740
RE (O/C)IRS Battery
20-Sep-1983Mos
0Hrs
0Ldg
24 A/FUnknownUnknown
RE (O/C)Main Battery
28-Mar-2014Mos
11,824.5Hrs
6,169Ldg
24 A/F9750W05383060W0020
RE (O/C)Monitor - External Power Relay
20-Sep-1983Mos
0Hrs
0Ldg
24 A/FUnknownUnknown
AWL - Life LimitRE05-10-20 ADG Uplock Actuator Assy (Squib) - In Service Limit
2.2 Years18-Jun-20184218-Dec-2014Mos
11,854.6Hrs
Ldg
24 A/F055046B575 11/2013
(NOTE: NOTE:Life limit is 60 months from date of manufacture or 42 months from date of installation whichever comes first.)
MandatoryRE (-)2009-23-09 Electrical power
22-Mar-2012Mos
11,578.6Hrs
6,004Ldg
24 A/FSB 601-0591Eff: 14-Dec-2009 Complied
With
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Modification – Air-Driven Generator System – R...601-0591A/F24
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM37/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Mandatory ≈27-Nov-2016T2015-25-05 Detect and Correct Broken Support Brackets of the Hydraulic Lines - Perform a One Time Detailed Inspection of the IDG Power Cables
1.3 Years28-Jul-201718Mos
382.67 Hrs≈12,423.87400Hrs
Ldg
24 A/FEff: 28-Jan-2016
Compliance Share DoubleDUE: 12,039.2 Hrs1. T 400 Hrs | 2. RE -Special Check/Rework – Integrated Drive Generator (IDG) and ...601-0625 Rev 1A/F24
Servicing - RecommendedRE24-00-00-301 Battery System - Operational Test (Cycling) of the Thermal Circuit Breakers
6.6 Months (+31
Days)21-Oct-2016-/+11221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
24 A/F
(ZONE: 221, 223, 232, 311) (SOURCE: MPD 3.2)
MRB ≈03-May-2017RE24-20-00-201 AC Generation Functional Test - Complete Generator System
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
24 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE24-21-00-202 Integrated Drive Generator System Differential Pressure Check
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
24 A/F
(SOURCE: TLMC 05-20-15)
Servicing - Recommended ≈18-Sep-2016RE24-21-00-301 Integrated Drive Generator Oil System Replenishing - Replenishing
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
24 A/F
Ref Ch.5:12-11-24 (ZONE: 410, 412) (ACCESS: 412-AB, 422-AB) (SOURCE: MPD 3.2)
MRB ≈13-Jul-2017RE24-21-16-204 IDG Oil-in Filter Assembly Remove, inspect and install new filter element
04-May-2004Mos
684 Hrs (+30)(12,725.2)-/+402,40010,325.2Hrs
Ldg
(PKG 2400 Hour)
24 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈13-Jul-2017RE24-21-21-205 IDG Oil-out Filter Assembly Remove, inspect and install new filter element
04-May-2004Mos
684 Hrs (+30)(12,725.2)-/+402,40010,325.2Hrs
Ldg
(PKG 2400 Hour)
24 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈15-Feb-2019RE24-22-00-206 Auxiliary Generator System GTCP36-100 APU (Pre SB 601-0568 or SB 601-0581) - Roll Rate Monitors Operational Test
08-Aug-2005Mos
1,520 Hrs (+40)9,379-/+402,4006,979Hrs
APUS
24 APU1
(SOURCE: TLMC 05-20-15)
MRB ≈03-Apr-2016RE24-22-00-214 Auxiliary Generator System - APU Generator Adaptor Dry Cavity - Drain Oil
10-Jan-2008Mos
145 Hrs (+40)8,004-/+404007,604Hrs
APUS
24 APU1
(SOURCE: TLMC 05-20-15) (NOTE: • GTCP36-100 APU (P/N 722882B and subsequent) and/or)
MRB ≈15-Feb-2019RE24-22-16-207 APU Generator Adapter Filter Element - Remove, inspect and install new filter element
08-Aug-2005Mos
1,520 Hrs (+40)9,379-/+402,4006,979Hrs
APUS
24 APU1
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM38/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE24-23-00-208 Air Driven Generator System Oil level check- Oil leakage check
15 Days (+30)21-Apr-2016-/+1621-Oct-2015Mos
Hrs
Ldg
24 A/F
(SOURCE: TLMC 05-20-15) (NOTE: The checks in section 5-50-09 of this manual apply immediately after any in-flight deployment of the ADG,
including the annual operational test. The checks aboveare to be carried out 6 months after the last in-flightdeployment)
MRBRE24-23-00-209 Air Driven Generator System Operational Test - ADG
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
24 A/F
(SOURCE: TLMC 05-20-15)
MRBRE24-23-46-210 ADG Auto-Deploy Control Unit Operational Test - ADG Auto-Deploy Control Unit
6.6 Months (+31
Days)(21-Oct-2016)-/+11221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
24 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE24-31-00-211 DC Static Conversion System Functional Test
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
24 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRBRE24-33-00-212 Battery System - Battery Capacity and Electrolyte Check
1 Year23-Apr-201755021-Oct-2015Days
3,959.9 Hrs16,001.14,00012,001.1Hrs
6,291Ldg
24 A/F
Ref.:CMM/PSP 608/608A 24-30-99 or 24-32-05 (SOURCE: TLMC 05-20-15)
MRBRE24-33-00-213 Battery System Functional Test - Main Battery Charger Thermal Sensor
6.6 Months (+31
Days)(21-Oct-2016)-/+11221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
24 A/F
(SOURCE: TLMC 05-20-15)
Servicing - Recommended ≈26-Jun-1985RE24-33-00-302 Battery System - Visual check of battery, paying particular attention to cells, case and vent system for deposits, leakage and corrosion
Mos
OVD100-/+40100Hrs
Ldg
24 A/F
(ZONE: 311) (SOURCE: MPD 3.2)
OptionalRE (-)601-0107 Modification - DC Power Generation - TRU 3 Replacement
Mos
Hrs
Ldg
24 A/F
OptionalT (A/R)601-0107 Rev 1 Modification - DC Power Generation - TRU 3 Replacement
Mos
Hrs
Ldg
24 A/FEff: 02-May-1986
RecommendedRE (-)601-0198 Modification - Air Driven Generator - Manual Release Handle
15-Apr-1988Mos
1,995Hrs
756Ldg
24 A/FEff: 18-Sep-1987 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM39/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0302 Special Check/Rectification - Battery Connector - Wire Connections
28-Mar-1989Mos
2,373Hrs
910Ldg
24 A/FEff: 06-Feb-1989 Complied With
RecommendedRE (-)601-0322 Modification - ADG Restow Pump - Addition of Warning Placard
21-Feb-1991Mos
3,142Hrs
1,250Ldg
24 A/FEff: 21-Sep-1990 Complied With
RecommendedRE (-)601-0356 Modification - Main Battery and AFT Equipment Bay - Venting and Drainage
Mos
Hrs
Ldg
24 A/F
RecommendedRE (-)601-0356 Rev 1 Modification - Main Battery and AFT Equipment Bay - Venting and Drainage
Mos
Hrs
Ldg
24 A/F
RecommendedRE (-)601-0356 Rev 2 Modification - Main Battery and AFT Equipment Bay - Venting and Drainage
Mos
Hrs
Ldg
24 A/F
RecommendedRE (-)601-0356 Rev 3 Modification - Main Battery and AFT Equipment Bay - Venting and Drainage
26-Jan-1995Mos
Hrs
Ldg
24 A/FEff: 31-May-1995 Complied With
RecommendedRE (-)601-0422 Special Check/Rework - Junction Box No. 5 (JB5) - Terminal Block Pin Sizes
30-Sep-1994Mos
4,399Hrs
1,768Ldg
24 A/FEff: 23-Jun-1994 Complied With
RecommendedRE (-)601-0428 Special Check/Rework - Shielded Wire - Wire Insulation
Mos
Hrs
Ldg
24 A/F
RecommendedRE (-)601-0428 Rev 1 Special Check/Rework - Shielded Wire - Wire Insulation
26-Jan-1996Mos
4,785Hrs
1,932Ldg
24 A/FEff: 29-Feb-1996 Complied With
RecommendedRE (-)601-0430 Special Check and Modification - Air Driven Generator - Uplock Assembly Replacement
30-Sep-1994Mos
4,399Hrs
1,768Ldg
24 A/FEff: 25-Apr-1994 Complied With
OptionalT (A/R)601-0445 Modification - Air-Driven Generator (ADG) System - Ecology Bottle Addition
Mos
Hrs
Ldg
24 A/FEff: 30-Apr-1996
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM40/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalT (A/R)601-0480 Modification - Aircraft Air-Driven Generator - Addition of a Time Delay Relay
Mos
Hrs
Ldg
24 A/FEff: 30-Aug-1996
RecommendedRE (-)601-0509 Modification - Battery System - Addition of Protective Resistor
Mos
Hrs
Ldg
24 A/F
RecommendedT (A/R)601-0509 Rev 1 Modification - Battery System - Addition of Protective Resistor
Mos
Hrs
Ldg
24 A/FEff: 15-Sep-2000
OptionalT (A/R)601-0515 Modification - Static Discharger - Installation of Additional Winglet Static Discharger
Mos
Hrs
Ldg
24 A/FEff: 30-Apr-1999
RecommendedRE (-)601-0516 Modification - Battery System - Installation of Battery Charger Output Protection
Mos
Hrs
Ldg
24 A/F
RecommendedT (A/R)601-0516 Rev 1 Modification - Battery System - Installation of Battery Charger Output Protection
Mos
Hrs
Ldg
24 A/FEff: 30-Jun-2000
RecommendedRE (-)601-0521 Modification - Integrated Drive Generator (IDG) System - Protection of IDG Harness Inside Pylon
Mos
Hrs
Ldg
24 A/F
RecommendedT (A/R)601-0534 Modification - Battery System - Conversion of the Main Battery, Part No. 600-59151-11 to a -13
Mos
Hrs
Ldg
24 A/FEff: 28-Sep-2001
RecommendedT (A/R)601-0548 Special Check/Rework - Integrated Drive Generator (IDG) System and Auxiliary AC Generation System - Replacement of Faultily Manufactured IDG and APU Generators
Mos
Hrs
Ldg
24 A/FEff: 31-Jan-2002
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Integrated Drive Generator (IDG) Syst...601-0548 Part AA/F24
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Integrated Drive Generator (IDG) Syst...601-0548 Part BA/F24
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Integrated Drive Generator (IDG) Syst...601-0548 Part CA/F24
RecommendedT (A/R)601-0548 Part A Special Check/Rework - Integrated Drive Generator (IDG) System and Auxiliary AC Generation System - Inspect IDG and APU Generators
Mos
Hrs
Ldg
24 A/FEff: 31-Jan-2002
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM41/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedT (A/R)601-0548 Part B Special Check/Rework - Integrated Drive Generator (IDG) System and Auxiliary AC Generation System - Replacement of Faultily Manufactured IDG
Mos
Hrs
Ldg
24 A/FEff: 31-Jan-2002
RecommendedT (A/R)601-0548 Part C Special Check/Rework - Integrated Drive Generator (IDG) System and Auxiliary AC Generation System - Replacement of Faultily Manufactured APU Generators
Mos
Hrs
Ldg
24 A/FEff: 31-Jan-2002
RecommendedRE (-)601-0591 Special Check/Modification – Air-Driven Generator System – Replacement of Chafing ADG Power Feed Wire
22-Mar-2012Mos
11,578.6Hrs
6,004Ldg
24 A/FEff: 23-Jul-2007 Complied With
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification – Air-Driven Generator System – I...601-0591 Part AA/F24
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification – Air-Driven Generator System – R...601-0591 Part BA/F24
RecommendedT (A/R)601-0591 Part A Special Check/Modification – Air-Driven Generator System – Inspect the ADG Power Feed Wire
Mos
Hrs
Ldg
24 A/FEff: 23-Jul-2007
RecommendedT (A/R)601-0591 Part B Special Check/Modification – Air-Driven Generator System – Replacement of Chafing ADG Power Feed Wire
Mos
Hrs
Ldg
24 A/FEff: 23-Jul-2007
RecommendedRE (-)601-0625 Special Check/Rework – Integrated Drive Generator (IDG) and Hydraulic Systems No.1 and No. 2 – Aft Equipment Bay Right IDG Power Cable and Adjacent Hydraulic
Lines Support Brackets
Mos
Hrs
Ldg
24 A/F
Recommended ≈09-Feb-2016T601-0625 Rev 1 Special Check/Rework – Integrated Drive Generator (IDG) and Hydraulic Systems No.1 and No. 2 – Aft Equipment Bay Right IDG Power Cable and Adjacent Hydraulic
Lines Support Brackets
Mos
OVD[12,039.2]400Hrs
Ldg
24 A/FEff: 13-Jan-2014
RecommendedT (A/R)601-1085 Modification - Engine Standard Configuration - Thrust Reverser and IDG Cable Clamps
Mos
Hrs
Ldg
24 A/FEff: 15-Sep-1994
Mandatory (Appliance AD)RE (-)82-21-04 JET ELECTRONICS AND TECHNOLOGY, INC. All Model PS-835 Series Emergency Power Supply Installations
18-Sep-1985Mos
Hrs
Ldg
24 A/FBY DATE OF MANUFACTUREEff: 21-Oct-1982 Not
Applicable
MandatoryRE (-)83-07-09 Wire Overheating
18-Sep-1985Mos
Hrs
Ldg
24 A/FComplied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM42/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryT (A/R)83-07-09 R1 Wire Overheating
Mos
Hrs
Ldg
24 A/FEff: 12-Nov-1993
Mandatory (Appliance AD)RE (-)87-06-09 MECHANICAL PRODUCTS, INC. Model 4001, 4200, 4310, and 8500 Series Circuit Breakers
29-Apr-1988Mos
Hrs
Ldg
24 A/FEff: 27-Apr-1987 Not Applicable
MandatoryRE (-)91-19-01 Air Driven Generator
18-Mar-1992Mos
Hrs
Ldg
24 A/FEff: 24-Sep-1991 Complied With
MandatoryRE (-)95-10-06 Shaft Pin
05-Nov-1998Mos
Hrs
Ldg
24 A/FSI 601-0430Eff: 12-Jun-1995 Complied
With
AlertRE (-)A601-0028 Special Check/Modification - AC Voltage and Frequency Sensor - Release Time
Mos
Hrs
Ldg
24 A/FEff: 05-Jul-1983
RecommendedT (A/R)A601-0069 Special Check/Rework - External Finish - Lightning Protection
Mos
Hrs
Ldg
24 A/FEff: 30-Jul-1984
AlertRE (-)A601-0097 Special Check/Replacement - IDG and APU - Generators
Mos
Hrs
Ldg
24 A/F
AlertT (A/R)A601-0097 Rev 1 Special Check/Replacement - IDG and APU - Generators
Mos
Hrs
Ldg
24 A/FEff: 22-Apr-1985
AlertRE (-)A601-0174 Special Check/Modification - Nacelle/Pylon Services - Elimination of Possible Chafing
Mos
Hrs
Ldg
24 A/F
AlertRE (-)A601-0174 Rev 1 Special Check/Modification - Nacelle/Pylon Services - Elimination of Possible Chafing
11-Apr-1985Mos
0Hrs
Ldg
24 A/FEff: 23-Dec-1987 Complied With
RecommendedRE (-)A601-0219 Special Check/Modification - Air Driven Generator - Harness Rerouting
11-Apr-1988Mos
Hrs
Ldg
24 A/FEff: 16-Sep-1987 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM43/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AlertRE (-)A601-0370 Special Check/Modification - Air-Driven Generator - Output Harness Chafing
24-Mar-1992Mos
Hrs
Ldg
24 A/FComplied With
AlertT (A/R)A601-0370 Rev 1 Special Check/Modification - Air-Driven Generator - Output Harness Chafing
Mos
Hrs
Ldg
24 A/FEff: 15-Apr-1993
AlertRE (-)A601-0416 Special Operational and Rigging Check - Air-Driven Generator - ADG Uplock Assembly
01-Nov-1993Mos
Hrs
Ldg
24 A/FEff: 01-Nov-1993 Complied With
AlertT (A/R)A601-0547 Special Check/Rework - AC Load Distribution - Replacement of Faultily Manufactured Leach "H" Series Relays
Mos
Hrs
Ldg
24 A/FEff: 28-Sep-2001
Nextdue Share EarliestDUE:1. T 100 Hrs | 2. RE -Special Check/Rework - AC Load Distribution - Replacement of...A601-0547 Part AA/F24
Nextdue Share EarliestDUE:1. T 200 Hrs | 2. RE -Special Check/Rework - AC Load Distribution - Replacement of...A601-0547 Part BA/F24
Nextdue Share EarliestDUE:1. T 300 Hrs | 2. RE -Special Check/Rework - AC Load Distribution - Replacement of...A601-0547 Part CA/F24
Nextdue Share EarliestDUE:1. T 500 Hrs | 2. RE -Special Check/Rework - AC Load Distribution - Replacement of...A601-0547 Part DA/F24
AlertRE (-)A601-0547 Part A Special Check/Rework - AC Load Distribution - Replacement of Faultily Manufactured Leach "H" Series Relays
Mos
Hrs
Ldg
24 A/FEff: 28-Sep-2001
(NOTE: NOTE: There are limited available quantities of “H” series relays,that are required for the incorporation of PART B, C and/or D.For this
reason, the special check in PART A is intended toverify if the suspect relays are installed in the aircraft beforeordering the relays and planning
the incorporation of PART B,C and/or D.)
AlertRE (-)A601-0547 Part B Special Check/Rework - AC Load Distribution - Replacement of Faultily Manufactured Leach "H" Series Relays
Mos
Hrs
Ldg
24 A/FEff: 28-Sep-2001
AlertRE (-)A601-0547 Part C Special Check/Rework - AC Load Distribution - Replacement of Faultily Manufactured Leach "H" Series Relays
Mos
Hrs
Ldg
24 A/FEff: 28-Sep-2001
AlertRE (-)A601-0547 Part D Special Check/Rework - AC Load Distribution - Replacement of Faultily Manufactured Leach "H" Series Relays
Mos
Hrs
Ldg
24 A/FEff: 28-Sep-2001
▼ 25 - EQUIPMENT/FURNISHINGS
RE (O/C)Emergency Locator Transmitter (ELT)
20-Sep-1983Mos
0Hrs
0Ldg
25 A/FUnknownUnknown
Assembly SubDUE: 31-Jul-20171. RE DueEmergency Locator Transmitter (ELT) BatteryBP-1030 / N/AA/F25
Component Inspection SimpleDUE: 17-Apr-20161. RE 12 MosEmergency Locator Transmitter Inspection and Test per FAR 91...FAR 91.207A/F25
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM44/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Life LimitRE (Due)Emergency Locator Transmitter (ELT) Battery
1.3 Years31-Jul-201731-Jul-2015Mos
11,905.8Hrs
6,221Ldg
25 A/F
Expiration Date 31-Jul-2017
BP-1030N/A
RE (O/C)First Aid Kit
20-Sep-1983Mos
0Hrs
0Ldg
25 A/FUnknownUnknown
RE (O/C)Galley Control Panel
20-Sep-1983Mos
0Hrs
0Ldg
25 A/FUnknownUnknown
RE (O/C)Hi Temp Oven
20-Sep-1983Mos
0Hrs
0Ldg
25 A/FUnknownUnknown
RE (O/C)Lap Belt
20-Sep-1983Mos
0Hrs0
0Ldg0
Pilot25 A/FNew1101020-29
UNKNOWN
RE (O/C)Life Raft
06-Sep-2001Mos
7,694.9Hrs
3,648Ldg
Aft25 A/FRAF1210-105T1135HP
RE (O/C)Life Raft
06-Sep-2001Mos
7,694.9Hrs
3,648Ldg
Fwd25 A/FRAF1210-105T1130HP
RE (O/C)Life Vest
Mos
Hrs
Ldg
No.125 A/FUnknownUnknown
Component Inspection SimpleDUE: 16-Feb-20201. RE DueLife Vest - Recertification25-61-CUS-001A/F25
RE (O/C)Life Vest
Mos
Hrs
Ldg
No.1025 A/FUnknownUnknown
Component Inspection SimpleDUE: 16-Feb-20201. RE DueLife Vest - Recertification25-61-CUS-001A/F25
RE (O/C)Life Vest
Mos
Hrs
Ldg
No.1125 A/FUnknownUnknown
Component Inspection SimpleDUE: 16-Feb-20201. RE DueLife Vest - Recertification25-61-CUS-001A/F25
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM45/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Life Vest
Mos
Hrs
Ldg
No.225 A/FUnknownUnknown
Component Inspection SimpleDUE: 16-Feb-20201. RE DueLife Vest - Recertification25-61-CUS-001A/F25
RE (O/C)Life Vest
Mos
Hrs
Ldg
No.325 A/FUnknownUnknown
Component Inspection SimpleDUE: 16-Feb-20201. RE DueLife Vest - Recertification25-61-CUS-001A/F25
RE (O/C)Life Vest
Mos
Hrs
Ldg
No.425 A/FUnknownUnknown
Component Inspection SimpleDUE: 16-Feb-20201. RE DueLife Vest - Recertification25-61-CUS-001A/F25
RE (O/C)Life Vest
Mos
Hrs
Ldg
No.525 A/FUnknownUnknown
Component Inspection SimpleDUE: 16-Feb-20201. RE DueLife Vest - Recertification25-61-CUS-001A/F25
RE (O/C)Life Vest
Mos
Hrs
Ldg
No.625 A/FUnknownUnknown
Component Inspection SimpleDUE: 16-Feb-20201. RE DueLife Vest - Recertification25-61-CUS-001A/F25
RE (O/C)Life Vest
Mos
Hrs
Ldg
No.725 A/FUnknownUnknown
Component Inspection SimpleDUE: 16-Feb-20201. RE DueLife Vest - Recertification25-61-CUS-001A/F25
RE (O/C)Life Vest
Mos
Hrs
Ldg
No.825 A/FUnknownUnknown
Component Inspection SimpleDUE: 16-Feb-20201. RE DueLife Vest - Recertification25-61-CUS-001A/F25
RE (O/C)Life Vest
Mos
Hrs
Ldg
No.925 A/FUnknownUnknown
Component Inspection SimpleDUE: 16-Feb-20201. RE DueLife Vest - Recertification25-61-CUS-001A/F25
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM46/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Life Vest (Crew)
Mos
Hrs
Ldg
Copilot25 A/FUnknownUnknown
Component Inspection SimpleDUE: 16-Feb-20201. RE DueLife Vest (Crew) - Recertification25-61-CUS-001A/F25
RE (O/C)Life Vest (Crew)
Mos
Hrs
Ldg
Pilot25 A/FUnknownUnknown
Component Inspection SimpleDUE: 16-Feb-20201. RE DueLife Vest (Crew) - Recertification25-61-CUS-001A/F25
RE (O/C)Oven Controller
20-Sep-1983Mos
0Hrs
0Ldg
25 A/FUnknownUnknown
RE (O/C)Panel
20-Sep-1983Mos
0Hrs
0Ldg
25 A/FUnknownUnknown
RE (O/C)Reel And Control Harness
20-Sep-1983Mos
0Hrs0
0Ldg0
No.125 A/FNew1S20B25A4X21
UNKNOWN
RE (O/C)Reel And Control Harness
20-Sep-1983Mos
0Hrs0
0Ldg0
No.225 A/FNew1S20B25A4X21
UNKNOWN
RE (O/C)Seat
20-Sep-1983Mos
0Hrs
0Ldg
Copilot25 A/FUnknownUnknown
RE (O/C)Seat
20-Sep-1983Mos
0Hrs
0Ldg
Pilot25 A/FUnknownUnknown
RE (O/C)Seat Belt
20-Sep-1983Mos
0Hrs0
0Ldg0
Copilot25 A/FNew1101020-31
UNKNOWN
Mandatory (Appliance AD)RE (-)2011-21-08 Paragraph (f)(1) SICMA AERO SEAT - Equipment/Furnishings - Passenger Seat Assemblies - do a general visual inspection of the backrest links having P/Ns 90-000200-104-1 and 90-
000200-104-2, in accordance with Part One of Sicma Aero Seat Service Bulletin 90-25-013, Issue 4
13-Jul-2012Mos
11,613.3Hrs
6,021Ldg
25 A/FBY PART NUMBER INSTALLEDEff: 23-Nov-2011 Not
Applicable
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM47/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Mandatory (Appliance AD)RE (-)2011-21-08 Paragraph (f)(4)(5) SICMA AERO SEAT - Equipment/Furnishings - Passenger Seat Assemblies - replace the links, P/Ns 90-000200-104-1 and 90-000200-104-2, with new improved links,
P/Ns 90-100200-104-1 and 90-100200-104-2
13-Jul-2012Mos
11,613.3Hrs
6,021Ldg
25 A/FBY PART NUMBER INSTALLEDEff: 23-Nov-2011 Not
Applicable
Mandatory (Appliance AD)T (A/R)2012-08-07 Equipment/Furnishings - To Detect Cracks in the Central and Lateral Spreaders on Passenger Seats
Mos
Hrs
Ldg
25 A/FEff: 09-May-2012
Mandatory (Appliance AD)T (A/R)2014-20-11 Zodiac Seats France - Equipment/Furnishings - Seats
Mos
Hrs
Ldg
25 A/FEff: 22-Oct-2014
MRB ≈03-May-2017RE25-11-00-201 Crew Seats/Safety Harness and Inertial Reel Visual Check, paying particular attention to the seat tracks, trackstops and adjustment cables
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
25 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
RE (Due)25-61-CUS-001 Life Vest - Recertification
3.9 Years16-Feb-202016-Feb-2010Mos
Hrs
Ldg
No.125 A/F
Expiration Date 16-Feb-2020
UnknownUnknown
RE (Due)25-61-CUS-001 Life Vest - Recertification
3.9 Years16-Feb-202016-Feb-2010Mos
Hrs
Ldg
No.1025 A/F
Expiration Date 16-Feb-2020
UnknownUnknown
RE (Due)25-61-CUS-001 Life Vest - Recertification
3.9 Years16-Feb-202016-Feb-2010Mos
Hrs
Ldg
No.1125 A/F
Expiration Date 16-Feb-2020
UnknownUnknown
RE (Due)25-61-CUS-001 Life Vest - Recertification
3.9 Years16-Feb-202016-Feb-2010Mos
Hrs
Ldg
No.225 A/F
Expiration Date 16-Feb-2020
UnknownUnknown
RE (Due)25-61-CUS-001 Life Vest - Recertification
3.9 Years16-Feb-202016-Feb-2010Mos
Hrs
Ldg
No.325 A/F
Expiration Date 16-Feb-2020
UnknownUnknown
RE (Due)25-61-CUS-001 Life Vest - Recertification
3.9 Years16-Feb-202016-Feb-2010Mos
Hrs
Ldg
No.425 A/F
Expiration Date 16-Feb-2020
UnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM48/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (Due)25-61-CUS-001 Life Vest - Recertification
3.9 Years16-Feb-202016-Feb-2010Mos
Hrs
Ldg
No.525 A/F
Expiration Date 16-Feb-2020
UnknownUnknown
RE (Due)25-61-CUS-001 Life Vest - Recertification
3.9 Years16-Feb-202016-Feb-2010Mos
Hrs
Ldg
No.625 A/F
Expiration Date 16-Feb-2020
UnknownUnknown
RE (Due)25-61-CUS-001 Life Vest - Recertification
3.9 Years16-Feb-202016-Feb-2010Mos
Hrs
Ldg
No.725 A/F
Expiration Date 16-Feb-2020
UnknownUnknown
RE (Due)25-61-CUS-001 Life Vest - Recertification
3.9 Years16-Feb-202016-Feb-2010Mos
Hrs
Ldg
No.825 A/F
Expiration Date 16-Feb-2020
UnknownUnknown
RE (Due)25-61-CUS-001 Life Vest - Recertification
3.9 Years16-Feb-202016-Feb-2010Mos
Hrs
Ldg
No.925 A/F
Expiration Date 16-Feb-2020
UnknownUnknown
RE (Due)25-61-CUS-001 Life Vest (Crew) - Recertification
3.9 Years16-Feb-202016-Feb-2010Mos
Hrs
Ldg
Copilot25 A/F
Expiration Date 16-Feb-2020
UnknownUnknown
RE (Due)25-61-CUS-001 Life Vest (Crew) - Recertification
3.9 Years16-Feb-202016-Feb-2010Mos
Hrs
Ldg
Pilot25 A/F
Expiration Date 16-Feb-2020
UnknownUnknown
ICARE25-CUS-011 Aircraft First Aid Kit - Inspection
44 Days20-May-20161220-May-2015Mos
Hrs
Ldg
25 A/F
(NOTE: 12 Month Inspection Per Manufacture's Instructions)
OptionalT (A/R)601-0071 Modification - Cockpit Headlining - Drainage Provision
Mos
Hrs
Ldg
25 A/FEff: 10-Jul-1985
OptionalT (A/R)601-0168 Modification - Pilots Eye Locator - Improved Mounting
Mos
Hrs
Ldg
25 A/FEff: 26-May-1987
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM49/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0191 Modification - Aft Distribution Box (JB4) - Vent Screen Cover
23-Mar-1992Mos
Hrs
Ldg
25 A/FComplied With
RecommendedT (A/R)601-0191 Rev 1 Modification - Aft Distribution Box (JB4) - Vent Screen Cover
Mos
Hrs
Ldg
25 A/FEff: 20-Jun-1988
RecommendedT (A/R)601-0567 Modification - Flight Compartment - Replacement of Camloc Fasteners on Rudder Pedal Protection Panels
Mos
Hrs
Ldg
25 A/FEff: 29-Oct-2004
Mandatory ≈23-Dec-2016RE74-08-09 R3 Equipment/furnishings - Equipment/furnishings - improper disposal of smoking materials in lavatory waste receptacles
05-Jun-2009Mos
417.4 Hrs12,458.61,00011,458.6Hrs
Ldg
25 A/FEff: 28-Mar-2012
Mandatory (Appliance AD)RE (-)83-11-03 Attendant Restraint System Rotary Buckle Assemblies
18-Sep-1985Mos
Hrs
Ldg
25 A/FEQUIPMENT NOT INSTALLEDEff: 18-Jul-1983 Not
Applicable
Mandatory (Appliance AD)RE (-)87-17-06 Occupant Restraint System Assemblies
29-Apr-1988Mos
1,995Hrs
756Ldg
25 A/FEff: 22-Sep-1987 Not Applicable
FAR91, FAR 91REFAR 91.207 Emergency Locator Transmitter Inspection and Test per FAR 91.207 (d)
11 Days17-Apr-20161217-Apr-2015Mos
Hrs
Ldg
25 A/FUnknownUnknown
▼ 26 - FIRE PROTECTION
RE (O/C)Auxiliary Power Unit Firex Container
24-Oct-2011Mos
11,543.4Hrs
5,985Ldg
26 A/F89788-299058EK
Component Inspection SimpleDUE: 21-Oct-20161. RE 12 MosAuxiliary Power Unit Firex Container - Check APU Firex Conta...26-21-11-206A/F26
Component Inspection Tso To
TsiDUE: 24-Oct-20161. RE 60 MosAuxiliary Power Unit Firex Container - Hydrostatic Test26-21-11-207A/F26
RE (O/C)Fire Detection Control
20-Sep-1983Mos
0Hrs0
0Ldg0
No.126 A/FNew377-02836
UNKNOWN
RE (O/C)Fire Detection Control
20-Sep-1983Mos
0Hrs0
0Ldg0
No.226 A/FNew377-02836
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM50/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Fire Detection Control
20-Sep-1983Mos
0Hrs
0Ldg
No.326 A/FUnknownUnknown
RE (O/C)Fire Detection Control
20-Sep-1983Mos
0Hrs
0Ldg
No.426 A/FUnknownUnknown
RE (O/C)Fire Detection Control
20-Sep-1983Mos
0Hrs
0Ldg
No.526 A/FUnknownUnknown
RE (O/C)Fire Detection Control
20-Sep-1983Mos
0Hrs
0Ldg
No.626 A/FUnknownUnknown
RE (O/C)Fire Sensing Element
20-Sep-1983Mos
0Hrs0
0Ldg0
No.126 A/FNew244-21086
UNKNOWN
RE (O/C)Fire Sensing Element
20-Sep-1983Mos
0Hrs
0Ldg
No.226 A/FUnknownUnknown
RE (O/C)Fire Sensing Element
20-Sep-1983Mos
0Hrs
0Ldg
No.326 A/FUnknownUnknown
RE (O/C)Fire Sensing Element
20-Sep-1983Mos
0Hrs
0Ldg
No.426 A/FUnknownUnknown
RE (O/C)Fire Sensing Element
20-Sep-1983Mos
0Hrs
0Ldg
No.526 A/FUnknownUnknown
RE (O/C)Fire Sensing Element
20-Sep-1983Mos
0Hrs
0Ldg
No.626 A/FUnknownUnknown
RE (O/C)Fire Sensing Element
20-Sep-1983Mos
0Hrs
0Ldg
No.726 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM51/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Fire Sensing Element
20-Sep-1983Mos
0Hrs
0Ldg
No.826 A/FUnknownUnknown
RE (O/C)Fire Sensing Element
20-Sep-1983Mos
0Hrs
0Ldg
No.926 A/FUnknownUnknown
RE (O/C)Fire Sensing Mlg Element
20-Sep-1983Mos
0Hrs
0Ldg
No.126 A/FUnknownUnknown
RE (O/C)Fire Sensing Mlg Element
20-Sep-1983Mos
0Hrs
0Ldg
No.226 A/FUnknownUnknown
AWL - Life LimitRE (O/C)Portable Fire Extinguisher
08-Jul-2011Mos
11,523.8Hrs
Ldg
Aft - Cabin26 A/FC352TSW-790480
(SOURCE: TLMC 05-10-20)
Component Inspection SimpleDUE: 21-Oct-20161. RE 12 MosPortable Fire Extinguisher - Check weight26-25-00-213A/F26
Component Inspection Tso To
TsiDUE: 08-Jul-20231. RE 144 MosPortable Fire Extinguisher - Hydrostatic Test26-25-00-214A/F26
AWL - Life LimitRE (O/C)Portable Fire Extinguisher
26-Jan-2011Mos
11,460.7Hrs
Ldg
Cockpit26 A/FC352TSUnknown
(SOURCE: TLMC 05-10-20)
Component Inspection SimpleDUE: 21-Oct-20161. RE 12 MosPortable Fire Extinguisher - Check weight26-25-00-213A/F26
Component Inspection Tso To
TsiDUE: 26-Jan-20231. RE 144 MosPortable Fire Extinguisher - Hydrostatic Test26-25-00-214A/F26
AWL - Life LimitRE (O/C)Portable Fire Extinguisher
20-Sep-1983Mos
0Hrs
0Ldg
Fwd - Cabin26 A/FUnknownUnknown
(SOURCE: TLMC 05-10-20)
AWL - Life LimitRE (O/C)Portable Fire Extinguisher
20-Sep-1983Mos
0Hrs
0Ldg
Fwd - Closet26 A/FUnknownUnknown
(SOURCE: TLMC 05-10-20)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM52/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Power Plant Firex Container
24-Oct-2011Mos
11,543.4Hrs
5,985Ldg
Left26 A/F8990745765U
Component Inspection SimpleDUE: 21-Oct-20161. RE 12 MosPower Plant Firex Container - Check Power Plant Firex Contai...26-23-11-210A/F26
Component Inspection Tso To
TsiDUE: 24-Oct-20161. RE 60 MosPower Plant Firex Containers - Hydrostatic Test26-23-11-211A/F26
RE (O/C)Power Plant Firex Container
24-Oct-2011Mos
11,543.4Hrs
5,985Ldg
Right26 A/F89907430292EL
Component Inspection SimpleDUE: 21-Oct-20161. RE 12 MosPower Plant Firex Container - Check Power Plant Firex Contai...26-23-11-210A/F26
Component Inspection Tso To
TsiDUE: 24-Oct-20161. RE 60 MosPower Plant Firex Containers - Hydrostatic Test26-23-11-211A/F26
Mandatory (Appliance AD)RE (-)2001-22-14 Overland Aviation Services - Fire Extinguishing System Bottle Cartridges
11-Jan-2002Mos
7,973.5Hrs
3,823Ldg
26 A/FSB 22-09-97Eff: 10-Dec-2001 Complied
With
MRB ≈18-Sep-2016RE26-10-11-201 Power Plant and APU Fire Sensing Cables Visual Check all visible portions of the firewires, particularly around mountings and runs through bulkheads
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
26 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE26-10-21-203 Main Landing Gear Bay Overheat Detection System Functional Test
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
26 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE26-21-00-204 Auxiliary Power Unit (APU) Fire Extinguishing Functional Test APU Fire Extinguishing System
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
26 A/F
(SOURCE: TLMC 05-20-15)
MRBRE26-21-11-206 Auxiliary Power Unit Firex Container - Check APU Firex Container
6.6 Months (+31
Days)21-Oct-2016-/+11221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
26 A/F
89788-299058EK
(SOURCE: TLMC 05-20-15)
MRBRE26-21-11-207 Auxiliary Power Unit Firex Container - Hydrostatic Test
6.7 Months (+31
Days)24-Oct-2016-/+16024-Oct-2011Mos
Hrs
Ldg
26 A/F
Hydrostatic Tested Date 24-Oct-2011
89788-299058EK
Ref.:CMM/PSP 608/608A 26-21-28, Ref.:Section 5-20-05 Para 10 Program Note B (SOURCE: TLMC 05-20-15)
MRBRE26-21-21-205 Auxiliary Power Unit Firex Discharge Line Visual Check
6.6 Months (+31
Days)(21-Oct-2016)-/+11221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
26 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM53/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE (N/A)26-23-00-208 Power Plant Fire Extinguishing (Pre SB 601-0171) Functional Test Power Plant Fire Extinguishing System
Mos
Hrs
Ldg
26 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈29-Feb-2016RE26-23-00-209 Power Plant Fire Extinguishing (Post SB 601-0171) Functional Test Power Plant Fire Extinguishing System
05-Apr-2013Mos
26.3 Hrs (+40)12,067.5-/+4030011,767.5Hrs
Ldg
26 A/F
(SOURCE: TLMC 05-20-15)
MRBRE26-23-11-210 Power Plant Firex Container - Check Power Plant Firex Container
6.6 Months (+31
Days)21-Oct-2016-/+11221-Oct-2015Mos
Hrs
Ldg
Left
(PKG 12 Month)
26 A/F
8990745765U
(SOURCE: TLMC 05-20-15)
MRBRE26-23-11-210 Power Plant Firex Container - Check Power Plant Firex Container
6.6 Months (+31
Days)21-Oct-2016-/+11221-Oct-2015Mos
Hrs
Ldg
Right
(PKG 12 Month)
26 A/F
89907430292EL
(SOURCE: TLMC 05-20-15)
MRBRE26-23-11-211 Power Plant Firex Containers - Hydrostatic Test
6.7 Months (+31
Days)24-Oct-2016-/+16024-Oct-2011Mos
Hrs
Ldg
Left26 A/F
Hydrostatic Tested Date 24-Oct-2011
8990745765U
Ref.:CMM/PSP 608/608A 26-20-81, Ref.:Section 5-20-05 Para 10 Program Note B (SOURCE: TLMC 05-20-15)
MRBRE26-23-11-211 Power Plant Firex Containers - Hydrostatic Test
6.7 Months (+31
Days)24-Oct-2016-/+16024-Oct-2011Mos
Hrs
Ldg
Right26 A/F
Hydrostatic Tested Date 24-Oct-2011
89907430292EL
Ref.:CMM/PSP 608/608A 26-20-81, Ref.:Section 5-20-05 Para 10 Program Note B (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE26-23-21-215 Power Plant Firex Discharge Lines Visual Check, paying particular attention for any chafing with the PRSOV sensing line
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
26 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE26-25-00-212 Portable Fire Extinguisher - Check pressure
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
26 A/F
(SOURCE: TLMC 05-20-15)
MRBRE26-25-00-213 Portable Fire Extinguisher - Check weight
6.6 Months (+31
Days)21-Oct-2016-/+11221-Oct-2015Mos
Hrs
Ldg
Aft - Cabin
(PKG 12 Month)
26 A/F
Weighted Date 21-Oct-2015
C352TSW-790480
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM54/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE26-25-00-213 Portable Fire Extinguisher - Check weight
6.6 Months (+31
Days)21-Oct-2016-/+11221-Oct-2015Mos
Hrs
Ldg
Cockpit
(PKG 12 Month)
26 A/F
Weighted Date 21-Oct-2015
C352TSUnknown
(SOURCE: TLMC 05-20-15)
MRBRE26-25-00-214 Portable Fire Extinguisher - Hydrostatic Test
7.3 Years (+31 Days)08-Jul-2023-/+114408-Jul-2011Mos
Hrs
Ldg
Aft - Cabin26 A/F
Hydrostatic Tested Date 08-Jul-2011
C352TSW-790480
Ref.:CMM/PSP 608/608A 26-100-9750, Ref.:Section 5-20-05 Para 10 Program Note B (SOURCE: TLMC 05-20-15)
MRBRE26-25-00-214 Portable Fire Extinguisher - Hydrostatic Test
6.8 Years (+31 Days)26-Jan-2023-/+114426-Jan-2011Mos
Hrs
Ldg
Cockpit26 A/F
Hydrostatic Tested Date 26-Jan-2011
C352TSUnknown
Ref.:CMM/PSP 608/608A 26-100-9750, Ref.:Section 5-20-05 Para 10 Program Note B (SOURCE: TLMC 05-20-15)
VendorRE26-NFPA-10 Portable Fire Extinguisher • 6 Years Inspection
1.3 Years08-Jul-20177208-Jul-2011Mos
Hrs
Ldg
26 A/FInspected Date 08-Jul-2011
VendorRE26-NFPA-10 Portable Fire Extinguisher • 6 Years Inspection
9.8 Months26-Jan-20177226-Jan-2011Mos
Hrs
Ldg
26 A/FInspected Date 26-Jan-2011
RecommendedRE (-)601-0123 Modification - Power Plant - Relocation of FIREX Bottle
17-Sep-1985Mos
607Hrs
262Ldg
26 A/FEff: 25-Apr-1985 Complied With
RecommendedRE (-)601-0171 Modification - Engine Fire Push and Master Caution Reset Switches - Replacement
23-Mar-1992Mos
Hrs
Ldg
26 A/FEff: 06-Jan-1987 Complied With
OptionalT (A/R)601-0315 Modification - APU Firex Container - Support Bracket
Mos
Hrs
Ldg
26 A/FEff: 08-Mar-1991
RecommendedRE (-)601-0321 Special Check/Modification - Power Plant Fire Extinguishing System - Two-Way Check Tee
25-Mar-1991Mos
3,182Hrs
1,266Ldg
26 A/FEff: 21-Jan-1991 Complied With
RecommendedRE (-)601-0574 Modification/Inspection - Fire Detection System - Improved Harness Routing for Jet Pipe Sensing Element
Mos
Hrs
Ldg
26 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM55/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedT (A/R)601-0589 Special Check/Modification - Fire Detection - Resistance Test and Replacement of Combustion Zone Sensing Elements Where Required
Mos
Hrs
Ldg
26 A/FEff: 26-Feb-2007
Nextdue Share EarliestDUE:1. T 400 Hrs | 2. RE -Special Check/Modification - Fire Detection - Resistance Tes...601-0589 Part AA/F26
Nextdue Share EarliestDUE:1. T 800 Hrs | 2. RE -Special Check/Modification - Fire Detection - Resistance Tes...601-0589 Part BA/F26
RecommendedRE (-)601-0589 Part A Special Check/Modification - Fire Detection - Resistance Test and Replacement of Combustion Zone Sensing Elements Where Required
Mos
Hrs
Ldg
26 A/FEff: 26-Feb-2007
RecommendedRE (-)601-0589 Part B Special Check/Modification - Fire Detection - Resistance Test and Replacement of Combustion Zone Sensing Elements Where Required
Mos
Hrs
Ldg
26 A/FEff: 26-Feb-2007
OptionalRE (-)601-1050 Modification - Engine Fire Sensing Cable - Support Bracket
Mos
Hrs
Ldg
26 A/F
OptionalT (A/R)601-1050 Rev 1 Modification - Engine Fire Sensing Cable - Support Bracket
Mos
Hrs
Ldg
26 A/FEff: 12-Jan-1987
RecommendedRE (-)601-1059 Modification - Firex Line Assembly - Clearance
02-May-1988Mos
1,995Hrs
756Ldg
26 A/FEff: 12-Oct-1987 Complied With
RecommendedRE (-)601-1068 Modification - Exhaust Nozzle Fairing - Fire Sensing Cable
Mos
Hrs
Ldg
26 A/F
RecommendedRE (-)601-1068 Rev 1 Modification - Exhaust Nozzle Fairing - Fire Sensing Cable
23-Mar-1992Mos
3,584Hrs
1,446Ldg
26 A/FEff: 06-Dec-1990 Complied With
MandatoryRE (-)92-13-09 Engine Fire Extinguishing System
24-Dec-2002Mos
9,122.1Hrs
4,527Ldg
26 A/FSB A601-0309Eff: 23-Jul-1992 Complied
With
Compliance Share DoubleDUE:1. T 50 Hrs | 2. RE -Special Check/Modification - Engine Fire Protection - Sensor...A601-0309A/F26
AlertRE (-)A601-0309 Special Check/Modification - Engine Fire Protection - Sensor System Wiring and Fire Extinguishing Bottle Squib Wiring
Mos
Hrs
Ldg
26 A/FEff: 08-Sep-1989
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM56/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AlertT (A/R)A601-1087 Modification - Fire Protection - Harness Re-Routing
Mos
Hrs
Ldg
26 A/FEff: 25-Apr-1994
▼ 27 - FLIGHT CONTROLS
RE (O/C)(Inner Flap) Actuator
20-Sep-1983Mos
0Hrs
0Ldg
Left Inboard27 A/FUnknownUnknown
RE (O/C)(Inner Flap) Actuator
20-Sep-1983Mos
0Hrs
0Ldg
Left Outboard27 A/FUnknownUnknown
RE (O/C)(Inner Flap) Actuator
20-Sep-1983Mos
0Hrs
0Ldg
Right Inboard27 A/FUnknownUnknown
RE (O/C)(Inner Flap) Actuator
20-Sep-1983Mos
0Hrs
0Ldg
Right Outboard27 A/FUnknownUnknown
RE (O/C)Aileron Cable Tension Regulator
20-Sep-1983Mos
0Hrs
0Ldg
Left27 A/FUnknownUnknown
RE (O/C)Aileron Cable Tension Regulator
20-Sep-1983Mos
0Hrs
0Ldg
Right27 A/FUnknownUnknown
RE (O/C)Aileron Flutter Damper
08-Aug-2003Mos
9,585.6Hrs
4,797Ldg
Left27 A/F600-75142-3HA13712
Component Inspection SimpleDUE:1. RE 600 HrsAileron Flutter Dampers - Check aileron flutter damper / Che...27-13-21-205A/F27
Component Inspection SimpleDUE:1. RE 4800 HrsAileron Flutter Dampers - Remove, carry out “Testing and Fau...27-13-21-206A/F27
RE (O/C)Aileron Flutter Damper
08-Aug-2003Mos
9,585.6Hrs
4,797Ldg
Right27 A/F600-75142-9HA13913
Component Inspection SimpleDUE:1. RE 600 HrsAileron Flutter Dampers - Check aileron flutter damper / Che...27-13-21-205A/F27
Component Inspection SimpleDUE:1. RE 4800 HrsAileron Flutter Dampers - Remove, carry out “Testing and Fau...27-13-21-206A/F27
RE (O/C)Aileron Trim (Roll) Actuator
20-Sep-1983Mos
0Hrs
0Ldg
27 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM57/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Altitude Transducer
20-Sep-1983Mos
0Hrs0
0Ldg0
Left27 A/FNew7001648-902
UNKNOWN
RE (O/C)Altitude Transducer
17-Sep-2001Mos
7,697.4Hrs
3,650Ldg
Right27 A/F7001648-90295081379
RE (O/C)Angle-of-Attack (AOA) Transducer
20-Sep-1983Mos
0Hrs
0Ldg
Left27 A/FUnknownUnknown
Component Inspection SimpleDUE: 12,055.3 Hrs1. RE 300 HrsAngle-of-Attack Vane Transducer Linearity - Functional Test ...27-39-11-101 *A/F27
Component Inspection Tso To
TsiDUE:1. RE N/AAngle-of-Attack Vane Transducer, Restoration - Overhaul of t...27-39-11-102 *A/F27
RE (O/C)Angle-of-Attack (AOA) Transducer
27-Feb-2005Mos
10,601.2Hrs
5,392Ldg
Right27 A/F600-59154-1247-098
Component Inspection SimpleDUE: 12,055.3 Hrs1. RE 300 HrsAngle-of-Attack Vane Transducer Linearity - Functional Test ...27-39-11-101 *A/F27
Component Inspection Tso To
TsiDUE:1. RE N/AAngle-of-Attack Vane Transducer, Restoration - Overhaul of t...27-39-11-102 *A/F27
RE (O/C)Control Column Wheel
20-Sep-1983Mos
0Hrs0
0Ldg0
Copilot27 A/FNew720-5716
UNKNOWN
RE (O/C)Control Column Wheel
20-Sep-1983Mos
0Hrs0
0Ldg0
Pilot27 A/FNew720-5715
UNKNOWN
RE (O/C)Control Surface Position Indicator
25-Jul-2008Mos
11,432Hrs
5,881Ldg
27 A/F600-50930-5147
RE (O/C)Elevator Flutter Damper
08-Aug-2003Mos
9,585.6Hrs
4,797Ldg
Left Inboard27 A/F1018100-7HA13933
Component Inspection SimpleDUE:1. RE 600 HrsElevator Flutter Dampers - Check elevator flutter damper27-33-11-216A/F27
Component Inspection SimpleDUE:1. RE 4800 HrsElevator Flutter Dampers - Remove, carry out “Testing and Fa...27-33-11-217A/F27
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM58/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Elevator Flutter Damper
08-Aug-2003Mos
9,585.6Hrs
4,797Ldg
Left Outboard27 A/F1018100-7HA13911
Component Inspection SimpleDUE:1. RE 600 HrsElevator Flutter Dampers - Check elevator flutter damper27-33-11-216A/F27
Component Inspection SimpleDUE:1. RE 4800 HrsElevator Flutter Dampers - Remove, carry out “Testing and Fa...27-33-11-217A/F27
RE (O/C)Elevator Flutter Damper
08-Aug-2003Mos
9,585.6Hrs
4,797Ldg
Right Inboard27 A/F1018100-7HA13910
Component Inspection SimpleDUE:1. RE 600 HrsElevator Flutter Dampers - Check elevator flutter damper27-33-11-216A/F27
Component Inspection SimpleDUE:1. RE 4800 HrsElevator Flutter Dampers - Remove, carry out “Testing and Fa...27-33-11-217A/F27
RE (O/C)Elevator Flutter Damper
08-Aug-2003Mos
9,585.6Hrs
4,797Ldg
Right Outboard27 A/F1018100-7HA13919
Component Inspection SimpleDUE:1. RE 600 HrsElevator Flutter Dampers - Check elevator flutter damper27-33-11-216A/F27
Component Inspection SimpleDUE:1. RE 4800 HrsElevator Flutter Dampers - Remove, carry out “Testing and Fa...27-33-11-217A/F27
RE (O/C)Elevator Load Limiter
20-Sep-1983Mos
0Hrs
0Ldg
Left27 A/FUnknownUnknown
RE (O/C)Elevator Load Limiter
20-Sep-1983Mos
0Hrs
0Ldg
Right27 A/FUnknownUnknown
RE (O/C)Flap Brake Detector Unit
20-Sep-1983Mos
0Hrs
0Ldg
Left27 A/FUnknownUnknown
RE (O/C)Flap Brake Detector Unit
01-Dec-2002Mos
9,037.1Hrs
4,479Ldg
Right27 A/F2022280-6102-469M
RE (O/C)Flap Control Unit
28-Nov-2002Mos
9,032.5Hrs
4,475Ldg
27 A/F8-341-02125-339
RE (O/C)Flap Control Unit
20-Sep-1983Mos
0Hrs
0Ldg
27 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM59/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Flap Drive Potentiometer (PDU)
20-Sep-1983Mos
0Hrs
0Ldg
27 A/FUnknownUnknown
RE (O/C)Flap Position Indicator
04-Mar-2003Mos
9,274.7Hrs
4,617Ldg
27 A/F600-59179-186110177
RE (O/C)Flap Position Transmitter
20-Sep-1983Mos
0Hrs0
0Ldg0
Left27 A/FNew600-93030-1
N/A
RE (O/C)Flap Position Transmitter
20-Sep-1983Mos
0Hrs0
0Ldg0
Right27 A/FNew600-93030-3
N/A
RE (O/C)Flap System Control Lever
20-Sep-1983Mos
0Hrs
0Ldg
27 A/FUnknownUnknown
RE (O/C)Flexible Drive Shaft
20-Sep-1983Mos
0Hrs
0Ldg
No.127 A/FUnknownUnknown
RE (O/C)Flexible Drive Shaft
20-Sep-1983Mos
0Hrs
0Ldg
No.1027 A/FUnknownUnknown
RE (O/C)Flexible Drive Shaft
20-Sep-1983Mos
0Hrs
0Ldg
No.227 A/FUnknownUnknown
RE (O/C)Flexible Drive Shaft
20-Sep-1983Mos
0Hrs
0Ldg
No.327 A/FUnknownUnknown
RE (O/C)Flexible Drive Shaft
20-Sep-1983Mos
0Hrs
0Ldg
No.427 A/FUnknownUnknown
RE (O/C)Flexible Drive Shaft
20-Sep-1983Mos
0Hrs
0Ldg
No.527 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM60/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Flexible Drive Shaft
20-Sep-1983Mos
0Hrs
0Ldg
No.627 A/FUnknownUnknown
RE (O/C)Flexible Drive Shaft
20-Sep-1983Mos
0Hrs
0Ldg
No.727 A/FUnknownUnknown
RE (O/C)Flexible Drive Shaft
20-Sep-1983Mos
0Hrs
0Ldg
No.827 A/FUnknownUnknown
RE (O/C)Flexible Drive Shaft
20-Sep-1983Mos
0Hrs
0Ldg
No.927 A/FUnknownUnknown
RE (O/C)Flight Control Monitor Unit
20-Sep-1983Mos
0Hrs
0Ldg
27 A/FUnknownUnknown
RE (O/C)Flight Spoiler Load Limiter
20-Sep-1983Mos
0Hrs
0Ldg
Left27 A/FUnknownUnknown
RE (O/C)Flight Spoiler Load Limiter
20-Sep-1983Mos
0Hrs
0Ldg
Right27 A/FUnknownUnknown
RE (O/C)Flight Spoiler Proximity Switch
20-Sep-1983Mos
0Hrs
0Ldg
Right27 A/FUnknownUnknown
AWL - Life Limit ≈02-Nov-2016REGround Spoiler PCU
10-Nov-2000Mos
7,089.9Hrs
262 Ldg6,5883,3003,288Ldg0
Left27 A/F600-75106-3307
AWL - Life Limit ≈02-Nov-2016REGround Spoiler PCU
10-Nov-2000Mos
7,089.9Hrs
262 Ldg6,5883,3003,288Ldg0
Right27 A/F600-75106-3308
RE (O/C)Ground Spoiler Select Manifold
20-Sep-1983Mos
0Hrs0
0Ldg0
27 A/FNew62130-7
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM61/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Horizontal Stab Trim Control Unit
28-Mar-2014Mos
11,824.5Hrs
6,169Ldg
27 A/F56417-005370
AWL - Life Limit ≈04-Jun-2137REHSTA Inst Pin, Lower Attach
20-Sep-1983Mos
0Hrs0
43,674 Ldg50,00050,0000Ldg0
Left27 A/FNewUNKNOWN
UNKNOWN
AWL - Life Limit ≈04-Jun-2137REHSTA Inst Pin, Lower Attach
20-Sep-1983Mos
0Hrs0
43,674 Ldg50,00050,0000Ldg0
Right27 A/FNewUNKNOWN
UNKNOWN
AWL - Life Limit ≈04-Jun-2137REHSTA Inst Pin, Upper Attach
20-Sep-1983Mos
0Hrs0
43,674 Ldg50,00050,0000Ldg0
Left27 A/FNew600-93033-1
UNKNOWN
AWL - Life Limit ≈04-Jun-2137REHSTA Inst Pin, Upper Attach
20-Sep-1983Mos
0Hrs0
43,674 Ldg50,00050,0000Ldg0
Right27 A/FNew600-93033-1
UNKNOWN
RE (O/C)Lateral Stall Warning Accelerometer
20-Sep-1983Mos
0Hrs0
0Ldg0
Left27 A/FNew4383A0-5P10
UNKNOWN
RE (O/C)Lateral Stall Warning Accelerometer
20-Sep-1983Mos
0Hrs0
0Ldg0
Right27 A/FNew4383A0-5P10
UNKNOWN
RE (O/C)Load Limiter
20-Sep-1983Mos
0Hrs
0Ldg
27 A/FUnknownUnknown
RE (O/C)Outboard Flap Actuator
12-May-2010Mos
Hrs
5,910Ldg
Left Inboard27 A/F600-93000-82UNKNOWN
Component Inspection Tso To
TsiDUE: 7,910 Ldg1. RE 2000 LdgOutboard Flap Actuator - Restoration of the Outboard Flap Ac...27-50-16-101 *A/F27
RE (O/C)Outboard Flap Actuator
12-May-2010Mos
Hrs
5,910Ldg
Left Outboard27 A/F600-93000-93UNKNOWN
Component Inspection Tso To
TsiDUE: 7,910 Ldg1. RE 2000 LdgOutboard Flap Actuator - Restoration of the Outboard Flap Ac...27-50-16-101 *A/F27
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM62/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Outboard Flap Actuator
12-May-2010Mos
Hrs
5,910Ldg
Right Inboard27 A/F600-93000-82UNKNOWN
Component Inspection Tso To
TsiDUE: 7,910 Ldg1. RE 2000 LdgOutboard Flap Actuator - Restoration of the Outboard Flap Ac...27-50-16-101 *A/F27
RE (O/C)Outboard Flap Actuator
12-May-2010Mos
Hrs
5,910Ldg
Right Outboard27 A/F600-93000-93UNKNOWN
Component Inspection Tso To
TsiDUE: 7,910 Ldg1. RE 2000 LdgOutboard Flap Actuator - Restoration of the Outboard Flap Ac...27-50-16-101 *A/F27
RE (O/C)Pitch Feel Simulator
20-Sep-1983Mos
0Hrs
0Ldg
Left27 A/FUnknownUnknown
Component Inspection SimpleDUE: 12,397.5 Hrs1. RE 1500 HrsPitch Feel Simulator - Functional Test of the Pitch Feel Sim...27-31-11-101A/F27
RE (O/C)Pitch Feel Simulator
20-Sep-1983Mos
0Hrs
0Ldg
Right27 A/FUnknownUnknown
Component Inspection SimpleDUE: 12,397.5 Hrs1. RE 1500 HrsPitch Feel Simulator - Functional Test of the Pitch Feel Sim...27-31-11-101A/F27
AWL - Life Limit ≈19-Dec-2031REPitch Trim Actuator
11-Mar-2000Mos
7,611.7 Hrs19,652.913,2006,452.9Hrs0
2,899Ldg0
27 A/FNew600-92301-65
346E
Component Inspection Tso To
TsiDUE: 13,052.9 Hrs1. T 6600 Hrs | 2. RE 6600 HrsPitch Trim Actuator - Overhaul27-40-16-101 *A/F27
RE (O/C)Position Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.127 A/FUnknownUnknown
RE (O/C)Position Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.227 A/FUnknownUnknown
RE (O/C)Position Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.327 A/FUnknownUnknown
RE (O/C)Position Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.427 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM63/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Position Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.527 A/FUnknownUnknown
RE (O/C)Position Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.627 A/FUnknownUnknown
RE (O/C)Position Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.727 A/FUnknownUnknown
RE (O/C)Position Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.827 A/FUnknownUnknown
RE (O/C)Power Control Aileron (PCU)
20-Sep-1983Mos
0Hrs
0Ldg
Left27 A/FUnknownUnknown
RE (O/C)Power Control Aileron (PCU)
20-Sep-1983Mos
0Hrs
0Ldg
Right27 A/FUnknownUnknown
RE (O/C)Power Control Flight Spoiler Unit
20-Sep-1983Mos
0Hrs
0Ldg
Left Inboard27 A/FUnknownUnknown
RE (O/C)Power Control Flight Spoiler Unit
20-Sep-1983Mos
0Hrs
0Ldg
Left Outboard27 A/FUnknownUnknown
RE (O/C)Power Control Flight Spoiler Unit
20-Sep-1983Mos
0Hrs
0Ldg
Right Inboard27 A/FUnknownUnknown
RE (O/C)Power Control Flight Spoiler Unit
20-Sep-1983Mos
0Hrs
0Ldg
Right Outboard27 A/FUnknownUnknown
RE (O/C)Power Control Ground Spoiler Unit
20-Sep-1983Mos
0Hrs
0Ldg
Left27 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM64/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Power Control Ground Spoiler Unit
20-Sep-1983Mos
0Hrs
0Ldg
Right27 A/FUnknownUnknown
RE (O/C)Power Control Rudder (PCU)
20-Sep-1983Mos
0Hrs
0Ldg
Lower27 A/FUnknownUnknown
RE (O/C)Power Control Rudder (PCU)
20-Sep-1983Mos
0Hrs
0Ldg
Mid27 A/FUnknownUnknown
RE (O/C)Power Control Rudder (PCU)
20-Sep-1983Mos
0Hrs
0Ldg
Upper27 A/FUnknownUnknown
RE (O/C)Power Control Unit Elevator (PCU)
20-Sep-1983Mos
0Hrs
0Ldg
No.127 A/FUnknownUnknown
RE (O/C)Power Control Unit Elevator (PCU)
20-Sep-1983Mos
0Hrs
0Ldg
No.227 A/FUnknownUnknown
RE (O/C)Power Control Unit Elevator (PCU)
20-Sep-1983Mos
0Hrs
0Ldg
No.327 A/FUnknownUnknown
RE (O/C)Power Control Unit Elevator (PCU)
20-Sep-1983Mos
0Hrs
0Ldg
No.427 A/FUnknownUnknown
RE (O/C)Power Drive Flap Control Unit
20-Sep-1983Mos
0Hrs
0Ldg
27 A/FUnknownUnknown
RE (O/C)Rudder Load Limiter
20-Sep-1983Mos
0Hrs
0Ldg
Lower27 A/FUnknownUnknown
RE (O/C)Rudder Load Limiter
20-Sep-1983Mos
0Hrs
0Ldg
Mid27 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM65/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Rudder Load Limiter
20-Sep-1983Mos
0Hrs
0Ldg
Upper27 A/FUnknownUnknown
RE (O/C)Rudder Position Transmitter
15-Dec-2004Mos
10,499.3Hrs
53,310Ldg
27 A/FLMT-199V11211690
RE (O/C)Spoiler Control Lever
20-Sep-1983Mos
0Hrs
0Ldg
27 A/FUnknownUnknown
RE (O/C)Stall Margin Indicator
20-Sep-1983Mos
0Hrs
0Ldg
Copilot27 A/FUnknownUnknown
RE (O/C)Stall Margin Indicator
20-Sep-1983Mos
0Hrs
0Ldg
Pilot27 A/FUnknownUnknown
RE (O/C)Stall Protection System (SPS), Stick Pusher Capstan Shaft
20-Sep-1983Mos
0Hrs
0Ldg
27 A/FUnknownUnknown
Component Inspection SimpleDUE: 12,397.5 Hrs1. RE 1500 HrsStall Protection System (SPS), Stick Pusher Capstan Shaft - ...27-39-00-104 *A/F27
RE (O/C)Stall Warning Computer
24-Mar-2009Mos
11,458.6Hrs
5,902Ldg
27 A/F600-59152-29014-0148 MI-60
RE (O/C)Stick Pusher Actuator
20-Sep-1983Mos
0Hrs0
0Ldg0
27 A/FNew501-1259-03
014-0148 MI-60
RE (O/C)Stick Shaker
20-Sep-1983Mos
0Hrs
0Ldg
Left27 A/FUnknownUnknown
RE (O/C)Stick Shaker
20-Sep-1983Mos
0Hrs
0Ldg
Right27 A/FUnknownUnknown
RE (O/C)Surface Trim Indicator
20-Sep-1983Mos
0Hrs
0Ldg
27 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM66/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Total Position Transducer
20-Sep-1983Mos
0Hrs
0Ldg
27 A/FUnknownUnknown
RE (O/C)Trim (Roll & Yaw) Actuator
20-Sep-1983Mos
0Hrs
0Ldg
27 A/FUnknownUnknown
RE (O/C)Yaw Damper Load Limiter
20-Sep-1983Mos
0Hrs
0Ldg
27 A/FUnknownUnknown
MandatoryRE (-)2003-22-12 Electronic flight instrument system (EFIS)
Mos
Hrs
Ldg
27 A/FEff: 12-Dec-2003
Nextdue Share EarliestDUE: 12,055.3 Hrs1. T 300 Hrs | 2. RE 300 HrsElectronic flight instrument system (EFIS) - Measurement, Re...2003-22-12 (Left) Paragraph (h)A/F27
Nextdue Share EarliestDUE: 12,055.3 Hrs1. T 300 Hrs | 2. RE 300 HrsElectronic flight instrument system (EFIS) - Measurement, Re...2003-22-12 (Right) Paragraph (h)A/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Electronic flight instrument system (EFIS) - Revision of Air...2003-22-12 Paragraph (a)A/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Electronic flight instrument system (EFIS) - All AOA Vane An...2003-22-12 Paragraph (d)A/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Electronic flight instrument system (EFIS) - One or More AOA...2003-22-12 Paragraph (e)A/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Electronic flight instrument system (EFIS) - Any AOA Vane An...2003-22-12 Paragraph (f)A/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Electronic flight instrument system (EFIS) - inspect the le...2003-22-12 Paragraph (j)(1)A/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Electronic flight instrument system (EFIS) - Concurrent Requ...2003-22-12 Paragraph (k)A/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Electronic flight instrument system (EFIS) - Concurrent Requ...2003-22-12 Paragraph (l)A/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Electronic flight instrument system (EFIS) - Alternative Met...2003-22-12 Paragraph (n)A/F27
Mandatory ≈20-Feb-2016RE2003-22-12 (Left) Paragraph
(h)
Electronic flight instrument system (EFIS) - Measurement, Repetitive Measurement and Corrective Actions
22-Mar-2013Mos
14.1 Hrs12,055.330011,755.3Hrs
Ldg
27 A/FSBEff: 12-Dec-2003 Complied
With
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Rework - Stall Protection System - Angle-of-At...A601-0550 Rev 1A/F27
Mandatory ≈20-Feb-2016RE2003-22-12 (Right) Paragraph
(h)
Electronic flight instrument system (EFIS) - Measurement, Repetitive Measurement and Corrective Actions
22-Mar-2013Mos
14.1 Hrs12,055.330011,755.3Hrs
Ldg
27 A/FSBEff: 12-Dec-2003 Complied
With
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Rework - Stall Protection System - Angle-of-At...A601-0550 Rev 1A/F27
MandatoryT (A/R)2003-22-12 Paragraph (a) Electronic flight instrument system (EFIS) - Revision of Airplane Flight Manual (AFM)
Mos
Hrs
Ldg
27 A/FEff: 12-Dec-2003
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM67/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryT (A/R)2003-22-12 Paragraph (d) Electronic flight instrument system (EFIS) - All AOA Vane Angles Within Tolerances: Disconnection and Measurement
Mos
Hrs
Ldg
27 A/FEff: 12-Dec-2003
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Rework - Stall Protection System - Angle-of-At...A601-0550 Rev 1A/F27
MandatoryT (A/R)2003-22-12 Paragraph (e) Electronic flight instrument system (EFIS) - One or More AOA Vane Angles Outside Tolerances, but All AOA Vane Angles Within Expanded Tolerances.
Mos
Hrs
Ldg
27 A/FEff: 12-Dec-2003
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Rework - Stall Protection System - Angle-of-At...A601-0550 Rev 1A/F27
MandatoryT (A/R)2003-22-12 Paragraph (f) Electronic flight instrument system (EFIS) - Any AOA Vane Angle Outside Tolerances
Mos
Hrs
Ldg
27 A/FEff: 12-Dec-2003
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Rework - Stall Protection System - Angle-of-At...A601-0550 Rev 1A/F27
MandatoryT (A/R)2003-22-12 Paragraph (j)(1) Electronic flight instrument system (EFIS) - inspect the left- and right-side AOA vane decal to verify that the correct decal is installed. For Model Cl-600-2A12 (CL-601)
and CL-600-2B16 (CL-601-3A and 3R)
Mos
Hrs
Ldg
27 A/FEff: 12-Dec-2003
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Rework - Stall Protection System - Inspection ...A601-0519A/F27
MandatoryT (A/R)2003-22-12 Paragraph (k) Electronic flight instrument system (EFIS) - Concurrent Requirements: Corrective Actions - Replace the AOA vane decal(s) with new vane decal(s), and ensure that the
new decal(s) is the correct type.
Mos
Hrs
Ldg
27 A/FEff: 12-Dec-2003
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Rework - Stall Protection System - Inspection ...A601-0519A/F27
MandatoryT (A/R)2003-22-12 Paragraph (l) Electronic flight instrument system (EFIS) - Concurrent Requirements: Corrective Actions - Remove existing decal(s), and do the alignment check(s) of the AOA vane
transducer.
Mos
Hrs
Ldg
27 A/FEff: 12-Dec-2003
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Rework - Stall Protection System - Angle-of-At...A601-0550 Rev 1A/F27
MandatoryT (A/R)2003-22-12 Paragraph (n) Electronic flight instrument system (EFIS) - Alternative Methods of Compliance.(refer to TLMC Chapter 5 task 27-35-04-101* for recurring inspection)
Mos
Hrs
Ldg
27 A/FEff: 12-Dec-2003
MandatoryRE (-)2004-09-37 Inboard flap actuator beam
05-Jun-2009Mos
11,458.6Hrs
5,902Ldg
27 A/FSB A601-0532Eff: 11-Jun-2004 Complied
With
Nextdue Share EarliestDUE: 6,565 Ldg1. T 1300 Ldg | 2. RE 100 LdgInboard flap actuator beam - Inspection/Repetitive Inspectio...2004-09-37 Paragraph (a)(b)A/F27
Nextdue Share EarliestDUE:1. RE -Inboard flap actuator beam - Terminating Actions (using para...2004-09-37 Paragraph (d)(e)A/F27
Nextdue Share EarliestDUE:1. RE -Inboard flap actuator beam - Terminating Actions (using para...2004-09-37 Paragraph (d)(f)A/F27
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM68/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Mandatory ≈09-Oct-2016T2004-09-37 Paragraph (a)(b) Inboard flap actuator beam - Inspection/Repetitive Inspection
Mos
Hrs
239 Ldg≈6,5651,300Ldg
27 A/FEff: 11-Jun-2004
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Modification - Flaps - Inspect Vane Brackets f...A601-0532 Rev 1A/F27
MandatoryRE (-)2004-09-37 Paragraph (d)(e) Inboard flap actuator beam - Terminating Actions (using paragraph (e))
Mos
Hrs
Ldg
27 A/FEff: 11-Jun-2004
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Modification - Flaps - Inspect Vane Brackets f...A601-0532 Rev 1A/F27
MandatoryRE (-)2004-09-37 Paragraph (d)(f) Inboard flap actuator beam - Terminating Actions (using paragraph (f))
Mos
Hrs
Ldg
27 A/FEff: 11-Jun-2004
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Modification - Flaps - Inspect Vane Brackets f...A601-0532 Rev 1A/F27
MandatoryRE (-)2004-25-19 Premature wear of the potentiometers in AOA transducers having a certain part number.
15-Apr-2005Mos
10,732.6Hrs
5,457Ldg
27 A/FBY AOA TRANSDUCER P/NEff: 04-Jan-2005 Not
Applicable
Nextdue Share EarliestDUE:1. T 7 Days | 2. RE -Premature wear of the potentiometers in AOA transducers havi...2004-25-19 Paragraph (f)A/F27
Nextdue Share EarliestDUE:1. RE -Premature wear of the potentiometers in AOA transducers havi...2004-25-19 Paragraph (g) LeftA/F27
Nextdue Share EarliestDUE:1. RE -Premature wear of the potentiometers in AOA transducers havi...2004-25-19 Paragraph (g) RightA/F27
MandatoryRE (-)2004-25-19 Paragraph (f) Premature wear of the potentiometers in AOA transducers having a certain part number - Airplane Flight Manual (AFM) Revisions.
15-Apr-2005Mos
10,732.6Hrs
5,457Ldg
27 A/FREVISED AFMEff: 04-Jan-2005 Complied
With
MandatoryRE (-)2004-25-19 Paragraph (g) Left Premature wear of the potentiometers in AOA transducers having certain part number - Repetitive Tests
Mos
Hrs
Ldg
27 A/FEff: 04-Jan-2004
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check - Stall Protection System - Angle-of-Attack (A...A601-0571A/F27
MandatoryRE (-)2004-25-19 Paragraph (g)
Right
Premature wear of the potentiometers in AOA transducers having certain part number - Repetitive Tests
Mos
Hrs
Ldg
27 A/FEff: 04-Jan-2005
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check - Stall Protection System - Angle-of-Attack (A...A601-0571A/F27
MandatoryRE (-)2005-26-04 Lower Gimbal Pin
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
27 A/FASB A601-0555Eff: 25-Jan-2006 Complied
With
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Modification - Horizontal Stabilizer Trim Cont...601-0555A/F27
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM69/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryRE (-)2006-02-04 Rudder balance spring assembly
20-Jan-2007Mos
10,976.2Hrs
5,614Ldg
27 A/FASB 601-0549Eff: 24-Feb-2006 Complied
With
Compliance Share DoubleDUE:1. T A/R | 2. RE -Modification - Rudder Control - Introduction of an Adjustabl...601-0549A/F27
MandatoryRE (-)2009-14-03 Flight Controls
23-Sep-2009Mos
11,459.7Hrs
5,904Ldg
27 A/FAFM REVISIONEff: 12-Aug-2009 Complied
With
MRB ≈18-Sep-2016RE27-11-00-201 Aileron, Flap Actuators and Attachments Visual Check
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
27 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-11-00-202 Aileron Control Check aileron backlash
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-11-11-203 Tension Regulator Operational Test - Tension Regulator
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE27-13-11-204 Anti-Float Mechanism Operational Test - Anti-Float Mechanism
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
27 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-13-21-205 Aileron Flutter Dampers - Check aileron flutter damper / Check flutter damper shear pin
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
Left
(PKG 600 Hour)
27 A/F
600-75142-3HA13712
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-13-21-205 Aileron Flutter Dampers - Check aileron flutter damper / Check flutter damper shear pin
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
Right
(PKG 600 Hour)
27 A/F
600-75142-9HA13913
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈24-Aug-2023RE27-13-21-206 Aileron Flutter Dampers - Remove, carry out “Testing and Fault Isolation” of Flutter Dampers and reinstall
08-Aug-2005Mos
3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs
Ldg
Left
(PKG 4800 Hour)
27 A/F
600-75142-3HA13712
Ref.:CMM/PSP 608/608A 27-09-01, Ref.:CMM/PSP 608/608A 27-13-21, Ref.:CMM/PSP 608/608A 27-13-22 (SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM70/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈24-Aug-2023RE27-13-21-206 Aileron Flutter Dampers - Remove, carry out “Testing and Fault Isolation” of Flutter Dampers and reinstall
08-Aug-2005Mos
3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs
Ldg
Right
(PKG 4800 Hour)
27 A/F
600-75142-9HA13913
Ref.:CMM/PSP 608/608A 27-09-01, Ref.:CMM/PSP 608/608A 27-13-21, Ref.:CMM/PSP 608/608A 27-13-22 (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-15-00-207 Roll Disconnect Mechanism Functional Test
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE27-17-00-208 Aileron Power Control Unit Operational Test
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
27 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-17-00-209 Aileron Power Control Unit Visual Check, paying particular attention for hydraulic fluidleakage
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-21-00-210 Rudder Control Check Rudder Backlash- Check PCU Input Load Limiter Travel - Visual Check of the following: (1) Load limiter balancing spring / (2) PCU input and
centering mechanism / (3) Rudder centering, preload and feel springs / (4) PCU’s for hydraulic fluid leakage
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈13-Jul-2017RE27-21-00-211 Rudder Control Rudder Anti-Jam Mechanism Functional Test
18-Oct-2003Mos
684 Hrs (+30)(12,725.2)-/+402,4009,808.2Hrs
Ldg
(PKG 2400 Hour)
27 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE27-25-00-212 Rudder Power Control Units Operational Test
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
27 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈13-Jul-2017RE27-30-00-235 Pitch Control System Pitch Trim Suppressor Unit - Bench Check
24-Oct-2004Mos
684 Hrs (+30)(12,725.2)-/+402,40010,459Hrs
Ldg
(PKG 2400 Hour)
27 A/F
Ref.:CMM/PSP 608/608A 27-30-04 (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-31-00-213 Elevator Control Check elevator backlash - Check PCU Input Jam Tolerant Mechanism Travel - Visual Check of the following: (1) Load limiter balancing springs (2 per
side) / (2) PCU input and centering mechanisms / (3) PCU’s for hydraulic fluid leakage
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE27-31-00-214 Elevator Control (Pre SB 601-0304) Visual Check of elevator control levers, Part Numbers 600-92354-7, 600-92358-1 and 600-92359-1, paying particular attention for
cracks in the hub area where the taper pinis installed
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
27 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM71/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈24-Oct-2017RE27-31-00-215 Elevator Control Elevator load limiters test
21-Oct-2004Mos
817.8 Hrs (+40)12,859-/+402,40010,459Hrs
Ldg
(PKG 2400 Hour)
27 A/F
(SOURCE: TLMC 05-20-15)
AWL ≈07-Nov-2016RE27-31-11-101 Pitch Feel Simulator - Functional Test of the Pitch Feel Simulator
26-Sep-2006Mos
356.3 Hrs12,397.51,50010,897.5Hrs
Ldg
Left27 A/FUnknownUnknown
(SOURCE: TLMC 05-10-30)
AWL ≈07-Nov-2016RE27-31-11-101 Pitch Feel Simulator - Functional Test of the Pitch Feel Simulator
26-Sep-2006Mos
356.3 Hrs12,397.51,50010,897.5Hrs
Ldg
Right27 A/FUnknownUnknown
(SOURCE: TLMC 05-10-30)
MRB ≈03-May-2017RE27-33-11-216 Elevator Flutter Dampers - Check elevator flutter damper
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
Left Inboard
(PKG 600 Hour)
27 A/F
1018100-7HA13933
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-33-11-216 Elevator Flutter Dampers - Check elevator flutter damper
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
Left Outboard
(PKG 600 Hour)
27 A/F
1018100-7HA13911
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-33-11-216 Elevator Flutter Dampers - Check elevator flutter damper
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
Right Inboard
(PKG 600 Hour)
27 A/F
1018100-7HA13910
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-33-11-216 Elevator Flutter Dampers - Check elevator flutter damper
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
Right Outboard
(PKG 600 Hour)
27 A/F
1018100-7HA13919
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈24-Aug-2023RE27-33-11-217 Elevator Flutter Dampers - Remove, carry out “Testing and Fault Isolation” of Flutter Damper and reinstall
08-Aug-2005Mos
3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs
Ldg
Left Inboard
(PKG 4800 Hour)
27 A/F
1018100-7HA13933
Ref.:CMM/PSP 608/608A 27-09-01, Ref.:CMM/PSP 608/608A 27-13-21, Ref.:CMM/PSP 608/608A 27-13-22 (SOURCE: TLMC 05-20-15)
MRB ≈24-Aug-2023RE27-33-11-217 Elevator Flutter Dampers - Remove, carry out “Testing and Fault Isolation” of Flutter Damper and reinstall
08-Aug-2005Mos
3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs
Ldg
Left Outboard
(PKG 4800 Hour)
27 A/F
1018100-7HA13911
Ref.:CMM/PSP 608/608A 27-09-01, Ref.:CMM/PSP 608/608A 27-13-21, Ref.:CMM/PSP 608/608A 27-13-22 (SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM72/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈24-Aug-2023RE27-33-11-217 Elevator Flutter Dampers - Remove, carry out “Testing and Fault Isolation” of Flutter Damper and reinstall
08-Aug-2005Mos
3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs
Ldg
Right Inboard
(PKG 4800 Hour)
27 A/F
1018100-7HA13910
Ref.:CMM/PSP 608/608A 27-09-01, Ref.:CMM/PSP 608/608A 27-13-21, Ref.:CMM/PSP 608/608A 27-13-22 (SOURCE: TLMC 05-20-15)
MRB ≈24-Aug-2023RE27-33-11-217 Elevator Flutter Dampers - Remove, carry out “Testing and Fault Isolation” of Flutter Damper and reinstall
08-Aug-2005Mos
3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs
Ldg
Right Outboard
(PKG 4800 Hour)
27 A/F
1018100-7HA13919
Ref.:CMM/PSP 608/608A 27-09-01, Ref.:CMM/PSP 608/608A 27-13-21, Ref.:CMM/PSP 608/608A 27-13-22 (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-35-00-218 Pitch Disconnect Mechanism Operational Test
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE27-37-00-219 Elevator Power Control Units Operational Test
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
27 A/F
(SOURCE: TLMC 05-20-15)
AWLRE (N/A)27-39-00-101 Stall Protection System (SPS) (Pre SB 601-0510) - Functional Test of the Flap Input
Mos
Hrs
Ldg
27 A/F
(SOURCE: TLMC 05-10-30)
AWLRE (N/A)27-39-00-102 Stall Protection System (SPS) (Pre SB 601-0510) - Functional Test of the Phase Advance and Sideslip Compensation
Mos
Hrs
Ldg
27 A/F
(SOURCE: TLMC 05-10-30)
AWL ≈03-Nov-2024RE27-39-00-103 Stall Protection System (SPS) (Post SB 601-0510) - Functional Test of the Flap and Sideslip Compensation Monitor
25-Jul-2008Mos
4,190.8 Hrs16,2324,80011,432Hrs
Ldg
27 A/F
(SOURCE: TLMC 05-10-30)
AWL ≈07-Nov-2016RE27-39-00-104 * Stall Protection System (SPS), Stick Pusher Capstan Shaft - Functional Test of the Stick Pusher Capstan Shaft, Part No. 600-59156-7 (Vendor Part No. 501-1258-01)
26-Sep-2006Mos
356.3 Hrs12,397.51,50010,897.5Hrs
Ldg
27 A/FUnknownUnknown
(SOURCE: TLMC 05-10-30)
MRB ≈03-May-2017RE27-39-00-220 Stall Protection System Operational Test
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈13-Jul-2017RE27-39-00-221 Stall Protection System Functional Test
04-May-2004Mos
684 Hrs (+30)(12,725.2)-/+402,40010,325.2Hrs
Ldg
(PKG 2400 Hour)
27 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM73/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈20-Feb-2016RE27-39-11-101 * Angle-of-Attack Vane Transducer Linearity - Functional Test of the Angle-of-Attack (AOA) Transducer Linearity
22-Mar-2013Mos
14.1 Hrs12,055.330011,755.3Hrs
Ldg
Left27 A/FUnknownUnknown
(SOURCE: TLMC 05-10-30)
AWL ≈20-Feb-2016RE27-39-11-101 * Angle-of-Attack Vane Transducer Linearity - Functional Test of the Angle-of-Attack (AOA) Transducer Linearity
22-Mar-2013Mos
14.1 Hrs12,055.330011,755.3Hrs
Ldg
Right27 A/F600-59154-1247-098
(SOURCE: TLMC 05-10-30)
AWLRE (N/A)27-39-11-102 * Angle-of-Attack Vane Transducer, Restoration - Overhaul of the Angle-of-Attack (AOA) Transducer,
Mos
Hrs
Ldg
Left27 A/FUnknownUnknown
(SOURCE: TLMC 05-10-30)
AWLRE (N/A)27-39-11-102 * Angle-of-Attack Vane Transducer, Restoration - Overhaul of the Angle-of-Attack (AOA) Transducer,
Mos
Hrs
Ldg
Right27 A/F600-59154-1247-098
(SOURCE: TLMC 05-10-30)
AWL ≈03-May-2017RE27-40-00-102 * Trim System Actuator Brake - Operational Test
10-Feb-2016Mos
590.8 Hrs12,63260012,041.2Hrs
6,326Ldg
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-10-30)
MRB ≈03-May-2017RE27-40-00-222 Horizontal Stabilizer Trim Control Pitch trim actuator backlash check
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE27-40-00-238 Pitch Trim Actuator - Lubricate horizontal stabilizer pitch trim actuator
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
27 A/F
(SOURCE: TLMC 05-20-15)
AWL ≈19-Mar-2018RE27-40-16-101 * Pitch Trim Actuator - Overhaul
11-Mar-2000Mos
1,011.7 Hrs13,052.96,6006,452.9Hrs
Ldg
27 A/F600-92301-65346E
Ref:MM/PSP 608/608A (SOURCE: TLMC 05-10-30)
MRB ≈03-May-2017RE27-40-16-223 Pitch Trim Actuator - Inspect pitch trim actuator
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
AWL ≈04-Jul-2020RE27-50-16-101 * Outboard Flap Actuator - Restoration of the Outboard Flap Actuator
12-May-2010Mos
Hrs
1,584 Ldg7,9102,0005,910Ldg
Left Inboard27 A/F600-93000-82UNKNOWN
(SOURCE: TLMC 05-10-30) (NOTE: For Component where flight cycles are Unknown)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM74/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈04-Jul-2020RE27-50-16-101 * Outboard Flap Actuator - Restoration of the Outboard Flap Actuator
12-May-2010Mos
Hrs
1,584 Ldg7,9102,0005,910Ldg
Left Outboard27 A/F600-93000-93UNKNOWN
(SOURCE: TLMC 05-10-30) (NOTE: For Component where flight cycles are Unknown)
AWL ≈04-Jul-2020RE27-50-16-101 * Outboard Flap Actuator - Restoration of the Outboard Flap Actuator
12-May-2010Mos
Hrs
1,584 Ldg7,9102,0005,910Ldg
Right Inboard27 A/F600-93000-82UNKNOWN
(SOURCE: TLMC 05-10-30) (NOTE: For Component where flight cycles are Unknown)
AWL ≈04-Jul-2020RE27-50-16-101 * Outboard Flap Actuator - Restoration of the Outboard Flap Actuator
12-May-2010Mos
Hrs
1,584 Ldg7,9102,0005,910Ldg
Right Outboard27 A/F600-93000-93UNKNOWN
(SOURCE: TLMC 05-10-30) (NOTE: For Component where flight cycles are Unknown)
MRB ≈15-Jun-2016RE27-50-16-224 Flap Actuator - Outboard flap actuator backlash check
18-Oct-2003Mos
167 Hrs (+40)12,208.2-/+402,4009,808.2Hrs
Ldg
(PKG 2400 Hour)
27 A/F
(SOURCE: TLMC 05-20-15) (NOTE: Both the inboard and outboard actuators of the outboard flap are to be checked.)
MRB ≈03-May-2017RE27-50-16-236 Flap Actuator Detailed Inspection
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈24-Oct-2017RE27-50-16-237 Flap Actuator Torque and Side Play Check
23-Oct-2004Mos
817.8 Hrs (+40)12,859-/+402,40010,459Hrs
Ldg
(PKG 2400 Hour)
27 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-50-21-225 Power Drive Unit (PDU) Operational Test of flap PDU motor brake
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-50-26-226 Asymmetry/Overspeed Detector and Brake Brake drag torque test
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-50-41-227 Flexible Drive Shaft Check flexible drive shaft casing
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
Servicing - Recommended ≈24-Aug-2018RE27-50-41-301 Flexible Drive Shaft - Check flexible drive shaft casing / Check flexible drive shaft inner core
08-Aug-2005Mos
1,218.6 Hrs (+40)13,259.8-/+402,40010,859.8Hrs
Ldg
(PKG 2400 Hour)
27 A/F
(ZONE: 500, 600) (ACCESS: 571/671-CB-FB, 581/681-AB-BB-CB-DB-EB-FB-GB) (SOURCE: MPD 3.2)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM75/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈03-May-2017RE27-61-00-229 Spoiler Control Visual Check of Flight Spoiler and Ground Spoiler Actuators, Attachments and Mechanisms, paying particular attention to the flight spoiler track roller,
cam and detent assembly for wear and freedom of movement
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-61-00-230 Spoiler Control (A/C 3001 to 3059 with SB 601-0113 NOT incorporated) - Operational Test of throttle switches
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE27-61-00-231 Spoiler Control/Scheduled Servicing Lubricate Flight Spoilers Flexshaft and Controlex Cable end
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
27 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈14-Oct-2016RE27-61-00-233 Spoiler Control (Pre SB 601-0113) Ground Spoiler/Thrust Reverser Separation Diode Test
11-Dec-2003Mos
325.5 Hrs (+40)12,366.7-/+402,4009,966.7Hrs
Ldg
(PKG 2400 Hour)
27 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE27-65-00-234 Flight Spoiler Power Control Units Operational Test
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
27 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE27-69-00-228 Ground Spoiler Actuators and Manifold Assembly (Pre SB 601-0224) Check Mechanical Locking Mechanism
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
27 A/F
(SOURCE: TLMC 05-20-15)
RecommendedRE (-)601-0020 Modification - Ground Spoiler Position Indication - Wiring Changes
Mos
Hrs
Ldg
27 A/F
RecommendedT (A/R)601-0020 Rev 1 Modification - Ground Spoiler Position Indication - Wiring Changes
Mos
Hrs
Ldg
27 A/FEff: 23-Oct-1984
OptionalRE (-)601-0035 Modification - Stall Protection System - Angle-of-Attack Vane Decal
Mos
Hrs
Ldg
27 A/F
OptionalRE (-)601-0035 Rev 1 Modification - Stall Protection System - Angle-of-Attack Vane Decal
01-Sep-1983Mos
0Hrs
0Ldg
27 A/FEff: 29-Aug-1984 Complied With
RecommendedRE (-)601-0036 Modification - Flight Spoiler Push/Pull Controls, Aileron Cables and and Flap Flexible Drive Shafts - Improved Clearances
Mos
Hrs
Ldg
27 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM76/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0036 Rev 1 Modification - Flight Spoiler Push/Pull Controls, Aileron Cables and and Flap Flexible Drive Shafts - Improved Clearances
Mos
Hrs
Ldg
27 A/F
RecommendedRE (-)601-0036 Rev 2 Modification - Flight Spoiler Push/Pull Controls, Aileron Cables and and Flap Flexible Drive Shafts - Improved Clearances
17-Sep-1983Mos
0Hrs
0Ldg
27 A/FEff: 25-Jun-1986 Complied With
RecommendedRE (-)601-0037 Modification - Flight Spoilers - Fillers and Toggles
Mos
Hrs
Ldg
27 A/FEff: 23-Jan-1984
OptionalRE (-)601-0040 Modification - Warning System - Flight Spoilers
17-Sep-1983Mos
0Hrs
0Ldg
27 A/FComplied With
OptionalT (A/R)601-0040 Rev 1 Modification - Warning System - Flight Spoilers
Mos
Hrs
Ldg
27 A/FEff: 09-Apr-1985
RecommendedRE (-)601-0055 Modification - Proximity Sensors - Rework
21-Feb-1995Mos
3,142Hrs
1,250Ldg
27 A/FComplied With
RecommendedT (A/R)601-0055 Rev 1 Modification - Proximity Sensors - Rework
Mos
Hrs
Ldg
27 A/FEff: 30-Jan-1986
RecommendedT (A/R)601-0058 Modification - Inboard Flaps - Forward Fairing Support Structure
Mos
Hrs
Ldg
27 A/FEff: 05-Apr-1985
RecommendedRE (-)601-0083 Special Check/Modification - Ailerons - Mixer Support Brackets
04-Sep-1985Mos
607Hrs
261Ldg
27 A/FEff: 21-May-1984 Complied With
RecommendedRE (-)601-0085 Modification - Elevator Controls - Replacement of Guard Pin and Addition of Rub Strip
12-Sep-1985Mos
607Hrs
261Ldg
27 A/FEff: 28-Sep-1984 Complied With
RecommendedRE (-)601-0090 Modification - Proximity Sensors - Improved Sealing
Mos
Hrs
Ldg
27 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM77/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0090 Rev 1 Modification - Proximity Sensors - Improved Sealing
28-Mar-1989Mos
2,373Hrs
910Ldg
27 A/FEff: 29-Jan-1986 Complied With
RecommendedRE (-)601-0095 Modification - Flight Spoiler Warning System - Elimination of Spurious Warnings
18-Sep-1985Mos
607Hrs
261Ldg
27 A/FEff: 27-Jun-1984 Complied With
RecommendedRE (-)601-0102 Modification - Lateral Accelerometers - Improved Installation
Mos
Hrs
Ldg
27 A/F
RecommendedRE (-)601-0102 Rev 1 Modification - Lateral Accelerometers - Improved Installation
23-Mar-1992Mos
Hrs
Ldg
27 A/FEff: 19-Sep-1986 Complied With
OptionalRE (-)601-0113 Modification - Ground Spoilers - Auto-Deployment
Mos
Hrs
Ldg
27 A/F
OptionalRE (-)601-0113 Rev 1 Modification - Ground Spoilers - Auto-Deployment
Mos
Hrs
Ldg
27 A/F
OptionalT (A/R)601-0113 Rev 2 Modification - Ground Spoilers - Auto-Deployment
Mos
Hrs
Ldg
27 A/FEff: 14-Dec-1987
RecommendedRE (-)601-0133 Modification - Outboard Flap Bute Doors - Hinge Pin Retention
16-Jul-1986Mos
952Hrs
403Ldg
27 A/FEff: 20-Mar-1985 Complied With
RecommendedRE (-)601-0136 Modification - Horizontal Stabilizer Trim Control - Transient Suppression Addition
Mos
Hrs
Ldg
27 A/F
RecommendedRE (-)601-0136 Rev 1 Modification - Horizontal Stabilizer Trim Control - Transient Suppression Addition
26-Jan-1987Mos
1,267Hrs
480Ldg
27 A/FEff: 14-Mar-1986 Complied With
RecommendedRE (-)601-0170 Special Check/Modification - Aileron Controls Pulley Brackets - Attachment Bolts
26-Jan-1987Mos
1,267Hrs
480Ldg
27 A/FEff: 14-Mar-1986 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:15 PM78/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalRE (-)601-0176 Stall Protection System - Stick Shaker
Mos
Hrs
Ldg
27 A/F
OptionalRE (-)601-0176 Rev 1 Stall Protection System - Stick Shaker
Mos
Hrs
Ldg
27 A/F
OptionalRE (-)601-0176 Rev 2 Stall Protection System - Stick Shaker
Mos
Hrs
Ldg
27 A/F
OptionalT (A/R)601-0176 Rev 3 Stall Protection System - Stick Shaker
Mos
Hrs
Ldg
27 A/FEff: 31-Aug-1995
RecommendedRE (-)601-0189 Special Check/Modification - Horizontal Stabilizer - Pitch Trim Actuator
Mos
Hrs
Ldg
27 A/FEff: 18-Aug-1986
RecommendedRE (-)601-0199 Special Check/Adjustment - Elevator - Wire Harness Reroute
01-Dec-1990Mos
3,058.6Hrs
1,212Ldg
27 A/FEff: 16-May-1988 Complied With
RecommendedRE (-)601-0204 Special Check/Modification - Rudder Control Yokes - Stop Bolt Clearance
07-Mar-1989Mos
2,373Hrs
910Ldg
27 A/FEff: 02-Jul-1987 Complied With
OptionalRE (-)601-0224 Modification - Ground Spoiler Actuators - Deletion of Life-Limiting Locks
Mos
Hrs
Ldg
27 A/F
OptionalT (A/R)601-0224 Rev 1 Modification - Ground Spoiler Actuators - Deletion of Life-Limiting Locks
Mos
Hrs
Ldg
27 A/FEff: 13-Jul-1990
RecommendedRE (-)601-0228 Wing Outboard Flaps - Identification Plates
Mos
Hrs
Ldg
27 A/FEff: 06-Oct-1987
RecommendedRE (-)601-0237 Modification - Stall Protection System - Computer Reliability Improvement
25-Apr-1988Mos
1,995Hrs
756Ldg
27 A/FComplied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM79/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedT (A/R)601-0237 Rev 1 Modification - Stall Protection System - Computer Reliability Improvement
Mos
Hrs
Ldg
27 A/FEff: 21-Dec-1989
OptionalT (A/R)601-0243 Modification - Aileron and Flight Spoiler Control Cables - Turnbuckle Relocation
Mos
Hrs
Ldg
27 A/FEff: 14-Mar-1988
RecommendedRE (-)601-0304 Special Check/Modification - Elevator Control Levers - Stress Corrosion
Mos
Hrs
Ldg
27 A/F
RecommendedRE (-)601-0304 Rev 1 Special Check/Modification - Elevator Control Levers - Stress Corrosion
21-Nov-1997Mos
Hrs
Ldg
27 A/FEff: 10-May-1991 Complied With
RecommendedRE (-)601-0312 Flap Actuators - Retaining Ring
24-Jan-1990Mos
2,653Hrs
1,022Ldg
27 A/FEff: 24-Nov-1989 Complied With
OptionalRE (-)601-0319 Modification - Aileron Flutter Dampers - Replacement
05-Aug-2003Mos
9,585.6Hrs
4,797Ldg
27 A/FEff: 22-Mar-1990 Complied With
RecommendedRE (-)601-0426 Special Check/Modification - Rudder Quadrant Assembly - Introduction of Sub-Assembly, Part No. K600-92600-3 or -7
Mos
Hrs
Ldg
27 A/F
RecommendedRE (-)601-0426 Rev 1 Special Check/Modification - Rudder Quadrant Assembly - Introduction of Sub-Assembly, Part No. K600-92600-3 or -7
28-Apr-1995Mos
4,555Hrs
1,824Ldg
27 A/FEff: 15-Nov-1994 Complied With
RecommendedRE (-)601-0438 Modification - Flap System - Asymmetry/Overspeed Detector and Brake Unit Wiring Harness
30-Sep-1994Mos
4,399Hrs
1,768Ldg
27 A/FEff: 23-Jun-1994 Complied With
RecommendedRE (-)601-0440 Modification - Flap Actuators - Attachment Bolt Replacement
26-Jan-1996Mos
4,785Hrs
1,932Ldg
27 A/FEff: 31-Mar-1995 Complied With
RecommendedRE (-)601-0457 Modification - Stall Protection System - Safety Stick Shaker Connector with Lockwire
06-Oct-1995Mos
4,704Hrs
1,894Ldg
27 A/FEff: 15-Aug-1995 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM80/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalT (A/R)601-0458 Modification - Flap Control Unit - Addition of Ground Studs and Shielded Wires
Mos
Hrs
Ldg
27 A/FEff: 15-Sep-1995
RecommendedRE (-)601-0477 Modification - Flap System - Introduction of New Proximity Switches in the Brake Detector Unit (BDU)
12-Nov-1997Mos
5,395Hrs
2,274Ldg
27 A/FEff: 28-Jun-1996 Complied With
OptionalRE (-)601-0479 Modification - Stall Protection System Addition of a Time Delay Relay
Mos
Hrs
Ldg
27 A/F
OptionalRE (-)601-0479 Rev 1 Modification - Stall Protection System Addition of a Time Delay Relay
23-Mar-2001Mos
Hrs
Ldg
27 A/FEff: 15-Jan-1997 Complied With
RecommendedRE (-)601-0498 Special Check/Rework - Control-Column Torque-Tube - Support Bearings and Pitch Disconnect Cable
05-Jan-2000Mos
Hrs
Ldg
27 A/FEff: 29-Oct-1999 Complied With
Nextdue Share EarliestDUE:1. T 400 Hrs | 2. RE -Special Check/Rework - Control-Column Torque-Tube - Support ...601-0498 Part AA/F27
Nextdue Share EarliestDUE:1. T 400 Hrs | 2. RE -Special Check/Rework - Control-Column Torque-Tube - Support ...601-0498 Part BA/F27
Nextdue Share EarliestDUE:1. T 1200 Hrs | 2. RE -Special Check/Rework - Control-Column Torque-Tube - Support ...601-0498 Part CA/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Control-Column Torque-Tube - Support ...601-0498 Part DA/F27
RecommendedRE (-)601-0498 Part A Special Check/Rework - Control-Column Torque-Tube - Support Bearings and Pitch Disconnect Cable
Mos
Hrs
Ldg
27 A/FEff: 29-Oct-1999
RecommendedRE (-)601-0498 Part B Special Check/Rework - Control-Column Torque-Tube - Support Bearings and Pitch Disconnect Cable
Mos
Hrs
Ldg
27 A/FEff: 29-Oct-1999
RecommendedRE (-)601-0498 Part C Special Check/Rework - Control-Column Torque-Tube - Support Bearings and Pitch Disconnect Cable
Mos
Hrs
Ldg
27 A/FEff: 29-Oct-1999
(NOTE: Recommended in less than 1,200 flight hours after the ServiceBulletin release date, if necessary as a result of PART A)
RecommendedT (A/R)601-0498 Part D Special Check/Rework - Control-Column Torque-Tube - Support Bearings and Pitch Disconnect Cable
Mos
Hrs
Ldg
27 A/FEff: 29-Oct-1999
(NOTE: Recommended before the next flight, if necessary as a resultof PART B.)
RecommendedRE (-)601-0510 Modification - Stall Protection System - Dormant Failures in the Stall Protection system (SPS) Computer
05-Jun-2009Mos
11,458.6Hrs
5,902Ldg
27 A/FEff: 05-Sep-2003 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM81/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0549 Modification - Rudder Control - Introduction of an Adjustable Balance Spring Assembly for the Rudder Control Surface
20-Jan-2007Mos
10,976.2Hrs
5,614Ldg
27 A/FEff: 04-Apr-2003 Complied With
RecommendedRE (-)601-0553 Modification - Wing Flap System - Serialization of Flap Actuator Beams
05-Aug-2003Mos
9,585.6Hrs
4,797Ldg
27 A/FEff: 30-Apr-2003 Complied With
RecommendedRE (-)601-0555 Special Check/Modification - Horizontal Stabilizer Trim Control - Possible Migration of the Horizontal Stabilizer Trim Actuator (HSTA) Lower Gimbal Pin
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
27 A/FEff: 31-Jan-2005 Complied With
RecommendedRE (-)601-0563 Special Check/Rework - Elevator System - Pitch Feel Simulator Disconnect Check and Replacement of Bearing and Lever Assembly
Mos
Hrs
Ldg
27 A/F
Nextdue Share EarliestDUE:1. RE -Special Check/Rework - Elevator System - Pitch Feel Simulato...601-0563 Part AA/F27
Nextdue Share EarliestDUE:1. RE -Special Check/Rework - Elevator System - Pitch Feel Simulato...601-0563 Part BA/F27
Nextdue Share EarliestDUE:1. RE -Special Check/Rework - Elevator System - Pitch Feel Simulato...601-0563 Part CA/F27
Nextdue Share EarliestDUE:1. RE -Special Check/Rework - Elevator System - Pitch Feel Simulato...601-0563 Part DA/F27
RecommendedRE (-)601-0563 Part A Special Check/Rework - Elevator System - Pitch Feel Simulator - Do a check of PFS serial number
25-Jul-2008Mos
11,432Hrs
5,881Ldg
27 A/FEff: 27-Feb-2004 Complied With
RecommendedRE (-)601-0563 Part B Special Check/Rework - Elevator System - Pitch Feel Simulator Disconnect Check
25-Jul-2008Mos
11,432Hrs
5,881Ldg
27 A/FEff: 27-Feb-2004 Complied With
RecommendedRE (-)601-0563 Part C Special Check/Rework - Elevator System - Pitch Feel Simulator Disconnect Check - Repeat check
25-Jul-2008Mos
11,432Hrs
5,881Ldg
27 A/FEff: 27-Feb-2004 Not Applicable
RecommendedRE (-)601-0563 Part D Special Check/Rework - Elevator System - Pitch Feel Simulator Disconnect Check and Replacement of Bearing and Lever Assembly
25-Jul-2008Mos
11,432Hrs
5,881Ldg
27 A/FEff: 27-Feb-2004 Complied With
RecommendedT (A/R)601-0563 Rev 1 Special Check/Rework - Elevator System - Pitch Feel Simulator Disconnect Check and Replacement of Bearing and Lever Assembly
Mos
Hrs
Ldg
27 A/FEff: 07-Nov-2005
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Elevator System - Pitch Feel Simulato...601-0563 Rev 1 Part AA/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Elevator System - Pitch Feel Simulato...601-0563 Rev 1 Part BA/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Elevator System - Pitch Feel Simulato...601-0563 Rev 1 Part CA/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Elevator System - Pitch Feel Simulato...601-0563 Rev 1 Part DA/F27
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM82/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedT (A/R)601-0563 Rev 1 Part A Special Check/Rework - Elevator System - Pitch Feel Simulator - Do a check of PFS serial number
Mos
Hrs
Ldg
27 A/FEff: 07-Nov-2005
RecommendedT (A/R)601-0563 Rev 1 Part B Special Check/Rework - Elevator System - Pitch Feel Simulator Disconnect Check
Mos
Hrs
Ldg
27 A/FEff: 07-Nov-2005
RecommendedT (A/R)601-0563 Rev 1 Part C Special Check/Rework - Elevator System - Pitch Feel Simulator Disconnect Check - Repeat check
Mos
Hrs
Ldg
27 A/FEff: 07-Nov-2005
RecommendedT (A/R)601-0563 Rev 1 Part D Special Check/Rework - Elevator System - Pitch Feel Simulator Disconnect Check and Replacement of Bearing and Lever Assembly
Mos
Hrs
Ldg
27 A/FEff: 07-Nov-2005
RecommendedT (A/R)601-0566 Special Check/Rework - Wing Flap System - Outboard Flap Actuators with Non-Conformant Trunnion Block Rotation
Mos
Hrs
Ldg
27 A/FEff: 31-Mar-2004
RecommendedRE (-)601-0576 Modification - Rudder - Replacement of Rudder System Stop Bolt Part No. 600-92689-1
Mos
Hrs
Ldg
27 A/F
RecommendedT (A/R)601-0576 Rev 1 Modification - Rudder - Replacement of Rudder System Stop Bolt Part No. 600-92689-1
Mos
Hrs
Ldg
27 A/FEff: 30-Aug-2006
OptionalRE (-)601-0577 Modification – Stall Protection System (SPS) – Introduction of Improved AOA Transducer Mounting and Sealing Installation
Mos
Hrs
Ldg
27 A/F
OptionalT (A/R)601-0577 Rev 1 Modification – Stall Protection System (SPS) – Introduction of Improved AOA Transducer Mounting and Sealing Installation
Mos
Hrs
Ldg
27 A/FEff: 27-Apr-2009
RecommendedT (A/R)601-0626 Modification – Horizontal Stabilizer Trim-Actuating System (HSTA) –Serialization of the Actuator Pins
1.9 Years[25-Feb-2018]Mos
689.6 Hrs[12,730.8]Hrs
Ldg
27 A/FEff: 25-Feb-2013
RecommendedT (-)601-0643 Special Check/Modification - Rudder Control System - Replace the Pilot's Rudder Pedal Bar Assembly or Rudder Pedal Assembly
Mos
Hrs
Ldg
27 A/FEff: 31-Aug-2015
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM83/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0643 Rev 1 Special Check/Modification - Rudder Control System - Replace the Pilot's Rudder Pedal Bar Assembly or Rudder Pedal Assembly
Mos
Hrs
Ldg
27 A/FEff: 31-Mar-2016
(AVG MAN HRS: 12)
MandatoryRE (-)82-01-01 Left and Right Controlex Cables
18-Sep-1985Mos
Hrs
Ldg
27 A/FBY AIRCRAFT SERIAL NUMBEREff: 04-Jan-1982 Not
Applicable
MandatoryRE (-)82-04-05 Aileron Power Control Unit
18-Sep-1985Mos
607Hrs
261Ldg
27 A/FBY AIRCRAFT SERIAL NUMBEREff: 04-Mar-1982 Not
Applicable
MandatoryRE (-)82-06-06 Flap Drive Shafts
18-Sep-1985Mos
607Hrs
261Ldg
27 A/FBY AIRCRAFT SERIAL NUMBEREff: 22-Mar-1982 Not
Applicable
MandatoryRE (-)83-07-51 R1 Flap Vane Support Assembly
18-Sep-1985Mos
Hrs
Ldg
27 A/FEff: 05-Jun-1984 Complied With
Compliance Share DoubleDUE:1. RE -Special Check/Modification - Wing Inboard Flap - Vane and As...A601-0010 Rev 2A/F27
MandatoryRE (-)94-08-15 Inspect Shoulder Bolts & Flap Actuator Housings
17-Jun-1994Mos
Hrs
Ldg
27 A/FASB A601-0415Eff: 20-May-1994 Complied
With
Compliance Share DoubleDUE:1. T 10 Hrs | 2. RE -Special Check - Flap Actuators - Attachment BoltsA601-0415A/F27
Mandatory ≈21-Feb-2016RE95-17-14 Horizontal Stabilizer Trim Actuator
07-Sep-2008Mos
14.5 Hrs12,055.760011,455.7Hrs
5,898Ldg
27 A/FSI A601-0443Complied With
Compliance Share DoubleDUE:1. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443A/F27
MandatoryRE (-)95-18-07 Inspect Rudder Control Quadrant
30-Nov-1995Mos
Hrs
Ldg
27 A/FSI A601-0426Eff: 30-Oct-1995 Complied
With
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Modification - Rudder Quadrant Assembly - Intr...601-0426 Rev 1A/F27
AlertRE (-)A601-0004 Special Check/Modificatiopn – Flap Structure – Wing Outboard Flap Vane and Associated Structure
06-Jan-2005Mos
11,613.3Hrs
6,021Ldg
27 A/FPART A - VISUAL INSPECTIONComplied With
AlertRE (-)A601-0004 Rev 1 Special Check/Modificatiopn – Flap Structure – Wing Outboard Flap Vane and Associated Structure
Mos
Hrs
Ldg
27 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM84/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AlertRE (-)A601-0004 Rev 2 Special Check/Modificatiopn – Flap Structure – Wing Outboard Flap Vane and Associated Structure
Mos
Hrs
Ldg
27 A/F
Alert ≈28-Feb-2017RE (-)A601-0004 Rev 3 Special Check/Modificatiopn – Flap Structure – Wing Outboard Flap Vane and Associated Structure
13-Nov-2015Mos
Hrs
379 Ldg[6,705]6,305Ldg
27 A/FEff: 22-Nov-1984
AlertRE (-)A601-0010 Special Check/Modification - Wing Inboard Flap - Vane and Associated Structure
20-Sep-1983Mos
0Hrs
0Ldg
27 A/FAT MANUFACTUTREComplied With
AlertRE (-)A601-0010 Rev 1 Special Check/Modification - Wing Inboard Flap - Vane and Associated Structure
Mos
Hrs
Ldg
27 A/F
AlertRE (-)A601-0010 Rev 2 Special Check/Modification - Wing Inboard Flap - Vane and Associated Structure
Mos
Hrs
Ldg
27 A/FEff: 22-Dec-1983
AlertT (A/R)A601-0056 Modification - Surface Trim Indicator - Replacement
Mos
Hrs
Ldg
27 A/FEff: 16-Mar-1984
AlertT (A/R)A601-0081 Special Check/Modification - No. 3 Hydraulic System Lines and Fittings - Clearance with Rudder
Mos
Hrs
Ldg
27 A/FEff: 14-Sep-1984
AlertRE (-)A601-0145 Modification - Pitch Trim Actuator - Yoke Pin Retention
27-Jan-1987Mos
0Hrs
Ldg
27 A/FEff: 03-Dec-1985 Complied With
AlertRE (-)A601-0332 Modification - Stall Protection System - Stick Pusher
Mos
Hrs
Ldg
27 A/F
AlertRE (-)A601-0332 Rev 1 Modification - Stall Protection System - Stick Pusher
04-Oct-1990Mos
Hrs
Ldg
27 A/FEff: 09-Jul-1991 Complied With
AlertRE (-)A601-0415 Special Check - Flap Actuators - Attachment Bolts
21-May-1993Mos
Hrs
Ldg
27 A/FEff: 25-Jun-1993 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM85/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AlertRE (-)A601-0421 Special Check/Modification - Rudder Control Quadrant Assembly
Mos
Hrs
Ldg
27 A/F
AlertRE (-)A601-0421 Rev 1 Special Check/Modification - Rudder Control Quadrant Assembly
Mos
Hrs
Ldg
27 A/F
AlertRE (-)A601-0421 Rev 2 Special Check/Modification - Rudder Control Quadrant Assembly
31-Oct-1993Mos
Hrs
Ldg
27 A/FEff: 22-Oct-1993 Complied With
AlertRE (-)A601-0443 Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - Overspeed Condition
Mos
Hrs
Ldg
27 A/F
Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Part AA/F27
Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Part BA/F27
Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Part CA/F27
AlertRE (-)A601-0443 Part A Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - HSTA brake operational check, if necessary do trouble-shooting of HSTA brake.
Mos
Hrs
Ldg
27 A/FEff: 11-Jan-1995
AlertRE (-)A601-0443 Part B Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - Do a trouble-Shooting of the Pitch trim Overspeed Condition
Mos
Hrs
Ldg
27 A/FEff: 11-Jan-1995
AlertRE (-)A601-0443 Part C Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - HSTA Replacement
Mos
Hrs
Ldg
27 A/FEff: 11-Jan-1995
AlertRE (-)A601-0443 Rev 1 Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - Overspeed Condition
Mos
Hrs
Ldg
27 A/F
Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Rev 1 Part AA/F27
Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Rev 1 Part BA/F27
Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Rev 1 Part CA/F27
AlertRE (-)A601-0443 Rev 1 Part A Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - HSTA brake operational check, if necessary do trouble-shooting of HSTA brake.
Mos
Hrs
Ldg
27 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM86/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AlertRE (-)A601-0443 Rev 1 Part B Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - Do a trouble-Shooting of the Pitch trim Overspeed Condition
Mos
Hrs
Ldg
27 A/F
AlertRE (-)A601-0443 Rev 1 Part C Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - HSTA Replacement
Mos
Hrs
Ldg
27 A/F
AlertRE (-)A601-0443 Rev 2 Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - Overspeed Condition
07-Sep-2008Mos
11,455.7Hrs
5,898Ldg
27 A/FEff: 15-May-1996 Complied With
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Rev 2 Part AA/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Rev 2 Part BA/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Horizontal Stabilizer Trim Actu...A601-0443 Rev 2 Part CA/F27
AlertT (A/R)A601-0443 Rev 2 Part A Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - HSTA brake operational check, if necessary do trouble-shooting of HSTA brake.
Mos
Hrs
Ldg
27 A/FEff: 15-May-1996
AlertT (A/R)A601-0443 Rev 2 Part B Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - Do a trouble-Shooting of the Pitch trim Overspeed Condition
Mos
Hrs
Ldg
27 A/FEff: 15-May-1996
AlertT (A/R)A601-0443 Rev 2 Part C Special Check/Modification - Horizontal Stabilizer Trim Actuator (HSTA) - HSTA Replacement
Mos
Hrs
Ldg
27 A/FEff: 15-May-1996
AlertRE (-)A601-0519 Special Check/Rework - Stall Protection System - Inspection and Replacement of Angle-of-Attack (AOA) Vane Decals
18-Nov-2003Mos
Hrs
Ldg
27 A/FEff: 30-Jul-1999 Complied With
AlertRE (-)A601-0532 Special Check/Modification - Flaps - Inspect Vane Brackets for Cracks, Replace Brackets and Remove Gaps Between Brackets and Mating Surfaces
05-Aug-2003Mos
9,585.6Hrs
4,797Ldg
27 A/FComplied With
Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Flaps - Inspect Vane Brackets f...A601-0532 Part AA/F27
Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Flaps - Inspect Vane Brackets f...A601-0532 Part BA/F27
Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Flaps - Inspect Vane Brackets f...A601-0532 Part CA/F27
AlertRE (-)A601-0532 Part A Special Check/Modification - Flaps - Inspect Vane Brackets for Cracks, Replace Brackets and Remove Gaps Between Brackets and Mating Surfaces - Visual Inpection
Mos
Hrs
Ldg
27 A/FEff: 29-Nov-2001
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM87/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AlertRE (-)A601-0532 Part B Special Check/Modification - Flaps - Inspect Vane Brackets for Cracks, Replace Brackets and Remove Gaps Between Brackets and Mating Surfaces - do a nondestructive
inspection (NDI)
Mos
Hrs
Ldg
27 A/FEff: 29-Nov-2001
AlertRE (-)A601-0532 Part C Special Check/Modification - Flaps - Inspect Vane Brackets for Cracks, Replace Brackets and Remove Gaps Between Brackets and Mating Surfaces - Replace all 12 vane
brackets aned remove all gaps.
Mos
Hrs
Ldg
27 A/FEff: 29-Nov-2001
AlertT (A/R)A601-0532 Rev 1 Special Check/Modification - Flaps - Inspect Vane Brackets for Cracks, Replace Brackets and Remove Gaps Between Brackets and Mating Surfaces
Mos
Hrs
Ldg
27 A/FEff: 08-Jul-2002
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Flaps - Inspect Vane Brackets f...A601-0532 Rev 1 Part AA/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Flaps - Inspect Vane Brackets f...A601-0532 Rev 1 Part BA/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Flaps - Inspect Vane Brackets f...A601-0532 Rev 1 Part CA/F27
AlertT (A/R)A601-0532 Rev 1 Part A Special Check/Modification - Flaps - Inspect Vane Brackets for Cracks, Replace Brackets and Remove Gaps Between Brackets and Mating Surfaces - Visual Inpection
Mos
Hrs
Ldg
27 A/FEff: 08-Jul-2002
AlertT (A/R)A601-0532 Rev 1 Part B Special Check/Modification - Flaps - Inspect Vane Brackets for Cracks, Replace Brackets and Remove Gaps Between Brackets and Mating Surfaces - do a nondestructive
inspection (NDI)
Mos
Hrs
Ldg
27 A/FEff: 08-Jul-2002
AlertT (A/R)A601-0532 Rev 1 Part C Special Check/Modification - Flaps - Inspect Vane Brackets for Cracks, Replace Brackets and Remove Gaps Between Brackets and Mating Surfaces - Replace all 12 vane
brackets aned remove all gaps.
Mos
Hrs
Ldg
27 A/FEff: 08-Jul-2002
AlertRE (-)A601-0540 Special Check - Flaps - Visually Examine Flap Actuator Beam Vane Brackets for Possible Cracks
01-Mar-2009Mos
Hrs
Ldg
27 A/FEff: 08-Dec-2000 Complied With
AlertRE (-)A601-0550 Special Check/Rework - Stall Protection System - Angle-of-Attack (AOA) Transducer Tolerance Check and Rework of Out-of-Tolerance AOA Transducer Assemblies
Mos
Hrs
Ldg
27 A/F
Nextdue Share EarliestDUE:1. RE -Special Check/Rework - Stall Protection System - Angle-of-At...A601-0550 Part AA/F27
Nextdue Share EarliestDUE:1. RE -Special Check/Rework - Stall Protection System - Rework of O...A601-0550 Part BA/F27
AlertRE (-)A601-0550 Part A Special Check/Rework - Stall Protection System - Angle-of-Attack (AOA) Transducer Tolerance Check
18-Nov-2003Mos
9,901.1Hrs
4,981Ldg
27 A/FEff: 07-Jan-2002 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM88/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AlertRE (-)A601-0550 Part B Special Check/Rework - Stall Protection System - Rework of Out-of-Tolerance AOA Transducer Assemblies
Mos
Hrs
Ldg
27 A/FEff: 07-Jan-2002
AlertT (A/R)A601-0550 Rev 1 Special Check/Rework - Stall Protection System - Angle-of-Attack (AOA) Transducer Tolerance Check and Rework of Out-of-Tolerance AOA Transducer Assemblies
Mos
Hrs
Ldg
27 A/FEff: 27-Feb-2004
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Stall Protection System - Angle-of-At...A601-0550 Rev 1 Part AA/F27
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework - Stall Protection System - Rework of O...A601-0550 Rev 1 Part BA/F27
AlertT (A/R)A601-0550 Rev 1 Part A Special Check/Rework - Stall Protection System - Angle-of-Attack (AOA) Transducer Tolerance Check
Mos
Hrs
Ldg
27 A/FEff: 27-Feb-2004
AlertT (A/R)A601-0550 Rev 1 Part B Special Check/Rework - Stall Protection System - Rework of Out-of-Tolerance AOA Transducer Assemblies
Mos
Hrs
Ldg
27 A/FEff: 27-Feb-2004
AlertT (A/R)A601-0571 Special Check - Stall Protection System - Angle-of-Attack (AOA) Transducer Linearity Check
Mos
Hrs
Ldg
27 A/FEff: 14-Oct-2004
MandatoryRE (-)CF-2002-05R1 Paragraph 1 Bombardier CL-600 “Challenger” – Angle of Attack Transducer, AFM Temporary Revision
Mos
Hrs
Ldg
27 A/FEff: 30-Jul-2004
MandatoryRE (-)CF-2002-05R1 PART A Bombardier CL-600 “Challenger” – Angle of Attack Transducer - Special Check
Mos
Hrs
Ldg
27 A/FEff: 30-Jul-2004
MandatoryRE (-)CF-2004-22 PART B Bombardier CL-600 “Challenger” – Angle of Attack Vane, Transducer Linearity Check
Mos
Hrs
Ldg
27 A/FEff: 26-Oct-2004
▼ 28 - FUEL
RE (O/C)2-Way APU Fuel Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
28 A/FNewAV16E1295
UNKNOWN
RE (O/C)3-Way APU Fuel Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
28 A/FNewAV23B1149-1
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM89/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Aux Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs0
0Ldg0
Left28 A/FNew391002-421
UNKNOWN
RE (O/C)Aux Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs0
0Ldg0
Right28 A/FNew391002-422
UNKNOWN
RE (O/C)Float Valve
20-Sep-1983Mos
0Hrs
0Ldg
Auxiliary28 A/FUnknownUnknown
RE (O/C)Float Valve
16-Aug-2002Mos
8,715.1Hrs
4,273Ldg
No.128 A/F2760131-1030813
RE (O/C)Float Valve
20-Sep-1983Mos
0Hrs
0Ldg
No.228 A/FUnknownUnknown
RE (O/C)Fuel Ejector Pump
20-Sep-1983Mos
0Hrs0
0Ldg0
Left28 A/FNew2780602-104
UNKNOWN
RE (O/C)Fuel Ejector Pump
20-Sep-1983Mos
0Hrs0
0Ldg0
Right28 A/FNew2780602-104
UNKNOWN
RE (O/C)Fuel Motorized Shutoff Valve
20-Sep-1983Mos
0Hrs
0Ldg
No.128 A/FUnknownUnknown
RE (O/C)Fuel Pump DC Cartridge
20-Sep-1983Mos
0Hrs
0Ldg
No.128 A/FUnknownUnknown
RE (O/C)Fuel Pump DC Cartridge
20-Sep-1983Mos
0Hrs
0Ldg
No.228 A/FUnknownUnknown
RE (O/C)Fuel Quantity Indicator
06-Apr-2004Mos
10,270.9Hrs
5,187Ldg
28 A/F478-286-102186
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM90/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.128 A/FUnknownUnknown
RE (O/C)Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.1028 A/FUnknownUnknown
RE (O/C)Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.1128 A/FUnknownUnknown
RE (O/C)Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.1228 A/FUnknownUnknown
RE (O/C)Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.1328 A/FUnknownUnknown
RE (O/C)Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.1428 A/FUnknownUnknown
RE (O/C)Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.1528 A/FUnknownUnknown
RE (O/C)Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.228 A/FUnknownUnknown
RE (O/C)Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs0
0Ldg0
No.328 A/FNew391002-438
UNKNOWN
RE (O/C)Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.428 A/FUnknownUnknown
RE (O/C)Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.528 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM91/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.628 A/FUnknownUnknown
RE (O/C)Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.728 A/FUnknownUnknown
RE (O/C)Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.828 A/FUnknownUnknown
RE (O/C)Fuel Quantity Transmitter
20-Sep-1983Mos
0Hrs
0Ldg
No.928 A/FUnknownUnknown
RE (O/C)Fuel Scavenger Ejector Pump
20-Sep-1983Mos
0Hrs0
0Ldg0
Left28 A/FNew2780472-102
UNKNOWN
RE (O/C)Fuel Scavenger Ejector Pump
20-Sep-1983Mos
0Hrs0
0Ldg0
Right28 A/FNew2780472-102
UNKNOWN
RE (O/C)Fuel Shutoff Valve
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
Left28 A/F601-62900-1P80257
RE (O/C)Fuel Shutoff Valve
20-Sep-1983Mos
0Hrs
0Ldg
Right28 A/FUnknownUnknown
RE (O/C)Fuel Tank Vent Valve
20-Sep-1983Mos
0Hrs
0Ldg
28 A/FUnknownUnknown
RE (O/C)Fuel Transfer Ejector Pump
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
Left28 A/F2780473-1030200
RE (O/C)Fuel Transfer Ejector Pump
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
Right28 A/F2780473-103010
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM92/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)No. 1 Pressure Switch
20-Sep-1983Mos
0Hrs
0Ldg
28 A/FUnknownUnknown
RE (O/C)No. 2 Pressure Switch
20-Sep-1983Mos
0Hrs
0Ldg
28 A/FUnknownUnknown
RE (O/C)Shutoff Valve
20-Sep-1983Mos
0Hrs
0Ldg
Auxiliary28 A/FUnknownUnknown
RE (O/C)Shutoff Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Left28 A/FNew2760129-101
UNKNOWN
RE (O/C)Shutoff Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Right28 A/FNew2760129-101
UNKNOWN
RE (O/C)Signal Conditioner
20-Sep-1983Mos
0Hrs0
0Ldg0
28 A/FNew473382
UNKNOWN
RE (O/C)Tank Fuel Vent Valve
20-Sep-1983Mos
0Hrs
0Ldg
No.128 A/FUnknownUnknown
RE (O/C)Tank Fuel Vent Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
No.228 A/FNew2780491-105
UNKNOWN
RE (O/C)Transfer Float Valve
26-Mar-2007Mos
11,045.9Hrs
5,659Ldg
Left28 A/F2950022-1020857
RE (O/C)Transfer Float Valve
20-Sep-1983Mos
0Hrs
0Ldg
Right28 A/FUnknownUnknown
MRBRE (N/A)28-10-00-201 Fuel Storage (Post SB 601-0262) Visual Check of tail tank vent line (external to tank)
Mos
Hrs
Ldg
28 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM93/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE (N/A)28-10-00-202 Fuel Storage (Post SB 601-0262) Visual Check of aft cone and lower fairing, paying particularattention for fuel leakage, damage to Strobe Light/Power Supply/Dump
Valve Wiring
Mos
Hrs
Ldg
28 A/F
(SOURCE: TLMC 05-20-15)
MRBRE (N/A)28-10-00-203 Fuel Storage (Post SB 601-0262) Visual Check of tail tank internal and external structure andcomponents, paying particular attention for corrosion andleakage
Mos
Hrs
Ldg
28 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE28-10-00-225 Fuel Tank Gravity Filler Cap Remove, inspect for condition and re-install
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
28 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈30-Dec-2016RE28-10-11-204 Fuel Tanks Check Fuel Tanks for Leaks- Visual Check (external), paying particular attention for corrosion
05-Feb-2004Mos
426.1 Hrs (+40)12,467.3-/+402,40010,067.3Hrs
Ldg
(PKG 2400 Hour)
28 A/F
(SOURCE: TLMC 05-20-15)
MRBRE28-10-21-206 Forward and Aft Auxiliary Fuel Tanks External Check
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
28 A/F
(SOURCE: TLMC 05-20-15)
MRBRE28-10-21-207 Forward and Aft Auxiliary Fuel Tanks External Check (Using Borescope)
5.8 Months (+30
Days)26-Sep-2016-/+112026-Sep-2006Mos
Hrs
Ldg
28 A/F
(SOURCE: TLMC 05-20-15)
MRBRE28-10-31-205 Fuel and Vent Line Shrouds Fuselage tank wall interspace and associated shrouds pressuretest
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
28 A/F
(SOURCE: TLMC 05-20-15)
MRBRE28-10-31-208 Fuel and Vent Line Shrouds Pressure test of the following shrouds: (1) APU Negative G Fuel Feed Line / (2) APU Fuel Return Line / (3) APU Fuel Feed Line / (4) Engine
Fuel Feed Line / (5) Motive Flow Line / (6) Fuselage Vent Lines
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
28 A/F
(SOURCE: TLMC 05-20-15)
MRBRE28-10-31-209 Fuel and Vent Line Shrouds (Post SB 601-0262) Tail tank fuel shroud pressure test
5.8 Months (+30
Days)(26-Sep-2016)6024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
28 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE28-10-31-211 Fuel and Vent Line Shrouds Visual Check of the Vent and Distribution Shroud Drains forBlockage and Leakage
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
28 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM94/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE (N/A)28-10-36-210 Tail Tank Vent System (Post SB 601-0262) Vent line check valve inspection
Mos
Hrs
Ldg
28 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈29-Dec-2030RE28-21-11-212 Collector Tanks Collector Tank Flapper Check Valves Check
05-Aug-2003Mos
7,144.4 Hrs (+40)(19,185.6)-/+409,6009,585.6Hrs
Ldg
(PKG 9600 Hour)
28 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈14-Oct-2016RE28-21-16-213 Firewall Fuel Shutoff Valve Internal leakage check
11-Dec-2003Mos
325.5 Hrs (+40)12,366.7-/+402,4009,966.7Hrs
Ldg
(PKG 2400 Hour)
28 A/F
(SOURCE: TLMC 05-20-15)
MRBRE28-21-26-215 Scavenge Fuel Ejector Visual Check of pump screen
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
28 A/F
(SOURCE: TLMC 05-20-15)
MRBRE (N/A)28-22-00-216 Tail Tank Fuel Transfer System/Pressure Refuel/Defuel System (Post SB 601-0262) Visual Check of all tail tank fuel lines at R.H.belly fairing (wing fillet), paying
particular attention for fuel leakage and corrosion
Mos
Hrs
Ldg
28 A/F
(SOURCE: TLMC 05-20-15)
MRBRE (N/A)28-22-00-217 Tail Tank Fuel Transfer System (Post SB 601-0262) Fuel transfer functional test
Mos
Hrs
Ldg
28 A/F
(SOURCE: TLMC 05-20-15)
MRBRE (N/A)28-22-05-218 Tail Tank Fuel Transfer Line Check Valve (Post SB 601-0262) Remove and install new valve
Mos
Hrs
Ldg
28 A/F
(SOURCE: TLMC 05-20-15)
MRBRE (N/A)28-22-11-219 Rotor Burst Detection System (Post SB 601-0262) Rotor burst detection system - shroud pressure check
Mos
Hrs
Ldg
28 A/F
(SOURCE: TLMC 05-20-15)
MRBRE (N/A)28-22-11-220 Rotor Burst Detection System (Post SB 601-0262) Functional Test
Mos
Hrs
Ldg
28 A/F
(SOURCE: TLMC 05-20-15)
MRBRE (N/A)28-22-16-221 Tail Tank System Level Switches (Post SB 601-0262) Warning system before fuel operational test
Mos
Hrs
Ldg
28 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM95/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE (N/A)28-22-21-222 Tail Tank Shutoff Valves (Post SB 601-0262) Shutoff valves internal leakage check
Mos
Hrs
Ldg
28 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈24-Aug-2023RE28-25-21-223 APU Return Line Check Valve Remove Check Valve and Perform Internal Leakage Test
08-Aug-2005Mos
3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs
Ldg
(PKG 4800 Hour)
28 A/F
Ref.:CMM/PSP 608/608A 28-20-27 (SOURCE: TLMC 05-20-15)
MRBRE (N/A)28-30-11-224 Fuel Jettison System (Post SB 601-0262) Fuel jettison system functional test
Mos
Hrs
Ldg
28 A/F
(SOURCE: TLMC 05-20-15)
RecommendedRE (-)601-0018 Modification - Main Auxiliary Fuel Tank - Level Control Valve (LCV)
Mos
Hrs
Ldg
28 A/F
RecommendedRE (-)601-0018 Rev 1 Modification - Main Auxiliary Fuel Tank - Level Control Valve (LCV)
Mos
Hrs
Ldg
28 A/FEff: 23-Apr-1984
RecommendedRE (-)601-0033 Special Check/Modification - Main and Auxiliary Fuel Tanks - Fuel Capacity
Mos
Hrs
Ldg
28 A/F
RecommendedT (A/R)601-0033 Rev 1 Special Check/Modification - Main and Auxiliary Fuel Tanks - Fuel Capacity
Mos
Hrs
Ldg
28 A/FEff: 13-Feb-1987
OptionalRE (-)601-0063 Modification - Fuel Booster Pumps - Replacement of Fuel Pump Canisters and Cartridges
Mos
Hrs
Ldg
28 A/F
OptionalRE (-)601-0063 Rev 1 Modification - Fuel Booster Pumps - Replacement of Fuel Pump Canisters and Cartridges
Mos
Hrs
Ldg
28 A/F
OptionalT (A/R)601-0063 Rev 2 Modification - Fuel Booster Pumps - Replacement of Fuel Pump Canisters and Cartridges
Mos
Hrs
Ldg
28 A/FEff: 06-Jul-1988
RecommendedRE (-)601-0075 Special Check/Modification - Fuel Quantity System - Wiring
Mos
Hrs
Ldg
28 A/FEff: 04-May-1985
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM96/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0114 Modification - Fuel Pressure Switches - Replacement
18-Sep-1985Mos
607Hrs
261Ldg
28 A/FEff: 22-Feb-1985 Complied With
RecommendedT (A/R)601-0117 Modification - Forward Auxiliary Fuel Tank - Transfer Drain Line
Mos
Hrs
Ldg
28 A/FEff: 30-Apr-1985
OptionalT (A/R)601-0160 Modification - Forward and Aft Auxiliary Fuel Tanks - Vent Shroud Line Sealing Plugs
Mos
Hrs
Ldg
28 A/FEff: 29-Apr-1987
RecommendedRE (-)601-0209 Modification - Transfer Ejector Screens - Addition
23-Mar-1992Mos
3,584Hrs
1,446Ldg
28 A/FEff: 15-Sep-1987 Complied With
RecommendedRE (-)601-0213 Modification - Main Fuel Tank Level Control Valves - Wiring Conduits
Mos
Hrs
Ldg
28 A/F
RecommendedT (A/R)601-0213 Rev 1 Modification - Main Fuel Tank Level Control Valves - Wiring Conduits
Mos
Hrs
Ldg
28 A/FEff: 21-Jun-1988
RecommendedRE (-)601-0217 Modification - Refuel/Defuel System - Fuel Spillage Prevention
Mos
Hrs
Ldg
28 A/F
RecommendedRE (-)601-0217 Rev 1 Modification - Refuel/Defuel System - Fuel Spillage Prevention
Mos
Hrs
Ldg
28 A/F
RecommendedRE (-)601-0217 Rev 2 Modification - Refuel/Defuel System - Fuel Spillage Prevention
Mos
Hrs
Ldg
28 A/F
RecommendedRE (-)601-0217 Rev 3 Modification - Refuel/Defuel System - Fuel Spillage Prevention
01-Oct-1991Mos
Hrs
Ldg
28 A/FEff: 17-Mar-1989 Complied With
RecommendedRE (-)601-0220 Modification - Motive Flow Fuel Line - Rerouting
Mos
Hrs
Ldg
28 A/FEff: 11-May-1988
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM97/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0222 Modification - Motive Flow Line Fittings - Identification
Mos
Hrs
Ldg
28 A/F
RecommendedRE (-)601-0222 Rev 1 Modification - Motive Flow Line Fittings - Identification
28-Mar-1989Mos
2,373Hrs
910Ldg
28 A/FEff: 15-May-1988 Complied With
RecommendedRE (-)601-0223 Modification - Refuel/Defuel System - Fuel Line Clearance
Mos
Hrs
Ldg
28 A/FEff: 24-Aug-1987
OptionalRE (-)601-0225 Modification - Fuel Balancing System - Powered Crossfeed System
Mos
Hrs
Ldg
28 A/F
OptionalT (A/R)601-0225 Rev 1 Modification - Fuel Balancing System - Powered Crossfeed System
Mos
Hrs
Ldg
28 A/FEff: 23-Mar-1990
RecommendedRE (-)601-0229 Modification - Motive Flow Lines - Addition of Spiral Wrap
Mos
Hrs
Ldg
28 A/F
RecommendedRE (-)601-0229 Rev 1 Modification - Motive Flow Lines - Addition of Spiral Wrap
Mos
Hrs
Ldg
28 A/F
RecommendedRE (-)601-0229 Rev 2 Modification - Motive Flow Lines - Addition of Spiral Wrap
28-Mar-1989Mos
2,373Hrs
910Ldg
28 A/FEff: 26-Oct-1989 Complied With
OptionalRE (-)601-0262 Modification - Fuel Storage - Tail Cone Fuel Tank Addition
Mos
Hrs
Ldg
28 A/F
OptionalRE (-)601-0262 Rev 1 Modification - Fuel Storage - Tail Cone Fuel Tank Addition
Mos
Hrs
Ldg
28 A/F
OptionalRE (-)601-0262 Rev 2 Modification - Fuel Storage - Tail Cone Fuel Tank Addition
Mos
Hrs
Ldg
28 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM98/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalT (A/R)601-0262 Rev 3 Modification - Fuel Storage - Tail Cone Fuel Tank Addition
Mos
Hrs
Ldg
28 A/FEff: 23-Jan-1992
OptionalT (A/R)601-0274 Modification - Refuel/Defuel Control Panel - Cover Assembly Rework
Mos
Hrs
Ldg
28 A/FEff: 14-Jul-1988
RecommendedRE (-)601-0318 Modification - NACA Scoop Vent Line - Deletion of Check Valve
Mos
Hrs
Ldg
28 A/F
RecommendedRE (-)601-0318 Rev 1 Modification - NACA Scoop Vent Line - Deletion of Check Valve
Mos
Hrs
Ldg
28 A/F
RecommendedRE (-)601-0318 Rev 2 Modification - NACA Scoop Vent Line - Deletion of Check Valve
02-Nov-1992Mos
Hrs
Ldg
28 A/FEff: 25-Jun-1993 Complied With
RecommendedRE (-)601-0320 Modification - Primary Ejector Pump and Fuel Feed Tube - Connector Assembly
Mos
Hrs
Ldg
28 A/F
RecommendedRE (-)601-0320 Rev 1 Modification - Primary Ejector Pump and Fuel Feed Tube - Connector Assembly
06-Oct-1992Mos
Hrs
Ldg
28 A/FEff: 22-Jun-1992 Complied With
RecommendedRE (-)601-0355 Modification - Tail Cone Fuel Tank - Addition of Back Up Pump
Mos
Hrs
Ldg
28 A/FEff: 27-Mar-1992
RecommendedRE (-)601-0361 Modification - Auxiliary Tank Fuel Lines - Elimination of Possible Chafing
Mos
Hrs
Ldg
28 A/F
RecommendedRE (-)601-0361 Rev 1 Modification - Auxiliary Tank Fuel Lines - Elimination of Possible Chafing
21-Feb-1991Mos
3,142Hrs
1,250Ldg
28 A/FEff: 25-Nov-1991 Complied With
RecommendedRE (-)601-0362 Modification - Tail Cone Fuel Tank - Improvements Double Click For Further Effectivity
Mos
Hrs
Ldg
28 A/FEff: 27-Mar-1992
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM99/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0364 Special Check/Modification - Wing Tank Fuel Access Panels - Introduction of Conductive Gasket
12-Oct-1992Mos
3,754Hrs
1,519Ldg
28 A/FEff: 18-Nov-1991 Complied With
OptionalRE (-)601-0371 Fuel Tanks - Replacement Of Float Switches
Mos
Hrs
Ldg
28 A/FEff: 27-Mar-1992
RecommendedRE (-)601-0386 Modification - Tail Cone Fuel Tank - Replacement of Dump Valve Support Bracket and/or Flanged Fitting
Mos
Hrs
Ldg
28 A/FEff: 27-Mar-1992
RecommendedRE (-)601-0391 Special Check/Rework - Tail Cone Fuel Tank - Lightning Protection
Mos
Hrs
Ldg
28 A/FEff: 27-Jan-1992
RecommendedRE (-)601-0392 Special Check/Modification - RH Engine Fuel Feed Line - Clearance with Fourteenth (14th) Stage Bleed Air Shutoff Valve
Mos
Hrs
Ldg
28 A/F
RecommendedT (A/R)601-0392 Rev 1 Special Check/Modification - RH Engine Fuel Feed Line - Clearance with Fourteenth (14th) Stage Bleed Air Shutoff Valve
Mos
Hrs
Ldg
28 A/FEff: 15-Jan-1993
RecommendedRE (-)601-0435 Modification - Wing Tank Fuel Access Panels, Part No. 601R10906-17 and Conductive Gasket Part No. 600-10910-3
28-Apr-1995Mos
4,555Hrs
1,824Ldg
28 A/FEff: 15-Sep-1994 Complied With
OptionalT (A/R)601-0508 Modification - Tail Tank System - Prevent False Low Fuel Indication
Mos
Hrs
Ldg
28 A/FEff: 31-May-1999
RecommendedRE (-)601-0513 Modification - Engine Standby and Auxiliary Power Unit (APU) Fuel Feed Systems - Replacement of Flexible Fuel Hoses
11-Dec-2001Mos
7,908.6Hrs
3,787Ldg
28 A/FEff: 31-Mar-2000 Complied With
RecommendedT (A/R)601-0525 Special Check/Modification - Fuel Feed System - Examine For Chafing on the Fuel Feed Lines and Add Brackets and Clamps
Mos
Hrs
Ldg
28 A/FEff: 30-Nov-1999
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Fuel Feed System - Examine For ...601-0525 Part AA/F28
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Fuel Feed System - Examine For ...601-0525 Part BA/F28
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM100/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedT (A/R)601-0525 Part A Special Check/Modification - Fuel Feed System - Examine For Chafing on the Fuel Feed Lines and Add Brackets and Clamps - Special Check
Mos
Hrs
Ldg
28 A/FEff: 30-Nov-1999
RecommendedT (A/R)601-0525 Part B Special Check/Modification - Fuel Feed System - Examine For Chafing on the Fuel Feed Lines and Add Brackets and Clamps - Rework
Mos
Hrs
Ldg
28 A/FEff: 30-Nov-1999
OptionalRE (-)601-0530 Modification - Fuel Storage - Removal of forward Auxiliary Fuel tank
Mos
Hrs
Ldg
28 A/FEff: 17-Dec-1999
OptionalT (A/R)601-0535 Modification - Fuel Storage - Deactivation of Forward Auxiliary Fuel Tank
Mos
Hrs
Ldg
28 A/FEff: 26-Feb-2007
OptionalRE (-)601-0536 Modification - Fuel Storage - Sustain Flight Operations with the Removal of the Forward Auxiliary Fuel Tank
Mos
Hrs
Ldg
28 A/F
OptionalT (A/R)601-0536 Rev 1 Modification - Fuel Storage - Sustain Flight Operations with the Removal of the Forward Auxiliary Fuel Tank
Mos
Hrs
Ldg
28 A/FEff: 12-Feb-2007
OptionalT (A/R)601-0605 Modification – Vent System Enhancement
Mos
Hrs
Ldg
28 A/FEff: 23-Nov-2009
RecommendedT601-0640 Special Check/Modification - Auxiliary Power Unit (APU) Fuel-Feed System - Possible Chafing of the APU Negative-G Fuel-Feed Drain Line
1.1 Years19-May-201724Mos
Hrs
Ldg
28 A/FEff: 19-May-2015
Nextdue Share EarliestDUE: 19-May-20171. T 24 Mos | 2. RE -Special Check - Auxiliary Power Unit (APU) Fuel-Feed System ...601-0640 Part AA/F28
Nextdue Share EarliestDUE: 19-May-20171. T 24 Mos | 2. RE -Modification - Auxiliary Power Unit (APU) Fuel-Feed System -...601-0640 Part BA/F28
RecommendedT601-0640 Part A Special Check - Auxiliary Power Unit (APU) Fuel-Feed System - Possible Chafing of the APU Negative-G Fuel-Feed Drain Line
1.1 Years19-May-201724Mos
Hrs
Ldg
28 A/FEff: 19-May-2015
(AVG MAN HRS: 0.5)
RecommendedT601-0640 Part B Modification - Auxiliary Power Unit (APU) Fuel-Feed System - Possible Chafing of the APU Negative-G Fuel-Feed Drain Line
1.1 Years19-May-201724Mos
Hrs
Ldg
28 A/FEff: 19-May-2015
(AVG MAN HRS: 8)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM101/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryRE (-)92-20-04 Tail Cone Fuel Tank
18-Mar-1992Mos
Hrs
Ldg
28 A/FBY CONFIGURATIONEff: 17-Nov-1992 Not
Applicable
Compliance Share DoubleDUE:1. RE -Special Check/Modification - Pressure Refuel/Defuel System -...A601-0381 Rev 2A/F28
MandatoryRE (-)98-03-02 Anti-Noise Filter on Standby & APU
30-Dec-2002Mos
9,147Hrs
4,540Ldg
28 A/FSB A601-0441Eff: 06-Mar-1998 Complied
With
AlertRE (-)A601-0175 Special Check/Modification - Scavenge Ejector Screens - Addition
Mos
Hrs
Ldg
28 A/F
AlertRE (-)A601-0175 Rev 1 Special Check/Modification - Scavenge Ejector Screens - Addition
Mos
Hrs
Ldg
28 A/F
AlertRE (-)A601-0175 Rev 2 Special Check/Modification - Scavenge Ejector Screens - Addition
26-Jan-1987Mos
1,267Hrs
480Ldg
28 A/FEff: 08-May-1987 Complied With
AlertRE (-)A601-0330 Special Check/Modification - Powered Crossfeed System - Fuel Line Cap Assembly Safetying
01-Oct-1991Mos
Hrs
Ldg
28 A/FEff: 07-May-1990 Not Applicable
AlertRE (-)A601-0381 Special Check/Modification - Pressure Refuel/Defuel System - Relocation of Sensing Line
Mos
Hrs
Ldg
28 A/F
AlertRE (-)A601-0381 Rev 1 Special Check/Modification - Pressure Refuel/Defuel System - Relocation of Sensing Line
Mos
Hrs
Ldg
28 A/F
AlertRE (-)A601-0381 Rev 2 Special Check/Modification - Pressure Refuel/Defuel System - Relocation of Sensing Line
Mos
Hrs
Ldg
28 A/FEff: 27-Jan-1992
AlertRE (-)A601-0441 Modification - Standby and APU Fuel Pump Assemblies - Sealing External Surfaces/Replacement of Anti-Noise (EMI) Filter
Mos
Hrs
Ldg
28 A/F
AlertRE (-)A601-0441 Rev 1 Modification - Standby and APU Fuel Pump Assemblies - Sealing External Surfaces/Replacement of Anti-Noise (EMI) Filter
28-Apr-1995Mos
4,555Hrs
1,824Ldg
28 A/FEff: 31-Mar-1995 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM102/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
▼ 29 - HYDRAULIC POWER
RE (O/C)Acoustic Filter
28-Feb-2007Mos
11,006.2Hrs
5,640Ldg
Left29 A/FAC9607F10Y3UNKNOWN
RE (O/C)Acoustic Filter
28-Feb-2007Mos
11,006.2Hrs
5,640Ldg
Right29 A/FAC2358F1279JUNKNOWN
RE (O/C)Air Pressure Indicator Gauge
20-Sep-1983Mos
0Hrs
0Ldg
No.129 A/FUnknownUnknown
RE (O/C)Air Pressure Indicator Gauge
20-Sep-1983Mos
0Hrs
0Ldg
No.229 A/FUnknownUnknown
RE (O/C)Air Pressure Indicator Gauge
20-Sep-1983Mos
0Hrs
0Ldg
No.329 A/FUnknownUnknown
RE (O/C)Air Pressure Indicator Gauge
20-Sep-1983Mos
0Hrs
0Ldg
No.429 A/FUnknownUnknown
RE (O/C)Air Pressure Indicator Gauge
20-Sep-1983Mos
0Hrs
0Ldg
No.529 A/FUnknownUnknown
RE (O/C)Electric Motor Driven Pump
20-Sep-1983Mos
0Hrs
0Ldg
No.129 A/FUnknownUnknown
RE (O/C)Engine Driven Hydraulic Pump
20-Sep-1983Mos
0Hrs0
0Ldg0
Left29 A/FNew601-75100-5
UNKNOWN
RE (O/C)Engine Driven Hydraulic Pump
18-Apr-2004Mos
10,295.1Hrs
5,200Ldg
Right29 A/F601-75100-5MX509255A
RE (O/C)Firewall Shut-Off Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Left29 A/FNewAV16B2069B1
N/A
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM103/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Firewall Shut-Off Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Right29 A/FNewAV16B2069B1
N/A
RE (O/C)Heat Hydraulic Fluid Exchanger
20-Sep-1983Mos
0Hrs
0Ldg
29 A/FUnknownUnknown
RE (O/C)Hydraulic Accumulator
20-Sep-1983Mos
0Hrs
0Ldg
No.129 A/FUnknownUnknown
RE (O/C)Hydraulic Accumulator
20-Sep-1983Mos
0Hrs
0Ldg
No.229 A/FUnknownUnknown
RE (O/C)Hydraulic Accumulator
20-Sep-1983Mos
0Hrs
0Ldg
No.329 A/FUnknownUnknown
RE (O/C)Hydraulic Assy Reservoir
20-Sep-1983Mos
0Hrs0
0Ldg0
No.129 A/FNew7301
UNKNOWN
RE (O/C)Hydraulic Assy Reservoir
20-Sep-1983Mos
0Hrs0
0Ldg0
No.229 A/FNew7302
UNKNOWN
RE (O/C)Hydraulic Assy Reservoir
20-Sep-1983Mos
0Hrs
0Ldg
No.329 A/FUnknownUnknown
RE (O/C)Hydraulic Motor
20-Sep-1983Mos
0Hrs
0Ldg
No.129 A/FUnknownUnknown
RE (O/C)Hydraulic Motor
20-Sep-1983Mos
0Hrs
0Ldg
No.229 A/FUnknownUnknown
RE (O/C)Hydraulic Motor
25-Jul-2008Mos
11,432Hrs
5,881Ldg
No.329 A/F9008D15-2XP2230
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM104/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Hydraulic Motor
20-Sep-1983Mos
0Hrs
0Ldg
No.429 A/FUnknownUnknown
RE (O/C)Hydraulic Pressure Indicator
20-Sep-1983Mos
0Hrs
0Ldg
No.129 A/FUnknownUnknown
RE (O/C)Hydraulic Pressure Indicator
20-Sep-1983Mos
0Hrs
0Ldg
No.229 A/FUnknownUnknown
RE (O/C)Hydraulic Pressure Indicator
20-Sep-1983Mos
0Hrs
0Ldg
No.329 A/FUnknownUnknown
RE (O/C)Hydraulic Pressure Switch
20-Sep-1983Mos
0Hrs
0Ldg
No.129 A/FUnknownUnknown
RE (O/C)Hydraulic Pressure Switch
20-Sep-1983Mos
0Hrs
0Ldg
No.229 A/FUnknownUnknown
RE (O/C)Hydraulic Pressure Switch
20-Sep-1983Mos
0Hrs
0Ldg
No.329 A/FUnknownUnknown
RE (O/C)Hydraulic Pressure Switch
20-Sep-1983Mos
0Hrs
0Ldg
No.429 A/FUnknownUnknown
RE (O/C)Hydraulic Pressure Switch
20-Sep-1983Mos
0Hrs
0Ldg
No.529 A/FUnknownUnknown
RE (O/C)Hydraulic Pressure Switch
20-Sep-1983Mos
0Hrs
0Ldg
No.629 A/FUnknownUnknown
RE (O/C)Hydraulic Pressure Transducer
20-Sep-1983Mos
0Hrs0
0Ldg0
No.129 A/FNew600-59174-17
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM105/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Hydraulic Pressure Transducer
20-Sep-1983Mos
0Hrs
0Ldg
No.229 A/FUnknownUnknown
RE (O/C)Hydraulic Pressure Transducer
20-Sep-1983Mos
0Hrs
0Ldg
No.329 A/FUnknownUnknown
RE (O/C)Hydraulic Pump
20-Sep-1983Mos
0Hrs
0Ldg
No.129 A/FUnknownUnknown
RE (O/C)Hydraulic Pump
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
No.229 A/F63108-03184787
RE (O/C)Hydraulic Pump
25-Jul-2008Mos
11,432Hrs
5,881Ldg
No.329 A/F63108-06180773
RE (O/C)Hydraulic Quantity Indicator
25-May-2004Mos
10,384.9Hrs
5,260Ldg
No.129 A/F115-080-380E0119
RE (O/C)Hydraulic Quantity Indicator
20-Sep-1983Mos
0Hrs0
0Ldg0
No.229 A/FNew115-080-3
80E0119
RE (O/C)Hydraulic Quantity Indicator
20-Sep-1983Mos
0Hrs0
0Ldg0
No.329 A/FNew115-080-3
80E0119
RE (O/C)Relief Valve
20-Sep-1983Mos
0Hrs
0Ldg
No.129 A/FUnknownUnknown
RE (O/C)Relief Valve
20-Sep-1983Mos
0Hrs
0Ldg
No.229 A/FUnknownUnknown
RE (O/C)Relief Valve
20-Sep-1983Mos
0Hrs
0Ldg
No.329 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM106/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryRE (-)2010-14-05 Hydraulic power
08-Jul-2011Mos
11,523.8Hrs
5,970Ldg
29 A/FEff: 05-Aug-2010 Complied With
Nextdue Share EarliestDUE:1. RE -Hydraulic power - inspect to determine the part numbers of ...2010-14-05 Paragraph (g)(1)A/F29
Nextdue Share EarliestDUE:1. RE -Hydraulic power - Replace the accumulator with a new, over...2010-14-05 Paragraph (g)(2) Brake No.2A/F29
Nextdue Share EarliestDUE:1. RE -Hydraulic power - Replace the accumulator with a new, over...2010-14-05 Paragraph (g)(2) Brake No.3A/F29
Nextdue Share EarliestDUE:1. RE -Hydraulic power - Replace the accumulator with a new, over...2010-14-05 Paragraph (g)(2) Hyd.Sys
No.1A/F29
Nextdue Share EarliestDUE:1. RE -Hydraulic power - Replace the accumulator with a new, over...2010-14-05 Paragraph (g)(2) Hyd.Sys
No.2A/F29
Nextdue Share EarliestDUE:1. RE -Hydraulic power - Replace the accumulator with a new, over...2010-14-05 Paragraph (g)(2) Hyd.Sys
No.3A/F29
MandatoryRE (-)2010-14-05 Paragraph (g)(1) Hydraulic power - inspect to determine the part numbers of the system accumulators numbers 1, 2, and 3 and brake accumulators numbers 2 and 3 that are installed
on the airplane.
Mos
Hrs
Ldg
29 A/FEff: 05-Aug-2010
MandatoryRE (-)2010-14-05 Paragraph (g)(2)
Brake No.2
Hydraulic power - Replace the accumulator with a new, overhauled, or refurbished accumulator with the same part number.
Mos
Hrs
Ldg
29 A/FEff: 05-Aug-2010
Compliance Share DoubleDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 2A/F29
MandatoryRE (-)2010-14-05 Paragraph (g)(2)
Brake No.3
Hydraulic power - Replace the accumulator with a new, overhauled, or refurbished accumulator with the same part number.
Mos
Hrs
Ldg
29 A/FEff: 05-Aug-2010
Compliance Share DoubleDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 2A/F29
MandatoryRE (-)2010-14-05 Paragraph (g)(2)
Hyd.Sys No.1
Hydraulic power - Replace the accumulator with a new, overhauled, or refurbished accumulator with the same part number.
Mos
Hrs
Ldg
29 A/FEff: 05-Aug-2010
Compliance Share DoubleDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 2A/F29
MandatoryRE (-)2010-14-05 Paragraph (g)(2)
Hyd.Sys No.2
Hydraulic power - Replace the accumulator with a new, overhauled, or refurbished accumulator with the same part number.
Mos
Hrs
Ldg
29 A/FEff: 05-Aug-2010
Compliance Share DoubleDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 2A/F29
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM107/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryRE (-)2010-14-05 Paragraph (g)(2)
Hyd.Sys No.3
Hydraulic power - Replace the accumulator with a new, overhauled, or refurbished accumulator with the same part number.
Mos
Hrs
Ldg
29 A/FEff: 05-Aug-2010
Compliance Share DoubleDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 2A/F29
MRB ≈18-Sep-2016RE29-00-00-201 Hydraulic Power Check Filter Differential Pressure Indicators on the following: (1) Case Drain Filters - No. 1, No. 2 and No. 3 Hydraulic Systems (6 locations) / (2)
Pressure and Return Manifold Filters - No. 1, No. 2 and No. 3 Hydraulic Systems (6 locations)
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
29 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE29-00-00-202 Hydraulic Power Internal leakage Check
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
29 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
Servicing - OptionalRE29-00-00-301 Hydraulic Power - Hydraulic fluid acidity check
10 Months (+29
Days)30-Jan-2017-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
29 A/F
(ZONE: 140, 310) (ACCESS: 112-BR, 190-DR, 311-BB) (SOURCE: MPD 3.3)
MRB ≈20-Oct-2017RE29-10-00-204 Main Systems Functional Test of Reservoir-Mounted Return Line Check Valve
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
29 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈24-Aug-2023RE29-10-00-205 Main Systems Remove No.1 and No.2 system hydraulic reservoir in-line check valves for bench check or install new valves
08-Aug-2005Mos
3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs
Ldg
(PKG 4800 Hour)
29 A/F
Ref.:CMM/PSP 608/608A 29-11-07 (SOURCE: TLMC 05-20-15)
MRB ≈24-Aug-2023RE29-10-00-206 Main Systems Remove No.3 system hydraulic reservoir in-line check valve forbench check or installnew valve
08-Aug-2005Mos
3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs
Ldg
(PKG 4800 Hour)
29 A/F
Ref.:CMM/PSP 608/608A 29-11-07 (SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE29-11-31-208 Case Drain Filter Check Filter Elements in No. 1, No. 2 and No. 3 HydraulicSystems (6 locations)
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
29 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE29-11-36-209 Pressure Manifold Check Filter Elements in No. 1, No. 2 and No. 3 HydraulicSystems (3 locations)
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
29 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE29-11-41-210 Return Manifold Check Filter Elements in No. 1, No. 2 and No. 3 HydraulicSystems (3 locations)
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
29 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM108/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈03-May-2017RE29-11-51-211 Heat Exchanger Visual Check, paying particular attention to security ofattachment
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
29 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE29-13-00-212 No. 3 Main System Visual Check pump installation areas for contamination by hydraulic fluid
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
29 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15) (NOTE: In case of shock mount contamination, refer to Section 5-50-10)
OptionalRE (-)601-0007 Modification - Hydraulic Systems No. 1 and No. 2 - Overboard Drains
01-Sep-1983Mos
Hrs
Ldg
29 A/FComplied With
OptionalT (A/R)601-0007 Rev 1 Modification - Hydraulic Systems No. 1 and No. 2 - Overboard Drains
Mos
Hrs
Ldg
29 A/FEff: 19-Dec-1985
RecommendedRE (-)601-0044 Modification - Main Systems - Replacement of Tube Assemblies
01-Sep-1983Mos
0Hrs
0Ldg
29 A/FEff: 21-Dec-1983 Complied With
OptionalRE (-)601-0066 Modification - No. 3 Hydraulic System - Cabin Noise Reduction
Mos
Hrs
Ldg
29 A/F
OptionalT (A/R)601-0066 Rev 1 Modification - No. 3 Hydraulic System - Cabin Noise Reduction
Mos
Hrs
Ldg
29 A/FEff: 06-Feb-1987
RecommendedRE (-)601-0077 Special Check/Modification - Underfloor Hydraulic Lines - Clearance with Fuel Line
Mos
Hrs
Ldg
29 A/FEff: 17-Aug-1984
RecommendedRE (-)601-0080 Special Check/Modification - Hydraulic Accumulator - Support Bracket
Mos
Hrs
Ldg
29 A/FEff: 09-Oct-1984
RecommendedRE (-)601-0088 Modification - No. 3 Hydraulic System - Reservoir Bleed Line
28-Mar-1989Mos
2,373Hrs
910Ldg
29 A/FComplied With
RecommendedT (A/R)601-0088 Rev 1 Modification - No. 3 Hydraulic System - Reservoir Bleed Line
Mos
Hrs
Ldg
29 A/FEff: 05-Sep-1985
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM109/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0089 Modification - No. 3 Hydraulic System Reservoir - AFT Mounting Pad
Mos
Hrs
Ldg
29 A/F
RecommendedT (A/R)601-0089 Rev 1 Modification - No. 3 Hydraulic System Reservoir - AFT Mounting Pad
Mos
Hrs
Ldg
29 A/FEff: 16-Sep-1985
RecommendedT (A/R)601-0098 Modification - Hydraulic Disconnect Fittings - Locking
Mos
Hrs
Ldg
29 A/FEff: 23-Aug-1984
RecommendedRE (-)601-0159 Modification - Hydraulic Hoses - Support Brackets
27-Jan-1987Mos
1,267Hrs
470Ldg
29 A/FEff: 17-Mar-1986 Complied With
RecommendedRE (-)601-0163 Modification - No. 3 Hydraulic System Pumps - Drain Reorientation
21-Feb-1991Mos
3,142Hrs
1,250Ldg
29 A/FEff: 18-Feb-1987 Complied With
RecommendedRE (-)601-0180 Modification - Hydraulic System Components - Protection Covers
Mos
Hrs
Ldg
29 A/F
RecommendedRE (-)601-0180 Rev 1 Modification - Hydraulic System Components - Protection Covers
Mos
Hrs
Ldg
29 A/FEff: 05-Feb-1988
RecommendedRE (-)601-0211 Modification - No. 3 Hydraulic System - Ecology Drain Bottles
29-Apr-1988Mos
1,995Hrs
756Ldg
29 A/FEff: 20-Apr-1988 Complied With
RecommendedRE (-)601-0269 Special Check/Modification - Pressure Manifold - Relief Valve Replacement
03-Mar-1989Mos
2,373Hrs
910Ldg
29 A/FEff: 07-Dec-1988 Complied With
RecommendedRE (-)601-0307 Modification - Main Systems - Replacement of Tube Assembly
31-Oct-1993Mos
4,142Hrs
1,668Ldg
29 A/FEff: 09-Jan-1990 Complied With
RecommendedRE (-)601-0328 Modification - Run-Around/Bypass Valve - Screw Replacement
04-Oct-1990Mos
2,979Hrs
1,177Ldg
29 A/FEff: 29-May-1990 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM110/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0388 Modification - No. 3 Hydraulic System - Replacement of Bulkhead Tee Reducers
14-Oct-1992Mos
3,754Hrs
1,519Ldg
29 A/FEff: 12-May-1992 Complied With
RecommendedRE (-)601-0414 Modification - Pressure Transducers - Introduction of Safety Lock-Wire
30-Sep-1994Mos
4,399Hrs
1,768Ldg
29 A/FEff: 25-Mar-1994 Complied With
RecommendedRE (-)601-0482 Modification – Hydraulic Tubes, Main Landing Gear Bay - Install New Re-Routed Tubes
12-Nov-1997Mos
5,395Hrs
2,274Ldg
29 A/FEff: 15-Apr-1997 Complied With
RecommendedRE (-)601-0541 Modification - Hydraulic System No. 1 and No. 2 - Replacement of Pressure Hose Assemblies at The Pylon Firewall
Mos
Hrs
Ldg
29 A/F
RecommendedT (A/R)601-0592 Modification – No. 3 Main System – Addition of Spacers for Accumulator Part No. 601R75138-3 Installation
Mos
Hrs
Ldg
29 A/FEff: 17-Dec-2007
RecommendedRE (-)601-0597 Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 1, No. 2 and No. 3 and Brake Accumulators No. 2 and No. 3 or Part Nos
08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/F
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 (Brake 2)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 (Brake 3)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 (Hyd Sys 1)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 (Hyd Sys 2)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 (Hyd Sys 3)A/F29
RecommendedRE (-)601-0597 (Brake 2) Modification – Hydraulic Power and Landing Gear – Replacement of Brake Accumulators No. 2 for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 10-Nov-2008
RecommendedRE (-)601-0597 (Brake 3) Modification – Hydraulic Power and Landing Gear – Replacement of Brake Accumulators No. 3 for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 10-Nov-2008
RecommendedRE (-)601-0597 (Hyd Sys 1) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 1 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 10-Nov-2008
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM111/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0597 (Hyd Sys 2) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 2 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 10-Nov-2008
RecommendedRE (-)601-0597 (Hyd Sys 3) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 3 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 10-Nov-2008
RecommendedRE (-)601-0597 Rev 1 Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 1, No. 2 and No. 3 and Brake Accumulators No. 2 and No. 3 or Part Nos
08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/F
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 1 (Brake 2)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 1 (Brake 3)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 1 (Hyd Sys 1)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 1 (Hyd Sys 2)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 1 (Hyd Sys 3)A/F29
RecommendedRE (-)601-0597 Rev 1 (Brake 2) Modification – Hydraulic Power and Landing Gear – Replacement of Brake Accumulators No. 2 for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 06-Jul-2009
RecommendedRE (-)601-0597 Rev 1 (Brake 3) Modification – Hydraulic Power and Landing Gear – Replacement of Brake Accumulators No. 3 for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 06-Jul-2009
RecommendedRE (-)601-0597 Rev 1 (Hyd Sys 1) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 1 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 06-Jul-2009
RecommendedRE (-)601-0597 Rev 1 (Hyd Sys 2) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 2 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 06-Jul-2009
RecommendedRE (-)601-0597 Rev 1 (Hyd Sys 3) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 3 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 06-Jul-2009
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM112/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0597 Rev 2 Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 1, No. 2 and No. 3 and Brake Accumulators No. 2 and No. 3 or Part Nos
08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/F
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 2 (Brake 2)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 2 (Brake 3)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 2 (Hyd Sys 1)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 2 (Hyd Sys 2)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 2 (Hyd Sys 3)A/F29
RecommendedRE (-)601-0597 Rev 2 (Brake 2) Modification – Hydraulic Power and Landing Gear – Replacement of Brake Accumulators No. 2 for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 10-May-2010
RecommendedRE (-)601-0597 Rev 2 (Brake 3) Modification – Hydraulic Power and Landing Gear – Replacement of Brake Accumulators No. 3 for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 10-May-2010
RecommendedRE (-)601-0597 Rev 2 (Hyd Sys 1) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 1 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 10-May-2010
RecommendedRE (-)601-0597 Rev 2 (Hyd Sys 2) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 2 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 10-May-2010
RecommendedRE (-)601-0597 Rev 2 (Hyd Sys 3) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 3 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 10-May-2010
RecommendedRE (-)601-0597 Rev 3 Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 1, No. 2 and No. 3 and Brake Accumulators No. 2 and No. 3 or Part Nos
08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/F
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 3 (Brake 2)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 3 (Brake 3)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 3 (Hyd Sys 1)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 3 (Hyd Sys 2)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 3 (Hyd Sys 3)A/F29
RecommendedRE (-)601-0597 Rev 3 (Brake 2) Modification – Hydraulic Power and Landing Gear – Replacement of Brake Accumulators No. 2 for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 10-Apr-2012
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM113/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0597 Rev 3 (Brake 3) Modification – Hydraulic Power and Landing Gear – Replacement of Brake Accumulators No. 3 for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 10-Apr-2012
RecommendedRE (-)601-0597 Rev 3 (Hyd Sys 1) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 1 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 10-Apr-2012
RecommendedRE (-)601-0597 Rev 3 (Hyd Sys 2) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 2 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 10-Apr-2012
RecommendedRE (-)601-0597 Rev 3 (Hyd Sys 3) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 3 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 10-Apr-2012
RecommendedT (A/R)601-0597 Rev 4 Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 1, No. 2 and No. 3 and Brake Accumulators No. 2 and No. 3 or Part Nos
08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 11-Jun-2015
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 4 (Brake 2)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 4 (Brake 3)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 4 (Hyd Sys 1)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 4 (Hyd Sys 2)A/F29
Nextdue Share EarliestDUE:1. RE -Modification – Hydraulic Power and Landing Gear – Replacemen...601-0597 Rev 4 (Hyd Sys 3)A/F29
RecommendedRE (-)601-0597 Rev 4 (Brake 2) Modification – Hydraulic Power and Landing Gear – Replacement of Brake Accumulators No. 2 for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 11-Jun-2015
RecommendedRE (-)601-0597 Rev 4 (Brake 3) Modification – Hydraulic Power and Landing Gear – Replacement of Brake Accumulators No. 3 for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 11-Jun-2015
RecommendedRE (-)601-0597 Rev 4 (Hyd Sys 1) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 1 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 11-Jun-2015
RecommendedRE (-)601-0597 Rev 4 (Hyd Sys 2) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 2 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 11-Jun-2015
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM114/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0597 Rev 4 (Hyd Sys 3) Modification – Hydraulic Power and Landing Gear – Replacement of System Accumulators No. 3 Hydraulic System for Part Nos 08-60163-002 and 08-60164-002
Mos
Hrs
Ldg
29 A/FEff: 11-Jun-2015
OptionalT (A/R)601-0618 Modification – No. 1 and No. 2 Main System – Replacement of the Hydraulic System No. 1 Accumulator
Mos
Hrs
Ldg
29 A/FEff: 14-May-2012
OptionalT (A/R)601-0619 Modification – No. 1 and No. 2 Main System – Replacement of the Hydraulic System No. 2 Accumulator
Mos
Hrs
Ldg
29 A/FEff: 14-May-2012
OptionalT (A/R)601-0620 Modification – No. 3 Main System – Replacement of the Hydraulic System No. 3 Accumulator
Mos
Hrs
Ldg
29 A/FEff: 14-May-2012
RecommendedT601-0633 Modification - No. 1 and No. 2 Main Systems - Relocation of the Hydraulic System No. 1 and No. 2 Accumulators
7.5 Years08-Oct-202396Mos
Hrs
Ldg
29 A/FEff: 08-Oct-2015
MandatoryRE (-)86-10-02 R1 Aileron And Elevator Flutter Dampers
18-Sep-1985Mos
Hrs
Ldg
29 A/FBY PART NUMBER INSTALLEDEff: 09-Feb-1990 Not
Applicable
MandatoryRE (-)86-10-02 R1 (1) Left Aileron Flutter Damper Fluid Check
18-Sep-1985Mos
Hrs
Ldg
29 A/FBY PART NUMBER INSTALLEDEff: 09-Feb-1990 Not
Applicable
MandatoryRE (-)86-10-02 R1 (2) Right Aileron Flutter Damper Fluid Check
18-Sep-1985Mos
Hrs
Ldg
29 A/FBY PART NUMBER INSTALLEDEff: 09-Feb-1990 Not
Applicable
MandatoryRE (-)86-10-02 R1 (3) Left Outboard Elevator Flutter Damper Fluid Check
18-Sep-1985Mos
Hrs
Ldg
29 A/FBY PART NUMBER INSTALLEDEff: 09-Feb-1990 Not
Applicable
MandatoryRE (-)86-10-02 R1 (4) Left Inboard Elevator Flutter Damper Fluid Check
18-Sep-1985Mos
Hrs
Ldg
29 A/FBY PART NUMBER INSTALLEDEff: 09-Feb-1990 Not
Applicable
MandatoryRE (-)86-10-02 R1 (5) Right Inboard Elevator Flutter Damper Fluid Check
18-Sep-1985Mos
Hrs
Ldg
29 A/FBY PART NUMBER INSTALLEDEff: 09-Feb-1990 Not
Applicable
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM115/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryRE (-)86-10-02 R1 (6) Right Outboard Elevator Flutter Damper Fluid Check
18-Sep-1985Mos
Hrs
Ldg
29 A/FBY PART NUMBER INSTALLEDEff: 09-Feb-1990 Not
Applicable
MandatoryRE (-)99-26-16 MLG Hydraulic And Fuel Lines
30-Dec-2002Mos
9,147Hrs
4,540Ldg
29 A/FSB 601-0482Eff: 01-Feb-2000 Complied
With
Compliance Share DoubleDUE:1. T A/R | 2. RE -Modification – Hydraulic Tubes, Main Landing Gear Bay - Inst...601-0482A/F29
AlertRE (-)A601-0082 Modification - No. 1 and 2 System Return Lines - Addition of Check Valve
20-Nov-1984Mos
Hrs
Ldg
29 A/FEff: 27-Aug-1984 Complied With
AlertT (A/R)A601-0108 Special Check/Modification - Hydraulic Line - Clearance with Left Main Wheel Bin
Mos
Hrs
Ldg
29 A/FEff: 24-Aug-1984
AlertT (A/R)A601-0138 Special Check/Modification - Tube Assemblies - Clearance
Mos
Hrs
Ldg
29 A/FEff: 15-Oct-1985
IsModSumT (A/R)IS600-29-0002 REV A Kit – Intro of Elbow Fitting on Ecology Bottle for the Hydraulic Resevoir #3
Mos
Hrs
Ldg
29 A/F
▼ 30 - ICE AND RAIN PROTECTION
RE (O/C)ADS Heater Control Unit
20-Sep-1983Mos
0Hrs
0Ldg
30 A/FUnknownUnknown
RE (O/C)Anti-Ice Controller
20-Sep-1983Mos
0Hrs
0Ldg
30 A/FUnknownUnknown
RE (O/C)Anti-Ice Modulating/Shutoff Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Left30 A/FNew3214442-3
N/A
RE (O/C)Anti-Ice Modulating/Shutoff Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Right30 A/FNew3214442-3
N/A
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM116/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Cowl Anti-Ice Pressure Switch
20-Sep-1983Mos
0Hrs
0Ldg
No.130 A/FUnknownUnknown
RE (O/C)Cowl Anti-Ice Pressure Switch
07-Jun-2003Mos
9,559.7Hrs
4,782Ldg
No.230 A/F98505-126811244
RE (O/C)Cowl Anti-Ice Valve
26-Mar-2007Mos
11,045.9Hrs
5,659Ldg
Left30 A/F300013000-0030284T
RE (O/C)Cowl Anti-Ice Valve
26-Mar-2005Mos
10,699.3Hrs
5,441Ldg
Right30 A/F734027B0496
RE (O/C)Ejector Interface Duct Assy
20-Sep-1983Mos
0Hrs0
0Ldg0
No.130 A/FNew228-56345-135
UNKNOWN
RE (O/C)Ejector Interface Duct Assy
20-Sep-1983Mos
0Hrs0
0Ldg0
No.230 A/FNew228-56345-135
UNKNOWN
RE (O/C)Ice Detector
20-Sep-1983Mos
0Hrs
0Ldg
No.130 A/FUnknownUnknown
RE (O/C)Ice Detector
20-Sep-1983Mos
0Hrs
0Ldg
No.230 A/FUnknownUnknown
RE (O/C)Over Pressure Relief Valve
28-Jan-2005Mos
10,580.3Hrs
5,376Ldg
Left30 A/F228-56480-801SB/3157
RE (O/C)Over Pressure Relief Valve
20-Sep-1983Mos
0Hrs
0Ldg
Right30 A/FUnknownUnknown
RE (O/C)Side Window Temperature Controller
20-Sep-1983Mos
0Hrs0
0Ldg0
Left30 A/FNew600-59100-13
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM117/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Side Window Temperature Controller
20-Sep-1983Mos
0Hrs0
0Ldg0
Right30 A/FNew600-59100-13
UNKNOWN
RE (O/C)Windshield Temperature Controller
20-Sep-1983Mos
0Hrs0
0Ldg0
Left30 A/FNew600-59100-11
UNKNOWN
RE (O/C)Windshield Temperature Controller
20-Sep-1983Mos
0Hrs0
0Ldg0
Right30 A/FNew600-59100-11
UNKNOWN
MandatoryRE (-)2005-04-07 Revision to Airplane Flight Manual (AFM) - New cold weather operations limitation - CANCELLED
20-Feb-2005Mos
10,595.3Hrs
5,386Ldg
30 A/FREVISED AFMEff: 22-Feb-2005 Complied
With
MandatoryRE (-)2008-08-06 Revision to Airplane Flight Manual (AFM) - New cold weather operations limitations - CANCELLED
25-Jul-2008Mos
11,432Hrs
5,881Ldg
30 A/FREVISED AFMEff: 21-Apr-2008 Complied
With
MandatoryRE (-)2008-21-09 Cold weather operation limitations
18-Mar-2009Mos
11,458.6Hrs
5,902Ldg
30 A/FFOUND P/C/WEff: 31-Oct-2008 Complied
With
MandatoryT (A/R)2009-06-05 Wing anti-ice piccolo duct failure
Mos
Hrs
Ldg
30 A/FEff: 28-Apr-2009
MandatoryRE (-)2009-06-05 R1 Wing anti-ice piccolo duct failure
17-Apr-2015Mos
11,905.8Hrs
6,221Ldg
30 A/FREPLACED ON 8/1/2000Eff: 28-Apr-2009 Complied
With
Nextdue Share EarliestDUE:1. T 1 Mos | 2. RE -Wing anti-ice piccolo duct failure - Airplane Flight Manual ...2009-06-05 R1 Paragraph (f) (1)A/F30
Nextdue Share EarliestDUE:1. RE -Wing anti-ice piccolo duct failure - Review the airplane mai...2009-06-05 R1 Paragraph (f) (2)A/F30
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Wing anti-ice piccolo duct failure - Identification of S/N's...2009-06-05 R1 Paragraph (f) (3)A/F30
MandatoryRE (-)2009-06-05 R1 Paragraph (f)
(1)
Wing anti-ice piccolo duct failure - Airplane Flight Manual (AFM) Revise
23-Sep-2009Mos
11,459.7Hrs
5,904Ldg
30 A/FREVISED AFMEff: 01-Apr-2010 Complied
With
(AVG MAN HRS: 37) (APX COST [USD]: 3,145)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM118/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryRE (-)2009-06-05 R1 Paragraph (f)
(2)
Wing anti-ice piccolo duct failure - Review the airplane maintenance records
Mos
Hrs
Ldg
30 A/FEff: 01-Apr-2010
Compliance Share SingleDUE:1. T A/R | 2. RE -Wing anti-ice piccolo duct failure - Identification of S/N's...2009-06-05 R1 Paragraph (f) (3)A/F30
MandatoryT (A/R)2009-06-05 R1 Paragraph (f)
(3)
Wing anti-ice piccolo duct failure - Identification of S/N's affected and Replacement
Mos
Hrs
Ldg
30 A/FEff: 01-Apr-2010
Compliance Share DoubleDUE: 12,932 Hrs1. T A/R | 2. RE -Special Check/Modification - Wing Anti-Icing - Anti-Ice Picc...601-0585A/F30
MandatoryRE (-)2011-09-09 Ice and Rain Protection and Pneumatic, respectively
13-May-2014Mos
11,839.6Hrs
6,172Ldg
30 A/FSB 590 NOT COMPLIED WITHEff: 19-Aug-2011 Not
Applicable
Not SetDUE:1. T A/R | 2. RE -Ice and Rain Protection and Pneumatic, respectively - Revise...2011-09-09 Paragraph (g)A/F30
Not SetDUE:1. T 4800 Hrs | 2. RE -Ice and Rain Protection and Pneumatic, respectively - Initia...2011-09-09 Paragraph (h)A/F30
MandatoryT (A/R)2011-09-09 Paragraph (g) Ice and Rain Protection and Pneumatic, respectively - Revise the Airworthiness Limitations Section of the Instructions for Continued Airworthiness
13-May-2014Mos
11,839.6Hrs
6,172Ldg
30 A/FSB 590 NOT COMPLIED WITHEff: 19-Aug-2011 Not
Applicable
MandatoryRE (-)2011-09-09 Paragraph (h) Ice and Rain Protection and Pneumatic, respectively - Initial Compliance Times for Airworthiness Limitations Tasks.
13-May-2014Mos
11,839.6Hrs
6,172Ldg
30 A/FSB 590 NOT COMPLIED WITHNot Applicable
AWLRE (N/A)30-11-00-101 * Wing Anti-Icing - Detailed Inspection of the Wing Duct Piccolo Tube (Post SB 601-0590)
Mos
Hrs
Ldg
30 A/F
(SOURCE: TLMC 05-10-30)
AWLRE (N/A)30-11-00-102 * Wing Anti-Icing - Functional Test of the Thermal Switches and Sensors (Post SB 601-0590)
Mos
Hrs
Ldg
30 A/F
(SOURCE: TLMC 05-10-30)
MRB ≈24-Oct-2017RE30-11-00-201 Wing Anti-Icing Check valve condition check
23-Oct-2004Mos
817.8 Hrs (+40)12,859-/+402,40010,459Hrs
Ldg
(PKG 2400 Hour)
30 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈29-Dec-2030RE30-11-00-202 Wing Anti-Icing Functional Test Wing Anti-Icing
05-Aug-2003Mos
7,144.4 Hrs (+40)(19,185.6)-/+409,6009,585.6Hrs
Ldg
(PKG 9600 Hour)
30 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM119/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE30-11-06-204 Wing Anti-Icing Ducting Visual Check of ducts, brackets, clamps and associated wiring, underfloor and in wing leading edge
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
30 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE30-11-06-212 Wing Anti-Ice Coupling (Pre SB 601-0433) Detailed inspection of the wing anti-ice expansion couplingbearings
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
30 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRBRE30-13-00-205 Anti-Icing Bleed Air Leak Detection Functional Test of thermal switches
5.8 Months (+30
Days)26-Sep-2016-/+112026-Sep-2006Mos
Hrs
Ldg
30 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE30-20-21-206 Nose Cowl Anti-Ice/Thrust Reverser Ducting Visual Check, paying particular attention for hot spots and discoloration
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
30 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈27-Jul-2016RE30-40-00-213 Windshield - Functional Test of the windshield rain repellant layer
30-Jan-2015Mos
221.5 Hrs12,262.740011,862.7Hrs
Ldg
Left30 A/F600-33030-259415
(SOURCE: TLMC 05-20-15) (NOTE: This task applies to Sully Glass Faceply Windshields, Part No. 270-462-00-XX and Sierracin Glass Faceply /
Windshields Part No. 158700-57 and Subs.)
MRB ≈27-Jul-2016RE30-40-00-213 Windshield - Functional Test of the windshield rain repellant layer
30-Jan-2015Mos
221.5 Hrs (+40)12,262.7-/+4040011,862.7Hrs
Ldg
Right30 A/F604-33030-2611030 REPAIR
(SOURCE: TLMC 05-20-15) (NOTE: This task applies to Sully Glass Faceply Windshields, Part No. 270-462-00-XX and Sierracin Glass Faceply /
Windshields Part No. 158700-57 and Subs.)
Servicing - Optional ≈25-Aug-2016RE30-40-00-301 Windshield/Side Window Aerodynamic Seal - Detailed Inspection
6.6 Months (+31
Days)21-Oct-2016-/+11221-Oct-2015Mos
259.9 Hrs (+40)12,301.1-/+4030012,001.1Hrs
6,291Ldg
30 A/F
(ZONE: 221, 223) (SOURCE: MPD 3.3)
MRB ≈20-Oct-2017RE30-41-00-210 Electrical Anti-Icing Functional Test of Heating Element - Functional Test of Sensors
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
30 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE30-41-16-211 Varistor Suppressor Nominal varistor voltage test - DC standby current test
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
30 A/F
Ref.:CMM/PSP 608/608A 30-40-01 (SOURCE: TLMC 05-20-15)
RecommendedRE (-)601-0015 Modification - Wing Anti-Icing System - Activation
Mos
Hrs
Ldg
30 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM120/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0015 Rev 1 Modification - Wing Anti-Icing System - Activation
Mos
Hrs
Ldg
30 A/FEff: 23-Apr-1984
RecommendedRE (-)601-0120 Modification - Anti-Ice System - Addition of Blocking Diodes
23-Mar-1992Mos
3,584Hrs
1,446Ldg
30 A/FEff: 02-Jul-1986 Complied With
OptionalRE (-)601-0142 Modification - Airfoil Anti-Icing - Removal of Guides
28-Oct-1988Mos
2,159Hrs
825Ldg
30 A/FEff: 06-May-1985 Complied With
RecommendedRE (-)601-0165 Modification - Windshield Anti-Icing and Demisting - Dual Heat Control
28-Mar-1989Mos
2,373Hrs
910Ldg
30 A/FEff: 28-Jul-1986 Complied With
RecommendedRE (-)601-0183 Modification - Anti-Ice Ducting - Insulation Boots
28-Mar-1989Mos
2,373Hrs
910Ldg
30 A/FEff: 11-Jun-1987 Complied With
RecommendedRE (-)601-0188 Modification - Leak Detection Elements - Dual Clip Assembly
28-Mar-1989Mos
2,373Hrs
910Ldg
30 A/FEff: 12-Mar-1987 Complied With
RecommendedRE (-)601-0190 Special Check/Rework - Bleed Air Leak Detector - Routing
28-Mar-1989Mos
2,373Hrs
910Ldg
30 A/FEff: 24-Sep-1986 Complied With
OptionalRE (-)601-0256 Modification - Ice Detector Light - Conversion for Certification
Mos
Hrs
Ldg
30 A/F
OptionalT (A/R)601-0256 Rev 1 Modification - Ice Detector Light - Conversion for Certification
Mos
Hrs
Ldg
30 A/FEff: 22-Feb-1991
RecommendedRE (-)601-0433 Modification - Wing Anti-Ice System - Coupling Assembly
Mos
Hrs
Ldg
30 A/F
RecommendedRE (-)601-0433 Rev 1 Modification - Wing Anti-Ice System - Coupling Assembly
26-Jan-1996Mos
4,785Hrs
1,932Ldg
30 A/FEff: 30-Nov-1995 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM121/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0471 Special Check/Rework - Wing Anti-Icing - Coupling/Boot-Cover Position at FS559.00
01-May-1996Mos
4,891Hrs
1,989Ldg
30 A/FEff: 15-Dec-1995 Complied With
Recommended ≈18-Dec-2017T (A/R)601-0585 Special Check/Modification - Wing Anti-Icing - Anti-Ice Piccolo Ducts Inspection/Replacement
Mos
890.8 Hrs[12,932]Hrs
Ldg
30 A/FEff: 30-Nov-2006
RecommendedRE (-)601-0608 Modification – Wing Anti-Icing – Take-Off Safety Enhancement (TOSE) Wing Anti-Ice Wiring Modification to Prevent Nuisance Indication on Take-Off
Mos
Hrs
Ldg
30 A/F
RecommendedT (A/R)601-0608 Rev 1 Modification – Wing Anti-Icing – Take-Off Safety Enhancement (TOSE) Wing Anti-Ice Wiring Modification to Prevent Nuisance Indication on Take-Off
Mos
Hrs
Ldg
30 A/FEff: 27-Jun-2011
RecommendedRE (-)601-1022 Special Check/Modification - Air Intake Anti-Icing - Valve Replacement
Mos
Hrs
Ldg
30 A/F
RecommendedT (A/R)601-1022 Rev 1 Special Check/Modification - Air Intake Anti-Icing - Valve Replacement
Mos
Hrs
Ldg
30 A/FEff: 02-Apr-1984
RecommendedRE (-)601-1064 Special Check/Modification - Anti-Ice System - Pressure Relief Valve
23-Feb-1990Mos
2,687Hrs
1,034Ldg
30 A/FEff: 28-Feb-1989 Complied With
AlertRE (-)A601-0008 Modification - Windshield Anti-Icing and Demisting - Addition of Suppressors
Mos
Hrs
Ldg
30 A/F
AlertRE (-)A601-0008 Rev 1 Modification - Windshield Anti-Icing and Demisting - Addition of Suppressors
Mos
Hrs
Ldg
30 A/FEff: 10-Feb-1984
AlertRE (-)A601-0556 Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tube and Connecting Duct Installation on Left and Right Wings
05-Aug-2003Mos
9,585.6Hrs
4,797Ldg
30 A/FEff: 24-Jan-2003 Complied With
Nextdue Share EarliestDUE:1. T 6 Mos, 250 Hrs | 2. RE -Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tub...A601-0556 Part AA/F30
Nextdue Share EarliestDUE:1. T 6 Mos, 250 Hrs | 2. RE -Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tub...A601-0556 Part BA/F30
Nextdue Share EarliestDUE:1. T 6 Mos, 250 Hrs | 2. RE -Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tub...A601-0556 Part CA/F30
Nextdue Share EarliestDUE:1. T 6 Mos, 250 Hrs | 2. RE -Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tub...A601-0556 Part DA/F30
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM122/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AlertRE (-)A601-0556 Part A Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tube and Connecting Duct Installation on Left and Right Wings
Mos
Hrs
Ldg
30 A/FEff: 23-Jan-2003
AlertRE (-)A601-0556 Part B Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tube and Connecting Duct Installation on Left and Right Wings
Mos
Hrs
Ldg
30 A/FEff: 23-Jan-2003
AlertRE (-)A601-0556 Part C Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tube and Connecting Duct Installation on Left and Right Wings
Mos
Hrs
Ldg
30 A/FEff: 23-Jan-2003
AlertRE (-)A601-0556 Part D Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tube and Connecting Duct Installation on Left and Right Wings
Mos
Hrs
Ldg
30 A/FEff: 23-Jan-2003
▼ 31 - INDICATING / RECORDING SYSTEM
RE (O/C)Aural Warning Test Panel
20-Sep-1983Mos
0Hrs
0Ldg
31 A/FUnknownUnknown
RE (O/C)Aural Warning Unit
30-Jan-2015Mos
11,862.7Hrs
6,194Ldg
31 A/F7001433-90182020233
RE (O/C)Circuit Breaker Box
20-Sep-1983Mos
0Hrs0
0Ldg0
31 A/FNew70-0197-3
UNKNOWN
RE (O/C)Dimming Module Assy
20-Sep-1983Mos
0Hrs
0Ldg
Copilot31 A/FUnknownUnknown
RE (O/C)Dimming Module Assy
20-Sep-1983Mos
0Hrs
0Ldg
Pilot31 A/FUnknownUnknown
RE (O/C)Flight Data Recorder (FDR)
20-Sep-1983Mos
0Hrs
0Ldg
31 A/FUnknownUnknown
Assembly SubDUE:1. RE N/AFlight Data Recorder (FDR) Underwater Locating DeviceUnknown / UnknownA/F31
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM123/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Life LimitRE (N/A)Flight Data Recorder (FDR) Underwater Locating Device
Mos
Hrs
Ldg
31 A/FUnknownUnknown
RE (O/C)Master Warning Caution Panel 10-Channel
07-Nov-2004Mos
10,460.5Hrs
5,308Ldg
31 A/F843347-3226
RE (O/C)Master Warning Caution Panel 8-Channel
20-Sep-1983Mos
0Hrs
0Ldg
31 A/FUnknownUnknown
MRB ≈03-May-2017RE31-51-00-201 Aural Warning System Operational Test of Fire Detection Warning (Bell) - Functional Test of: (1) Landing gear warning (Horn) / (2) Take-off configuration (TOC)
warning (Intermittent Horn)
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
31 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRBRE31-51-00-202 Aural Warning System Functional Test of: (1) Overspeed warning (Clacker) / (2) Flap overspeed warning (Wailer) (3) Altitude advisory (C Chord)
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
31 A/F
(SOURCE: TLMC 05-20-15)
RecommendedT (A/R)601-0119 Modification - Master Caution and Warning Light System - Legend Light Wiring
Mos
Hrs
Ldg
31 A/FEff: 20-Jan-1986
OptionalRE (-)601-0148 Modification - Master Caution and Warning System - Blocking Diode
26-Jan-1987Mos
1,267Hrs
480Ldg
31 A/FEff: 23-May-1985 Complied With
OptionalRE (-)601-0162 Modification - Master Caution and Warning System - Load Resistors
Mos
Hrs
Ldg
31 A/F
OptionalT (A/R)601-0162 Rev 1 Modification - Master Caution and Warning System - Load Resistors
Mos
Hrs
Ldg
31 A/FEff: 15-Apr-1992
RecommendedRE (-)601-0263 Modification - Pilots Facia Panel Flood Light - EMI Correction
21-Feb-1991Mos
3,142Hrs
1,250Ldg
31 A/FEff: 09-Feb-1989 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM124/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalT (A/R)601-0396 Modification - Aural Warning System - Take-off Configuration Warning (TOCW) Back Up
Mos
Hrs
Ldg
31 A/FEff: 15-Aug-1994
▼ 32 - LANDING GEAR
RE (O/C)Box Antiskid Control
15-Sep-2007Mos
11,184.3Hrs
5,748Ldg
32 A/F600-87000-103OCT92-0212
RE (O/C)Brake Control Valve
26-Jan-1996Mos
4,785Hrs
1,932Ldg
No.132 A/F600-75115-51542
RE (O/C)Brake Control Valve
26-Jan-1996Mos
4,785Hrs
1,932Ldg
No.232 A/F600-75115-51247
RE (O/C)Brake Hydraulic Accumulator
20-Sep-1983Mos
0Hrs
0Ldg
No.132 A/FUnknownUnknown
RE (O/C)Brake Hydraulic Accumulator
20-Sep-1983Mos
0Hrs
0Ldg
No.232 A/FUnknownUnknown
RE (O/C)Brake Hydraulic Fuse
20-Sep-1983Mos
0Hrs0
0Ldg0
No.132 A/FNew6190
UNKNOWN
RE (O/C)Brake Hydraulic Fuse
20-Sep-1983Mos
0Hrs0
0Ldg0
No.232 A/FNew6190
UNKNOWN
RE (O/C)Brake Hydraulic Fuse
20-Sep-1983Mos
0Hrs0
0Ldg0
No.332 A/FNew6190
UNKNOWN
RE (O/C)Brake Hydraulic Fuse
20-Sep-1983Mos
0Hrs0
0Ldg0
No.432 A/FNew6190
UNKNOWN
RE (O/C)Brake Pressure Indicator
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM125/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Brake Pressure Transducer
20-Sep-1983Mos
0Hrs
0Ldg
Left32 A/FUnknownUnknown
RE (O/C)Brake Pressure Transducer
20-Sep-1983Mos
0Hrs
0Ldg
Right32 A/FUnknownUnknown
RE (O/C)Extension and Retraction - Main Landing Gear Selector Valve
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
Component Inspection Tso To
TsiDUE:1. RE N/AExtension and Retraction - Main Landing Gear Selector Valve ...32-00-00-245A/F32
AWL - Life LimitRE (O/C)Hydraulic Accumulator Assy
20-Sep-1983Mos
0Hrs
0Ldg
No.132 A/FUnknownUnknown
AWL - Life LimitRE (O/C)Hydraulic Accumulator Assy
20-Sep-1983Mos
0Hrs
0Ldg
No.232 A/FUnknownUnknown
AWL - Life LimitRE (O/C)Hydraulic Accumulator Assy
20-Sep-1983Mos
0Hrs
0Ldg
No.332 A/FUnknownUnknown
AWL - Life LimitRE (O/C)Hydraulic Brake Control Valve
26-Jan-1996Mos
4,785Hrs0
1,932Ldg0
No.132 A/FNew600-75115-5
1542
AWL - Life LimitRE (O/C)Hydraulic Brake Control Valve
26-Jan-1996Mos
4,785Hrs0
1,932Ldg0
No.232 A/FNew600-75115-5
1247
RE (O/C)Inboard Brake Anti-Skid Valve
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
RE (O/C)Landing Gear Unit Control
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM126/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Main Gear Beam
20-Sep-1983Mos
0Hrs
0Ldg
Left32 A/FUnknownUnknown
RE (O/C)Main Gear Beam
20-Sep-1983Mos
0Hrs
0Ldg
Right32 A/FUnknownUnknown
RE (O/C)Main Landing Gear Assembly
22-Mar-2012Mos
Hrs
6,004Ldg2,278
Left32 A/FOverhauled601-85082-7
DCL272/00
Component Inspection SimpleDUE: 22-Mar-20171. RE 60 MosMain Landing Gear Assembly - Detailed Inspection32-10-00-237A/F32
Component Inspection Tso To
TsiDUE: 22-Mar-20221. RE 120 MosMain Landing Gear Assembly - Restoration32-10-00-238A/F32
RE (O/C)Main Landing Gear Assembly
22-Mar-2012Mos
Hrs
6,004Ldg2,278
Right32 A/FOverhauled601-85082-8
DCL269/00
Component Inspection SimpleDUE: 22-Mar-20171. RE 60 MosMain Landing Gear Assembly - Detailed Inspection32-10-00-237A/F32
Component Inspection Tso To
TsiDUE: 22-Mar-20221. RE 120 MosMain Landing Gear Assembly - Restoration32-10-00-238A/F32
RE (O/C)Main Wheel Assy
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
Left Inboard32 A/F5009029-1JAN93-0617
Assembly SubDUE:1. RE O/CMain Wheel TireUnknown / UnknownA/F32
Component Inspection SimpleDUE:1. RE T/CMain Wheel - NDT Check32-41-11-231A/F32
Component Inspection SimpleDUE: 6,358 Ldg1. T 1600 Ldg | 2. RA 1600 Ldg | 3. RA 1600 Ldg | 4. RE
800 LdgMain Wheel - Carry out all maintenance requirements in the “...32-41-11-232A/F32
RE (O/C)Main Wheel Assy
25-Jul-2008Mos
11,432Hrs
5,881Ldg
Left Outboard32 A/F5007045-2JAN84-235
Assembly SubDUE:1. RE O/CMain Wheel TireUnknown / UnknownA/F32
Assembly SubDUE:1. RE O/CMain Wheel TireUnknown / UnknownA/F32
Component Inspection SimpleDUE:1. RE T/CMain Wheel - NDT Check32-41-11-231A/F32
Component Inspection SimpleDUE: 6,681 Ldg1. T 1600 Ldg | 2. RA 1600 Ldg | 3. RA 1600 Ldg | 4. RE
800 LdgMain Wheel - Carry out all maintenance requirements in the “...32-41-11-232A/F32
Component Inspection SimpleDUE: 6,681 Ldg1. T 1600 Ldg | 2. RA 1600 Ldg | 3. RA 1600 Ldg | 4. RE
800 LdgMain Wheel - Carry out all maintenance requirements in the “...32-41-11-232A/F32
RE (O/C)Main Wheel Assy
25-Jul-2008Mos
11,432Hrs
5,881Ldg
Right Inboard32 A/F5009029-1JUN85-R494
Component Inspection SimpleDUE:1. RE T/CMain Wheel - NDT Check32-41-11-231A/F32
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM127/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Main Wheel Assy
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
Right Outboard32 A/F5009029-1NOV95-1044
Assembly SubDUE:1. RE O/CMain Wheel TireUnknown / UnknownA/F32
Component Inspection SimpleDUE:1. RE T/CMain Wheel - NDT Check32-41-11-231A/F32
Component Inspection SimpleDUE: 6,358 Ldg1. T 1600 Ldg | 2. RA 1600 Ldg | 3. RA 1600 Ldg | 4. RE
800 LdgMain Wheel - Carry out all maintenance requirements in the “...32-41-11-232A/F32
RE (O/C)Main Wheel Brake Unit
28-Jun-2004Mos
10,421.6Hrs
5,281Ldg
Left Inboard32 A/F5009027-5UNKNOWN
Component Inspection SimpleDUE:1. RE T/CMain Wheel Brake Unit - Brake channel check32-43-11-220A/F32
RE (O/C)Main Wheel Brake Unit
28-Jun-2004Mos
10,421.6Hrs
5,281Ldg
Left Outboard32 A/F5009027-5AUG82-495
Component Inspection SimpleDUE:1. RE T/CMain Wheel Brake Unit - Brake channel check32-43-11-220A/F32
RE (O/C)Main Wheel Brake Unit
28-Jun-2004Mos
10,421.6Hrs
5,281Ldg
Right Inboard32 A/F5009027-5OCT83-691
Component Inspection SimpleDUE:1. RE T/CMain Wheel Brake Unit - Brake channel check32-43-11-220A/F32
RE (O/C)Main Wheel Brake Unit
04-Dec-2003Mos
9,966.7Hrs
5,011Ldg
Right Outboard32 A/F5009027-5MAY82-426
Component Inspection SimpleDUE:1. RE T/CMain Wheel Brake Unit - Brake channel check32-43-11-220A/F32
AWL - Life LimitRE (O/C)Main Wheel Tire
20-Sep-1983Mos
0Hrs
0Ldg
Left Inboard32 A/FUnknownUnknown
AWL - Life LimitRE (O/C)Main Wheel Tire
20-Sep-1983Mos
0Hrs
0Ldg
Left Outboard32 A/FUnknownUnknown
AWL - Life LimitRE (O/C)Main Wheel Tire
20-Sep-1983Mos
0Hrs
0Ldg
Right Inboard32 A/FUnknownUnknown
AWL - Life LimitRE (O/C)Main Wheel Tire
20-Sep-1983Mos
0Hrs
0Ldg
Right Outboard32 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM128/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL - Life Limit ≈10-Oct-2147REMLG Axle
22-Mar-2012Mos
Hrs
47,400 Ldg53,72650,0006,004Ldg2,278
Left32 A/FOverhauled6433-1
MBM1029
AWL - Life Limit ≈10-Oct-2147REMLG Axle
22-Mar-2012Mos
Hrs
47,400 Ldg53,72650,0006,004Ldg2,278
Right32 A/FOverhauled6433-1
MBM1050
AWL - Life Limit ≈31-Oct-2016REMLG Door Hinge Fasteners
17-May-2013Mos
347.6 Hrs12,388.860011,788.8Hrs0
6,143Ldg0
Left32 A/FNew104467705
UNKNOWN
(NOTE: (Hinge Sector 600-31587-1/-2 not installed))
AWL - Life Limit ≈31-Oct-2016REMLG Door Hinge Fasteners
17-May-2013Mos
347.6 Hrs12,388.860011,788.8Hrs0
6,143Ldg0
Right32 A/FNew104467705
UNKNOWN
(NOTE: (Hinge Sector 600-31587-1/-2 not installed))
AWL - Life Limit ≈10-Oct-2147REMLG Door Stud
22-Mar-2012Mos
Hrs
47,400 Ldg53,72650,0006,004Ldg2,278
Left32 A/FOverhauled6349-1
1-3013/12
AWL - Life Limit ≈10-Oct-2147REMLG Door Stud
22-Mar-2012Mos
Hrs
47,400 Ldg53,72650,0006,004Ldg2,278
Right32 A/FOverhauled6349-1
2-3013/12
RE (O/C)MLG Downlock Assist Actuator
20-Sep-1983Mos
0Hrs0
0Ldg0
Left32 A/FNew600-85001-29
UNKNOWN
RE (O/C)MLG Downlock Assist Actuator
20-Sep-1983Mos
0Hrs0
0Ldg0
Right32 A/FNew600-85001-29
UNKNOWN
AWL - Life Limit ≈15-Sep-2179REMLG Eye Bolt
22-Mar-2012Mos
Hrs
58,895 Ldg65,22163,5366,004Ldg4,319
Left32 A/FOverhauled9025-1
DCL358
AWL - Life Limit ≈10-Oct-2182REMLG Eye Bolt
22-Mar-2012Mos
Hrs
60,997 Ldg67,32363,5366,004Ldg2,217
Right32 A/FOverhauled9025-1
MBM1083
AWL - Life LimitRE (O/C)MLG Main Fitting
20-Sep-1983Mos
0Hrs
0Ldg
Left32 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM129/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL - Life LimitRE (O/C)MLG Main Fitting
20-Sep-1983Mos
0Hrs
0Ldg
Right32 A/FUnknownUnknown
AWL - Life Limit ≈06-Jan-2137REMLG Main Fitting Assy
22-Mar-2012Mos
Hrs
43,526 Ldg49,85246,1266,004Ldg2,278
Left32 A/FOverhauled6316-217
DER-1035
Assembly SubDUE:1. RE O/CMLG Main FittingUnknown / UnknownA/F32
AWL - Life Limit ≈06-Jan-2137REMLG Main Fitting Assy
22-Mar-2012Mos
Hrs
43,526 Ldg49,85246,1266,004Ldg2,278
Right32 A/FOverhauled6316-10
DER-1047
Assembly SubDUE:1. RE O/CMLG Main FittingUnknown / UnknownA/F32
AWL - Life Limit ≈24-Jun-2141REMLG Pintle Pin
22-Mar-2012Mos
Hrs
45,134 Ldg51,46047,7346,004Ldg2,278
Left32 A/FOverhauled6324-1
MBM0704
AWL - Life Limit ≈24-Jun-2141REMLG Pintle Pin
22-Mar-2012Mos
Hrs
45,134 Ldg51,46047,7346,004Ldg2,278
Right32 A/FOverhauled6324-1
PLT1010
AWL - Life Limit ≈10-Oct-2147REMLG Pivot Pin
22-Mar-2012Mos
Hrs
47,400 Ldg53,72650,0006,004Ldg2,278
Left32 A/FOverhauled6329-3
MBM0537
AWL - Life Limit ≈10-Oct-2147REMLG Pivot Pin
22-Mar-2012Mos
Hrs
47,400 Ldg53,72650,0006,004Ldg2,278
Right32 A/FOverhauled6329-3
MBM0524
RE (O/C)MLG Shock Strut
22-Mar-2012Mos
Hrs
6,004Ldg2,278
Left32 A/FOverhauled601-85001-25
DCL552/00
RE (O/C)MLG Shock Strut
22-Mar-2012Mos
Hrs
6,004Ldg2,278
Right32 A/FOverhauled601-85001-25
DCL553/00
AWL - Life Limit ≈10-Oct-2147REMLG Shock Strut Cylinder
22-Mar-2012Mos
Hrs
47,400 Ldg53,72650,0006,004Ldg2,278
Left32 A/FOverhauled6216-1
DER1022
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM130/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL - Life Limit ≈10-Oct-2147REMLG Shock Strut Cylinder
22-Mar-2012Mos
Hrs
47,400 Ldg53,72650,0006,004Ldg2,278
Right32 A/FOverhauled6216-1
DER1007
AWL - Life Limit ≈10-Oct-2147REMLG Shock Strut Lower Pin
22-Mar-2012Mos
Hrs
47,400 Ldg53,72650,0006,004Ldg2,278
Left32 A/FOverhauled6232-1
DCL007
AWL - Life Limit ≈10-Oct-2147REMLG Shock Strut Lower Pin
22-Mar-2012Mos
Hrs
47,400 Ldg53,72650,0006,004Ldg2,278
Right32 A/FOverhauled6232-1
2-3013/06
AWL - Life Limit ≈10-Oct-2147REMLG Shock Strut Piston
22-Mar-2012Mos
Hrs
47,400 Ldg53,72650,0006,004Ldg2,278
Left32 A/FOverhauled6226-3
DCL618
AWL - Life Limit ≈10-Oct-2147REMLG Shock Strut Piston
22-Mar-2012Mos
Hrs
47,400 Ldg53,72650,0006,004Ldg2,278
Right32 A/FOverhauled6226-3
DCL622
AWL - Life Limit ≈21-Sep-2148REMLG Shock Strut Upper Pin
22-Mar-2012Mos
Hrs
47,741 Ldg54,06750,3416,004Ldg2,278
Left32 A/FOverhauled6232-3
MBM0071
AWL - Life Limit ≈23-Oct-2153REMLG Shock Strut Upper Pin
26-Sep-2006Mos
10,897.5Hrs0
49,573 Ldg55,89950,3415,558Ldg0
Right32 A/FNew6232-3
UNKNOWN
AWL - Life Limit ≈21-May-2092REMLG Side Brace to A/C Fitting Pin
22-Mar-2012Mos
Hrs
27,461 Ldg33,78730,0006,004Ldg2,217
Left32 A/FOverhauled600-10237-3
1-3013/12
AWL - Life Limit ≈21-May-2092REMLG Side Brace to A/C Fitting Pin
22-Mar-2012Mos
Hrs
27,461 Ldg33,78730,0006,004Ldg2,217
Right32 A/F600-10237-12-3013/12
RE (O/C)MLG Side Stay (W/ Harness) Actuator Assembly
22-Mar-2012Mos
Hrs
6,004Ldg4,319
Left32 A/FOverhauled600-85001-85
DCL114/89/95
RE (O/C)MLG Side Stay (W/ Harness) Actuator Assembly
22-Mar-2012Mos
Hrs
6,004Ldg8,072
Right32 A/FOverhauled600-85001-85
DCL104/89/00R
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM131/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL - Life Limit ≈09-Feb-2142REMLG Side Stay Cylinder
22-Mar-2012Mos
Hrs
45,359 Ldg51,68550,0006,004Ldg4,319
Left32 A/FOverhauled104467734
DCL328
AWL - Life Limit ≈11-Dec-2147REMLG Side Stay Cylinder
22-Mar-2012Mos
Hrs
47,461 Ldg53,78750,0006,004Ldg2,217
Right32 A/FOverhauled104467734
DER1052
AWL - Life Limit ≈11-Jan-2130REMLG Side Stay Pin
22-Mar-2012Mos
Hrs
41,011 Ldg47,33743,6116,004Ldg2,278
Left32 A/FOverhauled6318-3
MBM2111
AWL - Life Limit ≈11-Jan-2130REMLG Side Stay Pin
22-Mar-2012Mos
Hrs
41,011 Ldg47,33743,6116,004Ldg2,278
Right32 A/FOverhauled6318-3
MBM2143
AWL - Life Limit ≈03-Nov-2138REMLG Side Stay Piston Rod
22-Mar-2012Mos
Hrs
44,183 Ldg50,50950,0006,004Ldg5,495
Left32 A/FOverhauled104467816
DCL352
AWL - Life Limit ≈06-Sep-2131REMLG Side Stay Piston Rod
22-Mar-2012Mos
Hrs
41,606 Ldg47,93250,0006,004Ldg8,072
Right32 A/FOverhauled104467816
DCL308
AWL - Life Limit ≈10-Oct-2147REMLG Trailing Arm
22-Mar-2012Mos
Hrs
47,400 Ldg53,72650,0006,004Ldg2,278
Left32 A/FOverhauled6416-1
DCL641
AWL - Life Limit ≈10-Oct-2147REMLG Trailing Arm
22-Mar-2012Mos
Hrs
47,400 Ldg53,72650,0006,004Ldg2,278
Right32 A/FOverhauled6416-1
MBM1021
AWL - Life Limit ≈02-Jan-2168REMLG Uplock Actuator Assembly
20-Sep-1983Mos
0Hrs0
54,682 Ldg61,00861,0080Ldg0
Left32 A/FNew200815001
UNKNOWN
AWL - Life Limit ≈02-Jan-2168REMLG Uplock Actuator Assembly
20-Sep-1983Mos
0Hrs0
54,682 Ldg61,00861,0080Ldg0
Right32 A/FNew200815001
UNKNOWN
AWL - Life Limit ≈31-Dec-2062RENLG Attachment Pin (Main Fitting to Drag Brace)
22-Mar-2012Mos
Hrs
16,880 Ldg23,20619,4806,004Ldg2,278
32 A/FOverhauled200811721
MY808750
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM132/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL - Life LimitRE (O/C)NLG Axle Assy
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
Assembly SubDUE: 23,206 Ldg1. RE 19480 LdgNLG Axle Fitting200811308 / DCL0606A/F32
AWL - Life Limit ≈31-Dec-2062RENLG Axle Fitting
22-Mar-2012Mos
Hrs
16,880 Ldg23,20619,4806,004Ldg2,278
32 A/FOverhauled200811308
DCL0606
RE (O/C)NLG Drag Brace Assembly
22-Mar-2012Mos
Hrs
6,004Ldg2,278
32 A/FOverhauled600-85002-45
DCL284/00
AWL - Life Limit ≈31-Dec-2062RENLG Drag Brace Lower Link
22-Mar-2012Mos
Hrs
16,880 Ldg23,20619,4806,004Ldg2,278
32 A/FOverhauled200811311
MIL-0011
AWL - Life Limit ≈31-Dec-2062RENLG Drag Brace Upper Hinge Pin
22-Mar-2012Mos
Hrs
16,880 Ldg23,20619,4806,004Ldg2,278
32 A/FOverhauled200814624
PEG1141
AWL - Life Limit ≈31-Dec-2062RENLG Drag Brace Upper Link
22-Mar-2012Mos
Hrs
16,880 Ldg23,20619,4806,004Ldg2,278
32 A/FOverhauled7202-3
DER-1030
AWL - Life Limit ≈31-Dec-2062RENLG Drag Brace Upper Pivot Pin
22-Mar-2012Mos
Hrs
16,880 Ldg23,20619,4806,004Ldg2,278
Left32 A/FOverhauled200814601
PEG1051
AWL - Life Limit ≈31-Dec-2062RENLG Drag Brace Upper Pivot Pin
22-Mar-2012Mos
Hrs
16,880 Ldg23,20619,4806,004Ldg2,278
Right32 A/FOverhauled200814601
PEG1093
AWL - Life Limit ≈31-Dec-2062RENLG Main Fitting
22-Mar-2012Mos
Hrs
16,880 Ldg23,20619,4806,004Ldg2,278
32 A/FOverhauled200811316
TA1071
AWL - Life Limit ≈31-Dec-2062RENLG Pivot (Trunion) Pin
22-Mar-2012Mos
Hrs
16,880 Ldg23,20619,4806,004Ldg2,278
Left32 A/FOverhauled200811601
1/3013/12
AWL - Life Limit ≈31-Dec-2062RENLG Pivot (Trunion) Pin
22-Mar-2012Mos
Hrs
16,880 Ldg23,20619,4806,004Ldg2,278
Right32 A/FOverhauled200811601
2/3013/12
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM133/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)NLG Proximity Switch
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
RE (O/C)NLG Retraction Actuator
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
RE (O/C)NLG Retraction Actuator, Lower Pin
20-Sep-1983Mos
0Hrs0
0Ldg0
32 A/FNew200811773
UNKNOWN
RE (O/C)NLG Shock Strut
22-Mar-2012Mos
Hrs
6,004Ldg2,278
32 A/FOverhauled601-85002-13
DCL376/00
AWL - Life Limit ≈31-Dec-2062RENLG Shock Strut Sliding Tube
22-Mar-2012Mos
Hrs
16,880 Ldg23,20619,4806,004Ldg2,278
32 A/FOverhauled200811707
MBM0106
AWL - Life Limit ≈28-Apr-2069RENLG Sliding Tube to End Fitting Pin
22-Mar-2012Mos
Hrs0
19,158 Ldg25,48419,4806,004Ldg0
32 A/FNew200811602
11EXC0593
RE (O/C)NLG Steering Compensator
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
RE (O/C)NLG Steering Selector Valve
23-Feb-2003Mos
9,253.9Hrs
4,606Ldg
32 A/F150446002576
AWL - Life Limit ≈28-Feb-2143RENLG Uplock Assy
20-Sep-1983Mos
0Hrs0
45,739 Ldg52,06552,0650Ldg0
32 A/FNew600-85002-9
UNKNOWN
RE (O/C)Nose Landing Gear Assembly
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
Component Inspection SimpleDUE:1. RE 60 MosNose Landing Gear Assembly - Detailed Inspection32-20-00-239A/F32
Component Inspection Tso To
TsiDUE: 24-Oct-20211. RE 120 MosNose Landing Gear Assembly - Detailed Inspection32-20-00-240A/F32
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM134/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Nose Landing Gear Doors Actuator
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
RE (O/C)Nose Landing Gear Selector Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
No.132 A/FNew55540-2
UNKNOWN
RE (O/C)Nose Landing Gear Selector Valve
27-Apr-2002Mos
8,378.4Hrs
4,058Ldg
No.232 A/F55540-5250
RE (O/C)Nose Wheel Assy
15-Sep-2007Mos
11,184.3Hrs
5,748Ldg
Left32 A/F5006450-1MAR98-8484
Assembly SubDUE:1. RE O/CNose Wheel Tire184F23-2 / 60581162A/F32
Component Inspection SimpleDUE:1. RE T/CNose Wheel (Part Number 600-85003 All Dash Numbers) - NDT Ch...32-41-16-234A/F32
Component Inspection SimpleDUE: 6,358 Ldg1. T 1600 Ldg | 2. RA 1600 Ldg | 3. RA 1600 Ldg | 4. RE
800 LdgNose Wheel (Part Number 600-85003 All Dash Numbers) - Carry ...32-41-16-235A/F32
RE (O/C)Nose Wheel Assy
15-Sep-2007Mos
11,184.3Hrs
5,748Ldg
Right32 A/F5006450-1MAY90-0599
Assembly SubDUE:1. RE O/CNose Wheel Tire184F23-2 / 60581160A/F32
Component Inspection SimpleDUE:1. RE T/CNose Wheel (Part Number 600-85003 All Dash Numbers) - NDT Ch...32-41-16-234A/F32
Component Inspection SimpleDUE: 6,358 Ldg1. T 1600 Ldg | 2. RA 1600 Ldg | 3. RA 1600 Ldg | 4. RE
800 LdgNose Wheel (Part Number 600-85003 All Dash Numbers) - Carry ...32-41-16-235A/F32
RE (O/C)Nose Wheel Tire
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
Left32 A/F184F23-260581162
RE (O/C)Nose Wheel Tire
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
Right32 A/F184F23-260581160
RE (O/C)Nosewheel Steering Handwheel
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
RE (O/C)Nosewheel Steering, Electronic Control Module
20-Sep-1983Mos
0Hrs0
0Ldg0
32 A/FNew7040-11
UNKNOWN
Component Inspection SimpleDUE:1. RE 600 HrsNosewheel Steering - Functional test of Electronic Control M...32-50-00-236A/F32
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM135/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (A/R)NW Steering Arming Valve
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
RE (O/C)NWS Control Manifold
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
RE (O/C)Outboard Brake Anti-Skid Valve
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
RE (O/C)Parking Brake SOV Valve
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
RE (O/C)Proximity Switch
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
RE (O/C)Proximity Switch
05-Mar-2008Mos
11,387.8Hrs
5,856Ldg
Left Inboard32 A/F256K43-370377113
RE (O/C)Proximity Switch
25-Jul-2008Mos
11,432Hrs
5,881Ldg
Left Outboard32 A/F256K43-380727106
RE (O/C)Proximity Switch
25-Jul-2008Mos
11,432Hrs
5,881Ldg
Right Inboard32 A/F256K43-380767095
RE (O/C)Proximity Switch
05-Mar-2008Mos
11,387.8Hrs
5,856Ldg
Right Outboard32 A/F256K43-361657040
RE (O/C)Sector Mlg Door Hinge
20-Sep-1983Mos
0Hrs0
0Ldg0
Left32 A/FNew600-31195-7
UNKNOWN
RE (O/C)Sector Mlg Door Hinge
20-Sep-1983Mos
0Hrs0
0Ldg0
Right32 A/FNew600-31195-8
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM136/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Sensor, Nosewheel Steering, RVT
20-Sep-1983Mos
0Hrs
0Ldg
NLG32 A/FUnknownUnknown
AWL - Life Limit ≈24-Aug-2052RESliding Tube/End Fitting Special Bolt
20-Sep-1983Mos
0Hrs
13,154 Ldg19,48019,4800Ldg0
32 A/FUnknownUnknown
RE (O/C)Steering Potentiometer Control
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FUnknownUnknown
RE (O/C)Wheel Speed - Anti-Skid System Sensor
15-Sep-2007Mos
11,184.3Hrs
5,748Ldg
Left Inboard32 A/F600-87000-5JUN89-3019
RE (O/C)Wheel Speed - Anti-Skid System Sensor
15-Sep-2007Mos
11,184.3Hrs
5,748Ldg
Left Outboard32 A/F600-87000-5JAN81-1404
RE (O/C)Wheel Speed - Anti-Skid System Sensor
20-Sep-1983Mos
0Hrs
0Ldg
Right Inboard32 A/FUnknownUnknown
RE (O/C)Wheel Speed - Anti-Skid System Sensor
26-Mar-2007Mos
11,045.9Hrs
5,659Ldg
Right Outboard32 A/F6002504NOV86-1835
MandatoryRE (-)2000-19-01 Main Landing Gear
22-Mar-2001Mos
7,444.3Hrs
3,496Ldg
32 A/FSB 601-0024Eff: 25-Oct-2000 Complied
With
MandatoryRE (-)2000-24-01 Main Landing Gear Wheel Bay Protection Shields
31-Dec-2002Mos
9,154.3Hrs
4,543Ldg
32 A/FSB 601-0507Eff: 19-Dec-2000 Complied
With
Compliance Share DoubleDUE:1. T A/R | 2. RE -Modification - Main Landing Gear Bay Fairing - Add a Protect...601-0507A/F53
MandatoryRE (-)2005-15-04 Landing gear parts
11-Nov-2015Mos
12,012.8Hrs
6,303Ldg
32 A/F03/09/2012, 11578.6 previouslyEff: 30-Aug-2005 Complied
With
(NOTE: Superseded By FAA AD 2014-15-13)
Nextdue Share EarliestDUE:1. RE -Landing gear parts - Add Serial Numbers or Part Numbers2005-15-04 Paragraph (f)(1)A/F32
Nextdue Share EarliestDUE:1. RE -Landing gear parts - Add Serial Numbers or Part Numbers2005-15-04 Paragraph (f)(2)A/F32
Nextdue Share EarliestDUE:1. RE -Landing gear parts - Revise the Airworthiness Limitations Se...2005-15-04 Paragraph (h)A/F32
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM137/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryRE (-)2005-15-04 Paragraph (f)(1) Landing gear parts - Add Serial Numbers or Part Numbers
Mos
Hrs
Ldg
32 A/FEff: 30-Aug-2005
Compliance Share DoubleDUE:1. T A/R | 2. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 3A/F32
MandatoryRE (-)2005-15-04 Paragraph (f)(2) Landing gear parts - Add Serial Numbers or Part Numbers
Mos
Hrs
Ldg
32 A/FEff: 30-Aug-2005
Compliance Share DoubleDUE:1. T A/R | 2. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 3A/F32
MandatoryRE (-)2005-15-04 Paragraph (h) Landing gear parts - Revise the Airworthiness Limitations Section (ALS)
Mos
Hrs
Ldg
32 A/FEff: 30-Aug-2005
MandatoryRE (-)2007-14-02 Uncommanded partial retractions of the nose landing gear (NLG) - Prevent internal leakage of the selector valve - CANCELLED
25-Jul-2008Mos
11,432Hrs
5,881Ldg
32 A/FBY PART NUMBER INSTALLEDEff: 16-Aug-2007 Not
Applicable
MandatoryRE (-)2010-10-26 Landing Gear
02-Dec-2009Mos
11,460.7Hrs
5,905Ldg
32 A/FFOUND P/C/WEff: 25-Jun-2010 Complied
With
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Rework - Extension and Retraction - End Caps o...601-0558 Rev 3A/F32
MandatoryRE (-)2014-15-13 Landing Gear
23-Dec-2014Mos
11,855.8Hrs
6,191Ldg
32 A/F03/09/12, 11578.6 previouslyEff: 25-Sep-2014 Complied
With
Nextdue Share EarliestDUE:1. T 60 Mos | 2. RE -Landing Gear - add serial numbers and part numbers, as appl...2014-15-13 Paragraph (g)(1)A/F32
Nextdue Share EarliestDUE:1. T 120 Mos | 2. RE -Landing Gear - add serial numbers and part numbers, as appl...2014-15-13 Paragraph (g)(2)A/F32
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Landing Gear - if a component does not have a serial numbe...2014-15-13 Paragraph (h)A/F32
Nextdue Share EarliestDUE:1. RE -Landing Gear - ALS Revision2014-15-13 Paragraph (i)A/F32
Nextdue Share EarliestDUE: 25-Sep-20191. T 60 Mos | 2. RE -Landing Gear - add serial numbers and part numbers, to to l...2014-15-13 Paragraph (l) (2)A/F32
Nextdue Share EarliestDUE: 25-Sep-20241. T 120 Mos | 2. RE -Landing Gear - add serial numbers and part numbers, as appli...2014-15-13 Paragraph (l) (3)A/F32
MandatoryRE (-)2014-15-13 Paragraph (g)(1) Landing Gear - add serial numbers and part numbers, as applicable, to the parts identified in Part A of the applicable service bulletin.
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
32 A/FASB A600-0710,A601-0546Eff: 30-Aug-2005 Complied
With
Compliance Share DoubleDUE:1. T A/R | 2. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 3A/F32
MandatoryRE (-)2014-15-13 Paragraph (g)(2) Landing Gear - add serial numbers and part numbers, as applicable, to the parts identified in Part B of the applicable service bulletin.
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
32 A/FASB A600-0710,A601-0546Eff: 30-Aug-2005 Complied
With
Compliance Share DoubleDUE:1. T A/R | 2. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 3A/F32
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM138/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryT (A/R)2014-15-13 Paragraph (h) Landing Gear - if a component does not have a serial number and the CSN or TSN were not tracked, use the formula in the applicable Messier-Dowty service bulletin
to paragraph (g) of this AD to establish the TSN or CSN, and record the newly calculated TSN or CSN.in the airplane log books.
Mos
Hrs
Ldg
32 A/FEff: 25-Sep-2014
MandatoryRE (-)2014-15-13 Paragraph (i) Landing Gear - ALS Revision
26-Sep-2006Days
10,897.5Hrs
5,558Ldg
32 A/FASB A600-0710,A601-0546Eff: 30-Aug-2005 Complied
With
MandatoryT2014-15-13 Paragraph (l) (2) Landing Gear - add serial numbers and part numbers, to to left and right MLG side strut pins having P/N 6318-1 or 6318-3; and to left and right MLG hinge pins having
P/N 6329-3
3.5 Years25-Sep-201960Mos
Hrs
Ldg
32 A/FEff: 25-Sep-2014
Compliance Share DoubleDUE:1. T A/R | 2. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 3A/F32
MandatoryT2014-15-13 Paragraph (l) (3) Landing Gear - add serial numbers and part numbers, as applicable, to NLG main fitting/drag stay pins having P/N 200811721; NLG drag brace pivot pins having P/N
200814601; and left and right MLG pintle pins having P/N 6324-1
8.5 Years25-Sep-2024120Mos
Hrs
Ldg
32 A/FEff: 25-Sep-2014
Compliance Share DoubleDUE:1. T A/R | 2. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 3A/F32
MRBRE (N/A)32-00-00-245 Extension and Retraction - Main Landing Gear Selector Valve (Part No. 61750-1) - Restoration
Mos
Hrs
Ldg
32 A/FUnknownUnknown
(SOURCE: TLMC 05-20-15)
Servicing - RecommendedRE (See Note)32-00-00-301 Landing Gear - Cleaning of the Landing Gear
Mos
Hrs
Ldg
32 A/F
(ZONE: 710, 740) (SOURCE: MPD 3.2) (NOTE: This task is required after operation in airports that usepotassium acetate-based Runway De-
Icing fluid. Thecleaning and lubrication of the landing gears should beaccomplished at the earliest convenience after operationin such an
environment.)
MRB ≈03-May-2017RE32-05-11-201 Weight on Wheels Functional Test
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
32 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE32-10-00-210 Main Gear and Doors / Main Landing Gear Uplock /Emergency Extension Visual Check
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
32 A/F
Ref.:PSP 612 Part 9 VC-32-10-01 for Landing Gear check (SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (12,332 Hrs)1. RE 300 HrsMain Landing Gear - CPCP CheckC32-10-801A/F32
MRBRE32-10-00-237 Main Landing Gear Assembly - Detailed Inspection
11.7 Months (+31
Days)22-Mar-2017-/+16022-Mar-2012Mos
Hrs
Ldg
Left
(PKG 60 Month)
32 A/F
601-85082-7DCL272/00
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM139/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE32-10-00-237 Main Landing Gear Assembly - Detailed Inspection
11.7 Months (+31
Days)22-Mar-2017-/+16022-Mar-2012Mos
Hrs
Ldg
Right
(PKG 60 Month)
32 A/F
601-85082-8DCL269/00
(SOURCE: TLMC 05-20-15)
MRBRE32-10-00-238 Main Landing Gear Assembly - Restoration
6 Years (+31 Days)22-Mar-2022-/+112022-Mar-2012Mos
Hrs
Ldg
Left32 A/F601-85082-7DCL272/00
(SOURCE: TLMC 05-20-15)
MRBRE32-10-00-238 Main Landing Gear Assembly - Restoration
6 Years (+31 Days)22-Mar-2022-/+112022-Mar-2012Mos
Hrs
Ldg
Right32 A/F601-85082-8DCL269/00
(SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE32-10-00-241 Main Landing Gear Lubricate Landing Gear
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
32 A/F
(SOURCE: TLMC 05-20-15)
MRBRE32-10-36-204 Main Gear Trailing Arm Check transverse shear bolt
6.6 Months (+31
Days)(21-Oct-2016)-/+11221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
32 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE32-20-00-205 Nose Gear and Doors Visual Check
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
32 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (12,332 Hrs)1. RE 300 HrsNose Landing Gear - CPCP CheckC32-20-801A/F32
MRBRE32-20-00-239 Nose Landing Gear Assembly - Detailed Inspection
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
32 A/F
UnknownUnknown
(SOURCE: TLMC 05-20-15)
MRBRE32-20-00-240 Nose Landing Gear Assembly - Detailed Inspection
5.6 Years (+31 Days)24-Oct-2021-/+112024-Oct-2011Mos
Hrs
Ldg
32 A/FUnknownUnknown
(SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE32-20-00-242 Nose Landing Gear Lubricate Nose Landing Gear
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
32 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM140/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈03-May-2017RE32-30-00-207 Extension and Retraction Functional Test - Landing Gear Retraction System - Functional Test - Landing Gear Extension System
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
32 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE32-30-00-208 Extension and Retraction Landing gear control unit - check for zero output to selectorvalves
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
32 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈15-Jun-2016RE32-30-00-209 Extension and Retraction Priority Valves Functional Test
18-Oct-2003Mos
167 Hrs (+40)12,208.2-/+402,4009,808.2Hrs
Ldg
(PKG 2400 Hour)
32 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE32-30-26-206 Nose Gear Drag Brace Visual Check, paying particular attention to the hinge and attachment pin
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
32 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE32-30-51-211 Nose Landing Gear Uplock Visual Check, paying particular attention to the tension springand latch jaws. Ensure the latch jaws and the engaging pin on the leg are free
of contamination, corrosion and significant contact damage. Do not lubricate
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
32 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE32-35-00-212 Emergency Extension Functional Test
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
32 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE32-35-00-243 Emergency Extension Visual Check of the control path (except for straight runs undercabin floor), paying particular attention to security of the manul release cables
(per 20-40-00 Wire Cables - Inspection Procedures), pulleys and attachment linkages
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
32 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRBRE32-35-00-244 Emergency Extension Visual Check of the control path (straight runs under cabin floor), paying particular attention to security of the manua release cables (per 20-40-
00 Wire Cables - Inspection Procedures), turnbuckles and pulley
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
32 A/F
(SOURCE: TLMC 05-20-15)
MRBRE (T/C)32-41-11-231 Main Wheel - NDT Check
Mos
Hrs
Ldg
Left Inboard32 A/F5009029-1JAN93-0617
Ref.:PSP 612 Part 6 ET-32-41-01, Ref.:PSP 612 Part 7 MT-32-41-01 (SOURCE: TLMC 05-20-15) (NOTE: [1] Check interval is every 400 Wheel
Landings up to 4800 (except at 1600, 3200 and 4800), then at each subsequent tire change. [2] If any defects are found, a complete wheel
assembly inspection must be performed as per CMM/PSP 608/608A. [3] For 1600, 3200 and 4800 Wheel Landing checks refer to Chapter 5 Ref.
No. 32-41-11-232.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM141/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE (T/C)32-41-11-231 Main Wheel - NDT Check
Mos
Hrs
Ldg
Left Outboard32 A/F5007045-2JAN84-235
Ref.:PSP 612 Part 6 ET-32-41-01, Ref.:PSP 612 Part 7 MT-32-41-01 (SOURCE: TLMC 05-20-15) (NOTE: [1] Check interval is every 400 Wheel
Landings up to 4800 (except at 1600, 3200 and 4800), then at each subsequent tire change. [2] If any defects are found, a complete wheel
assembly inspection must be performed as per CMM/PSP 608/608A. [3] For 1600, 3200 and 4800 Wheel Landing checks refer to Chapter 5 Ref.
No. 32-41-11-232.)
MRBRE (T/C)32-41-11-231 Main Wheel - NDT Check
Mos
Hrs
Ldg
Right Inboard32 A/F5009029-1JUN85-R494
Ref.:PSP 612 Part 6 ET-32-41-01, Ref.:PSP 612 Part 7 MT-32-41-01 (SOURCE: TLMC 05-20-15) (NOTE: [1] Check interval is every 400 Wheel
Landings up to 4800 (except at 1600, 3200 and 4800), then at each subsequent tire change. [2] If any defects are found, a complete wheel
assembly inspection must be performed as per CMM/PSP 608/608A. [3] For 1600, 3200 and 4800 Wheel Landing checks refer to Chapter 5 Ref.
No. 32-41-11-232.)
MRBRE (T/C)32-41-11-231 Main Wheel - NDT Check
Mos
Hrs
Ldg
Right Outboard32 A/F5009029-1NOV95-1044
Ref.:PSP 612 Part 6 ET-32-41-01, Ref.:PSP 612 Part 7 MT-32-41-01 (SOURCE: TLMC 05-20-15) (NOTE: [1] Check interval is every 400 Wheel
Landings up to 4800 (except at 1600, 3200 and 4800), then at each subsequent tire change. [2] If any defects are found, a complete wheel
assembly inspection must be performed as per CMM/PSP 608/608A. [3] For 1600, 3200 and 4800 Wheel Landing checks refer to Chapter 5 Ref.
No. 32-41-11-232.)
MRB ≈12-Mar-2016RE32-41-11-232 Main Wheel - Carry out all maintenance requirements in the “CHECK” section of the CMM
26-Sep-2006Mos
Hrs
32 Ldg (+40)6,358-/+408005,558Ldg
Left Inboard32 A/F5009029-1JAN93-0617
Ref.:CMM/PSP 608/608A (SOURCE: TLMC 05-20-15) (NOTE: Check interval is every 1600, 3200 and 4800 Wheel Landings, then at each
subsequent 800 Wheel Landings.)
MRB ≈05-Feb-2017RE32-41-11-232 Main Wheel - Carry out all maintenance requirements in the “CHECK” section of the CMM
25-Jul-2008Mos
Hrs
355 Ldg (+40)6,681-/+408005,881Ldg
Left Outboard32 A/F5007045-2JAN84-235
Ref.:CMM/PSP 608/608A (SOURCE: TLMC 05-20-15) (NOTE: Check interval is every 1600, 3200 and 4800 Wheel Landings, then at each
subsequent 800 Wheel Landings.)
MRB ≈05-Feb-2017RE32-41-11-232 Main Wheel - Carry out all maintenance requirements in the “CHECK” section of the CMM
25-Jul-2008Mos
Hrs
355 Ldg (+40)6,681-/+408005,881Ldg
Left Outboard32 A/F5007045-2JAN84-235
Ref.:CMM/PSP 608/608A (SOURCE: TLMC 05-20-15) (NOTE: Check interval is every 1600, 3200 and 4800 Wheel Landings, then at each
subsequent 800 Wheel Landings.)
MRB ≈12-Mar-2016RE32-41-11-232 Main Wheel - Carry out all maintenance requirements in the “CHECK” section of the CMM
26-Sep-2006Mos
Hrs
32 Ldg (+40)6,358-/+408005,558Ldg
Right Outboard32 A/F5009029-1NOV95-1044
Ref.:CMM/PSP 608/608A (SOURCE: TLMC 05-20-15) (NOTE: Check interval is every 1600, 3200 and 4800 Wheel Landings, then at each
subsequent 800 Wheel Landings.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM142/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE (T/C)32-41-16-234 Nose Wheel (Part Number 600-85003 All Dash Numbers) - NDT Check
Mos
Hrs
Ldg
Left32 A/F5006450-1MAR98-8484
Ref.:PSP 612 Part 6 ET-32-41-02, Ref.:PSP 612 Part 7 MT-32-41-01 (SOURCE: TLMC 05-20-15) (NOTE: [1] Check interval is every 400 Wheel
Landings up to 4800 (except at 1600, 3200 and 4800), then at each subsequent tire change. [2] If any defects are found, a complete wheel
assembly inspection must be performed as per the respective vendor component maintenance manual. [3] For 1600, 3200 and 4800 Wheel
Landing checks refer to Chapter 5 Ref. No. (32-41-16-235).)
MRBRE (T/C)32-41-16-234 Nose Wheel (Part Number 600-85003 All Dash Numbers) - NDT Check
Mos
Hrs
Ldg
Right32 A/F5006450-1MAY90-0599
Ref.:PSP 612 Part 6 ET-32-41-02, Ref.:PSP 612 Part 7 MT-32-41-01 (SOURCE: TLMC 05-20-15) (NOTE: [1] Check interval is every 400 Wheel
Landings up to 4800 (except at 1600, 3200 and 4800), then at each subsequent tire change. [2] If any defects are found, a complete wheel
assembly inspection must be performed as per the respective vendor component maintenance manual. [3] For 1600, 3200 and 4800 Wheel
Landing checks refer to Chapter 5 Ref. No. (32-41-16-235).)
MRB ≈12-Mar-2016RE32-41-16-235 Nose Wheel (Part Number 600-85003 All Dash Numbers) - Carry out all maintenance requirements in the “CHECK” section of the CMM
26-Sep-2006Mos
Hrs
32 Ldg (+40)6,358-/+408005,558Ldg
Left32 A/F5006450-1MAR98-8484
Ref.:CMM/PSP 608/608A (SOURCE: TLMC 05-20-15)
MRB ≈12-Mar-2016RE32-41-16-235 Nose Wheel (Part Number 600-85003 All Dash Numbers) - Carry out all maintenance requirements in the “CHECK” section of the CMM
26-Sep-2006Mos
Hrs
32 Ldg (+40)6,358-/+408005,558Ldg
Right32 A/F5006450-1MAY90-0599
Ref.:CMM/PSP 608/608A (SOURCE: TLMC 05-20-15)
MRBRE (T/C)32-43-11-220 Main Wheel Brake Unit - Brake channel check
Mos
Hrs
Ldg
Left Inboard32 A/F5009027-5UNKNOWN
(SOURCE: TLMC 05-20-15)
MRBRE (T/C)32-43-11-220 Main Wheel Brake Unit - Brake channel check
Mos
Hrs
Ldg
Left Outboard32 A/F5009027-5AUG82-495
(SOURCE: TLMC 05-20-15)
MRBRE (T/C)32-43-11-220 Main Wheel Brake Unit - Brake channel check
Mos
Hrs
Ldg
Right Inboard32 A/F5009027-5OCT83-691
(SOURCE: TLMC 05-20-15)
MRBRE (T/C)32-43-11-220 Main Wheel Brake Unit - Brake channel check
Mos
Hrs
Ldg
Right Outboard32 A/F5009027-5MAY82-426
(SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE32-43-16-222 Accumulator/Hydraulic System - Replenishing Check accumulator charge pressure (Brake Accumulators Only)
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
32 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM143/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE32-43-16-223 Accumulator Visual Check of No. 2 and No. 3 System Brake Accumulators
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
32 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE32-43-21-216 Dual Brake Control Valve Assembly Visual Check visible portions of brake plungers, all linkages and push-pull cables forward of pressure bulkhead (FS202.75)
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
32 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE32-43-21-221 Dual Brake Control Valve Assembly Brake pressure decay check
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
32 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE32-45-11-217 Parking Brake Control Cable Assembly / Pilots and Co-Pilots Push Pull Brake Cables Visual Check of input mechanisms to brake control valve aft ofpressure bulkhead
FS202.75
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
32 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈13-Jul-2017RE32-45-31-224 Parking Brake Shutoff Valve Functional Test - Parking Brake Shut-Off Valve
11-Dec-2003Mos
684 Hrs (+30)(12,725.2)-/+402,4009,966.7Hrs
Ldg
(PKG 2400 Hour)
32 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE32-47-00-225 Anti-Skid System Anti-skid system operational test
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
32 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
≈18-Sep-2016RE32-47-00-226 Functional Test of Nose Wheel Steering Selector Valve
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)30012,041.2Hrs
Ldg
(PKG 300 Hour)
32 A/F
MRB ≈18-Sep-2016RE32-50-00-226 Nosewheel Steering Nosewheel Steering Selector and arming valves functional test
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
32 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE32-50-00-236 Nosewheel Steering - Functional test of Electronic Control Module, Part No.601-86100-9/-13, Vendor Part No. 7040-9/-11/-13/-15
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)60012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
32 A/F
7040-11UNKNOWN
(SOURCE: TLMC 05-20-15)
MRBRE (N/A)32-70-00-202 Gravel Runway Protection (Post SB 601-0112) Visual Check
Mos
Hrs
Ldg
32 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM144/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0019 Modification - N.L.G. Downlock No. 2 - Wiring Change
Mos
Hrs
Ldg
32 A/FEff: 14-Jun-1983
RecommendedRE (-)601-0022 Modification - Nose Landing Gear - Downlock Microswitch
Mos
Hrs
Ldg
32 A/FEff: 06-Sep-1983
RecommendedRE (-)601-0024 Modification - Main Landing Gear - Wheel Discs Sealing Cap (Blanking Plate), Brake Shields and Deflectors
Mos
Hrs
Ldg
32 A/F
RecommendedRE (-)601-0024 Rev 1 Modification - Main Landing Gear - Wheel Discs Sealing Cap (Blanking Plate), Brake Shields and Deflectors
Mos
Hrs
Ldg
32 A/F
RecommendedRE (-)601-0024 Rev 2 Modification - Main Landing Gear - Wheel Discs Sealing Cap (Blanking Plate), Brake Shields and Deflectors
Mos
Hrs
Ldg
32 A/F
RecommendedT (A/R)601-0024 Rev 3 Modification - Main Landing Gear - Wheel Discs Sealing Cap (Blanking Plate), Brake Shields and Deflectors
Mos
Hrs
Ldg
32 A/FEff: 27-Nov-1984
RecommendedRE (-)601-0034 Anti-Skid System - Wheel Spin-Up
Mos
Hrs
Ldg
32 A/F
RecommendedRE (-)601-0034 Rev 1 Anti-Skid System - Wheel Spin-Up
Mos
Hrs
Ldg
32 A/FEff: 16-Aug-1984
OptionalRE (-)601-0039 Modification - Landing Gear - Alternate Downlock Indication
Mos
Hrs
Ldg
32 A/F
OptionalT (A/R)601-0039 Rev 1 Modification - Landing Gear - Alternate Downlock Indication
Mos
Hrs
Ldg
32 A/FEff: 23-Jun-1986
RecommendedRE (-)601-0041 Modification - Nose Wheel Steering - Control Unit
Mos
Hrs
Ldg
32 A/FEff: 22-Dec-1983
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM145/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0079 Special Check/Modification - Parking Brake Valve - Fouling on APU Fuel Line
Mos
Hrs
Ldg
32 A/FEff: 24-Jul-1984
RecommendedRE (-)601-0091 Special Check/Modification - Electrical Harnesses - Installation
Mos
Hrs
Ldg
32 A/F
RecommendedT (A/R)601-0091 Rev 1 Special Check/Modification - Electrical Harnesses - Installation
Mos
Hrs
Ldg
32 A/FEff: 27-Jan-1986
RecommendedRE (-)601-0092 Modification - Steer-by-Wire System – Improvements
Mos
Hrs
Ldg
32 A/F
RecommendedRE (-)601-0092 Rev 1 Modification - Steer-by-Wire System – Improvements
Mos
Hrs
Ldg
32 A/F
RecommendedRE (-)601-0092 Rev 2 Modification - Steer-by-Wire System – Improvements
Mos
Hrs
Ldg
32 A/F
RecommendedRE (-)601-0092 Rev 3 Modification - Steer-by-Wire System – Improvements
Mos
Hrs
Ldg
32 A/F
RecommendedRE (-)601-0092 Rev 4 Modification - Steer-by-Wire System – Improvements
26-Jan-1987Mos
1,267Hrs
480Ldg
32 A/FEff: 08-Dec-1988 Complied With
RecommendedRE (-)601-0093 Special Check/Modification - Manual Release Cable - Grommets
Mos
Hrs
Ldg
32 A/FEff: 05-Jun-1984
OptionalRE (-)601-0100 Modification - Manual Release System - Handle and Lever Assemblies
Mos
Hrs
Ldg
32 A/F
OptionalRE (-)601-0100 Rev 1 Modification - Manual Release System - Handle and Lever Assemblies
25-Nov-2000Mos
Hrs
Ldg
32 A/FEff: 27-Jun-1987 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM146/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalRE (-)601-0112 Modification - Operation from Unpaved/Gravel Runways - Protection
Mos
Hrs
Ldg
32 A/F
OptionalT (A/R)601-0112 Rev 1 Modification - Operation from Unpaved/Gravel Runways - Protection
Mos
Hrs
Ldg
32 A/FEff: 16-Jun-1989
RecommendedRE (-)601-0146 Modification - Main Landing Gear - Door Hinge
02-May-1988Mos
1,995Hrs
756Ldg
32 A/FEff: 11-Aug-1986 Complied With
OptionalRE (-)601-0177 Modification - Nose Gear - Introduction of Earthing Point
Mos
Hrs
Ldg
32 A/F
OptionalRE (-)601-0177 Rev 1 Modification - Nose Gear - Introduction of Earthing Point
Mos
Hrs
Ldg
32 A/F
OptionalT (A/R)601-0177 Rev 2 Modification - Nose Gear - Introduction of Earthing Point
Mos
Hrs
Ldg
32 A/FEff: 21-Jun-1989
OptionalT (A/R)601-0203 Modification - Brake Control Mechanism - Plunger Assembly Replacement
Mos
Hrs
Ldg
32 A/FEff: 24-Feb-1989
RecommendedRE (-)601-0206 Modification - Priority Valve - Relocation to Aft MLG Bay Bulkhead
28-Mar-1989Mos
2,373Hrs
910Ldg
32 A/FEff: 17-Jul-1987 Complied With
RecommendedRE (-)601-0242 Modification - Steer-by-Wire - Reliability Improvements
28-Mar-1989Mos
2,373Hrs
910Ldg
32 A/FComplied With
RecommendedRE (-)601-0242 Rev 1 Modification - Steer-by-Wire - Reliability Improvements
28-Mar-1989Mos
2,373Hrs
910Ldg
32 A/FEff: 06-Jul-1989 Complied With
OptionalRE (-)601-0266 Modification - Nose Gear Doors - External Ground Operation
Mos
Hrs
Ldg
32 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM147/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalRE (-)601-0266 Rev 1 Modification - Nose Gear Doors - External Ground Operation
12-Nov-1997Mos
Hrs
Ldg
32 A/FEff: 22-Feb-1991 Complied With
RecommendedRE (-)601-0267 Modification - Nose Landing Gear - Shock Strut
Mos
Hrs
Ldg
32 A/F
RecommendedRE (-)601-0267 Rev 1 Modification - Nose Landing Gear - Shock Strut
Mos
Hrs
Ldg
32 A/F
RecommendedRE (-)601-0267 Rev 2 Modification - Nose Landing Gear - Shock Strut
01-Dec-1990Mos
3,058.6Hrs
1,212Ldg
32 A/FEff: 10-Jul-1989 Complied With
RecommendedRE (-)601-0285 Special Check/Modification - NLG and MLG Harness Assemblies - Replacement/Rerouting
Mos
Hrs
Ldg
32 A/F
RecommendedRE (-)601-0285 Rev 1 Special Check/Modification - NLG and MLG Harness Assemblies - Replacement/Rerouting
Mos
Hrs
Ldg
32 A/F
RecommendedT (A/R)601-0285 Rev 2 Special Check/Modification - NLG and MLG Harness Assemblies - Replacement/Rerouting
Mos
Hrs
Ldg
32 A/FEff: 15-Dec-1997
RecommendedRE (-)601-0299 Modification - Manual Release System - Cable Support Bracket Relocation
Mos
Hrs
Ldg
32 A/FEff: 15-Nov-1989
RecommendedRE (-)601-0303 Special Check/Modification - Main Landing Gear - Shock Strut Rebound Ring
01-Dec-1990Mos
3,058.6Hrs
1,212Ldg
32 A/FEff: 14-Jul-1989 Complied With
OptionalRE (-)601-0331 Modification - Main Landing Gear - Removal of Wheel Speed Sensor Set-Screw
12-Nov-1992Mos
3,754Hrs
1,519Ldg
32 A/FEff: 12-Oct-1990 Complied With
OptionalRE (-)601-0363 Modification - Landing Lights - Pulsating Light System
Mos
Hrs
Ldg
32 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM148/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalRE (-)601-0363 Rev 1 Modification - Landing Lights - Pulsating Light System
Mos
Hrs
Ldg
32 A/F
OptionalT (A/R)601-0363 Rev 2 Modification - Landing Lights - Pulsating Light System
Mos
Hrs
Ldg
32 A/FEff: 07-Jun-1993
RecommendedRE (-)601-0373 Special Check/Modification - Emergency Extension - Main Landing Gear Manual Release Cable and Dump Valve Lever
31-Oct-1993Mos
4,142Hrs
1,668Ldg
32 A/FEff: 26-Mar-1993 Complied With
RecommendedRE (-)601-0398 Special Check/Modification - Nose Gear Downlock Indication - Wire Correction
23-Oct-1992Mos
3,754Hrs
1,519Ldg
32 A/FEff: 30-Sep-1992 Complied With
OptionalT (A/R)601-0444 Modification - Main Landing Gear Priority Valve and Hydraulic Lines
Mos
Hrs
Ldg
32 A/FEff: 30-Apr-1996
RecommendedRE (-)601-0446 Modification - Nose-Gear Door Actuator Improvement to Ground Locking Capability
18-Nov-1996Mos
5,001Hrs
2,052Ldg
32 A/FEff: 29-Feb-1996 Complied With
OptionalT (A/R)601-0461 Modification - Left Nose Landing Gear (NLG) Door - Installation of Rubber Stop at Aft Hinge
Mos
Hrs
Ldg
32 A/FEff: 31-Oct-1995
OptionalRE (-)601-0469 Modification - Navigation Lights - Replace Navigation Light at Vertical Stabilizer
Mos
Hrs
Ldg
32 A/F
OptionalRE (-)601-0469 Rev 1 Modification - Navigation Lights - Replace Navigation Light at Vertical Stabilizer
Mos
Hrs
Ldg
32 A/F
OptionalT (A/R)601-0469 Rev 2 Modification - Navigation Lights - Replace Navigation Light at Vertical Stabilizer
Mos
Hrs
Ldg
32 A/FEff: 30-Apr-2004
RecommendedRE (-)601-0472 Special Check/Modification - MLG Door Mechanism - Possible Fouling Between Crank and Door Strut Link
18-Nov-1996Mos
5,001Hrs
2,052Ldg
32 A/FEff: 04-Apr-1996 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM149/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0494 Modification - Replace the Nose Landing Gear Selector Valve and Nose Gear Door Selector Valve, Part No. 55540-2 with Part No. 55540-5
12-Nov-1997Mos
5,395Hrs
2,274Ldg
32 A/FEff: 20-Dec-1996 Complied With
OptionalRE (-)601-0500 Brake System - Introduction of Restrictor in Nose Landing Gear (NLG) Retraction Line to Brake Metering Valve
05-Nov-1998Mos
5,824Hrs
2,521Ldg
32 A/FEff: 31-May-1999 Complied With
RecommendedRE (-)601-0526 Special Check/Modification - Weight-on- Wheel Proximity Switches - Prevent Uncommanded Deployment of the Air Driven Generator on the Ground
Mos
Hrs
Ldg
32 A/F
RecommendedRE (-)601-0526 Rev 1 Special Check/Modification - Weight-on- Wheel Proximity Switches - Prevent Uncommanded Deployment of the Air Driven Generator on the Ground
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
32 A/FEff: 31-Oct-2000 Complied With
OptionalT (A/R)601-0531 Modification - Nose Landing Gear - Introduction of Allowable Wear Limits and Replacement of the Structural Support Bushings for the NLG Trunnion and the NLG Drag
Brace Attachments
Mos
Hrs
Ldg
32 A/FEff: 30-Sep-2004
RecommendedRE (-)601-0545 Special Check/Rework - Nose Landing Gear (NLG) Extension and Retraction - examine NLG Uplock Pin For Jammed Condition
09-Sep-2001Mos
7,697.4Hrs
3,650Ldg
32 A/FEff: 29-Jun-2001 Complied With
RecommendedRE (-)601-0546 Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and MLG Component Serialization
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
32 A/FComplied With
Nextdue Share EarliestDUE:1. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Part AA/F32
Nextdue Share EarliestDUE:1. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Part BA/F32
RecommendedRE (-)601-0546 Part A Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and Left MLG Component Serialization
Mos
Hrs
Ldg
32 A/FEff: 31-May-2002
RecommendedRE (-)601-0546 Part B Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and Right MLG Component Serialization
Mos
Hrs
Ldg
32 A/FEff: 31-May-2002
RecommendedRE (-)601-0546 Rev 1 Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and MLG Component Serialization
Mos
Hrs
Ldg
32 A/F
Nextdue Share EarliestDUE:1. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 1 Part AA/F32
Nextdue Share EarliestDUE:1. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 1 Part BA/F32
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM150/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0546 Rev 1 Part A Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and Left MLG Component Serialization
Mos
Hrs
Ldg
32 A/FEff: 15-Dec-2003
RecommendedRE (-)601-0546 Rev 1 Part B Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and Right MLG Component Serialization
Mos
Hrs
Ldg
32 A/FEff: 15-Dec-2003
RecommendedRE (-)601-0546 Rev 2 Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and MLG Component Serialization
Mos
Hrs
Ldg
32 A/F
Nextdue Share EarliestDUE:1. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 2 Part AA/F32
Nextdue Share EarliestDUE:1. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 2 Part BA/F32
RecommendedRE (-)601-0546 Rev 2 Part A Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and Left MLG Component Serialization
Mos
Hrs
Ldg
32 A/FEff: 29-Oct-2007
RecommendedRE (-)601-0546 Rev 2 Part B Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and Right MLG Component Serialization
Mos
Hrs
Ldg
32 A/FEff: 29-Oct-2007
RecommendedT (A/R)601-0546 Rev 3 Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and MLG Component Serialization
Mos
Hrs
Ldg
32 A/FEff: 09-May-2011
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 3 Part AA/F32
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Modification - Nose Landing Gear (NLG) and Main Landing Gear...601-0546 Rev 3 Part BA/F32
RecommendedT (A/R)601-0546 Rev 3 Part A Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and Left MLG Component Serialization
Mos
Hrs
Ldg
32 A/FEff: 09-May-2011
RecommendedT (A/R)601-0546 Rev 3 Part B Modification - Nose Landing Gear (NLG) and Main Landing Gear (MLG) System - NLG and Right MLG Component Serialization
Mos
Hrs
Ldg
32 A/FEff: 09-May-2011
RecommendedRE (-)601-0558 Special Check/Rework - Extension and Retraction - End Caps on Nose Landing Gear (NLG) Selector Valve and Nose Gear Door Selector Valve Could Have Been
Incorrectly Lockwired During Assembly
Mos
Hrs
Ldg
32 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM151/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0558 Rev 1 Special Check/Rework - Extension and Retraction - End Caps on Nose Landing Gear (NLG) Selector Valve and Nose Gear Door Selector Valve Could Have Been
Incorrectly Lockwired During Assembly
Mos
Hrs
Ldg
32 A/F
RecommendedRE (-)601-0558 Rev 2 Special Check/Rework - Extension and Retraction - End Caps on Nose Landing Gear (NLG) Selector Valve and Nose Gear Door Selector Valve Could Have Been
Incorrectly Lockwired During Assembly
Mos
Hrs
Ldg
32 A/F
RecommendedRE (-)601-0558 Rev 3 Special Check/Rework - Extension and Retraction - End Caps on Nose Landing Gear (NLG) Selector Valve and Nose Gear Door Selector Valve Could Have Been
Incorrectly Lockwired During Assembly
02-Dec-2009Mos
11,460.7Hrs
5,905Ldg
32 A/FEff: 23-Feb-2009 Complied With
OptionalT (A/R)601-0569 Modification - Position and Warning - Installation and Rerouting of a New Nose Landing Gear Harness
Mos
Hrs
Ldg
32 A/FEff: 20-Feb-2006
OptionalRE (-)601-0598 Modification – Nose Landing Gear (NLG) – Towing Strap Placard Installation
Mos
Hrs
Ldg
32 A/F
OptionalT (A/R)601-0598 Rev 1 Modification – Nose Landing Gear (NLG) – Towing Strap Placard Installation
Mos
Hrs
Ldg
32 A/FEff: 14-Oct-2008
RecommendedT (A/R)601-0616 Modification – Nose Gear and Doors – Addition of Guides to Nose Landing Gear Unpaved/Gravel Runway Kit
Mos
Hrs
Ldg
32 A/FEff: 31-Oct-2011
OptionalT (A/R)601-0621 Modification – Main Brake System – Replacement of the Hydraulic System No. 2 Brake Accumulator
Mos
Hrs
Ldg
32 A/FEff: 14-May-2012
OptionalT (A/R)601-0622 Modification – Main Brake System – Replacement of the Hydraulic System No. 3 Brake Accumulator
Mos
Hrs
Ldg
32 A/FEff: 14-May-2012
OptionalT (A/R)601-0632 Modification – Brake Control Valve (BCV) – Incorporation of Optional BCV
Mos
Hrs
Ldg
32 A/FEff: 18-Mar-2014
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM152/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryRE (-)81-13-51 Wheel Brake Assembly
20-Sep-1983Mos
0Hrs
0Ldg
32 A/FBY AIRCRAFT MODELEff: 07-Dec-1981 Not
Applicable
MandatoryRE (-)82-06-05 Main Landing Gear Release Control System
18-Sep-1985Mos
Hrs
Ldg
32 A/FBY AIRCRAFT SERIAL NUMBEREff: 22-Mar-1982 Not
Applicable
MandatoryRE (-)82-09-51 R1 AFM, Supplement 2 Changes
18-Sep-1985Mos
Hrs
Ldg
32 A/FBY AIRCRAFT SERIAL NUMBEREff: 09-Sep-1982 Not
Applicable
AlertRE (-)A601-0072 Special Check/Adjustment - Main Landing Gear Harnesses - Location
Mos
Hrs
Ldg
32 A/FEff: 19-Jul-1984
AlertRE (-)A601-0115 Special Check/Modification - Main Landing Gear Harnesses - Routing
05-Sep-1985Mos
Hrs
Ldg
32 A/FEff: 08-Mar-1985 Complied With
AlertRE (-)A601-0329 Special Check/Modification - Main Landing Gear Door - Hinge and Fasteners
Mos
Hrs
Ldg
32 A/F
AlertRE (-)A601-0329 Rev 1 Special Check/Modification - Main Landing Gear Door - Hinge and Fasteners
Mos
Hrs
Ldg
32 A/F
AlertRE (-)A601-0329 Rev 2 Special Check/Modification - Main Landing Gear Door - Hinge and Fasteners
17-May-2013Mos
11,788.8Hrs
6,143Ldg
32 A/FEff: 14-Dec-1990 Complied With
CPCP ≈18-Sep-2016REC32-10-801 Main Landing Gear - CPCP Check
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
32 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with the Scheduled Maintenance Instruction Task 32-10-00-210)
CPCP ≈18-Sep-2016REC32-20-801 Nose Landing Gear - CPCP Check
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
32 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with the Scheduled Maintenance Instruction Task 32-20-00-205)
▼ 33 - LIGHTS
RE (O/C)Dimmer
20-Sep-1983Mos
0Hrs0
0Ldg0
Left33 A/FNew600-51519-1
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM153/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Dimmer
20-Sep-1983Mos
0Hrs0
0Ldg0
Right33 A/FNew600-51519-1
UNKNOWN
RE (O/C)Dimmer Control Assembly
20-Sep-1983Mos
0Hrs0
0Ldg0
Left33 A/FNew70-0180-3
UNKNOWN
RE (O/C)Dimmer Control Assembly
20-Sep-1983Mos
0Hrs
0Ldg
Right33 A/FUnknownUnknown
RE (O/C)Downwash Light Inverter
20-Sep-1983Mos
0Hrs
0Ldg
Left33 A/FUnknownUnknown
RE (O/C)Downwash Light Inverter
20-Sep-1983Mos
0Hrs
0Ldg
Right33 A/FUnknownUnknown
RE (O/C)Emergency Exit Light Battery Pack
20-Sep-1983Mos
0Hrs
0Ldg
No.133 A/FUnknownUnknown
RE (O/C)Emergency Exit Light Battery Pack
20-Sep-1983Mos
0Hrs
0Ldg
No.233 A/FUnknownUnknown
RE (O/C)Emergency Lighting Power Supplie
18-Dec-2014Mos
11,854.6Hrs
Ldg
Aft33 A/F60-1321-118594
Component Inspection SimpleDUE:1. RE 12 MosEmergency Lighting Inspect Power Supplies per Check section ...33-50-00-203A/F33
RE (O/C)Emergency Lighting Power Supplie
18-Dec-2014Mos
11,854.6Hrs
Ldg
Fwd33 A/F60-1321-122411
Component Inspection SimpleDUE:1. RE 12 MosEmergency Lighting Inspect Power Supplies per Check section ...33-50-00-203A/F33
RE (O/C)Fluorescent Light Inverter
20-Sep-1983Mos
0Hrs0
0Ldg0
Center33 A/FNew55-0521-4
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM154/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Fluorescent Light Inverter
20-Sep-1983Mos
0Hrs
0Ldg
Copilot33 A/FUnknownUnknown
RE (O/C)Fluorescent Light Inverter
20-Sep-1983Mos
0Hrs
0Ldg
Pilot33 A/FUnknownUnknown
RE (O/C)Incandescent Dimmer
20-Sep-1983Mos
0Hrs0
0Ldg0
Center33 A/FNew2-459-06
UNKNOWN
RE (O/C)Incandescent Dimmer
20-Sep-1983Mos
0Hrs0
0Ldg0
Left33 A/FNew2-459-06
UNKNOWN
RE (O/C)Incandescent Dimmer
11-Nov-2002Mos
7,968.7Hrs
3,821Ldg
Right33 A/F2-459-060697
RE (O/C)Overhead Power Supply Unit
20-Sep-1983Mos
0Hrs0
0Ldg0
33 A/FNew449-2
UNKNOWN
RE (O/C)Strobe Power Supply Unit
20-Sep-1983Mos
0Hrs0
0Ldg0
Left33 A/FNew60-2799-3
UNKNOWN
RE (O/C)Strobe Power Supply Unit
20-Sep-1983Mos
0Hrs0
0Ldg0
Right33 A/FNew60-2799-3
UNKNOWN
RE (O/C)Tail Anti-Collision/Pos Light Assembly
20-Sep-1983Mos
0Hrs0
0Ldg0
33 A/FNew30-1192-7
UNKNOWN
RE (O/C)Tail Strobe Power Supply Unit
20-Sep-1983Mos
0Hrs
0Ldg
33 A/FUnknownUnknown
RE (O/C)Upper Strobe Light
20-Sep-1983Mos
0Hrs
0Ldg
33 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM155/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Upper Tail Nav Light Assembly
20-Sep-1983Mos
0Hrs
0Ldg
33 A/FUnknownUnknown
RE (O/C)Wing Anti-Collision Light Assembly
20-Sep-1983Mos
0Hrs0
0Ldg0
Left33 A/FNew30-1467-1
UNKNOWN
RE (O/C)Wing Anti-Collision Light Assembly
31-Dec-2002Mos
9,155.9Hrs
4,544Ldg
Right33 A/F30-1467-19967
≈29-Feb-2016RE33-40-00-201 Exterior Lighting Visual and Operational Test
05-Apr-2013Mos
26.3 Hrs12,067.530011,767.5Hrs
Ldg
33 A/F
MRB ≈18-Sep-2016RE33-50-00-202 Emergency Lighting Visual Check- Operational Test
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
33 A/F
(SOURCE: TLMC 05-20-15)
MRBRE33-50-00-203 Emergency Lighting Inspect Power Supplies per Check section and carry out Capacity Check per Repair section of CMM/PSP 608/608A33-50-42, or install new Power
Supplies
6.6 Months (+31
Days)(21-Oct-2016)-/+11221-Oct-2015Mos
Hrs
Ldg
Aft
(PKG 12 Month)
33 A/F
60-1321-118594
(SOURCE: TLMC 05-20-15)
MRBRE33-50-00-203 Emergency Lighting Inspect Power Supplies per Check section and carry out Capacity Check per Repair section of CMM/PSP 608/608A33-50-42, or install new Power
Supplies
6.6 Months (+31
Days)(21-Oct-2016)-/+11221-Oct-2015Mos
Hrs
Ldg
Fwd
(PKG 12 Month)
33 A/F
60-1321-122411
(SOURCE: TLMC 05-20-15)
RecommendedRE (-)601-0067 Modification - Emergency Light Drains - Introduction
Mos
Hrs
Ldg
33 A/F
RecommendedRE (-)601-0067 Rev 1 Modification - Emergency Light Drains - Introduction
26-Jan-1987Mos
1,267Hrs
470Ldg
33 A/FEff: 09-Dec-1985 Complied With
RecommendedRE (-)601-0070 Modification - External Emergency Light Wiring - Protection
26-Jan-1987Mos
1,267Hrs
470Ldg
33 A/FEff: 26-Jun-1984 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM156/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalRE (-)601-0137 Modification - Rear Navigation Light - Shock Mount Addition
23-Feb-1990Mos
2,687Hrs
1,034Ldg
33 A/FEff: 31-Oct-1985 Complied With
OptionalT (A/R)601-0193 Modification - Center Pedestal - Third Light Dimmer
Mos
Hrs
Ldg
33 A/FEff: 15-Jun-1989
RecommendedRE (-)601-0227 Modification - Recognition/Taxi and Landing Lights - Wiring
23-Mar-1992Mos
3,584Hrs
1,446Ldg
33 A/FEff: 30-Jun-1988 Complied With
OptionalT (A/R)601-0294 Modification - Integral Lighting - Lamp Dimmer Power Supply Circuit Breaker and Wiring Replacement
Mos
Hrs
Ldg
33 A/FEff: 05-Jan-1990
OptionalT (A/R)601-0490 Modification - Power Supplies for AC Incandescent Lamp Dimmers - Separation of AC and DC Ground Connections
Mos
Hrs
Ldg
33 A/FEff: 31-Mar-1998
RecommendedRE (-)601-0527 Modification - Navigation Lights - Change of Circuit Breaker Rating From 3 AMPS to 2 AMPS
08-Feb-2000Mos
6,204.1Hrs
3,181Ldg
33 A/FEff: 29-Oct-1999 Complied With
OptionalT (A/R)601-0594 Modification – Navigation Lights – Introduction of Wing Tip Halogen Navigation Lights to Improve Reliability
Mos
Hrs
Ldg
33 A/FEff: 31-Mar-2008
IsModSumT (A/R)IS600-33-0001 REV A Kit - Introduction, Rear Navigation Light Spiral Cord / Boot (Service Loop)
Mos
Hrs
Ldg
33 A/F
▼ 34 - NAVIGATION
RE (O/C)ADF Antenna
20-Sep-1983Mos
0Hrs
0Ldg
No.134 A/FUnknownUnknown
RE (O/C)ADF Control
11-Jan-2003Mos
9,193.3Hrs
4,567Ldg
No.134 A/FG7026-0576
RE (O/C)ADF Receiver
20-Sep-1983Mos
0Hrs0
0Ldg0
No.134 A/FNew622-2362-001
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM157/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)ADF Receiver
20-Sep-1983Mos
0Hrs
0Ldg
No.234 A/FUnknownUnknown
RE (O/C)Air Data Computer
20-Sep-1983Mos
0Hrs0
0Ldg0
Left34 A/FNew7000700-637
01109199
Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosFunctional Test of the Air Data Computer34-13-00-101*A/F34
Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosAir Data Computer tests and inspections per FAR 91.411 Appen...FAR 91.411A/F34
RE (O/C)Air Data Computer
20-Sep-1983Mos
0Hrs0
0Ldg0
Right34 A/FNew7000700-637
86091747
Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosFunctional Test of the Air Data Computer34-13-00-101*A/F34
Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosAir Data Computer tests and inspections per FAR 91.411 Appen...FAR 91.411A/F34
RE (O/C)Altimeter
20-Sep-1983Mos
0Hrs
0Ldg
Left34 A/FUnknownUnknown
Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosAltimeter test and inspect per FAR 91.411 Appendix E part 43FAR 91.411A/F34
RE (O/C)Altimeter
20-Sep-1983Mos
0Hrs
0Ldg
Right34 A/FUnknownUnknown
Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosAltimeter test and inspect per FAR 91.411 Appendix E part 43FAR 91.411A/F34
RE (O/C)Altimeter
20-Sep-1983Mos
0Hrs0
0Ldg0
StandBy34 A/FNew8047-10
7536B
Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosAltimeter Standby Indicator tests and inspections per FAR 91...FAR 91.411A/F34
RE (O/C)Antenna
20-Sep-1983Mos
0Hrs0
0Ldg0
No.134 A/FNewS65-5366-7L
UNKNOWN
RE (O/C)Antenna
20-Sep-1983Mos
0Hrs0
0Ldg0
No.234 A/FNewS65-5366-7L
UNKNOWN
RE (O/C)Antenna
20-Sep-1983Mos
0Hrs
0Ldg
No.334 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM158/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Antenna
20-Sep-1983Mos
0Hrs
0Ldg
No.434 A/FUnknownUnknown
RE (O/C)ATC Control
23-Feb-2002Mos
8,131.2Hrs
3,914Ldg
34 A/F622-6523-20510222
RE (O/C)ATC Transponder System
24-Apr-2003Mos
9,417.5Hrs
4,702Ldg
No.134 A/F622-9210-0033731
Component Inspection SimpleDUE:1. RE 24 MosATC Transponder System - Functional Test34-54-00-207A/F34
Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosATC Transponder test and inspections per FAR 91.413 Appendix...FAR 91.413A/F34
RE (O/C)ATC Transponder System
20-Sep-1983Mos
0Hrs0
0Ldg0
No.234 A/FNew622-6210-003
3707
Component Inspection SimpleDUE:1. RE 24 MosATC Transponder System - Functional Test34-54-00-207A/F34
Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosATC Transponder test and inspections per FAR 91.413 Appendix...FAR 91.413A/F34
RE (O/C)Attitude Direction Indicator
08-Mar-2005Mos
0Hrs0
0Ldg0
No.134 A/FNew7000466-905
82031445
RE (O/C)Attitude Direction Indicator
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
No.234 A/F7000466-90580080258
RE (O/C)Battery, INS
21-Oct-2015Mos
12,001.1Hrs
Ldg
No.134 A/F27826-0028902788
Component Inspection SimpleDUE: 21-Apr-20161. RE 6 MosCapacity Check of INS Battery34-CUS-010A/F34
RE (O/C)Battery, INS
21-Oct-2015Mos
12,001.1Hrs
Ldg
No.234 A/F27826-0029805842
Component Inspection SimpleDUE: 21-Apr-20161. RE 6 MosCapacity Check of INS Battery.34-CUS-010A/F34
RE (O/C)Comparator Monitor Indicator
20-Sep-1983Mos
0Hrs0
0Ldg0
34 A/FNew2594732-601
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM159/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Course Deviation Indicator
20-Sep-1983Mos
0Hrs
0Ldg
34 A/FUnknownUnknown
RE (O/C)Data Management, AFIS Unit
20-Sep-1983Mos
0Hrs
0Ldg
34 A/FUnknownUnknown
RE (O/C)Digital Clock
26-Nov-2001Mos
7,890Hrs
3,779Ldg
Left34 A/F811B24652
Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosDigital Clocks - Remove and install new batteries34-62-00-303A/F34
RE (O/C)Digital Clock
30-Jan-2015Mos
11,862.7Hrs
6,194Ldg
Right34 A/F811BUNKNOWN
Component Inspection SimpleDUE: 30-Jan-20171. RE 24 MosDigital Clocks - Remove and install new batteries34-62-00-303A/F34
RE (O/C)Directional Gyro
18-Mar-2003Mos
9,319.8Hrs
4,641Ldg
No.134 A/F2587193-435055183
RE (O/C)Directional Gyro
20-Sep-1983Mos
0Hrs0
0Ldg0
No.234 A/FNew2587193-43
UNKNOWN
RE (O/C)DME Transceiver
20-Sep-1983Mos
0Hrs
0Ldg
Left34 A/FUnknownUnknown
RE (O/C)DME Transceiver
14-Oct-2003Mos
9,787.8Hrs
4,918Ldg
Right34 A/F622-1233-0017699
RE (O/C)EFIS Display
20-Sep-1983Mos
0Hrs
0Ldg
No.134 A/FUnknownUnknown
RE (O/C)EFIS Display
18-Dec-2014Mos
11,854.6Hrs
Ldg
No.234 A/FCG1121AB03050
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM160/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)EFIS Display
20-Sep-1983Mos
0Hrs
0Ldg
No.334 A/FUnknownUnknown
RE (O/C)EFIS Display
20-Sep-1983Mos
0Hrs
0Ldg
No.434 A/FUnknownUnknown
RE (O/C)EFIS Display
20-Sep-1983Mos
0Hrs
0Ldg
No.534 A/FUnknownUnknown
RE (O/C)EFIS Display
20-Sep-1983Mos
0Hrs
0Ldg
No.634 A/FUnknownUnknown
RE (O/C)EFIS Symbol Generator
20-Sep-1983Mos
0Hrs
0Ldg
No.134 A/FUnknownUnknown
RE (O/C)EFIS Symbol Generator
20-Sep-1983Mos
0Hrs
0Ldg
No.234 A/FUnknownUnknown
RE (O/C)Flight Director Computer
05-May-2002Mos
8,407.3Hrs
4,077Ldg
No.134 A/F4018369-90785014708
RE (O/C)Flight Director Computer
20-Sep-1983Mos
0Hrs0
0Ldg0
No.234 A/FNew4018369-905
UNKNOWN
RE (O/C)Flux Valve
20-Sep-1983Mos
0Hrs
0Ldg
Left34 A/FUnknownUnknown
RE (O/C)Flux Valve
20-Sep-1983Mos
0Hrs
0Ldg
Right34 A/FUnknownUnknown
RE (O/C)FMS CDI Unit
20-Sep-1983Mos
0Hrs
0Ldg
No.334 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM161/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Glideslope Antenna
20-Sep-1983Mos
0Hrs0
0Ldg0
34 A/FNewS41422-2
UNKNOWN
RE (O/C)GPWS Computer
20-Sep-1983Mos
0Hrs
0Ldg
34 A/FUnknownUnknown
RE (O/C)Gyro Compass Dual Remote Compensator
20-Sep-1983Mos
0Hrs0
0Ldg0
34 A/FNew2593379-1
UNKNOWN
RE (O/C)Horizon Situation Indicator
07-Mar-2002Mos
8,174.5Hrs
3,939Ldg
No.134 A/F7000469-90381020563
RE (O/C)Horizon Situation Indicator
20-Sep-1983Mos
0Hrs0
0Ldg0
No.234 A/FNew7000469-903
81040711
RE (O/C)Inertial Reference Unit (IRU)
20-Sep-1983Mos
0Hrs
0Ldg
No.134 A/FUnknownUnknown
RE (O/C)Inertial Reference Unit (IRU)
18-Dec-2014Mos
11,854.6Hrs
Ldg
No.234 A/FHG1066AD03099 REPAIR
RE (O/C)Inertial Reference Unit (IRU)
20-Sep-1983Mos
0Hrs
0Ldg
No.334 A/FUnknownUnknown
RE (O/C)Mach Airspeed Indicator
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
No.134 A/F35405-013123
RE (O/C)Mach Airspeed Indicator
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
No.234 A/F35405-013122
RE (O/C)Marker Beacon Antenna
20-Sep-1983Mos
0Hrs0
0Ldg0
34 A/FNewS35-1000-2
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM162/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)MFD Symbol Generator
20-Sep-1983Mos
0Hrs
0Ldg
34 A/FUnknownUnknown
RE (O/C)Nav Controller
11-Nov-2004Mos
10,470.9Hrs
5,316Ldg
No.134 A/FG7024-07110
RE (O/C)Navigation Receiver
20-Sep-1983Mos
0Hrs
0Ldg
No.134 A/FUnknownUnknown
RE (O/C)Navigation Receiver
20-Sep-1983Mos
0Hrs
0Ldg
No.234 A/FUnknownUnknown
AWL - RVSM, Life Limit ≈04-Nov-2018REPitot-Static Head
09-Oct-1992Mos
1,312.8 Hrs13,3549,6003,754Hrs0
1,519Ldg0
Left34 A/FNew856KV10
UNKNOWN
TLMC:34-11-11-101* (SOURCE: TLMC 05-10-13)
AWL - RVSM, Life Limit ≈04-Nov-2018REPitot-Static Head
09-Oct-1992Mos
1,312.8 Hrs13,3549,6003,754Hrs0
1,519Ldg0
Right34 A/FNew856KV10
UNKNOWN
TLMC:34-11-11-101* (SOURCE: TLMC 05-10-13)
RE (O/C)Radar Controller
20-Sep-1983Mos
0Hrs
0Ldg
No.134 A/FUnknownUnknown
RE (O/C)Radar Indicator
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
34 A/FMI-5853431258
RE (O/C)Radar Pedestal Antenna
20-Sep-1983Mos
0Hrs
0Ldg
34 A/FUnknownUnknown
RE (O/C)Radar Waveguide Assy
20-Sep-1983Mos
0Hrs
0Ldg
No.134 A/FUnknownUnknown
RE (O/C)Radio Altimeter
06-Apr-2005Mos
10,718Hrs
5,449Ldg
No.134 A/F622-2855-0022663
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM163/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Radio Altimeter
20-Sep-1983Mos
0Hrs
0Ldg
No.234 A/FUnknownUnknown
RE (O/C)Radio Altimeter Antenna
20-Sep-1983Mos
0Hrs0
0Ldg0
No.134 A/FNewS67-2002
UNKNOWN
RE (O/C)Radio Altimeter Antenna
20-Sep-1983Mos
0Hrs0
0Ldg0
No.234 A/FNewS67-2002
UNKNOWN
RE (O/C)Radio Magnetic Indicator
20-Aug-2003Mos
9,608.2Hrs
4,812Ldg
Left34 A/F3117LB2-1A3773
RE (O/C)Radio Magnetic Indicator
14-Oct-2003Mos
9,787.8Hrs
4,918Ldg
Right34 A/F3117LB2-1A2949
RE (O/C)Rate Gyro
06-Feb-2005Mos
10,582.5Hrs
5,379Ldg
No.134 A/F7007453-90302065494
RE (O/C)Rate Gyro
06-Feb-2005Mos
10,582.5Hrs
5,379Ldg
No.234 A/F7007453-90390112657
RE (O/C)Remote Controller
20-Sep-1983Mos
0Hrs0
0Ldg0
34 A/FNew4026206-904
UNKNOWN
RE (O/C)RMI Adapter
28-Jul-2004Mos
10,458.3Hrs
5,308Ldg
Left34 A/F622-1032-0014574
RE (O/C)RMI Adapter
20-Sep-1983Mos
0Hrs
0Ldg
Right34 A/FUnknownUnknown
RE (O/C)Standby Airspeed Indicator
20-Sep-1983Mos
0Hrs
0Ldg
34 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM164/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Standby Horizon Indicator
14-Dec-2003Mos
9,966.7Hrs
5,011Ldg
34 A/F501-1197-053501
RE (O/C)Standby Magnetic Compass
26-Sep-2006Mos
10,897.5Hrs
5,558Ldg
34 A/FPA170060345
Component Inspection SimpleDUE:1. RE 12 MosStandby Magnetic Compass - Compass Swing34-27-00-206A/F34
RE (O/C)Static Pressure Port
20-Sep-1983Mos
0Hrs0
0Ldg0
Left34 A/FNewST300-3HA
UNKNOWN
RE (O/C)Static Pressure Port
20-Sep-1983Mos
0Hrs0
0Ldg0
Right34 A/FNewST300-3HA
UNKNOWN
RE (O/C)TAS/TAT Indicator
21-Apr-2005Mos
10,740.1Hrs
5,462Ldg
34 A/F4031609-90483050462
RE (O/C)TCAS Antenna
20-Sep-1983Mos
0Hrs
0Ldg
Upper34 A/FUnknownUnknown
RE (O/C)TCAS Computer
20-Sep-1983Mos
0Hrs
0Ldg
34 A/FUnknownUnknown
RE (O/C)Total Temperature Sensor
20-Sep-1983Mos
0Hrs
0Ldg
34 A/FUnknownUnknown
RE (O/C)Vertical Gyro
08-Jul-2004Mos
10,455Hrs
5,305Ldg
No.134 A/F7000622-90280041424
RE (O/C)Vertical Gyro
20-Sep-1983Mos
0Hrs0
0Ldg0
No.234 A/FNew7000622-901
UNKNOWN
RE (O/C)Vertical Navigation Computer
03-Aug-2004Mos
10,458.3Hrs
5,306Ldg
34 A/F7004577-90285080284
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM165/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)VOR Receiver
27-Jun-2004Mos
10,421.6Hrs
5,281Ldg
Left34 A/F622-0876-20115207
RE (O/C)VOR Receiver
23-Nov-2004Mos
10,487.6Hrs83.4
5,325Ldg60
Right34 A/F622-0876-2018969
RE (O/C)VOR/ILS Antenna
20-Sep-1983Mos
0Hrs0
0Ldg0
Left34 A/FNewDMN4-17-1A
UNKNOWN
RE (O/C)VOR/ILS Antenna
20-Sep-1983Mos
0Hrs0
0Ldg0
Right34 A/FNewDMN4-17-1A
UNKNOWN
RE (O/C)VSI/TRA Indicator
09-Jul-2002Mos
8,603.4Hrs
4,190Ldg
Left34 A/F922-9728-3221444
RE (O/C)VSI/TRA Indicator
10-Nov-2003Mos
9,873.2Hrs
4,964Ldg
Right34 A/F922-9728-3221493
RE (O/C)Weather Radar Transceiver
05-Jun-2015Mos
11,940.5Hrs
6,249Ldg
34 A/FMI5582002695
Mandatory (Appliance AD)RE (-)2001-15-17 Rockwell Collins. CTL-92 - Transponder Control Panels
05-Sep-2001Mos
Hrs
Ldg
34 A/FBY PART S/N INSTALLEDEff: 20-Aug-2001 Not
Applicable
Mandatory (Appliance AD)RE (-)2002-13-07 Honeywell - Inertial Reference Units (IRU)
19-Jul-2002Mos
8,644.4Hrs
4,214Ldg
34 A/FBY IRU'S PART NUMBER INSTALLEDEff: 09-Aug-2002 Not
Applicable
Mandatory (Appliance AD)T2014-18-01 Rockwell Collins, Inc. - Navigation - inspect the airplane type code category strapping setting for a value of zero (0) or one (1) following Rockwell Collins, Inc. Service
Information Letter 07-2, 523-0810069-101000, TDR-94() SIL 07-02.
6.4 Months14-Oct-201624Mos
Hrs
Ldg
34 A/FEff: 14-Oct-2014
(AVG MAN HRS: 1) (APX COST [USD]: 85)
Mandatory (Appliance AD)T2015-0093 Paragraph (2) NORTHROP GRUMMAN LITEF GmbH - Navigation – Attitude Heading Reference System – Modification / Replacement
1.2 Years10-Jun-201724Mos
Hrs
Ldg
34 A/FEff: 10-Jun-2015
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM166/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Mandatory (Appliance AD)RE (-)2015-10-51-E EMERGENCY AD - Avidyne Integrated Flight Display (IFD) - Navigation - Incorporate Operational Limitations into Airplane Flight Manual (AFM) or Airplane Flight
Manual Supplement (AFMS) Limitation
11-Nov-2015Mos
12,012.8Hrs
6,303Ldg
34 A/FEQUIPMENT NOT INSTALLEDEff: 18-May-2015 Not
Applicable
MRB ≈18-Sep-2016RE34-11-00-201 Pitot Static System and Temperature Sensing System Visual Check
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
34 A/F
(SOURCE: TLMC 05-20-15)
MRBRE34-11-00-202 Pitot Static System and Temperature Sensing System Pitot static system moisture and contamination check
6.6 Months (+31
Days)(21-Oct-2016)-/+11221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
34 A/F
(SOURCE: TLMC 05-20-15)
MRBRE34-11-00-203 Pitot Static System and Temperature Sensing System Pressure leak tests
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
34 A/F
(SOURCE: TLMC 05-20-15)
MRBRE34-11-00-205 Pitot Static System and Temperature Sensing System Altimeter calibration check
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
34 A/F
Ref.:Section 5-20-05 Paragraph 10 Program Note G (SOURCE: TLMC 05-20-15)
MRBRE34-11-00-205 Pitot Static System and Temperature Sensing System Altimeter calibration check
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
34 A/F
Ref.:Section 5-20-05 Paragraph 10 Program Note G (SOURCE: TLMC 05-20-15)
MRBRE34-11-00-205 Pitot Static System and Temperature Sensing System Altimeter calibration check
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
34 A/F
Ref.:Section 5-20-05 Paragraph 10 Program Note G (SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE34-11-11-208 Pitot Static Heads Clean pitot drain holes
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
34 A/F
(SOURCE: TLMC 05-20-15)
AWL - RVSMRE34-13-00-101* Functional Test of the Air Data Computer
10 Months (+29
Days)30-Jan-2017-/+12430-Jan-2015Mos
Hrs
Ldg
Left34 A/F7000700-63701109199
(SOURCE: TLMC 05-10-13)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM167/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL - RVSMRE34-13-00-101* Functional Test of the Air Data Computer
10 Months (+29
Days)30-Jan-2017-/+12430-Jan-2015Mos
Hrs
Ldg
Right34 A/F7000700-63786091747
(SOURCE: TLMC 05-10-13)
MRBRE34-27-00-206 Standby Magnetic Compass - Compass Swing
6.6 Months (+31
Days)(21-Oct-2016)-/+11221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
34 A/F
PA170060345
Ref.:Section 5-20-05 Paragraph 10 Program Note G (SOURCE: TLMC 05-20-15)
Servicing - RecommendedRE (N/A)34-41-00-302 Weather Radar System (Aircraft 3050 and Subs and Post SB 601-0111) - Pressure line desiccator
11-Nov-2015Mos
Hrs
Ldg
34 A/F
(ZONE: 210) (SOURCE: MPD 3.2)
MRBRE34-54-00-207 ATC Transponder System - Functional Test
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
No.1
(PKG 24 Month)
34 A/F
622-9210-0033731
Ref.:Section 5-20-05 Paragraph 10 Program Note G (SOURCE: TLMC 05-20-15)
MRBRE34-54-00-207 ATC Transponder System - Functional Test
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
No.2
(PKG 24 Month)
34 A/F
622-6210-0033707
Ref.:Section 5-20-05 Paragraph 10 Program Note G (SOURCE: TLMC 05-20-15)
Servicing - RecommendedRE34-62-00-303 Digital Clocks - Remove and install new batteries
10 Months (+29
Days)30-Jan-2017-/+12430-Jan-2015Mos
11,862.7Hrs
6,194Ldg
Left
(PKG 24 Month)
34 A/F
811B24652
(ZONE: 220) (SOURCE: MPD 3.2)
Servicing - RecommendedRE34-62-00-303 Digital Clocks - Remove and install new batteries
10 Months (+29
Days)30-Jan-2017-/+12430-Jan-2015Mos
Hrs
Ldg
Right
(PKG 24 Month)
34 A/F
811BUNKNOWN
(ZONE: 220) (SOURCE: MPD 3.2)
Custom TaskRE34-CUS-005 24 Month RVSM Inspection Requirements
10 Months30-Jan-20172430-Jan-2015Mos
Hrs
Ldg
34 A/F
(NOTE: KSR Report R02-529 Page 1.2)
RE34-CUS-010 Capacity Check of INS Battery
15 Days21-Apr-2016621-Oct-2015Mos
12,001.1Hrs
Ldg
No.134 A/F27826-0028902788
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM168/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE34-CUS-010 Capacity Check of INS Battery.
15 Days21-Apr-2016621-Oct-2015Mos
12,001.1Hrs
Ldg
No.234 A/F27826-0029805842
OptionalRE (-)601-0053 Modification - Flight Director System - Localizer Mode
26-Jan-1987Mos
1,267Hrs
470Ldg
34 A/FComplied With
OptionalT (A/R)601-0053 Rev 1 Modification - Flight Director System - Localizer Mode
Mos
Hrs
Ldg
34 A/FEff: 29-May-1984
OptionalRE (-)601-0111 Modification - Pressurization - Waveguide Desiccator Addition
Mos
Hrs
Ldg
34 A/F
OptionalRE (-)601-0111 Rev 1 Modification - Pressurization - Waveguide Desiccator Addition
20-Jan-1987Mos
Hrs
Ldg
34 A/FEff: 05-Oct-1988 Complied With
OptionalRE (-)601-0118 Modification - Reduced Bank Angle Limit - Introduction
Mos
Hrs
Ldg
34 A/F
OptionalT (A/R)601-0118 Rev 1 Modification - Reduced Bank Angle Limit - Introduction
Mos
Hrs
Ldg
34 A/FEff: 17-Sep-1986
OptionalT (A/R)601-0128 Modification - Attitude Director Indicator - Radio Altimeter Display Range
Mos
Hrs
Ldg
34 A/FEff: 27-Sep-1985
OptionalT (A/R)601-0129 Modification - DME/Flight Director - Interface
Mos
Hrs
Ldg
34 A/FEff: 26-Sep-1985
RecommendedRE (-)601-0150 Special Check/Modification - Pitot Static System - Line Clearance
19-Jan-1987Mos
1,267Hrs
480Ldg
34 A/FEff: 20-Feb-1986 Complied With
OptionalRE (-)601-0182 Modification - Tacan System - Placard
Mos
Hrs
Ldg
34 A/FEff: 07-Apr-1986
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM169/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0226 Modification - Mach/Airspeed Indicator and Air Data Computer - VMO Warning
Mos
Hrs
Ldg
34 A/F
RecommendedRE (-)601-0226 Rev 1 Modification - Mach/Airspeed Indicator and Air Data Computer - VMO Warning
28-Oct-1988Mos
Hrs
Ldg
34 A/FEff: 16-Dec-1988 Complied With
RecommendedRE (-)601-0246 Modification - Symbol Generators - Speed Trend Vector Display
Mos
Hrs
Ldg
34 A/F
OptionalT (A/R)601-0273 Modification - Attitude and Direction Systems - Radio Magnetic and Horizontal Situation Indicators
Mos
Hrs
Ldg
34 A/FEff: 07-Dec-1988
RecommendedRE (-)601-0275 Modification - Electronic Flight Instrument System - Unit Replacement and Wiring Rework
Mos
Hrs
Ldg
34 A/F
RecommendedRE (-)601-0284 Modification - Waveguide Desiccator - Hardware Change
23-Mar-1992Mos
3,584Hrs
1,446Ldg
34 A/FEff: 05-Oct-1988 Complied With
RecommendedRE (-)601-0334 Modification - Pitot Static Lines - Improved Drainage
Mos
Hrs
Ldg
34 A/F
RecommendedRE (-)601-0334 Rev 1 Modification - Pitot Static Lines - Improved Drainage
23-Mar-1992Mos
3,584Hrs
1,446Ldg
34 A/FEff: 26-Feb-1993 Complied With
RecommendedRE (-)601-0377 Modification - Pitot-Static System - Introduction of Pitot-Static Head with Heated Base
Mos
Hrs
Ldg
34 A/F
RecommendedRE (-)601-0377 Rev 1 Modification - Pitot-Static System - Introduction of Pitot-Static Head with Heated Base
09-Oct-1992Mos
3,754Hrs
1,519Ldg
34 A/FEff: 15-Jan-1993 Complied With
RecommendedRE (-)601-0393 Pitot-Static Drain Line - Addition of Clamps and Clamping Plate
Mos
Hrs
Ldg
34 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM170/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalRE (-)601-0484 Reduced Vertical Separation Minimum (RVSM) to 1000 FT. Aircraft Qualification Requirements
14-Nov-1997Mos
5,395Hrs
2,274Ldg
34 A/FComplied With
OptionalRE (-)601-0484 Rev 1 Reduced Vertical Separation Minimum (RVSM) to 1000 FT. Aircraft Qualification Requirements
Mos
Hrs
Ldg
34 A/F
OptionalT (A/R)601-0484 Rev 2 Reduced Vertical Separation Minimum (RVSM) to 1000 FT. Aircraft Qualification Requirements
Mos
Hrs
Ldg
34 A/FEff: 30-Apr-2001
OptionalRE (-)601-0595 Modification – Standby Altitude Indicator (SAI) – Introduction of New AD20 Standby Altimeter
Mos
Hrs
Ldg
34 A/F
RecommendedRE (-)601-0617 Modification – Pitot-Static and Temperature Sensing System – Replacement of Pitot-Static Visual Drain Bottles to Larger Capacity Bottles
Mos
Hrs
Ldg
34 A/F
RecommendedRE (-)601-0617 Rev 1 Modification – Pitot-Static and Temperature Sensing System – Replacement of Pitot-Static Visual Drain Bottles to Larger Capacity Bottles
Mos
Hrs
Ldg
34 A/F
RecommendedRE (-)601-0617 Rev 2 Modification – Pitot-Static and Temperature Sensing System – Replacement of Pitot-Static Visual Drain Bottles to Larger Capacity Bottles
Mos
Hrs
Ldg
34 A/F
MandatoryT (A/R)91-10-01 Traffic Alert and Collision Avoidance Systems
Mos
Hrs
Ldg
34 A/FEff: 10-Mar-1992
FAR91RE (-)FAR 91.171 VOR - Test and Inspection per FAR 91.171
Mos
Hrs
Ldg
34 A/F
FAR91, FAR 91REFAR 91.411 Air Data Computer tests and inspections per FAR 91.411 Appendix E of Part 43
10 Months30-Jan-20172430-Jan-2015Mos
Hrs
Ldg
Left34 A/F
Inspected Date 30-Jan-2015
7000700-63701109199
FAR91, FAR 91REFAR 91.411 Air Data Computer tests and inspections per FAR 91.411 Appendix E of Part 43
10 Months30-Jan-20172430-Jan-2015Mos
Hrs
Ldg
Right34 A/F
Inspected Date 30-Jan-2015
7000700-63786091747
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM171/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
FAR91, FAR 91REFAR 91.411 Altimeter Standby Indicator tests and inspections per FAR 91.411
10 Months30-Jan-20172430-Jan-2015Mos
Hrs
Ldg
StandBy34 A/F8047-107536B
FAR91, FAR 91REFAR 91.411 Altimeter test and inspect per FAR 91.411 Appendix E part 43
10 Months30-Jan-20172430-Jan-2015Mos
Hrs
Ldg
Left34 A/F
Inspected Date 30-Jan-2015
UnknownUnknown
FAR91, FAR 91REFAR 91.411 Altimeter test and inspect per FAR 91.411 Appendix E part 43
10 Months30-Jan-20172430-Jan-2015Mos
Hrs
Ldg
Right34 A/F
Inspected Date 30-Jan-2015
UnknownUnknown
FAR91, FAR 91REFAR 91.413 ATC Transponder test and inspections per FAR 91.413 Appendix F of Part 43
10 Months30-Jan-20172430-Jan-2015Mos
Hrs
Ldg
No.134 A/F
Inspected Date 30-Jan-2015
622-9210-0033731
FAR91, FAR 91REFAR 91.413 ATC Transponder test and inspections per FAR 91.413 Appendix F of Part 43
10 Months30-Jan-20172430-Jan-2015Mos
Hrs
Ldg
No.234 A/F
Inspected Date 30-Jan-2015
622-6210-0033707
IsModSumT (A/R)IS600-34-0001 REV A Kit – Introduction of Alternate Antenna Installations with Conductive Gaskets
Mos
Hrs
Ldg
34 A/F
▼ 35 - OXYGEN
MRB, Life LimitRECrew Oxygen System , Cylinder
6.6 Years (+30 Days)05-Nov-2022-/+1m2405-Nov-1998Yrs
0Hrs0
0Ldg0
No.135 A/F
Manufactured Date 05-Nov-1998
New895-01077281-7086
TLMC:35-10-00-204, Ref:05-10-20 (SOURCE: TLMC 05-20-15, TLMC 05-10-20) (NOTE: Note: (As per CFR title 49, chapter 180.205 or in
accordance with the operator’s national requirements)
Component Inspection Tso To
TsiDUE: 20-Jan-20191. RE 60 MosOxygen Cylinder Assembly - Hydrostatic Test and Functional T...35-10-11-203A/F35
RE (O/C)Crew Oxygen System, Mask Assy
18-Dec-2014Mos
11,854.6Hrs
Ldg
No.135 A/FMC10-13-032252
Component Inspection Tso To
TsiDUE: 18-Dec-20201. RE 72 MosCrew Oxygen System - Restoration of the Oxygen Regulator Mas...35-10-00-205A/F35
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM172/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Crew Oxygen System, Mask Assy
18-Dec-2014Mos
11,854.6Hrs
Ldg
No.235 A/FMC10-13-03110851
Component Inspection Tso To
TsiDUE: 18-Dec-20201. RE 72 MosCrew Oxygen System - Restoration of the Oxygen Regulator Mas...35-10-00-205A/F35
RE (O/C)Crew Oxygen System, Mask Assy
18-Dec-2014Mos
11,854.6Hrs
Ldg
Observer35 A/F174326-078UNKNOWN
Component Inspection Tso To
TsiDUE: 18-Dec-20201. RE 72 MosCrew Oxygen System - Restoration of the Oxygen Regulator Mas...35-10-00-205A/F35
Life LimitREOxygen Cylinder Assembly
12.8 Years20-Jan-202918020-Jan-2014Mos
11,824.5Hrs
Ldg
Aft35 A/F
Manufactured Date 20-Jan-2014
895-01077281-30300
Component Inspection Tso To
TsiDUE: 20-Jan-20191. RE 60 MosOxygen Cylinder Assembly • Hydrostatic Test and Functional T...35-CUS-002A/F35
Life LimitREOxygen Cylinder Assembly
12.8 Years20-Jan-202918020-Jan-2014Mos
11,824.5Hrs
Ldg
Fwd35 A/F
Manufactured Date 20-Jan-2014
895-01015282-31610
Component Inspection Tso To
TsiDUE: 20-Jan-20191. RE 60 MosOxygen Cylinder Assembly • Hydrostatic Test and Functional T...35-CUS-002A/F35
RE (O/C)Oxygen Fill Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
35 A/FNew170080
UNKNOWN
RE (O/C)Oxygen Pressure Gauge
20-Sep-1983Mos
0Hrs0
0Ldg0
No.135 A/FNewG4225-001
UNKNOWN
RE (O/C)Oxygen Pressure Gauge
20-Sep-1983Mos
0Hrs0
0Ldg0
No.235 A/FNew171007
UNKNOWN
RE (O/C)Portable Oxygen Bottle
26-Jan-2011Mos
11,460.7Hrs
0Ldg
35 A/F5900-9CIA-YON937987
Assembly SubDUE:1. RE O/CPortable Oxygen Bottle - Regulator5900-9CIA-YON / 937987A/F35
Component Inspection Tso To
TsiDUE: 10-Feb-20211. RE 60 MosPortable Oxygen Bottle - Hydrostatic Test35-CUS-003A/F35
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM173/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Portable Oxygen Bottle - Regulator
26-Jan-2011Mos
11,460.7Hrs
0Ldg
35 A/F5900-9CIA-YON937987
Component Inspection Tso To
TsiDUE: 10-Feb-20211. RE 60 MosPortable Oxygen Bottle - Regulator - Functional Test35-CUS-004A/F35
RE (O/C)Regulator, Oxygen Cylinder Assembly
28-Mar-2014Mos
11,824.5Hrs
0Ldg
Aft35 A/F803213-01905
Component Inspection SimpleDUE: 28-Mar-20171. RE 36 MosCabin Oxygen Regulator Functional Check35-CUS-007A/F35
RE (O/C)Regulator, Oxygen Cylinder Assembly
28-Mar-2014Mos
11,824.5Hrs
0Ldg
Fwd35 A/F803213-011981
Component Inspection SimpleDUE: 28-Mar-20171. RE 36 MosCabin Oxygen Regulator Functional Check35-CUS-007A/F35
RE (O/C)Stowage - Oxygen Mask Box
20-Sep-1983Mos
0Hrs
0Ldg
No.135 A/FUnknownUnknown
RE (O/C)Stowage - Oxygen Mask Box
20-Sep-1983Mos
0Hrs
0Ldg
No.235 A/FUnknownUnknown
MandatoryT (A/R)174080-35-04 Oxygen - Passenger Oxygen System Mask In-Line Flow Indicator Replacement
Mos
Hrs
Ldg
35 A/FEff: 06-Sep-2010
(NOTE: This Service Bulletin applies to all aircraft that use passenger oxygen mask part numbers 174080-XX,174085-XX, 174095-XX, 174097-
XX, 174098-XX, and 174006-XX that were manufactured on or afterJanuary 1, 2002 and before March 1, 2006)
Mandatory (Appliance AD)RE (-)2011-01-09 B/E Aerospace - Oxygen - PBE units having PN 119003-11
08-Jul-2011Mos
11,523.8Hrs
5,970Ldg
35 A/FSB 119003-35-5Eff: 09-Feb-2011 Complied
With
(AVG MAN HRS: 1) (APX COST [USD]: 85) (NOTE: This AD applies to B/E Aerospace protective breathing equipment (PBE) units having part
number (P/N) 119003-11. Ref: BE SB 119003-35-5.)
Mandatory (Appliance AD)T2015-08-07 Paragraph (g) Zodiac Aerotechnics (formerly Intertechnique Aircraft Systems) - Oxygen - Flightcrew Oxygen Mask Regulators - Inspection
1.2 Years16-Jun-201724Mos
Hrs
Ldg
35 A/FEff: 16-Jun-2015
Mandatory (Appliance AD)T2015-08-07 Paragraph (h) Zodiac Aerotechnics (formerly Intertechnique Aircraft Systems) - Oxygen - Flightcrew Oxygen Mask Regulators - Replacement
1.2 Years16-Jun-201724Mos
Hrs
Ldg
35 A/FEff: 16-Jun-2015
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM174/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Mandatory (Appliance AD)RE (-)2015-23-09 Oxygen - Zodiac Aerotechnics (Formerly Intertechnique Aircraft Systems) Flight Crew Oxygen Mask Regulators - Inspection / Replacement Of Oxygen Mask Regulators
Mos
Hrs
Ldg
35 A/FEff: 28-Dec-2015
Nextdue Share EarliestDUE:1. RE -Oxygen - Inspect Each Flightcrew Oxygen Mask Regulator To Id...2015-23-09 Para (g)A/F35
Nextdue Share EarliestDUE:1. RE -Oxygen - Action For Affected Regulators2015-23-09 Para (h)A/F35
Nextdue Share EarliestDUE: 28-Dec-20161. T 12 Mos | 2. RE -Oxygen - Regulator Replacement2015-23-09 Para (i)A/F35
Mandatory (Appliance AD)RE (-)2015-23-09 Para (g) Oxygen - Inspect Each Flightcrew Oxygen Mask Regulator To Identify The Part Number And Serial Number
Mos
Hrs
Ldg
35 A/FEff: 28-Dec-2015
Mandatory (Appliance AD)RE (-)2015-23-09 Para (h) Oxygen - Action For Affected Regulators
Mos
Hrs
Ldg
35 A/FEff: 28-Dec-2015
Mandatory (Appliance AD)T2015-23-09 Para (i) Oxygen - Regulator Replacement
8.9 Months28-Dec-201612Mos
Hrs
Ldg
35 A/FEff: 28-Dec-2015
MRB ≈03-May-2017RE35-10-00-201 Crew Oxygen System Functional Test
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
35 A/F
(SOURCE: TLMC 05-20-15)
MRBRE35-10-00-205 Crew Oxygen System - Restoration of the Oxygen Regulator Mask Assembly
4.7 Years (+31 Days)18-Dec-2020-/+17218-Dec-2014Mos
Hrs
Ldg
No.135 A/F
Restored Date 18-Dec-2014
MC10-13-032252
Ref.:CMM/PSP 608/608A 35-13-63 (SOURCE: TLMC 05-20-15)
MRBRE35-10-00-205 Crew Oxygen System - Restoration of the Oxygen Regulator Mask Assembly
4.7 Years (+31 Days)18-Dec-2020-/+17218-Dec-2014Mos
Hrs
Ldg
No.235 A/F
Restored Date 18-Dec-2014
MC10-13-03110851
Ref.:CMM/PSP 608/608A 35-13-63 (SOURCE: TLMC 05-20-15)
MRBRE35-10-00-205 Crew Oxygen System - Restoration of the Oxygen Regulator Mask Assembly
4.7 Years18-Dec-20207218-Dec-2014Mos
Hrs
Ldg
Observer35 A/F
Restored Date 18-Dec-2014
174326-078UNKNOWN
(SOURCE: TLMC 05-20-15)
MRBRE35-10-11-203 Oxygen Cylinder Assembly - Hydrostatic Test and Functional Test of Pressure Regulator
2.8 Years (+31 Days)20-Jan-2019-/+16020-Jan-2014Mos
11,824.5Hrs
Ldg
No.135 A/F895-01077281-7086
Ref.:Section 5-20-05 Para 10 Program Note F (SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM175/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
VendorRE35-CUS-002 Oxygen Cylinder Assembly • Hydrostatic Test and Functional Test of pressure regulator
2.8 Years20-Jan-20196020-Jan-2014Mos
Hrs
Ldg
Aft35 A/F
Hydrostatic Tested Date 20-Jan-2014
895-01077281-30300
VendorRE35-CUS-002 Oxygen Cylinder Assembly • Hydrostatic Test and Functional Test of pressure regulator
2.8 Years20-Jan-20196020-Jan-2014Mos
Hrs
Ldg
Fwd35 A/F
Hydrostatic Tested Date 20-Jan-2014
895-01015282-31610
VendorRE35-CUS-003 Portable Oxygen Bottle - Hydrostatic Test
4.9 Years10-Feb-20216010-Feb-2016Mos
12,041.2Hrs
6,326Ldg
35 A/F
Hydrostatic Tested Date 10-Feb-2016
5900-9CIA-YON937987
VendorRE35-CUS-004 Portable Oxygen Bottle - Regulator - Functional Test
4.9 Years10-Feb-20216010-Feb-2016Mos
12,041.2Hrs
6,326Ldg
35 A/F5900-9CIA-YON937987
RE35-CUS-007 Cabin Oxygen Regulator Functional Check
11.9 Months28-Mar-20173628-Mar-2014Mos
11,824.5Hrs
Ldg
Aft35 A/F803213-01905
RE35-CUS-007 Cabin Oxygen Regulator Functional Check
11.9 Months28-Mar-20173628-Mar-2014Mos
11,824.5Hrs
Ldg
Fwd35 A/F803213-011981
RecommendedRE (-)601-0184 Modification - Oxygen Supply Line - Clearances
28-Mar-1989Mos
2,373Hrs
910Ldg
35 A/FEff: 16-Sep-1986 Complied With
RecommendedT (A/R)601-0614 Special Check/Modification – Crew Oxygen System – Verification and Replacement of Crew Oxygen Mask Inflatable Harness
Mos
Hrs
Ldg
35 A/FEff: 15-Aug-2011
AlertRE (-)A601-0449 Special Check/Modification - Oxygen Cylinder and EROS Pressure Regulator Assembly - Possible Loss of Oxygen Cylinder Pressure
Mos
Hrs
Ldg
35 A/F
Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Oxygen Cylinder and EROS Pressu...A601-0449 Part AA/F35
Nextdue Share EarliestDUE:1. RE -Special Check/Modification - Oxygen Cylinder and EROS Pressu...A601-0449 Part BA/F35
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Oxygen Cylinder and EROS Pressu...A601-0449 Rev 1 Part AA/F35
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Oxygen Cylinder and EROS Pressu...A601-0449 Rev 1 Part BA/F35
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM176/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AlertRE (-)A601-0449 Part A Special Check/Modification - Oxygen Cylinder and EROS Pressure Regulator Assembly - Possible Loss of Oxygen Cylinder Pressure - Cylinder pressure adjustment
Mos
Hrs
Ldg
35 A/FEff: 14-Jul-1995
AlertRE (-)A601-0449 Part B Special Check/Modification - Oxygen Cylinder and EROS Pressure Regulator Assembly - Possible Loss of Oxygen Cylinder Pressure - frangible disc replacement
Mos
Hrs
Ldg
35 A/FEff: 14-Jul-1995
AlertRE (-)A601-0449 Rev 1 Special Check/Modification - Oxygen Cylinder and EROS Pressure Regulator Assembly - Possible Loss of Oxygen Cylinder Pressure
06-Oct-1995Mos
11,455.7Hrs
5,898Ldg
35 A/FEff: 15-Aug-1995 Complied With
AlertT (A/R)A601-0449 Rev 1 Part A Special Check/Modification - Oxygen Cylinder and EROS Pressure Regulator Assembly - Possible Loss of Oxygen Cylinder Pressure - Cylinder pressure adjustment
Mos
Hrs
Ldg
35 A/FEff: 15-Aug-1995
AlertT (A/R)A601-0449 Rev 1 Part B Special Check/Modification - Oxygen Cylinder and EROS Pressure Regulator Assembly - Possible Loss of Oxygen Cylinder Pressure - frangible disc replacement
Mos
Hrs
Ldg
35 A/FEff: 15-Aug-1995
▼ 36 - PNEUMATIC
RE (O/C)10 Th Stage Bleed Air Isolation Valve
30-Jul-2002Mos
8,673.7Hrs
4,242Ldg
No.136 A/F979998-1P-185
RE (O/C)10 Th Stage Bleed Air Isolation Valve
20-Sep-1983Mos
0Hrs
0Ldg
No.236 A/FUnknownUnknown
RE (O/C)10 Th Stage Bleed Air Isolation Valve
20-Sep-1983Mos
0Hrs
0Ldg
No.336 A/FUnknownUnknown
RE (O/C)Bleed Air Pressure Indicator
20-Sep-1983Mos
0Hrs
0Ldg
36 A/FUnknownUnknown
RE (O/C)Bleed Air Shutoff Valve
03-Dec-2015Mos
12,019Hrs
6,308Ldg
Left36 A/F3289590-33419
RE (O/C)Bleed Air Shutoff Valve
04-Aug-2002Mos
8,685.2Hrs
4,252Ldg
Right36 A/F3289590-2P-128
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM177/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Check Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Left36 A/FNew3202232-1
UNKNOWN
RE (O/C)Check Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Right36 A/FNew3202232-1
UNKNOWN
RE (O/C)Engine Bleed Air Check Valve
20-Sep-1983Mos
0Hrs
0Ldg
Left36 A/FUnknownUnknown
RE (O/C)Engine Bleed Air Check Valve
20-Sep-1983Mos
0Hrs
0Ldg
Right36 A/FUnknownUnknown
RE (O/C)Engine Bleed Air Controller
20-Sep-1983Mos
0Hrs0
0Ldg0
Left36 A/FNew35008-32
N/A
RE (O/C)Engine Bleed Air Controller
20-Sep-1983Mos
0Hrs0
0Ldg0
Right36 A/FNew35008-32
N/A
RE (O/C)Pressure Regulating Shutoff Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Left36 A/FNew3214066-1
UNKNOWN
RE (O/C)Pressure Regulating Shutoff Valve
01-Apr-2004Mos
10,259.2Hrs
5,182Ldg
Right36 A/F898930-7-2811
RE (O/C)Pressure Transducer
20-Sep-1983Mos
0Hrs
0Ldg
No.136 A/FUnknownUnknown
RE (O/C)Pressure Transducer
20-Sep-1983Mos
0Hrs
0Ldg
No.236 A/FUnknownUnknown
MRB ≈03-May-2017RE36-10-00-201 Bleed Air Distribution Visual Check - Ducting
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
36 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM178/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0152 Modification - APU Bleed Air Duct - Check Valve Relocation
Mos
Hrs
Ldg
36 A/F
RecommendedRE (-)601-0152 Rev 1 Modification - APU Bleed Air Duct - Check Valve Relocation
Mos
Hrs
Ldg
36 A/F
RecommendedRE (-)601-0152 Rev 2 Modification - APU Bleed Air Duct - Check Valve Relocation
02-May-1988Mos
Hrs
Ldg
36 A/FEff: 01-Jun-1987 Complied With
RecommendedRE (-)601-0200 Special Check/Modification - Manifold Support Rod Assemblies - Thread-Inspection Holes
22-May-1988Mos
1,995Hrs
756Ldg
36 A/FEff: 20-Oct-1987 Complied With
RecommendedRE (-)601-0268 Modification - Aircraft Data Plate - Relocation
02-May-1988Mos
1,995Hrs
756Ldg
36 A/FEff: 22-Feb-1988 Complied With
RecommendedRE (-)601-0288 Special Check/Modification - Bleed Air Distribution - Tenth and Fourteenth Stage Duct Assembly Bleed Hole Location
Mos
Hrs
Ldg
36 A/F
RecommendedRE (-)601-0288 Rev 1 Special Check/Modification - Bleed Air Distribution - Tenth and Fourteenth Stage Duct Assembly Bleed Hole Location
Mos
Hrs
Ldg
36 A/F
RecommendedT (A/R)601-0288 Rev 2 Special Check/Modification - Bleed Air Distribution - Tenth and Fourteenth Stage Duct Assembly Bleed Hole Location
Mos
Hrs
Ldg
36 A/FEff: 30-Aug-1991
RecommendedRE (-)601-0460 Modification - APU Bleed Air Duct - Check Valve Reliability Improvement
18-Nov-1996Mos
5,001Hrs
2,052Ldg
36 A/FEff: 29-Feb-1996 Complied With
RecommendedRE (-)601-0600 Modification – Bleed-Air Leak Detection System – 10th Stage Bleed-Air Pressure Transducers Relocation
Mos
Hrs
Ldg
36 A/F
RecommendedT (A/R)601-0600 Rev 1 Modification – Bleed-Air Leak Detection System – 10th Stage Bleed-Air Pressure Transducers Relocation
Mos
Hrs
Ldg
36 A/FEff: 12-Sep-2012
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM179/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
▼ 38 - WATER/WASTE
RE (O/C)Galley Drain Mast
20-Sep-1983Mos
0Hrs
0Ldg
Fwd38 A/FUnknownUnknown
OptionalT (A/R)601-0606 Increase Inspection Interval for Lavatory Adjacent Structure
Mos
Hrs
Ldg
38 A/FEff: 14-Dec-2009
▼ 39 - ELECTRICAL - ELECTRONIC PANELS AND MULTIPURPOSE COMPONENTS
RecommendedRE (-)601-0009 Modification - Center Pedestal - Replacement of Landing and Taxi Lights Control Panel
17-Sep-1985Mos
607Hrs
262Ldg
39 A/FEff: 10-Jun-1983 Complied With
RecommendedRE (-)601-0101 Modification - JB2 and JB3 Connectors - Mating Assurance
Mos
Hrs
Ldg
39 A/F
RecommendedRE (-)601-0101 Rev 1 Modification - JB2 and JB3 Connectors - Mating Assurance
28-Mar-1989Mos
2,373Hrs
910Ldg
39 A/FEff: 14-Feb-1985 Complied With
RecommendedRE (-)601-0140 Modification - Terminal Block Mounted Component Boards - Isolation
26-Jan-1987Mos
1,267Hrs
480Ldg
39 A/FEff: 28-May-1985 Complied With
RecommendedRE (-)601-0291 Special Check/Modification - Pilot and Copilot Side Consoles- Elimination of Possible Wire Chafing
09-Mar-1989Mos
2,373Hrs
910Ldg
39 A/FEff: 12-Dec-1988 Complied With
OptionalT (A/R)601-0439 Modification - Center-Pedestal Panel Assemblies - Improved Air Flow
Mos
Hrs
Ldg
39 A/FEff: 15-Jun-1994
▼ 49 - AIRBORNE AUXILIARY POWER
RE (O/C)APU - APU Pneu Surge Valve
20-Sep-1983Mos
0Hrs0
0APUS0
49 APU1New978668-3-1
UNKNOWN
RE (O/C)APU - Bleed Air Check APU Valve
01-Sep-1983Mos
0Hrs
0APUS
49 APU1UnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM180/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)APU - Fuel Control Unit APU Fcu
31-Mar-2002Mos
4,756.3Hrs
4,756APUS
49 APU13882600-817679
RE (O/C)APU - Fuel Nozzle
03-Mar-2004Mos
6,114.2Hrs
6,114APUS
49 APU13830061-51VS07084
RE (O/C)APU - Fuel Solenoid Valve
01-Sep-1983Mos
0Hrs0
0APUS0
49 APU1New3888134-4
97-405
RE (O/C)APU - Hourmeter
01-Sep-1983Mos
0Hrs0
0APUS0
49 APU1New3888033-4
UNKNOWN
RE (O/C)APU - Igniter Plug
01-Sep-1983Mos
0Hrs
0APUS
49 APU1UnknownUnknown
RE (O/C)APU - Immersion Thermocouple
01-Sep-1983Mos
0Hrs0
0APUS0
49 APU1New3876003-1
020219-150
RE (O/C)APU - Low Oil Pressure Switch
03-Mar-2004Mos
6,114.2Hrs
6,114APUS
49 APU13876001-106032
RE (O/C)APU - Low Oil Pressure Switch
01-Sep-1983Mos
0Hrs
0APUS
49 APU1UnknownUnknown
RE (O/C)APU - Motion Pick Up Transducer
03-Mar-2004Mos
6,114.2Hrs
6,114APUS
49 APU13876000-18-05104-134
RE (O/C)APU - Oil Pressure Regulating Valve
01-Sep-1983Mos
0Hrs0
0APUS0
49 APU1New3880021-2
UNKNOWN
RE (O/C)APU - Oil Temperature High Switch
03-Mar-2004Mos
6,114.2Hrs
6,114APUS
49 APU13888030-10338
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM181/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)APU - Orifice Fitting
01-Sep-1983Mos
0Hrs
0APUS
49 APU1UnknownUnknown
RE (O/C)APU - Orifice Fitting
01-Sep-1983Mos
0Hrs
0APUS
49 APU1UnknownUnknown
RE (O/C)APU - Pneumatic Shutoff Valve
01-Sep-1983Mos
0Hrs0
0APUS0
49 APU1New109776-5
789C
RE (O/C)APU - Rotary Oil Pump
01-Sep-1983Mos
0Hrs0
0APUS0
49 APU1New3880000-2
UNKNOWN
RE (O/C)APU - Unit APU Ignition
01-Sep-1983Mos
0Hrs
0APUS
49 APU1UnknownUnknown
MRB, Life LimitRE (O/C)APU Bleed Air Supply / Bleed Air Manifold Check Valve
01-Sep-1983Mos
0Hrs
0APUS
49 APU1UnknownUnknown
TLMC:49-52-00-214, Ref.:Section 5-20-05 Para 10 Program Note E (SOURCE: TLMC 05-20-15)
RE (O/C)APU Control Panel
20-Sep-1983Mos
0Hrs0
0Ldg0
49 A/FNew600-51158-823
UNKNOWN
RE (O/C)APU EGT Indicator
20-Sep-1983Mos
0Hrs
0Ldg
49 A/FUnknownUnknown
RE (O/C)APU Fault Indicator
20-Sep-1983Mos
0Hrs0
0Ldg0
49 A/FNew601-53004-5
UNKNOWN
RE (O/C)APU Fuel Booster Pump
20-Sep-1983Mos
0Hrs
0Ldg
49 A/FUnknownUnknown
RE (O/C)APU RPM Indicator
20-Sep-1983Mos
0Hrs
0Ldg
49 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM182/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)APU Starter Motor
01-Sep-1983Mos
0Hrs
0APUS
49 APU1UnknownUnknown
Component Inspection SimpleDUE:1. RE N/AAPU Starter Motor (Part Number 519892-3, -4 and -5) - Remove...49-42-01-212APU149
Component Inspection SimpleDUE: 9,862 Hrs1. RE 2100 HrsAPU Starter Motor (Part Number 519892-6) - Remove, inspect a...49-42-01-219APU149
Life Limit ≈15-Aug-2182REAuxiliary Power Unit (APU) Compressor Rotor
22-Apr-2003Mos
92,141 Hrs100,000100,0005,549.2Hrs5,549.2
92,141 APUS100,000100,0005,549APUS5,549
49 APU1Overhauled3822101
001365100738
Life Limit ≈12-Apr-2031REAuxiliary Power Unit (APU) Turbine Rotor
20-Sep-2002Mos
7,355.9 Hrs15,214.910,0005,214.9Hrs0
7,355 APUS15,21410,0005,214APUS0
49 APU1New3615880-1
020134504309
RE (O/C)Electric Control Unit (APU ECU)
20-Sep-1983Mos
0Hrs
0Ldg
49 A/FUnknownUnknown
MRB ≈03-Apr-2016RE49-10-00-201 APU Power Plant - Remove and inspect combustion chamber, reinstall combustion chamber / Remove, clean, inspect and reinstall fuel nozzle assembly
10-Jan-2008Mos
145 Hrs (+40)8,004-/+404007,604Hrs
APUS
49 APU1
(SOURCE: TLMC 05-20-15)
MRBRE (N/A)49-10-00-205 APU Power Plant (Pre - any of the three following combinations of SB’s: GTCP 36-49-6057 and -6052, GTCP 36-49-6057 and -6074, GTCP 36-49-6057 and -6106) - Hot
section inspection and visual check of compressor rotor
Mos
Hrs
APUS
49 APU1
Ref.:PSP 608/608A Chapter 49-21-59 Section 49-20-00 (SOURCE: TLMC 05-20-15)
MRB ≈11-Sep-2016RE49-10-00-206 APU Power Plant (Post - any of the three following combinations of SB’s: GTCP 36-49-6057 and -6052, GTCP 36-49-6057 and -6074, GTCP 36-49-6057 and -6106) - Hot
section inspection and visual check of compressor rotor
03-Mar-2004Mos
355.2 Hrs (+40)8,214.2-/+402,1006,114.2Hrs
APUS
49 APU1
Ref.:PSP 608/608A Chapter 49-21-59 Section 49-20-00 (SOURCE: TLMC 05-20-15)
MRB ≈03-Apr-2016RE49-10-00-207 APU Power Plant - Remove, clean and carry out a visual check and reinstall combustor/plenum drain valves/orifice fittings
10-Jan-2008Mos
145 Hrs (+40)8,004-/+404007,604Hrs
APUS
49 APU1
Ref.:PSP 608/608A Chapter 49-21-59 Section 49-30-24 (SOURCE: TLMC 05-20-15)
MRB ≈03-Apr-2016RE49-10-10-202 APU Enclosure - Visual check
10-Jan-2008Mos
145 Hrs (+40)8,004-/+404007,604Hrs
APUS
49 APU1
(SOURCE: TLMC 05-20-15)
MRB ≈03-Apr-2016RE49-10-60-220 APU Air Intake and Supply/ APU Exhaust Duct - Visual Check of intake and exhaust, paying particular attention to adjacent skin and associated ducting
10-Jan-2008Mos
145 Hrs (+40)8,004-/+404007,604Hrs
APUS
49 APU1
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM183/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈03-Feb-2016RE49-30-10-208 APU Fuel Supply Filter (Post SB 601-0060) Remove, inspect and install new element
25-Jul-2008Mos
0 Hrs (+30.8)12,032-/+4060011,432Hrs
Ldg
49 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-Apr-2016RE49-31-02-209 APU Fuel Control Unit Fuel Filter - Remove, inspect and install new element
10-Jan-2008Mos
145 Hrs (+40)8,004-/+404007,604Hrs
APUS
49 APU1
Ref.:PSP 608/608A Chapter 49-21-59 Section 49-30-52 (SOURCE: TLMC 05-20-15)
MRBRE49-40-00-211 APU Starting and Ignition (Post SB 601-0099 and A/C 3045 to 3099) - Battery requirements - Battery Check
6.6 Months (+31
Days)(21-Oct-2016)1221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
49 A/F
Ref.:PSP 608/608A Section 24-30-03 (SOURCE: TLMC 05-20-15) (NOTE: Applicable to APU Model GTCP 36-100 Only)
MRBRE (N/A)49-42-01-212 APU Starter Motor (Part Number 519892-3, -4 and -5) - Remove, inspect and reinstall
Mos
Hrs
APUS
49 APU1UnknownUnknown
Ref.:PSP 608/608A Chapter 49-21-59 Section 49-40-35 (SOURCE: TLMC 05-20-15)
MRB ≈17-Feb-2020RE49-42-01-219 APU Starter Motor (Part Number 519892-6) - Remove, inspect and reinstall
20-May-2009Mos
2,003 Hrs9,8622,1007,762Hrs
APUS
49 APU1UnknownUnknown
Ref.:PSP 608/608A Chapter 49-21-59 Section 49-40-35 (SOURCE: TLMC 05-20-15)
MRB ≈03-Apr-2016RE49-43-02-213 APU Igniter Plug - Remove, clean, carry out a visual check and reinstall
10-Jan-2008Mos
145 Hrs (+40)8,004-/+404007,604Hrs
APUS
49 APU1
Ref.:PSP 608/608A Chapter 49-21-59 Section 49-40-35 (SOURCE: TLMC 05-20-15)
Servicing - OptionalRE (N/A)49-51-00-301 APU General - Restoration (On-Wing Cleaning) of the Auxiliary Power Unit (APU) Load Control Valve Filter
Mos
Hrs
APUS
49 APU1
(ZONE: 311, 312) (ACCESS: 311-BB-BZ) (SOURCE: MPD 3.3) (NOTE: This task applies to filter installed on APU 36-150CL Load Control Valve,
Part No. 3885091-4 only.)
MRB ≈03-Apr-2016RE49-90-00-216 APU Engine Oil System/Auxiliary Power Unit - Drain APU Oil Tank / Fill empty APU Oil Tank
10-Jan-2008Mos
145 Hrs (+40)8,004-/+404007,604Hrs
APUS
49 APU1
(SOURCE: TLMC 05-20-15) (NOTE: Operators participating in the Spectrometric Oil and Filter Analysis Program shall change lubricating oil and
oil filter element as directed in Allied-Signal Aerospace Service Information Letter (SIL) APU-49.)
MRBRE49-90-01-217 APU Magnetic Drain Plug - Remove magnetic element from drain plug, carry out a visual check and reinstall
44 Days (+31)20-May-2016-/+11220-May-2015Mos
400 Hrs (+40)8,259-/+404007,859Hrs
APUS
49 APU1
Ref.:PSP 608/608A Chapter 49-21-59 Section 49-90-48 (SOURCE: TLMC 05-20-15)
MRB ≈03-Apr-2016RE49-90-02-218 APU Engine Oil System Oil Filter - Remove, inspect and install new element
10-Jan-2008Mos
145 Hrs (+40)8,004-/+404007,604Hrs
APUS
49 APU1
Ref.:PSP 608/608A Chapter 49-21-59 Section 49-90-47 (SOURCE: TLMC 05-20-15) (NOTE: Operators participating in the Spectrometric Oil and
Filter Analysis Program shall change lubricating oil and oil filter element as directed in Allied-Signal Aerospace Service Information Letter (SIL)
APU-49.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM184/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0017 Modification - APU Inlet Duct Screen - Replacement
Mos
Hrs
Ldg
49 A/FEff: 17-Jan-1984
RecommendedRE (-)601-0054 Modification - APU Exhaust Duct - Addition of Shield
21-Mar-1985Mos
451Hrs
195Ldg
49 A/FEff: 02-Mar-1984 Complied With
RecommendedRE (-)601-0060 Modification - Auxiliary Power Unit - Fuel Supply
Mos
Hrs
Ldg
49 A/F
RecommendedRE (-)601-0060 Rev 1 Modification - Auxiliary Power Unit - Fuel Supply
Mos
Hrs
Ldg
49 A/F
RecommendedRE (-)601-0060 Rev 2 Modification - Auxiliary Power Unit - Fuel Supply
Mos
Hrs
Ldg
49 A/F
RecommendedRE (-)601-0060 Rev 3 Modification - Auxiliary Power Unit - Fuel Supply
02-May-1988Mos
Hrs
Ldg
49 A/FEff: 27-Oct-1989 Complied With
RecommendedRE (-)601-0064 Modification - APU Fuel Pump Control - Deletion of Connecting JB3 Wiring
01-Sep-1983Mos
0Hrs
0Ldg
49 A/FEff: 16-Apr-1984 Complied With
RecommendedRE (-)601-0068 Modification - APU Inler Duct - Damping Tape
Mos
Hrs
Ldg
49 A/FEff: 18-Jun-1984
RecommendedRE (-)601-0076 Special Check/Modification - APU Negative “G” Fuel Shroud - Drain Holes
18-Sep-1985Mos
607Hrs
261Ldg
49 A/FEff: 07-Jun-1984 Complied With
OptionalRE (-)601-0099 Modification - APU Start - Improvements
Mos
Hrs
Ldg
49 A/F
OptionalT (A/R)601-0099 Rev 1 Modification - APU Start - Improvements
Mos
Hrs
Ldg
49 A/FEff: 23-Sep-1986
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM185/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalT (A/R)601-0156 Modification - APU Enclosure - Fireproof Lining Improvements and Exhaust Duct Drainage Relocation
Mos
Hrs
Ldg
49 A/FEff: 12-Jan-1987
RecommendedRE (-)601-0172 Modification - APU Control - Introduction of Diodes
Mos
Hrs
Ldg
49 A/F
RecommendedRE (-)601-0172 Rev 1 Modification - APU Control - Introduction of Diodes
16-Jul-1986Mos
952Hrs
403Ldg
49 A/FEff: 12-Jun-1990 Complied With
RecommendedRE (-)601-0212 Modification - Exhaust Shield Assy - Replacement of Spacers
02-May-1988Mos
1,995Hrs
756Ldg
49 A/FEff: 29-May-1987 Complied With
OptionalT (A/R)601-0254 Modification - APU Installation - Spiral Wrap Addition
Mos
Hrs
Ldg
49 A/FEff: 11-Dec-1987
RecommendedRE (-)601-0290 Modification - Exhaust Shield - Crack Prevention
31-Oct-1993Mos
Hrs
Ldg
49 A/FComplied With
RecommendedRE (-)601-0290 Rev 1 Modification - Exhaust Shield - Crack Prevention
Mos
Hrs
Ldg
49 A/F
RecommendedT (A/R)601-0290 Rev 2 Modification - Exhaust Shield - Crack Prevention
Mos
Hrs
Ldg
49 A/FEff: 15-May-1993
OptionalT (A/R)601-0313 Modification - APU Gearbox - Oil Case Vent Fitting and Drain Adaptor
Mos
Hrs
Ldg
49 A/FEff: 14-Sep-1990
OptionalT (A/R)601-0455 Auxiliary Power Unit (APU) - High Voltage Ignition System (HVIS) - Modification - Fuel Return-Hose and Wire Bundle Clamps
Mos
Hrs
Ldg
49 A/FEff: 15-Aug-1995
OptionalT (A/R)601-0463 Modification - Auxiliary Battery System - HEATER/CHARGER ON/OFF Switch Removal
Mos
Hrs
Ldg
49 A/FEff: 29-Nov-1996
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM186/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalRE (-)601-0468 Modification - APU Gearbox Vent Line - Routing Improvement
Mos
Hrs
Ldg
49 A/F
OptionalT (A/R)601-0468 Rev 1 Modification - APU Gearbox Vent Line - Routing Improvement
Mos
Hrs
Ldg
49 A/FEff: 28-Nov-1997
RecommendedRE (-)601-0485 Modification - APU Enclosure - Improve Leak Resistance and Drainage
Mos
Hrs
Ldg
49 A/F
RecommendedRE (-)601-0485 Rev 1 Modification - APU Enclosure - Improve Leak Resistance and Drainage
Mos
Hrs
Ldg
49 A/F
RecommendedRE (-)601-0485 Rev 2 Modification - APU Enclosure - Improve Leak Resistance and Drainage
Mos
Hrs
Ldg
49 A/F
RecommendedRE (-)601-0485 Rev 3 Modification - APU Enclosure - Improve Leak Resistance and Drainage
Mos
Hrs
Ldg
49 A/F
RecommendedT (A/R)601-0485 Rev 4 Modification - APU Enclosure - Improve Leak Resistance and Drainage
Mos
Hrs
Ldg
49 A/FEff: 10-Mar-2010
RecommendedRE (-)601-0504 Modification - APU Exhaust - Replace Drain Tube, Part No. 601-97092-29 with Heat Resistant Tube, Part No. 601-97092-65
05-Nov-1998Mos
5,824Hrs
2,521Ldg
49 A/FEff: 15-Jul-1998 Complied With
RecommendedRE (-)601-0528 Special Check/Modification - Auxiliary Power Unit (APU) - Prevention of Fuselage Skin Heat Damage Under and Aft of the APU Exhaust Shield
06-Sep-2001Mos
7,694.9Hrs
3,648Ldg
49 A/FEff: 17-Oct-2000 Complied With
OptionalRE (-)601-0568 Modification - General - Introduction of the 36-150 (CL) Auxiliary Power Unit (APU)
Mos
Hrs
Ldg
49 A/F
OptionalT (A/R)601-0568 Rev 1 Modification - General - Introduction of the 36-150 (CL) Auxiliary Power Unit (APU)
Mos
Hrs
Ldg
49 A/FEff: 16-Apr-2007
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM187/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedT (A/R)601-0573 Modification - APU Bleed Air Supply - Installation of the Restrictor in the APU Bleed Air Ducting
Mos
Hrs
Ldg
49 A/FEff: 21-Jul-2005
OptionalRE (-)601-0580 Modification - General - Installation of Provisions for the 36-150 (CL) Auxiliary Power Unit (APU)
Mos
Hrs
Ldg
49 A/F
OptionalRE (-)601-0580 Rev 1 Modification - General - Installation of Provisions for the 36-150 (CL) Auxiliary Power Unit (APU)
Mos
Hrs
Ldg
49 A/FEff: 28-May-2007
OptionalRE (-)601-0581 Modification – General – Activation of the 36-150 (CL) Auxiliary Power Unit (APU)
Mos
Hrs
Ldg
49 A/FEff: 11-Feb-2008
OptionalT (A/R)601-0588 Modification - Exhaust - Introduction of the 36-150 (CL) Auxiliary Power Unit (APU) Stainless Steel Exhaust Extension
Mos
Hrs
Ldg
49 A/FEff: 17-Mar-2008
RecommendedRE (-)601-0615 Special Check/Modification – Auxiliary Power Unit (APU) Engine Oil System – Replacement of the APU Oil Filter Element
Mos
Hrs
Ldg
49 A/F
RecommendedT (A/R)601-0615 Rev 1 Special Check/Modification – Auxiliary Power Unit (APU) Engine Oil System – Replacement of the APU Oil Filter Element
Mos
Hrs
Ldg
49 A/FEff: 14-Nov-2011
AlertRE (-)A601-0074 Special Check/Modification - APU Exhaust - Nozzle
Mos
Hrs
Ldg
49 A/FBY DATE OF MANUFACTUREEff: 16-Nov-1984 Not
Applicable
RE (O/C)APU Auxiliary Power Unit (APU)
20-Sep-1983Mos
0Hrs
0Ldg
49 A/FUnknownUnknown
RE (-)D200906000072 Airborne Auxiliary Power - Gas Turbine Engine - Standard Storage And Preservation Guidelines
Mos
Hrs
APUS
49 APU1
RE (-)D200906000072 Rev 1 Airborne Auxiliary Power - Gas Turbine Engine - Standard Storage And Preservation Guidelines
Mos
Hrs
APUS
49 APU1
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM188/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (-)D200906000072 Rev 2 Airborne Auxiliary Power - Gas Turbine Engine - Standard Storage And Preservation Guidelines
Mos
Hrs
APUS
49 APU1
RE (-)D200906000072 Rev 3 Airborne Auxiliary Power - Gas Turbine Engine - Standard Storage And Preservation Guidelines
Mos
Hrs
APUS
49 APU1
T (A/R)D200906000072 Rev 4 Airborne Auxiliary Power - Gas Turbine Engine - Standard Storage And Preservation Guidelines
Mos
Hrs
APUS
49 APU1Eff: 12-Jan-2015
RE (-)D201110000029 Airborne Auxiliary Power Unit (APU) - Oil - General - Approved Oils
Mos
Hrs
APUS
49 APU1
RE (-)D201110000029 Rev 1 Airborne Auxiliary Power Unit (APU) - Oil - General - Approved Oils
Mos
Hrs
APUS
49 APU1
RE (-)D201110000029 Rev 2 Airborne Auxiliary Power Unit (APU) - Oil - General - Approved Oils
Mos
Hrs
APUS
49 APU1
RE (-)D201110000029 Rev 3 Airborne Auxiliary Power Unit (APU) - Oil - General - Approved Oils
Mos
Hrs
APUS
49 APU1
RE (-)D201110000029 Rev 4 Airborne Auxiliary Power Unit (APU) - Oil - General - Approved Oils
Mos
Hrs
APUS
49 APU1
T (A/R)D201110000029 Rev 5 Airborne Auxiliary Power Unit (APU) - Oil - General - Approved Oils
Mos
Hrs
APUS
49 APU1Eff: 23-Oct-2014
Service Information LetterRE (-)SIL No. APU-49 Revision 7 Implementation Of The Honeywell Spectrometric Oil And Filter Analysis Program (SOAP) For Honeywell Auxiliary Power Units (Apu’s)
Mos
Hrs
APUS
49 APU1Eff: 05-May-2003
Service Information LetterRE (-)SIL No. APU-49 Revision 8 Implementation Of The Honeywell Spectrometric Oil And Filter Analysis Program (SOAP) For Honeywell Auxiliary Power Units (Apu’s)
Mos
Hrs
APUS
49 APU1Eff: 11-Apr-2008
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM189/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Service Information Letter ≈19-Jun-2016RESIL No. APU-49 Revision 9 Implementation Of The Honeywell Spectrometric Oil And Filter Analysis Program (SOAP) For Honeywell Auxiliary Power Units (Apu’s)
10-Jan-2008Mos
245 Hrs8,1045007,604Hrs
APUS
49 APU1Complied With
(NOTE: The SOAP and filter analysis program was initially limited to the operators of the GTCP36-100/-150 Series Auxiliary Power Units
enrolled in the Honeywell Engines, Systems & Services APU Maintenance Service Plan (MSP). The program is now offered to all operators of
the Honeywell GTCP36-100/-150, RE100 and RE220 Series APUs.)
▼ 52 - DOORS
RE (O/C)Gas Passenger Door Spring
25-Jul-2008Mos
11,432Hrs
5,881Ldg
Aft52 A/F601R331911-7UNKNOWN
RE (O/C)Main Door Gas Spring
25-Jul-2008Mos
11,432Hrs
5,881Ldg
Fwd52 A/F601R331911-7UNKNOWN
RE (O/C)Mechanism Baggage Door Latch
20-Sep-1983Mos
0Hrs0
0Ldg0
52 A/FNew600-35025-1
UNKNOWN
MRB ≈18-Sep-2016RE52-00-00-201 Doors Visual Check of passenger/crew entrance door seal
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
52 A/F
(SOURCE: TLMC 05-20-15)
AWL ≈23-Oct-2017RE52-10-00-101 * Passenger Door Hinge - NDT Check
22-Jul-2004Mos
817.1 Hrs12,858.32,40010,458.3Hrs
Ldg
52 A/F
Ref.:PSP 612 Part 6 ET-52-10-01 (SOURCE: TLMC 05-10-30)
MRB ≈18-Sep-2016RE52-10-00-202 Passenger/Crew Entrance Door Visual Check that water drains are clear
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
52 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE52-12-00-203 Downward Opening Passenger/Crew Entrance Door Visual Check of hinge, paying particular attention to cracking and corrosion of the lugs (without disassembly of the
hinge)
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
52 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE (N/A)52-12-00-204 Downward Opening Door (Pre SB 601-0451) Internally Lubricate Passenger/Crew Entrance Door
Mos
812.3 Hrs (+40)(12,853.5)Hrs
Ldg
(PKG 1200 Hour)
52 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE52-12-00-205 Downward Opening Passenger/Crew Entrance Door Visual Check of all structure, paying particular attention to thefollowing: (1) Latch torque tube support brackets
and surrounding structure / (2) Tension rods (3) Underside of stair treads and angles
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
52 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM190/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈20-Oct-2017RE52-12-00-206 Downward Opening Passenger/Crew Entrance Door Functional Test
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
52 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE52-12-00-212 Downward Opening Passenger/Crew Entrance Door Scheduled Servicing Visual Check (External)- Externally Lubricate Passenger/Crew Entrance Door
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
52 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE52-12-00-213 Downward Opening Passenger/Crew Entrance Door Cam Latch Mechanism Functional Test
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
52 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE52-12-00-215 Downward Opening Door (Post SB 601-0451) Internally Lubricate Passenger/Crew Entrance Door
29-Oct-2012Mos
812.3 Hrs (+40)12,853.5-/+401,20011,653.5Hrs
Ldg
52 A/F
(SOURCE: TLMC 05-20-15)
AWL ≈10-Jan-2021RE52-20-00-103 * Overwing Emergency Exit - Attachment Fittings - Visual Check
21-Oct-2015Mos
2,359.9 Hrs14,401.12,40012,001.1Hrs
Ldg
52 A/F
Ref.:PSP 612 Part 9 VC-52-20-01 (SOURCE: TLMC 05-10-30)
MRBRE52-20-00-207 Overwing Emergency Exit Operational Test
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
52 A/F
(SOURCE: TLMC 05-20-15)
MRBRE52-20-00-208 Overwing Emergency Exit Betalight brightness check
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
52 A/F
(SOURCE: TLMC 05-20-15)
MRBRE52-20-00-209 Overwing Emergency Exit Visual Check of all structure, paying particular attention to the stops, fittings, attachments and to the door seal
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
52 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosOverwing Emergency Exit Door, External - CPCP Check includin...C52-00-801A/F52
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosOverwing Emergency Exit Door (Internal) - CPCP Check includi...C52-00-806A/F52
MRBRE52-20-00-216 Overwing Emergency Exit Lubricate the Overwing Emergency Exit Door
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
52 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM191/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE52-30-00-210 Baggage Compartment Door Visual Check of all structure, paying particular attention to the door alignment crotch fittings, surrounding structure and the door seal
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
52 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosBaggage Compartment Door Structure - CPCP Check including th...C52-00-802A/F52
MRB ≈20-Oct-2017RE52-70-00-211 Door Warning Functional Test - Baggage Door Switches- Functional Test - Passenger/Crew Entrance Door Switches
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
52 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE52-70-00-214 Door Warning - Passenger/Crew Entrance Door Switches Operational Test
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
52 A/F
(SOURCE: TLMC 05-20-15)
AWL ≈03-Feb-2016RE52-80-00-102 * Main Landing Gear Door Hinges - Visual Check
25-Jul-2008Mos
OVD12,03260011,432Hrs
Ldg
52 A/F
Ref.:PSP 612 Part 9 VC-52-10-03 (SOURCE: TLMC 05-10-30) (NOTE: Hinge sector 600-31587-1/2 not installed)
OptionalRE (-)601-0021 Modification - Baggage Compartment Door - Introduction of Interior Handle
Mos
Hrs
Ldg
52 A/F
OptionalRE (-)601-0021 Rev 1 Modification - Baggage Compartment Door - Introduction of Interior Handle
Mos
Hrs
Ldg
52 A/FEff: 27-Apr-1984
RecommendedRE (-)601-0065 Modification - Passenger/Crew Entrance Door - Addition of Strengthening Angles
18-Sep-1985Mos
607Hrs
261Ldg
52 A/FComplied With
RecommendedT (A/R)601-0065 Rev 1 Modification - Passenger/Crew Entrance Door - Addition of Strengthening Angles
Mos
Hrs
Ldg
52 A/FEff: 07-Mar-1985
RecommendedRE (-)601-0192 Modification - Passenger/Crew Entrance Door - Introduction of Improved Cranks and Collar
01-Dec-1990Mos
3,058.6Hrs
1,212Ldg
52 A/FEff: 23-Feb-1987 Complied With
OptionalT (A/R)601-0207 Modification - Overwing Emergency Exit - Improved Latch Mechanism
Mos
Hrs
Ldg
52 A/FEff: 08-Jun-1988
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM192/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalRE (-)601-0215 Modification - Baggage Door Proximity Switches - Mounting
Mos
Hrs
Ldg
52 A/F
OptionalT (A/R)601-0215 Rev 1 Modification - Baggage Door Proximity Switches - Mounting
Mos
Hrs
Ldg
52 A/FEff: 10-Jul-1992
OptionalT (A/R)601-0218 Modification - Passenger/Crew Entrance Door - Pull-out Handle
Mos
Hrs
Ldg
52 A/FEff: 12-Jan-1988
OptionalRE (-)601-0236 Modification - Passenger/Crew Entrance Door - Seal Improvement
02-May-1988Mos
1,995Hrs
756Ldg
52 A/FEff: 30-Sep-1987 Complied With
OptionalT (A/R)601-0270 Modification - Passenger/Crew Entrance Door - Support Mechanism Improvement
Mos
Hrs
Ldg
52 A/FEff: 23-Jan-1989
RecommendedRE (-)601-0335 Special Check/Modification - Passenger Door Stair Counterbalance System - Structure Reinforcement
Mos
Hrs
Ldg
52 A/F
RecommendedT (A/R)601-0335 Rev 1 Special Check/Modification - Passenger Door Stair Counterbalance System - Structure Reinforcement
Mos
Hrs
Ldg
52 A/FEff: 26-Aug-1991
OptionalT (A/R)601-0357 Modification - Downward Opening Door - Introduction of Reinforced Stair Assemblies
Mos
Hrs
Ldg
52 A/FEff: 22-Nov-1993
RecommendedRE (-)601-0395 Special Check/Rework - Passenger/Crew Entrance Door - Latching Mechanism
Mos
Hrs
Ldg
52 A/F
RecommendedRE (-)601-0395 Rev 1 Special Check/Rework - Passenger/Crew Entrance Door - Latching Mechanism
11-Aug-1992Mos
Hrs
Ldg
52 A/FEff: 25-Jun-1993 Complied With
OptionalT (A/R)601-0417 Modification - Passenger/Crew Entrance Door - Addition of Internal Door-Handle Stop
Mos
Hrs
Ldg
52 A/FEff: 13-Apr-1995
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM193/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalRE (-)601-0451 Modification - Passenger Door - Introduce Self Lubricating Bushings
17-Dec-2001Mos
7,908.1Hrs
3,787Ldg
52 A/FEff: 31-Oct-1997 Complied With
OptionalT (A/R)601-0465 Modification - Access Door for Refuel/Defuel Control Panel - Addition of Packer to Aft Latch
Mos
Hrs
Ldg
52 A/FEff: 31-Jan-1996
OptionalT (A/R)601-0483 Modification - Rear Fuselage Equipment Bay Door - Add Liquid Deflector
Mos
Hrs
Ldg
52 A/FEff: 30-Aug-1996
RecommendedRE (-)601-0587 Special Check/Rework - Passenger / Crew Entrance Door - Passenger Door Foot Inspection and Rework
25-Jul-2008Mos
11,432Hrs
5,881Ldg
52 A/FEff: 11-Dec-2006 Complied With
RecommendedRE (-)601-0604 Modification – Emergency Exit – Installation of New Silicone Rubber Seal to Prevent Water Ingress
Mos
Hrs
Ldg
52 A/F
RecommendedRE (-)601-0604 Rev 1 Modification – Emergency Exit – Installation of New Silicone Rubber Seal to Prevent Water Ingress
Mos
Hrs
Ldg
52 A/F
RecommendedT (A/R)601-0604 Rev 2 Modification – Emergency Exit – Installation of New Silicone Rubber Seal to Prevent Water Ingress
Mos
Hrs
Ldg
52 A/FEff: 06-May-2014
RecommendedRE (-)601-0613 Special Check/Modification – Passenger Door – Epoxy Ramp Removal and Corrosion Prevention
Mos
Hrs
Ldg
52 A/F
RecommendedRE (-)601-0613 Rev 1 Special Check/Modification – Passenger Door – Epoxy Ramp Removal and Corrosion Prevention
Mos
Hrs
Ldg
52 A/F
RecommendedT (A/R)601-0613 Rev 2 Special Check/Modification – Passenger Door – Epoxy Ramp Removal and Corrosion Prevention
Mos
Hrs
Ldg
52 A/FEff: 24-Sep-2013
MandatoryRE (-)82-06-04 Main Entry Door Unlatching System
18-Sep-1985Mos
Hrs
Ldg
52 A/FBY AIRCRAFT SERIAL NUMBEREff: 22-Mar-1982 Not
Applicable
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM194/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AlertRE (-)A601-0026 Special Check/Modification - Upper Electronics Equipment Bay Doors - Lightning Protection
Mos
Hrs
Ldg
52 A/F
AlertRE (-)A601-0026 Rev 1 Special Check/Modification - Upper Electronics Equipment Bay Doors - Lightning Protection
Mos
Hrs
Ldg
52 A/FEff: 14-Feb-1984
CPCPREC52-00-801 Overwing Emergency Exit Door, External - CPCP Check including the following items: (1) External stops, fittings, frame and door seal / (2) External skin
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
52 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with ScheduledMaintenance Instruction Task 52-20-00-209.)
CPCPREC52-00-802 Baggage Compartment Door Structure - CPCP Check including the following items: (1) Vertical and transverse members / (2) Inner and external skin and frames / (3)
Seal / (4) Fittings and stops
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
52 A/F
Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with ScheduledMaintenance Instruction Task
52-30-00-210.)
CPCPREC52-00-803 Passenger/Crew Entrance Door Structure (External) - CPCP Check including the following items: (1) External door skins / (2) External door frames / (3) Tension fittings,
rollers, center cam and latches / (4) Hinge and lugs (without removal)
2.5 Years (+30 Days)(26-Sep-2018)-/+14826-Sep-2014Mos
Hrs
Ldg
(PKG 48 Month)
52 A/F
(SOURCE: TLMC 05-30-20)
CPCPREC52-00-804 Main Landing Gear Doors - CPCP Check including the following items: (1) Door hinges (without removal) / (2) Door Structure
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
52 A/F
(SOURCE: TLMC 05-30-20)
CPCPREC52-00-805 Passenger/Crew Entrance Door Structure (Internal) - CPCP Check including the following items: (1) Door frames and beams / (2) Backup fittings and support structure /
(3) Inner skin / (4) Torque tubes structure and tension rods
5.8 Months (+30
Days)(26-Sep-2016)-/+16019-Sep-2013Mos
Hrs
Ldg
(PKG 60 Month)
52 A/F
Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20)
CPCPREC52-00-806 Overwing Emergency Exit Door (Internal) - CPCP Check including the following items: (1) Internal Structure
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
52 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 52-20-00-209.)
IsModSumT (A/R)IS600-52-0001 REV A Installation of Alternate Fasteners for Lower Electronics Bay Access Door, Nose Compartment
Mos
Hrs
Ldg
52 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM195/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
IsModSumT (A/R)IS600-52-0003 REV A Passenger Door-Rework Hinge Panel Assy 600-31980-1023 to Provide Alternate Part for 600-31980-1011
Mos
Hrs
Ldg
52 A/F
IsModSumT (A/R)IS600-52-0004 REV A Main Passenger Door Seal – Introduction of Drain Holes
Mos
Hrs
Ldg
52 A/F
▼ 53 - FUSELAGE
RE (O/C)Radome Assembly
20-Sep-1983Mos
0Hrs
0Ldg
53 A/FUnknownUnknown
MRB ≈18-Sep-2016RE53-00-00-201 Fuselage Visual Check (External)
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
53 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE53-00-00-202 Fuselage Visual Check of the external skin, paying particular attention to the following items for cracks and corrosion: (1) ADG door skin cut-out (zone 112) / (2) All
access panels and skin cut-out areas except windows (zone 240) / (3) Windshield sill installation and skin cut-out area (zone 220) / (4) Side window installation and skin
cut-out area (zone 240) / (5) Cabin window installation and skin cut-out area (zone 240) / (6) Baggage door installation and skin cut-out area (zone 251) / (7)
Equipment bay door installation and skin cut-out area (zone 310)
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
53 A/F
(SOURCE: TLMC 05-20-15)
MRBRE53-00-00-203 Fuselage Structure (Internal) - FS169.00 to FS202.75 - Visual Check
5.5 Years (+30 Days)30-Sep-2021-/+112030-Sep-2011Mos
Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-57 (SOURCE: TLMC 05-20-15) (NOTE: For aircraft that carried out check 53-00-00-203 at 180M as required prior
to Revision 29 (dated Jan 12/99), the 240M threshold of 53-00-00-203 does not apply and the next due interval should be accomplished 120M
from the completion date of the 180M check 53-00-00-203.)
Also ConsiderDUE: 26-Sep-20161. T 240 Mos | 2. RE 120 MosFuselage Structure (Internal), FS169.00 to FS202.75 - CPCP C...C53-00-803A/F53
MRBRE53-00-00-204 Fuselage Visual Check - External - along rivet lines, paying particular attention for signs of corrosion indicated by pulled rivets, discolored or blistered paint and/or
bulging skins
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosFuselage Upper External Skin, FS169.00 to FS621.00, above WL...C53-00-801A/F53
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosFuselage Lower External Skin, FS169.00 to FS621.00 - CPCP Ch...C53-00-802A/F53
MRBRE53-00-00-231 Fuselage Structure (Internal) - FS202.75 to FS621.00, below Floor Visual Check
3.4 Years (+31 Days)18-Aug-2019-/+16018-Aug-2014Mos
Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-59 (SOURCE: TLMC 05-20-15)
Also ConsiderDUE: 26-Sep-20161. T 180 Mos | 2. RE 60 MosFuselage Structure (Internal), FS202.75 to FS621.00 below Fl...C53-00-819A/F53
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM196/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE53-00-00-232 Fuselage Structure (Internal) - FS202.75 to FS621.00, above Floor - Visual Check
5.5 Years (+30 Days)30-Sep-2021-/+112030-Sep-2011Mos
Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-58 (SOURCE: TLMC 05-20-15) (NOTE: For aircraft that carried out check 53-00-00-203 at 180M as required prior
to Revision 29 (dated Jan 12/99), the 240M threshold of 53-00-00-203 does not apply and the next due interval should be accomplished 120M
from the completion date of the 180M check 53-00-00-203.)
Also ConsiderDUE: 26-Sep-20161. T 240 Mos | 2. RE 120 MosFuselage Structure (Internal), FS202.75 to FS621.00 above Fl...C53-00-820A/F53
MRBRE53-00-00-233 Fuselage Structure (Internal) - FS621.00 to FS755.00 Visual Check
2.4 Years (+31 Days)15-Aug-2018-/+16015-Aug-2013Mos
Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-60 (SOURCE: TLMC 05-20-15)
Also ConsiderDUE: 26-Sep-20161. T 180 Mos | 2. RE 60 MosFuselage Structure (Internal), FS621.00 to VS67.5% - CPCP Ch...C53-00-821A/F53
AWL ≈20-Oct-2017RE53-10-00-101 * Windshield Upper Sill - FS234.00 and BL2.50 - Visual Check
29-Oct-2012Mos
812.3 Hrs12,853.51,20011,653.5Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-14 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-102 * Underfloor Pressure Bulkhead - FS409.00 - Visual Check (Pre SB 601-0503)
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
(SOURCE: TLMC 05-10-30) (NOTE: NOTE: The Inspection Threshold Interval starts at the incorporation date of SB 601-0503.)
AWL ≈20-Oct-2017RE53-10-00-103 * Keel Longeron - NDT Check
29-Oct-2012Mos
812.3 Hrs12,853.51,20011,653.5Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 6 ET-53-10-05 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2017T53-10-00-104 * Floor Beam Attachment to Pressure Bulkhead - FS621.00 - Visual Check
Mos
558.8 Hrs12,60012,600Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-30 (SOURCE: TLMC 05-10-30)
AWL ≈03-Aug-2018RE53-10-00-105 * Windshield Lower Sill - FS209.00 - Visual Check
25-Jul-2008Mos
1,190.8 Hrs13,2321,80011,432Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-11 (SOURCE: TLMC 05-10-30)
AWL ≈24-Aug-2018RE53-10-00-106 * Rear Pressure Bulkhead Web - Feed-Through Holes and Cut-Outs - FS621.00 - Visual Check
08-Aug-2005Mos
1,218.6 Hrs13,259.82,40010,859.8Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-31 (SOURCE: TLMC 05-10-30)
AWL ≈10-Jan-2021RE53-10-00-107 * Windshield Lower Sill - FS235.00, FS249.00 and FS264.00 - Visual Check
21-Oct-2015Mos
2,359.9 Hrs14,401.12,40012,001.1Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-12 (SOURCE: TLMC 05-10-30)
AWL ≈21-Sep-2020RE53-10-00-108 * Forward Fuselage Frame - FS220.00 and WL103.90 - Visual Check
23-Dec-2014Mos
2,214.6 Hrs14,255.82,40011,855.8Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-15 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM197/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈09-Apr-2022T53-10-00-109 * Integral Attachment Frame - FS513.00 and BL16.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-28 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-110 * Overwing Emergency Exit and Surround Structure - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 6 ET-53-10-04 (SOURCE: TLMC 05-10-30)
AWL ≈23-Jul-2021RE53-10-00-112 * Rear Pressure Bulkhead Web - Under the Vertical Stiffeners - Visual Check
10-Aug-2004Mos
2,617.1 Hrs14,658.34,20010,458.3Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-32 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-113 * Rear Pressure Bulkhead, Floor Beams, Fuselage Skin Panels and Associated Structure at FS621.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-37 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈24-Aug-2023RE53-10-00-115 * Forward Pressure Bulkhead Vertical Stiffeners - FS202.75 and BL22.00 - NDT Check
08-Aug-2005Mos
3,618.6 Hrs15,659.84,80010,859.8Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 6 ET-53-30-10 (SOURCE: TLMC 05-10-30)
AWL ≈22-Sep-2023RE53-10-00-116 * Fuselage Frame Drag Angle - FS755.00 and BL5.28 - NDT Check
26-Sep-2006Mos
3,656.3 Hrs15,697.54,80010,897.5Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 6 ET-53-30-10 (SOURCE: TLMC 05-10-30)
AWL ≈10-Jan-2041T53-10-00-117 * Longitudinal Floor Beams - FS513.00 and BL18.00 - Visual Check
21-Oct-2015Mos
11,959.9 Hrs24,001.112,00012,001.1Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-27 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈09-Apr-2022T53-10-00-119 * Stiffening Vertical Angles on Forward Face of Engine Support Beam - FS625.30 - Visual Check of stiffening vertical angles on the forward face of the engine support
beam at FS625.30 for cracks or distortion. Pay particular attention to stiffeners 601-35006-41, -75 and -77
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-39 (SOURCE: TLMC 05-10-30)
AWL ≈23-Mar-2026RE53-10-00-121 * Transverse Beam - Aft Pressure Bulkhead - FS621.00 - Visual Check
26-Sep-2006Mos
4,856.3 Hrs16,897.56,00010,897.5Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-29 (SOURCE: TLMC 05-10-30)
AWL ≈21-Jan-2017RE53-10-00-122 * Forward Pressure Bulkhead Web - FS202.75 - Visual Check
03-Apr-2000Mos
454 Hrs12,495.26,0006,495.2Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-02 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-123 * Longitudinal Floor Beams - FS484.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-24 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM198/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈29-Mar-2027RE53-10-00-124 * Intercostals and Clips - FS621.00 to FS625.30 - Visual Check
05-Aug-2003Mos
5,344.4 Hrs17,385.67,8009,585.6Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-33 (SOURCE: TLMC 05-10-30)
AWL ≈24-Mar-2027RE53-10-00-125 * Pressure Bulkhead Stiffener - FS621.00 - Visual Check
02-Nov-2002Mos
5,338.5 Hrs17,379.78,4008,979.7Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-35 (SOURCE: TLMC 05-10-30)
AWL ≈29-Dec-2030RE53-10-00-126 * Side Panel End Post - FS280.00 - NDT Check
05-Aug-2003Mos
7,144.4 Hrs19,185.69,6009,585.6Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 6 ET-53-10-01 (SOURCE: TLMC 05-10-30)
AWL ≈29-Dec-2030RE53-10-00-127 * Overwing Floor Intercostal - FS421.00, FS427.00, FS439.00, FS449.85, FS461.5, FS469.58, FS476.72 and FS484.00 - Visual Check
05-Aug-2003Mos
7,144.4 Hrs19,185.69,6009,585.6Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-21 (SOURCE: TLMC 05-10-30)
AWL ≈29-Dec-2030RE53-10-00-128 * Cleat - Frame to Longeron - FS439.00, FS461.00, FS484.00, FS499.00, FS529.00 and FS544.00 - Visual Check
05-Aug-2003Mos
7,144.4 Hrs19,185.69,6009,585.6Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-22 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-129 * Floor Structure and Underfloor Longerons - FS513.00 and BL45.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-26 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈09-Jan-2021T53-10-00-130 * Keel Longeron Links and Bolts - Visual Check
Mos
2,358.8 Hrs14,40014,400Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-25 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-132 * Passenger Door and Surrounding Structure - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-18 (SOURCE: TLMC 05-10-30)
AWL ≈14-Mar-2040T53-10-00-133 * Pressure Floor - Wing Tie Beam - FS460.00 - Visual Check
Mos
Hrs
8,674 Ldg15,00015,000Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-23 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-134 * Fuselage Frame Cap Angle - FS755.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-42 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-135 * Fuselage Frame at FS755.00 - Vertical Stabilizer Front Spar Attachment - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-44 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM199/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈09-Apr-2022T53-10-00-136 * Forward Pressure Bulkhead Vertical Member Near BL22.00 and WL79.50 - WL93.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-04 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-137 * Fuselage Frame at FS235.00 Upper Cap Angle at BL8.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-16 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-138 * Pilot Floor Connection Clips at BL13.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-05 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-139 * Forward Pressure Bulkhead Web at WL79.50 to WL91.70 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-03 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-140 * NLG Beam Web below Drag Beam - FS210.00 to FS215.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-06 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-141 * NLG Drag Strut at FS213.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-08 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-142 * NLG Beam Vertical Stiffener Clip - FS215.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-09 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-143 * NLG Beam Upper Cap - FS210.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-07 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-144 * NLG Beam Lower Cap at FS224.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-10 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-145 * Overwing Emergency Exit - Surround Structure - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-19 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-146 * Passenger Door Frames - FS310.00 and FS349.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-17 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM200/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈09-Apr-2022T53-10-00-147 * Frame Assembly Pressure Bulkhead - Vertical Stiffener - FS621.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-36 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-148 * Rear Pressure Bulkhead - FS621.00 - Frame Cap - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-34 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-149 * Rear Pressure Bulkhead Vertical Stiffener - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-38 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-150 * Outer Flange Cap Splice Angle - FS625.30 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 6 ET-53-10-07 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-151 * Frame Splice - FS672.20, Stringer 6 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-41 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-152 * Fuselage Frame FS755.00 Web BL5.50 and WL125.00 to WL131.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-43 (SOURCE: TLMC 05-10-30)
AWLRE (N/A)53-10-00-153 * Stringers #8 (L/R), 17 (L/R) and 24 (L/R) Between Frames VS55.62% and VS67.5% of the Vertical Stabilizer Chord (Post SB 601-0262) - Visual Check
Mos
Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-45 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-177 * Fuselage to Frame Attachment - FS424.00 and WL73.00 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 6 ET-53-10-09 (SOURCE: TLMC 05-10-30)
AWLRE (N/A)53-10-00-187 * Machined Strap - FS409.00 and LBL6.00 to RBL6.00 (Post SB 601-0503) - TBD
Mos
Hrs
Ldg
53 A/F
(SOURCE: TLMC 05-10-30)
AWLRE (N/A)53-10-00-188 * Fuselage Frame Cap - FS409.00 and LBL18.00 and RBL18.00 (Post SB 601-0503) - TBD
Mos
Hrs
Ldg
53 A/F
(SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-10-00-195 * Bonded Doubler Aft of FS617.00 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 4 UT-53-30-01 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM201/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈14-Nov-2031T53-10-00-197 * Rear Pressure Bulkhead Web - FS621.00, Fwd Face - NDT Check
Mos
Hrs
5,674 Ldg12,00012,000Ldg
53 A/F
Ref.:PSP 612 Part 6 ET-53-10-15, Ref.:PSP 612 Part 4 UT-53-10-03 (SOURCE: TLMC 05-10-30)
AWL ≈14-Mar-2020T53-10-00-198 * Engine Support Beam - Visual Check
Mos
Hrs
1,474 Ldg7,8007,800Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-10-81 (SOURCE: TLMC 05-10-30)
MRBRE53-10-00-205 Main Frame (Pressure Bulkhead FS202.75) Visual Check of the bulkhead web and doublers around the feed through holes, paying particular attention for cracks
andcorrosion
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
MRBRE53-10-00-206 Main Frame (FS625.30 and Engine Support Beam Attachment) Visual Check - Internal
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
MRBRE53-10-00-207 Main Frame (Keel Longerons) Visual Check of the following items, paying particular attentionfor cracks and corrosion: (1) The forward wing box to longeron
attachment links and bolts / (2) The aft wing box to longeron attachment fittings and bolts / (3) The fuselage skin adjacent to the longeron to fuselageattachment area
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosKeel Longerons and Surround Structure - CPCP Check including...C53-00-804A/F53
MRBRE53-10-00-208 Main Frame (FS755.00) Visual Check, paying particular attention to the machined attachment fittings for the vertical stabilizer front spar and adjacent web
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosFuselage Frame Attachment at FS755.00 and Skin at FS710.00 t...C53-00-805A/F53
MRBRE53-10-00-209 Main Frame (Floor Beam End Fittings at FS621.00) Visual Check, paying particular attention to: The fasteners and surrounding areas. The pressure bulkhead skin
adjacent to the fitting
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
MRBRE53-10-00-210 Main Frame (Passenger Door Surround Structure) Visual Check of the following items, paying particular attention for cracks and corrosion: (1) The external fuselage
skin adjacent to the hinges / (2) The internal bonded doubler at the door corners
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosPassenger Door Surround Structure - CPCP Check including the...C53-00-806A/F53
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM202/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE53-10-00-211 Main Frame (Overwing Emergency Exit Surround Structure) Visual Check of the following items, paying particular attention for cracks and corrosion: (1) The external
fuselage skin at the door corners / (2) The internal bonded doubler at the door corners (3) The upper and lower sill members
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosOverwing Emergency Exit Door Structure - CPCP Check includin...C53-00-807A/F53
MRBRE53-10-00-212 Main Frame (Baggage Door Surround Structure) Visual Check of the following items, paying particular attention for cracks and corrosion: (1) The external fuselage skin
at the door corners / (2) The internal bonded doubler at the door corners / (3) The lower sill members
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosBaggage Door Surround Structure - CPCP Check including the f...C53-00-808A/F53
MRBRE53-10-00-213 Main Frame (Equipment Bay Door Surround Structure) Visual Check of the following items, paying particular attention for cracks and corrosion: (1) The external
fuselage skin at the door corners / (2) The internal bonded doubler at the door corners / (3) The door hinge support structures
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosMain Frame (Equipment Bay Door Surround Structure) - CPCP Ch...C53-00-809A/F53
MRBRE53-10-00-214 Main Frame - Fuselage Floor Beam Splices Visual Check
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
MRBRE53-10-00-215 Main Frame (Frame Assembly FS424.00) Visual Check, paying particular attention to the integral wing attachment lug and the underfloor longeron attachment points
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing to Fuselage Integral Attachment at FS424.00 and BL45.00...C53-00-810A/F53
MRBRE53-10-00-216 Main Frame (Frame Assembly FS473.15) Visual Check, paying particular attention to the integral wing attachment lug and the underfloor longeron attachment points
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing to Fuselage Integral Attachment at FS473.15 and BL45.00...C53-00-811A/F53
MRBRE53-10-00-217 Main Frame (Frame Assembly FS513.00) Visual Check, paying particular attention to: (1) The inboard and outboard integral wing attachment lugs / (2) The fuselage to
wing attachment link / (3) The underfloor longeron attachment points
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing to Fuselage Integral Attachment at FS513.00 and BL13.00...C53-00-812A/F53
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM203/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE53-10-00-218 Main Frame (Frame Assembly FS640.00 and Engine Support Beam Attachment) Visual Check - Internal
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
MRBRE53-10-00-219 Main Frame (Frame Assembly FS654.50) Visual Check - Internal
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
MRBRE53-10-00-220 Main Frame (FS672.20 and FS682.20) Visual Check - Internal
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
AWL - Repair ≈28-May-2034RE53-10-00-406 Repair − Pressure Bulkhead, FS 409 (NDT and Visual Check)
Mos
8,782.8 Hrs20,82420,824Hrs
Ldg
53 A/F
Ref.:PSP 612, Part 4, VT−53−10−02, Ref.:PSP 612, Part 6, ET−53−10−10, Ref.:PSP 612, Part 9, VC−53−30−36 (ZONE: 131,132) (SOURCE: TLMC 5
-10-25)
AWL ≈14-Jul-2023T53-10-01-101 * Upper Latch Pins of the Passenger Door - NDT Check
Mos
Hrs
2,674 Ldg9,0009,000Ldg
53 A/F
Ref.:PSP 612 Part 7 MT-53-40-02 (SOURCE: TLMC 05-10-30)
AWL ≈14-Mar-2040T53-10-01-102 * Splice Strap and Skin at Stringer 20L and 20R Between FS559.00 and FS621.00 - NDT Check
Mos
Hrs
8,674 Ldg15,00015,000Ldg
53 A/F
Ref.:PSP 612 Part 6 ET-53-10-17 (SOURCE: TLMC 05-10-30)
MRBRE53-10-11-228 Floor Structure Under Toilet and Galley (without removal) carry out a Detailed Inspection of all accessible structure using a Borescope, paying particular attention for
corrosive spillage
6.6 Months (+31
Days)(21-Oct-2016)-/+11221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
MRBRE53-10-11-230 Floor Structure (Pre or Post SB 601-0372) - Remove Toilet, Galley and Floor Boards, carry out a Detailed Inspection of all under-floor structure (including beams),
paying particular attention for corrosive spillage.
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
Ref.:SRM PSP 607 53-25-07 (SOURCE: TLMC 05-20-15) (NOTE: Remove tape for pre SB 601-0372)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosFloor Structure, FS589.00 to FS621.00 - CPCP Check including...C53-00-818A/F53
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosFloor Structure, FS169.00 to FS280.00 - CPCP Check including...C53-00-823A/F53
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosFloor Structure, FS280.00 to FS424.00 - CPCP Check including...C53-00-824A/F53
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosFloor Structure, FS424.00 to FS589.00 - CPCP Check including...C53-00-825A/F53
AWL ≈09-Apr-2022T53-20-00-154 * Pilot’s Floor Web Adjacent to Pressure Bulkhead - FS203.00 and BL16.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-20-01 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM204/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈20-Jul-2031T53-30-00-155 * Cabin Window Cut-Outs - NDT Check
29-Oct-2012Mos
7,412.3 Hrs19,453.57,80011,653.5Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 6 ET-53-30-01 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈09-Apr-2022T53-30-00-157 * Light Fuselage Frames FS220.00 to FS605.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-30-10 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-30-00-159 * Fuselage Skin Panel - FS625.30, Stringer 0.0 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-30-12 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈23-Dec-2029T53-30-00-161 * Stringer Splice - FS513.00, Stringer 13 - Visual Check
26-Sep-2006Mos
6,656.3 Hrs18,697.57,80010,897.5Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-30-09 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈09-Apr-2022T53-30-00-163 * Cabin Window Surround Structures FS364.00 to FS529.00, Stringers 10 to 13 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-30-04 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈09-Apr-2022T53-30-00-165 * Skin and Stringer Splice at FS559.00, Stringer 0.0 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-30-11 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈29-Dec-2030RE53-30-00-166 * Fuselage Skin at NLG Cut-Out - FS235.00 - Visual Check
05-Aug-2003Mos
7,144.4 Hrs19,185.69,6009,585.6Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-30-02 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-30-00-168 * Wing to Fuselage Attachment Frame - FS513.00 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 6 ET-53-30-02 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈09-Apr-2022T53-30-00-170 * Stringer Splice at FS473.00, Stringer 3 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-30-08 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-30-00-171 * Skin Splice at Stringer 0 - FS439.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-30-06 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-30-00-172 * Skin Splice - FS424.00 to FS439.00, Stringer 8 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-30-05 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM205/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈09-Apr-2022T53-30-00-173 * Stringer Splice - Stringer 1 L&R FS718.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-30-14 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-30-00-174 * Fuselage Stringer Splice at Stringer 0, Forward of FS718.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-30-14 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-30-00-175 * Baggage Door and Surround Structure - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 6 ET-53-30-12 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-30-00-176 * Pressure Skin/Floor Angle at WL73.00 Between FS409.00 and FS559.00 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 6 ET-53-30-04 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-30-00-178 * Fuselage Frame Ref VS55.625%, Stringer 5 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-30-15 (SOURCE: TLMC 05-10-30)
AWLRE (N/A)53-30-00-179 * Drag Angle at Frame 67.5% of the Vertical Stabilizer Chord (Post SB 601-0262) - NDT Check
Mos
Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 6 ET-53-30-07 (SOURCE: TLMC 05-10-30)
AWLRE (N/A)53-30-00-180 * Skin Over Drag Angle and Frame at 67.5% and Over Stringers #8 (L/R), 17 (L/R) and 24 (L/R) Between Frames 55.62% and 67.5% of Vertical Stabilizer Chord (Post SB
601-0262) - Visual Check
Mos
Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-30-20 (SOURCE: TLMC 05-10-30)
AWL ≈20-Feb-2016RE53-30-00-185 * Structures Adjacent to Overboard Lavatory Services (External) - Visual Check
22-Mar-2013Mos
14.1 Hrs12,055.330011,755.3Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-30-01 (SOURCE: TLMC 05-10-30) (NOTE: This check is not required if you have done the internal visual check, 53-30
-00-186, every 3600 hours. If you have not done 53-30-00-185 but now want to, you must do both 53-30-00-185 and 53-30-00-186 before
you change to 53-30-00-185.)
AWLRE (N/A)53-30-00-186 * Structures Adjacent to Overboard Lavatory Services (Internal) - Visual Check
Mos
Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-30-01 (SOURCE: TLMC 05-10-30)
MRBRE53-30-00-221 Cabin Window Cut-Outs NDT Check
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
Ref.:PSP 612 Part 6 ET-53-30-08 (SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosCabin Window Cut-Outs and Surround Structure FS364.00 to FS5...C53-00-813A/F53
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM206/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE53-30-00-222 Plates/Skins (Side Skin Panel FS409.00 and WL73.50) Visual Check, paying particular attention to the external corner area at the wing cut-out
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
MRBRE53-30-00-224 Lower Fuselage Skins (External) NDT Check
OVD(11-Dec-2015)-/+19611-Dec-2007Mos
Hrs
Ldg
(PKG 96 Month)
53 A/F
Ref.:PSP 612 Part 6 ET-53-30-06 (SOURCE: TLMC 05-20-15)
MRB ≈17-Nov-2016RE53-30-00-229 Intercostals and Door Surround Structure (Pre SB 601-0335) Visual Check
11-Nov-2015Mos
Hrs
277 Ldg (+40)6,603-/+403006,303Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-30-22 (SOURCE: TLMC 05-20-15)
AWL - Repair ≈06-Apr-2022RE53-30-00-401 Repair − Fuselage Skin FS 235.0, BL 6.0 (NDT and Visual Check)
03-May-2002Mos
2,955.3 Hrs14,996.56,6008,396.5Hrs
Ldg
53 A/F
Ref.:PSP 612, Part 6, ET−53−30−09, Ref.:PSP 612, Part 9, VC−53−30−25 (ZONE: 114,115,121,122) (SOURCE: TLMC 5-10-25)
AWL - Repair ≈06-Apr-2022RE53-30-00-401 Repair − Fuselage Skin FS 235.0, BL 6.0 (NDT and Visual Check)
03-May-2002Mos
2,955.3 Hrs14,996.56,6008,396.5Hrs
Ldg
53 A/F
Ref.:PSP 612, Part 6, ET−53−30−09, Ref.:PSP 612, Part 9, VC−53−30−25 (ZONE: 114,115,121,122,) (SOURCE: TLMC 5-10-25)
AWL ≈09-Apr-2022T53-40-00-181 * Integral Frame Attachment Lugs - FS424.00 and BL45.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-40-01 (SOURCE: TLMC 05-10-30)
AWLRE (N/A)53-40-00-182 * Tail Tank Attachment Bolts (Post SB 601-0262) - NDT Check
Mos
Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 7 MT-53-40-01 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-40-00-183 * Integral Frame Attachment Lugs - FS473.00 and BL45.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-40-03 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-40-00-184 * Integral Frame Attachment Lugs - FS513.00 and BL45.00 and BL13.50 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-40-04 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-40-00-189 * Integral Frame Attachment Bolts - FS424.00 and BL45.00 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 4 UT-53-40-01 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T53-40-00-190 * Integral Frame Attachment Bolts - FS473.00 and BL45.00 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 4 UT-53-40-02 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM207/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈09-Apr-2022T53-40-00-191 * Integral Frame Attachment Bolts - FS513.00 and BL45.00 and BL13.50 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 4 UT-53-40-03 (SOURCE: TLMC 05-10-30)
AWL ≈10-Jan-2021RE53-40-00-192 * Overwing Emergency Exit - Surround Structure and Attachment Fittings - Visual Check
21-Oct-2015Mos
2,359.9 Hrs14,401.12,40012,001.1Hrs
Ldg
53 A/F
Ref.:PSP 612 Part 9 VC-53-40-05 (SOURCE: TLMC 05-10-30)
MRBRE53-40-00-225 Attachment Fittings (Nose Gear Trunnion Assembly) Visual Check, paying particular attention to: (1) The drag brace and the nose gear trunnion fitting for cracks / (2)
The web of the trunnion box assembly adjacent to trunnion fitting assembly for evidence of cracking or buckling
6.6 Months (+31
Days)(21-Oct-2016)-/+11221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (21-Oct-2016)1. RE 48 MosNose Landing Gear Wheel Well Structure - CPCP Check includin...C53-00-815A/F53
MRB ≈29-Dec-2030RE53-50-00-226 Tail Cone Visual Check of interior surface, frames, access door, door surrounding structure and fasteners
05-Aug-2003Mos
7,144.4 Hrs (+40)(19,185.6)-/+409,6009,585.6Hrs
Ldg
(PKG 9600 Hour)
53 A/F
(SOURCE: TLMC 05-20-15)
MRBRE53-50-11-227 Nose Radome Visual Check, paying particular attention to interior surface and attachments
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosNose Radome - CPCP Check including the following items: (1) ...C53-00-817A/F53
RecommendedRE (-)601-0078 Special Check/Modification - Upper Mid-Fuselage (Left Side) - Stringers
Mos
Hrs
Ldg
53 A/FEff: 22-Oct-1984
RecommendedRE (-)601-0094 Special Check/Rework - Fuselage Frame Station 394.00 - Missing Rivets
26-Jan-1987Mos
1,267Hrs
480Ldg
53 A/FComplied With
RecommendedT (A/R)601-0094 Rev 1 Special Check/Rework - Fuselage Frame Station 394.00 - Missing Rivets
Mos
Hrs
Ldg
53 A/FEff: 10-Dec-1984
RecommendedRE (-)601-0161 Special Check/Rework - Mid Fuselage - Undersize Hi-Lok Fasteners and Missing Gusset
Mos
Hrs
Ldg
53 A/F
RecommendedRE (-)601-0161 Rev 1 Special Check/Rework - Mid Fuselage - Undersize Hi-Lok Fasteners and Missing Gusset
27-Jan-1987Mos
1,267Hrs
470Ldg
53 A/FEff: 06-Jun-1987 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM208/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0164 Modification - Seat Tracks - Primary Stop
Mos
Hrs
Ldg
53 A/F
RecommendedRE (-)601-0164 Rev 1 Modification - Seat Tracks - Primary Stop
28-Mar-1989Mos
2,373Hrs
910Ldg
53 A/FEff: 26-Jun-1986 Complied With
OptionalRE (-)601-0169 Special Check/Rework - Floor Beam - Clearance for Access to Vent Valve on Forward Fuselage Fuel Tank
Mos
Hrs
Ldg
53 A/FEff: 02-May-1986
OptionalRE (-)601-0173 Modification - Tail Cone - Static Discharger
Mos
Hrs
Ldg
53 A/F
OptionalT (A/R)601-0173 Rev 1 Modification - Tail Cone - Static Discharger
Mos
Hrs
Ldg
53 A/FEff: 18-Jun-1990
RecommendedRE (-)601-0178 Modification - Front Wing-to-Fuselage Fairings - Center Splice Joint Fasteners
27-Jan-1987Mos
1,267Hrs
470Ldg
53 A/FEff: 11-Aug-1986 Complied With
OptionalRE (-)601-0179 Passenger Door Frame - Addition of Drain Holes and Tubes
Mos
Hrs
Ldg
53 A/F
OptionalT (A/R)601-0179 Rev 1 Passenger Door Frame - Addition of Drain Holes and Tubes
Mos
Hrs
Ldg
53 A/FEff: 14-Oct-1988
RecommendedRE (-)601-0194 Modification - Main Frame - Main Landing Gear Support Structure
Mos
Hrs
Ldg
53 A/FEff: 03-Apr-1987
RecommendedRE (-)601-0201 Modification - Rear Pressure Bulkhead - Introduction of Doublers
12-Nov-1992Mos
3,754Hrs
1,519Ldg
53 A/FEff: 04-Dec-1987 Complied With
OptionalT (A/R)601-0214 Modification - Rear Fuselage Equipment Bay - Installation of Tow Bar
Mos
Hrs
Ldg
53 A/FEff: 09-Mar-1988
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM209/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0372 Modification - Cabin Fuselage Floor Structure - Improved Isolation Between Floor Beams and Floor Panels
Mos
Hrs
Ldg
53 A/F
RecommendedRE (-)601-0372 Rev 1 Modification - Cabin Fuselage Floor Structure - Improved Isolation Between Floor Beams and Floor Panels
Mos
Hrs
Ldg
53 A/F
RecommendedRE (-)601-0372 Rev 2 Modification - Cabin Fuselage Floor Structure - Improved Isolation Between Floor Beams and Floor Panels
26-Jan-1996Mos
4,785Hrs
1,932Ldg
53 A/FEff: 31-May-1999 Complied With
OptionalT (A/R)601-0412 Modification - Wheel Bin Brushes - Introduction of Three-Piece Wheel-Bin Brush
Mos
Hrs
Ldg
53 A/FEff: 15-Sep-1994
OptionalT (A/R)601-0452 Modification - Right Main Wheel Bin - Replacement of Fasteners on the Inboard Access Panel 144-BZ
Mos
Hrs
Ldg
53 A/FEff: 31-Aug-1995
OptionalT (A/R)601-0459 Modification - Rear Fuselage Frame Assembly Install Doublers for APU Hoist
Mos
Hrs
Ldg
53 A/FEff: 30-Nov-1995
OptionalT (A/R)601-0487 Modification - Tail Cone Fuel Tank Assembly - Increase Strobe Light Reliability
Mos
Hrs
Ldg
53 A/FEff: 30-Apr-1998
OptionalRE (-)601-0488 Modification - Main Landing Gear Fairing - Installation of Removable Fasteners
08-Nov-1998Mos
5,824Hrs
2,521Ldg
53 A/FEff: 29-Nov-1996 Complied With
RecommendedRE (-)601-0501 Special Check - Inspection of Underfloor Pressure Bulkhead at FS409.00
04-May-2004Mos
10,325.2Hrs
5,223Ldg
53 A/FEff: 12-Sep-1997 Complied With
RecommendedRE (-)601-0503 Special Check/Modification - Middle Fuselage - FS409.00 Pressure Bulkhead Reinforcement
Mos
Hrs
Ldg
53 A/F
RecommendedT (A/R)601-0503 Rev 1 Special Check/Modification - Middle Fuselage - FS409.00 Pressure Bulkhead Reinforcement
Mos
Hrs
Ldg
53 A/FEff: 17-Mar-2008
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM210/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0507 Modification - Main Landing Gear Bay Fairing - Add a Protection Shield Against Ice Build-up on Aileron Cables
05-Nov-1998Mos
Hrs
Ldg
53 A/FEff: 30-Jun-1998 Complied With
RecommendedRE (-)601-0537 Modification - Main Frame - Addition of a Liquid Deflector Around Aft Equipment Compartment Door
15-Sep-2007Mos
11,184.3Hrs
5,748Ldg
53 A/FComplied With
RecommendedT (A/R)601-0537 Rev 1 Modification - Main Frame - Addition of a Liquid Deflector Around Aft Equipment Compartment Door
Mos
Hrs
Ldg
53 A/FEff: 30-Jan-2004
RecommendedT (A/R)601-0565 Modification - Aerodynamic Fairings - Installation of Decals on the Tail Cone Assembly
Mos
Hrs
Ldg
53 A/FEff: 05-Oct-2006
RecommendedRE (-)601-0586 Special Check/Modification – Floor – Addition of Seat Track Extensions
Mos
Hrs
Ldg
53 A/F
Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Floor – Addition of Seat Track ...601-0586 Part AA/F53
Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Floor – Addition of Seat Track ...601-0586 Part BA/F53
RecommendedRE (-)601-0586 Part A Special Check/Modification – Floor – Addition of Seat Track Extensions - Verify Applicability
Mos
Hrs
Ldg
53 A/FEff: 24-Sep-2007
RecommendedRE (-)601-0586 Part B Special Check/Modification – Floor – Addition of Seat Track Extensions - Modification
Mos
Hrs
Ldg
53 A/FEff: 24-Sep-2007
RecommendedRE (-)601-0586 Rev 1 Special Check/Modification – Floor – Addition of Seat Track Extensions
Mos
Hrs
Ldg
53 A/F
Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Floor – Addition of Seat Track ...601-0586 Rev 1 Part AA/F53
Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Floor – Addition of Seat Track ...601-0586 Rev 1 Part BA/F53
RecommendedRE (-)601-0586 Rev 1 Part A Special Check/Modification – Floor – Addition of Seat Track Extensions - Verify Applicability
Mos
Hrs
Ldg
53 A/FEff: 09-Oct-2007
RecommendedRE (-)601-0586 Rev 1 Part B Special Check/Modification – Floor – Addition of Seat Track Extensions - Modification
Mos
Hrs
Ldg
53 A/FEff: 09-Oct-2007
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM211/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0586 Rev 2 Special Check/Modification – Floor – Addition of Seat Track Extensions
25-Jul-2008Mos
11,432Hrs
5,881Ldg
53 A/FComplied With
Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Floor – Addition of Seat Track ...601-0586 Rev 2 Part AA/F53
Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Floor – Addition of Seat Track ...601-0586 Rev 2 Part BA/F53
RecommendedRE (-)601-0586 Rev 2 Part A Special Check/Modification – Floor – Addition of Seat Track Extensions - Verify Applicability
Mos
Hrs
Ldg
53 A/FEff: 28-Apr-2008
RecommendedRE (-)601-0586 Rev 2 Part B Special Check/Modification – Floor – Addition of Seat Track Extensions - Modification
Mos
Hrs
Ldg
53 A/FEff: 28-Apr-2008
RecommendedT (A/R)601-0586 Rev 3 Special Check/Modification – Floor – Addition of Seat Track Extensions
Mos
Hrs
Ldg
53 A/FEff: 21-Jul-2008
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification – Floor – Addition of Seat Track ...601-0586 Rev 3 Part AA/F53
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification – Floor – Addition of Seat Track ...601-0586 Rev 3 Part BA/F53
RecommendedT (A/R)601-0586 Rev 3 Part A Special Check/Modification – Floor – Addition of Seat Track Extensions - Verify Applicability
Mos
Hrs
Ldg
53 A/FEff: 21-Jul-2008
RecommendedT (A/R)601-0586 Rev 3 Part B Special Check/Modification – Floor – Addition of Seat Track Extensions - Modification
Mos
Hrs
Ldg
53 A/FEff: 21-Jul-2008
RecommendedT (A/R)601-0596 Special Check/Rework – Floor – Inspect the Under Floor Support Channel for FOD and Clean the Area
Mos
Hrs
Ldg
53 A/FEff: 21-Jul-2008
RecommendedT601-0612 Special Check – Floor Structure – Inspection and Torque, if Required, of the Bolts Attaching the Floor Beam Assembly Installed Over the Fwd and Aft Auxiliary Fuel
Tanks
3.2 Years05-Jul-201996Mos
Hrs
Ldg
53 A/FEff: 05-Jul-2011
MandatoryRE (-)97-24-02 R1 Pressure bulkhead
18-Mar-2009Mos
11,458.6Hrs
5,902Ldg
53 A/FAMOCEff: 13-Feb-2004 Complied
With
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check - Inspection of Underfloor Pressure Bulkhead a...601-0501A/F53
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM212/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
CPCPREC53-00-801 Fuselage Upper External Skin, FS169.00 to FS621.00, above WL73.50 - CPCP Check including the following items: (1) Skin splices of main frame, FS513.00 Stringers 11
to 13 / (2) Skin splice at FS450.00 and WL73.00 / (3) Skin splice at FS439.00 Stringer 0.0 / (4) Skin at FS559.00 Stringer 0.0 / (5) Skin splice at FS424.00 to FS439.00
Stringer 8 / (6) Frame splice at FS424.00 and WL73.00 / (7) Splice at FS473.00 Stringer 3 / (8) Skin panel at light frames / (9) Antenna cut-outs (without removal) / (10)
Skin around cabin windows, doors and cockpit windows
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 53-00-00-204.)
CPCPREC53-00-802 Fuselage Lower External Skin, FS169.00 to FS621.00 - CPCP Check including the following items: (1) Nose landing gear cut-out at FS235.00 / (2) Fuselage skin including
area covered by fairings / (3) Fuselage skin as viewed from MLG bay / (4) Antenna cut-outs (without removal) and access doors
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 53-00-00-204.)
CPCPREC53-00-803 Fuselage Structure (Internal), FS169.00 to FS202.75 - CPCP Check including the following items: (1) Aft face of bulkhead FS169.00 / (2) Forward web of bulkhead
FS202.75 / (3) Vertical stiffeners of bulkhead FS202.75 / (4) Internal skins, frames and stringers / (5) Floor beams
5.8 Months (+30
Days)26-Sep-2016-/+112026-Sep-2006Mos
Hrs
Ldg
53 A/F
(SOURCE: TLMC 05-30-20) (NOTE: [1] Remove insulation blankets, do not removeself-adhesive panels. [2] This task can be done in conjunction
with Scheduled Maintenance Instruction Task 53-00-00-203.)
CPCPREC53-00-804 Keel Longerons and Surround Structure - CPCP Check including the following items: (1) Forward wing box to longeron attachment links and bolts / (2) Aft wing box to
longeron attachment fittings and bolts / (3) Fuselage skin adjacent to the longerons
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task
53-10-00-207.)
CPCPREC53-00-805 Fuselage Frame Attachment at FS755.00 and Skin at FS710.00 to FS718.00, Stringers 1L to 1R - CPCP Check including the following items: (1) Fuselage frame and drag
angle / (2) Attachment fitting for the vertical stabilizer / (3) Adjacent Web / (4) Skin area at FS718.00, stringers 1L to 1R
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 53-10-00-208.)
CPCPREC53-00-806 Passenger Door Surround Structure - CPCP Check including the following items: (1) The external fuselage skin adjacent to the hinges / (2) The internal bonded doubler
at the four corners / (3) Upper sill, lower cap and plate / (4) Lower sill, butt strap and sill longeron / (5) Frame at FS310.00 and FS349.00 / (6) Fittings and Latches
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 53-10-00-210.)
CPCPREC53-00-807 Overwing Emergency Exit Door Structure - CPCP Check including the following items: (1) External skin at the door structure four corners / (2) Internal doubler at the
door structure four corners / (3) Upper and lower sill members / (4) Latch fittings, frame stop fittings and hinge support fittings
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 53-10-00-211.)
CPCPREC53-00-808 Baggage Door Surround Structure - CPCP Check including the following items: (1) External fuselage skin at the four corners / (2) Internal bonded doubler at the four
corners / (3) Lower sill members
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 53-10-00-212.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM213/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
CPCPREC53-00-809 Main Frame (Equipment Bay Door Surround Structure) - CPCP Check including the following items: (1) The external fuselage skin at the door corners / (2) The internal
bonded doubler at the door corners / (3) The door hinge support structures
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 53-10-00-213.)
CPCPREC53-00-810 Wing to Fuselage Integral Attachment at FS424.00 and BL45.00 - CPCP Check including the following items: (1) Wing to fuselage integral bolts / (2) Bolts, nuts and
safety pins (without removal of bolts)
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 53-10-00-215.)
CPCPREC53-00-811 Wing to Fuselage Integral Attachment at FS473.15 and BL45.00 - CPCP Check including the following items: (1) Wing to fuselage integral bolts / (2) Bolts, nuts and
safety pins (without removal of bolts)
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 53-10-00-216.)
CPCPREC53-00-812 Wing to Fuselage Integral Attachment at FS513.00 and BL13.00 and BL45.00 - CPCP Check including the following items: (1) Attachment frame at FS513.00 and BL13.00
/ (2) Frame flanges, webs / (3) Dragbrace fitting of the floor support beam / (4) Wing to fuselage lugs at BL45.00 / (5) Bolts, nuts and safety pins (without removal of
bolts)
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with ScheduledMaintenance Instruction Task 53-10-00-217.)
CPCPREC53-00-813 Cabin Window Cut-Outs and Surround Structure FS364.00 to FS529.00 (FS364.00 to FS559.00 Post SB 601-0006) - CPCP Check including the following items: (1)
External skin around the window cut-outs (9 inches lateraland 20 inches vertical) / (2) Stringer runouts
5.8 Months (+30
Days)(26-Sep-2016)6026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 53-30-00-221.)
CPCPREC53-00-814 Fuselage External Skin Panels, FS621.00 to VS67.5% - CPCP Check including the following items: (1) Area Corresponding to Stringer 5 at VS55.62% / (2) Area
Corresponding to Stringer 0 at FS630.00 and (1) NLG drag strut / (2) NLG beam vertical stiffener clip / (3) NLG beam upper and lower caps / (4) Web and internal skin
of the wheel well
2.5 Years (+30 Days)(26-Sep-2018)-/+14826-Sep-2014Mos
Hrs
Ldg
(PKG 48 Month)
53 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 53-40-00-225.)
CPCPREC53-00-815 Nose Landing Gear Wheel Well Structure - CPCP Check including the following items: (1) NLG drag strut / (2) NLG beam vertical stiffener clip / (3) NLG beam upper and
lower caps / (4) Web and internal skin of the wheel well
2.5 Years (+30 Days)(26-Sep-2018)-/+14826-Sep-2014Mos
Hrs
Ldg
(PKG 48 Month)
53 A/F
(ZONE: 110, 240) (ACCESS: 711-AL-AR) (SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with ScheduledMaintenance
Instruction Task 53−40−00−225.)
CPCPREC53-00-816 Tail Cone Assembly (Pre SB 601-0262) - CPCP Check including the following items: (1) Exterior surfaces and surrounding structure / (2) Interior surfaces / (3) Frames
and access doors
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-30-20)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM214/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
CPCPREC53-00-817 Nose Radome - CPCP Check including the following items: (1) Interior surface / (2) Attachments and (1) Floor beams, channels and joint channels / (2) Floor support
fittings and intercostals / (3) Floor plates, splices and doublers / (4) Profile plates floor attachment at bulkhead FS621.00
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: [1] Remove insulation blankets. [2] Check for fluid spillage under galley and
lavatory. [3]This task can be done in conjunction with Scheduled Maintenance Instruction Task 53-50-11-227 and Task 53-10-11-230.)
CPCPREC53-00-818 Floor Structure, FS589.00 to FS621.00 - CPCP Check including the following items: (1) Floor beams, channels and joint channels / (2) Floor support fittings and
intercostals / (3) Floor plates, splices and doublers / (4) Profile plates floor attachment at bulkhead FS621.00
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
Ref.:PSP 607 51-54-153/3 (ZONE: 251, 252) (ACCESS: 151-DZ-EZ-FZ, 152-CZ-DZ) (SOURCE: TLMC 05-30-20) (NOTE: [1] Remove insulation
blankets.[2] Check for fluid spillage under galley and lavatory.[3] This task can be done in conjunction with ScheduledMaintenance Instruction
Task 53−10−11−230.)
CPCPREC53-00-819 Fuselage Structure (Internal), FS202.75 to FS621.00 below Floor - CPCP Check including the following items: (1) Aft face of web of bulkhead at FS202.75 / (2) Bulkhead
at FS280.00 / (3) Internal skins, frames, splices / (4) Stringers, longerons, brackets, cleats / (5) Forward face of bulkhead at FS621.00 / (6) Forward face of bulkhead at
FS409.00 / (7) Aft face of bulkhead at FS559.00
5.8 Months (+30
Days)26-Sep-2016-/+16026-Sep-2011Mos
Hrs
Ldg
53 A/F
Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: [1] Remove insulation blankets, do not remove lavatory. [2]This task can be done
in conjunction with Scheduled Maintenance Instruction Task 53-00-00-231.)
CPCPREC53-00-820 Fuselage Structure (Internal), FS202.75 to FS621.00 above Floor - CPCP Check including the following items: (1) Aft face of web of bulkhead FS202.75 / (2) Bulkhead
FS280.00 / (3) Internal skins, frames, splices / (4) Stringers, longerons, brackets, cleats / (5) Forward face of bulkhead FS621.00 / (6) Internal cabin windows surround
structure / (7) Internal overwing exit structure / (8) Passenger door internal surround structure / (9) Internal baggage door surround structure / (10) Internal antenna
cut-outs / (11) Area around sound dampening panels
5.8 Months (+30
Days)26-Sep-2016-/+112026-Sep-2006Mos
Hrs
Ldg
53 A/F
Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: [1] Do not remove self-adhesive sound damping. [2] This task can be done in
conjunction with Scheduled Maintenance Instruction Task 53-00-00-232. [3] Removal of furnishings and equipment may be required to
complete the check.)
CPCPREC53-00-821 Fuselage Structure (Internal), FS621.00 to VS67.5% - CPCP Check including the following items: (1) Aft face of web of bulkhead FS621.00 / (2) Bulkhead FS755.00 / (3)
Frame VS55.0%, forward face of frame VS67.5% / (4) Internal skins, frames, splices / (5) Stringers, longerons, brackets, cleats / (6) Aft equipment door internal
structure / (7) Engine support beam / (8) Transverse beam / (9) Intercostal / (10) Internal antenna cut-outs
5.8 Months (+30
Days)26-Sep-2016-/+16026-Sep-2011Mos
Hrs
Ldg
53 A/F
(SOURCE: TLMC 05-30-20) (NOTE: [1] Do not remove self-adhesive sound damping, [2] This task can be done in conjunction with Scheduled
Maintenance Instruction Task 53-00-00-233.)
CPCPREC53-00-822 Tail Cone (Post SB 601-0262) - CPCP Check including the following items: (1) Aft face of VS67.5% / (2) Forward bulkhead of tail tank / (3) Exterior skins and doors
5.8 Months (+30
Days)(26-Sep-2016)6026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-30-20) (NOTE: Use a borescope and monitor)
CPCPREC53-00-823 Floor Structure, FS169.00 to FS280.00 - CPCP Check including the following items: (1) Floor beams, channels and joint channels / (2) Floor support fittings, intercostals,
brackets and splices / (3) Flight compartment floor structure and central walkway
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
(SOURCE: TLMC 05-30-20) (NOTE: [1] Remove insulation blankets, carpets and seats. [2] Check for spillage under forward galley. [3] This task
can be done in conjunction with Scheduled Maintenance Instruction Task 53-10-11-230.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM215/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
CPCPREC53-00-824 Floor Structure, FS280.00 to FS424.00 - CPCP Check including the following items: (1) Floor beams, channels, beam plates and angles(2) Floor support fittings,
intercostals, struts and brackets(3) Floor sill structure (webs)(4) Pressure floor skin panels
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: [1] Check for fluid spillage under forward galley. [2] This task can be done in
conjunction with ScheduledMaintenance Instruction Task 53-10-11-230.)
CPCPREC53-00-825 Floor Structure, FS424.00 to FS589.00 - CPCP Check including the following items: (1) Floor beams, channels and joint channels / (2) Floor support fittings and
intercostals / (3) Pressurized floor skin panel and flanged panels / (4) Pressure floor wing tie beam and longerons
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: [1] Remove insulation blankets [2] Check for fluid spillage. If spillage is found,
removepanels 152-AZ/BZ [3] This task can be done in conjunction with Scheduled Maintenance Instruction Task 53-10-11-230)
CPCPREC53-00-826 Structure Adjacent to Overboard Lavatory Services (External) - CPCP Check including the following items: (1) Fuselage skin doubler (by looking through the splash
guard) / (2) Fuselage skin for 2 inches around the edge of the doubler
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20)
CPCPREC53-00-827 Fuselage Frame FS409.00, Aft Face, External - CPCP Check including the following items: (1) Bulkhead Web / (2) Frame Cap Members / (3) Machined Strap (Post SB 601-
0503)
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
53 A/F
Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20)
MandatoryRE (-)CF-1997-16R2 Paragraph 1 Bombardier CL-600 "Challenger" - FS409 Bulkhead Fatigue Cracks, Detailed Visual Inspection
Mos
Hrs
Ldg
53 A/FEff: 15-Oct-1997
IsModSumT (A/R)IS600-53-0002 REV A Alternative CRES Fasteners for Door Assy Fwd Fuselage
Mos
Hrs
Ldg
53 A/F
▼ 54 - NACELLES/PYLONS
MRB ≈18-Sep-2016RE54-00-00-201 Nacelles/Pylons Visual Check - External
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
54 A/F
(SOURCE: TLMC 05-20-15)
MRBRE54-00-00-202 Nacelles/Pylons (Pylon Structure) Visual Check - Internal
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
54 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosNacelles/Pylons, Internal (Pylon Structure) - CPCP CheckC54-00-802A/F54
AWL ≈09-Apr-2022T54-10-00-101 * Engine Supporting Beam Upper Cap - FS625.30 and BL38.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
54 A/F
Ref.:PSP 612 Part 9 VC-54-10-01 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM216/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈09-Apr-2022T54-10-00-102 * Pylon Spar/Fuselage Frame Attachment - FS672.20 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
54 A/F
Ref.:PSP 612 Part 6 ET-54-10-04 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T54-10-00-103 * Pylon Spar Upper Cap - FS625.30 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
54 A/F
Ref.:PSP 612 Part 6 ET-54-10-01 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T54-10-00-104 * Pylon Canted Rib - Upper Splice at FS672.20 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
54 A/F
Ref.:PSP 612 Part 9 VC-54-10-02 (SOURCE: TLMC 05-10-30)
AWL ≈14-Mar-2040T54-10-00-106 * Rib Upper Cap, Skin and Doubler from FS672.20 to FS682.00 - NDT Check
Mos
Hrs
8,674 Ldg15,00015,000Ldg
54 A/F
Ref.:PSP 612 Part 6 ET-54-10-03 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T54-30-00-105 * Pylon Upper Skin - FS682.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
54 A/F
Ref.:PSP 612 Part 9 VC-54-30-01 (SOURCE: TLMC 05-10-30)
RecommendedRE (-)601-0073 Modification - Pylon Structure - Panel Fasteners
Mos
Hrs
Ldg
54 A/FEff: 21-Jan-1986
RecommendedRE (-)601-0087 Modification - Pylon Firewall - Addition of Doubler
Mos
Hrs
Ldg
54 A/F
RecommendedT (A/R)601-0087 Rev 1 Modification - Pylon Firewall - Addition of Doubler
Mos
Hrs
Ldg
54 A/FEff: 30-Nov-1984
RecommendedRE (-)601-0462 Special Check/Rework – Aft Engine Mount Support Rib Fasteners
Mos
Hrs
Ldg
54 A/F
Nextdue Share EarliestDUE:1. RE -Special Check/Rework – Aft Engine Mount Support Rib Fastener...601-0462 Part AA/F54
Nextdue Share EarliestDUE:1. RE -Special Check/Rework – Aft Engine Mount Support Rib Fastener...601-0462 Part BA/F54
RecommendedRE (-)601-0462 Part A Special Check/Rework – Aft Engine Mount Support Rib Fasteners - Left Engine
Mos
Hrs
Ldg
54 A/FEff: 31-Oct-1995
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM217/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0462 Part B Special Check/Rework – Aft Engine Mount Support Rib Fasteners - Right Engine
Mos
Hrs
Ldg
54 A/FEff: 31-Oct-1995
RecommendedRE (-)601-0462 Rev 1 Special Check/Rework – Aft Engine Mount Support Rib Fasteners
18-Nov-1996Mos
5,001Hrs
2,052Ldg
54 A/FEff: 14-Jun-1996 Complied With
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework – Aft Engine Mount Support Rib Fastener...601-0462 Rev 1 Part AA/F54
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Rework – Aft Engine Mount Support Rib Fastener...601-0462 Rev 1 Part BA/F54
RecommendedT (A/R)601-0462 Rev 1 Part A Special Check/Rework – Aft Engine Mount Support Rib Fasteners - Left Engine
Mos
Hrs
Ldg
54 A/FEff: 14-Jun-1996
RecommendedT (A/R)601-0462 Rev 1 Part B Special Check/Rework – Aft Engine Mount Support Rib Fasteners - Right Engine
Mos
Hrs
Ldg
54 A/FEff: 14-Jun-1996
CPCPREC54-00-801 Nacelles/Pylons, External - CPCP Check
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
54 A/F
(SOURCE: TLMC 05-30-20)
CPCPREC54-00-802 Nacelles/Pylons, Internal (Pylon Structure) - CPCP Check
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
54 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 54-00-00-202.)
MandatoryRE (-)CF-2015-09R1 Nacelle/Pylon – Non-conforming Bushing Holes on the Engine Mount Rib
Mos
Hrs
Ldg
54 A/FEff: 13-Jul-2015
IsModSumT (A/R)IS600-54-0001 REV A Pylon Trailing Edge Attachment Modification
Mos
Hrs
Ldg
54 A/F
▼ 55 - STABILIZERS
RE (O/C)Elevator Assy
20-Sep-1983Mos
0Hrs0
0Ldg0
Left55 A/FNew600-24025-1007
UNKNOWN
RE (O/C)Elevator Assy
20-Sep-1983Mos
0Hrs0
0Ldg0
Right55 A/FNew600-24025-1008
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM218/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Horizontal Assy Stabilizer
20-Sep-1983Mos
0Hrs
0Ldg
55 A/FUnknownUnknown
RE (O/C)Rudder Assy
20-Sep-1983Mos
0Hrs0
0Ldg0
55 A/FNew600-22000-1001
UNKNOWN
AWL ≈19-Apr-2025RE55-00-00-127 * Pitch Trim Actuator - Visual Check
11-Mar-2000Mos
4,411.7 Hrs16,452.910,0006,452.9Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-00-01 (SOURCE: TLMC 05-10-30)
MRB ≈18-Sep-2016RE55-00-00-201 Stabilizers Visual Check - External
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
55 A/F
(SOURCE: TLMC 05-20-15)
AWL ≈09-Apr-2022T55-10-00-101 * Horizontal Stabilizer Rear Spar - Centerline Splice - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-10-05 (SOURCE: TLMC 05-10-30)
AWL ≈23-Jul-2021RE55-10-00-102 * Horizontal Stabilizer Rear Spar Upper Cap at Rib 1, BL6.00 - NDT Check
19-Jul-2004Mos
2,617.1 Hrs14,658.34,20010,458.3Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 6 ET-55-10-01 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-10-00-103 * Horizontal Stabilizer - Rear Spar Upper Cap and Splice - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-10-04 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-10-00-104 * Horizontal Stabilizer Front Spar Upper Cap Splice - BL6.00 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 6 ET-55-10-02 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-10-00-105 * Horizontal Stabilizer - Upper Stringer 1 - BL6.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-10-03 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-10-00-106 * Horizontal Stabilizer - Centerline Rib - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-10-02 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM219/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE55-10-00-202 Horizontal Stabilizer Visual Check of the following items paying particular attention for cracks, and corrosion: (1) The rear spar splice on the left and right side
specifically,theweb attachments and the cap splice fittins / (2) The front spar splice on the left and right side specifically - the web in the area of the screw jack fitting -
the front and back faces of the web splice - the spar splice fittings and the attachment fitting which joins the web to the machined rib at BL6.00 (3) The visor fittings
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
55 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (30-Jan-2017)1. RE 48 MosHorizontal Stabilizer Front Spar - CPCP Check including the ...C55-00-806A/F55
MRBRE55-10-00-203 Horizontal Stabilizer Visual Check of the following items, paying particular attention for cracks and corrosion: (1) The rear spar web adjacent to the elevator hinge
fittings / (2) PCU support structure
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
55 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosHorizontal Stabilizer Rear Spar - CPCP Check including the f...C55-00-807A/F55
MRBRE55-10-00-204 Horizontal Stabilizer Visual Check - Internal - Structure at BL10.00L to BL10.00R
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
55 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosHorizontal Stabilizer Internal Structure - CPCP Check includ...C55-00-808A/F55
MRBRE55-10-00-205 Horizontal Stabilizer Visual Check of internal structure, complete
7.4 Years (+31 Days)15-Aug-2023-/+112015-Aug-2013Mos
Hrs
Ldg
55 A/F
(SOURCE: TLMC 05-20-15)
MRBRE55-10-11-206 Horizontal Stabilizer Visual Check (Upon removal of the inner pivot pin only) of the inner and outer pivot pins. Reinstall inner pivot pin
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
55 A/F
(SOURCE: TLMC 05-20-15)
AWL ≈17-Oct-2020RE55-20-00-107 * Elevator/Horizontal Stabilizer PCU and Supporting Hinges - NDT Check
17-Nov-2000Mos
2,248.7 Hrs14,289.97,2007,089.9Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 6 ET-55-20-01 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-20-00-108 * Elevator, Skin and Front Spar - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-20-01 (SOURCE: TLMC 05-10-30)
MRB ≈18-Sep-2016RE55-20-00-207 Elevators and Rudder Visual Check - External
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
55 A/F
(SOURCE: TLMC 05-20-15)
AWL ≈09-Apr-2022T55-30-00-109 * Vertical Stabilizer - Mid Spar Cap at Rib 1 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-30-04 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM220/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈09-Apr-2022T55-30-00-110 * Vertical Stabilizer - Front Spar - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-30-01 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-30-00-111 * Vertical Stabilizer - Front Spar Cap FS755.00 and WL137.50 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-30-02 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-30-00-112 * Vertical Stabilizer - Stringer Splice - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-30-03 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-30-00-113 * Vertical Stabilizer - Stringer Splice - VS31.875% at Rib 2 and VS55.625% at Rib 3 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-30-06 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-30-00-114 * Vertical Stabilizer - Rear Spar - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 6 ET-55-30-03 Pre SB 601-0262, Ref.:PSP 612 Part TBD Post SB 601-0262 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-30-00-115 * Vertical Stabilizer - Front Spar Cap at Rib 1 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 6 ET-55-30-01 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-30-00-116 * Vertical Stabilizer - Rear Spar Web at Rib 7 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-30-07 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-30-00-117 * Vertical Stabilizer - Front Spar Cap Splice Strap - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 6 ET-55-30-02 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-30-00-118 * Vertical Stabilizer - Access Hole - Skin Cut-Out - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-30-05 (SOURCE: TLMC 05-10-30)
MRBRE55-30-00-209 Vertical Stabilizer Visual Check of the Canted Top Rib for cracks and corrosion, paying particular attention to: (1) the front spar attachment / (2) the mid spar
attachment / (3) the rear spar attachment / (4) the upper rear spar splice to the canted rib.
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
55 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM221/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE55-30-00-210 Vertical Stabilizer Visual Check of the following items, paying particular attention for cracks and corrosion: (1) The rear spar frame assembly at FS815.00, specifically-
the web adjacent to the spar attachment - the spar caps - the fuselage skin adjacent to the spar caps. / (2) The front spar, specifically - the machined cruciform
attachment fittings at the sparbase - the spar web adjacent to the fitting - the splice with the vertical stabilizer cap rib the fuselage skin adjacent to the cruciform
fittin. / (3) Mid spar, specificall - the machined caps at the spar base - the spar web at the spar base, adjacent to the machined caps - the splice to the machined cap rib.
/ (4) Rear spar lower, specifically, the web and caps adjacent to the rudder hinge fittings / (5) The mid spar frame assembly at FS785.00, specifically - the web adjacent
to the rear attachment - the spar caps and the adjacent fuselage skin.
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
55 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosVertical Stabilizer Front Spar - CPCP Check including the fo...C55-00-802A/F55
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosVertical Stabilizer Internal Structure - CPCP Check includin...C55-00-803A/F55
AWL ≈22-Apr-2023RE55-40-00-119 * Rudder/Vertical Stabilizer Support and PCU Hinge Fittings - NDT Check
10-Sep-2001Mos
3,456.2 Hrs15,497.47,8007,697.4Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 6 ET-55-40-01 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-40-00-120 * Rudder, Skin and Front Spar - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-40-01 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-50-00-121 * Vertical Stabilizer Pitch Trim Actuator Pivot Lugs - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 6 ET-55-50-02 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-50-00-122 * Vertical Stabilizer/Horizontal Stabilizer Pivot Fitting - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 4 UT-55-50-01 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-50-00-123 * Horizontal Stabilizer - Pivot Fitting Lugs - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-50-02 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T55-50-00-124 * Horizontal Stabilizer Bathtub Fittings - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-50-01 (SOURCE: TLMC 05-10-30)
AWL ≈29-Dec-2030RE55-50-00-125 * Rudder - Hinge Bolts - Visual Check
05-Aug-2003Mos
7,144.4 Hrs19,185.69,6009,585.6Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-50-03 (SOURCE: TLMC 05-10-30)
AWL ≈29-Dec-2030RE55-50-00-126 * Elevator - Hinge Bolts - Visual Check
05-Aug-2003Mos
7,144.4 Hrs19,185.69,6009,585.6Hrs
Ldg
55 A/F
Ref.:PSP 612 Part 9 VC-55-50-04 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM222/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE55-50-00-211 Attachment Fittings Visual Check of Horizontal Stabilizer Pivot Fittings, paying particular attention between the fasteners on either side of the lugs
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
55 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (30-Jan-2017)1. RE 48 MosHorizontal and Vertical Stabilizer - CPCP Check including th...C55-00-809A/F55
MRBRE55-50-00-212 Attachment Fittings Visual Check of the vertical stabilizer pivot fittings, paying particular attention to: (1) The fitting lugs / (2) Integrity of the attachments / (3) The
adjacent web and cap of the vertical stabilizer top rib
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
55 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (30-Jan-2017)1. RE 48 MosHorizontal and Vertical Stabilizer - CPCP Check including th...C55-00-809A/F55
MRBRE55-50-00-213 Attachment Fittings Visual Check of Horizontal Stabilizer - Pitch Trim Actuator Fittings, paying particular attention to: (1) The ballscrew yoke, attachment / (2) The
fitting lugs / (3) Integrity of the fasteners / (4) Front spar web splice and backup fittings attached to theupper and lower horizontal stabilizer skins
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
55 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (30-Jan-2017)1. RE 48 MosVertical Stabilizer, Pitch Trim Actuator Attachment Structur...C55-00-804A/F55
Also ConsiderDUE: (30-Jan-2017)1. RE 48 MosHorizontal Stabilizer, Pitch Trim Actuator Attachment - CPCP...C55-00-810A/F55
MRBRE55-50-00-214 Attachment Fittings Visual Check of the vertical stabilizer to rudder center hinge fitting, paying particular attention to: (1) The lugs for elongation and wear / (2) The
integrity of the fitting attachments on both sides of the rear spar
11.9 Months (+31
Days)(28-Mar-2017)-/+13628-Mar-2014Mos
Hrs
Ldg
(PKG 36 Month)
55 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (28-Mar-2017)1. RE 36 MosVertical Stabilizer Rear Spar Structure - CPCP Check includi...C55-00-805A/F55
MRBRE55-50-00-215 Attachment Fittings Visual Check of the rudder actuator/hinge fitting, paying particular attention to: (1) The lugs for elongation and wear / (2) The integrity of the
fitting attachments on both sides of the rear spar
11.9 Months (+31
Days)(28-Mar-2017)-/+13628-Mar-2014Mos
Hrs
Ldg
(PKG 36 Month)
55 A/F
(SOURCE: TLMC 05-20-15)
MRBRE55-50-00-216 Attachment Fittings Visual Check of the rudder attachment fittings, paying particular attention to: (1) The integral attachment fork end of each machined fitting / (2)
The stabilizer skin mounting support brackets and the adjacent skin
11.9 Months (+31
Days)(28-Mar-2017)-/+13628-Mar-2014Mos
Hrs
Ldg
(PKG 36 Month)
55 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (28-Mar-2017)1. RE 36 MosRudder External Skin, Structure and Attachments - CPCP Check...C55-00-812A/F55
MRBRE55-50-00-217 Attachment Fittings Visual Check of Hinge Fitting on Horizontal Stabilizer BL15.25, paying particular attention to: (1) The adjacent spar web / (2) The internal backup
fittings / (3) The fitting lugs for elongation and wear
11.9 Months (+31
Days)(28-Mar-2017)-/+13628-Mar-2014Mos
Hrs
Ldg
(PKG 36 Month)
55 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM223/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE55-50-00-218 Attachment Fittings Visual Check of PCU Fittings, Horizontal Stabilizer, paying particular attention to the lugs of the elevator PCU
11.9 Months (+31
Days)(28-Mar-2017)-/+13628-Mar-2014Mos
Hrs
Ldg
(PKG 36 Month)
55 A/F
(SOURCE: TLMC 05-20-15)
MRBRE55-50-00-219 Attachment Fittings Visual Check of PCU and Elevator, paying particular attention to the integritiy of fasteners, fitting lugs and the adjacent spar web
11.9 Months (+31
Days)(28-Mar-2017)-/+13628-Mar-2014Mos
Hrs
Ldg
(PKG 36 Month)
55 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (28-Mar-2017)1. RE 36 MosElevator External Skin, Structure and Attachments - CPCP Che...C55-00-813A/F55
MRB ≈24-Aug-2023RE55-50-00-220 Stabilizers Structure NDT Check of the vertical stabilizer to rudder hinge bolts for cracks
08-Aug-2005Mos
3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs
Ldg
(PKG 4800 Hour)
55 A/F
Ref.:PSP 612 Part 8 PT-55-50-02 (SOURCE: TLMC 05-20-15) (NOTE: This check may be traded - off for bolt replacement if economically
justifiable or convenient.)
MRB ≈24-Aug-2023RE55-50-00-221 Stabilizers Structure NDT Check of the horizontal stabilizer to elevator hinge bolts for cracks
08-Aug-2005Mos
3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs
Ldg
(PKG 4800 Hour)
55 A/F
Ref.:PSP 612 Part 8 PT-55-50-01 (SOURCE: TLMC 05-20-15) (NOTE: This check may be traded - off for bolt replacement if economically
justifiable or convenient.)
RecommendedRE (-)601-0116 Modification - Horiz/Stab to Vert/Stab Fairing - Drainage Provision and Corrosion Prevention
26-Jan-1987Mos
1,267Hrs
480Ldg
55 A/FComplied With
RecommendedT (A/R)601-0116 Rev 1 Modification - Horiz/Stab to Vert/Stab Fairing - Drainage Provision and Corrosion Prevention
Mos
Hrs
Ldg
55 A/FEff: 14-Jul-1986
RecommendedRE (-)601-0185 Special Check/Rework - Vertical Stabilizer - Missing Rivets
28-Mar-1989Mos
2,373Hrs
910Ldg
55 A/FComplied With
RecommendedT (A/R)601-0185 Rev 1 Special Check/Rework - Vertical Stabilizer - Missing Rivets
Mos
Hrs
Ldg
55 A/FEff: 21-May-1987
CPCPREC55-00-801 Vertical Stabilizer External Surfaces - CPCP Check including the following items: (1) Vertical Stabilizer External Surfaces
2.5 Years (+30 Days)(26-Sep-2018)-/+14826-Sep-2014Mos
Hrs
Ldg
(PKG 48 Month)
55 A/F
(SOURCE: TLMC 05-30-20)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM224/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
CPCPREC55-00-802 Vertical Stabilizer Front Spar - CPCP Check including the following items: (1) Forward face of the front spar / (2) Front spar to fuselage attachment fittings / (3) Splice
straps / (4) Fuselage skin adjacent to spar caps
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
55 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 55-30-00-210.)
CPCPREC55-00-803 Vertical Stabilizer Internal Structure - CPCP Check including the following items: (1) Front, mid and rear spar / (2) Skins (internal), ribs and stringers / (3) Rudder PCU
support (backup) structure / (4) Stringer splices at VS31.87% and VS55.62%
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
55 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 55-30-00-210.)
CPCPREC55-00-804 Vertical Stabilizer, Pitch Trim Actuator Attachment Structure - CPCP Check including the following items: (1) Attachment lugs and fittings to vertical stabilizer / (2)
Vertical stabilizer skin around fittings / (3) Pitch trim actuator attachment bolts (without removal) / (4) Top canted rib
2.5 Years (+30 Days)(26-Sep-2018)-/+14826-Sep-2014Mos
Hrs
Ldg
(PKG 48 Month)
55 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 55-50-00-213.)
CPCPREC55-00-805 Vertical Stabilizer Rear Spar Structure - CPCP Check including the following items: (1) Aft face of rear spar / (2) Hinge fittings and lugs / (3) Spar cap area at attachment
to fuselage / (4) Web at rib 1 area
11.9 Months (+31
Days)(28-Mar-2017)-/+13628-Mar-2014Mos
Hrs
Ldg
(PKG 36 Month)
55 A/F
(SOURCE: TLMC 05-30-20) (NOTE: [1] Deflect and secure rudder. [2] This task can be done in conjunction with Scheduled Maintenance
Instruction Task 55-50-00-214.)
CPCPREC55-00-806 Horizontal Stabilizer Front Spar - CPCP Check including the following items: (1) Front spar upper and lower cap and web / (2) Front spar splices / (3) Attachment
fittings of web to machined ribs / (4) Front spar covered by skin
2.5 Years (+30 Days)(26-Sep-2018)-/+14826-Sep-2014Mos
Hrs
Ldg
(PKG 48 Month)
55 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 55-10-00-202.)
CPCPREC55-00-807 Horizontal Stabilizer Rear Spar - CPCP Check including the following items: (1) Rear spar upper and lower cap and web / (2) Rear spar splices / (3) Hinge fittings and
lugs
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Jan-2011Mos
Hrs
Ldg
(PKG 60 Month)
55 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 55-10-00-203.)
CPCPREC55-00-808 Horizontal Stabilizer Internal Structure - CPCP Check including the following items: (1) Upper and lower internal skins / (2) Internal upper and lower skin splices / (3)
Ribs and stringers / (4) Internal PCU support attachment fittings / (5) Backup fittings / (6) Centerline structure assembly
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Jan-2011Mos
Hrs
Ldg
(PKG 60 Month)
55 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 55-10-00-204.)
CPCPREC55-00-809 Horizontal and Vertical Stabilizer - CPCP Check including the following items: (1) Horizontal Stabilizer pivot fittings / (2) Vertical Stabilizer pivot fittings / (3) Vertical
Stabilizer skin around pivot fittings / (4) Pivot pins (without removal)
2.5 Years (+30 Days)(26-Sep-2018)-/+14826-Sep-2014Mos
Hrs
Ldg
(PKG 48 Month)
55 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 55-50-00-211 and 55-50
-00-212.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM225/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
CPCPREC55-00-810 Horizontal Stabilizer, Pitch Trim Actuator Attachment - CPCP Check including the following items: (1) Attachment lugs and fittings / (2) Bathtub fittings / (3) Upper and
lower horizontal stabilizer skin splices
2.5 Years (+30 Days)(26-Sep-2018)-/+14826-Sep-2014Mos
Hrs
Ldg
(PKG 48 Month)
55 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with ScheduledMaintenance Instruction Task 55-50-00-213.)
CPCPREC55-00-811 Horizontal Stabilizer, External Surfaces - CPCP Check including the following items: (1) Upper and lower skin panels
2.5 Years (+30 Days)(26-Sep-2018)-/+14826-Sep-2014Mos
Hrs
Ldg
(PKG 48 Month)
55 A/F
(SOURCE: TLMC 05-30-20)
CPCPREC55-00-812 Rudder External Skin, Structure and Attachments - CPCP Check including the following items: (1) Rudder front spar assembly / (2) Hinge fittings and PCU attachments /
(3) Hinge attachment bolts (without removal)
11.9 Months (+31
Days)(28-Mar-2017)-/+13628-Mar-2014Mos
Hrs
Ldg
(PKG 36 Month)
55 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 55-50-00-216.)
CPCPREC55-00-813 Elevator External Skin, Structure and Attachments - CPCP Check including the following items: (1) Elevator front spar assembly / (2) Hinge and PCU attachment fittings
/ (3) Attachment bolts (without removal)
11.9 Months (+31
Days)(28-Mar-2017)-/+13628-Mar-2014Mos
Hrs
Ldg
(PKG 36 Month)
55 A/F
(SOURCE: TLMC 05-30-20) (NOTE: [1] Deflect and secure rudder [2] This task can be done in conjunction with Scheduled Maintenance
Instruction Task and 55-50-00-219.)
▼ 56 - WINDOWS
RE (O/C)Cabin Window
20-Sep-1983Mos
0Hrs
0Ldg
No.156 A/FUnknownUnknown
RE (O/C)Cabin Window
20-Sep-1983Mos
0Hrs
0Ldg
No.1056 A/FUnknownUnknown
RE (O/C)Cabin Window
20-Sep-1983Mos
0Hrs
0Ldg
No.256 A/FUnknownUnknown
RE (O/C)Cabin Window
20-Sep-1983Mos
0Hrs
0Ldg
No.356 A/FUnknownUnknown
RE (O/C)Cabin Window
20-Sep-1983Mos
0Hrs
0Ldg
No.456 A/FUnknownUnknown
RE (O/C)Cabin Window
20-Sep-1983Mos
0Hrs
0Ldg
No.556 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM226/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Cabin Window
20-Sep-1983Mos
0Hrs
0Ldg
No.656 A/FUnknownUnknown
RE (O/C)Cabin Window
20-Sep-1983Mos
0Hrs
0Ldg
No.756 A/FUnknownUnknown
RE (O/C)Cabin Window
20-Sep-1983Mos
0Hrs
0Ldg
No.856 A/FUnknownUnknown
RE (O/C)Cabin Window
20-Sep-1983Mos
0Hrs
0Ldg
No.956 A/FUnknownUnknown
RE (O/C)Cockpit Side Window
17-Jan-2004Mos
10,047.9Hrs
5,053Ldg
Left56 A/F600-33030-217867
RE (O/C)Cockpit Side Window
17-Jan-2004Mos
10,047.9Hrs
5,053Ldg
Right56 A/F600-33030-227800
RE (O/C)Windshield
07-Sep-2005Mos
10,813.8Hrs
5,509Ldg
Left56 A/F600-33030-259415
Component Inspection SimpleDUE: 12,262.7 Hrs1. RE 400 HrsWindshield - Functional Test of the windshield rain repellan...30-40-00-213A/F30
RE (O/C)Windshield
18-Dec-2014Mos
11,854.6Hrs363.5
Ldg
Right56 A/FOverhauled604-33030-26
11030 REPAIR
Component Inspection SimpleDUE: 12,262.7 Hrs1. RE 400 HrsWindshield - Functional Test of the windshield rain repellan...30-40-00-213A/F30
AWL ≈03-May-2017RE56-10-00-101 * Side Window Glazings - Prism Checks - Visual Check
10-Feb-2016Mos
590.8 Hrs12,63260012,041.2Hrs
6,326Ldg
56 A/F
Ref.:PSP 612 Part 9 VC-56-10-01 (Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-10-30)
AWL ≈20-Oct-2017RE56-10-00-102 * Windshield and Side Window Glazings - Prism Checks - Visual Check
29-Oct-2012Mos
812.3 Hrs12,853.51,20011,653.5Hrs
Ldg
56 A/F
Ref.:PSP 612 Part 9 VC-56-10-02 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM227/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈24-Aug-2018RE56-10-00-104 * Windshield and Side Window ’T’ Plate Fasteners - NDT Check
08-Aug-2005Mos
1,218.6 Hrs13,259.82,40010,859.8Hrs
Ldg
56 A/F
Ref.:PSP 612 Part 8 PT-56-10-01 (SOURCE: TLMC 05-10-30) (NOTE: It is acceptable to replace the fasteners with new fasteners in lieu of this
inspection.)
AWL ≈24-Aug-2018RE56-10-00-105 * Windshield and Side Window Lower T-Caps - Visual Check
08-Aug-2005Mos
1,218.6 Hrs13,259.82,40010,859.8Hrs
Ldg
56 A/F
Ref.:PSP 612 Part 9 VC-56-10-03 (SOURCE: TLMC 05-10-30)
AWL ≈29-Dec-2030RE56-10-00-106 * Windshield and Side Window Glazing - All Fasteners - NDT Check of the fasteners for cracks. Pay particular attention to the first thread and directly underneath the
countersink head. NDT Check all fasteners attaching glazings to sill, centre post, side strap and end post
05-Aug-2003Mos
7,144.4 Hrs19,185.69,6009,585.6Hrs
Ldg
56 A/F
Ref.:PSP 612 Part 8 PT-56-10-02 (SOURCE: TLMC 05-10-30) (NOTE: It is acceptable to replace the fasteners with new fasteners in lieu of this
inspection.)
MRB ≈18-Sep-2016RE56-10-00-201 Flight Compartment Windows Visual Check - Internal and External, paying particular attention to the aerodynamic seal
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
56 A/F
(SOURCE: TLMC 05-20-15)
OptionalRE (-)601-0006 Modification - Cabin Windows - Additional Installation
Mos
Hrs
Ldg
56 A/F
OptionalRE (-)601-0006 Rev 1 Modification - Cabin Windows - Additional Installation
Mos
Hrs
Ldg
56 A/F
OptionalRE (-)601-0006 Rev 2 Modification - Cabin Windows - Additional Installation
Mos
Hrs
Ldg
56 A/F
OptionalRE (-)601-0006 Rev 3 Modification - Cabin Windows - Additional Installation
Mos
Hrs
Ldg
56 A/F
OptionalRE (-)601-0006 Rev 4 Modification - Cabin Windows - Additional Installation
Mos
Hrs
Ldg
56 A/F
OptionalRE (-)601-0006 Rev 5 Modification - Cabin Windows - Additional Installation
Mos
Hrs
Ldg
56 A/F
OptionalT (A/R)601-0006 Rev 6 Modification - Cabin Windows - Additional Installation
Mos
Hrs
Ldg
56 A/FEff: 29-Apr-2013
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM228/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0027 Modification - Terminal Block - Hardware Replacement
26-Jan-1987Mos
1,267Hrs
470Ldg
56 A/FComplied With
RecommendedT (A/R)601-0027 Rev 1 Modification - Terminal Block - Hardware Replacement
Mos
Hrs
Ldg
56 A/FEff: 03-Feb-1984
RecommendedRE (-)601-0030 Modification - Windshields/Side Windows - Warning Placard
Mos
Hrs
Ldg
56 A/F
RecommendedRE (-)601-0030 Rev 1 Modification - Windshields/Side Windows - Warning Placard
Mos
Hrs
Ldg
56 A/FEff: 15-Jan-1985
OptionalT (A/R)601-0059 Modification - Flight Compartment - Improved Access for Windshield Replacement
Mos
Hrs
Ldg
56 A/FEff: 15-Aug-1985
OptionalT (A/R)601-0572 Modification - Flight Compartment Windows - Installation of the Center Post Strip Assemblies
Mos
Hrs
Ldg
56 A/FEff: 13-Mar-2006
▼ 57 - WINGS
AWL - Life Limit ≈24-Apr-2026REAileron Anti-Float Spring
20-Sep-1983Mos
0Hrs0
3,674 Ldg10,00010,0000Ldg0
Left57 A/FNew600-10057-5
UNKNOWN
AWL - Life Limit ≈24-Apr-2026REAileron Anti-Float Spring
20-Sep-1983Mos
0Hrs0
3,674 Ldg10,00010,0000Ldg0
Right57 A/FNew600-10057-6
UNKNOWN
RE (O/C)Aileron Assy
20-Sep-1983Mos
0Hrs0
0Ldg0
Left57 A/FNew600-13000-811
UNKNOWN
RE (O/C)Aileron Assy
20-Sep-1983Mos
0Hrs0
0Ldg0
Right57 A/FNew600-13000-812
UNKNOWN
RE (O/C)Flap Inboard Vane Assy
20-Sep-1983Mos
0Hrs0
0Ldg0
Left57 A/FNew600-14302-3
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM229/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Flap Inboard Vane Assy
20-Sep-1983Mos
0Hrs0
0Ldg0
Right57 A/FNew600-14302-4
UNKNOWN
RE (O/C)Flight Spoiler
20-Sep-1983Mos
0Hrs0
0Ldg0
Left57 A/FNew600-10602-35
UNKNOWN
RE (O/C)Flight Spoiler
20-Sep-1983Mos
0Hrs0
0Ldg0
Right57 A/FNew600-10602-36
UNKNOWN
RE (O/C)Ground Spoiler
20-Sep-1983Mos
0Hrs0
0Ldg0
Left57 A/FNew600-10502-1
UNKNOWN
RE (O/C)Ground Spoiler
20-Sep-1983Mos
0Hrs0
0Ldg0
Right57 A/FNew600-10502-2
UNKNOWN
RE (O/C)Inboard Flap Assy
20-Sep-1983Mos
0Hrs
0Ldg
Left57 A/FUnknownUnknown
RE (O/C)Inboard Flap Assy
20-Sep-1983Mos
0Hrs
0Ldg
Right57 A/FUnknownUnknown
AWL - Life Limit ≈14-Mar-2025REInboard Flap Vane Support Beam
20-Sep-1983Mos
0Hrs0
3,274 Ldg9,6009,6000Ldg0
Left No.157 A/FNew600-14250-15
UNKNOWN
AWL - Life Limit ≈14-Mar-2025REInboard Flap Vane Support Beam
20-Sep-1983Mos
0Hrs0
3,274 Ldg9,6009,6000Ldg0
Left No.257 A/FNew600-14250-15
UNKNOWN
AWL - Life Limit ≈14-Mar-2025REInboard Flap Vane Support Beam
20-Sep-1983Mos
0Hrs0
3,274 Ldg9,6009,6000Ldg0
Left No.357 A/FNew600-14250-15
UNKNOWN
AWL - Life Limit ≈14-Mar-2025REInboard Flap Vane Support Beam
20-Sep-1983Mos
0Hrs0
3,274 Ldg9,6009,6000Ldg0
Right No.157 A/FNew600-14250-15
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM230/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL - Life Limit ≈14-Mar-2025REInboard Flap Vane Support Beam
20-Sep-1983Mos
0Hrs0
3,274 Ldg9,6009,6000Ldg0
Right No.257 A/FNew600-14250-15
UNKNOWN
AWL - Life Limit ≈14-Mar-2025REInboard Flap Vane Support Beam
20-Sep-1983Mos
0Hrs0
3,274 Ldg9,6009,6000Ldg0
Right No.357 A/FNew600-14250-15
UNKNOWN
RE (O/C)Outboard Flap Assy
20-Sep-1983Mos
0Hrs
0Ldg
Left57 A/FUnknownUnknown
RE (O/C)Outboard Flap Assy
20-Sep-1983Mos
0Hrs
0Ldg
Right57 A/FUnknownUnknown
MandatoryRE (-)2014-03-17 Wings - fractured fastener heads found on the inboard flap hinge-box forward fitting at wing station (WS) 76.50
28-Mar-2014Mos
11,824.5Hrs
6,169Ldg
57 A/FBY INSPECTIONEff: 06-Mar-2014 Complied
With
Mandatory ≈29-Apr-2016RE2015-02-23 Wings
13-Nov-2015Mos
12,014.3Hrs
79 Ldg6,4051006,305Ldg
57 A/FBY INSPECTIONComplied With
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Rev 2A/F57
Mandatory ≈04-Oct-2020RE (-)2015-07-02 Wings
Mos
Hrs
1,674 Ldg[8,000]Ldg
57 A/FEff: 04-Jun-2015
Nextdue Share EarliestDUE:1. T 60 Days | 2. RE -Wings - Maintenance or Inspection Program Revision2015-07-02 Paragraph (g)A/F57
Nextdue Share EarliestDUE: 04-Jun-2019, 14,169 Ldg1. T 48 Mos, 7900 Ldg | 2. RE -Wings - Lug Edge Measurement and Inspection2015-07-02 Paragraph (h)(Inbd)A/F57
Nextdue Share EarliestDUE: 04-Jun-2019, 14,269 Ldg1. T 48 Mos, 8000 Ldg | 2. RE -Wings - Lug Edge Measurement and Inspection2015-07-02 Paragraph (h)(Outb)A/F57
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Wings - Corrective Actions2015-07-02 Paragraph (i)A/F57
MandatoryRE (-)2015-07-02 Paragraph (g) Wings - Maintenance or Inspection Program Revision
21-Oct-2015Mos
12,001.1Hrs
6,291Ldg
57 A/FREVISED AMMEff: 04-Jun-2015 Complied
With
MandatoryT2015-07-02 Paragraph (h)
(Inbd)
Wings - Lug Edge Measurement and Inspection
3.2 Years04-Jun-201948Mos
Hrs
7,843 Ldg≈14,1697,900Ldg
57 A/FEff: 04-Jun-2015
(NOTE: Inboard Flaps having less than or equal to 7400 total flight cycles as of the effective date of this AD.)
Compliance Share DoubleDUE: 26-Sep-2017, 7,900 Ldg1. T 48 Mos | 2. RE -Special Check – Flap Hinge Box – Forward Lugs Edge to Edge D...601-0631A/F57
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM231/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryT2015-07-02 Paragraph (h)
(Outb)
Wings - Lug Edge Measurement and Inspection
3.2 Years04-Jun-201948Mos
Hrs
7,943 Ldg≈14,2698,000Ldg
57 A/FEff: 04-Jun-2015
(NOTE: Outboard Flaps having equal to or less than 7500 total flight cycles as of the effective date of this AD.)
Compliance Share DoubleDUE: 26-Sep-2017, 7,900 Ldg1. T 48 Mos | 2. RE -Special Check – Flap Hinge Box – Forward Lugs Edge to Edge D...601-0631A/F57
MandatoryT (A/R)2015-07-02 Paragraph (i) Wings - Corrective Actions
Mos
Hrs
Ldg
57 A/FEff: 04-Jun-2015
MRB ≈30-Dec-2016RE57-00-00-202 Wing Structure Visual Check of leading edge external surface
05-Feb-2004Mos
426.1 Hrs (+40)12,467.3-/+402,40010,067.3Hrs
Ldg
(PKG 2400 Hour)
57 A/F
(SOURCE: TLMC 05-20-15)
MRBRE57-00-00-203 Wing Structure Visual Check of the following areas: (1) Wing leading edges for Piccolo tube failure or evidence of internal structural damage (hot spots, discoloration,
distortion and loose rivets) / (2) Lower Plank external surface between wing stations WS148.00 and WS196.00 / (3) Lower Plank external surface between wing stations
WS247.00 and WS288.00 / (4) Outboard of wing station WS324.00 / (5) Wing trailing edge
6.6 Months (+31
Days)(21-Oct-2016)-/+11221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
57 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (21-Oct-2016)1. RE 24 MosWing Lower External Surface, BL0.00 to WS353.00 - CPCP Check...C57-00-802A/F57
MRBRE57-00-00-204 Wing Structure - Wing Box Visual Check of the following items, paying particular attention for cracks and corrosion: (1) Upper wing box skin in the area between the
front and rear spars and span wise from BL0.00 to WS148.00 / (2) Upper skin splice at BL0.00 and the adjacent skin / (3) The upper two span wise lap splices on either
side of the center wing plank / (4) The upper fasteners and adjacent areas / (5) Lower wing box skin in the area between the front and rear spars and span wise from
BL0.00 to WS148.00 / (6) Lower skin splice at BL0.00 and the adjacent skin / (7) The lower two span wise lap splices on either side of the center wing plank / (8) The
lower skin around inspection panels and water drains / (9) The lower fasteners and the adjacent areas
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing Upper Surface, BL0.00 to BL50.00 - CPCP Check: (1) Wing...C57-00-803A/F57
AWL ≈09-Apr-2022T57-10-00-101 * Lower Wing Plank and Rear Spar - WS45.00 and WS47.00 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 2 RT-57-10-01 (SOURCE: TLMC 05-10-30)
AWL ≈20-Oct-2017RE57-10-00-102 * Lower Wing Plank - Rear Spar WS178.00 and WS189.00 - NDT Check
29-Oct-2012Mos
812.3 Hrs12,853.51,20011,653.5Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-10-02 (SOURCE: TLMC 05-10-30)
AWL ≈20-Oct-2017RE57-10-00-103 * Lower Wing Plank - Rear Spar at WS166.00 - NDT Check
29-Oct-2012Mos
812.3 Hrs12,853.51,20011,653.5Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-12 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM232/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈09-Apr-2022T57-10-00-104 * Front Spar Web at Lower Wing Plank - WS45.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-10-08 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈09-Apr-2022T57-10-00-106 * Front Spar Splice at the Lower Wing Plank - WS29.42 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-10-09 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈24-Aug-2023T57-10-00-108 * Lower Wing Plank and Rear Spar at WS148.00 - Visual Check
29-Jun-2006Mos
3,618.6 Hrs15,659.84,80010,859.8Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-18 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈29-Dec-2030RE57-10-00-109 * Wing Box - Internal Structure - Visual Check
05-Aug-2003Mos
7,144.4 Hrs19,185.69,6009,585.6Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-10-01 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-10-00-110 * Lower Wing Plank - Rear Spar - WS242.00 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-10-05 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-10-00-111 * Lower Wing Plank - Rear Spar at WS260.00 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-10-03 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-10-00-112 * Lower Wing Plank - Rear Spar at WS217.00 and WS222.00 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-10-04 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-10-00-113 * Rear Spar/Lower Wing Plank at WS219.00 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 2 RT-57-10-02 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-10-00-114 * Lower Wing Plank - WS314.50, Butt Strap and Front Spar - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-10-07 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-10-00-115 * Lower Wing Plank - WS315.00, Butt Strap and Rear Spar - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-10-06 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM233/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE57-10-00-205 Main Frame (Wing Center Section Internal Structure) Visual Check
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing Structure Between the Front Spar and Rear Spar, BL0.00 ...C57-00-804A/F57
MRBRE57-10-00-206 Main Frame (Front Spar Splice WS29.42) Visual Check (Internal and External) of the area around the front spar splice, paying particular attention to the webs, caps,
splices, rib and fastener surround area
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing Front Spar, BL0.00 to WS50.00 - CPCP Check of the follo...C57-00-805A/F57
MRBRE57-10-00-207 Main Frame (Wing Inboard Box Internal Structure WS45.00 to WS65.70 and WS85.50 to WS106.00) Visual Check
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-20-15) (NOTE: If evidence of corrosion or other defects are found, progressively check the adjacent outboard tank cavity,
until a defect free area is located.)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing Structure Between the Front Spar and Rear Spar, WS45.00...C57-00-806A/F57
MRBRE57-10-00-208 Main Frame (Wing Outboard Box Internal Structure WS148.00 to WS163.00 and WS199.00 to WS220.00) Visual Check
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-20-15) (NOTE: If evidence of corrossion or other defects are found, progressively check the adjacent outboard tank cavity,
until a defect free area is located)
MRBRE57-10-00-209 Main Frame (Rear Spar Splice at WS45.00) Visual Check (Internal and External) of the area around the rear spar splice, paying particular attention to the webs, caps,
splices,rib and fastener surround area
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing Rear Spar, BL0.00 to WS66.00 (External) - CPCP Check in...C57-00-807A/F57
AWL ≈10-Jan-2021RE57-20-00-116 * Wing Tip - External Surface - Visual Check
21-Oct-2015Mos
2,359.9 Hrs14,401.12,40012,001.1Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-20-01 (SOURCE: TLMC 05-10-30)
MRBRE57-20-00-210 Auxiliary Structure (Winglet) Visual Check (Internal and External), paying particular attention to front/rear spars and attachment to the wing
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWingtip/Winglet Assembly (Internal/External) - CPCP Check in...C57-00-808A/F57
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM234/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE57-20-00-211 Auxiliary Structure Visual Check of Wing Trailing Edge and Wing Leading Edge internal structure
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing Rear Spar and Auxiliary Spar, WS50.00 to WS353.00 - CPC...C57-00-809A/F57
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing Rear Spar and Auxiliary Spar, WS66.00 to WS148.00 - CPC...C57-00-811A/F57
AWL ≈20-Jan-2024T57-30-00-117 * Lower Center Wing Plank - WS65.00, Stringers 14 and 15 - NDT Check
29-Oct-2012Mos
3,812.3 Hrs15,853.54,20011,653.5Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-08 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈20-Oct-2017RE57-30-00-118 * Lower Wing Plank Near Main Landing Gear Trunnion - WS65.75 - NDT Check
29-Oct-2012Mos
812.3 Hrs12,853.51,20011,653.5Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-01 (SOURCE: TLMC 05-10-30)
AWL ≈20-Oct-2017RE57-30-00-119 * Lower Wing Plank - Auxiliary Spar Access Hole at WS85.00 - NDT Check
29-Oct-2012Mos
812.3 Hrs12,853.51,20011,653.5Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-02 (SOURCE: TLMC 05-10-30)
AWL ≈03-May-2017RE57-30-00-120 * Lower Wing Plank - WS88.00, Between Stringers 14 and 15 - Visual Check
25-Jul-2008Mos
590.8 Hrs12,6321,20011,432Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-13 (SOURCE: TLMC 05-10-30)
AWL ≈20-Oct-2017RE57-30-00-121 * Lower Center Wing Plank at WS45.00 - Stringers 14 and 15, Center and Forward Splice - NDT Check
29-Oct-2012Mos
812.3 Hrs12,853.51,20011,653.5Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-06 (SOURCE: TLMC 05-10-30)
AWL ≈20-Jan-2024T57-30-00-122 * Lower Center Wing Plank - WS65.00, Stringer 10 - NDT Check
29-Oct-2012Mos
3,812.3 Hrs15,853.54,20011,653.5Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-09 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈03-May-2017RE57-30-00-124 * Lower Center Wing Plank - WS45.00, Stringer 10 - NDT Check
25-Jul-2008Mos
590.8 Hrs12,6321,20011,432Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-10 (SOURCE: TLMC 05-10-30)
AWL ≈20-Oct-2032T57-30-00-125 * Lower Wing Planks - WS45.00, Stringers 15 and 16 - NDT Check
29-Oct-2012Mos
8,012.3 Hrs20,053.58,40011,653.5Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-11 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈20-Oct-2017RE57-30-00-126 * Wing Upper Cover - Visual Check
29-Oct-2012Mos
812.3 Hrs12,853.51,20011,653.5Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-28 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM235/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈20-Oct-2017RE57-30-00-127 * Lower Wing Plank - Aft Edge - WS163.00 to WS170.50 - NDT Check
29-Oct-2012Mos
812.3 Hrs12,853.51,20011,653.5Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-10-01 (SOURCE: TLMC 05-10-30)
AWL ≈20-Oct-2017RE57-30-00-128 * Lower Wing Planks - WS86.00, Stringers 14 to 17 - NDT Check
29-Oct-2012Mos
812.3 Hrs12,853.51,20011,653.5Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-14 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-30-00-129 * Lower Wing Planks - WS163.00, Stringer 15 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-15 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈09-Apr-2022T57-30-00-130 * Lower Wing Plank - WS148.00, Stringer 19 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 2 RT-57-30-01 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈09-Apr-2022T57-30-00-131 * Lower Wing Plank - Centerline Splice, Stringers 15 and 16 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-04 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-30-00-132 * Lower Wing Plank - WS94.00, Stringer 23 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-14 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-30-00-133 * Lower Wing Plank - WS106.40, Stringer 10 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-15 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-30-00-134 * Lower Wing Plank - WS106.40, Stringers 15 and 16 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-16 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-30-00-135 * Lower Wing Plank - WS127.50, Stringers 9 and 10 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-17 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-30-00-136 * Lower Wing Plank - WS199.00, Stringers 6 and 7 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-21 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-30-00-137 * Lower Wing Plank - WS199.00, Stringer 17 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-22 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM236/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈09-Apr-2022T57-30-00-138 * Lower Wing Plank - WS220.00, Stringer 7 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-23 (SOURCE: TLMC 05-10-30)
AWL ≈03-Feb-2021T57-30-00-139 * Lower Wing Plank - WS148.00, Stringers 8 and 9 - NDT Check
25-Jul-2008Mos
2,390.8 Hrs14,4323,00011,432Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-05 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈03-Feb-2021T57-30-00-140 * Lower Center Wing Plank - WS148.00, Stringer 15 - NDT Check
25-Jul-2008Mos
2,390.8 Hrs14,4323,00011,432Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-03 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈03-Aug-2018RE57-30-00-141 * Lower Center Wing Panel - Access Hole, WS112.00, Stringer 10 - NDT Check
25-Jul-2008Mos
1,190.8 Hrs13,2321,80011,432Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-04 (SOURCE: TLMC 05-10-30)
AWL ≈24-May-2017RE57-30-00-142 * Fuel Tank Water Drain Port - WS48.00, Stringer 17 - Visual Check
08-Aug-2005Mos
618.6 Hrs12,659.81,80010,859.8Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-01 (SOURCE: TLMC 05-10-30)
AWL ≈03-Aug-2018RE57-30-00-143 * Lower Center Wing Plank - Access Hole, WS220.00,Stringer 10 - NDT Check
25-Jul-2008Mos
1,190.8 Hrs13,2321,80011,432Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-07 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-30-00-145 * Lower Wing Plank - WS45.00, Stringer 8 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-05 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈10-Jan-2036T57-30-00-150 * Lower Forward Wing Plank - WS65.75, Stringer 17 - NDT Check
21-Oct-2015Mos
9,559.9 Hrs21,601.19,60012,001.1Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-13 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈09-Apr-2022T57-30-00-153 * Lower Aft Wing Plank at the Rear Spar Between WS59.00 and WS65.75 - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-16 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈09-Apr-2022T57-30-00-155 * Lower Wing Plank - WS242.00, Stringer 9 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-26 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-30-00-156 * Lower Wing Plank - WS242.00 Inboard/Outboard and WS238.00, Stringer 16 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-24 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM237/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈09-Apr-2022T57-30-00-159 * Lower Wing Plank - WS264.00, Stringers 6 and 7 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-27 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-30-00-160 * Lower Wing Plank Centerline Splice Between Stringer 8 and Stringer 9 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-03 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈09-Apr-2022T57-30-00-162 * Lower Wing Plank - WS242.00, Stringer 7 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-25 (SOURCE: TLMC 05-10-30)
MRB ≈30-Dec-2016RE57-30-00-212 Plates/Skins (Upper Wing Box) Visual Check - External
05-Feb-2004Mos
426.1 Hrs (+40)12,467.3-/+402,40010,067.3Hrs
Ldg
(PKG 2400 Hour)
57 A/F
(SOURCE: TLMC 05-20-15)
MRBRE57-30-00-213 Plates/Skins (Wing Box Lower Skin BL0.00 to WS148.00) Visual Check - External
6.6 Months (+31
Days)(21-Oct-2016)-/+11221-Oct-2015Mos
Hrs
Ldg
(PKG 12 Month)
57 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (21-Oct-2016)1. RE 60 MosWing Upper External Surface, WS50.00 to WS353.00 - CPCP Chec...C57-00-819A/F57
AWL - Repair ≈14-Feb-2017RE57-30-00-401 Wing Fuel Access Holes (NDT and Visual Check)
25-Jul-2008Mos
485.8 Hrs12,5271,09511,432Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-20, Ref.:PSP 612 Part 9 VC-57-30-45 (ZONE: 500) (ACCESS: 140-DL,550-GB) (SOURCE: TLMC 5-10-25)
AWL - Repair ≈20-Sep-2017RE57-30-00-401 Wing Fuel Access Holes (NDT and Visual Check)
25-Jul-2008Mos
773.8 Hrs12,8151,38311,432Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-20, Ref.:PSP 612 Part 9 VC-57-30-45 (ZONE: 500,600,) (ACCESS: 540-BB-CB-DB-EB-FB-GB,550-AB-BB-DB-EB-
FB,140-DR-ER) (SOURCE: TLMC 5-10-25) (NOTE: Additional Aceess Panel: 640-AB-FB-GB,650-AB-CB-FB-GB-HB)
AWL - Repair ≈13-Apr-2016RE57-30-00-401 Wing Fuel Access Holes (NDT and Visual Check)
26-Dec-2007Mos
84.1 Hrs12,125.394111,184.3Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-20, Ref.:PSP 612 Part 9 VC-57-30-45 (ZONE: 500,600) (ACCESS: 550-CB,650-BB-DB-EB) (SOURCE: TLMC 5-10-25)
AWL - Repair ≈16-Nov-2016RE57-30-00-401 Wing Fuel Access Holes (NDT and Visual Check)
02-Apr-2005Mos
367.8 Hrs12,4091,69110,718Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-30-20, Ref.:PSP 612 Part 9 VC-57-30-45 (ZONE: 600,) (ACCESS: 650-CB) (SOURCE: TLMC 5-10-25)
AWL - Repair ≈04-Dec-2016RE57-30-00-402 Fuel Tank Water Drain Holes (Visual Check) Wing Station: 244.0
25-Jul-2008Mos
391.8 Hrs12,4331,00111,432Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-41 (ZONE: 500) (ACCESS: 550-DB) (SOURCE: TLMC 5-10-25)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM238/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL - Repair ≈08-Jun-2017RE57-30-00-402 Fuel Tank Water Drain Holes (Visual Check)Wing Station: 48.0,68.7,88.5,151.0
25-Jul-2008Mos
637.8 Hrs12,6791,24711,432Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-30-41 (ZONE: 500,600) (ACCESS: 640-BB,540-DB,540-EB,550-AB) (SOURCE: TLMC 5-10-25)
≈10-Nov-2016RE57-30-00-407 Wing Lower Plank/Rear Spar, LBL42.5-38
Mos
359.8 Hrs12,40112,401Hrs
Ldg
57 A/F
AWL ≈14-Mar-2040T57-40-00-163 * Inboard Flap - Forward Attachment Fittings - Visual Check
Mos
Hrs
8,674 Ldg15,00015,000Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-40-01 (SOURCE: TLMC 05-10-30) (NOTE: Post SB A601-0135)
AWL ≈14-Mar-2040T57-40-00-165 * Outboard Flap Arm - Forward Upper Lugs, WS220.00 - NDT Check
Mos
Hrs
8,674 Ldg15,00015,000Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-40-07 (SOURCE: TLMC 05-10-30)
AWL ≈14-Mar-2040T57-40-00-166 * Inboard Flap - Flap Arm Lower Lugs - NDT Check
Mos
Hrs
8,674 Ldg15,00015,000Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-40-04 (SOURCE: TLMC 05-10-30)
AWL ≈14-Mar-2040T57-40-00-167 * Outboard Flap Wing/Hinge Box Forward Fitting - NDT Check
Mos
Hrs
8,674 Ldg15,00015,000Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-40-08 (SOURCE: TLMC 05-10-30)
AWL ≈14-Mar-2040T57-40-00-168 * Outboard Flap-Vane Support Fittings - Flap Stations 189.57, 235.84 and 280.66 - Visual Check
Mos
Hrs
8,674 Ldg15,00015,000Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-40-03 (SOURCE: TLMC 05-10-30)
AWL ≈22-Jan-2022RE57-40-00-171 * Flight Spoilers Wing/Hinge Attachment Points - NDT Check
08-Apr-2015Mos
2,855.9 Hrs14,897.13,00011,897.1Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-40-01 (SOURCE: TLMC 05-10-30)
AWL ≈14-Mar-2040T57-40-00-172 * Outboard Flap - Hinge Box Lower Flange Supports - NDT Check
Mos
Hrs
8,674 Ldg15,00015,000Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-40-09 (SOURCE: TLMC 05-10-30)
AWL ≈14-Mar-2040T57-40-00-173 * Inboard Flap - Forward Attachment Lugs - NDT Check
Mos
Hrs
8,674 Ldg15,00015,000Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-40-05 (SOURCE: TLMC 05-10-30)
AWL ≈29-Jun-2018RE57-40-00-174 * Inboard Flap - Hinge Supports Part Numbers 600-10116-13 and 600-10117-13 - NDT Check
24-Oct-2011Mos
Hrs
859 Ldg7,1851,2005,985Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-40-02 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM239/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈04-Oct-2020T57-40-00-175 * Outboard Flap - Hinge Box Forward Attachment Lugs - NDT Check
Mos
Hrs
1,674 Ldg8,0008,000Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-40-10 Part B (SOURCE: TLMC 05-10-30)
AWL ≈24-Dec-2017T57-40-00-178 * Inboard Flap - WS127.25 Wing Rib Backup Fitting - NDT Check
Mos
Hrs
674 Ldg7,0007,000Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-40-03 (SOURCE: TLMC 05-10-30)
AWL ≈10-Apr-2032RE57-40-00-179 * Wing to Fuselage Attachment Fitting Lugs FS424.00 and BL45.00 - Visual Check
21-Oct-2015Mos
7,759.9 Hrs19,801.17,80012,001.1Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-40-07 (SOURCE: TLMC 05-10-30) (NOTE: Post SB 601-0280)
AWL ≈14-Mar-2040T57-40-00-180 * Inboard Flap - Vane Carriages - NDT Check
Mos
Hrs
8,674 Ldg15,00015,000Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-40-06 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-40-00-183 * Wing/Fuselage Attachment Fitting Lugs, FS473.00 and BL45.00, FS513.00 and BL45.00, FS513.00 and BL13.50 - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-40-02 (SOURCE: TLMC 05-10-30)
AWL ≈29-Dec-2030RE57-40-00-189 * Aileron - Hinge Bolts - Visual Check
05-Aug-2003Mos
7,144.4 Hrs19,185.69,6009,585.6Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-40-05 (SOURCE: TLMC 05-10-30)
AWL ≈14-Mar-2040T57-40-00-198 * Flap Hinge Bolt Attachments - NDT Check
Mos
Hrs
8,674 Ldg15,00015,000Ldg
57 A/F
Ref.:PSP 612 Part 8 PT-57-40-01 (SOURCE: TLMC 05-10-30)
AWL ≈29-Dec-2030RE57-40-00-199 * Flight Spoiler - Hinge Bolts - Visual Check
05-Aug-2003Mos
7,144.4 Hrs19,185.69,6009,585.6Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-40-06 (SOURCE: TLMC 05-10-30)
MRB ≈30-Dec-2016RE57-40-00-214 Attachment Fittings - Main Gear Side Brace (MLG Actuator Pickup) Visual Check of structure, paying particular attention to the following items: (1) The wing upper aft
panel and intercostal for deterioration of protective treatments / (2) The wing to fuselage attachment lug / (3) The area surrounding actuator bolt holes / (4) The
fasteners for looseness / (5) The area adjacent to the fasteners / (6) The adjacent spar web and the upper wing skin
05-Feb-2004Mos
426.1 Hrs (+40)12,467.3-/+402,40010,067.3Hrs
Ldg
(PKG 2400 Hour)
57 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈24-Aug-2023RE57-40-00-215 Wing Structure NDT Check of wing to aileron hinge bolts for cracks
05-Aug-2005Mos
3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs
Ldg
(PKG 4800 Hour)
57 A/F
Ref.:PSP 612 Part 8 PT-57-40-02 (SOURCE: TLMC 05-20-15) (NOTE: This check may be traded-off for bolt replacement ifeconomically justifiable
or convenient.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM240/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈24-Aug-2023RE57-40-00-216 Wing to Flap Hinge Bolts NDT Check
08-Aug-2005Mos
3,618.6 Hrs (+40)(15,659.8)-/+404,80010,859.8Hrs
Ldg
(PKG 4800 Hour)
57 A/F
Ref.:PSP 612 Part 8 PT-57-40-03 (SOURCE: TLMC 05-20-15) (NOTE: This check may be traded-off for bolt replacement ifeconomically justifiable
or convenient.)
MRBRE57-40-00-217 Attachment Fittings (Main Gear Trunnion) Visual Check (as externally visible) by gaining access through the MLG bay and trailing edge structure with the flaps
extended, paying particular attention to the following items: (1) Integrity of the area surrounding fastener holes / (2) Auxiliary and rear spar splices to the trunnion
fitting (looking for distortion in the spars) / (3) The area surrounding the bushing
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-20-15)
MRBRE57-40-00-218 Attachment Fittings (Wing to Fuselage Attach Assembly FS424.00, FWD) Visual Check assembly as visible, paying particular attention to the following items: (1)
Deterioration of protective treatments / (2) The area surrounding the fastener holes / (3) The wing to fuselage attachment lug
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing to Fuselage Attachment Fitting, FS424.00 and BL45.00 - ...C57-00-812A/F57
MRBRE57-40-00-219 Attachment Fittings (Wing to Fuselage Attachment Fitting FS473.15, Center) Visual Check assembly as visible, paying particular attention tothe following items: (1)
Deterioration of protective treatments / (2) Integrity of bolt hole surround areas / (3) Wing to fuselage attachment lug
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosWing to Fuselage Attachment Fitting, FS473.15 and BL45.00 - ...C57-00-813A/F57
MRBRE57-40-00-220 Attachment Fittings (Hinge/Actuator Aileron) Visual Check (Upon removal of the upper and lower aerodynamic seals), paying particular attention to the following
items: (1) Deterioration of protective treatments / (2) The area of the hinge and actuator bolt holes / (3) Wear in the hinge and actuator attachment fitting bolt holes
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-20-15)
MRBRE57-40-00-221 Attachment Fittings (Flap Hinges) Visual Check (Upon extension of the flaps) of the hinge arm assembly, paying particular attention to the following items: (1) The
hinge arm attachment point on the flap surface / (2) The area surrounding the clevis pin / (3) The area adjacent to the fasteners on the machined plates ofthe hinge
arm / (4) Wear of the clevis pin and bolt holes of the flap hinge arm attachment points
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosOutboard Flap (External) - CPCP Check including the followin...C57-00-814A/F57
AWL ≈24-Jun-2020T57-40-01-101 * Inboard Flap - Hinge Box Forward Lugs - NDT Check
Mos
Hrs
1,574 Ldg7,9007,900Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-40-10 Part A (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM241/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRBRE57-50-00-222 Flight Control Surfaces (Ailerons, Spoilers and Flaps) Visual Check of the external surfaces of Ailerons, Spoilers, Inboard Flaps and Outboard Flaps. Inspect for condition
of external surfaces as well as externally visible flaws indicating damage in the internal structure
5.8 Months (+30
Days)(26-Sep-2016)-/+16024-Oct-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-20-15)
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosInboard Flap (External) - CPCP Check including the following...C57-00-815A/F57
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosAileron (External) - CPCP Check including the following item...C57-00-817A/F57
Also ConsiderDUE: (26-Sep-2016)1. RE 60 MosFlight Spoiler (External) - CPCP Check including the followi...C57-00-818A/F57
AWL ≈23-Apr-2020RE57-51-00-186 * Ailerons - Visual Check
10-Aug-2004Mos
2,017.1 Hrs14,058.33,60010,458.3Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-51-01 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T57-51-00-187 * Ailerons - Upper and Lower Skin and Front Spar - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-51-02 (SOURCE: TLMC 05-10-30)
AWL ≈14-Jul-2023T57-53-00-161 * Outboard Flap-Vane Support Struts - Flap Stations 171.94 and 296.00 - NDT Check
Mos
Hrs
2,674 Ldg9,0009,000Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-53-08 (SOURCE: TLMC 05-10-30)
AWL ≈14-Mar-2040T57-53-00-164 * Outboard Flap-Vane Intermediate Support - Flap Stations 209.39 and 254.96 - NDT Check
Mos
Hrs
8,674 Ldg15,00015,000Ldg
57 A/F
Ref.:PSP 612 Part 4 UT-57-53-01, Ref.:PSP 612 Part 6 ET-57-53-09 (SOURCE: TLMC 05-10-30)
AWL ≈14-Mar-2040T57-53-00-176 * Outboard Flap-Vane Intermediate Support Fittings - Flap Stations 209.39 and 254.96 - NDT Check
Mos
Hrs
8,674 Ldg15,00015,000Ldg
57 A/F
Ref.:PSP 612 Part 4 UT-57-53-02, Ref.:PSP 612 Part 6 ET-57-53-06 (SOURCE: TLMC 05-10-30)
AWL ≈14-Mar-2040T57-53-00-181 * Outboard Flap-Vane End Ramps - Flap Stations 171.94 and 296 - NDT Check
Mos
Hrs
8,674 Ldg15,00015,000Ldg
57 A/F
Ref.:PSP 612 Part 4 UT-57-53-02, Ref.:PSP 612 Part 6 ET-57-53-06 (SOURCE: TLMC 05-10-30)
AWL ≈14-Mar-2040T57-53-00-182 * Outboard Flap - Forward Lugs - NDT Check
Mos
Hrs
8,674 Ldg15,00015,000Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-53-05 (SOURCE: TLMC 05-10-30)
AWL ≈04-Feb-2029T57-53-00-190 * Inboard Flap - Front Spar - Visual Check
Mos
Hrs
4,674 Ldg11,00011,000Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-53-01 (SOURCE: TLMC 05-10-30)
AWL ≈21-Apr-2031T57-53-00-191 * Inboard Flap - Vane Support Attachment Brackets - NDT Check
05-Aug-2003Mos
Hrs
5,471 Ldg11,7977,0004,797Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-53-01 (SOURCE: TLMC 05-10-30) (NOTE: Post SB A601-0532 with: (1) No gaps/cracks at original bracket)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM242/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈24-Apr-2026T57-53-00-192 * Outboard Flap-Vane Tangs (End Support) - Flap Stations 189.57, 235.84 and 280.66 - NDT Check
Mos
Hrs
3,674 Ldg10,00010,000Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-53-02 (SOURCE: TLMC 05-10-30)
AWL ≈24-Apr-2026T57-53-00-194 * Outboard Flap - Front Spar - NDT Check
Mos
Hrs
3,674 Ldg10,00010,000Ldg
57 A/F
Ref.:PSP 612 Part 6 ET-57-53-03 (SOURCE: TLMC 05-10-30)
MRB ≈30-Dec-2016RE57-53-00-224 Flaps (Inboard Flap Vane Assembly) Visual Check (Upon removal of the lower access panels) of each of the vane actuating assemblies. Reinstall lower access panels.
05-Feb-2004Mos
426.1 Hrs (+40)12,467.3-/+402,40010,067.3Hrs
Ldg
(PKG 2400 Hour)
57 A/F
(SOURCE: TLMC 05-20-15)
AWL ≈09-Apr-2022T57-55-00-197 Flight Spoiler - Upper and Lower Skin - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
57 A/F
Ref.:PSP 612 Part 9 VC-57-55-01 (SOURCE: TLMC 05-10-30)
RecommendedRE (-)601-0013 Modification - Rear Spar Bute Door Area - Fastener Substitution
Mos
Hrs
Ldg
57 A/F
RecommendedRE (-)601-0013 Rev 1 Modification - Rear Spar Bute Door Area - Fastener Substitution
Mos
Hrs
Ldg
57 A/FEff: 24-Oct-1984
RecommendedRE (-)601-0025 Special Check/Modification - Outboard Flap - CAM Follower Engagement
17-Sep-1985Mos
607Hrs
262Ldg
57 A/FEff: 06-Sep-1983 Complied With
RecommendedRE (-)601-0029 Modification - Wing Trailing Edge and Outboard Flap Vane - Rubbing Strip Addition
28-Mar-1989Mos
Hrs
Ldg
57 A/FComplied With
RecommendedT (A/R)601-0029 Rev 1 Modification - Wing Trailing Edge and Outboard Flap Vane - Rubbing Strip Addition
Mos
Hrs
Ldg
57 A/FEff: 24-May-1985
RecommendedRE (-)601-0134 Modification - Inboard Flap Hinge Forward Fairings - Upper Edge Strengthening
Mos
Hrs
Ldg
57 A/F
RecommendedRE (-)601-0134 Rev 1 Modification - Inboard Flap Hinge Forward Fairings - Upper Edge Strengthening
Mos
Hrs
Ldg
57 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM243/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0134 Rev 2 Modification - Inboard Flap Hinge Forward Fairings - Upper Edge Strengthening
26-Jan-1987Mos
1,267Hrs
480Ldg
57 A/FEff: 28-Mar-1988 Complied With
OptionalT (A/R)601-0202 Modification - Auxiliary Spar Assemblies and Access Panels - Deflector Plates and Drain Holes
Mos
Hrs
Ldg
57 A/FEff: 31-Aug-1987
RecommendedRE (-)601-0221 Modification - Leading Edge Bleed Air Access Panels - Ground Stud Relocation
28-Mar-1989Mos
2,373Hrs
910Ldg
57 A/FEff: 21-Oct-1988 Complied With
OptionalRE (-)601-0260 Modification - Inboard Trailing Edge - Gusset ReplacementInboard Trailing Edge - Gusset Replacement
Mos
Hrs
Ldg
57 A/F
OptionalT (A/R)601-0260 Rev 1 Modification - Inboard Trailing Edge - Gusset ReplacementInboard Trailing Edge - Gusset Replacement
Mos
Hrs
Ldg
57 A/FEff: 30-Nov-1989
RecommendedRE (-)601-0610 Special Check – Inboard Flaps – Forward Lugs
Mos
Hrs
Ldg
57 A/F
Recommended ≈14-Mar-2040T (A/R)601-0610 Rev 1 Special Check – Inboard Flaps – Forward Lugs
Mos
Hrs
8,674 Ldg[15,000]Ldg
57 A/FEff: 27-Apr-2011
RecommendedT (A/R)601-0611 Rework/Modification – Ailerons – Addition of Drain Holes on Aileron PCU Access Panels
Mos
Hrs
Ldg
57 A/FEff: 19-Mar-2012
RecommendedRE (-)601-0624 Special Check/Modification – Attachment Fittings – Wings Box Main Landing Gear (MLG) Side Brace Fittings
8.5 Months[18-Dec-2016]18-Dec-2014Mos
11,854.6Hrs
Ldg
57 A/FPART AEff: 01-Oct-2012 Complied
With
RecommendedT601-0631 Special Check – Flap Hinge Box – Forward Lugs Edge to Edge Distance
1.5 Years[26-Sep-2017]48Mos
Hrs
1,574 Ldg[7,900]Ldg
57 A/FEff: 26-Sep-2013
RecommendedT (A/R)601-0636 Special Check/Rework – Attachment Fittings – Serialization of Main Landing Gear (MLG) Side-Brace Fitting-Shaft Part No. 600-10237-3
Mos
Hrs
Ldg
57 A/FEff: 09-Sep-2014
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM244/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Mandatory ≈28-Feb-2017RE84-13-03 R1 Flap Vane Support Straps
13-Nov-2015Mos
12,014.3Hrs
379 Ldg6,7054006,305Ldg
57 A/FSI A601-004.R3Eff: 26-Jul-1985 Complied
With
AlertRE (-)A601-0096 Special Check/Modification - Aileron - Hinge/Actuator Fitting
Mos
Hrs
Ldg
57 A/F
AlertRE (-)A601-0096 Rev 1 Special Check/Modification - Aileron - Hinge/Actuator Fitting
27-Feb-1999Mos
5,912Hrs
2,584Ldg
57 A/FEff: 25-Nov-1985 Complied With
AlertRE (-)A601-0135 Modification - Inboard Flap Hinge Arm Forward Fittings - Fastener Replacement
Mos
Hrs
Ldg
57 A/F
AlertRE (-)A601-0135 Rev 1 Modification - Inboard Flap Hinge Arm Forward Fittings - Fastener Replacement
26-Jan-1987Mos
Hrs
Ldg
57 A/FEff: 03-Apr-1986 Complied With
AlertRE (-)A601-0554 Special Check - Plates/Skins - Possible Development of Crack(s) on Lower Wing Plank at WS148.02 (Rear Spar)
Mos
Hrs
Ldg
57 A/F
AlertRE (-)A601-0554 Rev 1 Special Check - Plates/Skins - Possible Development of Crack(s) on Lower Wing Plank at WS148.02 (Rear Spar)
24-Mar-2003Mos
9,346.7Hrs
4,655Ldg
57 A/FEff: 30-Jan-2004 Complied With
AlertRE (-)A601-0627 Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners
OVD[26-Sep-2015]Mos
Hrs
Ldg
57 A/F
Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Part AA/F57
Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Part BA/F57
Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Part CA/F57
AlertRE (-)A601-0627 Part A Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Inspection
Mos
Hrs
Ldg
57 A/FEff: 26-Sep-2013
AlertRE (-)A601-0627 Part B Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Removal / Re-Installation
Mos
Hrs
Ldg
57 A/FEff: 26-Sep-2013
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM245/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AlertRE (-)A601-0627 Part C Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Fwd Fasteners Heads correctly oriented.
Mos
Hrs
Ldg
57 A/FEff: 26-Sep-2013
AlertRE (-)A601-0627 Rev 1 Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners
Mos
Hrs
Ldg
57 A/F
Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Rev 1 Part AA/F57
Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Rev 1 Part BA/F57
Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Rev 1 Part CA/F57
AlertRE (-)A601-0627 Rev 1 Part A Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Inspection
Mos
Hrs
Ldg
57 A/FEff: 26-Feb-2014
AlertRE (-)A601-0627 Rev 1 Part B Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Removal / Re-Installation
Mos
Hrs
Ldg
57 A/FEff: 26-Feb-2014
AlertRE (-)A601-0627 Rev 1 Part C Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Fwd Fasteners Heads correctly oriented.
Mos
Hrs
Ldg
57 A/FEff: 26-Feb-2014
AlertT (A/R)A601-0627 Rev 2 Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners
Mos
Hrs
Ldg
57 A/FEff: 09-Dec-2014
Nextdue Share EarliestDUE:1. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Rev 2 Part AA/F57
Nextdue Share EarliestDUE: 26-Sep-20171. T 24 Mos | 2. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Rev 2 Part BA/F57
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification – Attachment Fittings – Inboard F...A601-0627 Rev 2 Part CA/F57
AlertRE (-)A601-0627 Rev 2 Part A Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Inspection
13-Nov-2015Mos
12,014.3Hrs
6,305Ldg
57 A/FEff: 09-Dec-2014 Complied With
AlertTA601-0627 Rev 2 Part B Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Removal / Re-Installation
1.5 Years[26-Sep-2017]24Mos
Hrs
Ldg
57 A/FEff: 09-Dec-2014
AlertT (A/R)A601-0627 Rev 2 Part C Special Check/Modification – Attachment Fittings – Inboard Flap Hinge Box Forward Attachment Fittings Fasteners - Fwd Fasteners Heads correctly oriented.
Mos
Hrs
Ldg
57 A/FEff: 09-Dec-2014
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM246/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
CPCPREC57-00-801 Wing Front Spar and Leading Edge WS50.00 to WS353.00 - CPCP Check of the following items: (1) Forward face of the front spar / (2) Leading edge structure (internal
and external) / (3) Wing anti-ice installations / (4) Piccolo installations
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20)
CPCPREC57-00-802 Wing Lower External Surface, BL0.00 to WS353.00 - CPCP Check including the following items: (1) Wing lower skins / (2) Skin splices / (3) Splice plates
10 Months (+29
Days)(30-Jan-2017)-/+12430-Jan-2015Mos
Hrs
Ldg
(PKG 24 Month)
57 A/F
(SOURCE: TLMC 05-30-20) (NOTE: [1] With fuselage fairings installed [2] This task can be done in conjunction with Scheduled Maintenance
Instruction Task 57-00-00-203.)
CPCPREC57-00-803 Wing Upper Surface, BL0.00 to BL50.00 - CPCP Check: (1) Wing upper external surface / (2) Wing upper skin splice
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction
Task 57-00-00-204.)
CPCPREC57-00-804 Wing Structure Between the Front Spar and Rear Spar, BL0.00 to BL45.00 - CPCP Check including the following items: (1) Wing structure (2) Area around all access
panel openings, internal and external.
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 57-10-00-205.)
CPCPREC57-00-805 Wing Front Spar, BL0.00 to WS50.00 - CPCP Check of the following items: (1) Forward face of the front spar, wing center section / (2) Splices, web, caps and machined
fittings
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction
Task 57-10-00-206.)
CPCPREC57-00-806 Wing Structure Between the Front Spar and Rear Spar, WS45.00 to WS353.00 (Internal) - CPCP Check including the following items: (1) Wing structure / (2) Machined
backup fittings / (3) Area around access panel openings (internal and external)
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 57-10-00-207.)
CPCPREC57-00-807 Wing Rear Spar, BL0.00 to WS66.00 (External) - CPCP Check including the following items: (1) Aft face of the rear spar / (2) All attachments / (3) MLG trunnion and
MLG door attachment
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction
Task 57-10-00-209.)
CPCPREC57-00-808 Wingtip/Winglet Assembly (Internal/External) - CPCP Check including the following items: (1) Wingtip/winglet assembly / (2) Attachment to the wing
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 57-20-00-210.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM247/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
CPCPREC57-00-809 Wing Rear Spar and Auxiliary Spar, WS50.00 to WS353.00 - CPCP Check including the following items: (1) Attachment fittings and hinges / (2) Auxiliary spar aft face
WS50.00 to WS148.00 / (3) Web / (4) Rear spar aft face WS148.00 to WS353.00
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-30-20) (NOTE: [1] Lower and secure flaps. [2] This task can be done in conjunction with Scheduled Maintenance Instruction
Task 57-20-00-211.)
CPCPREC57-00-810 Main Landing Gear Actuator Fitting at Wing Box FS513.00 and BL13.50 - CPCP Check including the following items: (1) Actuator fitting(2) Wing upper aft panel(3)
Intercostal and spar web(4) Bolt (without removal)
2.5 Years (+30 Days)(26-Sep-2018)-/+14826-Sep-2014Mos
Hrs
Ldg
(PKG 48 Month)
57 A/F
Ref.:PSP 607 51-54-153/3 (SOURCE: TLMC 05-30-20)
CPCPREC57-00-811 Wing Rear Spar and Auxiliary Spar, WS66.00 to WS148.00 - CPCP Check of all internal structure between and including: (1) Rear spar / (2) Auxiliary spar / (3) Wing
planks
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 57-20-00-211.)
CPCPREC57-00-812 Wing to Fuselage Attachment Fitting, FS424.00 and BL45.00 - CPCP Check including the following items: (1) Adjacent wing plank / (2) Lugs and attachment fittings
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 57-40-00-218.)
CPCPREC57-00-813 Wing to Fuselage Attachment Fitting, FS473.15 and BL45.00 - CPCP Check including the following items: (1) Attachment lugs and fittings / (2) Adjacent wing plank
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 57-40-00-219.)
CPCPREC57-00-814 Outboard Flap (External) - CPCP Check including the following items: (1) External surfaces / (2) Hinge arm assemblies and attachment fittings / (3) Hinge bolts
(without removal) / (4) Vanes and vane support structures / (5) Flap front spar / (6) Wing plank under the fairings
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 57-40-00-221.)
CPCPREC57-00-815 Inboard Flap (External) - CPCP Check including the following items: (1) External surfaces / (2) Vane and vane attachment brackets / (3) Front spar / (4) Hinge arm
assemblies, hinge bolts (without removal) andattachment fittings / (5) Attachment points on the flap and wing surfaces / (6) Backup fittings in the wing / (7) Wing
plank under fairings
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 57-50-00-222.)
CPCPREC57-00-816 Inboard Flap Vane Actuating Assemblies - CPCP Check including the following: (1) Vane actuating assemblies
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-30-20)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM248/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
CPCPREC57-00-817 Aileron (External) - CPCP Check including the following items: (1) External surfaces / (2) Hinge fittings and lugs / (3) Hinge bolts (without removal)
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 57-50-00-222.)
CPCPREC57-00-818 Flight Spoiler (External) - CPCP Check including the following items: (1) External surfaces / (2) Hinge fittings and lugs / (3) Hinge bolts (without removal)
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-30-20) (NOTE: [1] Extend spoliers. [2] This task can be done in conjunction with Scheduled Maintenance Instruction Task
57-50-00-222.)
CPCPREC57-00-819 Wing Upper External Surface, WS50.00 to WS353.00 - CPCP Check including the following items: (1) Upper surface
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-30-20) (NOTE: This task can be done in conjunction with Scheduled Maintenance Instruction Task 57-30-00-213.)
CPCPREC57-00-820 Wing to Fuselage Attachment Fitting, WS513.00 and BL45.00 - CPCP Check including the following items: (1) Adjacent wing plank / (2) Lower link bolt (without
removal) / (3) Link
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
57 A/F
(SOURCE: TLMC 05-30-20)
Mandatory ≈02-Mar-2016TCF-2014-01 Paragraph C2, C3
Inboard
Flap Hinge Box – Non-Conforming Forward Lugs Edge Distance, Special Check Inboard
Mos
Hrs
22 Ldg≈6,348250Ldg
57 A/FEff: 17-Jan-2014
Mandatory ≈27-Aug-2016TCF-2014-01 Paragraph C2, C3
Outboard
Flap Hinge Box – Non-Conforming Forward Lugs Edge Distance, Special Check Outboard
Mos
Hrs
196 Ldg≈6,522250Ldg
57 A/FEff: 26-Sep-2013
IsModSumT (A/R)IS600-57-0001 REV A Kit-Flap Box Hinge Bushings Instl – Improved Corrosion Protection
Mos
Hrs
Ldg
57 A/F
▼ 71 - POWER PLANT
RE (O/C)Engine Aft Mount
20-Sep-1983Mos
0Hrs0
0Ldg0
Left71 A/FNew601-37002-1
UNKNOWN
RE (O/C)Engine Aft Mount
20-Sep-1983Mos
0Hrs0
0Ldg0
Right71 A/FNew601-37002-1
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM249/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Engine Forward Mount
20-Sep-1983Mos
0Hrs0
0Ldg0
Left71 A/FNew601-37001-1
UNKNOWN
RE (O/C)Engine Forward Mount
20-Sep-1983Mos
0Hrs0
0Ldg0
Right71 A/FNew601-37001-2
UNKNOWN
MandatoryT2013-05-06 Modification of the left-hand engine thrust control mechanism
18 Days[24-Apr-2016]36Mos
5,725.9 Hrs[17,767.1]6,000Hrs
Ldg
71 A/FEff: 24-Apr-2013
Compliance Share DoubleDUE:1. T A/R | 2. RE -Modification – Core Cowl Doors – Installation of a Hold Open...601-0609A/F71
RecommendedRE (-)601-0014 Special Check/Modification - Forward Engine Mount - Bushings
Mos
Hrs
Ldg
71 A/FEff: 08-Feb-1984
RecommendedT (A/R)601-0153 Modification - Forward Engine Mount - Retention Bolts
Mos
Hrs
Ldg
71 A/FEff: 08-Oct-1985
RecommendedRE (-)601-0181 Modification - Flight Control Systems and Engine Sensors - E.M.I. Protection
Mos
Hrs
Ldg
71 A/F
RecommendedRE (-)601-0181 Rev 1 Modification - Flight Control Systems and Engine Sensors - E.M.I. Protection
Mos
Hrs
Ldg
71 A/FEff: 23-Apr-1986
RecommendedRE (-)601-0474 Special Check/Modification - Forward Engine Mount - Replacement of Nuts and Damaged Bolts
18-Nov-1996Mos
5,001Hrs
2,052Ldg
71 A/FEff: 14-Jun-1996 Complied With
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Forward Engine Mount - Replacem...601-0474 Part AA/F71
Nextdue Share EarliestDUE:1. T A/R | 2. RE -Special Check/Modification - Forward Engine Mount - Replacem...601-0474 Part BA/F71
RecommendedT (A/R)601-0474 Part A Special Check/Modification - Forward Engine Mount - Replacement of Nuts and Damaged Bolts - Left Engine
Mos
Hrs
Ldg
71 A/FEff: 14-Jun-1996
RecommendedT (A/R)601-0474 Part B Special Check/Modification - Forward Engine Mount - Replacement of Nuts and Damaged Bolts - Right Engine
Mos
Hrs
Ldg
71 A/FEff: 14-Jun-1996
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM250/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedT (A/R)601-0522 Special Check/Rework - Engine Mounts - Serialization of Engine Mounts and Yoke Fitting Assembly
Mos
Hrs
Ldg
71 A/FEff: 30-Sep-2003
RecommendedT (A/R)601-0599 Modification – Cowlings – Addition of Warning Placards to Correctly Install Fasteners
Mos
Hrs
Ldg
71 A/FEff: 18-Aug-2008
RecommendedT (A/R)601-0609 Modification – Core Cowl Doors – Installation of a Hold Open Rod Bracket to Prevent Malfunction of the L/H Engine Fuel Control Unit
Mos
Hrs
Ldg
71 A/FEff: 31-Aug-2011
OptionalT (A/R)601-1003 Modification - Core Cowl Assemblies - Interchangeability
Mos
Hrs
Ldg
71 A/FEff: 01-May-1985
RecommendedRE (-)601-1004 Modification - Upper and Lower Core Cowl Doors - Strut Stay Brace
02-May-1988Mos
1,995Hrs
756Ldg
71 A/FEff: 09-Jan-1987 Complied With
RecommendedRE (-)601-1027 Modification - Service Pylon - IDG Hose Restraints
02-May-1988Mos
1,995Hrs
756Ldg
71 A/FEff: 06-Jun-1984 Complied With
RecommendedT (A/R)601-1028 Special Check/Modification - Left Lower Core Cowl Stay Brace - Clearance Between Stow Bracket and Power Lever
Mos
Hrs
Ldg
71 A/FEff: 10-Apr-1984
RecommendedT (A/R)601-1031 Special Check/Modification - Nose Cowl Fixed Side Panel - Forward Engine Mount Aperture
Mos
Hrs
Ldg
71 A/FEff: 25-Feb-1987
RecommendedRE (-)601-1032 Modification - Nose Cowl Assembly - Drain Hole Relocation
18-Sep-1985Mos
607Hrs
261Ldg
71 A/FEff: 05-Dec-1984 Complied With
RecommendedRE (-)601-1035 Modification - Wiring Harness - Clamping
02-May-1988Mos
1,995Hrs
756Ldg
71 A/FEff: 22-Nov-1985 Complied With
RecommendedRE (-)601-1036 Modification - Drain and Vent System - Combustor Drain Line Support
18-Sep-1985Mos
607Hrs
261Ldg
71 A/FEff: 26-Jul-1984 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM251/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-1051 Special Check/Modification - Fixed Nose Cowls - Electrical Connectors
02-May-1988Mos
1,995Hrs
756Ldg
71 A/FEff: 26-Nov-1985 Complied With
RecommendedRE (-)601-1052 Modification - Lower Core Cowl Door - Alignment
Mos
Hrs
Ldg
71 A/F
RecommendedRE (-)601-1052 Rev 1 Modification - Lower Core Cowl Door - Alignment
02-May-1988Mos
1,995Hrs
756Ldg
71 A/FEff: 20-Oct-1987 Complied With
RecommendedRE (-)601-1053 Special Check and Modification - Upper Access Cowl - Clearances
Mos
Hrs
Ldg
71 A/F
RecommendedRE (-)601-1053 Rev 1 Special Check and Modification - Upper Access Cowl - Clearances
Mos
Hrs
Ldg
71 A/F
RecommendedRE (-)601-1053 Rev 2 Special Check and Modification - Upper Access Cowl - Clearances
25-Oct-1988Mos
Hrs
Ldg
71 A/FEff: 06-Aug-1990 Complied With
RecommendedRE (-)601-1055 Special Check/Rework - Core Cowl Doors - Undersize Exhaust Port
02-May-1988Mos
1,995Hrs
756Ldg
71 A/FEff: 26-Feb-1987 Complied With
RecommendedRE (-)601-1062 Modification - Oil Scavenge Tube - Reorientation of Clamp
02-May-1988Mos
1,995Hrs
756Ldg
71 A/FEff: 05-Nov-1987 Complied With
OptionalRE (-)601-1072 Modification - Exhaust Nozzle Fairing - Prevention of Heat Shield Delamination
27-Feb-1999Mos
5,912Hrs
2,584Ldg
71 A/FEff: 31-Oct-1990 Complied With
RecommendedRE (-)601-1078 Special Check/Modification - Upper Access Cowl - Clearance with Ballscrew Actuators
21-Feb-1991Mos
3,142Hrs
1,250Ldg
71 A/FEff: 30-Jul-1990 Complied With
RecommendedRE (-)601-1083 Modification - Core Cowl Doors - Improved Fire Resistance and Containment
26-Jan-1996Mos
4,785Hrs
1,932Ldg
71 A/FEff: 15-Aug-1994 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM252/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedT (A/R)601-1090 Modification - Core Cowl Doors - Larger Vent Holes in Aft Frame
Mos
Hrs
Ldg
71 A/FEff: 16-Jan-1995
RecommendedT (A/R)601-1091 Modification - Upper Access Cowl Install Shorter Screws
Mos
Hrs
Ldg
71 A/FEff: 31-Jan-1995
AWL ≈23-Feb-2016RE71-10-00-101 * (Left) Nose Cowl Actuator Support Fitting - Forward Attachment Lugs - NDT Check
08-Aug-2005Mos
18.6 Hrs12,059.81,20010,859.8Hrs
Ldg
71 A/F
Ref.:PSP 612 Part 6 ET-71-10-01 (SOURCE: TLMC 05-10-30)
AWL ≈23-Feb-2016RE71-10-00-101 * (Right) Nose Cowl Actuator Support Fitting - Forward Attachment Lugs - NDT Check
08-Aug-2005Mos
18.6 Hrs12,059.81,20010,859.8Hrs
Ldg
71 A/F
Ref.:PSP 612 Part 6 ET-71-10-01 (SOURCE: TLMC 05-10-30)
AWL ≈09-Oct-2019T71-10-00-102 * Forward Nacelle Structure at the Engine Nacelle Joint - NDT Check
Mos
1,758.8 Hrs13,80013,800Hrs
Ldg
71 A/F
Ref.:PSP 612 Part 6 ET-71-10-02 (SOURCE: TLMC 05-10-30)
MRB ≈18-Sep-2016RE71-10-11-209 Nose Cowl Assembly Visual Check
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
71 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE71-10-16-201 Translating Cowl Doors Visual Check, paying particular attention to the trailing edge upper and lower doors
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
71 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE71-12-01-202 Core Cowl Doors Check Core Cowl
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
71 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈09-Mar-2019RE71-13-01-206 Core Cowl Fixed Side Panel Visual Check of the pylon installation and casting including oil cooler installation
30-Dec-2004Mos
1,478.4 Hrs (+40)13,519.6-/+403,00010,519.6Hrs
Ldg
71 A/F
(SOURCE: TLMC 05-20-15)
AWL ≈09-Apr-2022T71-20-00-103 * Aft Engine Mount - Thrust Fitting - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
71 A/F
Ref.:PSP 612 Part 6 ET-71-20-01 (SOURCE: TLMC 05-10-30)
AWL ≈29-Mar-2042RE71-20-00-104 * Engine Mount Yoke - Lower Lug - NDT Check
05-Aug-2003Mos
12,544.4 Hrs24,585.615,0009,585.6Hrs
Ldg
71 A/F
Ref.:PSP 612 Part 6 ET-71-20-02 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM253/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈09-Apr-2022T71-20-00-105 * Forward Engine Mount Upper Link - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
71 A/F
Ref.:PSP 612 Part 4 UT-71-20-01 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T71-20-00-106 * Forward Engine Mount Upper Bolts - NDT Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
71 A/F
Ref.:PSP 612 Part 4 UT-71-20-02, Ref.:PSP 612 Part 6 ET-71-20-03, Ref.:PSP 612 Part 8 PT-71-20-01 (SOURCE: TLMC 05-10-30)
AlertT (A/R)A601-1010 Special Check/Replacement - Throttle Control - Gearbox
Mos
Hrs
Ldg
71 A/FEff: 24-Aug-1983
CPCPREC71-00-801 Forward Engine Mount - CPCP Check including the following items: (without removal of engine) (1) Yoke assembly / (2) Link assembly / (3) Attachment bolts
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
71 A/F
(SOURCE: TLMC 05-30-20)
CPCPREC71-00-802 Aft Engine Mount - CPCP Check including the following items: (without removal of engine) (1) Thrust fitting
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
71 A/F
(SOURCE: TLMC 05-30-20)
CPCPREC71-00-803 Forward Nacelle and Nose Cowl Actuator Support Fitting - CPCP Check (without removal of engine)
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
71 A/F
(SOURCE: TLMC 05-30-20)
RE (O/C)Engine - No.1 Powerplant
20-Sep-1983Mos
0Hrs
0Ldg
71 A/FUnknownUnknown
RE (O/C)Engine - No.2 Powerplant
20-Sep-1983Mos
0Hrs
0Ldg
71 A/FUnknownUnknown
▼ 72 - ENGINE
RE (O/C)Accessory Gearbox
27-Jun-2005Mos
10,839Hrs
5,949Enc
72 ENG26014T81G24HCP00906
RE (O/C)Accessory Gearbox
31-May-2005Mos
10,956Hrs
5,990Enc
72 ENG16014T81G24HPC00814
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM254/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Balance Piston Stationary Air Seal
20-Sep-1983Mos
0Hrs
0Enc
72 ENG1UnknownUnknown
RE (O/C)Balance Piston Stationary Air Seal
20-Sep-1983Mos
0Hrs
0Enc
72 ENG2UnknownUnknown
RE (O/C)Ball Bearing
20-Sep-1983Mos
0Hrs
0Enc
No.172 ENG1UnknownUnknown
RE (O/C)Ball Bearing
20-Sep-1983Mos
0Hrs
0Enc
No.172 ENG2UnknownUnknown
RE (O/C)Ball Bearing
20-Sep-1983Mos
0Hrs
0Enc
No.272 ENG1UnknownUnknown
RE (O/C)Ball Bearing
20-Sep-1983Mos
0Hrs
0Enc
No.272 ENG2UnknownUnknown
RE (O/C)Ball Bearing
20-Sep-1983Mos
0Hrs
0Enc
No.372 ENG1UnknownUnknown
RE (O/C)Ball Bearing
20-Sep-1983Mos
0Hrs
0Enc
No.372 ENG2UnknownUnknown
RE (O/C)Ball Duplex Bearing
20-Sep-1983Mos
0Hrs
0Enc
72 ENG1UnknownUnknown
RE (O/C)Ball Duplex Bearing
20-Sep-1983Mos
0Hrs
0Enc
72 ENG2UnknownUnknown
RE (O/C)Combustion Frame
20-Sep-1983Mos
0Hrs
0Enc
72 ENG1UnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM255/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Combustion Frame
20-Sep-1983Mos
0Hrs
0Enc
72 ENG2UnknownUnknown
≈01-Jul-2069RECompressor Rotor Disk (Stage 9)
27-Jun-2005Mos
10,839Hrs0
19,221 Enc25,94920,0005,949Enc0
72 ENG2New6087T01P03
NCE337AC
Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit) (NOTE: Subject to inspection by Airworthiness Directive 99-22-10 and AMOC dated March 24,
2004.)
≈01-Jul-2069RECompressor Rotor Disk (Stage 9)
31-May-2005Mos
10,956Hrs0
19,221 Enc25,99020,0005,990Enc0
72 ENG1New6087T01P03
NCE671AC
Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit) (NOTE: Subject to inspection by Airworthiness Directive 99-22-10 and AMOC dated March 24,
2004.)
≈21-Jul-2046RECompressor Rotor Forward Shaft
27-Jun-2005Mos
10,839Hrs0
10,961 Enc17,68911,7405,949Enc0
72 ENG2New5037T01P03
GATS9134
Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit)
≈01-Dec-2029RECompressor Rotor Forward Shaft
31-May-2005Mos
10,956Hrs10,956
4,971 Enc11,74011,7405,990Enc5,990
72 ENG1Overhauled5037T01P03
GATR1090
Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit)
≈11-Aug-2030RECompressor Rotor Forward Spool (3 - 8 Stage)
27-Jun-2005Mos
10,839Hrs0
5,221 Enc11,9496,0005,949Enc0
72 ENG2New6078T56P05
GATHF97K
Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit) (NOTE: For forward HPC spools, part number (P/N) 6078T56P01 (Subject to inspection by
Airworthiness Directive 99-22-10), , which have accumulated fewer than 6,000 cycles since new (CSN) on the effective date of this AD, remove
prior to accumulating 6,000 CSN.)
≈11-Aug-2030RECompressor Rotor Forward Spool (3 - 8 Stage)
31-May-2005Mos
10,956Hrs0
5,221 Enc11,9906,0005,990Enc0
72 ENG1New6078T56P05
GWN07DE5
Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit) (NOTE: For forward HPC spools, part number (P/N) 6078T56P01 (Subject to inspection by
Airworthiness Directive 99-22-10), , which have accumulated fewer than 6,000 cycles since new (CSN) on the effective date of this AD, remove
prior to accumulating 6,000 CSN.)
≈01-Nov-2077RECompressor Rotor Rear Shaft
27-Jun-2005Mos
10,839Hrs0
22,221 Enc28,94923,0005,949Enc0
72 ENG2New6087T03P03
GWN0943K
Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit)
≈01-Nov-2077RECompressor Rotor Rear Shaft
31-May-2005Mos
10,956Hrs0
22,221 Enc28,99023,0005,990Enc0
72 ENG1New6087T03P03
GEE1FRFN
Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM256/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
≈09-Dec-2037RECompressor Rotor Rear Shaft CDP Seal
27-Jun-2005Mos
10,839Hrs10,839
7,859 Enc14,58714,4005,949Enc5,762
72 ENG2Overhauled4019T38P01
APV15195
Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit)
≈21-Apr-2037RECompressor Rotor Rear Shaft CDP Seal
31-May-2005Mos
10,956Hrs10,956
7,631 Enc14,40014,4005,990Enc5,990
72 ENG1Overhauled4019T38P01
APV12114
Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit)
≈02-Mar-2061RECompressor Rotor Rear Spool (Stage 10 - 14)
27-Jun-2005Mos
10,839Hrs0
16,221 Enc22,94917,0005,949Enc0
72 ENG2New5087T46P02
GATHFDL2
Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit) (NOTE: Subject to inspection by Airworthiness Directive 99-22-10 and AMOC dated March 24,
2004.)
≈02-Mar-2061RECompressor Rotor Rear Spool (Stage 10 - 14)
31-May-2005Mos
10,956Hrs0
16,221 Enc22,99017,0005,990Enc0
72 ENG1New5087T46P02
GATHFE9G
Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit) (NOTE: Subject to inspection by Airworthiness Directive 99-22-10 and AMOC dated March 24,
2004.)
RE (O/C)Engine Combustion Liner
27-Jun-2005Mos
10,839Hrs3,043
5,949Enc1,792
72 ENG2Overhauled5021T51G02
GGMUW068
RE (O/C)Engine Combustion Liner
31-May-2005Mos
10,956Hrs
5,990Enc
72 ENG15021T51G02GGMVC780
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.172 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.172 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1072 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1072 ENG2UnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM257/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1172 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1172 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1272 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1272 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1372 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1372 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1472 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1472 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1572 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1572 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1672 ENG1UnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM258/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1672 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1772 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1772 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1872 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1872 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1972 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.1972 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.272 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.272 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2072 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2072 ENG2UnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM259/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2172 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2172 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2272 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2272 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2372 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2372 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2472 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2472 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2572 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2572 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2672 ENG1UnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM260/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2672 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2772 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2772 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2872 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.2872 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.372 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.372 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.472 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.472 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.572 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.572 ENG2UnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM261/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.672 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.672 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.772 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.772 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.872 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.872 ENG2UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.972 ENG1UnknownUnknown
RE (O/C)Fan Blade
20-Sep-1983Mos
0Hrs
0Enc
No.972 ENG2UnknownUnknown
RE (O/C)Fan case Assy
20-Sep-1983Mos
0Hrs
0Enc
Aft72 ENG1UnknownUnknown
RE (O/C)Fan case Assy
20-Sep-1983Mos
0Hrs
0Enc
Aft72 ENG2UnknownUnknown
RE (O/C)Fan case Assy
20-Sep-1983Mos
0Hrs
0Enc
Fwd72 ENG1UnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM262/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Fan case Assy
20-Sep-1983Mos
0Hrs
0Enc
Fwd72 ENG2UnknownUnknown
≈16-Jun-2082REFan Disk
05-Jul-2009Mos
11,437.8Hrs0
23,886 Enc30,61424,3006,314Enc0
72 ENG2New6078T57G06
GEE1GPLT
Ref:EMM 5-11-01 (SOURCE: EMM - Life Limit)
≈11-Dec-2038REFan Disk
31-May-2005Mos
10,956Hrs0
8,221 Enc14,9909,0005,990Enc0
72 ENG1New3078T00G01
GEE1FR6L
Ref:EMM 5-11-01 (SOURCE: EMM - Life Limit)
≈21-Dec-2038REFan Drive Shaft
31-May-2005Mos
10,956Hrs10,956
8,231 Enc15,00015,0005,990Enc5,990
72 ENG1Overhauled6036T78P02
REA0976H
Ref:EMM 5-11-01 (SOURCE: EMM - Life Limit)
≈02-Feb-2039REFan Drive Shaft
20-Sep-1983Mos
0Hrs0
8,272 Enc15,00015,0000Enc0
72 ENG2New6036T78P02
UNKNOWN
Ref:EMM 5-11-01 (SOURCE: EMM - Life Limit)
≈13-Feb-2109REFan Forward Shaft
27-Jul-2005Mos
10,839Hrs6,418
33,483 Enc40,21138,2805,949Enc4,018
72 ENG2Overhauled6017T63P05
GATWF998
Ref:EMM 5-11-01 (SOURCE: EMM - Life Limit)
≈21-Aug-2103REFan Forward Shaft
31-May-2005Mos
10,956Hrs10,956
31,511 Enc38,28038,2805,990Enc5,990
72 ENG1Overhauled6017T63P05
GATP8695
Ref:EMM 5-11-01 (SOURCE: EMM - Life Limit)
RE (O/C)Fan Rotor Assy
20-Sep-1983Mos
0Hrs
0Enc
72 ENG1UnknownUnknown
RE (O/C)Fan Rotor Assy
20-Sep-1983Mos
0Hrs
0Enc
72 ENG2UnknownUnknown
RE (O/C)Fan Speed Sensor
20-Sep-1983Mos
0Hrs
0Enc
72 ENG1UnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM263/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Fan Speed Sensor
20-Sep-1983Mos
0Hrs
0Enc
72 ENG2UnknownUnknown
RE (O/C)HPT Assembly Stator
20-Sep-1983Mos
0Hrs
0Enc
72 ENG1UnknownUnknown
RE (O/C)HPT Assembly Stator
20-Sep-1983Mos
0Hrs
0Enc
72 ENG2UnknownUnknown
RE (O/C)HPT Rotor Assy
20-Sep-1983Mos
0Hrs
0Enc
72 ENG1UnknownUnknown
RE (O/C)HPT Rotor Assy
20-Sep-1983Mos
0Hrs
0Enc
72 ENG2UnknownUnknown
≈11-Aug-2030REHPT Rotor Balance Piston Air Seal
27-Jun-2005Mos
10,839Hrs0
5,221 Enc11,9496,0005,949Enc0
72 ENG2New6078T90P01
NCE5484AF
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
≈11-Aug-2030REHPT Rotor Balance Piston Air Seal
31-May-2005Mos
10,956Hrs0
5,221 Enc11,9906,0005,990Enc0
72 ENG1New6078T90P01
NCE0564Y
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
≈11-Aug-2030REHPT Rotor Inner Torque Coupling
27-Jun-2005Mos
10,839Hrs0
5,221 Enc11,9496,0005,949Enc0
72 ENG2New5079T02P01
GATHF3HJ
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
≈11-Aug-2030REHPT Rotor Inner Torque Coupling
31-May-2005Mos
10,956Hrs0
5,221 Enc11,9906,0005,990Enc0
72 ENG1New5079T02P01
GATP8672
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
≈11-Aug-2030REHPT Rotor Outer Torque Coupling
27-Jun-2005Mos
10,839Hrs0
5,221 Enc11,9496,0005,949Enc0
72 ENG2New5041T67P02
GATHEF3E
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM264/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
≈11-Aug-2030REHPT Rotor Outer Torque Coupling
31-May-2005Mos
10,956Hrs0
5,221 Enc11,9906,0005,990Enc0
72 ENG1New5041T67P02
GATHEF39
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
≈11-Aug-2030REHPT Rotor Shaft
27-Jun-2005Mos
10,839Hrs0
5,221 Enc11,9496,0005,949Enc0
72 ENG2New6017T00P05
GEE1FRNE
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
≈11-Aug-2030REHPT Rotor Shaft
31-May-2005Mos
10,956Hrs0
5,221 Enc11,9906,0005,990Enc0
72 ENG1New6017T00P05
GEE1FRNG
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
≈11-Aug-2030REHPT Rotor Stage 1 Cooling Aft Plate
27-Jun-2005Mos
10,839Hrs0
5,221 Enc11,9496,0005,949Enc0
72 ENG2New5041T70P03
GATCWHJ2
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
≈11-Aug-2030REHPT Rotor Stage 1 Cooling Aft Plate
31-May-2005Mos
10,956Hrs0
5,221 Enc11,9906,0005,990Enc0
72 ENG1New5041T70P03
NCE4602Y
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
≈11-Aug-2030REHPT Rotor Stage 1 Front Cooling Plate
27-Jun-2005Mos
Hrs0
5,221 Enc11,9496,0005,949Enc0
72 ENG2New4027T15P02
NCE155AA
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
≈11-Aug-2030REHPT Rotor Stage 1 Front Cooling Plate
31-May-2005Mos
Hrs0
5,221 Enc11,9906,0005,990Enc0
72 ENG1New4027T15P02
NCE150AA
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
≈11-Aug-2030REHPT Rotor Stage 1 Turbine Disk
27-Jun-2005Mos
10,839Hrs0
5,221 Enc11,9496,0005,949Enc0
72 ENG2New6031T89P02
GATHWA3W1
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
≈11-Aug-2030REHPT Rotor Stage 1 Turbine Disk
31-May-2005Mos
10,956Hrs0
5,221 Enc11,9906,0005,990Enc0
72 ENG1New6078T93P02
GATHD55D
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM265/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
≈04-Aug-2020REHPT Rotor Stage 2 Rear Cooling Plate
27-Jun-2005Mos
Hrs
1,614 Enc8,3426,0005,949Enc3,607
72 ENG2New5023T97P02
GATADJ07
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
≈11-Aug-2030REHPT Rotor Stage 2 Rear Cooling Plate
31-May-2005Mos
Hrs0
5,221 Enc11,9906,0005,990Enc0
72 ENG1New5023T97P02
NCE847AC
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
≈11-Aug-2030REHPT Rotor Stage 2 Turbine Disk
27-Jun-2005Mos
10,839Hrs0
5,221 Enc11,9496,0005,949Enc0
72 ENG2New6078T94P02
GATHE4TT
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
≈11-Aug-2030REHPT Rotor Stage 2 Turbine Disk
31-May-2005Mos
10,956Hrs0
5,221 Enc11,9906,0005,990Enc0
72 ENG1New6078T94P02
GATHE4TP
Ref:EMM 5-11-03 (SOURCE: EMM - Life Limit)
≈22-Feb-2021REHPT Stage 2 Nozzle Ring
05-Jun-2009Mos
2,417.4 Hrs14,554.83,00011,554.8Hrs0
6,355Enc
72 ENG14019T91P03UNKNOWN
≈24-Nov-2019REHPT Stage 2 Nozzle Ring
28-Jul-2005Mos
1,818.6 Hrs13,8393,00010,839Hrs0
5,949Enc
72 ENG2UNKNOWNUNKNOWN
≈23-May-2027REHPT Stage 2 Studs
05-Jun-2009Mos
5,417.4 Hrs17,554.86,00011,554.8Hrs0
6,355Enc
72 ENG1UNKNOWNUNKNOWN
≈23-Feb-2026REHPT Stage 2 Studs
27-Jun-2005Mos
4,818.6 Hrs16,8396,00010,839Hrs0
5,949Enc
72 ENG2UNKNOWNUNKNOWN
RE (O/C)LPT Rotor Assy
20-Sep-1983Mos
0Hrs
0Enc
72 ENG1UnknownUnknown
RE (O/C)LPT Rotor Assy
20-Sep-1983Mos
0Hrs
0Enc
72 ENG2UnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM266/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
≈02-Feb-2039RELPT Rotor Drive Cone
27-Jun-2005Mos
10,839Hrs10,839
8,272 Enc15,00015,0005,949Enc5,949
72 ENG2Overhauled4922T18P01
GATP7954
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
≈21-Dec-2038RELPT Rotor Drive Cone
31-May-2005Mos
10,956Hrs10,956
8,231 Enc15,00015,0005,990Enc5,990
72 ENG1Overhauled4922T18P01
GATP7964
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
≈22-Mar-2093RELPT Rotor Rear Shaft
27-Jun-2005Mos
10,839Hrs10,739
27,762 Enc34,49034,4905,949Enc5,949
72 ENG2Overhauled4922T19P01
GAT51376
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
≈11-Feb-2093RELPT Rotor Rear Shaft
31-May-2005Mos
10,956Hrs10,956
27,721 Enc34,49034,4905,990Enc5,990
72 ENG1Overhauled4922T19P01
GATR19P01
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
≈11-Aug-2055RELPT Rotor Stage 3 Disk
27-Jun-2005Mos
10,839Hrs0
14,221 Enc20,94915,0005,949Enc0
72 ENG2New6078T91P02
GATHFM4C
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
≈11-Aug-2055RELPT Rotor Stage 3 Disk
31-May-2005Mos
10,956Hrs0
14,221 Enc20,99015,0005,990Enc0
72 ENG1New6078T91P02
GATHF0E3
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
≈02-Mar-2061RELPT Rotor Stage 4 Disk
27-Jun-2005Mos
10,839Hrs0
16,221 Enc22,94917,0005,949Enc0
72 ENG2New6078T02P03
GATHE2TK
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
≈02-Mar-2061RELPT Rotor Stage 4 Disk
31-May-2005Mos
10,956Hrs0
16,221 Enc22,99017,0005,990Enc0
72 ENG1New6078T02P03
GATHE57H
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
≈02-Feb-2039RELPT Rotor Stage 5 Disk
27-Jun-2005Mos
10,839Hrs10,839
8,272 Enc15,00015,0005,949Enc5,949
72 ENG2Overhauled6078T92P02
GATHF6KF
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM267/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
≈11-Aug-2055RELPT Rotor Stage 5 Disk
31-May-2005Mos
10,956Hrs0
14,221 Enc20,99015,0005,990Enc0
72 ENG1New6078T92P02
GATHELWF
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
≈22-Jun-2019RELPT Rotor Stage 6 Disk
27-Jun-2005Mos
10,839Hrs10,839
1,212 Enc7,9407,9405,949Enc5,949
72 ENG2Overhauled4922T17P01
GATT0117
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
≈11-May-2019RELPT Rotor Stage 6 Disk
31-May-2005Mos
10,956Hrs10,956
1,171 Enc7,9407,9405,990Enc5,990
72 ENG1Overhauled4922T17P01
GATP3216
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
≈02-Jan-2080RELPT Rotor Stage Turbine Seal (3 - 4)
27-Jun-2005Mos
10,839Hrs10,839
23,002 Enc29,73029,7305,949Enc5,949
72 ENG2Overhauled4922T20P01
ABIA0784
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
≈21-Nov-2079RELPT Rotor Stage Turbine Seal (3 - 4)
31-May-2005Mos
10,956Hrs10,956
22,961 Enc29,73029,7305,990Enc5,990
72 ENG1Overhauled4922T20P01
ABIA2176
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
≈02-Jan-2080RELPT Rotor Stage Turbine Seal (4 - 5)
27-Jun-2005Mos
10,839Hrs10,839
23,002 Enc29,73029,7305,949Enc5,949
72 ENG2Overhauled4922T21P01
HAAB0694
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
≈21-Dec-2088RELPT Rotor Stage Turbine Seal (4 - 5)
31-May-2005Mos
10,956Hrs10,956
26,231 Enc33,00033,0005,990Enc5,990
72 ENG1Overhauled4922T21P01
HAAB2843
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
≈02-Jan-2080RELPT Rotor Stage Turbine Seal (5 - 6)
27-Jun-2005Mos
10,839Hrs10,839
23,002 Enc29,73029,7305,949Enc5,949
72 ENG2Overhauled4922T22P01
ABIA0719
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
≈21-Nov-2079RELPT Rotor Stage Turbine Seal (5 - 6)
31-May-2005Mos
10,956Hrs10,956
22,961 Enc29,73029,7305,990Enc5,990
72 ENG1Overhauled4922T22P01
HAAB1278
Ref:EMM 5-11-04 (SOURCE: EMM - Life Limit)
RE (O/C)LPT Stator Assy
20-Sep-1983Mos
0Hrs
0Enc
72 ENG1UnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM268/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)LPT Stator Assy
20-Sep-1983Mos
0Hrs
0Enc
72 ENG2UnknownUnknown
RE (O/C)LPT Transition Turbine Outer Liner
20-Sep-1983Mos
0Hrs
0Enc
72 ENG1UnknownUnknown
RE (O/C)LPT Transition Turbine Outer Liner
20-Sep-1983Mos
0Hrs
0Enc
72 ENG2UnknownUnknown
RE (O/C)Power Take Off Assembly Drive
27-Jun-2005Mos
10,839Hrs10,839
5,949Enc5,949
72 ENG2Overhauled6037T72G19
HCP01212
RE (O/C)Power Take Off Assembly Drive
31-May-2005Mos
10,956Hrs
5,990Enc
72 ENG16037T72G19HPC01002
RE (O/C)Roller Bearing
20-Sep-1983Mos
0Hrs
0Enc
No.472 ENG1UnknownUnknown
RE (O/C)Roller Bearing
20-Sep-1983Mos
0Hrs
0Enc
No.472 ENG2UnknownUnknown
RE (O/C)Roller Bearing
20-Sep-1983Mos
0Hrs
0Enc
No.572 ENG1UnknownUnknown
RE (O/C)Roller Bearing
20-Sep-1983Mos
0Hrs
0Enc
No.572 ENG2UnknownUnknown
RE (O/C)Roller Bearing
20-Sep-1983Mos
0Hrs
0Enc
No.672 ENG1UnknownUnknown
RE (O/C)Roller Bearing
20-Sep-1983Mos
0Hrs
0Enc
No.672 ENG2UnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM269/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Roller Bearing
20-Sep-1983Mos
0Hrs
0Enc
No.772 ENG1UnknownUnknown
RE (O/C)Roller Bearing
20-Sep-1983Mos
0Hrs
0Enc
No.772 ENG2UnknownUnknown
≈11-Aug-2055REStage 1 Compressor Rotor Disk
27-Jun-2005Mos
10,839Hrs0
14,221 Enc20,94915,0005,949Enc0
72 ENG2New6087T00G02
GATFHEAW
Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit)
≈11-Aug-2055REStage 1 Compressor Rotor Disk
31-May-2005Mos
10,956Hrs0
14,221 Enc20,99015,0005,990Enc0
72 ENG1New6087T00G02
GATHF3G0
Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit)
RE (O/C)Stage 1 HPT Blades
27-Jun-2005Mos
10,839Hrs
5,949Enc
72 ENG26078T19P10UNKNOWN
RE (O/C)Stage 1 HPT Blades
31-May-2005Mos
10,956Hrs10,956
5,990Enc5,990
72 ENG1Overhauled6078T19P07
UNKNOWN
≈09-Aug-2039REStage 2 Compressor Rotor Disk
27-Jun-2005Mos
10,839Hrs
8,459 Enc15,18715,0005,949Enc5,762
72 ENG26036T91P01GATR6493
Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit)
≈21-Dec-2038REStage 2 Compressor Rotor Disk
31-May-2005Mos
10,956Hrs10,956
8,231 Enc15,00015,0005,990Enc5,990
72 ENG1Overhauled6036T91P01
GATM2467
Ref:EMM 5-11-02 (SOURCE: EMM - Life Limit)
EMM - Life Limit ≈11-Aug-2030REStage 2 Front Cooling Plate
27-Jun-2005Mos
Hrs0
5,221 Enc11,9496,0005,949Enc0
72 ENG2New5042T29P01
NCE027AA
EMM - Life Limit ≈11-Aug-2030REStage 2 Front Cooling Plate
31-May-2005Mos
Hrs0
5,221 Enc11,9906,0005,990Enc0
72 ENG1New5042T29P01
NCE026AA
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM270/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Stage 2 HPT Blade
20-Sep-1983Mos
0Hrs
0Enc
72 ENG1UnknownUnknown
RE (O/C)Stage 2 HPT Blade
20-Sep-1983Mos
0Hrs
0Enc
72 ENG2UnknownUnknown
RE (O/C)Thermocouple Assy
27-Jun-2005Mos
10,839Hrs10,839
5,949Enc5,949
Left72 ENG2Overhauled6040T41P01
GDB04982
RE (O/C)Thermocouple Assy
31-May-2005Mos
10,956Hrs10,956
5,990Enc5,990
Left72 ENG1Overhauled6040T41P01
GDB05018
RE (O/C)Thermocouple Assy
27-Jun-2005Mos
10,839Hrs
5,949Enc
Right72 ENG26030T40P01GDB07353
RE (O/C)Thermocouple Assy
31-May-2005Mos
10,956Hrs10,956
5,990Enc5,990
Right72 ENG1Overhauled6040T41P01
GDB05209
RE (O/C)Transition Turbine Case
20-Sep-1983Mos
0Hrs
0Enc
72 ENG1UnknownUnknown
RE (O/C)Transition Turbine Case
20-Sep-1983Mos
0Hrs
0Enc
72 ENG2UnknownUnknown
RE (O/C)Turbine High Pressure Inner Casing
20-Sep-1983Mos
0Hrs
0Enc
72 ENG1UnknownUnknown
RE (O/C)Turbine High Pressure Inner Casing
20-Sep-1983Mos
0Hrs
0Enc
72 ENG2UnknownUnknown
RE (O/C)Turbine High Pressure Outer Casing
20-Sep-1983Mos
0Hrs
0Enc
72 ENG1UnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM271/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Turbine High Pressure Outer Casing
20-Sep-1983Mos
0Hrs
0Enc
72 ENG2UnknownUnknown
RE (O/C)Turbine Low Pressure Casing
20-Sep-1983Mos
0Hrs
0Enc
72 ENG1UnknownUnknown
RE (O/C)Turbine Low Pressure Casing
20-Sep-1983Mos
0Hrs
0Enc
72 ENG2UnknownUnknown
MandatoryRE (-)2001-10-03 Rupture of Fan Disk (Superseded By FAA AD 2006-05-04)
31-May-2001Mos
Hrs
Enc
72 ENG1NEW PART INSTALLEDEff: 31-May-2001 Not
Applicable
MandatoryRE (-)2001-10-03 Rupture of Fan Disk (Superseded By FAA AD 2006-05-04)
31-May-2001Mos
Hrs
Enc
72 ENG2Eff: 31-May-2001 Complied With
MandatoryRE (-)2001-12-06 General Electric Company - Lubrication System for the Engine Bearings
Mos
Hrs
Enc
72 ENG1Eff: 20-Jul-2001
MandatoryRE (-)2001-12-06 General Electric Company - Lubrication System for the Engine Bearings
Mos
Hrs
Enc
72 ENG2Eff: 20-Jul-2001
MandatoryRE (-)2001-12-06 Paragraph (a) General Electric Company - Lubrication System for the Engine Bearings - Magnetic Chip Detector Indicator check
22-Mar-2013Mos
11,734.5Hrs
6,520Enc
72 ENG2Eff: 20-Jul-2001 Complied With
MandatoryRE (-)2001-12-06 Paragraph (a) General Electric Company - Lubrication System for the Engine Bearings - Magnetic Chip Detector Indicator check
20-Jul-2001Mos
Hrs
Enc
72 ENG1FOUND P/C/WEff: 20-Jul-2001 Complied
With
MandatoryRE (-)2001-12-06 Paragraph (d) General Electric Company - Lubrication System for the Engine Bearings - Replacement of Air Seal
08-Mar-2002Mos
Hrs
Enc
72 ENG2Eff: 20-Jul-2001 Complied With
MandatoryRE (-)2001-12-06 Paragraph (d) General Electric Company - Lubrication System for the Engine Bearings - Replacement of Air Seal
20-Jul-2001Mos
Hrs
Enc
72 ENG1FOUND P/C/WEff: 20-Jul-2001 Complied
With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM272/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryRE (-)2004-26-02 Certain high pressure compressor (HPC)
11-Jul-2008Mos
11,411.2Hrs
6,293Enc
72 ENG2Eff: 26-Jan-2005 Not Applicable
MandatoryRE (-)2004-26-02 Certain high pressure compressor (HPC)
26-Jan-2005Mos
Hrs
Enc
72 ENG1Eff: 26-Jan-2005 Not Applicable
Mandatory ≈05-Jan-2024RE2006-04-12 General Electric Company - Stage 5 low pressure turbine (LPT) disks
26-Dec-2012Mos
11,775.4Hrs
2,845 Enc9,6143,1006,514Enc
72 ENG1
Nextdue Share EarliestDUE:1. RE -General Electric Company - Stage 5 low pressure turbine (LPT...2006-04-12 Paragraph (f)(2)(h)(1)ENG172
Nextdue Share EarliestDUE:1. RE -General Electric Company - Stage 5 low pressure turbine (LPT...2006-04-12 Paragraph (m)ENG172
Nextdue Share LatestDUE:1. T 2469 Days | 2. RE -General Electric Company - Stage 5 low pressure turbine (LPT...2006-04-12 Paragraph (n)ENG172
Mandatory ≈05-Jan-2024RE2006-04-12 General Electric Company - Stage 5 low pressure turbine (LPT) disks
26-Dec-2012Mos
11,658.4Hrs
2,845 Enc9,5733,1006,473Enc
72 ENG2
Nextdue Share EarliestDUE:1. RE -General Electric Company - Stage 5 low pressure turbine (LPT...2006-04-12 Paragraph (f)(2)(h)(1)ENG272
Nextdue Share EarliestDUE:1. RE -General Electric Company - Stage 5 low pressure turbine (LPT...2006-04-12 Paragraph (m)ENG272
Nextdue Share LatestDUE:1. T 2469 Days | 2. RE -General Electric Company - Stage 5 low pressure turbine (LPT...2006-04-12 Paragraph (n)ENG272
MandatoryRE (-)2006-04-12 Paragraph (f)(2)(h)
(1)
General Electric Company - Stage 5 low pressure turbine (LPT) disks - For engines installed in Bombardier Canadair BJ airplanes, perform an initial visual inspection
and ECI of stage 5 LPT disks and stage 6 LPT disks
Mos
Hrs
Enc
72 ENG1Eff: 30-Mar-2006
Compliance Share DoubleDUE:1. RE -ENGINE - Low Pressure Turbine (LPT) Rotor (72-53-00) - Repl...72-A0148 R02ENG172
MandatoryRE (-)2006-04-12 Paragraph (f)(2)(h)
(1)
General Electric Company - Stage 5 low pressure turbine (LPT) disks - For engines installed in Bombardier Canadair BJ airplanes, perform an initial visual inspection
and ECI of stage 5 LPT disks and stage 6 LPT disks
Mos
Hrs
Enc
72 ENG2Eff: 30-Mar-2006
Compliance Share DoubleDUE:1. RE -ENGINE - Low Pressure Turbine (LPT) Rotor (72-53-00) - Repl...72-A0148 R02ENG272
MandatoryRE (-)2006-04-12 Paragraph (m) General Electric Company - Stage 5 low pressure turbine (LPT) disks - Optional Terminating Action
Mos
Hrs
Enc
72 ENG1Eff: 30-Mar-2006
MandatoryRE (-)2006-04-12 Paragraph (m) General Electric Company - Stage 5 low pressure turbine (LPT) disks - Optional Terminating Action
Mos
Hrs
Enc
72 ENG2Eff: 30-Mar-2006
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM273/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryRE (-)2006-04-12 Paragraph (n) General Electric Company - Stage 5 low pressure turbine (LPT) disks - Terminating Action
Days
Hrs
Enc
72 ENG1Eff: 30-Mar-2006
MandatoryRE (-)2006-04-12 Paragraph (n) General Electric Company - Stage 5 low pressure turbine (LPT) disks - Terminating Action
Days
Hrs
Enc
72 ENG2Eff: 30-Mar-2006
MandatoryRE (-)2006-05-04 Fan Disk
Mos
Hrs
Enc
72 ENG1Eff: 07-Apr-2006
(NOTE: SUPERSEDED BY FAA AD 2007-07-07)
MandatoryRE (-)2006-05-04 Fan Disk
Mos
Hrs
Enc
72 ENG2Eff: 07-Apr-2006
(NOTE: SUPERSEDED BY FAA AD 2007-07-07)
MandatoryRE (-)2007-07-07 Fan Disk Inspection
Mos
Hrs
Enc
72 ENG1Eff: 30-Mar-2007
(NOTE: SUPERSEDED BY FAA AD 2009-26-09)
MandatoryRE (-)2007-07-07 Fan Disk Inspection
Mos
Hrs
Enc
72 ENG2Eff: 30-Mar-2007
(NOTE: SUPERSEDED BY FAA AD 2009-26-09)
MandatoryRE (-)2007-07-07R1 Fan disk inspection
25-Jul-2008Mos
11,528.2Hrs
6,334Enc
72 ENG1Eff: 12-Sep-2007 Not Applicable
(NOTE: SUPERSEDED BY FAA AD 2009-26-09)
MandatoryRE (-)2007-07-07R1 Fan disk inspection
25-Jul-2008Mos
11,411.2Hrs
6,293Enc
72 ENG2Eff: 12-Sep-2007 Complied With
(NOTE: SUPERSEDED BY FAA AD 2009-26-09)
Mandatory ≈22-Feb-2021T (A/R)2009-07-12 General Electric Company - High-pressure (HP) - Remove the 4-step seals, P/Ns 4923T54G01, 6019T90G03, 6037T99G01, 6037T99G02, and 6037T99G03. Incorporate an
8-step seal, either by modifying the existing 4-step seal to an 8-step seal, or by replacing it with an 8-step seal.
Mos
2,417.4 Hrs[14,554.8]Hrs
Enc
72 ENG1Eff: 07-May-2009
Compliance Share DoubleDUE:1. RE -ENGINE - (72-42-00) - Rework of the Air Balance Piston Stati...72-0217 R00ENG172
Mandatory ≈24-Nov-2019T (A/R)2009-07-12 General Electric Company - High-pressure (HP) - Remove the 4-step seals, P/Ns 4923T54G01, 6019T90G03, 6037T99G01, 6037T99G02, and 6037T99G03. Incorporate an
8-step seal, either by modifying the existing 4-step seal to an 8-step seal, or by replacing it with an 8-step seal.
Mos
1,818.6 Hrs[13,839]Hrs
Enc
72 ENG2Eff: 07-May-2009
Compliance Share DoubleDUE:1. T A/R | 2. RE -ENGINE - (72-42-00) - Rework of the Air Balance Piston Stati...72-0217 R00ENG272
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM274/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryRE (-)2009-24-11 Fan blade and aft actuator head hoses (SUPERSEDED BY FAA AD 2010-01-04)
Mos
Hrs
Enc
72 ENG1Eff: 04-Jan-2010
(NOTE: SUPERSEDED BY FAA AD 2010-01-04)
Nextdue Share EarliestDUE:1. RE -Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34...2009-24-11 Paragraph (l)(1)(2)ENG172
Nextdue Share EarliestDUE:1. RE -Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34...2009-24-11 Paragraph (l)(3)(4)(6)ENG172
Nextdue Share EarliestDUE:1. RE -Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34...2009-24-11 Paragraph (l)(8)(9)(10)ENG172
MandatoryRE (-)2009-24-11 Fan blade and aft actuator head hoses (SUPERSEDED BY FAA AD 2010-01-04)
Mos
Hrs
Enc
72 ENG2Eff: 04-Jan-2010
(NOTE: SUPERSEDED BY FAA AD 2010-01-04)
Nextdue Share EarliestDUE:1. RE -Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34...2009-24-11 Paragraph (l)(1)(2)ENG272
Nextdue Share EarliestDUE:1. RE -Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34...2009-24-11 Paragraph (l)(3)(4)(6)ENG272
Nextdue Share EarliestDUE:1. RE -Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34...2009-24-11 Paragraph (l)(8)(9)(10)ENG272
MandatoryRE (-)2009-24-11 Paragraph (l)(1)(2) Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1- Remove fan blades from service.(SUPERSEDED BY FAA AD 2010-01-04)
Mos
Hrs
Enc
72 ENG1Eff: 04-Jan-2010
MandatoryRE (-)2009-24-11 Paragraph (l)(1)(2) Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1- Remove fan blades from service.(SUPERSEDED BY FAA AD 2010-01-04)
Mos
Hrs
Enc
72 ENG2Eff: 04-Jan-2010
MandatoryRE (-)2009-24-11 Paragraph (l)(3)(4)
(6)
Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1- Initial / Repetitive Eddy Current Inspection (ECI) of the fan blades.
(SUPERSEDED BY FAA AD 2010-01-04)
Mos
Hrs
Enc
72 ENG1Eff: 04-Jan-2010
MandatoryRE (-)2009-24-11 Paragraph (l)(3)(4)
(6)
Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1- Initial / Repetitive Eddy Current Inspection (ECI) of the fan blades.
(SUPERSEDED BY FAA AD 2010-01-04)
Mos
Hrs
Enc
72 ENG2Eff: 04-Jan-2010
MandatoryRE (-)2009-24-11 Paragraph (l)(8)(9)
(10)
Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1- Initial / Repetitive Inspection of the Fan Blade Abradable Rub Strip for
Wear.(SUPERSEDED BY FAA AD 2010-01-04)
Mos
Hrs
Enc
72 ENG1Eff: 04-Jan-2010
MandatoryRE (-)2009-24-11 Paragraph (l)(8)(9)
(10)
Fan blade and aft actuator head hoses CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1- Initial / Repetitive Inspection of the Fan Blade Abradable Rub Strip for
Wear.(SUPERSEDED BY FAA AD 2010-01-04)
Mos
Hrs
Enc
72 ENG2Eff: 04-Jan-2010
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM275/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryRE (-)2009-26-09 General Electric Company - Fan disks
Mos
Hrs
Enc
72 ENG1Eff: 11-Feb-2010
Nextdue Share EarliestDUE:1. T A/R | 2. RE -General Electric Company - Fan disks - Removing Certain Fan ...2009-26-09 Paragraph (f)(g)ENG172
MandatoryRE (-)2009-26-09 General Electric Company - Fan disks
Mos
Hrs
Enc
72 ENG2Eff: 11-Feb-2010
Nextdue Share EarliestDUE:1. T A/R | 2. RE -General Electric Company - Fan disks - Removing Certain Fan ...2009-26-09 Paragraph (f)(g)ENG272
MandatoryT (A/R)2009-26-09 Paragraph (f)(g) General Electric Company - Fan disks - Removing Certain Fan Disks From Service
Mos
Hrs
Enc
72 ENG1Eff: 11-Feb-2010
Not SetDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04ENG172
MandatoryT (A/R)2009-26-09 Paragraph (f)(g) General Electric Company - Fan disks - Removing Certain Fan Disks From Service
Mos
Hrs
Enc
72 ENG2Eff: 11-Feb-2010
Not SetDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04ENG272
Mandatory ≈18-Jul-2023RE2009-26-09 Paragraph (k) General Electric Company - Fan disks - For CF34-3A1, CF34-1A, CF34-3A, CF34-3A2 and CF34-3B, Inspections of Tier 1 Fan Disks
22-Mar-2012Mos
11,674.8Hrs
2,678 Enc9,4473,0006,447Enc
72 ENG1SB 72-A0212Eff: 11-Feb-2010 Complied
With
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04 (Tier 1)ENG172
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Eddy Cur...72-A0234 R00ENG172
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - On Wing Repetitive ...72-A0235 R00ENG172
Mandatory ≈18-Jul-2023RE2009-26-09 Paragraph (k) General Electric Company - Fan disks - For CF34-3A1, CF34-1A, CF34-3A, CF34-3A2 and CF34-3B, Inspections of Tier 1 Fan Disks
19-Mar-2012Mos
Hrs
2,678 Enc9,4063,0006,406Enc
72 ENG2Eff: 11-Feb-2010
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04 (Tier 1)ENG272
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Eddy Cur...72-A0234 R00ENG272
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - On Wing Repetitive ...72-A0235 R00ENG272
Mandatory ≈18-Jul-2023RE2009-26-09 Paragraph (l) General Electric Company - Fan disks - For CF34-3A1, CF34-1A, CF34-3A, CF34-3A2 and CF34-3B, Inspections of Tier 2 Fan Disks
22-Mar-2012Mos
11,674.8Hrs
2,678 Enc9,4473,0006,447Enc
72 ENG1SB 72-A0233Eff: 11-Feb-2010 Complied
With
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04 (Tier 2)ENG172
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Eddy Cur...72-A0234 R00ENG172
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - On Wing Repetitive ...72-A0235 R00ENG172
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM276/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Mandatory ≈18-Jul-2023RE2009-26-09 Paragraph (l) General Electric Company - Fan disks - For CF34-3A1, CF34-1A, CF34-3A, CF34-3A2 and CF34-3B, Inspections of Tier 2 Fan Disks
19-Mar-2012Mos
11,557.8Hrs
2,678 Enc9,4063,0006,406Enc
72 ENG2Eff: 11-Feb-2010
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04 (Tier 2)ENG272
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Eddy Cur...72-A0234 R00ENG272
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - On Wing Repetitive ...72-A0235 R00ENG272
MandatoryRE (-)2009-26-09 Paragraph (m) General Electric Company - Fan disks - For CF34-3A1, CF34-1A, CF34-3A, CF34-3A2 and CF34-3B, Inspections of Tier 3 Fan Disks
Mos
Hrs
Enc
72 ENG1Eff: 11-Feb-2010
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04 (Tier 3)ENG172
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Eddy Cur...72-A0234 R00ENG172
MandatoryRE (-)2009-26-09 Paragraph (m) General Electric Company - Fan disks - For CF34-3A1, CF34-1A, CF34-3A, CF34-3A2 and CF34-3B, Inspections of Tier 3 Fan Disks
Mos
Hrs
Enc
72 ENG2Eff: 11-Feb-2010
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04 (Tier 3)ENG272
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Eddy Cur...72-A0234 R00ENG272
MandatoryRE (-)2009-26-09 Paragraph (o) General Electric Company - Fan Disks - Mandatory Terminating Action
Mos
Hrs
Enc
72 ENG1Eff: 11-Feb-2010
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04ENG172
MandatoryRE (-)2009-26-09 Paragraph (o) General Electric Company - Fan Disks - Mandatory Terminating Action
Mos
Hrs
Enc
72 ENG2Eff: 11-Feb-2010
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04ENG272
MandatoryRE (-)2010-01-04 General Electric Company - Fan blade
Mos
Hrs
Enc
72 ENG1Eff: 30-Apr-2010
Nextdue Share EarliestDUE: 7,645 Enc1. T 1200 Enc | 2. RE -General Electric Company - Fan blade - For CF34-1A, CF34-3A,...2010-01-04 Paragraph (l)(1)(2)ENG172
Nextdue Share EarliestDUE: 6,795 Enc1. T 350 Enc | 2. RE 600 EncGeneral Electric Company - Fan blade - For CF34-1A, CF34-3A,...2010-01-04 Paragraph (l)(3)(4)(6)ENG172
Nextdue Share EarliestDUE: 12,215.2 Hrs, 6,826 Enc1. T 1220 Enc | 2. RE 100 Hrs, 75 Enc (later)General Electric Company - Fan blade - For CF34-1A, CF34-3A,...2010-01-04 Paragraph (l)(8)(9)(10)ENG172
MandatoryRE (-)2010-01-04 General Electric Company - Fan blade
Mos
Hrs
Enc
72 ENG2Eff: 30-Apr-2010
Nextdue Share EarliestDUE: 7,604 Enc1. T 1200 Enc | 2. RE -General Electric Company - Fan blade - For CF34-1A, CF34-3A,...2010-01-04 Paragraph (l)(1)(2)ENG272
Nextdue Share EarliestDUE: 6,754 Enc1. T 350 Enc | 2. RE 600 EncGeneral Electric Company - Fan blade - For CF34-1A, CF34-3A,...2010-01-04 Paragraph (l)(3)(4)(6)ENG272
Nextdue Share EarliestDUE: 12,098.2 Hrs, 6,785 Enc1. T 1220 Enc | 2. RE 100 Hrs, 75 Enc (later)General Electric Company - Fan blade - For CF34-1A, CF34-3A,...2010-01-04 Paragraph (l)(8)(9)(10)ENG272
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM277/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Mandatory ≈16-Jul-2018T2010-01-04 Paragraph (l)(1)(2) General Electric Company - Fan blade - For CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1 - Remove fan blades from service.
Mos
Hrs
876 Enc[7,645]1,200Enc
72 ENG1Eff: 25-Jan-2010
Mandatory ≈16-Jul-2018T2010-01-04 Paragraph (l)(1)(2) General Electric Company - Fan blade - For CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1 - Remove fan blades from service.
Mos
Hrs
876 Enc[7,604]1,200Enc
72 ENG2Eff: 25-Jan-2010
Mandatory ≈06-Mar-2016T2010-01-04 Paragraph (l)(3)(4)
(6)
General Electric Company - Fan blade - For CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1, Initial / Repetitive Eddy Current Inspection of the Fan Blades
Mos
Hrs
26 Enc[6,795]350Enc
72 ENG1Eff: 25-Jan-2010
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG172
Mandatory ≈06-Mar-2016T2010-01-04 Paragraph (l)(3)(4)
(6)
General Electric Company - Fan blade - For CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1, Initial / Repetitive Eddy Current Inspection of the Fan Blades
Mos
Hrs
26 Enc[6,754]350Enc
72 ENG2Eff: 25-Jan-2010
Compliance Share DoubleDUE: 6,914 Enc1. T 350 Enc | 2. RE 600 EncENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG272
Mandatory ≈08-Apr-2016RE2010-01-04 Paragraph (l)(8)(9)
(10)
General Electric Company - Fan blade - For CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1, Initial / Repetitive Visual Inspection of the Fan Blade Abradable Rub
Strip for Wear
03-Dec-2015Mos
77.8 Hrs12,215.210012,115.2Hrs
57 Enc6,826756,751Enc
72 ENG1SB 72-0250Complied With
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Stator (72-23-00) - Visual Inspection of Fan Ca...72-0231 R02ENG172
Mandatory ≈08-Apr-2016RE2010-01-04 Paragraph (l)(8)(9)
(10)
General Electric Company - Fan blade - For CF34-1A, CF34-3A, CF34-3A2, CF34-3B and CF34-3A1, Initial / Repetitive Visual Inspection of the Fan Blade Abradable Rub
Strip for Wear
03-Dec-2015Mos
77.8 Hrs12,098.210011,998.2Hrs
57 Enc6,785756,710Enc
72 ENG2SB 72-0250Complied With
Compliance Share DoubleDUE:1. RE -ENGINE - Fan Stator (72-23-00) - Visual Inspection of Fan Ca...72-0231 R02ENG272
MRB ≈25-Sep-2016RE72-00-00-201 Engine - General - Visual Check of Fan Stator for the following: (1) Flowpath Aluminum skin for dents and cracks / (2) Abradable Rub Strip for rubbing
10-Feb-2016Mos
300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs
6,728Enc
(PKG 300 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈25-Sep-2016RE72-00-00-201 Engine - General - Visual Check of Fan Stator for the following: (1) Flowpath Aluminum skin for dents and cracks / (2) Abradable Rub Strip for rubbing
10-Feb-2016Mos
300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs
6,769Enc
(PKG 300 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈25-Sep-2016RE72-00-00-203 Engine - General - Carry out a visual check of the following: (1) Engine Mounts / (2) Fan Rotor / (3) Fan Stator / (4) Compressor Case / (5) Front Frame, paying particular
attention around AGB Mount Pads / (6) Accessory Gearbox
10-Feb-2016Mos
300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs
6,769Enc
(PKG 300 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM278/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈25-Sep-2016RE72-00-00-203 Engine - General - Carry out a visual check of the following: (1) Engine Mounts / (2) Fan Rotor / (3) Fan Stator / (4) Compressor Case / (5) Front Frame, paying particular
attention around AGB Mount Pads / (6) Accessory Gearbox
10-Feb-2016Mos
300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs
6,728Enc
(PKG 300 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈25-Sep-2016RE72-00-00-206 Engine - General - Visual Check of engine external lines, ports, flanges, clamps, brackets, electrical connectors, engine surface and accessories
10-Feb-2016Mos
300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs
6,728Enc
(PKG 300 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈25-Sep-2016RE72-00-00-206 Engine - General - Visual Check of engine external lines, ports, flanges, clamps, brackets, electrical connectors, engine surface and accessories
10-Feb-2016Mos
300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs
6,769Enc
(PKG 300 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈25-Sep-2016RE72-00-00-208 Engine - General - Visual check of high pressure turbine section casing, paying particular attention for cracks, bulges, hot spots and security of centre body
10-Feb-2016Mos
300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs
6,769Enc
(PKG 300 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈25-Sep-2016RE72-00-00-208 Engine - General - Visual check of high pressure turbine section casing, paying particular attention for cracks, bulges, hot spots and security of centre body
10-Feb-2016Mos
300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs
6,728Enc
(PKG 300 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈10-May-2017RE72-00-00-209 Engine - General - Carry out a visual check of the following: (1) Compressor assembly for missing lock tabs on visible Variable Vane Outer Shanknuts / (2) Fan Rotor
Blade Removal Port, Water Drain for blockage / Borescope inspection of outer transition liner. This inspection applies to Engine 350489 and below as instructed in G.E.
SB 72-32 that have not been modified to SB 72-38
10-Feb-2016Mos
600 Hrs (+40)(12,737.4)-/+4060012,137.4Hrs
6,769Enc
(PKG 600 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE72-00-00-209 Engine - General - Carry out a visual check of the following: (1) Compressor assembly for missing lock tabs on visible Variable Vane Outer Shanknuts / (2) Fan Rotor
Blade Removal Port, Water Drain for blockage / Borescope inspection of outer transition liner. This inspection applies to Engine 350489 and below as instructed in G.E.
SB 72-32 that have not been modified to SB 72-38
10-Feb-2016Mos
590.8 Hrs (+40)(12,611.2)-/+4060012,020.4Hrs
6,728Enc
(PKG 600 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE72-00-00-210 Engine - General - Borescope inspection of combustion liner / Visual Check for cracks in combustion chamber frame / Borescope inspection of fuel injectors, paying
particular attention to centering in swirlers / Borescope inspection of outer transition liner. This inspection applies to Engine 350489 and below as instructed in G.E. SB
72-32 that have not been modified to SB 72-38
29-Oct-2012Mos
812.3 Hrs (+40)(12,949.7)-/+401,20011,749.7Hrs
Enc
(PKG 1200 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE72-00-00-210 Engine - General - Borescope inspection of combustion liner / Visual Check for cracks in combustion chamber frame / Borescope inspection of fuel injectors, paying
particular attention to centering in swirlers / Borescope inspection of outer transition liner. This inspection applies to Engine 350489 and below as instructed in G.E. SB
72-32 that have not been modified to SB 72-38
29-Oct-2012Mos
812.3 Hrs (+40)(12,832.7)-/+401,20011,632.7Hrs
Enc
(PKG 1200 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM279/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈20-Oct-2017RE72-00-00-211 Engine - General - Borescope inspection of turbine section, stage 1 nozzle and HPT stage 1 blades
29-Oct-2012Mos
812.3 Hrs (+40)(12,949.7)-/+401,20011,749.7Hrs
Enc
(PKG 1200 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE72-00-00-211 Engine - General - Borescope inspection of turbine section, stage 1 nozzle and HPT stage 1 blades
29-Oct-2012Mos
812.3 Hrs (+40)(12,832.7)-/+401,20011,632.7Hrs
Enc
(PKG 1200 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE72-00-00-212 Engine - General (Pre G.E. SB (CF34) 72-11) - Borescope inspection of Power Take-Off (PTO) Part Number 6037T72G01 or 6037T72G06 for forward movement of Carbon
Sleeve
29-Oct-2012Mos
812.3 Hrs (+40)(12,949.7)-/+401,20011,749.7Hrs
Enc
(PKG 1200 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE72-00-00-212 Engine - General (Pre G.E. SB (CF34) 72-11) - Borescope inspection of Power Take-Off (PTO) Part Number 6037T72G01 or 6037T72G06 for forward movement of Carbon
Sleeve
29-Oct-2012Mos
812.3 Hrs (+40)(12,832.7)-/+401,20011,632.7Hrs
Enc
(PKG 1200 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈22-Feb-2021RE72-00-00-213 Engine - General - Mid point inspection
05-Jun-2009Mos
2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
Compliance Share SingleDUE: 05-Jun-20191. RE 120 MosEngine - General - Borescope Inspection of Engine72-00-00-217 (10 Yrs)ENG172
MRB ≈24-Nov-2019RE72-00-00-213 Engine - General - Mid point inspection
28-Jul-2005Mos
1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
Compliance Share SingleDUE: 27-Jul-20251. RE 120 MosEngine - General - Borescope Inspection of Engine72-00-00-217 (10 Yrs)ENG272
MRB ≈22-Feb-2021RE72-00-00-215 Engine - General - Borescope Compressor / Visual Check of visible areas of compressor casings / Visual Check of variable vanes, paying particular attention for nicks,
dents, cracks and excessive movement
05-Jun-2009Mos
2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈24-Nov-2019RE72-00-00-215 Engine - General - Borescope Compressor / Visual Check of visible areas of compressor casings / Visual Check of variable vanes, paying particular attention for nicks,
dents, cracks and excessive movement
28-Jul-2005Mos
1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈23-May-2027RE72-00-00-217 Engine - General - Overhaul
05-Jun-2009Mos
5,417.4 Hrs (+40)17,554.8-/+406,00011,554.8Hrs
Enc
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15) (NOTE: If an engine does not reach 3000 hours TSN/TBO before 10 years
since engine installation, a complete borescope inspection of engine must be accomplished.)
Compliance Share SingleDUE: 05-Jun-20191. RE 120 MosEngine - General - Borescope Inspection of Engine72-00-00-217 (10 Yrs)ENG172
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM280/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈23-Feb-2026RE72-00-00-217 Engine - General - Overhaul
28-Jul-2005Mos
4,818.6 Hrs (+40)16,839-/+406,00010,839Hrs
Enc
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15) (NOTE: If an engine does not reach 3000 hours TSN/TBO before 10 years
since engine installation, a complete borescope inspection of engine must be accomplished.)
Compliance Share SingleDUE: 27-Jul-20251. RE 120 MosEngine - General - Borescope Inspection of Engine72-00-00-217 (10 Yrs)ENG272
MRBRE72-00-00-217 (10 Yrs) Engine - General - Borescope Inspection of Engine
9.3 Years (+31 Days)27-Jul-2025-/+112010-Feb-2016Mos
12,020.4Hrs
6,728Enc
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (Tol. Adjustment: -193d) (SOURCE: TLMC 05-20-15)
MRBRE72-00-00-217 (10 Yrs) Engine - General - Borescope Inspection of Engine
3.2 Years (+30 Days)05-Jun-2019-/+112005-Jun-2009Mos
Hrs
Enc
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈22-Feb-2021RE72-00-00-218 Engine - General - Detailed Inspection of engine accessory gearbox mounts
05-Jun-2009Mos
2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈24-Nov-2019RE72-00-00-218 Engine - General - Detailed Inspection of engine accessory gearbox mounts
28-Jul-2005Mos
1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE72-00-00-219 Engine - General - Oil Sample Check
10-Feb-2016Mos
590.8 Hrs (+40)(12,611.2)-/+4060012,020.4Hrs
6,728Enc
(PKG 600 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈10-May-2017RE72-00-00-219 Engine - General - Oil Sample Check
10-Feb-2016Mos
600 Hrs (+40)(12,737.4)-/+4060012,137.4Hrs
6,769Enc
(PKG 600 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE72-00-00-220 Engine - General (Pre SB 75-2) - B-Sump pressure measurement check
29-Oct-2012Mos
812.3 Hrs (+40)(12,949.7)-/+401,20011,749.7Hrs
Enc
(PKG 1200 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE72-00-00-220 Engine - General (Pre SB 75-2) - B-Sump pressure measurement check
29-Oct-2012Mos
812.3 Hrs (+40)(12,832.7)-/+401,20011,632.7Hrs
Enc
(PKG 1200 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈22-Feb-2021RE72-00-00-221 Engine - General - Visual Check of 6 o’clock c-sump scavenge tube and groove for internal coking
05-Jun-2009Mos
2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈24-Nov-2019RE72-00-00-221 Engine - General - Visual Check of 6 o’clock c-sump scavenge tube and groove for internal coking
28-Jul-2005Mos
1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM281/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈22-Feb-2021RE72-00-00-222 Engine - General - Visual Check of LPT stator assembly P/N 6020T15G14 for tack welding of the pin and clip assemblies. Rework and re-identify if required
05-Jun-2009Mos
2,417.4 Hrs (+40)(14,554.8)3,00011,554.8Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈24-Nov-2019RE72-00-00-222 Engine - General - Visual Check of LPT stator assembly P/N 6020T15G14 for tack welding of the pin and clip assemblies. Rework and re-identify if required
28-Jul-2005Mos
1,818.6 Hrs (+40)(13,839)3,00010,839Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈22-Feb-2021RE72-00-00-223 Engine - General - Visual Check of HPT stage 1 and stage 2 shrouds
05-Jun-2009Mos
2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈24-Nov-2019RE72-00-00-223 Engine - General - Visual Check of HPT stage 1 and stage 2 shrouds
28-Jul-2005Mos
1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈22-Feb-2021RE72-00-00-224 Engine - General - Inspect/Check turbine thermocouple harness
05-Jun-2009Mos
2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈24-Nov-2019RE72-00-00-224 Engine - General - Inspect/Check turbine thermocouple harness
28-Jul-2005Mos
1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈22-Feb-2021RE72-00-00-225 Engine - General - Visual Check of turbine nozzles
05-Jun-2009Mos
2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈24-Nov-2019RE72-00-00-225 Engine - General - Visual Check of turbine nozzles
28-Jul-2005Mos
1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈22-Feb-2021RE72-00-00-226 Engine - General - Detailed visual inspection of the swirlers after removal of the injectors
05-Jun-2009Mos
2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈24-Nov-2019RE72-00-00-226 Engine - General - Detailed visual inspection of the swirlers after removal of the injectors
28-Jul-2005Mos
1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈22-Feb-2021RE72-00-00-227 Engine - General - Visual Check of primary swirlers, paying particular attention for wear
05-Jun-2009Mos
2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM282/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈24-Nov-2019RE72-00-00-227 Engine - General - Visual Check of primary swirlers, paying particular attention for wear
28-Jul-2005Mos
1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈22-Feb-2021RE72-00-00-228 Engine - General - Visual Check of stage 1 and stage 2 nozzle assemblies
05-Jun-2009Mos
2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈24-Nov-2019RE72-00-00-228 Engine - General - Visual Check of stage 1 and stage 2 nozzle assemblies
28-Jul-2005Mos
1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈22-Feb-2021RE72-00-00-229 Engine - General - Visual Check of combustion liner after disassembly
Mos
2,417.4 Hrs (+40)(14,554.8)-/+403,000Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈24-Nov-2019RE72-00-00-229 Engine - General - Visual Check of combustion liner after disassembly
Mos
1,818.6 Hrs (+40)(13,839)-/+403,000Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈22-Feb-2021RE72-00-00-230 Engine - General - Check combustion section fuel injector heat shields for looseness
05-Jun-2009Mos
2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈24-Nov-2019RE72-00-00-230 Engine - General - Check combustion section fuel injector heat shields for looseness
28-Jul-2005Mos
1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈22-Feb-2021RE72-00-00-231 Engine - General - Visual Check of fan disk to ensure bushings are not protruding
05-Jun-2009Mos
2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈24-Nov-2019RE72-00-00-231 Engine - General - Visual Check of fan disk to ensure bushings are not protruding
28-Jul-2005Mos
1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs
Enc
(PKG 3000 Eng Hour)
72 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
Servicing - Optional ≈25-Sep-2016RE72-00-00-301 Engine - General - Compressor Waterwash
10-Feb-2016Mos
300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs
6,769Enc
(PKG 300 Eng Hour)
72 ENG1
Ref.:G.E. M.M. SEI-580 Section 5-21-00, Ref.:G.E. M.M. SEI-780 (ZONE: 410, 420) (ACCESS: 412-AT, 414-AT, 422-AT, 424-AT) (SOURCE: MPD 3.3)
(NOTE: For engine model CF34-1A/-3A/-3A2, it is recommended that this task be done prior to the Power Assurance Check.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM283/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Servicing - Optional ≈25-Sep-2016RE72-00-00-301 Engine - General - Compressor Waterwash
10-Feb-2016Mos
300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs
6,728Enc
(PKG 300 Eng Hour)
72 ENG2
Ref.:G.E. M.M. SEI-580 Section 5-21-00, Ref.:G.E. M.M. SEI-780 (ZONE: 410, 420) (ACCESS: 412-AT, 414-AT, 422-AT, 424-AT) (SOURCE: MPD 3.3)
(NOTE: For engine model CF34-1A/-3A/-3A2, it is recommended that this task be done prior to the Power Assurance Check.)
Servicing - Optional ≈25-Sep-2016RE72-00-00-302 Engine - General (Engine model CF34-1A/-3A/-3A2 only) - Power Assurance Check
10-Feb-2016Mos
300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs
6,728Enc
(PKG 300 Eng Hour)
72 ENG2
Ref.:G.E. M.M. SEI-580 Section 5-21-00 (ZONE: 220, 410, 420) (SOURCE: MPD 3.3) (NOTE: It is recommended that this task be done following
the Compressor Waterwash Check.)
Servicing - Optional ≈25-Sep-2016RE72-00-00-302 Engine - General (Engine model CF34-1A/-3A/-3A2 only) - Power Assurance Check
10-Feb-2016Mos
300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs
6,769Enc
(PKG 300 Eng Hour)
72 ENG1
Ref.:G.E. M.M. SEI-580 Section 5-21-00 (ZONE: 220, 410, 420) (SOURCE: MPD 3.3) (NOTE: It is recommended that this task be done following
the Compressor Waterwash Check.)
Recommended ≈20-Dec-1989T72-0005 R06 ENGINE - Life Improvement of Certain High-Pressure and Low-Pressure Turbine Parts by Rework
Mos
OVD3,0003,000Hrs
Enc
72 ENG1
Recommended ≈20-Dec-1989T72-0005 R06 ENGINE - Life Improvement of Certain High-Pressure and Low-Pressure Turbine Parts by Rework
Mos
OVD3,0003,000Hrs
Enc
72 ENG2
RecommendedRE (-)72-0008 R02 ENGINE Modification of CF341A Engines to CF343A Engines
Mos
Hrs
Enc
72 ENG1Eff: 04-Oct-1989
RecommendedRE (-)72-0008 R02 ENGINE Modification of CF341A Engines to CF343A Engines
Mos
Hrs
Enc
72 ENG2Eff: 04-Oct-1989
RecommendedRE (-)72-0010 R02 ENGINE - Power Takeoff (PTO) Drive Assembly: Replacement of Duplex Ball Bearing
Mos
Hrs
Enc
72 ENG1Eff: 25-Apr-1991
Also ConsiderDUE:1. RE -ENGINE - Power Takeoff (PTO) Drive Assembly: Rework of PTO D...72-0011 R03ENG172
Also ConsiderDUE:1. RE -ENGINE - Power Take off (PTO) Drive Assembly: Increased Torq...72-0013 R00ENG172
RecommendedRE (-)72-0010 R02 ENGINE - Power Takeoff (PTO) Drive Assembly: Replacement of Duplex Ball Bearing
Mos
Hrs
Enc
72 ENG2Eff: 25-Apr-1991
Also ConsiderDUE:1. RE -ENGINE - Power Takeoff (PTO) Drive Assembly: Rework of PTO D...72-0011 R03ENG272
Also ConsiderDUE:1. RE -ENGINE - Power Take off (PTO) Drive Assembly: Increased Torq...72-0013 R00ENG272
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM284/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)72-0011 R00 ENGINE Power Takeoff (PTO) Drive Assembly: Rework of PTO Drive Assembly
Mos
Hrs
Enc
72 ENG1Eff: 09-Jun-1989
RecommendedRE (-)72-0011 R00 ENGINE Power Takeoff (PTO) Drive Assembly: Rework of PTO Drive Assembly
Mos
Hrs
Enc
72 ENG2Eff: 09-Jun-1989
RecommendedRE (-)72-0011 R01 ENGINE Power Takeoff (PTO) Drive Assembly: Rework of PTO Drive Assembly
Mos
Hrs
Enc
72 ENG1Eff: 31-Aug-1989
RecommendedRE (-)72-0011 R01 ENGINE Power Takeoff (PTO) Drive Assembly: Rework of PTO Drive Assembly
Mos
Hrs
Enc
72 ENG2Eff: 31-Aug-1989
RecommendedRE (-)72-0011 R02 ENGINE Power Takeoff (PTO) Drive Assembly: Rework of PTO Drive Assembly
Mos
Hrs
Enc
72 ENG1Eff: 25-Apr-1991
RecommendedRE (-)72-0011 R02 ENGINE Power Takeoff (PTO) Drive Assembly: Rework of PTO Drive Assembly
Mos
Hrs
Enc
72 ENG2Eff: 25-Apr-1991
RecommendedRE (-)72-0011 R03 ENGINE - Power Takeoff (PTO) Drive Assembly: Rework of PTO Drive Assembly
Mos
Hrs
Enc
72 ENG1Eff: 27-Apr-2005
RecommendedRE (-)72-0011 R03 ENGINE - Power Takeoff (PTO) Drive Assembly: Rework of PTO Drive Assembly
Mos
Hrs
Enc
72 ENG2Eff: 27-Apr-2005
RecommendedRE (-)72-0013 R00 ENGINE - Power Take off (PTO) Drive Assembly: Increased Torque on Horizontal and Vertical Axis Locknuts
Mos
Hrs
Enc
72 ENG1Eff: 25-Apr-1991
Also ConsiderDUE:1. RE -ENGINE - Power Takeoff (PTO) Drive Assembly: Rework of PTO D...72-0011 R03ENG172
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2...72-0263 R00ENG172
RecommendedRE (-)72-0013 R00 ENGINE - Power Take off (PTO) Drive Assembly: Increased Torque on Horizontal and Vertical Axis Locknuts
Mos
Hrs
Enc
72 ENG2Eff: 25-Apr-1991
Also ConsiderDUE:1. RE -ENGINE - Power Takeoff (PTO) Drive Assembly: Rework of PTO D...72-0011 R03ENG272
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2...72-0263 R00ENG272
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM285/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)72-0014 R00 ENGINE - Accessory Drive Gearbox (AGB): Replacement of Axis-A Duplex Bearing and Axis-BB Ball Bearing
Mos
Hrs
Enc
72 ENG1Eff: 07-May-1991
RecommendedRE (-)72-0014 R00 ENGINE - Accessory Drive Gearbox (AGB): Replacement of Axis-A Duplex Bearing and Axis-BB Ball Bearing
Mos
Hrs
Enc
72 ENG2Eff: 07-May-1991
RecommendedRE (-)72-0014 R01 ENGINE - Accessory Drive Gearbox (AGB): Replacement of Axis-A Duplex Bearing and Axis-BB Ball Bearing
Mos
Hrs
Enc
72 ENG1Eff: 16-Dec-1991
RecommendedRE (-)72-0014 R01 ENGINE - Accessory Drive Gearbox (AGB): Replacement of Axis-A Duplex Bearing and Axis-BB Ball Bearing
Mos
Hrs
Enc
72 ENG2Eff: 16-Dec-1991
RecommendedRE (-)72-0014 R02 ENGINE - Accessory Drive Gearbox (AGB): Replacement of Axis-A Duplex Bearing and Axis-BB Ball Bearing
Mos
Hrs
Enc
72 ENG1Eff: 07-Jan-1992
Also ConsiderDUE:1. RE -ENGINE - Accessory Gearbox Assembly (72-62-00) - Introductio...72-0260 R03ENG172
RecommendedRE (-)72-0014 R02 ENGINE - Accessory Drive Gearbox (AGB): Replacement of Axis-A Duplex Bearing and Axis-BB Ball Bearing
Mos
Hrs
Enc
72 ENG2Eff: 07-Jan-1992
Also ConsiderDUE:1. RE -ENGINE - Accessory Gearbox Assembly (72-62-00) - Introductio...72-0260 R03ENG272
RecommendedT (A/R)72-0014 R03 ENGINE - Accessory Drive Gearbox (AGB): Replacement of Axis-A Duplex Bearing and Axis-BB Ball Bearing
Mos
Hrs
Enc
72 ENG1Eff: 30-Jun-2015
(NOTE: Effectivity: Engines which do not have AGB PN 6014T81G24)
RecommendedT (A/R)72-0014 R03 ENGINE - Accessory Drive Gearbox (AGB): Replacement of Axis-A Duplex Bearing and Axis-BB Ball Bearing
Mos
Hrs
Enc
72 ENG2Eff: 30-Jun-2015
(NOTE: Effectivity: Engines which do not have AGB PN 6014T81G24)
RecommendedRE (-)72-0015 R02 ENGINE - On-Wing Replacement of Accessory Drive Gearbox (AGB) Axis-BB Ball Bearing
Mos
Hrs
Enc
72 ENG1Eff: 03-Aug-1995
RecommendedRE (-)72-0015 R02 ENGINE - On-Wing Replacement of Accessory Drive Gearbox (AGB) Axis-BB Ball Bearing
Mos
Hrs
Enc
72 ENG2Eff: 03-Aug-1995
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM286/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)72-0016 R00 ENGINE Rework of the Forward Fan Shaft
Mos
Hrs
Enc
72 ENG1Eff: 01-May-1991
RecommendedRE (-)72-0016 R00 ENGINE Rework of the Forward Fan Shaft
Mos
Hrs
Enc
72 ENG2Eff: 01-May-1991
RecommendedRE (-)72-0016 R01 ENGINE Rework of the Forward Fan Shaft
Mos
Hrs
Enc
72 ENG1Eff: 12-Feb-1993
RecommendedRE (-)72-0016 R01 ENGINE Rework of the Forward Fan Shaft
Mos
Hrs
Enc
72 ENG2Eff: 12-Feb-1993
RecommendedRE (-)72-0016 R02 ENGINE - Rework of the Forward Fan Shaft
Mos
Hrs
Enc
72 ENG1Eff: 17-Aug-2007
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2...72-0263 R00ENG172
RecommendedRE (-)72-0016 R02 ENGINE - Rework of the Forward Fan Shaft
Mos
Hrs
Enc
72 ENG2Eff: 17-Aug-2007
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2...72-0263 R00ENG272
RecommendedRE (-)72-0017 R02 ENGINE - Rework of Fan Disk PN 6020T62G04 Using Enlarged Bushings
Mos
Hrs
Enc
72 ENG1Eff: 21-Apr-1993
RecommendedRE (-)72-0017 R02 ENGINE - Rework of Fan Disk PN 6020T62G04 Using Enlarged Bushings
Mos
Hrs
Enc
72 ENG2Eff: 21-Apr-1993
RecommendedT (A/R)72-0019 R02 ENGINE - Improved Coating for Compressor Stator Casing and Compressor Rotor Front and Rear Spools
Mos
Hrs
Enc
72 ENG1Eff: 21-Apr-1993
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM287/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedT (A/R)72-0019 R02 ENGINE - Improved Coating for Compressor Stator Casing and Compressor Rotor Front and Rear Spools
Mos
Hrs
Enc
72 ENG2Eff: 21-Apr-1993
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
RecommendedRE (-)72-0021 R00 ENGINE - Power Takeoff (PTO) Drive Assembly: Replacement of Radial Duplex Bearing
Mos
Hrs
Enc
72 ENG1Eff: 01-May-1991
RecommendedRE (-)72-0021 R00 ENGINE - Power Takeoff (PTO) Drive Assembly: Replacement of Radial Duplex Bearing
Mos
Hrs
Enc
72 ENG2Eff: 01-May-1991
RecommendedRE (-)72-0021 R01 ENGINE - Power Takeoff (PTO) Drive Assembly: Replacement of Radial Duplex Bearing
Mos
Hrs
Enc
72 ENG1Eff: 17-Dec-1991
RecommendedRE (-)72-0021 R01 ENGINE - Power Takeoff (PTO) Drive Assembly: Replacement of Radial Duplex Bearing
Mos
Hrs
Enc
72 ENG2Eff: 17-Dec-1991
RecommendedRE (-)72-0021 R02 ENGINE - Power Takeoff (PTO) Drive Assembly: Replacement of Radial Duplex Bearing
Mos
Hrs
Enc
72 ENG1Eff: 21-Apr-1993
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2...72-0263 R00ENG172
RecommendedRE (-)72-0021 R02 ENGINE - Power Takeoff (PTO) Drive Assembly: Replacement of Radial Duplex Bearing
Mos
Hrs
Enc
72 ENG2Eff: 21-Apr-1993
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2...72-0263 R00ENG272
RecommendedRE (-)72-0022 R01 ENGINE - Replacement of Combustion Liner Primary Swirlers
Mos
Hrs
Enc
72 ENG1Eff: 05-Dec-1991
RecommendedRE (-)72-0022 R01 ENGINE - Replacement of Combustion Liner Primary Swirlers
Mos
Hrs
Enc
72 ENG2Eff: 05-Dec-1991
RecommendedRE (-)72-0023 R03 ENGINE - Replacement of CF34-3A/-3A2 Stage 1 High-Pressure Turbine (HPT) Blades, and Stages 1 and 2 Wire Seals
Mos
Hrs
Enc
72 ENG1
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM288/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)72-0023 R03 ENGINE - Replacement of CF34-3A/-3A2 Stage 1 High-Pressure Turbine (HPT) Blades, and Stages 1 and 2 Wire Seals
Mos
Hrs
Enc
72 ENG2
RecommendedRE (-)72-0027 R01 ENGINE - Inspection of Low-Pressure Turbine (LPT) Borescope Plugs PN 5071T39G02 and Installation of LPT Borescope Plug Covers PN 3904T92P01
Mos
Hrs
Enc
72 ENG1Eff: 24-Jan-1994
Also ConsiderDUE:1. RE -ENGINE - Rework of the Borescope Plug Bosses on the Low-Pres...72-0037 R01ENG172
RecommendedRE (-)72-0027 R01 ENGINE - Inspection of Low-Pressure Turbine (LPT) Borescope Plugs PN 5071T39G02 and Installation of LPT Borescope Plug Covers PN 3904T92P01
Mos
Hrs
Enc
72 ENG2Eff: 24-Jan-1994
Also ConsiderDUE:1. RE -ENGINE - Rework of the Borescope Plug Bosses on the Low-Pres...72-0037 R01ENG272
RecommendedRE (-)72-0028 R00 ENGINE - Accessory Drive Gearbox (AGB): Improved Axis-BB Rear Ball Bearing
Mos
Hrs
Enc
72 ENG1Eff: 21-Oct-1992
Also ConsiderDUE:1. RE -ENGINE - Accessory Gearbox Assembly (72-62-00) - Introductio...72-0260 R03ENG172
RecommendedRE (-)72-0028 R00 ENGINE - Accessory Drive Gearbox (AGB): Improved Axis-BB Rear Ball Bearing
Mos
Hrs
Enc
72 ENG2Eff: 21-Oct-1992
Also ConsiderDUE:1. RE -ENGINE - Accessory Gearbox Assembly (72-62-00) - Introductio...72-0260 R03ENG272
RecommendedRE (-)72-0028 R01 ENGINE - Accessory Drive Gearbox (AGB): Improved Axis-BB Rear Ball Bearing
Mos
Hrs
Enc
72 ENG1Eff: 08-Jul-2015
RecommendedRE (-)72-0028 R01 ENGINE - Accessory Drive Gearbox (AGB): Improved Axis-BB Rear Ball Bearing
Mos
Hrs
Enc
72 ENG2Eff: 08-Jul-2015
RecommendedRE (-)72-0030 R00 ENGINE Asbestos Elimination
Mos
Hrs
Enc
72 ENG1Eff: 30-Jul-1993
RecommendedRE (-)72-0030 R00 ENGINE Asbestos Elimination
Mos
Hrs
Enc
72 ENG2Eff: 30-Jul-1993
RecommendedRE (-)72-0030 R01 ENGINE Asbestos Elimination
Mos
Hrs
Enc
72 ENG1Eff: 08-Mar-1995
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM289/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)72-0030 R01 ENGINE Asbestos Elimination
Mos
Hrs
Enc
72 ENG2Eff: 08-Mar-1995
RecommendedRE (-)72-0030 R02 ENGINE - Asbestos Elimination
Mos
Hrs
Enc
72 ENG1Eff: 22-Jan-2008
RecommendedRE (-)72-0030 R02 ENGINE - Asbestos Elimination
Mos
Hrs
Enc
72 ENG2Eff: 22-Jan-2008
RecommendedT (A/R)72-0030 R03 ENGINE - Asbestos Elimination
Mos
Hrs
Enc
72 ENG1Eff: 18-Jul-2008
RecommendedT (A/R)72-0030 R03 ENGINE - Asbestos Elimination
Mos
Hrs
Enc
72 ENG2Eff: 18-Jul-2008
OptionalT (A/R)72-0031 R01 ENGINE - Replacement of CF34-1A/-3A/-3A2 Stage 1 High-Pressure Turbine (HPT) Blades, Stage 1 High-Pressure Turbine (HPT) Baffles, and Stages 1 and 2 Wire Seals
Mos
Hrs
Enc
72 ENG1Eff: 15-Jul-1993
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
OptionalT (A/R)72-0031 R01 ENGINE - Replacement of CF34-1A/-3A/-3A2 Stage 1 High-Pressure Turbine (HPT) Blades, Stage 1 High-Pressure Turbine (HPT) Baffles, and Stages 1 and 2 Wire Seals
Mos
Hrs
Enc
72 ENG2Eff: 15-Jul-1993
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
RecommendedRE (-)72-0032 R01 ENGINE - Borescope Inspection of the Turbine Transition Assembly Outer Liner
Mos
Hrs
Enc
72 ENG1Eff: 20-Oct-1993
(NOTE: For engines over 1,200 hours, inspect within the next 300 hours. For engines below 1,200 hours, inspect at first scheduled 1,200 hour
borescope inspection.)
RecommendedRE (-)72-0032 R01 ENGINE - Borescope Inspection of the Turbine Transition Assembly Outer Liner
Mos
Hrs
Enc
72 ENG2Eff: 20-Oct-1993
(NOTE: For engines over 1,200 hours, inspect within the next 300 hours. For engines below 1,200 hours, inspect at first scheduled 1,200 hour
borescope inspection.)
RecommendedRE (-)72-0034 R01 ENGINE - Replacement of CF34-1A Stage 1 High-Pressure Turbine (HPT) Blades, and Stages 1 and 2 Wire Seals
Mos
Hrs
Enc
72 ENG1Eff: 20-Oct-1993
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM290/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)72-0034 R01 ENGINE - Replacement of CF34-1A Stage 1 High-Pressure Turbine (HPT) Blades, and Stages 1 and 2 Wire Seals
Mos
Hrs
Enc
72 ENG2Eff: 20-Oct-1993
Category 7RE (-)72-0035 R00 ENGINE Rear Main Mount: Rework of Additional Hole for Fire Detection System Harness
Mos
Hrs
Enc
72 ENG1Eff: 17-Jan-2003
Category 7RE (-)72-0035 R00 ENGINE Rear Main Mount: Rework of Additional Hole for Fire Detection System Harness
Mos
Hrs
Enc
72 ENG2Eff: 17-Jan-2003
Cat. 7 - OptionalT (A/R)72-0035 R01 ENGINE - Rear Main Mount: Rework of Additional Hole for Fire Detection System Harness
Mos
Hrs
Enc
72 ENG1Eff: 17-Jan-2003
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
Cat. 7 - OptionalT (A/R)72-0035 R01 ENGINE - Rear Main Mount: Rework of Additional Hole for Fire Detection System Harness
Mos
Hrs
Enc
72 ENG2Eff: 17-Jan-2003
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
Cat. 3 - RecommendedRE (-)72-0037 R01 ENGINE - Rework of the Borescope Plug Bosses on the Low-Pressure Turbine Casing
Mos
Hrs
Enc
72 ENG1Eff: 28-Jun-2000
Cat. 3 - RecommendedRE (-)72-0037 R01 ENGINE - Rework of the Borescope Plug Bosses on the Low-Pressure Turbine Casing
Mos
Hrs
Enc
72 ENG2Eff: 28-Jun-2000
RecommendedRE (-)72-0038 R02 ENGINE - Replacement of Forward Transition Liner Seal and Turbine Transition Outer Liner
Mos
Hrs
Enc
72 ENG1
(NOTE: It is recommended that this Service Bulletin be accomplished within the next 300 hours for those operators that have completed the
3000 hour hot section inspection and retained the original liner and seal in their unmodified condition (not hardcoated).It is recommended for
those operators that have not completed the 3000 hours hot section inspection that this Service Bulletin be accomplished at the 3000 hour hot
section inspection.)
RecommendedRE (-)72-0038 R02 ENGINE - Replacement of Forward Transition Liner Seal and Turbine Transition Outer Liner
Mos
Hrs
Enc
72 ENG2
(NOTE: It is recommended that this Service Bulletin be accomplished within the next 300 hours for those operators that have completed the
3000 hour hot section inspection and retained the original liner and seal in their unmodified condition (not hardcoated).It is recommended for
those operators that have not completed the 3000 hours hot section inspection that this Service Bulletin be accomplished at the 3000 hour hot
section inspection.)
OptionalT (A/R)72-0039 R00 ENGINE - Rework of Rear C-Sump Cover: Vent Tube Screen
Mos
Hrs
Enc
72 ENG1Eff: 26-Jan-1994
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM291/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalT (A/R)72-0039 R00 ENGINE - Rework of Rear C-Sump Cover: Vent Tube Screen
Mos
Hrs
Enc
72 ENG2Eff: 26-Jan-1994
Category 4RE (-)72-0040 R00 ENGINE Rework of the Compressor Rotor Assembly
Mos
Hrs
Enc
72 ENG1Eff: 18-Feb-1994
Category 4RE (-)72-0040 R00 ENGINE Rework of the Compressor Rotor Assembly
Mos
Hrs
Enc
72 ENG2Eff: 18-Feb-1994
Cat. 4 - RecommendedT (A/R)72-0040 R01 ENGINE - Rework of the Compressor Rotor Assembly
Mos
Hrs
Enc
72 ENG1Eff: 30-Aug-2006
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
Cat. 4 - RecommendedT (A/R)72-0040 R01 ENGINE - Rework of the Compressor Rotor Assembly
Mos
Hrs
Enc
72 ENG2Eff: 30-Aug-2006
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
RecommendedRE (-)72-0041 R00 ENGINE - Replacement of the Borescope Plug in the High-Pressure Turbine Casing
Mos
Hrs
Enc
72 ENG1Eff: 05-May-1994
RecommendedRE (-)72-0041 R00 ENGINE - Replacement of the Borescope Plug in the High-Pressure Turbine Casing
Mos
Hrs
Enc
72 ENG2Eff: 05-May-1994
RecommendedRE (-)72-0043 R00 ENGINE - Replacement of the Engine Identification Plate
Mos
Hrs
Enc
72 ENG1Eff: 10-Jun-1994
RecommendedRE (-)72-0043 R00 ENGINE - Replacement of the Engine Identification Plate
Mos
Hrs
Enc
72 ENG2Eff: 10-Jun-1994
RecommendedRE (-)72-0046 R00 ENGINE - One-Time Visual and Torque Inspection of the Total Temperature and Pressure Boss Cap
Mos
Hrs
Enc
72 ENG1Eff: 08-Dec-1994
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM292/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)72-0046 R00 ENGINE - One-Time Visual and Torque Inspection of the Total Temperature and Pressure Boss Cap
Mos
Hrs
Enc
72 ENG2Eff: 08-Dec-1994
Category 9RE (-)72-0048 R00 ENGINE General Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG1Eff: 26-Jan-1995
Category 9RE (-)72-0048 R00 ENGINE General Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG2Eff: 26-Jan-1995
Category 9RE (-)72-0048 R01 ENGINE General Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG1Eff: 08-Sep-1995
Category 9RE (-)72-0048 R01 ENGINE General Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG2Eff: 08-Sep-1995
Category 9RE (-)72-0048 R02 ENGINE General Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG1Eff: 26-Apr-1999
Category 9RE (-)72-0048 R02 ENGINE General Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG2Eff: 26-Apr-1999
Category 9RE (-)72-0048 R03 ENGINE General Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG1Eff: 29-Jun-2001
Category 9RE (-)72-0048 R03 ENGINE General Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG2Eff: 29-Jun-2001
Category 9RE (-)72-0048 R04 ENGINE General Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG1Eff: 28-Aug-2001
Category 9RE (-)72-0048 R04 ENGINE General Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG2Eff: 28-Aug-2001
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM293/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 9 - InformationalRE (-)72-0048 R05 ENGINE - General - Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG1Eff: 21-Apr-2005
Cat. 9 - InformationalRE (-)72-0048 R05 ENGINE - General - Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG2Eff: 21-Apr-2005
Cat. 9 - InformationalRE (-)72-0048 R06 ENGINE - General - Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG1Eff: 18-May-2006
Cat. 9 - InformationalRE (-)72-0048 R06 ENGINE - General - Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG2Eff: 18-May-2006
Cat. 9 - InformationalRE (-)72-0048 R07 ENGINE - General - Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG1Eff: 23-Apr-2012
Cat. 9 - InformationalRE (-)72-0048 R07 ENGINE - General - Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG2Eff: 23-Apr-2012
Cat. 9 - InformationalRE (-)72-0048 R08 ENGINE - General - Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG1Eff: 05-Nov-2013
Cat. 9 - InformationalRE (-)72-0048 R08 ENGINE - General - Hardware Exposed to Abnormal Operating Events
Mos
Hrs
Enc
72 ENG2Eff: 05-Nov-2013
RecommendedRE (-)72-0049 R01 ENGINE - Introduction of Kalrez Preformed Packing PN J1400P044
Mos
Hrs
Enc
72 ENG1Eff: 04-Dec-1995
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
RecommendedRE (-)72-0049 R01 ENGINE - Introduction of Kalrez Preformed Packing PN J1400P044
Mos
Hrs
Enc
72 ENG2Eff: 04-Dec-1995
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM294/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Category 1RE (-)72-0051 R00 ENGINE General (720000) Compliance and Interchangeability Statements Used in CF34BJ Service Bulletins
Mos
Hrs
Enc
72 ENG1Eff: 15-Jun-1995
Category 1RE (-)72-0051 R00 ENGINE General (720000) Compliance and Interchangeability Statements Used in CF34BJ Service Bulletins
Mos
Hrs
Enc
72 ENG2Eff: 15-Jun-1995
Cat. 9 - InformationalT (A/R)72-0051 R01 ENGINE - General (72-00-00) - Compliance and Interchangeability Statements Used in CF34-BJ Service Bulletins
Mos
Hrs
Enc
72 ENG1Eff: 11-May-2012
Cat. 9 - InformationalT (A/R)72-0051 R01 ENGINE - General (72-00-00) - Compliance and Interchangeability Statements Used in CF34-BJ Service Bulletins
Mos
Hrs
Enc
72 ENG2Eff: 11-May-2012
OptionalT (A/R)72-0052 R00 ENGINE - Alternate Parts for Upgrade of Compressor Rotor Assemblies During LCF Changes
Mos
Hrs
Enc
72 ENG1Eff: 25-Jan-1996
OptionalT (A/R)72-0052 R00 ENGINE - Alternate Parts for Upgrade of Compressor Rotor Assemblies During LCF Changes
Mos
Hrs
Enc
72 ENG2Eff: 25-Jan-1996
RecommendedRE (-)72-0053 R00 ENGINE - Recommended Upgrade Program to Reduce Unscheduled Engine Removals for CF34-1A/-3A/-3A2 Model Engines
Mos
+500Hrs
Enc
72 ENG1Eff: 27-Sep-1996
(NOTE: Compliance Operators of affected CF34-1A/-3A/-3A2 model engines will receive GE financial participation, if they comply with this
Service Bulletin prior to or concurrent with hot section inspection, between 2000-2500 hours TSN.)
RecommendedRE (-)72-0053 R00 ENGINE - Recommended Upgrade Program to Reduce Unscheduled Engine Removals for CF34-1A/-3A/-3A2 Model Engines
Mos
+500Hrs
Enc
72 ENG2Eff: 27-Sep-1996
(NOTE: Compliance Operators of affected CF34-1A/-3A/-3A2 model engines will receive GE financial participation, if they comply with this
Service Bulletin prior to or concurrent with hot section inspection, between 2000-2500 hours TSN.)
Category 3RE (-)72-0054 R00 ENGINE Rework of the HighPressure Turbine Stator Borescope Plugs to Threaded Configuration
Mos
Hrs
Enc
72 ENG1Eff: 04-Dec-1995
Category 3RE (-)72-0054 R00 ENGINE Rework of the HighPressure Turbine Stator Borescope Plugs to Threaded Configuration
Mos
Hrs
Enc
72 ENG2Eff: 04-Dec-1995
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM295/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Category 3RE (-)72-0054 R01 ENGINE Rework of the HighPressure Turbine Stator Borescope Plugs to Threaded Configuration
Mos
Hrs
Enc
72 ENG1
Category 3RE (-)72-0054 R01 ENGINE Rework of the HighPressure Turbine Stator Borescope Plugs to Threaded Configuration
Mos
Hrs
Enc
72 ENG2
Category 3RE (-)72-0054 R02 ENGINE Rework of the HighPressure Turbine Stator Borescope Plugs to Threaded Configuration
Mos
Hrs
Enc
72 ENG1Eff: 08-Jun-2000
Category 3RE (-)72-0054 R02 ENGINE Rework of the HighPressure Turbine Stator Borescope Plugs to Threaded Configuration
Mos
Hrs
Enc
72 ENG2Eff: 08-Jun-2000
Cat. 3 - RecommendedRE (-)72-0054 R03 ENGINE - Rework of the High-Pressure Turbine Stator Borescope Plugs to Threaded Configuration
Mos
Hrs
Enc
72 ENG1Eff: 14-Mar-2007
Cat. 3 - RecommendedRE (-)72-0054 R03 ENGINE - Rework of the High-Pressure Turbine Stator Borescope Plugs to Threaded Configuration
Mos
Hrs
Enc
72 ENG2Eff: 14-Mar-2007
RecommendedRE (-)72-0055 R00 ENGINE Fan Rotor Introduction of Improved LCF Fan Disks
Mos
Hrs
Enc
72 ENG1Eff: 17-Jan-2003
RecommendedRE (-)72-0055 R00 ENGINE Fan Rotor Introduction of Improved LCF Fan Disks
Mos
Hrs
Enc
72 ENG2Eff: 17-Jan-2003
RecommendedRE (-)72-0055 R01 ENGINE - Fan Rotor - Introduction of Improved LCF Fan Disks
Mos
Hrs
Enc
72 ENG1Eff: 17-Jan-2003
RecommendedRE (-)72-0055 R01 ENGINE - Fan Rotor - Introduction of Improved LCF Fan Disks
Mos
Hrs
Enc
72 ENG2Eff: 17-Jan-2003
RecommendedRE (-)72-0056 R00 ENGINE - Engine Waterwash at 300-Hours
Mos
Hrs
Enc
72 ENG1Eff: 22-Jul-1996
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM296/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)72-0056 R00 ENGINE - Engine Waterwash at 300-Hours
Mos
Hrs
Enc
72 ENG2Eff: 22-Jul-1996
RecommendedRE (-)72-0057 R00 FUEL SYSTEM - Accessory Drive Gearbox (AGB) - Replacement of Axis-J Ball Bearing PN 4017T02P01/P03 with New Roller Bearing PN 4017T12P03/P04
Mos
Hrs
Enc
72 ENG1Eff: 18-Mar-1997
RecommendedRE (-)72-0057 R00 FUEL SYSTEM - Accessory Drive Gearbox (AGB) - Replacement of Axis-J Ball Bearing PN 4017T02P01/P03 with New Roller Bearing PN 4017T12P03/P04
Mos
Hrs
Enc
72 ENG2Eff: 18-Mar-1997
RecommendedRE (-)72-0057 R01 FUEL SYSTEM - Accessory Drive Gearbox (AGB) - Replacement of Axis-J Ball Bearing PN 4017T02P01/P03 with New Roller Bearing PN 4017T12P03/P04
Mos
Hrs
Enc
72 ENG1Eff: 01-Jan-1998
RecommendedRE (-)72-0057 R01 FUEL SYSTEM - Accessory Drive Gearbox (AGB) - Replacement of Axis-J Ball Bearing PN 4017T02P01/P03 with New Roller Bearing PN 4017T12P03/P04
Mos
Hrs
Enc
72 ENG2Eff: 01-Jan-1998
RecommendedRE (-)72-0057 R02 FUEL SYSTEM - Accessory Drive Gearbox (AGB) - Replacement of Axis-J Ball Bearing PN 4017T02P01/P03 with New Roller Bearing PN 4017T12P03/P04
Mos
Hrs
Enc
72 ENG1Eff: 06-Jun-1999
RecommendedRE (-)72-0057 R02 FUEL SYSTEM - Accessory Drive Gearbox (AGB) - Replacement of Axis-J Ball Bearing PN 4017T02P01/P03 with New Roller Bearing PN 4017T12P03/P04
Mos
Hrs
Enc
72 ENG2Eff: 06-Jun-1999
RecommendedRE (-)72-0057 R03 FUEL SYSTEM - Accessory Drive Gearbox (AGB) - Replacement of Axis-J Ball Bearing PN 4017T02P01/P03 with New Roller Bearing PN 4017T12P03/P04
Mos
Hrs
Enc
72 ENG1Eff: 11-Feb-1999
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
Also ConsiderDUE:1. RE -ENGINE - Accessory Gearbox Assembly (72-62-00) - Introductio...72-0260 R03ENG172
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2...72-0263 R00ENG172
RecommendedRE (-)72-0057 R03 FUEL SYSTEM - Accessory Drive Gearbox (AGB) - Replacement of Axis-J Ball Bearing PN 4017T02P01/P03 with New Roller Bearing PN 4017T12P03/P04
Mos
Hrs
Enc
72 ENG2Eff: 11-Feb-1999
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
Also ConsiderDUE:1. RE -ENGINE - Accessory Gearbox Assembly (72-62-00) - Introductio...72-0260 R03ENG272
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2...72-0263 R00ENG272
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM297/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)72-0058 R00 ENGINE Compressor VanetoBlade Axial Clearance Increase
Mos
Hrs
Enc
72 ENG1Eff: 08-Apr-1997
RecommendedRE (-)72-0058 R00 ENGINE Compressor VanetoBlade Axial Clearance Increase
Mos
Hrs
Enc
72 ENG2Eff: 08-Apr-1997
RecommendedRE (-)72-0058 R01 ENGINE Compressor VanetoBlade Axial Clearance Increase
Mos
Hrs
Enc
72 ENG1Eff: 12-Nov-1999
RecommendedRE (-)72-0058 R01 ENGINE Compressor VanetoBlade Axial Clearance Increase
Mos
Hrs
Enc
72 ENG2Eff: 12-Nov-1999
RecommendedRE (-)72-0058 R02 ENGINE - Compressor Vane-to-Blade Axial Clearance Increase
Mos
Hrs
Enc
72 ENG1Eff: 13-Jan-2004
RecommendedRE (-)72-0058 R02 ENGINE - Compressor Vane-to-Blade Axial Clearance Increase
Mos
Hrs
Enc
72 ENG2Eff: 13-Jan-2004
RecommendedT (A/R)72-0058 R03 ENGINE - Compressor Vane-to-Blade Axial Clearance Increase
Mos
Hrs
Enc
72 ENG1Eff: 27-Apr-2006
RecommendedT (A/R)72-0058 R03 ENGINE - Compressor Vane-to-Blade Axial Clearance Increase
Mos
Hrs
Enc
72 ENG2Eff: 27-Apr-2006
Category 3RE (-)72-0060 R00 ENGINE Rework of the Power Takeoff (PTO) Assemblies PN 6037T72G12/G16/G17 and Introduction of PTO Assembly PN 6037T72G18
Mos
Hrs
Enc
72 ENG1Eff: 16-Apr-1997
Category 3RE (-)72-0060 R00 ENGINE Rework of the Power Takeoff (PTO) Assemblies PN 6037T72G12/G16/G17 and Introduction of PTO Assembly PN 6037T72G18
Mos
Hrs
Enc
72 ENG2Eff: 16-Apr-1997
Category 3RE (-)72-0060 R01 ENGINE Rework of the Power Takeoff (PTO) Assemblies PN 6037T72G12/G16/G17 and Introduction of PTO Assembly PN 6037T72G18
Mos
Hrs
Enc
72 ENG1
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM298/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Category 3RE (-)72-0060 R01 ENGINE Rework of the Power Takeoff (PTO) Assemblies PN 6037T72G12/G16/G17 and Introduction of PTO Assembly PN 6037T72G18
Mos
Hrs
Enc
72 ENG2
Category 3RE (-)72-0060 R02 ENGINE Rework of the Power Takeoff (PTO) Assemblies PN 6037T72G12/G16/G17 and Introduction of PTO Assembly PN 6037T72G18
Mos
Hrs
Enc
72 ENG1
Category 3RE (-)72-0060 R02 ENGINE Rework of the Power Takeoff (PTO) Assemblies PN 6037T72G12/G16/G17 and Introduction of PTO Assembly PN 6037T72G18
Mos
Hrs
Enc
72 ENG2
Cat. 3 - RecommendedT (A/R)72-0060 R03 ENGINE - Rework of the Power Takeoff (PTO) Assemblies PN 6037T72G12/G16/G17 and Introduction of PTO Assembly PN 6037T72G18
Mos
Hrs
Enc
72 ENG1Eff: 11-Mar-2003
Cat. 3 - RecommendedT (A/R)72-0060 R03 ENGINE - Rework of the Power Takeoff (PTO) Assemblies PN 6037T72G12/G16/G17 and Introduction of PTO Assembly PN 6037T72G18
Mos
Hrs
Enc
72 ENG2Eff: 11-Mar-2003
RecommendedRE (-)72-0061 R00 ENGINE - Stage 1 Compressor Rotor Disk PN 6087T00G02 Broach Spacing
Mos
Hrs
Enc
72 ENG1Eff: 19-May-1997
RecommendedRE (-)72-0061 R00 ENGINE - Stage 1 Compressor Rotor Disk PN 6087T00G02 Broach Spacing
Mos
Hrs
Enc
72 ENG2Eff: 19-May-1997
RecommendedT (A/R)72-0062 R00 ENGINE - Introduction of Improved High-Pressure Turbine (HPT) Stage 1 Blades with Internal Coating
Mos
Hrs
Enc
72 ENG1Eff: 18-Jul-1997
RecommendedT (A/R)72-0062 R00 ENGINE - Introduction of Improved High-Pressure Turbine (HPT) Stage 1 Blades with Internal Coating
Mos
Hrs
Enc
72 ENG2Eff: 18-Jul-1997
RecommendedRE (-)72-0063 R00 ENGINE - Rework of Compressor Forward Shaft PN 5037T01P03 to PN 5037T01P04 and Introduction of New Compressor Forward Shaft PN 5037T01P04
Mos
Hrs
Enc
72 ENG1Eff: 17-Jan-2003
RecommendedRE (-)72-0063 R00 ENGINE - Rework of Compressor Forward Shaft PN 5037T01P03 to PN 5037T01P04 and Introduction of New Compressor Forward Shaft PN 5037T01P04
Mos
Hrs
Enc
72 ENG2Eff: 17-Jan-2003
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM299/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)72-0063 R01 ENGINE - Rework of Compressor Forward Shaft PN 5037T01P03 to PN 5037T01P04 and Introduction of New Compressor Forward Shaft PN 5037T01P04
Mos
Hrs
Enc
72 ENG1Eff: 17-Jan-2003
RecommendedRE (-)72-0063 R01 ENGINE - Rework of Compressor Forward Shaft PN 5037T01P03 to PN 5037T01P04 and Introduction of New Compressor Forward Shaft PN 5037T01P04
Mos
Hrs
Enc
72 ENG2Eff: 17-Jan-2003
RecommendedT (A/R)72-0064 R00 ENGINE - Compressor Stator - Elimination of Splitline Pins from Compressor Inner Shrouds
Mos
Hrs
Enc
72 ENG1Eff: 23-Oct-1997
RecommendedT (A/R)72-0064 R00 ENGINE - Compressor Stator - Elimination of Splitline Pins from Compressor Inner Shrouds
Mos
Hrs
Enc
72 ENG2Eff: 23-Oct-1997
Cat. 7 - OptionalRE (-)72-0065 R00 ENGINE - Interchangeability of CF34-3B and CF34-3B1 Engine Models
Mos
Hrs
Enc
72 ENG1Eff: 10-Jun-2003
Cat. 7 - OptionalRE (-)72-0065 R00 ENGINE - Interchangeability of CF34-3B and CF34-3B1 Engine Models
Mos
Hrs
Enc
72 ENG2Eff: 10-Jun-2003
Cat. 7 - OptionalRE (-)72-0065 R01 ENGINE - Interchangeability of CF34-3B and CF34-3B1 Engine Models
Mos
Hrs
Enc
72 ENG1Eff: 10-Jun-2003
Cat. 7 - OptionalRE (-)72-0065 R01 ENGINE - Interchangeability of CF34-3B and CF34-3B1 Engine Models
Mos
Hrs
Enc
72 ENG2Eff: 10-Jun-2003
RecommendedRE (-)72-0066 R00 ENGINE - Fan Rotor - Forward Fan Shaft Design Change
Mos
Hrs
Enc
72 ENG1Eff: 19-Feb-1998
RecommendedRE (-)72-0066 R00 ENGINE - Fan Rotor - Forward Fan Shaft Design Change
Mos
Hrs
Enc
72 ENG2Eff: 19-Feb-1998
RecommendedRE (-)72-0067 R02 ENGINE - CF34-3B Fleet Leader Sampling Program
Mos
Hrs
Enc
72 ENG1Eff: 11-Dec-1998
(NOTE: A CF34-3B turbofan engine which is identified as a "Fleet Leader" (a fleet leader is an engine that has accumulated more hours and/or
more cycles than other engines).)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM300/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)72-0067 R02 ENGINE - CF34-3B Fleet Leader Sampling Program
Mos
Hrs
Enc
72 ENG2Eff: 11-Dec-1998
(NOTE: A CF34-3B turbofan engine which is identified as a "Fleet Leader" (a fleet leader is an engine that has accumulated more hours and/or
more cycles than other engines).)
RecommendedRE (-)72-0068 R00 ENGINE - General - Engine Service Record (Logbook) Entry for the CF34-3B HPT Balance Piston Seal
Mos
Hrs
Enc
72 ENG1Eff: 23-Apr-1998
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
RecommendedRE (-)72-0068 R00 ENGINE - General - Engine Service Record (Logbook) Entry for the CF34-3B HPT Balance Piston Seal
Mos
Hrs
Enc
72 ENG2Eff: 23-Apr-1998
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
RecommendedT (A/R)72-0069 R01 ENGINE - Turbine Transition Assembly - Replacement of the Self-Locking Nuts on the Thermocouple Probes and on the PT5 Pressure Probe or Plug
Mos
Hrs
Enc
72 ENG1Eff: 04-Mar-1999
RecommendedT (A/R)72-0069 R01 ENGINE - Turbine Transition Assembly - Replacement of the Self-Locking Nuts on the Thermocouple Probes and on the PT5 Pressure Probe or Plug
Mos
Hrs
Enc
72 ENG2Eff: 04-Mar-1999
RecommendedRE (-)72-0070 R00 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank Clevis
Mos
Hrs
Enc
72 ENG1Eff: 01-Oct-1998
RecommendedRE (-)72-0070 R00 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank Clevis
Mos
Hrs
Enc
72 ENG2Eff: 01-Oct-1998
RecommendedRE (-)72-0070 R01 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank Clevis
Mos
Hrs
Enc
72 ENG1Eff: 06-Apr-1999
RecommendedRE (-)72-0070 R01 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank Clevis
Mos
Hrs
Enc
72 ENG2Eff: 06-Apr-1999
RecommendedRE (-)72-0070 R02 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank Clevis
Mos
Hrs
Enc
72 ENG1Eff: 09-Jun-1999
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM301/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)72-0070 R02 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank Clevis
Mos
Hrs
Enc
72 ENG2Eff: 09-Jun-1999
RecommendedRE (-)72-0070 R03 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank Clevis
Mos
Hrs
Enc
72 ENG1Eff: 05-Jan-2011
RecommendedRE (-)72-0070 R03 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank Clevis
Mos
Hrs
Enc
72 ENG2Eff: 05-Jan-2011
RecommendedT (-)72-0070 R04 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank and Clevis Bushing
Mos
Hrs
Enc
72 ENG1
(NOTE: For engines with less than 5,000 hours time-since-new (TSN), or for engines with less than 5,000 hours time-since-repair (TSR) (refer to
step 1.D.(7)), it is recommended that an initial clevis bushing inspection be performed at the next opportunity, but not to exceed 5,000 hours
TSN or TSR. All four bushings (for each engine) should be inspected.)
RecommendedT (-)72-0070 R04 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank and Clevis Bushing
Mos
Hrs
Enc
72 ENG2
(NOTE: For engines with less than 5,000 hours time-since-new (TSN), or for engines with less than 5,000 hours time-since-repair (TSR) (refer to
step 1.D.(7)), it is recommended that an initial clevis bushing inspection be performed at the next opportunity, but not to exceed 5,000 hours
TSN or TSR. All four bushings (for each engine) should be inspected.)
RecommendedRE (-)72-0070 R05 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank and Clevis Bushing
Mos
Hrs
Enc
72 ENG1
(NOTE: For engines with less than 5,000 hours time-since-new (TSN), or for engines with less than 5,000 hours time-since-repair (TSR) (refer to
step 1.D.(7)), it is recommended that an initial clevis bushing inspection be performed at the next opportunity, but not to exceed 5,000 hours
TSN or TSR. All four bushings (for each engine) should be inspected.)
RecommendedRE (-)72-0070 R05 ENGINE - Compressor Stator - Inspection and Rework of VG Actuator Bellcrank and Clevis Bushing
Mos
Hrs
Enc
72 ENG2
(NOTE: For engines with less than 5,000 hours time-since-new (TSN), or for engines with less than 5,000 hours time-since-repair (TSR) (refer to
step 1.D.(7)), it is recommended that an initial clevis bushing inspection be performed at the next opportunity, but not to exceed 5,000 hours
TSN or TSR. All four bushings (for each engine) should be inspected.)
RecommendedT (A/R)72-0071 R00 ENGINE - Compressor Rotor - Introduction of Stages 5 through 9 Compressor Rotor Blades with Improved Wear-Resistant Dovetail Coating
Mos
Hrs
Enc
72 ENG1Eff: 09-Nov-1998
RecommendedT (A/R)72-0071 R00 ENGINE - Compressor Rotor - Introduction of Stages 5 through 9 Compressor Rotor Blades with Improved Wear-Resistant Dovetail Coating
Mos
Hrs
Enc
72 ENG2Eff: 09-Nov-1998
RecommendedRE (-)72-0072 R00 ENGINE - Compressor Stator - Introduction of Improved VG Actuator Rings
Mos
Hrs
Enc
72 ENG1Eff: 19-Nov-1998
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM302/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)72-0072 R00 ENGINE - Compressor Stator - Introduction of Improved VG Actuator Rings
Mos
Hrs
Enc
72 ENG2Eff: 19-Nov-1998
RecommendedRE (-)72-0072 R01 ENGINE - Compressor Stator - Introduction of Improved VG Actuator Rings
Mos
Hrs
Enc
72 ENG1Eff: 03-Mar-1999
RecommendedRE (-)72-0072 R01 ENGINE - Compressor Stator - Introduction of Improved VG Actuator Rings
Mos
Hrs
Enc
72 ENG2Eff: 03-Mar-1999
RecommendedT (A/R)72-0072 R02 ENGINE - Compressor Stator - Introduction of Improved VG Actuator Rings
Mos
Hrs
Enc
72 ENG1Eff: 30-Mar-2004
RecommendedT (A/R)72-0072 R02 ENGINE - Compressor Stator - Introduction of Improved VG Actuator Rings
Mos
Hrs
Enc
72 ENG2Eff: 30-Mar-2004
Category 5RE (-)72-0073 R00 ENGINE Eddy Current and Ultrasonic Inspections of the Fan Disk and Compressor Forward Spool
Mos
Hrs
Enc
72 ENG1Eff: 11-Dec-1998
Category 5RE (-)72-0073 R00 ENGINE Eddy Current and Ultrasonic Inspections of the Fan Disk and Compressor Forward Spool
Mos
Hrs
Enc
72 ENG2Eff: 11-Dec-1998
Category 5RE (-)72-0073 R01 ENGINE Eddy Current and Ultrasonic Inspections of the Fan Disk and Compressor Forward Spool
Mos
Hrs
Enc
72 ENG1Eff: 03-Mar-1999
Category 5RE (-)72-0073 R01 ENGINE Eddy Current and Ultrasonic Inspections of the Fan Disk and Compressor Forward Spool
Mos
Hrs
Enc
72 ENG2Eff: 03-Mar-1999
Category 5RE (-)72-0073 R02 ENGINE Eddy Current and Ultrasonic Inspections of the Fan Disk and Compressor Forward Spool
Mos
Hrs
Enc
72 ENG1Eff: 04-May-1999
Category 5RE (-)72-0073 R02 ENGINE Eddy Current and Ultrasonic Inspections of the Fan Disk and Compressor Forward Spool
Mos
Hrs
Enc
72 ENG2Eff: 04-May-1999
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM303/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 5 - RecommendedRE (-)72-0073 R03 ENGINE - Eddy Current and Ultrasonic Inspections of the Fan Disk and Compressor Forward Spool
Mos
Hrs
Enc
72 ENG1Eff: 18-Feb-2009
Cat. 5 - RecommendedRE (-)72-0073 R03 ENGINE - Eddy Current and Ultrasonic Inspections of the Fan Disk and Compressor Forward Spool
Mos
Hrs
Enc
72 ENG2Eff: 18-Feb-2009
RecommendedRE (-)72-0074 R00 ENGINE - Compressor (72-30-00) - Introduction of Improved VG Actuator Shaft and Bellcrank Assembly
Mos
Hrs
Enc
72 ENG1Eff: 24-Nov-1998
RecommendedRE (-)72-0074 R00 ENGINE - Compressor (72-30-00) - Introduction of Improved VG Actuator Shaft and Bellcrank Assembly
Mos
Hrs
Enc
72 ENG2Eff: 24-Nov-1998
RecommendedRE (-)72-0074 R01 ENGINE - Compressor (72-30-00) - Introduction of Improved VG Actuator Shaft and Bellcrank Assembly
Mos
Hrs
Enc
72 ENG1Eff: 06-Apr-1999
RecommendedRE (-)72-0074 R01 ENGINE - Compressor (72-30-00) - Introduction of Improved VG Actuator Shaft and Bellcrank Assembly
Mos
Hrs
Enc
72 ENG2Eff: 06-Apr-1999
RecommendedRE (-)72-0074 R02 ENGINE - Compressor (72-30-00) - Introduction of Improved VG Actuator Shaft and Bellcrank Assembly
Mos
Hrs
Enc
72 ENG1Eff: 30-Sep-1999
RecommendedRE (-)72-0074 R02 ENGINE - Compressor (72-30-00) - Introduction of Improved VG Actuator Shaft and Bellcrank Assembly
Mos
Hrs
Enc
72 ENG2Eff: 30-Sep-1999
RecommendedRE (-)72-0074 R03 ENGINE - Compressor (72-30-00) - Introduction of Improved VG Actuator Shaft and Bellcrank Assembly
Mos
Hrs
Enc
72 ENG1Eff: 02-Aug-2006
RecommendedRE (-)72-0074 R03 ENGINE - Compressor (72-30-00) - Introduction of Improved VG Actuator Shaft and Bellcrank Assembly
Mos
Hrs
Enc
72 ENG2Eff: 02-Aug-2006
RecommendedT (A/R)72-0074 R04 ENGINE - Compressor (72-30-00) - Introduction of Improved VG Actuator Shaft and Bellcrank Assembly
Mos
Hrs
Enc
72 ENG1Eff: 14-Aug-2006
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM304/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedT (A/R)72-0074 R04 ENGINE - Compressor (72-30-00) - Introduction of Improved VG Actuator Shaft and Bellcrank Assembly
Mos
Hrs
Enc
72 ENG2Eff: 14-Aug-2006
RecommendedT (A/R)72-0074 R05 ENGINE - Compressor (72-30-00) - Introduction of Improved VG Actuator Shaft and Bellcrank Assembly
Mos
Hrs
Enc
72 ENG1
RecommendedT (A/R)72-0074 R05 ENGINE - Compressor (72-30-00) - Introduction of Improved VG Actuator Shaft and Bellcrank Assembly
Mos
Hrs
Enc
72 ENG2
Cat. 3 - RecommendedRE (-)72-0075 R00 ENGINE - Combustion Section - Improved Rear Main Mount Firewall Seals
Mos
Hrs
Enc
72 ENG1Eff: 14-Jan-1999
Cat. 3 - RecommendedRE (-)72-0075 R00 ENGINE - Combustion Section - Improved Rear Main Mount Firewall Seals
Mos
Hrs
Enc
72 ENG2Eff: 14-Jan-1999
Cat. 3 - RecommendedRE (-)72-0075 R01 ENGINE - Combustion Section - Improved Rear Main Mount Firewall Seals
Mos
Hrs
Enc
72 ENG1Eff: 19-Feb-1999
Cat. 3 - RecommendedRE (-)72-0075 R01 ENGINE - Combustion Section - Improved Rear Main Mount Firewall Seals
Mos
Hrs
Enc
72 ENG2Eff: 19-Feb-1999
Cat. 3 - RecommendedRE (-)72-0075 R02 ENGINE - Combustion Section - Improved Rear Main Mount Firewall Seals
Mos
Hrs
Enc
72 ENG1Eff: 14-Mar-2003
Cat. 3 - RecommendedRE (-)72-0075 R02 ENGINE - Combustion Section - Improved Rear Main Mount Firewall Seals
Mos
Hrs
Enc
72 ENG2Eff: 14-Mar-2003
Cat. 5 - RecommendedT (A/R)72-0075 R03 ENGINE - Combustion Section - Improved Rear Main Mount Firewall Seals
Mos
Hrs
Enc
72 ENG1Eff: 05-May-2008
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM305/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 5 - RecommendedT (A/R)72-0075 R03 ENGINE - Combustion Section - Improved Rear Main Mount Firewall Seals
Mos
Hrs
Enc
72 ENG2Eff: 05-May-2008
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
Category 3RE (-)72-0077 R00 ENGINE HPT Stator Assembly (724500) Rework of Interstage Turbine Seal, and Introduction of Improved Seal Pin and Retaining Ring Sector
Mos
Hrs
Enc
72 ENG1Eff: 31-Mar-1999
Category 3RE (-)72-0077 R00 ENGINE HPT Stator Assembly (724500) Rework of Interstage Turbine Seal, and Introduction of Improved Seal Pin and Retaining Ring Sector
Mos
Hrs
Enc
72 ENG2Eff: 31-Mar-1999
Category 3RE (-)72-0077 R01 ENGINE HPT Stator Assembly (724500) Rework of Interstage Turbine Seal, and Introduction of Improved Seal Pin and Retaining Ring Sector
Mos
Hrs
Enc
72 ENG1Eff: 06-May-1999
Category 3RE (-)72-0077 R01 ENGINE HPT Stator Assembly (724500) Rework of Interstage Turbine Seal, and Introduction of Improved Seal Pin and Retaining Ring Sector
Mos
Hrs
Enc
72 ENG2Eff: 06-May-1999
Category 3RE (-)72-0077 R02 ENGINE HPT Stator Assembly (724500) Rework of Interstage Turbine Seal, and Introduction of Improved Seal Pin and Retaining Ring Sector
Mos
Hrs
Enc
72 ENG1Eff: 21-Jan-2000
Category 3RE (-)72-0077 R02 ENGINE HPT Stator Assembly (724500) Rework of Interstage Turbine Seal, and Introduction of Improved Seal Pin and Retaining Ring Sector
Mos
Hrs
Enc
72 ENG2Eff: 21-Jan-2000
Category 3RE (-)72-0077 R03 ENGINE HPT Stator Assembly (724500) Rework of Interstage Turbine Seal, and Introduction of Improved Seal Pin and Retaining Ring Sector
Mos
Hrs
Enc
72 ENG1Eff: 08-Jun-2000
Category 3RE (-)72-0077 R03 ENGINE HPT Stator Assembly (724500) Rework of Interstage Turbine Seal, and Introduction of Improved Seal Pin and Retaining Ring Sector
Mos
Hrs
Enc
72 ENG2Eff: 08-Jun-2000
Cat. 3 - RecommendedRE (-)72-0077 R04 ENGINE - HPT Stator Assembly (72-45-00) - Rework of Interstage Turbine Seal and Introduction of Improved Seal Pin and Retaining Ring Sector
Mos
Hrs
Enc
72 ENG1Eff: 12-May-2006
Cat. 3 - RecommendedRE (-)72-0077 R04 ENGINE - HPT Stator Assembly (72-45-00) - Rework of Interstage Turbine Seal and Introduction of Improved Seal Pin and Retaining Ring Sector
Mos
Hrs
Enc
72 ENG2Eff: 12-May-2006
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM306/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 3 - RecommendedT (A/R)72-0077 R05 ENGINE - HPT Stator Assembly (72-45-00) - Rework of Interstage Turbine Seal and Introduction of Improved Seal Pin and Retaining Ring Sector
Mos
Hrs
Enc
72 ENG1Eff: 30-Oct-2006
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
Cat. 3 - RecommendedT (A/R)72-0077 R05 ENGINE - HPT Stator Assembly (72-45-00) - Rework of Interstage Turbine Seal and Introduction of Improved Seal Pin and Retaining Ring Sector
Mos
Hrs
Enc
72 ENG2Eff: 30-Oct-2006
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
RecommendedRE (-)72-0078 R00 ENGINE - Turbine Section - Improved LPT Rotor Assemblies
Mos
Hrs
Enc
72 ENG1Eff: 03-Feb-1999
RecommendedRE (-)72-0078 R00 ENGINE - Turbine Section - Improved LPT Rotor Assemblies
Mos
Hrs
Enc
72 ENG2Eff: 03-Feb-1999
Cat. 6 - RecommendedRE (-)72-0079 R01 ENGINE - Turbine Section - Improved HPT Stator Assembly and Turbine Transition Assembly
Mos
Hrs
Enc
72 ENG1Eff: 08-Jun-2000
Cat. 6 - RecommendedRE (-)72-0079 R01 ENGINE - Turbine Section - Improved HPT Stator Assembly and Turbine Transition Assembly
Mos
Hrs
Enc
72 ENG2Eff: 08-Jun-2000
RecommendedRE (-)72-0080 R01 ENGINE - Fan Rotor - Replacement of No. 1 Ball bearing Manufacturing Lot
Mos
Hrs
Enc
72 ENG1Eff: 09-Jun-1999
RecommendedRE (-)72-0080 R01 ENGINE - Fan Rotor - Replacement of No. 1 Ball bearing Manufacturing Lot
Mos
Hrs
Enc
72 ENG2Eff: 09-Jun-1999
Cat. 3 - RecommendedRE (-)72-0081 R00 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - CF34 Combustion Liner Shell and Dome Part Number and Serial Number Tracking
Mos
Hrs
Enc
72 ENG1Eff: 07-Jul-1999
Also ConsiderDUE:1. RE -ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - In...72-0087 R02ENG172
Cat. 3 - RecommendedRE (-)72-0081 R00 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - CF34 Combustion Liner Shell and Dome Part Number and Serial Number Tracking
Mos
Hrs
Enc
72 ENG2Eff: 07-Jul-1999
Also ConsiderDUE:1. RE -ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - In...72-0087 R02ENG272
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM307/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 2 - RecommendedRE (-)72-0082 R02 ENGINE - Compressor Stator Assembly (72-32-00) - CF34 Compressor Variable Vane Actuating Arm Wear at the Compressor Splitline
12-Nov-1999Mos
Hrs
Enc
72 ENG1BY PART S/N INSTALLEDEff: 12-Nov-1999 Not
Applicable
Also ConsiderDUE:1. RE -ENGINE - Compressor Stator Assembly (72-32-00) - CF34 Compre...72-0134 R01ENG172
Cat. 2 - RecommendedRE (-)72-0082 R02 ENGINE - Compressor Stator Assembly (72-32-00) - CF34 Compressor Variable Vane Actuating Arm Wear at the Compressor Splitline
Mos
Hrs
Enc
72 ENG2Eff: 12-Nov-1999
Also ConsiderDUE:1. RE -ENGINE - Compressor Stator Assembly (72-32-00) - CF34 Compre...72-0134 R01ENG272
Cat. 7 - OptionalRE (-)72-0083 R01 ENGINE - High Pressure Turbine Stator (72-45-00) - Rework of HPT Stator Assembly and Introduction of Improved Durability Stage 2 HPT Nozzle and HPT Inner Case
and Spline Seals
Mos
Hrs
Enc
72 ENG1Eff: 27-Apr-2005
Cat. 7 - OptionalRE (-)72-0083 R01 ENGINE - High Pressure Turbine Stator (72-45-00) - Rework of HPT Stator Assembly and Introduction of Improved Durability Stage 2 HPT Nozzle and HPT Inner Case
and Spline Seals
Mos
Hrs
Enc
72 ENG2Eff: 27-Apr-2005
Cat. 5 - RecommendedRE (-)72-0084 R01 ENGINE - Compressor Rotor Assembly (72-33-00) - Re-identification of Compressor Rotor Assemblies
Mos
Hrs
Enc
72 ENG1Eff: 08-Jun-2000
Cat. 5 - RecommendedRE (-)72-0084 R01 ENGINE - Compressor Rotor Assembly (72-33-00) - Re-identification of Compressor Rotor Assemblies
Mos
Hrs
Enc
72 ENG2Eff: 08-Jun-2000
Cat. 7 - OptionalRE (-)72-0087 R01 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - Introduction of Improved Combustion Liner
Mos
Hrs
Enc
72 ENG1Eff: 21-Oct-2004
Cat. 7 - OptionalRE (-)72-0087 R01 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - Introduction of Improved Combustion Liner
Mos
Hrs
Enc
72 ENG2Eff: 21-Oct-2004
Cat. 7 - OptionalRE (-)72-0087 R02 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - Introduction of Improved Combustion Liner
Mos
Hrs
Enc
72 ENG1Eff: 02-Jan-2007
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Combustion Liner Assembly (72-42-00) - Introduction...72-0240 R00ENG172
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM308/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 7 - OptionalRE (-)72-0087 R02 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - Introduction of Improved Combustion Liner
Mos
Hrs
Enc
72 ENG2Eff: 02-Jan-2007
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Combustion Liner Assembly (72-42-00) - Introduction...72-0240 R00ENG272
Cat. 7 - OptionalT (A/R)72-0089 R00 ENGINE - HPT Rotor (72-46-00) - Introduction of Improved Stage 2 HPT Blades
Mos
Hrs
Enc
72 ENG1Eff: 03-Nov-2000
Cat. 7 - OptionalT (A/R)72-0089 R00 ENGINE - HPT Rotor (72-46-00) - Introduction of Improved Stage 2 HPT Blades
Mos
Hrs
Enc
72 ENG2Eff: 03-Nov-2000
Cat. 3 - RecommendedT (A/R)72-0090 R00 ENGINE - Add Safety Wire at the Total Temperature and Pressure Boss Cap
Mos
Hrs
Enc
72 ENG1Eff: 28-Feb-2001
Cat. 3 - RecommendedT (A/R)72-0090 R00 ENGINE - Add Safety Wire at the Total Temperature and Pressure Boss Cap
Mos
Hrs
Enc
72 ENG2Eff: 28-Feb-2001
Cat. 2 - RecommendedRE (-)72-0091 R00 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection
Mos
Hrs
Enc
72 ENG1Eff: 16-Nov-2001
Cat. 2 - RecommendedRE (-)72-0091 R00 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection
Mos
Hrs
Enc
72 ENG2Eff: 16-Nov-2001
Cat. 2 - RecommendedRE (-)72-0091 R01 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection
Mos
Hrs
Enc
72 ENG1Eff: 09-Oct-2002
(NOTE: If it is recorded in the engine log book that the fan blade pin holes were inspected while in an overhaul shop in accordance with one of
the documents listed below, the intent of the 18,000 CSN requirement of this Service Bulletin has been met. • IFM 20 (dated 04-28-00) •
IFM 20 Revision 1 (dated 05-05-00) • IFM 20 Revision 2 (dated 05-08-00)GE recommends subsequent re-inspection of the affected fan
blades, in compliance with this Service Bulletin, at 3,000 cycle intervals until fan blades with reworked pin holes are available and installed on
the engine.)
Cat. 2 - RecommendedRE (-)72-0091 R01 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection
Mos
Hrs
Enc
72 ENG2Eff: 09-Oct-2002
(NOTE: If it is recorded in the engine log book that the fan blade pin holes were inspected while in an overhaul shop in accordance with one of
the documents listed below, the intent of the 18,000 CSN requirement of this Service Bulletin has been met. • IFM 20 (dated 04-28-00) •
IFM 20 Revision 1 (dated 05-05-00) • IFM 20 Revision 2 (dated 05-08-00)GE recommends subsequent re-inspection of the affected fan
blades, in compliance with this Service Bulletin, at 3,000 cycle intervals until fan blades with reworked pin holes are available and installed on
the engine.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM309/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 2 - RecommendedRE (-)72-0091 R02 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection
Mos
Hrs
Enc
72 ENG1Eff: 14-Jan-2005
(NOTE: If it is recorded in the engine log book that the fan blade pin holes were inspected while in an overhaul shop in accordance with one of
the documents listed below, the intent of the 18,000 CSN requirement of this Service Bulletin has been met. • IFM 20 (dated 04-28-00) •
IFM 20 Revision 1 (dated 05-05-00) • IFM 20 Revision 2 (dated 05-08-00)GE recommends subsequent re-inspection of the affected fan
blades, in compliance with this Service Bulletin, at 3,000 cycle intervals until fan blades with reworked pin holes are available and installed on
the engine.)
Cat. 2 - RecommendedRE (-)72-0091 R02 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection
Mos
Hrs
Enc
72 ENG2Eff: 14-Jan-2005
(NOTE: If it is recorded in the engine log book that the fan blade pin holes were inspected while in an overhaul shop in accordance with one of
the documents listed below, the intent of the 18,000 CSN requirement of this Service Bulletin has been met. • IFM 20 (dated 04-28-00) •
IFM 20 Revision 1 (dated 05-05-00) • IFM 20 Revision 2 (dated 05-08-00)GE recommends subsequent re-inspection of the affected fan
blades, in compliance with this Service Bulletin, at 3,000 cycle intervals until fan blades with reworked pin holes are available and installed on
the engine.)
Cat. 2 - RecommendedRE (-)72-0091 R03 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection
Mos
Hrs
Enc
72 ENG1Eff: 29-Jul-2010
(NOTE: If it is recorded in the engine log book that the fan blade pin holes were inspected while in an overhaul shop in accordance with one of
the documents listed below, the intent of the 18,000 CSN requirement of this Service Bulletin has been met. • IFM 20 (dated 04-28-00) •
IFM 20 Revision 1 (dated 05-05-00) • IFM 20 Revision 2 (dated 05-08-00)GE recommends subsequent re-inspection of the affected fan
blades, in compliance with this Service Bulletin, at 3,000 cycle intervals until fan blades with reworked pin holes are available and installed on
the engine.)
Cat. 2 - RecommendedRE (-)72-0091 R03 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection
Mos
Hrs
Enc
72 ENG2Eff: 29-Jul-2010
(NOTE: If it is recorded in the engine log book that the fan blade pin holes were inspected while in an overhaul shop in accordance with one of
the documents listed below, the intent of the 18,000 CSN requirement of this Service Bulletin has been met. • IFM 20 (dated 04-28-00) •
IFM 20 Revision 1 (dated 05-05-00) • IFM 20 Revision 2 (dated 05-08-00)GE recommends subsequent re-inspection of the affected fan
blades, in compliance with this Service Bulletin, at 3,000 cycle intervals until fan blades with reworked pin holes are available and installed on
the engine.)
Cat. 2 - RecommendedRE (-)72-0091 R04 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection
Mos
Hrs
Enc
72 ENG1Eff: 16-Sep-2010
(NOTE: If it is recorded in the engine log book that the fan blade pin holes were inspected while in an overhaul shop in accordance with one of
the documents listed below, the intent of the 18,000 CSN requirement of this Service Bulletin has been met. • IFM 20 (dated 04-28-00) •
IFM 20 Revision 1 (dated 05-05-00) • IFM 20 Revision 2 (dated 05-08-00)GE recommends subsequent re-inspection of the affected fan
blades, in compliance with this Service Bulletin, at 3,000 cycle intervals until fan blades with reworked pin holes are available and installed on
the engine.)
Cat. 2 - RecommendedRE (-)72-0091 R04 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection
Mos
Hrs
Enc
72 ENG2Eff: 16-Sep-2010
(NOTE: If it is recorded in the engine log book that the fan blade pin holes were inspected while in an overhaul shop in accordance with one of
the documents listed below, the intent of the 18,000 CSN requirement of this Service Bulletin has been met. • IFM 20 (dated 04-28-00) •
IFM 20 Revision 1 (dated 05-05-00) • IFM 20 Revision 2 (dated 05-08-00)GE recommends subsequent re-inspection of the affected fan
blades, in compliance with this Service Bulletin, at 3,000 cycle intervals until fan blades with reworked pin holes are available and installed on
the engine.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM310/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 2 - RecommendedRE (-)72-0091 R05 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection
Mos
Hrs
Enc
72 ENG1Eff: 08-Nov-2010
(NOTE: If it is recorded in the engine log book that the fan blade pin holes were inspected while in an overhaul shop in accordance with one of
the documents listed below, the intent of the 18,000 CSN requirement of this Service Bulletin has been met. • IFM 20 (dated 04-28-00) •
IFM 20 Revision 1 (dated 05-05-00) • IFM 20 Revision 2 (dated 05-08-00)GE recommends subsequent re-inspection of the affected fan
blades, in compliance with this Service Bulletin, at 3,000 cycle intervals until fan blades with reworked pin holes are available and installed on
the engine.)
Cat. 2 - RecommendedRE (-)72-0091 R05 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection
Mos
Hrs
Enc
72 ENG2Eff: 08-Nov-2010
(NOTE: If it is recorded in the engine log book that the fan blade pin holes were inspected while in an overhaul shop in accordance with one of
the documents listed below, the intent of the 18,000 CSN requirement of this Service Bulletin has been met. • IFM 20 (dated 04-28-00) •
IFM 20 Revision 1 (dated 05-05-00) • IFM 20 Revision 2 (dated 05-08-00)GE recommends subsequent re-inspection of the affected fan
blades, in compliance with this Service Bulletin, at 3,000 cycle intervals until fan blades with reworked pin holes are available and installed on
the engine.)
Cat. 2 - Recommended ≈21-Apr-2047RE (-)72-0091 R06 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection
Mos
Hrs
11,231 Enc[18,000]0Enc
72 ENG1Eff: 01-Jun-2011
Cat. 2 - RecommendedRE (-)72-0091 R06 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection
Mos
Hrs
Enc
72 ENG2Eff: 01-Jun-2011
Category 2 ≈21-Apr-2047RE (-)72-0091 R07 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection
Mos
Hrs
11,231 Enc[18,000]Enc
72 ENG1Eff: 13-Apr-2015
Also ConsiderDUE:1. RE -ENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG172
Category 2RE (-)72-0091 R07 ENGINE - Fan Section Module (72-21-00) - Fan Blade Pin Hole Inspection
Mos
Hrs
Enc
72 ENG2Eff: 13-Apr-2015
Also ConsiderDUE: 6,914 Enc1. T 350 Enc | 2. RE 600 EncENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG272
Cat. 5 - RecommendedRE (-)72-0092 R01 HPT Stator Assembly - Introduction of Improved Borescope Plug
Mos
Hrs
Enc
72 ENG1Eff: 14-Dec-2001
Cat. 5 - RecommendedRE (-)72-0092 R01 HPT Stator Assembly - Introduction of Improved Borescope Plug
Mos
Hrs
Enc
72 ENG2Eff: 14-Dec-2001
Cat. 4 - RecommendedRE (-)72-0093 R00 HPT Rotor Assembly (72-46-00) - Introduction of Improved No. 5 Bearing Rotating Air Seal
Mos
Hrs
Enc
72 ENG1Eff: 23-Jul-2001
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM311/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 4 - RecommendedRE (-)72-0093 R00 HPT Rotor Assembly (72-46-00) - Introduction of Improved No. 5 Bearing Rotating Air Seal
Mos
Hrs
Enc
72 ENG2Eff: 23-Jul-2001
Cat. 4 - RecommendedT (-)72-0093 R01 HPT Rotor Assembly (72-46-00) - Introduction of Improved No. 5 Bearing Rotating Air Seal
Mos
Hrs
Enc
72 ENG1Eff: 23-Jul-2001
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
Cat. 4 - RecommendedT (-)72-0093 R01 HPT Rotor Assembly (72-46-00) - Introduction of Improved No. 5 Bearing Rotating Air Seal
Mos
Hrs
Enc
72 ENG2Eff: 23-Jul-2001
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
Cat. 4 - RecommendedT (A/R)72-0093 R02 HPT Rotor Assembly (72-46-00) - Introduction of Improved No. 5 Bearing Rotating Air Seal
Mos
Hrs
Enc
72 ENG1Eff: 27-Apr-2015
Cat. 4 - RecommendedT (A/R)72-0093 R02 HPT Rotor Assembly (72-46-00) - Introduction of Improved No. 5 Bearing Rotating Air Seal
Mos
Hrs
Enc
72 ENG2Eff: 27-Apr-2015
Cat. 7 - OptionalRE (-)72-0095 R00 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - Introduction of Improved-Durability Stage 1 Turbine Nozzle
Mos
Hrs
Enc
72 ENG1Eff: 20-Mar-2001
Cat. 7 - OptionalRE (-)72-0095 R00 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - Introduction of Improved-Durability Stage 1 Turbine Nozzle
Mos
Hrs
Enc
72 ENG2Eff: 20-Mar-2001
Cat. 7 - OptionalT (A/R)72-0095 R01 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - Introduction of Improved-Durability Stage 1 Turbine Nozzle
Mos
Hrs
Enc
72 ENG1Eff: 08-Dec-2008
Cat. 7 - OptionalT (A/R)72-0095 R01 ENGINE - Combustion Liner and Stage 1 Nozzle (72-42-00) - Introduction of Improved-Durability Stage 1 Turbine Nozzle
Mos
Hrs
Enc
72 ENG2Eff: 08-Dec-2008
Cat. 2 - RecommendedRE (-)72-0096 R00 ENGINE - Compressor Section (72-30-00) - Inspection of Compressor Casings and Spools
Mos
Hrs
Enc
72 ENG1Eff: 02-Jul-2002
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM312/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 2 - RecommendedRE (-)72-0096 R00 ENGINE - Compressor Section (72-30-00) - Inspection of Compressor Casings and Spools
Mos
Hrs
Enc
72 ENG2Eff: 02-Jul-2002
Cat. 2 - RecommendedRE (-)72-0098 R02 (LPT Stage 6
Disk)
ENGINE - Low-Pressure Turbine Rotor (72-53-00) - Replacement of Selected CF34 Low-Pressure Turbine Stage 6 Disks.
Mos
Hrs
Enc
72 ENG1Eff: 16-Nov-2004
Cat. 2 - RecommendedRE (-)72-0098 R02 (LPT Stage 6
Disk)
ENGINE - Low-Pressure Turbine Rotor (72-53-00) - Replacement of Selected CF34 Low-Pressure Turbine Stage 6 Disks.
Mos
Hrs
Enc
72 ENG2Eff: 16-Nov-2004
InformationalT (A/R)72-0099 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 24-Jun-2001
InformationalT (A/R)72-0099 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 24-Jun-2001
InformationalRE (-)72-0101 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 29-Jul-2001
InformationalRE (-)72-0101 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 29-Jul-2001
Cat. 4 - RecommendedT (A/R)72-0102 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of Improved Ball Bearing Design for Axes -P, -J, and -K Bearings
Mos
Hrs
Enc
72 ENG1Eff: 07-Sep-2001
(NOTE: This Service Bulletin is not applicable to the CF34 turbofan engines affected that have accessory gearbox assemblies with AGB bearings
PN 5071T20P01 installed)
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
Cat. 4 - RecommendedT (A/R)72-0102 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of Improved Ball Bearing Design for Axes -P, -J, and -K Bearings
Mos
Hrs
Enc
72 ENG2Eff: 07-Sep-2001
(NOTE: This Service Bulletin is not applicable to the CF34 turbofan engines affected that have accessory gearbox assemblies with AGB bearings
PN 5071T20P01 installed)
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
Category 7RE (-)72-0104 R00 ENGINE - High-Pressure Turbine Rotor (72-46-00) Introduction of Improved HPT Stage 1 Blades PN 6078T19P10 and PN 6078T19P11
Mos
Hrs
Enc
72 ENG1Eff: 01-Oct-2001
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM313/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Category 7RE (-)72-0104 R00 ENGINE - High-Pressure Turbine Rotor (72-46-00) Introduction of Improved HPT Stage 1 Blades PN 6078T19P10 and PN 6078T19P11
Mos
Hrs
Enc
72 ENG2Eff: 01-Oct-2001
Cat. 7 - OptionalRE (-)72-0104 R01 ENGINE - High-Pressure Turbine Rotor (72-46-00) - Introduction of Improved HPT Stage 1 Blades PN 6078T19P10 and PN 6078T19P11
Mos
Hrs
Enc
72 ENG1Eff: 23-Feb-2005
Cat. 7 - OptionalRE (-)72-0104 R01 ENGINE - High-Pressure Turbine Rotor (72-46-00) - Introduction of Improved HPT Stage 1 Blades PN 6078T19P10 and PN 6078T19P11
Mos
Hrs
Enc
72 ENG2Eff: 23-Feb-2005
Cat. 7 - OptionalT (A/R)72-0104 R02 ENGINE - High-Pressure Turbine Rotor (72-46-00) - Introduction of Improved HPT Stage 1 Blades PN 6078T19P10 and PN 6078T19P11
Mos
Hrs
Enc
72 ENG1Eff: 05-Nov-2013
Cat. 7 - OptionalT (A/R)72-0104 R02 ENGINE - High-Pressure Turbine Rotor (72-46-00) - Introduction of Improved HPT Stage 1 Blades PN 6078T19P10 and PN 6078T19P11
Mos
Hrs
Enc
72 ENG2Eff: 05-Nov-2013
Cat. 6 - RecommendedRE (-)72-0105 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Assembly PN 6014T81G32 with Metal Peening on Axes L, P, and K Gears
Mos
Hrs
Enc
72 ENG1Eff: 13-Dec-2001
Cat. 6 - RecommendedRE (-)72-0105 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Assembly PN 6014T81G32 with Metal Peening on Axes L, P, and K Gears
Mos
Hrs
Enc
72 ENG2Eff: 13-Dec-2001
Cat. 6 - RecommendedRE (-)72-0105 R01 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Assembly PN 6014T81G32 with Metal Peening on Axes L, P, and K Gears
Mos
Hrs
Enc
72 ENG1Eff: 22-Sep-2014
Cat. 6 - RecommendedRE (-)72-0105 R01 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Assembly PN 6014T81G32 with Metal Peening on Axes L, P, and K Gears
Mos
Hrs
Enc
72 ENG2Eff: 22-Sep-2014
Cat. 6 - RecommendedRE (-)72-0105 R02 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Assembly PN 6014T81G32 with Metal Peening on Axes L, P, and K Gears
Mos
Hrs
Enc
72 ENG1Eff: 29-Sep-2014
Cat. 6 - RecommendedRE (-)72-0105 R02 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Assembly PN 6014T81G32 with Metal Peening on Axes L, P, and K Gears
Mos
Hrs
Enc
72 ENG2Eff: 29-Sep-2014
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM314/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 7 - OptionalRE (-)72-0106 R00 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement
Mos
Hrs
Enc
72 ENG1Eff: 01-Mar-2002
Cat. 7 - OptionalRE (-)72-0106 R00 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement
Mos
Hrs
Enc
72 ENG2Eff: 01-Mar-2002
Cat. 7 - OptionalRE (-)72-0106 R01 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement
Mos
Hrs
Enc
72 ENG1Eff: 07-Nov-2002
Cat. 7 - OptionalRE (-)72-0106 R01 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement
Mos
Hrs
Enc
72 ENG2Eff: 07-Nov-2002
Cat. 4 - RecommendedRE (-)72-0106 R02 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement
Mos
Hrs
Enc
72 ENG1Eff: 17-Jun-2003
Cat. 4 - RecommendedRE (-)72-0106 R02 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement
Mos
Hrs
Enc
72 ENG2Eff: 17-Jun-2003
Cat. 4 - RecommendedRE (-)72-0106 R03 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement
Mos
Hrs
Enc
72 ENG1Eff: 16-Sep-2003
Cat. 4 - RecommendedRE (-)72-0106 R03 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement
Mos
Hrs
Enc
72 ENG2Eff: 16-Sep-2003
Cat. 4 - RecommendedRE (-)72-0106 R04 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 CompressorRotor Blade Replacement
Mos
Hrs
Enc
72 ENG1Eff: 21-Jan-2004
Cat. 4 - RecommendedRE (-)72-0106 R04 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 CompressorRotor Blade Replacement
Mos
Hrs
Enc
72 ENG2Eff: 21-Jan-2004
Cat. 4 - RecommendedRE (-)72-0106 R05 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement
Mos
Hrs
Enc
72 ENG1Eff: 26-Feb-2004
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM315/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 4 - RecommendedRE (-)72-0106 R05 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement
Mos
Hrs
Enc
72 ENG2Eff: 26-Feb-2004
Cat. 4 - RecommendedRE (-)72-0106 R06 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement
Mos
Hrs
Enc
72 ENG1Eff: 09-Jun-2005
Cat. 4 - RecommendedRE (-)72-0106 R06 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement
Mos
Hrs
Enc
72 ENG2Eff: 09-Jun-2005
Cat. 4 - RecommendedT (A/R)72-0106 R07 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement
Mos
Hrs
Enc
72 ENG1Eff: 07-Nov-2005
Cat. 4 - RecommendedT (A/R)72-0106 R07 ENGINE - Compressor Rotor Assembly (72-33-00) - Stage 9 Compressor Rotor Blade Replacement
Mos
Hrs
Enc
72 ENG2Eff: 07-Nov-2005
Cat. 8 - InformationalRE (-)72-0107 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 10-May-2002
Cat. 8 - InformationalRE (-)72-0107 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 10-May-2002
Cat. 8 - InformationalRE (-)72-0107 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 10-May-2002
Cat. 8 - InformationalRE (-)72-0107 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 10-May-2002
Cat. 7 - OptionalRE (-)72-0108 R00 ENGINE - High Pressure Turbine Rotor (72-46-00) or High Pressure Turbine Rotor (72-52-00) - Improved Durability Stage 2 HPT Blade with Airfoil Cavity Coating
Mos
Hrs
Enc
72 ENG1Eff: 01-Mar-2002
Cat. 7 - OptionalRE (-)72-0108 R00 ENGINE - High Pressure Turbine Rotor (72-46-00) or High Pressure Turbine Rotor (72-52-00) - Improved Durability Stage 2 HPT Blade with Airfoil Cavity Coating
Mos
Hrs
Enc
72 ENG2Eff: 01-Mar-2002
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM316/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 4 - RecommendedRE (-)72-0108 R01 ENGINE - High Pressure Turbine Rotor (72-46-00) or High Pressure Turbine Rotor (72-52-00) - Improved Durability Stage 2 HPT Blade with Airfoil Cavity Coating
Mos
Hrs
Enc
72 ENG1Eff: 21-Oct-2003
Cat. 4 - RecommendedRE (-)72-0108 R01 ENGINE - High Pressure Turbine Rotor (72-46-00) or High Pressure Turbine Rotor (72-52-00) - Improved Durability Stage 2 HPT Blade with Airfoil Cavity Coating
Mos
Hrs
Enc
72 ENG2Eff: 21-Oct-2003
Cat. 4 - RecommendedRE (-)72-0108 R02 ENGINE - High Pressure Turbine Rotor (72-46-00) or High Pressure Turbine Rotor (72-52-00) - Improved Durability Stage 2 HPT Blade with Airfoil Cavity Coating
Mos
Hrs
Enc
72 ENG1Eff: 16-Nov-2004
Cat. 4 - RecommendedRE (-)72-0108 R02 ENGINE - High Pressure Turbine Rotor (72-46-00) or High Pressure Turbine Rotor (72-52-00) - Improved Durability Stage 2 HPT Blade with Airfoil Cavity Coating
Mos
Hrs
Enc
72 ENG2Eff: 16-Nov-2004
Cat. 4 - RecommendedRE (-)72-0108 R03 ENGINE - High Pressure Turbine Rotor (72-46-00) or High Pressure Turbine Rotor (72-52-00) - Improved Durability Stage 2 HPT Blade with Airfoil Cavity Coating
Mos
Hrs
Enc
72 ENG1Eff: 23-Feb-2005
Cat. 4 - RecommendedRE (-)72-0108 R03 ENGINE - High Pressure Turbine Rotor (72-46-00) or High Pressure Turbine Rotor (72-52-00) - Improved Durability Stage 2 HPT Blade with Airfoil Cavity Coating
Mos
Hrs
Enc
72 ENG2Eff: 23-Feb-2005
Cat. 4 - RecommendedT (A/R)72-0108 R04 ENGINE - High Pressure Turbine Rotor (72-46-00) or High Pressure Turbine Rotor (72-52-00) - Improved Durability Stage 2 HPT Blade with Airfoil Cavity Coating
Mos
Hrs
Enc
72 ENG1Eff: 23-Feb-2006
Cat. 4 - RecommendedT (A/R)72-0108 R04 ENGINE - High Pressure Turbine Rotor (72-46-00) or High Pressure Turbine Rotor (72-52-00) - Improved Durability Stage 2 HPT Blade with Airfoil Cavity Coating
Mos
Hrs
Enc
72 ENG2Eff: 23-Feb-2006
Cat. 2 - RecommendedRE (-)72-0109 R00 ENGINE - Compressor Stator (72-32-00) - Inspection and Rework of VG Shaft Aft Bearing Support
25-Jul-2008Mos
11,528.2Hrs
6,334Enc
72 ENG1BY PART S/N INSTALLEDEff: 21-May-2002 Not
Applicable
(NOTE: This Service Bulletin is not applicable to CF34 turbofan engines with VG actuator shaft aft bearing support PN 5024T65G03 identified
with supplier code 56946 if the support has been identified with the "R" marking.)
Cat. 2 - RecommendedRE (-)72-0109 R00 ENGINE - Compressor Stator (72-32-00) - Inspection and Rework of VG Shaft Aft Bearing Support
25-Jul-2008Mos
11,411.2Hrs
6,293Enc
72 ENG2BY PART S/N INSTALLEDEff: 21-May-2002 Not
Applicable
(NOTE: This Service Bulletin is not applicable to CF34 turbofan engines with VG actuator shaft aft bearing support PN 5024T65G03 identified
with supplier code 56946 if the support has been identified with the "R" marking.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM317/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 2 - RecommendedRE (-)72-0109 R01 ENGINE - Compressor Stator (72-32-00) - Inspection and Rework of VG Shaft Aft Bearing Support
Mos
Hrs
Enc
72 ENG1Eff: 03-Mar-2003
(NOTE: This Service Bulletin is not applicable to CF34 turbofan engines with VG actuator shaft aft bearing support PN 5024T65G03 identified
with supplier code 56946 if the support has been identified with the "R" marking.)
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Compressor Stator (72-32-00) - Replacement of VG Sh...72-0110 R01ENG172
Cat. 2 - RecommendedRE (-)72-0109 R01 ENGINE - Compressor Stator (72-32-00) - Inspection and Rework of VG Shaft Aft Bearing Support
Mos
Hrs
Enc
72 ENG2Eff: 03-Mar-2003
(NOTE: This Service Bulletin is not applicable to CF34 turbofan engines with VG actuator shaft aft bearing support PN 5024T65G03 identified
with supplier code 56946 if the support has been identified with the "R" marking.)
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Compressor Stator (72-32-00) - Replacement of VG Sh...72-0110 R01ENG272
Cat. 3 - RecommendedRE (-)72-0110 R00 ENGINE - Compressor Stator (72-32-00) - Replacement of VG Shaft Aft Bearing Support
Mos
Hrs
Enc
72 ENG1Eff: 21-May-2002
(NOTE: This Service Bulletin is not applicable to CF34 turbofan engines with VG actuator shaft aft bearing support PN 5024T65G03 identified
with supplier code 56946 if the support has been identified with the rework "R" marking.
For each of the affected engines it is recommended that both VG shaft aft supports be removed and replaced at the next shop visit after
receipt of this Service Bulletin.)
Cat. 3 - RecommendedRE (-)72-0110 R00 ENGINE - Compressor Stator (72-32-00) - Replacement of VG Shaft Aft Bearing Support
Mos
Hrs
Enc
72 ENG2Eff: 21-May-2002
(NOTE: This Service Bulletin is not applicable to CF34 turbofan engines with VG actuator shaft aft bearing support PN 5024T65G03 identified
with supplier code 56946 if the support has been identified with the rework "R" marking.
For each of the affected engines it is recommended that both VG shaft aft supports be removed and replaced at the next shop visit after
receipt of this Service Bulletin.)
Cat. 3 - RecommendedT (A/R)72-0110 R01 ENGINE - Compressor Stator (72-32-00) - Replacement of VG Shaft Aft Bearing Support
Mos
Hrs
Enc
72 ENG1Eff: 27-Feb-2003
(NOTE: This Service Bulletin is not applicable to CF34 turbofan engines with VG actuator shaft aft bearing support PN 5024T65G03 identified
with supplier code 56946 if the support has been identified with the rework "R" marking.
For each of the affected engines it is recommended that both VG shaft aft supports be removed and replaced at the next shop visit after
receipt of this Service Bulletin.)
Cat. 3 - RecommendedT (A/R)72-0110 R01 ENGINE - Compressor Stator (72-32-00) - Replacement of VG Shaft Aft Bearing Support
Mos
Hrs
Enc
72 ENG2Eff: 27-Feb-2003
(NOTE: This Service Bulletin is not applicable to CF34 turbofan engines with VG actuator shaft aft bearing support PN 5024T65G03 identified
with supplier code 56946 if the support has been identified with the rework "R" marking.
For each of the affected engines it is recommended that both VG shaft aft supports be removed and replaced at the next shop visit after
receipt of this Service Bulletin.)
Cat. 2 - RecommendedRE (-)72-0111 R00 ENGINE - Compressor Stator (72-32-00) - Inspection and Temporary Loctite Rework of VG Shaft Aft Bearing Support
Mos
Hrs
Enc
72 ENG1Eff: 02-Apr-2002
(NOTE: This Service Bulletin is not applicable to CF34 turbofan engines with VG actuator shaft aft bearing support PN 5024T65G03 identified
with supplier code 56946 if the supports at both the 2:00 and 8:00 VG shaft locations have been identified with the rework "R" marking.)
Cat. 2 - RecommendedRE (-)72-0111 R00 ENGINE - Compressor Stator (72-32-00) - Inspection and Temporary Loctite Rework of VG Shaft Aft Bearing Support
Mos
Hrs
Enc
72 ENG2Eff: 02-Apr-2002
(NOTE: This Service Bulletin is not applicable to CF34 turbofan engines with VG actuator shaft aft bearing support PN 5024T65G03 identified
with supplier code 56946 if the supports at both the 2:00 and 8:00 VG shaft locations have been identified with the rework "R" marking.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM318/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 2 - RecommendedRE (-)72-0111 R01 ENGINE - Compressor Stator (72-32-00) - Inspection and Temporary Loctite Rework of VG Shaft Aft Bearing Support
Mos
Hrs
Enc
72 ENG1Eff: 03-Mar-2003
(NOTE: This Service Bulletin is not applicable to CF34 turbofan engines with VG actuator shaft aft bearing support PN 5024T65G03 identified
with supplier code 56946 if the supports at both the 2:00 and 8:00 VG shaft locations have been identified with the rework "R" marking.)
Cat. 2 - RecommendedRE (-)72-0111 R01 ENGINE - Compressor Stator (72-32-00) - Inspection and Temporary Loctite Rework of VG Shaft Aft Bearing Support
Mos
Hrs
Enc
72 ENG2Eff: 03-Mar-2003
(NOTE: This Service Bulletin is not applicable to CF34 turbofan engines with VG actuator shaft aft bearing support PN 5024T65G03 identified
with supplier code 56946 if the supports at both the 2:00 and 8:00 VG shaft locations have been identified with the rework "R" marking.)
Cat. 2 - RecommendedRE (-)72-0111 R02 ENGINE - Compressor Stator (72-32-00) - Inspection and Temporary Loctite Rework of VG Shaft Aft Bearing Support
Mos
Hrs
Enc
72 ENG1Eff: 06-May-2003
(NOTE: This Service Bulletin is not applicable to CF34 turbofan engines with VG actuator shaft aft bearing support PN 5024T65G03 identified
with supplier code 56946 if the supports at both the 2:00 and 8:00 VG shaft locations have been identified with the rework "R" marking.)
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Compressor Stator (72-32-00) - Replacement of VG Sh...72-0110 R01ENG172
Cat. 2 - RecommendedRE (-)72-0111 R02 ENGINE - Compressor Stator (72-32-00) - Inspection and Temporary Loctite Rework of VG Shaft Aft Bearing Support
Mos
Hrs
Enc
72 ENG2Eff: 06-May-2003
(NOTE: This Service Bulletin is not applicable to CF34 turbofan engines with VG actuator shaft aft bearing support PN 5024T65G03 identified
with supplier code 56946 if the supports at both the 2:00 and 8:00 VG shaft locations have been identified with the rework "R" marking.)
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Compressor Stator (72-32-00) - Replacement of VG Sh...72-0110 R01ENG272
Cat. 8 - InformationalRE (-)72-0112 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 28-Mar-2002
Cat. 8 - InformationalRE (-)72-0112 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 28-Mar-2002
Cat. 8 - InformationalT (A/R)72-0112 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 29-Apr-2002
Cat. 8 - InformationalT (A/R)72-0112 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 29-Apr-2002
Cat. 8 - InformationalT (A/R)72-0115 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 12-Jun-2002
Cat. 8 - InformationalT (A/R)72-0115 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 12-Jun-2002
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM319/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 8 - InformationalT (A/R)72-0116 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 23-Sep-2002
Cat. 8 - InformationalT (A/R)72-0116 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 23-Sep-2002
Cat. 7 - OptionalT (A/R)72-0120 R00 ENGINE - Compressor Rotor Components (72-33-00) - Introduction of Improved Stages 3 and 5 Compressor Rotor Locking Nut Halves
Mos
Hrs
Enc
72 ENG1Eff: 29-Jul-2002
Cat. 7 - OptionalT (A/R)72-0120 R00 ENGINE - Compressor Rotor Components (72-33-00) - Introduction of Improved Stages 3 and 5 Compressor Rotor Locking Nut Halves
Mos
Hrs
Enc
72 ENG2Eff: 29-Jul-2002
Cat. 8 - InformationalT (A/R)72-0121 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 14-Aug-2002
Cat. 8 - InformationalT (A/R)72-0121 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 14-Aug-2002
Cat. 8 - InformationalRE (-)72-0123 R00 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair
Mos
Hrs
Enc
72 ENG1Eff: 13-Dec-2002
Cat. 8 - InformationalRE (-)72-0123 R00 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair
Mos
Hrs
Enc
72 ENG2Eff: 13-Dec-2002
Cat. 7 - OptionalRE (-)72-0123 R01 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair
Mos
Hrs
Enc
72 ENG1Eff: 11-Aug-2008
Cat. 7 - OptionalRE (-)72-0123 R01 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair
Mos
Hrs
Enc
72 ENG2Eff: 11-Aug-2008
Cat. 7 - OptionalT (-)72-0123 R02 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair
Mos
Hrs
Enc
72 ENG1Eff: 05-Aug-2013
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM320/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 7 - OptionalT (-)72-0123 R02 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair
Mos
Hrs
Enc
72 ENG2Eff: 05-Aug-2013
Category 7T (-)72-0123 R03 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair
Mos
Hrs
Enc
72 ENG1Eff: 09-Apr-2015
Also ConsiderDUE:1. RE -ENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG172
Category 7T (-)72-0123 R03 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair
Mos
Hrs
Enc
72 ENG2Eff: 09-Apr-2015
Also ConsiderDUE: 6,914 Enc1. T 350 Enc | 2. RE 600 EncENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG272
Category 7T (A/R)72-0123 R04 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair
Mos
Hrs
Enc
72 ENG1Eff: 21-Oct-2015
Also ConsiderDUE:1. RE -ENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG172
Category 7T (A/R)72-0123 R04 ENGINE - General (72-00-00) - Introduction of Fan Blade Bushing Repair
Mos
Hrs
Enc
72 ENG2Eff: 21-Oct-2015
Also ConsiderDUE: 6,914 Enc1. T 350 Enc | 2. RE 600 EncENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG272
Cat. 9 - InformationalT (A/R)72-0124 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 07-Nov-2002
Cat. 9 - InformationalT (A/R)72-0124 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 07-Nov-2002
Cat. 7 - OptionalRE (-)72-0125 R00 ENGINE - Fan Rotor Assembly (72-33-00) - Rework of Fan Blades PN 6018T30P06 and PN 6018T30P13
Mos
Hrs
Enc
72 ENG1Eff: 03-Feb-2003
Cat. 7 - OptionalRE (-)72-0125 R00 ENGINE - Fan Rotor Assembly (72-33-00) - Rework of Fan Blades PN 6018T30P06 and PN 6018T30P13
Mos
Hrs
Enc
72 ENG2Eff: 03-Feb-2003
Cat. 7 - OptionalRE (-)72-0125 R01 ENGINE - Fan Rotor Assembly (72-33-00) - Rework of Fan Blades PN 6018T30P03 PN 6018T30P05 PN 6018T30P06 PN 6018T30P07 PN 6018T30P13 and PN
5922T34P01
Mos
Hrs
Enc
72 ENG1Eff: 19-Jun-2003
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM321/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 7 - OptionalRE (-)72-0125 R01 ENGINE - Fan Rotor Assembly (72-33-00) - Rework of Fan Blades PN 6018T30P03 PN 6018T30P05 PN 6018T30P06 PN 6018T30P07 PN 6018T30P13 and PN
5922T34P01
Mos
Hrs
Enc
72 ENG2Eff: 19-Jun-2003
Cat. 7 - OptionalT (A/R)72-0125 R02 ENGINE - Fan Rotor Assembly (72-21-00) - Rework of Fan Blades P/N 4923T56G02 P/N 4923T56G05 P/N 4923T56G07 P/N 4923T56G09 P/N 5922T34P01 P/N
6018T30P03 P/N 6018T30P06 and P/N 6018T30P13
Mos
Hrs
Enc
72 ENG1Eff: 09-Jan-2008
Cat. 7 - OptionalT (A/R)72-0125 R02 ENGINE - Fan Rotor Assembly (72-21-00) - Rework of Fan Blades P/N 4923T56G02 P/N 4923T56G05 P/N 4923T56G07 P/N 4923T56G09 P/N 5922T34P01 P/N
6018T30P03 P/N 6018T30P06 and P/N 6018T30P13
Mos
Hrs
Enc
72 ENG2Eff: 09-Jan-2008
Cat. 9 - InformationalRE (-)72-0126 R00 ENGINE - Fan Stator Assembly (72-23-00) - Rework of Fan Case Outer Spacers and Introduction of a New Aft Fan Case
Mos
Hrs
Enc
72 ENG1Eff: 03-Feb-2003
Cat. 9 - InformationalRE (-)72-0126 R00 ENGINE - Fan Stator Assembly (72-23-00) - Rework of Fan Case Outer Spacers and Introduction of a New Aft Fan Case
Mos
Hrs
Enc
72 ENG2Eff: 03-Feb-2003
Cat. 7 - OptionalT (A/R)72-0126 R01 ENGINE - Fan Stator Assembly (72-23-00) - Rework of Fan Case Outer Spacers and Introduction of a New Aft Fan Case
Mos
Hrs
Enc
72 ENG1Eff: 11-Mar-2003
Cat. 7 - OptionalT (A/R)72-0126 R01 ENGINE - Fan Stator Assembly (72-23-00) - Rework of Fan Case Outer Spacers and Introduction of a New Aft Fan Case
Mos
Hrs
Enc
72 ENG2Eff: 11-Mar-2003
Cat. 9 - InformationalRE (-)72-0127 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 02-Dec-2002
Cat. 9 - InformationalRE (-)72-0127 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 02-Dec-2002
Cat. 9 - InformationalT (A/R)72-0127 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 10-Dec-2002
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM322/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 9 - InformationalT (A/R)72-0127 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 10-Dec-2002
Cat. 7 - OptionalRE (-)72-0128 R00 ENGINE - Compressor Stator Assembly (72-32-00) - Introduction of New Stage 1 and Stage 2 Compressor Shroud Seals PN 5026T64G14 PN 5026T64G13 and PN
5026T62G11
Mos
Hrs
Enc
72 ENG1Eff: 17-Jan-2003
Cat. 7 - OptionalRE (-)72-0128 R00 ENGINE - Compressor Stator Assembly (72-32-00) - Introduction of New Stage 1 and Stage 2 Compressor Shroud Seals PN 5026T64G14 PN 5026T64G13 and PN
5026T62G11
Mos
Hrs
Enc
72 ENG2Eff: 17-Jan-2003
Cat. 7 - OptionalT (A/R)72-0128 R01 ENGINE - Compressor Stator Assembly (72-32-00) - Introduction of New Stage 1 and Stage 2 Compressor Shroud Seals PN 5026T64G14 PN 5026T64G13 and PN
5026T62G11
Mos
Hrs
Enc
72 ENG1Eff: 05-Feb-2007
Cat. 7 - OptionalT (A/R)72-0128 R01 ENGINE - Compressor Stator Assembly (72-32-00) - Introduction of New Stage 1 and Stage 2 Compressor Shroud Seals PN 5026T64G14 PN 5026T64G13 and PN
5026T62G11
Mos
Hrs
Enc
72 ENG2Eff: 05-Feb-2007
Cat. 9 - InformationalRE (-)72-0129 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 22-Dec-2002
Cat. 9 - InformationalRE (-)72-0129 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 22-Dec-2002
Cat. 8 - InformationalRE (-)72-0129 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 05-Apr-2006
Cat. 8 - InformationalRE (-)72-0129 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 05-Apr-2006
Cat. 8 - InformationalT (A/R)72-0129 R02 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 22-Jan-2008
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM323/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 8 - InformationalT (A/R)72-0129 R02 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 22-Jan-2008
Cat. 9 - InformationalT (A/R)72-0130 R00 ENGINE - General - Spare Parts Release for CF34 Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 06-Feb-2003
Cat. 9 - InformationalT (A/R)72-0130 R00 ENGINE - General - Spare Parts Release for CF34 Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 06-Feb-2003
Cat. 9 - InformationalT (A/R)72-0132 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 23-Feb-2003
Cat. 9 - InformationalT (A/R)72-0132 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 23-Feb-2003
Cat. 2 - RecommendedRE (-)72-0134 R01 ENGINE - Compressor Stator Assembly (72-32-00) - CF34 Compressor Variable Vane Actuating Arm Wear at the Compressor Splitline
Mos
Hrs
Enc
72 ENG1Eff: 27-Apr-2004
Cat. 2 - RecommendedRE (-)72-0134 R01 ENGINE - Compressor Stator Assembly (72-32-00) - CF34 Compressor Variable Vane Actuating Arm Wear at the Compressor Splitline
Mos
Hrs
Enc
72 ENG2Eff: 27-Apr-2004
Cat. 8 - InformationalT (A/R)72-0135 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 27-Jul-2003
Cat. 8 - InformationalT (A/R)72-0135 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 27-Jul-2003
Cat. 8 - InformationalT (A/R)72-0137 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 02-Sep-2003
Cat. 8 - InformationalT (A/R)72-0137 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 02-Sep-2003
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM324/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 8 - InformationalT (A/R)72-0139 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 30-Sep-2003
Cat. 8 - InformationalT (A/R)72-0139 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 30-Sep-2003
Cat. 8 - InformationalRE (-)72-0141 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3BTurbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 26-Oct-2003
Cat. 8 - InformationalRE (-)72-0141 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3BTurbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 26-Oct-2003
Cat. 8 - InformationalT (A/R)72-0141 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 20-Jan-2004
Cat. 8 - InformationalT (A/R)72-0141 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 20-Jan-2004
Cat. 9 - InformationalRE (-)72-0142 R00 ENGINE - Compressor Rotor (72-33-00) - Life Limited Stages 3 thru 8Compressor Rotor Spool PN 6078T56P05 Part Introduction
Mos
Hrs
Enc
72 ENG1Eff: 24-Nov-2003
Cat. 9 - InformationalRE (-)72-0142 R00 ENGINE - Compressor Rotor (72-33-00) - Life Limited Stages 3 thru 8Compressor Rotor Spool PN 6078T56P05 Part Introduction
Mos
Hrs
Enc
72 ENG2Eff: 24-Nov-2003
Cat. 9 - InformationalRE (-)72-0142 R01 ENGINE - Compressor Rotor (72-33-00) - Life Limited Stages 3 thru 8Compressor Rotor Spool PN 6078T56P05 Part Introduction
Mos
Hrs
Enc
72 ENG1Eff: 20-Jan-2004
Cat. 9 - InformationalRE (-)72-0142 R01 ENGINE - Compressor Rotor (72-33-00) - Life Limited Stages 3 thru 8Compressor Rotor Spool PN 6078T56P05 Part Introduction
Mos
Hrs
Enc
72 ENG2Eff: 20-Jan-2004
Cat. 9 - InformationalT (A/R)72-0142 R02 ENGINE - Compressor Rotor (72-33-00) - Life Limited Stages 3 thru 8 Compressor Rotor Spool PN 6078T56P05 Part Introduction
Mos
Hrs
Enc
72 ENG1Eff: 11-May-2004
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM325/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 9 - InformationalT (A/R)72-0142 R02 ENGINE - Compressor Rotor (72-33-00) - Life Limited Stages 3 thru 8 Compressor Rotor Spool PN 6078T56P05 Part Introduction
Mos
Hrs
Enc
72 ENG2Eff: 11-May-2004
Cat. 8 - InformationalT (A/R)72-0143 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 03-Dec-2003
Cat. 8 - InformationalT (A/R)72-0143 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 03-Dec-2003
Cat. 8 - InformationalT (A/R)72-0144 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 21-Dec-2003
Cat. 8 - InformationalT (A/R)72-0144 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 21-Dec-2003
Cat. 8 - InformationalRE (-)72-0145 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 25-Jan-2004
Cat. 8 - InformationalRE (-)72-0145 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 25-Jan-2004
Cat. 8 - InformationalT (A/R)72-0145 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 24-Feb-2004
Cat. 8 - InformationalT (A/R)72-0145 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 24-Feb-2004
Cat. 5 - RecommendedRE (-)72-0147 R00 ENGINE - Compressor Stator (72-32-00) - Removal of Inlet Guide Vane (IGV) and Stages 1 through 5 Self-Locking Nut PN 4037T84P03 (No Longer Valid)
Mos
Hrs
Enc
72 ENG1Eff: 30-Mar-2004
(NOTE: GE is requesting operators not to comply with this service bulletin)
Cat. 5 - RecommendedRE (-)72-0147 R00 ENGINE - Compressor Stator (72-32-00) - Removal of Inlet Guide Vane (IGV) and Stages 1 through 5 Self-Locking Nut PN 4037T84P03 (No Longer Valid)
Mos
Hrs
Enc
72 ENG2Eff: 30-Mar-2004
(NOTE: GE is requesting operators not to comply with this service bulletin)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM326/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 9 - InformationalT (A/R)72-0147 R01 ENGINE - Compressor Stator (72-32-00) - Removal of Inlet Guide Vane (IGV) and Stages 1 through 5 Self-Locking Nut PN 4037T84P03 (No Longer Valid)
Mos
Hrs
Enc
72 ENG1Eff: 01-Jun-2005
(NOTE: GE is requesting operators not to comply with this service bulletin)
Cat. 9 - InformationalT (A/R)72-0147 R01 ENGINE - Compressor Stator (72-32-00) - Removal of Inlet Guide Vane (IGV) and Stages 1 through 5 Self-Locking Nut PN 4037T84P03 (No Longer Valid)
Mos
Hrs
Enc
72 ENG2Eff: 01-Jun-2005
(NOTE: GE is requesting operators not to comply with this service bulletin)
Cat. 8 - InformationalT (A/R)72-0150 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 07-Apr-2004
Cat. 8 - InformationalT (A/R)72-0150 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 07-Apr-2004
Cat. 8 - InformationalT (A/R)72-0156 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 25-Apr-2004
Cat. 8 - InformationalT (A/R)72-0156 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 25-Apr-2004
Cat. 2 - RecommendedRE (-)72-0157 R00 ENGINE - Compressor Stator (72-32-00) - Stages IGV thru 5 Self-Locking Nut Field Inspection
Mos
Hrs
Enc
72 ENG1Eff: 02-Jun-2004
Cat. 2 - RecommendedRE (-)72-0157 R00 ENGINE - Compressor Stator (72-32-00) - Stages IGV thru 5 Self-Locking Nut Field Inspection
Mos
Hrs
Enc
72 ENG2Eff: 02-Jun-2004
Cat. 2 - RecommendedRE (-)72-0157 R01 ENGINE - Compressor Stator (72-32-00) - Stages IGV thru 5 Self-Locking Nut Field Inspection
Mos
Hrs
Enc
72 ENG1Eff: 18-Mar-2005
Cat. 2 - RecommendedRE (-)72-0157 R01 ENGINE - Compressor Stator (72-32-00) - Stages IGV thru 5 Self-Locking Nut Field Inspection
Mos
Hrs
Enc
72 ENG2Eff: 18-Mar-2005
Cat. 2 - RecommendedRE (-)72-0157 R02 ENGINE - Compressor Stator (72-32-00) - Stages IGV thru 5 Self-Locking Nut Field Inspection
Mos
Hrs
Enc
72 ENG1
(NOTE: GE recommends that all engines that have reused stages IGV thru 5 self-locking nuts, with a single tab engaged on the tab washer be
inspected within 4,000 flight hours time since overhaul (TSO).)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM327/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 2 - RecommendedRE (-)72-0157 R02 ENGINE - Compressor Stator (72-32-00) - Stages IGV thru 5 Self-Locking Nut Field Inspection
Mos
Hrs
Enc
72 ENG2
(NOTE: GE recommends that all engines that have reused stages IGV thru 5 self-locking nuts, with a single tab engaged on the tab washer be
inspected within 4,000 flight hours time since overhaul (TSO).)
Cat. 7 - OptionalRE (-)72-0160 R00 ENGINE ~ Low Pressure Turbine Rotor (72-53-00) - Life Limited Low Pressure Turbine Disks Stages 3 Thru 6 PN 6078T91P02 PN 6078T02P04 PN 6078T92P02 and PN
6078T89P03 Parts Introduction.
Mos
Hrs
Enc
72 ENG1Eff: 08-Sep-2004
Cat. 7 - OptionalRE (-)72-0160 R00 ENGINE ~ Low Pressure Turbine Rotor (72-53-00) - Life Limited Low Pressure Turbine Disks Stages 3 Thru 6 PN 6078T91P02 PN 6078T02P04 PN 6078T92P02 and PN
6078T89P03 Parts Introduction.
Mos
Hrs
Enc
72 ENG2Eff: 08-Sep-2004
Cat. 7 - OptionalT (A/R)72-0160 R01 ENGINE - Low Pressure Turbine Rotor (72-53-00) - Life Limited Low Pressure Turbine Disks Stages 3 Thru 6 PN 6078T91P02 PN 6078T02P04 PN 6078T92P02 and PN
6078T89P03 Parts Introduction.
Mos
Hrs
Enc
72 ENG1Eff: 21-Nov-2011
Cat. 7 - OptionalT (A/R)72-0160 R01 ENGINE - Low Pressure Turbine Rotor (72-53-00) - Life Limited Low Pressure Turbine Disks Stages 3 Thru 6 PN 6078T91P02 PN 6078T02P04 PN 6078T92P02 and PN
6078T89P03 Parts Introduction.
Mos
Hrs
Enc
72 ENG2Eff: 21-Nov-2011
Cat. 7 - OptionalT (A/R)72-0161 R00 ENGINE - High Pressure Turbine Stator (72-45-00) - Introduction of Reworked Stage 2 High Pressure Turbine Seal Shroud Segments PN 5902T33G01
Mos
Hrs
Enc
72 ENG1Eff: 09-Dec-2004
Cat. 7 - OptionalT (A/R)72-0161 R00 ENGINE - High Pressure Turbine Stator (72-45-00) - Introduction of Reworked Stage 2 High Pressure Turbine Seal Shroud Segments PN 5902T33G01
Mos
Hrs
Enc
72 ENG2Eff: 09-Dec-2004
Cat. 7 - OptionalT (A/R)72-0162 R00 ENGINE - High Pressure Turbine Stator (72-45-00) - Introduction of Reworked Stage 1 High Pressure Turbine Seal Shroud Segments PN 5902T32G01
Mos
Hrs
Enc
72 ENG1Eff: 09-Dec-2004
Cat. 7 - OptionalT (A/R)72-0162 R00 ENGINE - High Pressure Turbine Stator (72-45-00) - Introduction of Reworked Stage 1 High Pressure Turbine Seal Shroud Segments PN 5902T32G01
Mos
Hrs
Enc
72 ENG2Eff: 09-Dec-2004
Cat. 5 - RecommendedRE (-)72-0163 R00 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG1Eff: 18-Aug-2004
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM328/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 5 - RecommendedRE (-)72-0163 R00 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG2Eff: 18-Aug-2004
Cat. 5 - RecommendedRE (-)72-0163 R01 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG1Eff: 21-Oct-2004
Cat. 5 - RecommendedRE (-)72-0163 R01 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG2Eff: 21-Oct-2004
Cat. 5 - RecommendedRE (-)72-0163 R02 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG1Eff: 02-Dec-2004
Cat. 5 - RecommendedRE (-)72-0163 R02 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG2Eff: 02-Dec-2004
Cat. 5 - RecommendedRE (-)72-0163 R03 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG1Eff: 06-Jul-2005
Cat. 5 - RecommendedRE (-)72-0163 R03 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG2Eff: 06-Jul-2005
Cat. 5 - RecommendedRE (-)72-0163 R04 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG1Eff: 31-Aug-2005
Cat. 5 - RecommendedRE (-)72-0163 R04 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG2Eff: 31-Aug-2005
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM329/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 5 - RecommendedRE (-)72-0163 R05 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG1Eff: 15-Dec-2005
Cat. 5 - RecommendedRE (-)72-0163 R05 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG2Eff: 15-Dec-2005
Cat. 5 - RecommendedRE (-)72-0163 R06 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG1Eff: 31-Mar-2006
Cat. 5 - RecommendedRE (-)72-0163 R06 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG2Eff: 31-Mar-2006
Cat. 5 - RecommendedRE (-)72-0163 R07 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG1Eff: 07-Jun-2007
Cat. 5 - RecommendedRE (-)72-0163 R07 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG2Eff: 07-Jun-2007
Cat. 5 - RecommendedT (A/R)72-0163 R08 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG1Eff: 30-Jul-2008
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
Cat. 5 - RecommendedT (A/R)72-0163 R08 ENGINE - Power Takeoff Drive Assembly - (72-64-00) - Introduction of PTO Drive Assembly PN 6037T72G19 and Front Frame-to-PTO Oil Tube Assembly PN
6012T90G02
Mos
Hrs
Enc
72 ENG2Eff: 30-Jul-2008
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
Cat. 8 - InformationalT (A/R)72-0164 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 20-Jun-2004
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM330/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 8 - InformationalT (A/R)72-0164 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 20-Jun-2004
Cat. 8 - InformationalT (A/R)72-0165 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 25-Jul-2004
Cat. 8 - InformationalT (A/R)72-0165 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 25-Jul-2004
Cat. 7 - OptionalRE (-)72-0166 R00 ENGINE - High Pressure Turbine Rotor (72-46-00) - Introduction of Destructive Evaluation Method for Stage 1 High Pressure Turbine Blades
Mos
Hrs
Enc
72 ENG1Eff: 03-Nov-2004
Cat. 7 - OptionalRE (-)72-0166 R00 ENGINE - High Pressure Turbine Rotor (72-46-00) - Introduction of Destructive Evaluation Method for Stage 1 High Pressure Turbine Blades
Mos
Hrs
Enc
72 ENG2Eff: 03-Nov-2004
Cat. 7 - OptionalT (A/R)72-0166 R01 ENGINE - High Pressure Turbine Rotor (72-46-00) - Introduction of Destructive Evaluation Method for Stage 1 High Pressure Turbine Blades
Mos
Hrs
Enc
72 ENG1Eff: 26-Mar-2012
Cat. 7 - OptionalT (A/R)72-0166 R01 ENGINE - High Pressure Turbine Rotor (72-46-00) - Introduction of Destructive Evaluation Method for Stage 1 High Pressure Turbine Blades
Mos
Hrs
Enc
72 ENG2Eff: 26-Mar-2012
Cat. 8 - InformationalT (A/R)72-0170 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 22-Aug-2004
Cat. 8 - InformationalT (A/R)72-0170 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 22-Aug-2004
Cat. 7 - OptionalRE (-)72-0171 R00 ENGINE - Fan Stator Assembly (72-23-00) - Introduction of New No. 1 and 2 Bearing Housing Assembly PN 6047T69G04
Mos
Hrs
Enc
72 ENG1Eff: 20-Jan-2005
Cat. 7 - OptionalRE (-)72-0171 R00 ENGINE - Fan Stator Assembly (72-23-00) - Introduction of New No. 1 and 2 Bearing Housing Assembly PN 6047T69G04
Mos
Hrs
Enc
72 ENG2Eff: 20-Jan-2005
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM331/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 7 - OptionalT (A/R)72-0171 R01 ENGINE - Fan Stator Assembly (72-23-00) - Introduction of New No. 1 and 2 Bearing Housing Assembly PN 6047T69G04
Mos
Hrs
Enc
72 ENG1Eff: 15-Dec-2005
Cat. 7 - OptionalT (A/R)72-0171 R01 ENGINE - Fan Stator Assembly (72-23-00) - Introduction of New No. 1 and 2 Bearing Housing Assembly PN 6047T69G04
Mos
Hrs
Enc
72 ENG2Eff: 15-Dec-2005
Cat. 7 - OptionalRE (-)72-0172 R00 ENGINE - Low Pressure Turbine Stator Assembly (72-54-00) - Introduction of Stage 3 through 6 Shroud and Seal Sectors
Mos
Hrs
Enc
72 ENG1Eff: 02-Dec-2004
Cat. 7 - OptionalRE (-)72-0172 R00 ENGINE - Low Pressure Turbine Stator Assembly (72-54-00) - Introduction of Stage 3 through 6 Shroud and Seal Sectors
Mos
Hrs
Enc
72 ENG2Eff: 02-Dec-2004
Cat. 8 - InformationalT (A/R)72-0173 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 24-Oct-2004
Cat. 8 - InformationalT (A/R)72-0173 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 24-Oct-2004
Cat. 5 - RecommendedRE (-)72-0175 R00 ENGINE - Compressor Rotor (72-00-00) - Removal of the Stages 10 through 14 Compressor Rotor Spool PN 6037T83P03 PN 6037T83P04 and PN 6087T02P01
Mos
Hrs
Enc
72 ENG1Eff: 30-Mar-2005
(NOTE: GE recommends that you replace and discard the stages 10 through 14 compressor rotor spool PN 6037T83P03, PN 6037T83P04, and
PN 6087T02P01 when they are removed from the engine/module)
Cat. 5 - RecommendedRE (-)72-0175 R00 ENGINE - Compressor Rotor (72-00-00) - Removal of the Stages 10 through 14 Compressor Rotor Spool PN 6037T83P03 PN 6037T83P04 and PN 6087T02P01
Mos
Hrs
Enc
72 ENG2Eff: 30-Mar-2005
(NOTE: GE recommends that you replace and discard the stages 10 through 14 compressor rotor spool PN 6037T83P03, PN 6037T83P04, and
PN 6087T02P01 when they are removed from the engine/module)
Cat. 5 - RecommendedRE (-)72-0175 R01 ENGINE - Compressor Rotor (72-00-00) - Removal of the Stages 10 through 14 Compressor Rotor Spool PN 6037T83P03 PN 6037T83P04 and PN 6087T02P01
Mos
Hrs
Enc
72 ENG1Eff: 15-Dec-2005
(NOTE: GE recommends that you replace and discard the stages 10 through 14 compressor rotor spool PN 6037T83P03, PN 6037T83P04, and
PN 6087T02P01 when they are removed from the engine/module)
Cat. 5 - RecommendedRE (-)72-0175 R01 ENGINE - Compressor Rotor (72-00-00) - Removal of the Stages 10 through 14 Compressor Rotor Spool PN 6037T83P03 PN 6037T83P04 and PN 6087T02P01
Mos
Hrs
Enc
72 ENG2Eff: 15-Dec-2005
(NOTE: GE recommends that you replace and discard the stages 10 through 14 compressor rotor spool PN 6037T83P03, PN 6037T83P04, and
PN 6087T02P01 when they are removed from the engine/module)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM332/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 3 - RecommendedT (A/R)72-0175 R02 ENGINE - Compressor Rotor (72-00-00) - Removal of the Stages 10 through 14 Compressor Rotor Spool PN 6037T83P03 PN 6037T83P04 and PN 6087T02P01
Mos
Hrs
Enc
72 ENG1Eff: 29-May-2012
(NOTE: GE recommends that you replace and discard the stages 10 through 14 compressor rotor spool PN 6037T83P03, PN 6037T83P04, and
PN 6087T02P01 when they are removed from the engine/module)
Cat. 3 - RecommendedT (A/R)72-0175 R02 ENGINE - Compressor Rotor (72-00-00) - Removal of the Stages 10 through 14 Compressor Rotor Spool PN 6037T83P03 PN 6037T83P04 and PN 6087T02P01
Mos
Hrs
Enc
72 ENG2Eff: 29-May-2012
(NOTE: GE recommends that you replace and discard the stages 10 through 14 compressor rotor spool PN 6037T83P03, PN 6037T83P04, and
PN 6087T02P01 when they are removed from the engine/module)
Cat. 4 - RecommendedRE (-)72-0176 R00 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of No. 5 Roller Bearings PN 5042T13P04 PN 5042T13P05 PN 5022T87P04 and PN
5022T87P05
Mos
Hrs
Enc
72 ENG1Eff: 17-Dec-2004
Cat. 4 - RecommendedRE (-)72-0176 R00 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of No. 5 Roller Bearings PN 5042T13P04 PN 5042T13P05 PN 5022T87P04 and PN
5022T87P05
Mos
Hrs
Enc
72 ENG2Eff: 17-Dec-2004
Cat. 4 - RecommendedRE (-)72-0176 R01 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of No. 5 Roller Bearings PN 5042T13P04 PN 5042T13P05 PN 5022T87P04 and PN
5022T87P05
Mos
Hrs
Enc
72 ENG1Eff: 18-Feb-2005
Cat. 4 - RecommendedRE (-)72-0176 R01 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of No. 5 Roller Bearings PN 5042T13P04 PN 5042T13P05 PN 5022T87P04 and PN
5022T87P05
Mos
Hrs
Enc
72 ENG2Eff: 18-Feb-2005
Cat. 4 - RecommendedRE (-)72-0176 R02 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of No. 5 Roller Bearings PN 5042T13P04 PN 5042T13P05 PN 5022T87P04 and PN
5022T87P05
Mos
Hrs
Enc
72 ENG1Eff: 06-Apr-2005
Cat. 4 - RecommendedRE (-)72-0176 R02 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of No. 5 Roller Bearings PN 5042T13P04 PN 5042T13P05 PN 5022T87P04 and PN
5022T87P05
Mos
Hrs
Enc
72 ENG2Eff: 06-Apr-2005
Cat. 4 - RecommendedRE (-)72-0176 R03 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of No. 5 Roller Bearings PN 5042T13P04 PN 5042T13P05 PN 5022T87P04 and PN
5022T87P05
Mos
Hrs
Enc
72 ENG1Eff: 15-Dec-2005
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM333/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 4 - RecommendedRE (-)72-0176 R03 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of No. 5 Roller Bearings PN 5042T13P04 PN 5042T13P05 PN 5022T87P04 and PN
5022T87P05
Mos
Hrs
Enc
72 ENG2Eff: 15-Dec-2005
Cat. 4 - RecommendedT (A/R)72-0176 R04 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of No. 5 Roller Bearings PN 5042T13P04 PN 5042T13P05 PN 5022T87P04 and PN
5022T87P05
Mos
Hrs
Enc
72 ENG1Eff: 10-Jul-2006
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
Cat. 4 - RecommendedT (A/R)72-0176 R04 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of No. 5 Roller Bearings PN 5042T13P04 PN 5042T13P05 PN 5022T87P04 and PN
5022T87P05
Mos
Hrs
Enc
72 ENG2Eff: 10-Jul-2006
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
Cat. 8 - InformationalT (A/R)72-0177 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2 Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 30-Jan-2005
Cat. 8 - InformationalT (A/R)72-0177 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2 Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 30-Jan-2005
Cat. 5 - RecommendedRE (-)72-0179 R00 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud PN 5026T65G06
Mos
Hrs
Enc
72 ENG1Eff: 06-Apr-2005
(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned
IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the
IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is
removed from the engine.)
Cat. 5 - RecommendedRE (-)72-0179 R00 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud PN 5026T65G06
Mos
Hrs
Enc
72 ENG2Eff: 06-Apr-2005
(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned
IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the
IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is
removed from the engine.)
Cat. 5 - RecommendedRE (-)72-0179 R01 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud PN 5026T65G06
Mos
Hrs
Enc
72 ENG1Eff: 24-May-2005
(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned
IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the
IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is
removed from the engine.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM334/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 5 - RecommendedRE (-)72-0179 R01 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud PN 5026T65G06
Mos
Hrs
Enc
72 ENG2Eff: 24-May-2005
(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned
IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the
IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is
removed from the engine.)
Cat. 5 - RecommendedRE (-)72-0179 R02 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud PN 5026T65G06
Mos
Hrs
Enc
72 ENG1Eff: 15-Dec-2005
(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned
IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the
IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is
removed from the engine.)
Cat. 5 - RecommendedRE (-)72-0179 R02 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud PN 5026T65G06
Mos
Hrs
Enc
72 ENG2Eff: 15-Dec-2005
(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned
IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the
IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is
removed from the engine.)
Cat. 5 - RecommendedRE (-)72-0179 R03 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud PN 5026T65G06
Mos
Hrs
Enc
72 ENG1Eff: 08-Aug-2006
(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned
IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the
IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is
removed from the engine.)
Cat. 5 - RecommendedRE (-)72-0179 R03 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud PN 5026T65G06
Mos
Hrs
Enc
72 ENG2Eff: 08-Aug-2006
(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned
IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the
IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is
removed from the engine.)
Cat. 5 - RecommendedRE (-)72-0179 R04 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud PN 5026T65G06
Mos
Hrs
Enc
72 ENG1Eff: 07-Sep-2007
(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned
IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the
IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is
removed from the engine.)
Cat. 5 - RecommendedRE (-)72-0179 R04 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud PN 5026T65G06
Mos
Hrs
Enc
72 ENG2Eff: 07-Sep-2007
(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned
IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the
IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is
removed from the engine.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM335/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 5 - RecommendedRE (-)72-0179 R05 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud PN 5026T65G06
Mos
Hrs
Enc
72 ENG1Eff: 01-Jul-2008
(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned
IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the
IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is
removed from the engine.)
Cat. 5 - RecommendedRE (-)72-0179 R05 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud PN 5026T65G06
Mos
Hrs
Enc
72 ENG2Eff: 01-Jul-2008
(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned
IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the
IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is
removed from the engine.)
Cat. 3 - RecommendedRE (-)72-0179 R06 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud P/N 5026T65G06
Mos
Hrs
Enc
72 ENG1Eff: 20-Sep-2010
(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned
IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the
IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is
removed from the engine.)
Cat. 3 - RecommendedRE (-)72-0179 R06 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud P/N 5026T65G06
Mos
Hrs
Enc
72 ENG2Eff: 20-Sep-2010
(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned
IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the
IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is
removed from the engine.)
Cat. 3 - RecommendedT (A/R)72-0179 R07 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud P/N 5026T65G06
Mos
Hrs
Enc
72 ENG1Eff: 04-Apr-2011
(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned
IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the
IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is
removed from the engine.)
Cat. 3 - RecommendedT (A/R)72-0179 R07 ENGINE - Compressor Stator (72-32-00) - Introduction of a New Redesigned IGV Inner Support Shroud P/N 5026T65G06
Mos
Hrs
Enc
72 ENG2Eff: 04-Apr-2011
(NOTE: For CF34-3B engines: Category 3GE recommends that the IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned
IGV inner support shroud P/N 5026T65G06 at next engine shop visit.For CF34-1A and CF34-3A engines: Category 5GE recommends that the
IGV inner support shroud P/N 5026T65G05 be replaced with the redesigned IGV inner support shroud P/N 5026T65G06 when the part is
removed from the engine.)
Cat. 7 - OptionalRE (-)72-0181 R04 ENGINE - High Pressure Turbine Stator (72-45-00) - Introduction of N2 Alloy Stage 1 HP Turbine Shrouds Shroud Hangers Segment Seals
Mos
Hrs
Enc
72 ENG1Eff: 20-Aug-2008
Cat. 7 - OptionalRE (-)72-0181 R04 ENGINE - High Pressure Turbine Stator (72-45-00) - Introduction of N2 Alloy Stage 1 HP Turbine Shrouds Shroud Hangers Segment Seals
Mos
Hrs
Enc
72 ENG2Eff: 20-Aug-2008
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM336/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 7 - OptionalRE (-)72-0181 R05 ENGINE - High Pressure Turbine Stator (72-45-00) - Introduction of N2 Alloy Stage 1 HP Turbine Shrouds Shroud Hangers Segment Seals
Mos
Hrs
Enc
72 ENG1Eff: 24-Jun-2014
Cat. 7 - OptionalRE (-)72-0181 R05 ENGINE - High Pressure Turbine Stator (72-45-00) - Introduction of N2 Alloy Stage 1 HP Turbine Shrouds Shroud Hangers Segment Seals
Mos
Hrs
Enc
72 ENG2Eff: 24-Jun-2014
Cat. 6 - RecommendedRE (-)72-0182 R00 ENGINE - Combustion Liner Assembly (72-41-00) - Combustion Liner Field Modification and Repair Configuration
Mos
Hrs
Enc
72 ENG1Eff: 09-Feb-2006
Cat. 6 - RecommendedRE (-)72-0182 R00 ENGINE - Combustion Liner Assembly (72-41-00) - Combustion Liner Field Modification and Repair Configuration
Mos
Hrs
Enc
72 ENG2Eff: 09-Feb-2006
Cat. 6 - RecommendedRE (-)72-0182 R01 ENGINE - Combustion Liner Assembly (72-41-00) - Combustion Liner Field Modification and Repair Configuration
Mos
Hrs
Enc
72 ENG1Eff: 30-Mar-2006
Cat. 6 - RecommendedRE (-)72-0182 R01 ENGINE - Combustion Liner Assembly (72-41-00) - Combustion Liner Field Modification and Repair Configuration
Mos
Hrs
Enc
72 ENG2Eff: 30-Mar-2006
Cat. 6 - RecommendedRE (-)72-0182 R02 ENGINE - Combustion Liner Assembly (72-41-00) - Combustion Liner Field Modification and Repair Configuration
Mos
Hrs
Enc
72 ENG1Eff: 18-May-2006
Cat. 6 - RecommendedRE (-)72-0182 R02 ENGINE - Combustion Liner Assembly (72-41-00) - Combustion Liner Field Modification and Repair Configuration
Mos
Hrs
Enc
72 ENG2Eff: 18-May-2006
Cat. 6 - RecommendedT (A/R)72-0182 R03 ENGINE - Combustion Liner Assembly (72-41-00) - Combustion Liner Field Modification and Repair Configuration
Mos
Hrs
Enc
72 ENG1Eff: 22-Jun-2006
Cat. 6 - RecommendedT (A/R)72-0182 R03 ENGINE - Combustion Liner Assembly (72-41-00) - Combustion Liner Field Modification and Repair Configuration
Mos
Hrs
Enc
72 ENG2Eff: 22-Jun-2006
Cat. 8 - InformationalRE (-)72-0184 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 29-May-2005
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM337/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 8 - InformationalRE (-)72-0184 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 29-May-2005
Cat. 8 - InformationalT (A/R)72-0184 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 15-Aug-2007
Cat. 8 - InformationalT (A/R)72-0184 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 15-Aug-2007
Cat. 6 - RecommendedT (A/R)72-0185 R00 ENGINE - Combustion Chamber Frame and B-Sump Assembly (72-41-00) - Introduction of Reworked B-Sump Housing PN 4923T00G01
Mos
Hrs
Enc
72 ENG1Eff: 29-Sep-2005
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
Cat. 6 - RecommendedT (A/R)72-0185 R00 ENGINE - Combustion Chamber Frame and B-Sump Assembly (72-41-00) - Introduction of Reworked B-Sump Housing PN 4923T00G01
Mos
Hrs
Enc
72 ENG2Eff: 29-Sep-2005
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
Cat. 8 - InformationalT (A/R)72-0188 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 28-Aug-2005
Cat. 8 - InformationalT (A/R)72-0188 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 28-Aug-2005
Cat. 8 - InformationalRE (-)72-0189 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 25-Oct-2005
Cat. 8 - InformationalRE (-)72-0189 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 25-Oct-2005
Cat. 8 - InformationalT (A/R)72-0189 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 11-May-2006
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM338/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 8 - InformationalT (A/R)72-0189 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 11-May-2006
Cat. 5 - RecommendedRE (-)72-0190 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Carbon Seals PNs 5018T49P05 5016T32P05 and 4138T09P03
Mos
Hrs
Enc
72 ENG1Eff: 22-Nov-2005
Cat. 5 - RecommendedRE (-)72-0190 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Carbon Seals PNs 5018T49P05 5016T32P05 and 4138T09P03
Mos
Hrs
Enc
72 ENG2Eff: 22-Nov-2005
Cat. 5 - RecommendedRE (-)72-0190 R01 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Carbon Seals PNs 4138T09P02 4138T09P03 5016T32P05 5016T32P06 5018T48P04
5018T48P05 5018T49P05 and 5018T49P06
Mos
Hrs
Enc
72 ENG1Eff: 14-Jun-2007
Cat. 5 - RecommendedRE (-)72-0190 R01 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Carbon Seals PNs 4138T09P02 4138T09P03 5016T32P05 5016T32P06 5018T48P04
5018T48P05 5018T49P05 and 5018T49P06
Mos
Hrs
Enc
72 ENG2Eff: 14-Jun-2007
Cat. 5 - RecommendedRE (-)72-0190 R02 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Carbon Seals PNs 4138T09P02 4138T09P03 5016T32P05 5016T32P06 5018T48P04
5018T48P05 5018T49P05 and 5018T49P06
Mos
Hrs
Enc
72 ENG1Eff: 03-Jan-2008
Cat. 5 - RecommendedRE (-)72-0190 R02 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Carbon Seals PNs 4138T09P02 4138T09P03 5016T32P05 5016T32P06 5018T48P04
5018T48P05 5018T49P05 and 5018T49P06
Mos
Hrs
Enc
72 ENG2Eff: 03-Jan-2008
Cat. 5 - RecommendedRE (-)72-0190 R03 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Carbon Seals PNs 4138T09P02 4138T09P03 5016T32P05 5016T32P06 5018T48P04
5018T48P05 5018T49P05 and 5018T49P06
Mos
Hrs
Enc
72 ENG1Eff: 20-Aug-2008
Cat. 5 - RecommendedT (A/R)72-0190 R03 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of AGB Carbon Seals PNs 4138T09P02 4138T09P03 5016T32P05 5016T32P06 5018T48P04
5018T48P05 5018T49P05 and 5018T49P06
Mos
Hrs
Enc
72 ENG2Eff: 20-Aug-2008
Cat. 2 - RecommendedRE (-)72-0193 R00 ENGINE - Compressor Stator Assembly (72-32-00) - Inspection of HPC Stage 2 VG Turnbuckles
25-Jul-2008Mos
11,528.2Hrs
6,334Enc
72 ENG1Complied With
(NOTE: GE recommends that you do this Service Bulletin as soon as possible without effect on revenue service but within 2,500 cycles since
last shop visit. If over 2,500 cycles since last shop visit or within 250 cycles since issuance of this Service Bulletin for ESNs affected)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM339/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 2 - RecommendedRE (-)72-0193 R00 ENGINE - Compressor Stator Assembly (72-32-00) - Inspection of HPC Stage 2 VG Turnbuckles
25-Jul-2008Mos
11,411.2Hrs
6,293Enc
72 ENG2Eff: 18-May-2006 Not Applicable
Cat. 7 - OptionalRE (-)72-0195 R00 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2 Model Engine
Mos
Hrs
Enc
72 ENG1Eff: 09-Jun-2006
Cat. 7 - OptionalRE (-)72-0195 R00 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2 Model Engine
Mos
Hrs
Enc
72 ENG2Eff: 09-Jun-2006
Cat. 7 - OptionalRE (-)72-0195 R01 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG1Eff: 16-Feb-2010
Cat. 7 - OptionalRE (-)72-0195 R01 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG2Eff: 16-Feb-2010
Cat. 7 - OptionalRE (-)72-0195 R02 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG1Eff: 21-Apr-2010
Cat. 7 - OptionalRE (-)72-0195 R02 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG2Eff: 21-Apr-2010
Cat. 7 - OptionalRE (-)72-0195 R03 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG1Eff: 18-Aug-2010
Cat. 7 - OptionalRE (-)72-0195 R03 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG2Eff: 18-Aug-2010
Cat. 7 - OptionalRE (-)72-0195 R04 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG1Eff: 06-Apr-2011
Cat. 7 - OptionalRE (-)72-0195 R04 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG2Eff: 06-Apr-2011
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM340/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 7 - OptionalRE (-)72-0195 R05 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG1Eff: 31-Oct-2011
Cat. 7 - OptionalRE (-)72-0195 R05 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG2Eff: 31-Oct-2011
Cat. 7 - OptionalRE (-)72-0195 R06 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG1Eff: 09-Feb-2012
Cat. 7 - OptionalRE (-)72-0195 R06 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG2Eff: 09-Feb-2012
Cat. 7 - OptionalRE (-)72-0195 R07 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG1Eff: 29-Aug-2012
Cat. 7 - OptionalRE (-)72-0195 R07 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG2Eff: 29-Aug-2012
Cat. 7 - OptionalRE (-)72-0195 R08 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG1Eff: 16-Jul-2013
Cat. 7 - OptionalRE (-)72-0195 R08 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG2Eff: 16-Jul-2013
Category 7RE (-)72-0195 R09 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG1Eff: 10-Feb-2015
(AVG MAN HRS: 200)
Category 7RE (-)72-0195 R09 ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A Model Engines to CF34-3A2
Mos
Hrs
Enc
72 ENG2Eff: 10-Feb-2015
(AVG MAN HRS: 200)
Cat. 8 - InformationalT (A/R)72-0196 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 30-Apr-2006
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM341/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 8 - InformationalT (A/R)72-0196 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 30-Apr-2006
Cat. 5 - RecommendedRE (-)72-0197 R00 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retain Ring PN AS3217-127
Mos
Hrs
Enc
72 ENG1Eff: 12-Jun-2006
Cat. 5 - RecommendedRE (-)72-0197 R00 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retain Ring PN AS3217-127
Mos
Hrs
Enc
72 ENG2Eff: 12-Jun-2006
Cat. 5 - RecommendedRE (-)72-0197 R01 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retain Ring PN AS3217-127
Mos
Hrs
Enc
72 ENG1Eff: 12-Oct-2006
Cat. 5 - RecommendedRE (-)72-0197 R01 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retain Ring PN AS3217-127
Mos
Hrs
Enc
72 ENG2Eff: 12-Oct-2006
Cat. 5 - RecommendedRE (-)72-0197 R02 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retain Ring PN AS3217-127
Mos
Hrs
Enc
72 ENG1Eff: 10-Apr-2007
Cat. 5 - RecommendedRE (-)72-0197 R02 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retain Ring PN AS3217-127
Mos
Hrs
Enc
72 ENG2Eff: 10-Apr-2007
Cat. 5 - RecommendedT (-)72-0197 R03 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retainer Ring PN AS3217-127
Mos
Hrs
Enc
72 ENG1Eff: 11-Aug-2008
Cat. 5 - RecommendedT (-)72-0197 R03 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retainer Ring PN AS3217-127
Mos
Hrs
Enc
72 ENG2Eff: 11-Aug-2008
Cat. 5 - RecommendedRE (-)72-0197 R04 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retainer Ring PN AS3217-127
Mos
Hrs
Enc
72 ENG1Eff: 08-Jan-2015
Cat. 5 - RecommendedT (-)72-0197 R04 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retainer Ring PN AS3217-127
Mos
Hrs
Enc
72 ENG2Eff: 08-Jan-2015
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM342/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 5 - RecommendedRE (-)72-0197 R05 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retainer Ring PN AS3217-127
Mos
Hrs
Enc
72 ENG1Eff: 01-Jun-2015
Cat. 5 - RecommendedT (A/R)72-0197 R05 ENGINE - Accessory Drive Section (72-62-00) - Introduction of Improved Accessory Gear Box Axis K Cranking Plug PN 4189T24G01 and Retainer Ring PN AS3217-127
Mos
Hrs
Enc
72 ENG2Eff: 01-Jun-2015
Cat. 8 - InformationalT (A/R)72-0198 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 28-May-2006
Cat. 8 - InformationalT (A/R)72-0198 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 28-May-2006
Cat. 6 - RecommendedRE (-)72-0201 R00 ENGINE - (72-42-00) - Rework of the Stage 1 HPT Nozzle Support
Mos
Hrs
Enc
72 ENG1Eff: 13-Apr-2007
Cat. 6 - RecommendedRE (-)72-0201 R00 ENGINE - (72-42-00) - Rework of the Stage 1 HPT Nozzle Support
Mos
Hrs
Enc
72 ENG2Eff: 13-Apr-2007
Cat. 6 - RecommendedT (A/R)72-0201 R01 ENGINE - (72-42-00) - Rework of the Stage 1 HPT Nozzle Support
Mos
Hrs
Enc
72 ENG1Eff: 16-Nov-2007
Cat. 6 - RecommendedT (A/R)72-0201 R01 ENGINE - (72-42-00) - Rework of the Stage 1 HPT Nozzle Support
Mos
Hrs
Enc
72 ENG2Eff: 16-Nov-2007
Cat. 7 - OptionalRE (-)72-0203 R00 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Stage 3 Shroud Sector PN 5099T32G02 for CF34-3A1 Engine Models
Mos
Hrs
Enc
72 ENG1Eff: 04-Oct-2006
Cat. 7 - OptionalRE (-)72-0203 R00 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Stage 3 Shroud Sector PN 5099T32G02 for CF34-3A1 Engine Models
Mos
Hrs
Enc
72 ENG2Eff: 04-Oct-2006
Cat. 7 - OptionalRE (-)72-0203 R01 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Stage 3 Shroud Sector PN 5099T32G02 for CF34-3A1 Engine Models
Mos
Hrs
Enc
72 ENG1Eff: 26-Jan-2007
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM343/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 7 - OptionalRE (-)72-0203 R01 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Stage 3 Shroud Sector PN 5099T32G02 for CF34-3A1 Engine Models
Mos
Hrs
Enc
72 ENG2Eff: 26-Jan-2007
Cat. 7 - OptionalRE (-)72-0203 R02 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Stage 3 Shroud Sector PN 5099T32G02 for CF34-3A1 Engine Models
Mos
Hrs
Enc
72 ENG1Eff: 11-Apr-2007
Cat. 7 - OptionalRE (-)72-0203 R02 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Stage 3 Shroud Sector PN 5099T32G02 for CF34-3A1 Engine Models
Mos
Hrs
Enc
72 ENG2Eff: 11-Apr-2007
Cat. 7 - OptionalRE (-)72-0203 R03 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Stage 3 Shroud Sector PN 5099T32G02 PN 6020T00G04 and PN 6020T00G06 for use on
CF34-1A/-3A/-3A2/-3A1 Engine Models.
Mos
Hrs
Enc
72 ENG1Eff: 20-May-2009
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - I...72-0241 R01ENG172
Cat. 7 - OptionalRE (-)72-0203 R03 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Stage 3 Shroud Sector PN 5099T32G02 PN 6020T00G04 and PN 6020T00G06 for use on
CF34-1A/-3A/-3A2/-3A1 Engine Models.
Mos
Hrs
Enc
72 ENG2Eff: 20-May-2009
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - I...72-0241 R01ENG272
Cat. 7 - OptionalRE (-)72-0204 R00 ENGINE - Turbine Transition Assembly (72-51-00) - Rework of HPT Stator Components for Borescope Capability
Mos
Hrs
Enc
72 ENG1Eff: 05-Jan-2007
Cat. 7 - OptionalRE (-)72-0204 R00 ENGINE - Turbine Transition Assembly (72-51-00) - Rework of HPT Stator Components for Borescope Capability
Mos
Hrs
Enc
72 ENG2Eff: 05-Jan-2007
Cat. 7 - OptionalT (A/R)72-0204 R01 ENGINE - Turbine Transition Assembly (72-51-00) - Rework of HPT Stator Components for Borescope Capability
Mos
Hrs
Enc
72 ENG1Eff: 02-Aug-2007
Cat. 7 - OptionalT (A/R)72-0204 R01 ENGINE - Turbine Transition Assembly (72-51-00) - Rework of HPT Stator Components for Borescope Capability
Mos
Hrs
Enc
72 ENG2Eff: 02-Aug-2007
Cat. 8 - InformationalRE (-)72-0205 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 27-Aug-2006
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM344/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 8 - InformationalRE (-)72-0205 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 27-Aug-2006
Cat. 8 - InformationalRE (-)72-0205 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 15-Oct-2008
Cat. 8 - InformationalRE (-)72-0205 R01 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 15-Oct-2008
Cat. 8 - InformationalT (A/R)72-0205 R02 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 08-Feb-2013
Cat. 8 - InformationalT (A/R)72-0205 R02 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 08-Feb-2013
Cat. 7 - OptionalRE (-)72-0206 R00 ENGINE - High Pressure Turbine Stator Assembly (72-45-00) - Introduction of Alternate Blind Rivets to Replace Aft Flange Gang Channels
Mos
Hrs
Enc
72 ENG1Eff: 21-Nov-2006
Cat. 7 - OptionalRE (-)72-0206 R00 ENGINE - High Pressure Turbine Stator Assembly (72-45-00) - Introduction of Alternate Blind Rivets to Replace Aft Flange Gang Channels
Mos
Hrs
Enc
72 ENG2Eff: 21-Nov-2006
Cat. 7 - OptionalT (A/R)72-0206 R01 ENGINE - High Pressure Turbine Stator Assembly (72-45-00) - Introduction of Alternate Blind Rivets to Replace Aft Flange Gang Channels
Mos
Hrs
Enc
72 ENG1Eff: 02-Jun-2009
Cat. 7 - OptionalT (A/R)72-0206 R01 ENGINE - High Pressure Turbine Stator Assembly (72-45-00) - Introduction of Alternate Blind Rivets to Replace Aft Flange Gang Channels
Mos
Hrs
Enc
72 ENG2Eff: 02-Jun-2009
Cat. 8 - InformationalT (A/R)72-0207 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 26-Nov-2006
Cat. 8 - InformationalT (A/R)72-0207 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 26-Nov-2006
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM345/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 3 - Recommended ≈21-Apr-2047T72-0209 R00 ENGINE - Fan Rotor (72-21-00) - Introduction of a Redesigned Fan Blade Retaining Pin
Mos
Hrs
11,231 Enc18,00018,000Enc
72 ENG1
(NOTE: GE recommends if the engine is over 18,000 cycles to replace with the new fan blade retaining pins at the next shop visit.)
Cat. 3 - Recommended ≈02-Jun-2047T72-0209 R00 ENGINE - Fan Rotor (72-21-00) - Introduction of a Redesigned Fan Blade Retaining Pin
Mos
Hrs
11,272 Enc18,00018,000Enc
72 ENG2
(NOTE: GE recommends if the engine is over 18,000 cycles to replace with the new fan blade retaining pins at the next shop visit.)
Cat. 8 - InformationalT (A/R)72-0210 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 15-Feb-2007
Cat. 8 - InformationalT (A/R)72-0210 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 15-Feb-2007
Cat. 7 - OptionalT (A/R)72-0214 R00 ENGINE - Fan Rotor Assembly and Components (72-21-00) - Introduction of Spiral Painting to the Forward Outer Spinner
Mos
Hrs
Enc
72 ENG1Eff: 05-May-2008
Cat. 7 - OptionalT (A/R)72-0214 R00 ENGINE - Fan Rotor Assembly and Components (72-21-00) - Introduction of Spiral Painting to the Forward Outer Spinner
Mos
Hrs
Enc
72 ENG2Eff: 05-May-2008
Cat. 3 - RecommendedRE (-)72-0215 R00 ENGINE - Fan Rotor Assembly (72-21-00) - ECI Inspection of Fan Blade Pin Hole
Mos
Hrs
Enc
72 ENG1Eff: 14-Jun-2007
(NOTE: Inspection recommended anytime fan blades are in for shop visit, provided blades have been in service 3,000 cycles or more since
prior shop visit inspection.)
Cat. 3 - RecommendedRE (-)72-0215 R00 ENGINE - Fan Rotor Assembly (72-21-00) - ECI Inspection of Fan Blade Pin Hole
Mos
Hrs
Enc
72 ENG2Eff: 14-Jun-2007
(NOTE: Inspection recommended anytime fan blades are in for shop visit, provided blades have been in service 3,000 cycles or more since
prior shop visit inspection.)
Cat. 3 - RecommendedRE (-)72-0215 R01 ENGINE - Fan Rotor Assembly (72-21-00) - ECI Inspection of Fan Blade Pin Hole
25-Jul-2008Mos
11,411.2Hrs
6,293Enc
72 ENG2BY PART S/N INSTALLEDEff: 07-Aug-2007 Not
Applicable
(NOTE: Inspection recommended anytime fan blades are in for shop visit, provided blades have been in service 3,000 cycles or more since
prior shop visit inspection.)
Cat. 3 - RecommendedRE (-)72-0215 R01 ENGINE - Fan Rotor Assembly (72-21-00) - ECI Inspection of Fan Blade Pin Hole
Mos
Hrs
Enc
72 ENG1Eff: 07-Aug-2007
(NOTE: Inspection recommended anytime fan blades are in for shop visit, provided blades have been in service 3,000 cycles or more since
prior shop visit inspection.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM346/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 3 - RecommendedT (-)72-0215 R02 ENGINE - Fan Rotor Assembly (72-21-00) - ECI Inspection of Fan Blade Pin Hole
Mos
Hrs
Enc
72 ENG1Eff: 01-Jun-2011
(NOTE: Inspection recommended anytime fan blades are in for shop visit, provided blades have been in service 3,000 cycles or more since
prior shop visit inspection.)
Cat. 3 - RecommendedT (-)72-0215 R02 ENGINE - Fan Rotor Assembly (72-21-00) - ECI Inspection of Fan Blade Pin Hole
Mos
Hrs
Enc
72 ENG2Eff: 01-Jun-2011
(NOTE: Inspection recommended anytime fan blades are in for shop visit, provided blades have been in service 3,000 cycles or more since
prior shop visit inspection.)
Category 3T (A/R)72-0215 R03 ENGINE - Fan Rotor Assembly (72-21-00) - ECI Inspection of Fan Blade Pin Hole
Mos
Hrs
Enc
72 ENG1Eff: 14-Apr-2015
(AVG MAN HRS: 7) (NOTE: The fan blades P/N 6018T30P14 with serial numbers (S/N) thatstart with "MAE" are affected by this Service Bulletin)
Also ConsiderDUE:1. RE -ENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG172
Category 3T (A/R)72-0215 R03 ENGINE - Fan Rotor Assembly (72-21-00) - ECI Inspection of Fan Blade Pin Hole
Mos
Hrs
Enc
72 ENG2Eff: 14-Apr-2015
(AVG MAN HRS: 7) (NOTE: The fan blades P/N 6018T30P14 with serial numbers (S/N) thatstart with "MAE" are affected by this Service Bulletin)
Also ConsiderDUE: 6,914 Enc1. T 350 Enc | 2. RE 600 EncENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG272
Cat. 8 - InformationalT (A/R)72-0216 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 27-May-2007
Cat. 8 - InformationalT (A/R)72-0216 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 27-May-2007
Cat. 5 - RecommendedRE (-)72-0217 R00 ENGINE - (72-42-00) - Rework of the Air Balance Piston Stationary Seal
Mos
Hrs
Enc
72 ENG1Eff: 27-Jul-2007
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - (72-42-00) - Rework of the Stage 1 HPT Nozzle Suppo...72-0201 R01ENG172
Cat. 5 - RecommendedT (A/R)72-0217 R00 ENGINE - (72-42-00) - Rework of the Air Balance Piston Stationary Seal
Mos
Hrs
Enc
72 ENG2Eff: 27-Jul-2007
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - (72-42-00) - Rework of the Stage 1 HPT Nozzle Suppo...72-0201 R01ENG272
Cat. 8 - InformationalT (A/R)72-0218 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 23-Sep-2007
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM347/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 8 - InformationalT (A/R)72-0218 R00 ENGINE - General - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 23-Sep-2007
Cat. 8 - InformationalT (A/R)72-0219 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Engines
Mos
Hrs
Enc
72 ENG1Eff: 28-Oct-2007
Cat. 8 - InformationalT (A/R)72-0219 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Engines
Mos
Hrs
Enc
72 ENG2Eff: 28-Oct-2007
Cat. 7 - OptionalRE (-)72-0221 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Introduction of Fan Blade P/N 6018T30P15
Mos
Hrs
Enc
72 ENG1Eff: 07-Jan-2008
Cat. 7 - OptionalRE (-)72-0221 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Introduction of Fan Blade P/N 6018T30P15
Mos
Hrs
Enc
72 ENG2Eff: 07-Jan-2008
Cat. 7 - OptionalRE (-)72-0221 R01 ENGINE - Fan Rotor Assembly (72-21-00) - Introduction of Fan Blade P/N 6018T30P15
Mos
Hrs
Enc
72 ENG1Eff: 30-Jan-2009
Cat. 7 - OptionalT (A/R)72-0221 R01 ENGINE - Fan Rotor Assembly (72-21-00) - Introduction of Fan Blade P/N 6018T30P15
Mos
Hrs
Enc
72 ENG2Eff: 30-Jan-2009
Cat. 7 - OptionalRE (-)72-0222 R00 ENGINE - General - Introduction of a New Hydraulic Drain Line
Mos
Hrs
Enc
72 ENG1Eff: 09-Jan-2008
Cat. 7 - OptionalRE (-)72-0222 R00 ENGINE - General - Introduction of a New Hydraulic Drain Line
Mos
Hrs
Enc
72 ENG2Eff: 09-Jan-2008
Cat. 7 - OptionalRE (-)72-0222 R01 ENGINE - General - Introduction of a New Hydraulic Drain Line
Mos
Hrs
Enc
72 ENG1Eff: 12-Jul-2011
Cat. 7 - OptionalRE (-)72-0222 R01 ENGINE - General - Introduction of a New Hydraulic Drain Line
Mos
Hrs
Enc
72 ENG2Eff: 12-Jul-2011
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM348/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 7 - OptionalRE (-)72-0222 R02 ENGINE - General - Introduction of a New Hydraulic Drain Line
Mos
Hrs
Enc
72 ENG1Eff: 11-May-2013
Cat. 7 - OptionalRE (-)72-0222 R02 ENGINE - General - Introduction of a New Hydraulic Drain Line
Mos
Hrs
Enc
72 ENG2Eff: 11-May-2013
Cat. 8 - InformationalT (A/R)72-0223 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Engines
Mos
Hrs
Enc
72 ENG1Eff: 23-Dec-2007
Cat. 8 - InformationalT (A/R)72-0223 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Engines
Mos
Hrs
Enc
72 ENG2Eff: 23-Dec-2007
Cat. 8 - InformationalT (A/R)72-0224 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2 Engines
Mos
Hrs
Enc
72 ENG1Eff: 08-Feb-2008
Cat. 8 - InformationalT (A/R)72-0224 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2 Engines
Mos
Hrs
Enc
72 ENG2Eff: 08-Feb-2008
Cat. 3 - RecommendedT (A/R)72-0225 R00 ENGINE - Compressor Rotor Assembly (72-33-00) - Reblade of Engines Shipped with Non-Standard Stage 9 Compressor Blade Count
Mos
Hrs
Enc
72 ENG1Eff: 11-Feb-2008
(NOTE: THIS SERVICE BULLETIN IS FOR LIMITED DISTRIBUTION)
Cat. 3 - RecommendedT (A/R)72-0225 R00 ENGINE - Compressor Rotor Assembly (72-33-00) - Reblade of Engines Shipped with Non-Standard Stage 9 Compressor Blade Count
Mos
Hrs
Enc
72 ENG2Eff: 11-Feb-2008
(NOTE: THIS SERVICE BULLETIN IS FOR LIMITED DISTRIBUTION)
Cat. 8 - InformationalT (A/R)72-0226 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Engines
Mos
Hrs
Enc
72 ENG1Eff: 10-Mar-2008
Cat. 8 - InformationalT (A/R)72-0226 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Engines
Mos
Hrs
Enc
72 ENG2Eff: 10-Mar-2008
Cat. 8 - InformationalT (A/R)72-0227 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A2 Engines
Mos
Hrs
Enc
72 ENG1Eff: 11-Mar-2008
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM349/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 8 - InformationalT (A/R)72-0227 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A2 Engines
Mos
Hrs
Enc
72 ENG2Eff: 11-Mar-2008
Cat. 8 - InformationalT (A/R)72-0228 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Engines
Mos
Hrs
Enc
72 ENG1Eff: 28-Mar-2008
Cat. 8 - InformationalT (A/R)72-0228 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Engines
Mos
Hrs
Enc
72 ENG2Eff: 28-Mar-2008
Cat. 2 - RecommendedRE (-)72-0229 R00 ENGINE - Fan Rotor (72-21-00) - Field Management Program of Fan Blades P/N 6018T30P14 Made From VSMPO Mill Source Material
25-Jul-2008Mos
11,528.2Hrs
6,334Enc
72 ENG1BY PART S/N INSTALLEDEff: 10-Apr-2008 Not
Applicable
(NOTE: If the CSN on the part reaches 1,200 CSN prior to completing the ECI per this Service Bulletin, it is recommended that a visual
inspection of the fan containment case abradable rub strip be completed at repeat intervals as described in CF34-BJ S/B 72-0231 until the ECI
or fan blade replacement can be complied with. It does not apply to field modified fan blades P/N 4923T56G08, even if the serial number is
listed in paragraph 4., APPENDIX A and paragraph 5., APPENDIX B. Refer to CF34-BJ S/B 72-0230 for these blades.)
Cat. 2 - RecommendedRE (-)72-0229 R00 ENGINE - Fan Rotor (72-21-00) - Field Management Program of Fan Blades P/N 6018T30P14 Made From VSMPO Mill Source Material
Mos
Hrs
Enc
72 ENG2Eff: 10-Apr-2008
(NOTE: If the CSN on the part reaches 1,200 CSN prior to completing the ECI per this Service Bulletin, it is recommended that a visual
inspection of the fan containment case abradable rub strip be completed at repeat intervals as described in CF34-BJ S/B 72-0231 until the ECI
or fan blade replacement can be complied with. It does not apply to field modified fan blades P/N 4923T56G08, even if the serial number is
listed in paragraph 4., APPENDIX A and paragraph 5., APPENDIX B. Refer to CF34-BJ S/B 72-0230 for these blades.)
Cat. 2 - Recommended ≈16-Aug-2016RE72-0229 R01 ENGINE - Fan Rotor (72-21-00) - Field Management Program of Fan Blades P/N 6018T30P14 Made From VSMPO Mill Source Material
20-May-2009Mos
11,437.8Hrs
186 Enc6,9146006,314Enc
72 ENG2BY PART NUMBER INSTALLEDEff: 10-Apr-2008 Not
Applicable
(NOTE: If the CSN on the part reaches 1,200 CSN prior to completing the ECI per this Service Bulletin, it is recommended that a visual
inspection of the fan containment case abradable rub strip be completed at repeat intervals as described in CF34-BJ S/B 72-0231 until the ECI
or fan blade replacement can be complied with. It does not apply to field modified fan blades P/N 4923T56G08, even if the serial number is
listed in paragraph 4., APPENDIX A and paragraph 5., APPENDIX B. Refer to CF34-BJ S/B 72-0230 for these blades.)
Cat. 2 - RecommendedRE (-)72-0229 R01 ENGINE - Fan Rotor (72-21-00) - Field Management Program of Fan Blades P/N 6018T30P14 Made From VSMPO Mill Source Material
Mos
Hrs
Enc
72 ENG1Eff: 30-Jul-2008
Cat. 2 - RecommendedRE (-)72-0230 R00 ENGINE - Fan Rotor (72-21-00) - Field Management Program of Fan Blades P/N 4923T56G08 Made From VSMPO Mill Source Material
20-May-2009Mos
11,437.8Hrs
6,314Enc
72 ENG2BY PART NUMBER INSTALLEDEff: 10-Apr-2008 Not
Applicable
Cat. 2 - RecommendedRE (-)72-0230 R00 ENGINE - Fan Rotor (72-21-00) - Field Management Program of Fan Blades P/N 4923T56G08 Made From VSMPO Mill Source Material
25-Jul-2008Mos
11,528.2Hrs
6,334Enc
72 ENG1BY PART S/N INSTALLEDEff: 10-Apr-2008 Not
Applicable
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM350/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 2 - Recommended ≈31-Mar-2018T72-0230 R01 ENGINE - Fan Rotor (72-21-00) - Field Management Program of Fan Blades P/N 4923T56G08 Made From VSMPO Mill Source Material
Mos
Hrs
770 Enc≈7,5391,200Enc
72 ENG1Eff: 30-Jul-2008
(NOTE: GE recommends that you do this Service Bulletin without effect on revenue service as close as possible, but prior to 1,200 additional
flight cycles from when the pinhole bushing was installed.)
Also ConsiderDUE:1. RE -ENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG172
Cat. 2 - Recommended ≈31-Mar-2018T72-0230 R01 ENGINE - Fan Rotor (72-21-00) - Field Management Program of Fan Blades P/N 4923T56G08 Made From VSMPO Mill Source Material
Mos
Hrs
770 Enc≈7,4981,200Enc
72 ENG2Eff: 30-Jul-2008
(NOTE: GE recommends that you do this Service Bulletin without effect on revenue service as close as possible, but prior to 1,200 additional
flight cycles from when the pinhole bushing was installed.)
Also ConsiderDUE: 6,914 Enc1. T 350 Enc | 2. RE 600 EncENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG272
Cat. 2 - RecommendedRE (-)72-0231 R00 ENGINE - Fan Stator (72-23-00) - Visual Inspection of Fan Case Abradable Rub Strip for Fan Blade Tip Contact
Mos
Hrs
Enc
72 ENG1Eff: 31-Jul-2008
Cat. 2 - RecommendedRE (-)72-0231 R00 ENGINE - Fan Stator (72-23-00) - Visual Inspection of Fan Case Abradable Rub Strip for Fan Blade Tip Contact
Mos
Hrs
Enc
72 ENG2Eff: 31-Jul-2008
Cat. 2 - RecommendedRE (-)72-0231 R01 ENGINE - Fan Stator (72-23-00) - Visual Inspection of Fan Case Abradable Rub Strip for Fan Blade Tip Contact
Mos
Hrs
Enc
72 ENG1Eff: 01-Oct-2008
Cat. 2 - RecommendedRE (-)72-0231 R01 ENGINE - Fan Stator (72-23-00) - Visual Inspection of Fan Case Abradable Rub Strip for Fan Blade Tip Contact
Mos
Hrs
Enc
72 ENG2Eff: 01-Oct-2008
Cat. 2 - RecommendedRE (-)72-0231 R02 ENGINE - Fan Stator (72-23-00) - Visual Inspection of Fan Case Abradable Rub Strip for Fan Blade Tip Contact
20-May-2009Mos
11,437.8Hrs
6,314Enc
72 ENG2Eff: 26-Nov-2008 Not Applicable
Also ConsiderDUE: 6,914 Enc1. T 350 Enc | 2. RE 600 EncENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG272
Cat. 2 - RecommendedRE (-)72-0231 R02 ENGINE - Fan Stator (72-23-00) - Visual Inspection of Fan Case Abradable Rub Strip for Fan Blade Tip Contact
25-Jul-2008Mos
11,528.2Hrs
6,334Enc
72 ENG1BY PART S/N INSTALLEDEff: 26-Nov-2008 Not
Applicable
Also ConsiderDUE:1. RE -ENGINE - Fan Rotor (72-21-00) - Field Management Program of ...72-0229 R01ENG172
Cat. 8 - InformationalT (A/R)72-0232 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A Engines
Mos
Hrs
Enc
72 ENG1Eff: 19-Aug-2008
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM351/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 8 - InformationalT (A/R)72-0232 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A Engines
Mos
Hrs
Enc
72 ENG2Eff: 19-Aug-2008
Cat. 8 - InformationalRE (-)72-0236 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Engines
Mos
Hrs
Enc
72 ENG1Eff: 03-Oct-2008
Cat. 8 - InformationalRE (-)72-0236 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Engines
Mos
Hrs
Enc
72 ENG2Eff: 03-Oct-2008
Cat. 8 - InformationalT (A/R)72-0236 R01 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Engines
Mos
Hrs
Enc
72 ENG1Eff: 16-Oct-2008
Cat. 8 - InformationalT (A/R)72-0236 R01 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Engines
Mos
Hrs
Enc
72 ENG2Eff: 16-Oct-2008
Cat. 8 - InformationalT (A/R)72-0237 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A2/-3B Engines
Mos
Hrs
Enc
72 ENG1Eff: 14-Oct-2008
Cat. 8 - InformationalT (A/R)72-0237 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A2/-3B Engines
Mos
Hrs
Enc
72 ENG2Eff: 14-Oct-2008
Cat. 2 - RecommendedRE (-)72-0238 R00 ENGINE - Compressor Rotor Assembly (72-33-00) - Stages 3 through 8 Compressor Rotor Spool - Field Management Plan Due to Quality Issue
Mos
Hrs
Enc
72 ENG1Eff: 16-Jan-2009
Cat. 2 - RecommendedRE (-)72-0238 R00 ENGINE - Compressor Rotor Assembly (72-33-00) - Stages 3 through 8 Compressor Rotor Spool - Field Management Plan Due to Quality Issue
Mos
Hrs
Enc
72 ENG2Eff: 16-Jan-2009
Cat. 7 - OptionalT (A/R)72-0240 R00 ENGINE - Combustion Liner Assembly (72-42-00) - Introduction of Combustor Inner Liner
Mos
Hrs
Enc
72 ENG1Eff: 08-Jun-2009
Cat. 7 - OptionalT (A/R)72-0240 R00 ENGINE - Combustion Liner Assembly (72-42-00) - Introduction of Combustor Inner Liner
Mos
Hrs
Enc
72 ENG2Eff: 08-Jun-2009
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM352/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 7 - OptionalRE (-)72-0241 R00 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Shroud Sector Part Numbers for Stage 4 and Stage 5
Mos
Hrs
Enc
72 ENG1Eff: 20-May-2009
Cat. 7 - OptionalRE (-)72-0241 R00 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Shroud Sector Part Numbers for Stage 4 and Stage 5
Mos
Hrs
Enc
72 ENG2Eff: 20-May-2009
Cat. 7 - OptionalT (A/R)72-0241 R01 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Shroud Sector Part Numbers for Stage 4 and Stage 5
Mos
Hrs
Enc
72 ENG1Eff: 15-Jan-2013
Cat. 7 - OptionalT (A/R)72-0241 R01 ENGINE - Low Pressure Turbine Stator Assembly (72-52-00) - Introduction of Shroud Sector Part Numbers for Stage 4 and Stage 5
Mos
Hrs
Enc
72 ENG2Eff: 15-Jan-2013
Cat. 8 - InformationalT (A/R)72-0242 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Engines
Mos
Hrs
Enc
72 ENG1Eff: 03-Mar-2009
Cat. 8 - InformationalT (A/R)72-0242 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Engines
Mos
Hrs
Enc
72 ENG2Eff: 03-Mar-2009
Cat. 8 - InformationalT (A/R)72-0243 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Engines
Mos
Hrs
Enc
72 ENG1Eff: 17-Jun-2009
Cat. 8 - InformationalT (A/R)72-0243 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A1/-3A2/-3B Engines
Mos
Hrs
Enc
72 ENG2Eff: 17-Jun-2009
Cat. 8 - InformationalT (A/R)72-0246 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A2 Engines
Mos
Hrs
Enc
72 ENG1Eff: 24-Aug-2009
Cat. 8 - InformationalT (A/R)72-0246 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-1A/-3A/-3A2 Engines
Mos
Hrs
Enc
72 ENG2Eff: 24-Aug-2009
Cat. 7 - OptionalRE (-)72-0247 R00 ENGINE - Compressor Stator - Introduction of New VG Spindle Nut P/N 4037T84P04
Mos
Hrs
Enc
72 ENG1Eff: 24-Mar-2010
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM353/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 7 - OptionalRE (-)72-0247 R00 ENGINE - Compressor Stator - Introduction of New VG Spindle Nut P/N 4037T84P04
Mos
Hrs
Enc
72 ENG2Eff: 24-Mar-2010
Cat. 7 - OptionalRE (-)72-0247 R01 ENGINE - Compressor Stator - Introduction of New VG Spindle Nut P/N 4037T84P04
Mos
Hrs
Enc
72 ENG1Eff: 20-Jul-2010
Cat. 7 - OptionalRE (-)72-0247 R01 ENGINE - Compressor Stator - Introduction of New VG Spindle Nut P/N 4037T84P04
Mos
Hrs
Enc
72 ENG2Eff: 20-Jul-2010
Cat. 8 - InformationalT (A/R)72-0249 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Engines
Mos
Hrs
Enc
72 ENG1Eff: 10-Aug-2010
Cat. 8 - InformationalT (A/R)72-0249 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Engines
Mos
Hrs
Enc
72 ENG2Eff: 10-Aug-2010
Cat. 2 - RecommendedRE (-)72-0250 R00 ENGINE - Fan Rotor (72-21-00) - Replacement of Fan Blades P/N 6018T30P14 or P/N 4923T56G08 Made from ALLVAC Mill Source Material
Mos
Hrs
Enc
72 ENG1Eff: 30-Aug-2010
Cat. 2 - RecommendedRE (-)72-0250 R00 ENGINE - Fan Rotor (72-21-00) - Replacement of Fan Blades P/N 6018T30P14 or P/N 4923T56G08 Made from ALLVAC Mill Source Material
Mos
Hrs
Enc
72 ENG2Eff: 30-Aug-2010
Cat. 2 - RecommendedRE (-)72-0250 R01 ENGINE - Fan Rotor (72-21-00) - Replacement of Fan Blades P/N 6018T30P14 or P/N 4923T56G08 Made from ALLVAC Mill Source Material
03-Dec-2015Mos
12,115.2Hrs
6,751Enc
72 ENG1Eff: 01-Sep-2010 Complied With
Cat. 2 - RecommendedRE (-)72-0250 R01 ENGINE - Fan Rotor (72-21-00) - Replacement of Fan Blades P/N 6018T30P14 or P/N 4923T56G08 Made from ALLVAC Mill Source Material
03-Dec-2015Mos
11,998.2Hrs
6,710Enc
72 ENG2Eff: 01-Sep-2010 Complied With
Cat. 7 - OptionalRE (-)72-0251 R00 ENGINE - Compressor Rotor (72-33-00) - Inspection for Part Number Remarking and Introduction of Stage 1 Compressor Rotor Blisk P/N 5087T84P02
Mos
Hrs
Enc
72 ENG1Eff: 24-Jan-2011
Cat. 7 - OptionalRE (-)72-0251 R00 ENGINE - Compressor Rotor (72-33-00) - Inspection for Part Number Remarking and Introduction of Stage 1 Compressor Rotor Blisk P/N 5087T84P02
Mos
Hrs
Enc
72 ENG2Eff: 24-Jan-2011
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM354/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 7 - OptionalRE (-)72-0251 R01 ENGINE - Compressor Rotor (72-33-00) - Inspection for Part Number Remarking and Introduction of Stage 1 Compressor Rotor Blisk P/N 5087T84P02
Mos
Hrs
Enc
72 ENG1Eff: 23-Feb-2011
Cat. 7 - OptionalRE (-)72-0251 R01 ENGINE - Compressor Rotor (72-33-00) - Inspection for Part Number Remarking and Introduction of Stage 1 Compressor Rotor Blisk P/N 5087T84P02
Mos
Hrs
Enc
72 ENG2Eff: 23-Feb-2011
Cat. 7 - OptionalRE (-)72-0251 R02 ENGINE - Compressor Rotor (72-33-00) - Inspection for Part Number Remarking and Introduction of Stage 1 Compressor Rotor Blisk P/N 5087T84P02
Mos
Hrs
Enc
72 ENG1Eff: 14-Apr-2011
Cat. 7 - OptionalRE (-)72-0251 R02 ENGINE - Compressor Rotor (72-33-00) - Inspection for Part Number Remarking and Introduction of Stage 1 Compressor Rotor Blisk P/N 5087T84P02
Mos
Hrs
Enc
72 ENG2Eff: 14-Apr-2011
Cat. 6 - RecommendedRE (-)72-0252 R00 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of Improved No. 5 Roller Bearing P/N 5042T13P06
Mos
Hrs
Enc
72 ENG1Eff: 31-Mar-2011
Cat. 6 - RecommendedRE (-)72-0252 R00 ENGINE - Combustion Chamber Frame and B-Sump (72-41-00) - Introduction of Improved No. 5 Roller Bearing P/N 5042T13P06
Mos
Hrs
Enc
72 ENG2Eff: 31-Mar-2011
Cat. 8 - InformationalT (A/R)72-0253 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 04-May-2011
Cat. 8 - InformationalT (A/R)72-0253 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 04-May-2011
Cat. 9 - InformationalT (A/R)72-0254 R00 ENGINE - General (72-00-00) - CF34-BJ Engine Serialization - Manufacturing Sequence
Mos
Hrs
Enc
72 ENG1Eff: 09-Sep-2011
Cat. 9 - InformationalT (A/R)72-0254 R00 ENGINE - General (72-00-00) - CF34-BJ Engine Serialization - Manufacturing Sequence
Mos
Hrs
Enc
72 ENG2Eff: 09-Sep-2011
Cat. 3 - RecommendedRE (-)72-0256 R00 ENGINE - Stages IGV Through 13 Compressor Stator (72-32-00) - Introduction of Redesigned Pinned IGV Inner Support Shroud IGV Outer Bushing IGV Bushing and
IGV Upper and Lower Shroud Ring Segments
Mos
Hrs
Enc
72 ENG1Eff: 13-Apr-2012
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM355/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 3 - RecommendedRE (-)72-0256 R00 ENGINE - Stages IGV Through 13 Compressor Stator (72-32-00) - Introduction of Redesigned Pinned IGV Inner Support Shroud IGV Outer Bushing IGV Bushing and
IGV Upper and Lower Shroud Ring Segments
Mos
Hrs
Enc
72 ENG2Eff: 13-Apr-2012
Cat. 3 - RecommendedRE (-)72-0256 R01 ENGINE - Stages IGV Through 13 Compressor Stator (72-32-00) - Introduction of Redesigned Pinned IGV Inner Support Shroud IGV Outer Bushing IGV Bushing and
IGV Upper and Lower Shroud Ring Segments
Mos
Hrs
Enc
72 ENG1Eff: 05-Nov-2013
Cat. 3 - RecommendedRE (-)72-0256 R01 ENGINE - Stages IGV Through 13 Compressor Stator (72-32-00) - Introduction of Redesigned Pinned IGV Inner Support Shroud IGV Outer Bushing IGV Bushing and
IGV Upper and Lower Shroud Ring Segments
Mos
Hrs
Enc
72 ENG2Eff: 05-Nov-2013
Cat. 5 - RecommendedT (A/R)72-0258 R00 ENGINE - Fan Stator (72-23-00) - Introduction of New Shim P/N 2448M31P01
Mos
Hrs
Enc
72 ENG1Eff: 30-Jul-2012
Cat. 5 - RecommendedT (A/R)72-0258 R00 ENGINE - Fan Stator (72-23-00) - Introduction of New Shim P/N 2448M31P01
Mos
Hrs
Enc
72 ENG2Eff: 30-Jul-2012
Cat. 8 - InformationalT (A/R)72-0259 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 17-May-2013
Cat. 8 - InformationalT (A/R)72-0259 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 17-May-2013
Cat. 7 - OptionalRE (-)72-0260 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of Alternate Accessory Gearbox Assembly Hardware
Mos
Hrs
Enc
72 ENG1Eff: 16-Jan-2013
Cat. 7 - OptionalRE (-)72-0260 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of Alternate Accessory Gearbox Assembly Hardware
Mos
Hrs
Enc
72 ENG2Eff: 16-Jan-2013
Cat. 7 - OptionalRE (-)72-0260 R01 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of Alternate Accessory Gearbox Assembly Hardware
Mos
Hrs
Enc
72 ENG1Eff: 19-Apr-2013
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM356/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 7 - OptionalRE (-)72-0260 R01 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of Alternate Accessory Gearbox Assembly Hardware
Mos
Hrs
Enc
72 ENG2Eff: 19-Apr-2013
Cat. 7 - OptionalRE (-)72-0260 R02 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of Alternate Accessory Gearbox Assembly Hardware
Mos
Hrs
Enc
72 ENG1Eff: 19-Aug-2013
Cat. 7 - OptionalRE (-)72-0260 R02 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of Alternate Accessory Gearbox Assembly Hardware
Mos
Hrs
Enc
72 ENG2Eff: 19-Aug-2013
Cat. 7 - OptionalRE (-)72-0260 R03 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of Alternate Accessory Gearbox Assembly Hardware
Mos
Hrs
Enc
72 ENG1Eff: 04-Oct-2013
Cat. 7 - OptionalRE (-)72-0260 R03 ENGINE - Accessory Gearbox Assembly (72-62-00) - Introduction of Alternate Accessory Gearbox Assembly Hardware
Mos
Hrs
Enc
72 ENG2Eff: 04-Oct-2013
Category 7T (A/R)72-0263 R00 ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2 Engines from a Scheduled Interval Maintenance Plan to a Combined Scheduled Interval and Task
Oriented Maintenance Plan
Mos
Hrs
Enc
72 ENG1Eff: 08-Apr-2013
Category 7T (A/R)72-0263 R00 ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2 Engines from a Scheduled Interval Maintenance Plan to a Combined Scheduled Interval and Task
Oriented Maintenance Plan
Mos
Hrs
Enc
72 ENG2Eff: 08-Apr-2013
Category 7RE (-)72-0263 R01 ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2 Engines from a Scheduled Interval Maintenance Plan to a Combined Scheduled Interval and Task
Oriented Maintenance Plan
Mos
Hrs
Enc
72 ENG1Eff: 25-Nov-2014
(AVG MAN HRS: 1)
Category 7RE (-)72-0263 R01 ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2 Engines from a Scheduled Interval Maintenance Plan to a Combined Scheduled Interval and Task
Oriented Maintenance Plan
Mos
Hrs
Enc
72 ENG2Eff: 25-Nov-2014
(AVG MAN HRS: 1)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM357/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Category 7T (A/R)72-0263 R02 ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2 Engines from a Scheduled Interval Maintenance Plan to a Combined Scheduled Interval and Task
Oriented Maintenance Plan
Mos
Hrs
Enc
72 ENG1Eff: 27-Jan-2015
(AVG MAN HRS: 60)
Also ConsiderDUE:1. RE -ENGINE - Power Take off (PTO) Drive Assembly: Increased Torq...72-0013 R00ENG172
Also ConsiderDUE:1. RE -ENGINE - Rework of the Forward Fan Shaft72-0016 R02ENG172
Also ConsiderDUE:1. RE -ENGINE - Power Takeoff (PTO) Drive Assembly: Replacement of ...72-0021 R02ENG172
Also ConsiderDUE:1. RE -FUEL SYSTEM - Accessory Drive Gearbox (AGB) - Replacement of...72-0057 R03ENG172
Category 7T (A/R)72-0263 R02 ENGINE - General (72-00-00) - Change of CF34-3A and CF34-3A2 Engines from a Scheduled Interval Maintenance Plan to a Combined Scheduled Interval and Task
Oriented Maintenance Plan
Mos
Hrs
Enc
72 ENG2Eff: 27-Jan-2015
(AVG MAN HRS: 60)
Also ConsiderDUE:1. RE -ENGINE - Power Take off (PTO) Drive Assembly: Increased Torq...72-0013 R00ENG272
Also ConsiderDUE:1. RE -ENGINE - Rework of the Forward Fan Shaft72-0016 R02ENG272
Also ConsiderDUE:1. RE -ENGINE - Power Takeoff (PTO) Drive Assembly: Replacement of ...72-0021 R02ENG272
Also ConsiderDUE:1. RE -FUEL SYSTEM - Accessory Drive Gearbox (AGB) - Replacement of...72-0057 R03ENG272
Cat. 9 - InformationalT (A/R)72-0265 R00 ENGINE - Fan Stator (72-23-00) - Patent Plates Deleted from CF34-BJ (SEI-581) IPC
Mos
Hrs
Enc
72 ENG1Eff: 19-Apr-2013
Cat. 9 - InformationalT (A/R)72-0265 R00 ENGINE - Fan Stator (72-23-00) - Patent Plates Deleted from CF34-BJ (SEI-581) IPC
Mos
Hrs
Enc
72 ENG2Eff: 19-Apr-2013
Cat. 9 - InformationalT (A/R)72-0266 R00 ENGINE - High Pressure Turbine Rotor (72-46-00) - Part Usage Clarification
Mos
Hrs
Enc
72 ENG1Eff: 04-Oct-2013
Cat. 9 - InformationalT (A/R)72-0266 R00 ENGINE - High Pressure Turbine Rotor (72-46-00) - Part Usage Clarification
Mos
Hrs
Enc
72 ENG2Eff: 04-Oct-2013
Cat. 2 - RecommendedRE (-)72-0270 R00 ENGINE - Fan Stator Assembly (72-00-23) - Forward Mount Rib Inspection
Mos
Hrs
Enc
72 ENG1Eff: 20-Aug-2013
(NOTE: This Service Bulletin is applicable to all CF34-BJ engines that have been removed from wing at least one time.)
Cat. 2 - RecommendedRE (-)72-0270 R00 ENGINE - Fan Stator Assembly (72-00-23) - Forward Mount Rib Inspection
Mos
Hrs
Enc
72 ENG2Eff: 20-Aug-2013
(NOTE: This Service Bulletin is applicable to all CF34-BJ engines that have been removed from wing at least one time.)
Cat. 2 - RecommendedRE (-)72-0270 R01 ENGINE - Fan Stator Assembly (72-00-23) - Forward Mount Rib Inspection
Mos
Hrs
Enc
72 ENG1Eff: 05-Nov-2013
(NOTE: This Service Bulletin is applicable to all CF34-BJ engines that have been removed from wing at least one time.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM358/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 2 - RecommendedRE (-)72-0270 R01 ENGINE - Fan Stator Assembly (72-00-23) - Forward Mount Rib Inspection
Mos
Hrs
Enc
72 ENG2Eff: 05-Nov-2013
(NOTE: This Service Bulletin is applicable to all CF34-BJ engines that have been removed from wing at least one time.)
Cat. 2 - RecommendedT (-)72-0270 R02 ENGINE - Fan Stator Assembly (72-00-23) - Forward Mount Rib Inspection
Mos
Hrs
Enc
72 ENG1Eff: 15-Apr-2014
(NOTE: This Service Bulletin is applicable to all CF34-BJ engines that have been removed from wing at least one time.)
Cat. 2 - RecommendedT (-)72-0270 R02 ENGINE - Fan Stator Assembly (72-00-23) - Forward Mount Rib Inspection
Mos
Hrs
Enc
72 ENG2Eff: 15-Apr-2014
(NOTE: This Service Bulletin is applicable to all CF34-BJ engines that have been removed from wing at least one time.)
Cat. 2 - RecommendedT (-)72-0270 R03 ENGINE - Fan Stator Assembly (72-00-23) - Forward Mount Rib Inspection
Mos
Hrs
Enc
72 ENG1Eff: 09-Jan-2015
Cat. 2 - RecommendedT (-)72-0270 R03 ENGINE - Fan Stator Assembly (72-00-23) - Forward Mount Rib Inspection
Mos
Hrs
Enc
72 ENG2Eff: 09-Jan-2015
Cat. 2 - RecommendedT (A/R)72-0270 R04 ENGINE - Fan Stator Assembly (72-00-23) - Forward Mount Rib Inspection
Mos
Hrs
Enc
72 ENG1Eff: 29-May-2015
Cat. 2 - RecommendedT (A/R)72-0270 R04 ENGINE - Fan Stator Assembly (72-00-23) - Forward Mount Rib Inspection
Mos
Hrs
Enc
72 ENG2Eff: 29-May-2015
Category 8T (A/R)72-0272 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Engines
Mos
Hrs
Enc
72 ENG1Eff: 20-Mar-2015
Category 8T (A/R)72-0272 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Engines
Mos
Hrs
Enc
72 ENG2Eff: 20-Mar-2015
Cat. 3 - RecommendedRE (-)72-0276 R00 ENGINE - Exhaust Components (72-54-00) - Release of New Improved Scavenge Adapter and Scavenge Connector to the CF34-BJ Engine Models
Mos
Hrs
Enc
72 ENG1Eff: 13-Mar-2014
Cat. 3 - RecommendedRE (-)72-0276 R00 ENGINE - Exhaust Components (72-54-00) - Release of New Improved Scavenge Adapter and Scavenge Connector to the CF34-BJ Engine Models
Mos
Hrs
Enc
72 ENG2Eff: 13-Mar-2014
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM359/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 7 - OptionalRE (-)72-0277 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Introduction of New Self-Wrenching Bolt P/N 4020T53P04
Mos
Hrs
Enc
72 ENG1Eff: 02-Apr-2014
Cat. 7 - OptionalRE (-)72-0277 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Introduction of New Self-Wrenching Bolt P/N 4020T53P04
Mos
Hrs
Enc
72 ENG2Eff: 02-Apr-2014
Cat. 8 - InformationalT (A/R)72-0280 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 16-May-2014
Cat. 8 - InformationalT (A/R)72-0280 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 16-May-2014
Cat. 6 - RecommendedRE (-)72-0281 R00 ENGINE - Combustion Section (72-43-00) - Introduction of New Support Bracket P/N 2583M77G01 For White W3 Cable Assembly
Mos
Hrs
Enc
72 ENG1Eff: 03-Oct-2014
(AVG MAN HRS: 2)
Cat. 6 - RecommendedRE (-)72-0281 R00 ENGINE - Combustion Section (72-43-00) - Introduction of New Support Bracket P/N 2583M77G01 For White W3 Cable Assembly
Mos
Hrs
Enc
72 ENG2Eff: 03-Oct-2014
(AVG MAN HRS: 2)
Cat. 8 - InformationalRE (-)72-0284 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Turbofan Engines
Mos
Hrs
Enc
72 ENG1Eff: 03-Oct-2014
Cat. 8 - InformationalRE (-)72-0284 R00 ENGINE - General (72-00-00) - Spare Parts Release for CF34-BJ Turbofan Engines
Mos
Hrs
Enc
72 ENG2Eff: 03-Oct-2014
Cat. 7 - OptionalRE (-)72-0287 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - CF34 Accessory Gearbox (AGB) Interchangeability Modifications
Mos
Hrs
Enc
72 ENG1Eff: 23-Oct-2014
(AVG MAN HRS: 6)
Cat. 7 - OptionalRE (-)72-0287 R00 ENGINE - Accessory Gearbox Assembly (72-62-00) - CF34 Accessory Gearbox (AGB) Interchangeability Modifications
Mos
Hrs
Enc
72 ENG2Eff: 23-Oct-2014
(AVG MAN HRS: 6)
Category 3T (A/R)72-0294 R00 Engine - Compressor Stator Assembly (72-00-32) - Inspection of VG System to Check For Looseness
Mos
Hrs
Enc
72 ENG1Eff: 12-Aug-2015
(AVG MAN HRS: 8)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM360/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Category 3T (A/R)72-0294 R00 Engine - Compressor Stator Assembly (72-00-32) - Inspection of VG System to Check For Looseness
Mos
Hrs
Enc
72 ENG2Eff: 12-Aug-2015
(AVG MAN HRS: 8)
Category 4T (A/R)72-0296 R00 Engine - Turbine Transition Assembly - Replacement of Silver Plated Nuts with Dry-Film Coated Nuts on Thermocouple Probes and PT5 Probe
Mos
Hrs
Enc
72 ENG1Eff: 11-Mar-2016
(AVG MAN HRS: 4) (NOTE: The plain nut P/N MS9357-10, washer tab lock (washer) P/N3056T13P01, and self-locking nut P/N R1181P004
(used with nowasher) are affected by this Service Bulletin)
Category 4T (A/R)72-0296 R00 Engine - Turbine Transition Assembly - Replacement of Silver Plated Nuts with Dry-Film Coated Nuts on Thermocouple Probes and PT5 Probe
Mos
Hrs
Enc
72 ENG2Eff: 11-Mar-2016
(AVG MAN HRS: 4) (NOTE: The plain nut P/N MS9357-10, washer tab lock (washer) P/N3056T13P01, and self-locking nut P/N R1181P004
(used with nowasher) are affected by this Service Bulletin)
Cat. 9 - InformationalRE (-)72-A0088 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Management Plan
Mos
Hrs
Enc
72 ENG1Eff: 21-Sep-2000
Cat. 9 - InformationalRE (-)72-A0088 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Management Plan
Mos
Hrs
Enc
72 ENG2Eff: 21-Sep-2000
Cat. 9 - InformationalRE (-)72-A0088 R01 ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Management Plan
Mos
Hrs
Enc
72 ENG1Eff: 30-Oct-2000
Cat. 9 - InformationalRE (-)72-A0088 R01 ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Management Plan
Mos
Hrs
Enc
72 ENG2Eff: 30-Oct-2000
Cat. 9 - InformationalRE (-)72-A0088 R02 ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Management Plan
Mos
Hrs
Enc
72 ENG1Eff: 15-Jun-2001
Cat. 9 - InformationalRE (-)72-A0088 R02 ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Management Plan
Mos
Hrs
Enc
72 ENG2Eff: 15-Jun-2001
Cat. 1 - RecommendedRE (-)72-A0088 R03 ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Management Plan
13-May-2005Mos
Hrs
Enc
72 ENG1NEW PART INSTALLEDEff: 13-May-2005 Not
Applicable
(NOTE: Information only. GE recommends you no longer do this Alert Service Bulletin. This Alert Service Bulletin is superseded by CF34-BJ S/B
72-A0212.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM361/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 1 - RecommendedRE (-)72-A0088 R03 ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Management Plan
13-May-2005Mos
Hrs
Enc
72 ENG2Eff: 13-May-2005 Complied With
(NOTE: Information only. GE recommends you no longer do this Alert Service Bulletin. This Alert Service Bulletin is superseded by CF34-BJ S/B
72-A0212.)
Cat. 9 - InformationalT (A/R)72-A0088 R04 ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Management Plan
Mos
Hrs
Enc
72 ENG1Eff: 13-Mar-2007
(NOTE: Information only. GE recommends you no longer do this Alert Service Bulletin. This Alert Service Bulletin is superseded by CF34-BJ S/B
72-A0212.)
Cat. 9 - InformationalT (A/R)72-A0088 R04 ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Management Plan
Mos
Hrs
Enc
72 ENG2Eff: 13-Mar-2007
(NOTE: Information only. GE recommends you no longer do this Alert Service Bulletin. This Alert Service Bulletin is superseded by CF34-BJ S/B
72-A0212.)
Cat. 2 - RecommendedRE (-)72-A0097 R00 ENGINE - High Pressure Turbine Stator (72-45-00) - One-Time Inspection of HPT Borescope Plugs
Mos
Hrs
Enc
72 ENG1Eff: 16-Jul-2001
Cat. 2 - RecommendedRE (-)72-A0097 R00 ENGINE - High Pressure Turbine Stator (72-45-00) - One-Time Inspection of HPT Borescope Plugs
Mos
Hrs
Enc
72 ENG2Eff: 16-Jul-2001
Cat. 1 - RecommendedRE (-)72-A0140 R00 ENGINE - Compressor Rotor (72-33-00) - Compressor Rotor Spool Stages 3 thru 8 Field Management Plan
Mos
Hrs
Enc
72 ENG1Eff: 13-Apr-2004
(NOTE: GE recommends that you do this Service Bulletin on the affected compressor rotor spool stages 3 thru 8, PN 6078T56P03 and PN
6078T56P04, with greater than 6,000 accumulated cycles as follows (Refer to Maintenance Manual SEI-580, Chapter 5-11-02 or SEI-780,
Chapter 5-11-02 as applicable): (a) If the applicable Engine Manual Chapter 5 life limit for the affected compressor rotor spool stages 3 thru
8, is less than 22,000 part operating cycles-since-new (CSN), do at piece part exposure for compressor rotor spool stages 3 thru 8 with greater
than 6,000 accumulated cycles, or at the Chapter 5 life limit, whichever is lower. (b) If the applicable Engine Manual Chapter 5 life limit for the
affected compressor rotor spool stages 3 thru 8, is greater than 22,000 part operating cycles since new, do at piece part exposure for
compressor rotor spool stages 3 thru 8 with greater than 6,000 accumulated cycles, but prior to accumulating 22,000 part operating cycles
since new.)
Cat. 1 - RecommendedRE (-)72-A0140 R00 ENGINE - Compressor Rotor (72-33-00) - Compressor Rotor Spool Stages 3 thru 8 Field Management Plan
Mos
Hrs
Enc
72 ENG2Eff: 13-Apr-2004
(NOTE: GE recommends that you do this Service Bulletin on the affected compressor rotor spool stages 3 thru 8, PN 6078T56P03 and PN
6078T56P04, with greater than 6,000 accumulated cycles as follows (Refer to Maintenance Manual SEI-580, Chapter 5-11-02 or SEI-780,
Chapter 5-11-02 as applicable): (a) If the applicable Engine Manual Chapter 5 life limit for the affected compressor rotor spool stages 3 thru
8, is less than 22,000 part operating cycles-since-new (CSN), do at piece part exposure for compressor rotor spool stages 3 thru 8 with greater
than 6,000 accumulated cycles, or at the Chapter 5 life limit, whichever is lower. (b) If the applicable Engine Manual Chapter 5 life limit for the
affected compressor rotor spool stages 3 thru 8, is greater than 22,000 part operating cycles since new, do at piece part exposure for
compressor rotor spool stages 3 thru 8 with greater than 6,000 accumulated cycles, but prior to accumulating 22,000 part operating cycles
since new.)
Cat. 1 - RecommendedRE (-)72-A0140 R01 ENGINE - Compressor Rotor (72-33-00) - Compressor Rotor Spool Stages 3 thru 8 Field Management Plan
13-May-2005Mos
Hrs
Enc
72 ENG1BY PART S/N INSTALLEDEff: 15-Jun-2004 Not
Applicable
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM362/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 1 - RecommendedRE (-)72-A0140 R01 ENGINE - Compressor Rotor (72-33-00) - Compressor Rotor Spool Stages 3 thru 8 Field Management Plan
15-Jun-2004Mos
Hrs
Enc
72 ENG2Eff: 15-Jun-2004 Not Applicable
Cat. 3 - RecommendedRE (-)72-A0148 R00 ENGINE - Low Pressure Turbine (LPT) Rotor (72-53-00) - Replacement or Inspection of Stages 5 and 6 LPT Rotor Disks and Inspection of Stages 3 and 4 LPT Disk Arms
for Arc Out
Mos
Hrs
Enc
72 ENG1Eff: 02-Sep-2004
(NOTE: GE recommends that you do this Alert Service Bulletin at the next piece part exposure of affected stage 5 and/or stage 6 LPT disks.
NOTE: Alert Service Bulletin CF34-BJ 72-A0152 requires removal of LPT modules or engines which contain stage 5 and/or stage 6 disk list in
Appendix (Table 1 or Table 2) within specific intervals, based on accumulated cycles on the affected stage 5 and stage 6 LPT disk, for
replacement or performance of the inspections in this Alert Service Bulletin CF34-BJ 72-A0148. Refer to Alert Service Bulletin CF34-BJ 72-
A0152, Removal Plan to Inspect or replace LPT disks for arc-out indications. Inspection Limitations: A. Prior to January 1, 2010, affected
stage 5 and stage 6 LPT disks listed in (Table 1) may be inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the
disk(s) are reinstalled in the engine or LPT module they were removed from. B. January 1, 2010 and later, stage 5 and stage 6 LPT disks listed
in (Table 1) may be re-inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the stage 5 and stage 6 was initially
inspected prior to January 1, 2010 and the disk(s) are reinstalled in the engine or LPT module they were removed from. C. Disks not inspected
prior to January 1, 2010 in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 must be replaced with disks not listed in Appendix
(Table 1 or Table 2) of this Alert Service Bulletin. Replace disks listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-
BJ 72-0098. Use of replacement engines or LPT modules: Replacement engine or LPT module is defines as an engine or LPT module not
installed on an operational aircraft on August 31, 2004. The replacement engine or LPT module will contain a stage 5 and stage 6 LPT disks
not listed in Appendix (Table 1 or Table 2) of this Alert Service Bulletin CF34-BJ 72-A0148. OR A. Prior to January 1, 2010, replacement
engines or LPT modules shall contain stage 5 or stage 6 LPT disks listed in Appendix (Table 1) and visually inspected in accordance with this
Alert Service Bulletin CF34-BJ 72-A0148. B. January 1, 2010 and later, the replacement engine or module contains a stage 5 and or stage 6
LPT disk listed in Appendix (Table 1) and initially inspected prior to June 1, 2005 and are in compliance with the interval inspection requirement
in Alert Service Bulletin CF34-BJ 72-A0152. C. Replacement engine or LPT modules containing a stage 5 or stage 6 disk listed in Appendix
(Table 1) and not inspected prior to June 1, 2005, the suspect disk must be replaced with a disk not listed in the Appendix (Table 1 or Table 2)
of this Alert Service Bulletin. D. Replace disk listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-BJ S/B 72-0098.)
Cat. 3 - RecommendedRE (-)72-A0148 R00 ENGINE - Low Pressure Turbine (LPT) Rotor (72-53-00) - Replacement or Inspection of Stages 5 and 6 LPT Rotor Disks and Inspection of Stages 3 and 4 LPT Disk Arms
for Arc Out
Mos
Hrs
Enc
72 ENG2Eff: 02-Sep-2004
(NOTE: GE recommends that you do this Alert Service Bulletin at the next piece part exposure of affected stage 5 and/or stage 6 LPT disks.
NOTE: Alert Service Bulletin CF34-BJ 72-A0152 requires removal of LPT modules or engines which contain stage 5 and/or stage 6 disk list in
Appendix (Table 1 or Table 2) within specific intervals, based on accumulated cycles on the affected stage 5 and stage 6 LPT disk, for
replacement or performance of the inspections in this Alert Service Bulletin CF34-BJ 72-A0148. Refer to Alert Service Bulletin CF34-BJ 72-
A0152, Removal Plan to Inspect or replace LPT disks for arc-out indications. Inspection Limitations: A. Prior to January 1, 2010, affected
stage 5 and stage 6 LPT disks listed in (Table 1) may be inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the
disk(s) are reinstalled in the engine or LPT module they were removed from. B. January 1, 2010 and later, stage 5 and stage 6 LPT disks listed
in (Table 1) may be re-inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the stage 5 and stage 6 was initially
inspected prior to January 1, 2010 and the disk(s) are reinstalled in the engine or LPT module they were removed from. C. Disks not inspected
prior to January 1, 2010 in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 must be replaced with disks not listed in Appendix
(Table 1 or Table 2) of this Alert Service Bulletin. Replace disks listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-
BJ 72-0098. Use of replacement engines or LPT modules: Replacement engine or LPT module is defines as an engine or LPT module not
installed on an operational aircraft on August 31, 2004. The replacement engine or LPT module will contain a stage 5 and stage 6 LPT disks
not listed in Appendix (Table 1 or Table 2) of this Alert Service Bulletin CF34-BJ 72-A0148. OR A. Prior to January 1, 2010, replacement
engines or LPT modules shall contain stage 5 or stage 6 LPT disks listed in Appendix (Table 1) and visually inspected in accordance with this
Alert Service Bulletin CF34-BJ 72-A0148. B. January 1, 2010 and later, the replacement engine or module contains a stage 5 and or stage 6
LPT disk listed in Appendix (Table 1) and initially inspected prior to June 1, 2005 and are in compliance with the interval inspection requirement
in Alert Service Bulletin CF34-BJ 72-A0152. C. Replacement engine or LPT modules containing a stage 5 or stage 6 disk listed in Appendix
(Table 1) and not inspected prior to June 1, 2005, the suspect disk must be replaced with a disk not listed in the Appendix (Table 1 or Table 2)
of this Alert Service Bulletin. D. Replace disk listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-BJ S/B 72-0098.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM363/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 5 - RecommendedRE (-)72-A0148 R01 ENGINE - Low Pressure Turbine (LPT) Rotor (72-53-00) - Replacement or Inspection of Stages 5 and 6 LPT Rotor Disks and Inspection of Stages 3 and 4 LPT Disk Arms
for Arc Out
Mos
Hrs
Enc
72 ENG1Eff: 10-Mar-2005
(NOTE: GE recommends that you do this Alert Service Bulletin at the next piece part exposure of affected stage 5 and/or stage 6 LPT disks.
NOTE: Alert Service Bulletin CF34-BJ 72-A0152 requires removal of LPT modules or engines which contain stage 5 and/or stage 6 disk list in
Appendix (Table 1 or Table 2) within specific intervals, based on accumulated cycles on the affected stage 5 and stage 6 LPT disk, for
replacement or performance of the inspections in this Alert Service Bulletin CF34-BJ 72-A0148. Refer to Alert Service Bulletin CF34-BJ 72-
A0152, Removal Plan to Inspect or replace LPT disks for arc-out indications. Inspection Limitations: A. Prior to January 1, 2010, affected
stage 5 and stage 6 LPT disks listed in (Table 1) may be inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the
disk(s) are reinstalled in the engine or LPT module they were removed from. B. January 1, 2010 and later, stage 5 and stage 6 LPT disks listed
in (Table 1) may be re-inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the stage 5 and stage 6 was initially
inspected prior to January 1, 2010 and the disk(s) are reinstalled in the engine or LPT module they were removed from. C. Disks not inspected
prior to January 1, 2010 in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 must be replaced with disks not listed in Appendix
(Table 1 or Table 2) of this Alert Service Bulletin. Replace disks listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-
BJ 72-0098. Use of replacement engines or LPT modules: Replacement engine or LPT module is defines as an engine or LPT module not
installed on an operational aircraft on August 31, 2004. The replacement engine or LPT module will contain a stage 5 and stage 6 LPT disks
not listed in Appendix (Table 1 or Table 2) of this Alert Service Bulletin CF34-BJ 72-A0148. OR A. Prior to January 1, 2010, replacement
engines or LPT modules shall contain stage 5 or stage 6 LPT disks listed in Appendix (Table 1) and visually inspected in accordance with this
Alert Service Bulletin CF34-BJ 72-A0148. B. January 1, 2010 and later, the replacement engine or module contains a stage 5 and or stage 6
LPT disk listed in Appendix (Table 1) and initially inspected prior to June 1, 2005 and are in compliance with the interval inspection requirement
in Alert Service Bulletin CF34-BJ 72-A0152. C. Replacement engine or LPT modules containing a stage 5 or stage 6 disk listed in Appendix
(Table 1) and not inspected prior to June 1, 2005, the suspect disk must be replaced with a disk not listed in the Appendix (Table 1 or Table 2)
of this Alert Service Bulletin. D. Replace disk listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-BJ S/B 72-0098.)
Cat. 5 - RecommendedRE (-)72-A0148 R01 ENGINE - Low Pressure Turbine (LPT) Rotor (72-53-00) - Replacement or Inspection of Stages 5 and 6 LPT Rotor Disks and Inspection of Stages 3 and 4 LPT Disk Arms
for Arc Out
Mos
Hrs
Enc
72 ENG2Eff: 10-Mar-2005
(NOTE: GE recommends that you do this Alert Service Bulletin at the next piece part exposure of affected stage 5 and/or stage 6 LPT disks.
NOTE: Alert Service Bulletin CF34-BJ 72-A0152 requires removal of LPT modules or engines which contain stage 5 and/or stage 6 disk list in
Appendix (Table 1 or Table 2) within specific intervals, based on accumulated cycles on the affected stage 5 and stage 6 LPT disk, for
replacement or performance of the inspections in this Alert Service Bulletin CF34-BJ 72-A0148. Refer to Alert Service Bulletin CF34-BJ 72-
A0152, Removal Plan to Inspect or replace LPT disks for arc-out indications. Inspection Limitations: A. Prior to January 1, 2010, affected
stage 5 and stage 6 LPT disks listed in (Table 1) may be inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the
disk(s) are reinstalled in the engine or LPT module they were removed from. B. January 1, 2010 and later, stage 5 and stage 6 LPT disks listed
in (Table 1) may be re-inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the stage 5 and stage 6 was initially
inspected prior to January 1, 2010 and the disk(s) are reinstalled in the engine or LPT module they were removed from. C. Disks not inspected
prior to January 1, 2010 in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 must be replaced with disks not listed in Appendix
(Table 1 or Table 2) of this Alert Service Bulletin. Replace disks listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-
BJ 72-0098. Use of replacement engines or LPT modules: Replacement engine or LPT module is defines as an engine or LPT module not
installed on an operational aircraft on August 31, 2004. The replacement engine or LPT module will contain a stage 5 and stage 6 LPT disks
not listed in Appendix (Table 1 or Table 2) of this Alert Service Bulletin CF34-BJ 72-A0148. OR A. Prior to January 1, 2010, replacement
engines or LPT modules shall contain stage 5 or stage 6 LPT disks listed in Appendix (Table 1) and visually inspected in accordance with this
Alert Service Bulletin CF34-BJ 72-A0148. B. January 1, 2010 and later, the replacement engine or module contains a stage 5 and or stage 6
LPT disk listed in Appendix (Table 1) and initially inspected prior to June 1, 2005 and are in compliance with the interval inspection requirement
in Alert Service Bulletin CF34-BJ 72-A0152. C. Replacement engine or LPT modules containing a stage 5 or stage 6 disk listed in Appendix
(Table 1) and not inspected prior to June 1, 2005, the suspect disk must be replaced with a disk not listed in the Appendix (Table 1 or Table 2)
of this Alert Service Bulletin. D. Replace disk listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-BJ S/B 72-0098.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM364/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 5 - RecommendedRE (-)72-A0148 R02 ENGINE - Low Pressure Turbine (LPT) Rotor (72-53-00) - Replacement or Inspection of Stages 5 and 6 LPT Rotor Disks and Inspection of Stages 3 and 4 LPT Disk Arms
for Arc Out
Mos
Hrs
Enc
72 ENG1Eff: 24-May-2005
(NOTE: GE recommends that you do this Alert Service Bulletin at the next piece part exposure of affected stage 5 and/or stage 6 LPT disks.
NOTE: Alert Service Bulletin CF34-BJ 72-A0152 requires removal of LPT modules or engines which contain stage 5 and/or stage 6 disk list in
Appendix (Table 1 or Table 2) within specific intervals, based on accumulated cycles on the affected stage 5 and stage 6 LPT disk, for
replacement or performance of the inspections in this Alert Service Bulletin CF34-BJ 72-A0148. Refer to Alert Service Bulletin CF34-BJ 72-
A0152, Removal Plan to Inspect or replace LPT disks for arc-out indications. Inspection Limitations: A. Prior to January 1, 2010, affected
stage 5 and stage 6 LPT disks listed in (Table 1) may be inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the
disk(s) are reinstalled in the engine or LPT module they were removed from. B. January 1, 2010 and later, stage 5 and stage 6 LPT disks listed
in (Table 1) may be re-inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the stage 5 and stage 6 was initially
inspected prior to January 1, 2010 and the disk(s) are reinstalled in the engine or LPT module they were removed from. C. Disks not inspected
prior to January 1, 2010 in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 must be replaced with disks not listed in Appendix
(Table 1 or Table 2) of this Alert Service Bulletin. Replace disks listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-
BJ 72-0098. Use of replacement engines or LPT modules: Replacement engine or LPT module is defines as an engine or LPT module not
installed on an operational aircraft on August 31, 2004. The replacement engine or LPT module will contain a stage 5 and stage 6 LPT disks
not listed in Appendix (Table 1 or Table 2) of this Alert Service Bulletin CF34-BJ 72-A0148. OR A. Prior to January 1, 2010, replacement
engines or LPT modules shall contain stage 5 or stage 6 LPT disks listed in Appendix (Table 1) and visually inspected in accordance with this
Alert Service Bulletin CF34-BJ 72-A0148. B. January 1, 2010 and later, the replacement engine or module contains a stage 5 and or stage 6
LPT disk listed in Appendix (Table 1) and initially inspected prior to June 1, 2005 and are in compliance with the interval inspection requirement
in Alert Service Bulletin CF34-BJ 72-A0152. C. Replacement engine or LPT modules containing a stage 5 or stage 6 disk listed in Appendix
(Table 1) and not inspected prior to June 1, 2005, the suspect disk must be replaced with a disk not listed in the Appendix (Table 1 or Table 2)
of this Alert Service Bulletin. D. Replace disk listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-BJ S/B 72-0098.)
Cat. 5 - RecommendedRE (-)72-A0148 R02 ENGINE - Low Pressure Turbine (LPT) Rotor (72-53-00) - Replacement or Inspection of Stages 5 and 6 LPT Rotor Disks and Inspection of Stages 3 and 4 LPT Disk Arms
for Arc Out
Mos
Hrs
Enc
72 ENG2Eff: 24-May-2005
(NOTE: GE recommends that you do this Alert Service Bulletin at the next piece part exposure of affected stage 5 and/or stage 6 LPT disks.
NOTE: Alert Service Bulletin CF34-BJ 72-A0152 requires removal of LPT modules or engines which contain stage 5 and/or stage 6 disk list in
Appendix (Table 1 or Table 2) within specific intervals, based on accumulated cycles on the affected stage 5 and stage 6 LPT disk, for
replacement or performance of the inspections in this Alert Service Bulletin CF34-BJ 72-A0148. Refer to Alert Service Bulletin CF34-BJ 72-
A0152, Removal Plan to Inspect or replace LPT disks for arc-out indications. Inspection Limitations: A. Prior to January 1, 2010, affected
stage 5 and stage 6 LPT disks listed in (Table 1) may be inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the
disk(s) are reinstalled in the engine or LPT module they were removed from. B. January 1, 2010 and later, stage 5 and stage 6 LPT disks listed
in (Table 1) may be re-inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the stage 5 and stage 6 was initially
inspected prior to January 1, 2010 and the disk(s) are reinstalled in the engine or LPT module they were removed from. C. Disks not inspected
prior to January 1, 2010 in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 must be replaced with disks not listed in Appendix
(Table 1 or Table 2) of this Alert Service Bulletin. Replace disks listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-
BJ 72-0098. Use of replacement engines or LPT modules: Replacement engine or LPT module is defines as an engine or LPT module not
installed on an operational aircraft on August 31, 2004. The replacement engine or LPT module will contain a stage 5 and stage 6 LPT disks
not listed in Appendix (Table 1 or Table 2) of this Alert Service Bulletin CF34-BJ 72-A0148. OR A. Prior to January 1, 2010, replacement
engines or LPT modules shall contain stage 5 or stage 6 LPT disks listed in Appendix (Table 1) and visually inspected in accordance with this
Alert Service Bulletin CF34-BJ 72-A0148. B. January 1, 2010 and later, the replacement engine or module contains a stage 5 and or stage 6
LPT disk listed in Appendix (Table 1) and initially inspected prior to June 1, 2005 and are in compliance with the interval inspection requirement
in Alert Service Bulletin CF34-BJ 72-A0152. C. Replacement engine or LPT modules containing a stage 5 or stage 6 disk listed in Appendix
(Table 1) and not inspected prior to June 1, 2005, the suspect disk must be replaced with a disk not listed in the Appendix (Table 1 or Table 2)
of this Alert Service Bulletin. D. Replace disk listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-BJ S/B 72-0098.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM365/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 5 - RecommendedRE (-)72-A0148 R03 ENGINE - Low Pressure Turbine (LPT) Rotor (72-53-00) - Replacement or Inspection of Stages 5 and 6 LPT Rotor Disks and Inspection of Stages 3 and 4 LPT Disk Arms
for Arc Out
06-May-2009Mos
11,438.9Hrs
6,316Enc
72 ENG2Eff: 05-Aug-2009 Complied With
(NOTE: GE recommends that you do this Alert Service Bulletin at the next piece part exposure of affected stage 5 and/or stage 6 LPT disks.
NOTE: Alert Service Bulletin CF34-BJ 72-A0152 requires removal of LPT modules or engines which contain stage 5 and/or stage 6 disk list in
Appendix (Table 1 or Table 2) within specific intervals, based on accumulated cycles on the affected stage 5 and stage 6 LPT disk, for
replacement or performance of the inspections in this Alert Service Bulletin CF34-BJ 72-A0148. Refer to Alert Service Bulletin CF34-BJ 72-
A0152, Removal Plan to Inspect or replace LPT disks for arc-out indications. Inspection Limitations: A. Prior to January 1, 2010, affected
stage 5 and stage 6 LPT disks listed in (Table 1) may be inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the
disk(s) are reinstalled in the engine or LPT module they were removed from. B. January 1, 2010 and later, stage 5 and stage 6 LPT disks listed
in (Table 1) may be re-inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the stage 5 and stage 6 was initially
inspected prior to January 1, 2010 and the disk(s) are reinstalled in the engine or LPT module they were removed from. C. Disks not inspected
prior to January 1, 2010 in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 must be replaced with disks not listed in Appendix
(Table 1 or Table 2) of this Alert Service Bulletin. Replace disks listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-
BJ 72-0098. Use of replacement engines or LPT modules: Replacement engine or LPT module is defines as an engine or LPT module not
installed on an operational aircraft on August 31, 2004. The replacement engine or LPT module will contain a stage 5 and stage 6 LPT disks
not listed in Appendix (Table 1 or Table 2) of this Alert Service Bulletin CF34-BJ 72-A0148. OR A. Prior to January 1, 2010, replacement
engines or LPT modules shall contain stage 5 or stage 6 LPT disks listed in Appendix (Table 1) and visually inspected in accordance with this
Alert Service Bulletin CF34-BJ 72-A0148. B. January 1, 2010 and later, the replacement engine or module contains a stage 5 and or stage 6
LPT disk listed in Appendix (Table 1) and initially inspected prior to June 1, 2005 and are in compliance with the interval inspection requirement
in Alert Service Bulletin CF34-BJ 72-A0152. C. Replacement engine or LPT modules containing a stage 5 or stage 6 disk listed in Appendix
(Table 1) and not inspected prior to June 1, 2005, the suspect disk must be replaced with a disk not listed in the Appendix (Table 1 or Table 2)
of this Alert Service Bulletin. D. Replace disk listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-BJ S/B 72-0098.)
Cat. 5 - RecommendedRE (-)72-A0148 R03 ENGINE - Low Pressure Turbine (LPT) Rotor (72-53-00) - Replacement or Inspection of Stages 5 and 6 LPT Rotor Disks and Inspection of Stages 3 and 4 LPT Disk Arms
for Arc Out
01-Apr-2009Mos
11,555.9Hrs
6,357Enc
72 ENG1Eff: 05-Aug-2009 Complied With
(NOTE: GE recommends that you do this Alert Service Bulletin at the next piece part exposure of affected stage 5 and/or stage 6 LPT disks.
NOTE: Alert Service Bulletin CF34-BJ 72-A0152 requires removal of LPT modules or engines which contain stage 5 and/or stage 6 disk list in
Appendix (Table 1 or Table 2) within specific intervals, based on accumulated cycles on the affected stage 5 and stage 6 LPT disk, for
replacement or performance of the inspections in this Alert Service Bulletin CF34-BJ 72-A0148. Refer to Alert Service Bulletin CF34-BJ 72-
A0152, Removal Plan to Inspect or replace LPT disks for arc-out indications. Inspection Limitations: A. Prior to January 1, 2010, affected
stage 5 and stage 6 LPT disks listed in (Table 1) may be inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the
disk(s) are reinstalled in the engine or LPT module they were removed from. B. January 1, 2010 and later, stage 5 and stage 6 LPT disks listed
in (Table 1) may be re-inspected in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 provided the stage 5 and stage 6 was initially
inspected prior to January 1, 2010 and the disk(s) are reinstalled in the engine or LPT module they were removed from. C. Disks not inspected
prior to January 1, 2010 in accordance with this Alert Service Bulletin CF34-BJ 72-A0148 must be replaced with disks not listed in Appendix
(Table 1 or Table 2) of this Alert Service Bulletin. Replace disks listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-
BJ 72-0098. Use of replacement engines or LPT modules: Replacement engine or LPT module is defines as an engine or LPT module not
installed on an operational aircraft on August 31, 2004. The replacement engine or LPT module will contain a stage 5 and stage 6 LPT disks
not listed in Appendix (Table 1 or Table 2) of this Alert Service Bulletin CF34-BJ 72-A0148. OR A. Prior to January 1, 2010, replacement
engines or LPT modules shall contain stage 5 or stage 6 LPT disks listed in Appendix (Table 1) and visually inspected in accordance with this
Alert Service Bulletin CF34-BJ 72-A0148. B. January 1, 2010 and later, the replacement engine or module contains a stage 5 and or stage 6
LPT disk listed in Appendix (Table 1) and initially inspected prior to June 1, 2005 and are in compliance with the interval inspection requirement
in Alert Service Bulletin CF34-BJ 72-A0152. C. Replacement engine or LPT modules containing a stage 5 or stage 6 disk listed in Appendix
(Table 1) and not inspected prior to June 1, 2005, the suspect disk must be replaced with a disk not listed in the Appendix (Table 1 or Table 2)
of this Alert Service Bulletin. D. Replace disk listed in Appendix (Table 2). Do not inspect or return to service. Refer to CF34-BJ S/B 72-0098.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM366/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 1 - RecommendedRE (-)72-A0152 R00 ENGINE - Low Pressure Turbine Rotor (72-53-00) - Removal Plan to Replace or Inspect LPT Disks for Arc-out Indications
Mos
Hrs
Enc
72 ENG1Eff: 10-Mar-2005
(NOTE: It is recommended that all CF34-1A, -3A, -3A1, -3A2 and CF34-3B engines or LPT modules, that have the affected stage 5 or stage 6
LPT disks installed, be removed within the following intervals, for replacement or performance of the LPT disk inspections in CF34-BJ Alert
Service Bulletin 72-A0148:(a) LPT stage 5 and 6 disks with greater than or equal to 14,750 cycles since new (CSN) on the effective date of this
Alert Service Bulletin and which have not been fluorescent penetrant inspected (FPI) at a prior piece part exposure, prior to accumulating an
additional 250 cycles in service (CIS) since the effective date of this Alert Service Bulletin.(b) LPT stage 5 and 6 disks with greater than or equal
to 14,750 CSN on the effective date of this Alert Service Bulletin and which have been fluorescent penetrant inspected (FPI) at a prior piece part
exposure, prior to accumulating an additional 500 CIS since the effective date of this Alert Service Bulletin.(c) LPT stage 5 and 6 disks with
greater than or equal to 14,500 CSN and less than 14,750 CSN, on the effective date of this Alert Service Bulletin, at piece part exposure, but
prior to accumulating an additional 500 CIS since the effective date of this Alert Service Bulletin.(d) LPT stage 5 and 6 disks with greater than or
equal to 14,250 CSN and less than 14,500 CSN, on the effective date of this Alert Service Bulletin, at piece part exposure, but prior to
accumulating an additional 750 CIS since the effective date of this Alert Service Bulletin.(e) LPT stage 5 and 6 disks with greater than or equal
to 13,000 CSN and less than 14,250 CSN, on the effective date of this Alert Service Bulletin, at piece part exposure, but prior to accumulating
an additional 1,000 CIS since the effective date of this Alert Service Bulletin.(f) LPT stage 5 and 6 disks with greater than or equal to 2,500 CSN
and less than 13,000 CSN on the effective date of this Alert Service Bulletin, at piece part exposure, but prior to accumulating an additional
4,000 CIS since the effective date of this Alert Service Bulletin, or 14,000 CSN, whichever comes first.g) LPT stage 5 and 6 disks with fewer than
2,500 CSN on the effective date of this Alert Service Bulletin, at piece part exposure, but no later than 6,500 CSN.(2) Replace all affected disk on
or before January 1, 2013, not to exceed published life cycles of the disks. (3) Re-inspection of all affected LPT disks. Remove affected engines
or LPT modules and reinspect all affected disk every 3,100 disk cycles since last inspection, not to exceed 3,100 disk cycles since last inspection
as defined in Alert Service Bulletin CF34-BJ S/B 72-A0148, until the affected disks are replaced with disks not listed in the Appendix (Table 1 or
Table 2) not to exceed the published life limits of the LPT disks, refer to the current revision of SEI-580 or SEI-780, Chapter 05 which ever is
applicable.)
Cat. 1 - RecommendedRE (-)72-A0152 R00 ENGINE - Low Pressure Turbine Rotor (72-53-00) - Removal Plan to Replace or Inspect LPT Disks for Arc-out Indications
Mos
Hrs
Enc
72 ENG2Eff: 10-Mar-2005
(NOTE: It is recommended that all CF34-1A, -3A, -3A1, -3A2 and CF34-3B engines or LPT modules, that have the affected stage 5 or stage 6
LPT disks installed, be removed within the following intervals, for replacement or performance of the LPT disk inspections in CF34-BJ Alert
Service Bulletin 72-A0148:(a) LPT stage 5 and 6 disks with greater than or equal to 14,750 cycles since new (CSN) on the effective date of this
Alert Service Bulletin and which have not been fluorescent penetrant inspected (FPI) at a prior piece part exposure, prior to accumulating an
additional 250 cycles in service (CIS) since the effective date of this Alert Service Bulletin.(b) LPT stage 5 and 6 disks with greater than or equal
to 14,750 CSN on the effective date of this Alert Service Bulletin and which have been fluorescent penetrant inspected (FPI) at a prior piece part
exposure, prior to accumulating an additional 500 CIS since the effective date of this Alert Service Bulletin.(c) LPT stage 5 and 6 disks with
greater than or equal to 14,500 CSN and less than 14,750 CSN, on the effective date of this Alert Service Bulletin, at piece part exposure, but
prior to accumulating an additional 500 CIS since the effective date of this Alert Service Bulletin.(d) LPT stage 5 and 6 disks with greater than or
equal to 14,250 CSN and less than 14,500 CSN, on the effective date of this Alert Service Bulletin, at piece part exposure, but prior to
accumulating an additional 750 CIS since the effective date of this Alert Service Bulletin.(e) LPT stage 5 and 6 disks with greater than or equal
to 13,000 CSN and less than 14,250 CSN, on the effective date of this Alert Service Bulletin, at piece part exposure, but prior to accumulating
an additional 1,000 CIS since the effective date of this Alert Service Bulletin.(f) LPT stage 5 and 6 disks with greater than or equal to 2,500 CSN
and less than 13,000 CSN on the effective date of this Alert Service Bulletin, at piece part exposure, but prior to accumulating an additional
4,000 CIS since the effective date of this Alert Service Bulletin, or 14,000 CSN, whichever comes first.g) LPT stage 5 and 6 disks with fewer than
2,500 CSN on the effective date of this Alert Service Bulletin, at piece part exposure, but no later than 6,500 CSN.(2) Replace all affected disk on
or before January 1, 2013, not to exceed published life cycles of the disks. (3) Re-inspection of all affected LPT disks. Remove affected engines
or LPT modules and reinspect all affected disk every 3,100 disk cycles since last inspection, not to exceed 3,100 disk cycles since last inspection
as defined in Alert Service Bulletin CF34-BJ S/B 72-A0148, until the affected disks are replaced with disks not listed in the Appendix (Table 1 or
Table 2) not to exceed the published life limits of the LPT disks, refer to the current revision of SEI-580 or SEI-780, Chapter 05 which ever is
applicable.)
Cat. 1 - RecommendedRE (-)72-A0152 R01 ENGINE - Low Pressure Turbine Rotor (72-53-00) - Removal Plan to Replace or Inspect LPT Disks for Arc-out Indications
25-Jan-2013Mos
Hrs
6,521Enc
72 ENG1Eff: 24-May-2005
(NOTE: 9621)
Cat. 1 - RecommendedRE (-)72-A0152 R01 ENGINE - Low Pressure Turbine Rotor (72-53-00) - Removal Plan to Replace or Inspect LPT Disks for Arc-out Indications
25-Jan-2013Mos
Hrs
6,480Enc
72 ENG2Eff: 24-May-2005
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM367/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 1 - Recommended ≈12-Jan-2024RE72-A0152 R02 ENGINE - Low Pressure Turbine Rotor (72-53-00) - Removal Plan to Replace or Inspect LPT Disks for Arc-out Indications
25-Jan-2013Mos
11,802.2Hrs
2,852 Enc9,6213,1006,521Enc
72 ENG1Eff: 05-Aug-2009 Complied With
Cat. 1 - Recommended ≈12-Jan-2024RE72-A0152 R02 ENGINE - Low Pressure Turbine Rotor (72-53-00) - Removal Plan to Replace or Inspect LPT Disks for Arc-out Indications
25-Jan-2013Mos
11,685.2Hrs
2,852 Enc9,5803,1006,480Enc
72 ENG2Eff: 05-Aug-2009 Complied With
Cat. 2 - RecommendedRE (-)72-A0200 R00 ENGINE - Low Pressure Turbine (72-53-00) - Inspection of LPT Modules
Mos
Hrs
Enc
72 ENG1Eff: 29-Jun-2006
(NOTE: This Alert Service Bulletin is applicable to CF34-3B turbofan engines that do not have new/reworked stage 3 shroud sector P/N
5099T32G02 featuring an improved integral heat shield as well as CF34-3A1 engines that are converted to CF34-3B1)
Cat. 2 - RecommendedRE (-)72-A0200 R00 ENGINE - Low Pressure Turbine (72-53-00) - Inspection of LPT Modules
Mos
Hrs
Enc
72 ENG2Eff: 29-Jun-2006
(NOTE: This Alert Service Bulletin is applicable to CF34-3B turbofan engines that do not have new/reworked stage 3 shroud sector P/N
5099T32G02 featuring an improved integral heat shield as well as CF34-3A1 engines that are converted to CF34-3B1)
Cat. 2 - RecommendedRE (-)72-A0200 R01 ENGINE - Low Pressure Turbine (72-53-00) - Inspection of LPT Modules
Mos
Hrs
Enc
72 ENG1Eff: 04-Oct-2006
(NOTE: This Alert Service Bulletin is applicable to CF34-3B turbofan engines that do not have new/reworked stage 3 shroud sector P/N
5099T32G02 featuring an improved integral heat shield as well as CF34-3A1 engines that are converted to CF34-3B1)
Cat. 2 - RecommendedRE (-)72-A0200 R01 ENGINE - Low Pressure Turbine (72-53-00) - Inspection of LPT Modules
Mos
Hrs
Enc
72 ENG2Eff: 04-Oct-2006
(NOTE: This Alert Service Bulletin is applicable to CF34-3B turbofan engines that do not have new/reworked stage 3 shroud sector P/N
5099T32G02 featuring an improved integral heat shield as well as CF34-3A1 engines that are converted to CF34-3B1)
Cat. 2 - Recommended ≈10-Oct-2036RE (-)72-A0200 R02 ENGINE - Low Pressure Turbine (72-53-00) - Inspection of LPT Modules
Mos
9,919.4 Hrs[22,056.8]Hrs
Enc
72 ENG1Eff: 21-Feb-2007
(NOTE: This Alert Service Bulletin is applicable to CF34-3B turbofan engines that do not have new/reworked stage 3 shroud sector P/N
5099T32G02 featuring an improved integral heat shield as well as CF34-3A1 engines that are converted to CF34-3B1)
Cat. 2 - Recommended ≈10-Oct-2036RE (-)72-A0200 R02 ENGINE - Low Pressure Turbine (72-53-00) - Inspection of LPT Modules
Mos
9,919.4 Hrs[21,939.8]Hrs
Enc
72 ENG2Eff: 21-Feb-2007
(NOTE: This Alert Service Bulletin is applicable to CF34-3B turbofan engines that do not have new/reworked stage 3 shroud sector P/N
5099T32G02 featuring an improved integral heat shield as well as CF34-3A1 engines that are converted to CF34-3B1)
Cat. 2 - RecommendedRE (-)72-A0200 R03 ENGINE - Low Pressure Turbine (72-52-00) - Inspection of LPT Modules
Mos
Hrs
Enc
72 ENG1Eff: 21-May-2010
(NOTE: This Alert Service Bulletin is applicable to CF34-3B turbofan engines that do not have new/reworked stage 3 shroud sector P/N
5099T32G02 featuring an improved integral heat shield as well as CF34-3A1 engines that are converted to CF34-3B1)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM368/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 2 - RecommendedRE (-)72-A0200 R03 ENGINE - Low Pressure Turbine (72-52-00) - Inspection of LPT Modules
Mos
Hrs
Enc
72 ENG2Eff: 21-May-2010
(NOTE: This Alert Service Bulletin is applicable to CF34-3B turbofan engines that do not have new/reworked stage 3 shroud sector P/N
5099T32G02 featuring an improved integral heat shield as well as CF34-3A1 engines that are converted to CF34-3B1)
Cat. 2 - Recommended ≈10-Oct-2036RE (-)72-A0200 R04 ENGINE - Low Pressure Turbine (72-52-00) - Inspection of LPT Modules
Mos
9,919.4 Hrs[22,056.8]Hrs
Enc
72 ENG1Eff: 21-Jul-2010
Cat. 2 - Recommended ≈10-Oct-2036RE (-)72-A0200 R04 ENGINE - Low Pressure Turbine (72-52-00) - Inspection of LPT Modules
Mos
9,919.4 Hrs[21,939.8]Hrs
Enc
72 ENG2Eff: 21-Jul-2010
Cat. 1 - RecommendedRE (-)72-A0212 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG1Eff: 07-Mar-2007
Cat. 1 - RecommendedRE (-)72-A0212 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG2Eff: 07-Mar-2007
Cat. 1 - RecommendedRE (-)72-A0212 R01 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG1Eff: 16-Mar-2007
Cat. 1 - RecommendedRE (-)72-A0212 R01 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG2Eff: 16-Mar-2007
Cat. 1 - RecommendedRE (-)72-A0212 R02 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG1Eff: 22-Mar-2007
Cat. 1 - RecommendedRE (-)72-A0212 R02 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG2Eff: 22-Mar-2007
Cat. 1 - RecommendedRE (-)72-A0212 R03 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG1Eff: 27-Jun-2007
Cat. 1 - RecommendedRE (-)72-A0212 R03 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG2Eff: 27-Jun-2007
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM369/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 1 - RecommendedRE (-)72-A0212 R04 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
22-Mar-2012Mos
11,674.8Hrs
6,447Enc
72 ENG1BY PART S/N INSTALLEDEff: 27-Oct-2008 Not
Applicable
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Mana...72-A0088 R04ENG172
Nextdue Share EarliestDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04 (Tier 1)ENG172
Nextdue Share EarliestDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04 (Tier 2)ENG172
Nextdue Share EarliestDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04 (Tier 3)ENG172
Cat. 1 - RecommendedRE (-)72-A0212 R04 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
19-Mar-2012Mos
11,557.8Hrs
6,406Enc
72 ENG2Eff: 27-Oct-2008 Complied With
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Fan Disk Field Mana...72-A0088 R04ENG272
Nextdue Share EarliestDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04 (Tier 1)ENG272
Nextdue Share EarliestDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04 (Tier 2)ENG272
Nextdue Share EarliestDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R04 (Tier 3)ENG272
Cat. 1 - RecommendedRE (-)72-A0212 R04 (Tier 1) ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG1Eff: 27-Oct-2008
Cat. 1 - RecommendedRE (-)72-A0212 R04 (Tier 1) ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG2Eff: 27-Oct-2008
Cat. 1 - RecommendedRE (-)72-A0212 R04 (Tier 2) ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG1Eff: 27-Oct-2008
Cat. 1 - RecommendedRE (-)72-A0212 R04 (Tier 2) ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG2Eff: 27-Oct-2008
Cat. 1 - RecommendedRE (-)72-A0212 R04 (Tier 3) ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG1Eff: 27-Oct-2008
Cat. 1 - RecommendedRE (-)72-A0212 R04 (Tier 3) ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG2Eff: 27-Oct-2008
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM370/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 1 - RecommendedRE (-)72-A0212 R05 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG1Eff: 29-May-2015
(AVG MAN HRS: 12)
Nextdue Share EarliestDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R05 (Tier 1)ENG172
Nextdue Share EarliestDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R05 (Tier 2)ENG172
Nextdue Share EarliestDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R05 (Tier 3)ENG172
Cat. 1 - RecommendedRE (-)72-A0212 R05 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG2Eff: 29-May-2015
(AVG MAN HRS: 12)
Nextdue Share EarliestDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R05 (Tier 1)ENG272
Nextdue Share EarliestDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R05 (Tier 2)ENG272
Nextdue Share EarliestDUE:1. RE -ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspecti...72-A0212 R05 (Tier 3)ENG272
Cat. 1 - RecommendedRE (-)72-A0212 R05 (Tier 1) ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG1Eff: 29-May-2015
(AVG MAN HRS: 12)
Cat. 1 - RecommendedRE (-)72-A0212 R05 (Tier 1) ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG2Eff: 29-May-2015
(AVG MAN HRS: 12)
Cat. 1 - RecommendedRE (-)72-A0212 R05 (Tier 2) ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG1Eff: 29-May-2015
(AVG MAN HRS: 12)
Cat. 1 - RecommendedRE (-)72-A0212 R05 (Tier 2) ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG2Eff: 29-May-2015
(AVG MAN HRS: 12)
Cat. 1 - RecommendedRE (-)72-A0212 R05 (Tier 3) ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG1Eff: 29-May-2015
(AVG MAN HRS: 12)
Cat. 1 - RecommendedRE (-)72-A0212 R05 (Tier 3) ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG2Eff: 29-May-2015
(AVG MAN HRS: 12)
Cat. 3 - RecommendedRE (-)72-A0234 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Eddy Current and Redundant Tactile Enhanced Visual Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG1Eff: 27-Oct-2008
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM371/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 3 - RecommendedRE (-)72-A0234 R00 ENGINE - Fan Rotor Assembly (72-21-00) - Shop Level Eddy Current and Redundant Tactile Enhanced Visual Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG2Eff: 27-Oct-2008
Cat. 2 - RecommendedRE (-)72-A0235 R00 ENGINE - Fan Rotor Assembly (72-21-00) - On Wing Repetitive Eddy Current Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG1Eff: 27-Oct-2008
Cat. 2 - RecommendedRE (-)72-A0235 R00 ENGINE - Fan Rotor Assembly (72-21-00) - On Wing Repetitive Eddy Current Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG2Eff: 27-Oct-2008
Cat. 2 - RecommendedRE (-)72-A0235 R01 ENGINE - Fan Rotor Assembly (72-21-00) - On Wing Repetitive Eddy Current Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG1Eff: 01-Jun-2015
(AVG MAN HRS: 2)
Cat. 2 - RecommendedRE (-)72-A0235 R01 ENGINE - Fan Rotor Assembly (72-21-00) - On Wing Repetitive Eddy Current Inspection for Fan Disk Arc-Out Indications
Mos
Hrs
Enc
72 ENG2Eff: 01-Jun-2015
(AVG MAN HRS: 2)
EMM - Life Limit ≈22-Feb-2021RE72-EMM-001 No.5 Bearing Carbon Seal Preformed Packing - Replace
05-Jun-2009Mos
2,417.4 Hrs14,554.83,00011,554.8Hrs
6,355Enc
72 ENG1
Ref:EMM 5-11-05 (SOURCE: EMM - Life Limit)
EMM - Life Limit ≈24-Nov-2019RE72-EMM-001 No.5 Bearing Carbon Seal Preformed Packing - Replace
28-Jul-2005Mos
1,818.6 Hrs13,8393,00010,839Hrs
5,949Enc
72 ENG2
Ref:EMM 5-11-05 (SOURCE: EMM - Life Limit)
EMM - Life Limit ≈22-Feb-2021RE72-EMM-002 High Pressure Turbine Stage 2 Nozzle Retaining Ring Sector - Replace
05-Jun-2009Mos
2,417.4 Hrs14,554.83,00011,554.8Hrs
6,355Enc
72 ENG1
Ref:EMM 5-11-05 (SOURCE: EMM - Life Limit)
EMM - Life Limit ≈24-Nov-2019RE72-EMM-002 High Pressure Turbine Stage 2 Nozzle Retaining Ring Sector - Replace
28-Jul-2005Mos
1,818.6 Hrs13,8393,00010,839Hrs
5,949Enc
72 ENG2
Ref:EMM 5-11-05 (SOURCE: EMM - Life Limit)
MandatoryRE (-)88-06-07 Fuel Controls
23-Mar-1988Mos
Hrs
Enc
72 ENG1PER SB 73-05 & SB 73-06Eff: 23-Mar-1988 Not
Applicable
MandatoryRE (-)88-06-07 Fuel Controls
23-Mar-1988Mos
Hrs
Enc
72 ENG2PER SB 73-05 & SB 73-06Eff: 23-Mar-1988 Not
Applicable
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM372/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MandatoryRE (-)97-06-14 Fan Disk
11-Jul-2008Mos
11,411.2Hrs
6,293Enc
72 ENG2BY PART S/N INSTALLEDEff: 27-May-1997 Not
Applicable
MandatoryRE (-)97-06-14 Fan Disk
11-Mar-1997Mos
Hrs
Enc
72 ENG1NEW FAN INSTALLEDEff: 27-May-1997 Not
Applicable
MandatoryRE (-)97-06-15 HPC Stage 1 rotor disk
11-Jul-2008Mos
11,411.2Hrs
6,293Enc
72 ENG2Not Applicable
(NOTE: Engines with high pressure compressor (HPC) stage 1 rotor disks, part number 6040T79G01, installed)
MandatoryRE (-)97-06-15 HPC Stage 1 rotor disk
14-Mar-1997Mos
Hrs
Enc
72 ENG1NEW PART INSTALLEDNot Applicable
(NOTE: Engines with high pressure compressor (HPC) stage 1 rotor disks, part number 6040T79G01, installed)
MandatoryRE (-)99-22-10 High Pressure Compressor (HPC) Spool and Disk
27-Dec-1999Mos
Hrs
Enc
72 ENG1NEW PART INSTALLEDEff: 27-Dec-1999 Not
Applicable
MandatoryRE (-)99-22-10 High Pressure Compressor (HPC) Spool and Disk
27-Dec-1999Mos
Hrs
Enc
72 ENG2Eff: 27-Dec-1999 Complied With
▼ 73 - ENGINE - FUEL AND CONTROL
RE (O/C)Compressor Inlet Temperature Sensor
27-Jun-2005Mos
10,839Hrs10,839
5,949Enc5,949
73 ENG2Overhauled4071T72P01
WYG30324
RE (O/C)Compressor Inlet Temperature Sensor
31-May-2005Mos
10,956Hrs10,956
5,990Enc5,990
73 ENG1Overhauled4071T72P01
WYG30240
RE (O/C)Fuel Distributor
20-Sep-1983Mos
0Hrs
0Enc
73 ENG1UnknownUnknown
RE (O/C)Fuel Distributor
20-Sep-1983Mos
0Hrs
0Enc
73 ENG2UnknownUnknown
RE (O/C)Fuel Flow Indicator
20-Sep-1983Mos
0Hrs
0Ldg
73 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM373/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Fuel Flowmeter
20-Sep-1983Mos
0Hrs
0Ldg
Left73 A/FUnknownUnknown
RE (O/C)Fuel Flowmeter
20-Sep-1983Mos
0Hrs
0Ldg
Right73 A/FUnknownUnknown
RE (O/C)Fuel Heater
27-Jun-2005Mos
10,839Hrs10,839
5,949Enc5,949
73 ENG2Overhauled5023T57P02
JAD05017
RE (O/C)Fuel Heater
31-May-2005Mos
10,956Hrs10,956
5,990Enc5,990
73 ENG1Overhauled5023T57P02
JD05009
RE (O/C)Fuel Pressure Warning Low Switch
20-Sep-1983Mos
0Hrs
0Ldg
Left73 A/FUnknownUnknown
RE (O/C)Fuel Pressure Warning Low Switch
20-Sep-1983Mos
0Hrs
0Ldg
Right73 A/FUnknownUnknown
RE (O/C)Fuel Pump
27-Jun-2005Mos
10,839Hrs
Enc
73 ENG26052T06P05CDWE0453
RE (O/C)Fuel Pump
31-May-2005Mos
10,956Hrs
Enc
73 ENG16052T06P05CDWE0452
RE (O/C)Fuel Temp Indicator
12-Jan-2002Mos
7,973.5Hrs
3,823Ldg
73 A/F600-50919-1182050019M
RE (O/C)Main Fuel Control (MFC)
27-Jun-2005Mos
10,839Hrs
5,949Enc
73 ENG26047T74P13WYG33540
RE (O/C)Main Fuel Control (MFC)
31-May-2005Mos
10,956Hrs8,961
5,990Enc5,136
73 ENG1Overhauled6047T74P13
WYG33573
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM374/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Temperature Bulb
20-Sep-1983Mos
0Hrs
0Ldg
No.173 A/FUnknownUnknown
RE (O/C)Temperature Bulb
20-Sep-1983Mos
0Hrs
0Ldg
No.273 A/FUnknownUnknown
RE (O/C)Temperature Bulb
20-Sep-1983Mos
0Hrs
0Ldg
No.373 A/FUnknownUnknown
RE (O/C)Temperature Bulb
20-Sep-1983Mos
0Hrs
0Ldg
No.473 A/FUnknownUnknown
RecommendedRE (-)601-0216 Modification - Press Fuel Line and N2 Filter Harness - Compatibility with CECO Fuel Pump
Mos
Hrs
Ldg
73 A/F
RecommendedRE (-)601-0216 Rev 1 Modification - Press Fuel Line and N2 Filter Harness - Compatibility with CECO Fuel Pump
01-Oct-1991Mos
Hrs
Ldg
73 A/FEff: 30-Apr-1990 Complied With
RecommendedRE (-)601-0593 Special Check/Modification – Fuel System – Russian and Ukrainian Fuel Requirement
1.1 Years[19-May-2017]19-May-2009Mos
Hrs
Ldg
73 A/FEff: 19-May-2009
RecommendedT (A/R)601-1029 Modification - Engine Fuel Supply - Right Fuel Heater Exhaust Duct
Mos
Hrs
Ldg
73 A/FEff: 07-Sep-1984
RecommendedRE (-)601-1039 Special Check/Modification - Motive Flow Line - Fouling on Variable Guide Vane Bellcrank Clevis
16-Jul-1986Mos
952Hrs
403Ldg
73 A/FComplied With
RecommendedRE (-)601-1039 Rev 1 Special Check/Modification - Motive Flow Line - Fouling on Variable Guide Vane Bellcrank Clevis
Mos
Hrs
Ldg
73 A/F
RecommendedT (A/R)601-1039 Rev 2 Special Check/Modification - Motive Flow Line - Fouling on Variable Guide Vane Bellcrank Clevis
Mos
Hrs
Ldg
73 A/FEff: 18-Sep-1987
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM375/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-1043 Modification - Fuel Low Pressure Warning System - Switch Replacement and/or Clamping
02-May-1988Mos
1,995Hrs
756Ldg
73 A/FEff: 22-Feb-1985 Complied With
RE (-)72-0255 R00 ENGINE - Fan Stator (72-23-00) - Engine Mount Quality Issue
Mos
Hrs
Enc
73 ENG1Eff: 02-Feb-2012
RE (-)72-0255 R00 ENGINE - Fan Stator (72-23-00) - Engine Mount Quality Issue
Mos
Hrs
Enc
73 ENG2Eff: 02-Feb-2012
T (A/R)72-0255 R01 ENGINE - Fan Stator (72-23-00) - Engine Mount Quality Issue
Mos
Hrs
Enc
73 ENG1Eff: 02-Feb-2012
(NOTE: THIS SERVICE BULLETIN IS FOR LIMITED DISTRIBUTION)
T (A/R)72-0255 R01 ENGINE - Fan Stator (72-23-00) - Engine Mount Quality Issue
Mos
Hrs
Enc
73 ENG2Eff: 02-Feb-2012
(NOTE: THIS SERVICE BULLETIN IS FOR LIMITED DISTRIBUTION)
RecommendedRE (-)73-0001 R00 FUEL SYSTEM - Replacement of Flex-Metal Hose Assemblies
Mos
Hrs
Enc
73 ENG1
RecommendedRE (-)73-0001 R00 FUEL SYSTEM - Replacement of Flex-Metal Hose Assemblies
Mos
Hrs
Enc
73 ENG2
RecommendedRE (-)73-0003 R00 FUEL SYSTEM - Servicing/Inspection (73-00-00) - Use of Fuel System Anti-icing Additive and Inspection of Fuel Heater
Mos
Hrs
Enc
73 ENG1Eff: 05-Apr-1985
RecommendedRE (-)73-0003 R00 FUEL SYSTEM - Servicing/Inspection (73-00-00) - Use of Fuel System Anti-icing Additive and Inspection of Fuel Heater
Mos
Hrs
Enc
73 ENG2Eff: 05-Apr-1985
RecommendedRE (-)73-0003 R01 FUEL SYSTEM - Servicing/Inspection (73-00-00) - Use of Fuel System Anti-icing Additive and Inspection of Fuel Heater
Mos
Hrs
Enc
73 ENG1Eff: 17-Jul-1985
RecommendedRE (-)73-0003 R01 FUEL SYSTEM - Servicing/Inspection (73-00-00) - Use of Fuel System Anti-icing Additive and Inspection of Fuel Heater
Mos
Hrs
Enc
73 ENG2Eff: 17-Jul-1985
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM376/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)73-0003 R02 FUEL SYSTEM - Servicing/Inspection (73-00-00) - Use of Fuel System Anti-icing Additive and Inspection of Fuel Heater
Mos
Hrs
Enc
73 ENG1Eff: 15-Nov-1985
RecommendedRE (-)73-0003 R02 FUEL SYSTEM - Servicing/Inspection (73-00-00) - Use of Fuel System Anti-icing Additive and Inspection of Fuel Heater
Mos
Hrs
Enc
73 ENG2Eff: 15-Nov-1985
RecommendedRE (-)73-0003 R03 FUEL SYSTEM - Servicing/Inspection (73-00-00) - Use of Fuel System Anti-icing Additive and Inspection of Fuel Heater
Mos
Hrs
Enc
73 ENG1Eff: 12-Dec-1985
RecommendedRE (-)73-0003 R03 FUEL SYSTEM - Servicing/Inspection (73-00-00) - Use of Fuel System Anti-icing Additive and Inspection of Fuel Heater
Mos
Hrs
Enc
73 ENG2Eff: 12-Dec-1985
RecommendedT (A/R)73-0003 R04 FUEL SYSTEM - Servicing/Inspection (73-00-00) - Use of Fuel System Anti-icing Additive and Inspection of Fuel Heater
Mos
Hrs
Enc
73 ENG1Eff: 26-Nov-2008
RecommendedT (A/R)73-0003 R04 FUEL SYSTEM - Servicing/Inspection (73-00-00) - Use of Fuel System Anti-icing Additive and Inspection of Fuel Heater
Mos
Hrs
Enc
73 ENG2Eff: 26-Nov-2008
RecommendedT (A/R)73-0007 R00 FUEL SYSTEM - Fuel Distributor Assembly: Removal and Replacement
Mos
Hrs
Enc
73 ENG1Eff: 02-Jan-1990
RecommendedT (A/R)73-0007 R00 FUEL SYSTEM - Fuel Distributor Assembly: Removal and Replacement
Mos
Hrs
Enc
73 ENG2Eff: 02-Jan-1990
RecommendedRE (-)73-0008 R01 FUEL SYSTEM - Fuel Injector Coupling Nuts: Inspection and Retorque
Mos
Hrs
Enc
73 ENG1Eff: 14-Jan-1991
Also ConsiderDUE:1. T 100 Hrs | 2. RE -FUEL SYSTEM - Replacement of Loose Fuel Injectors73-0013 R00ENG173
RecommendedRE (-)73-0008 R01 FUEL SYSTEM - Fuel Injector Coupling Nuts: Inspection and Retorque
Mos
Hrs
Enc
73 ENG2Eff: 14-Jan-1991
Also ConsiderDUE:1. T 100 Hrs | 2. RE -FUEL SYSTEM - Replacement of Loose Fuel Injectors73-0013 R00ENG273
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM377/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)73-0009 R00 FUEL SYSTEM - Removal of Nylon Indicator Plug PN JAD 52-01315-1 From Main Fuel Filter Assembly
Mos
Hrs
Enc
73 ENG1Eff: 02-May-1991
(NOTE: All CF34-1A and CF34-3A engines, below serial number 350436 which have indicator plug PN JAD 52-01315-1 installed in main fuel
filter assembly GE PN 5050T60P01 (vendor PN 74D10-6).)
RecommendedRE (-)73-0009 R00 FUEL SYSTEM - Removal of Nylon Indicator Plug PN JAD 52-01315-1 From Main Fuel Filter Assembly
Mos
Hrs
Enc
73 ENG2Eff: 02-May-1991
(NOTE: All CF34-1A and CF34-3A engines, below serial number 350436 which have indicator plug PN JAD 52-01315-1 installed in main fuel
filter assembly GE PN 5050T60P01 (vendor PN 74D10-6).)
RecommendedRE (-)73-0010 R01 FUEL SYSTEM - Improved Main Drive Shaft and Face Seal Ring on CECO Fuel Pumps
Mos
Hrs
Enc
73 ENG1Eff: 21-Apr-1993
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
RecommendedRE (-)73-0010 R01 FUEL SYSTEM - Improved Main Drive Shaft and Face Seal Ring on CECO Fuel Pumps
Mos
Hrs
Enc
73 ENG2Eff: 21-Apr-1993
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
RecommendedRE (-)73-0011 R01 FUEL SYSTEM - Main Fuel Control - Improved Main Fuel Control PN 6047T74P09
Mos
Hrs
Enc
73 ENG1Eff: 26-Mar-1992
RecommendedRE (-)73-0011 R01 FUEL SYSTEM - Main Fuel Control - Improved Main Fuel Control PN 6047T74P09
Mos
Hrs
Enc
73 ENG2Eff: 26-Mar-1992
RecommendedRE (-)73-0012 R00 FUEL SYSTEM - Main Fuel Control - Improved Main Fuel Control PN 6047T74P01, P02, P03, and P07
Mos
Hrs
Enc
73 ENG1Eff: 01-May-1991
Also ConsiderDUE: 06-May-2014, 14,674.8 Hrs1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of...73-A0033 R07ENG173
RecommendedRE (-)73-0012 R00 FUEL SYSTEM - Main Fuel Control - Improved Main Fuel Control PN 6047T74P01, P02, P03, and P07
Mos
Hrs
Enc
73 ENG2Eff: 01-May-1991
Also ConsiderDUE:1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of...73-A0033 R07ENG273
RecommendedRE (-)73-0013 R00 FUEL SYSTEM - Replacement of Loose Fuel Injectors
Mos
Hrs
Enc
73 ENG1Eff: 12-Jun-1991
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM378/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)73-0013 R00 FUEL SYSTEM - Replacement of Loose Fuel Injectors
Mos
Hrs
Enc
73 ENG2Eff: 12-Jun-1991
RecommendedRE (-)73-0014 R02 FUEL SYSTEM - Main Fuel Control PN 6047T74P09 - Rework of CDP Sensor Body Assembly
Mos
Hrs
Enc
73 ENG1Eff: 14-Mar-1994
RecommendedRE (-)73-0014 R02 FUEL SYSTEM - Main Fuel Control PN 6047T74P09 - Rework of CDP Sensor Body Assembly
Mos
Hrs
Enc
73 ENG2Eff: 14-Mar-1994
RecommendedRE (-)73-0015 R01 FUEL SYSTEM - Replacement of the Main Fuel Control To Prevent Flameout Re-occurrence
Mos
Hrs
Enc
73 ENG1Eff: 14-Mar-1994
Also ConsiderDUE:1. RE -FUEL SYSTEM - T2 Sensor Tube and Hose Assembly and Fuel Mani...73-0016 R00ENG173
RecommendedRE (-)73-0015 R01 FUEL SYSTEM - Replacement of the Main Fuel Control To Prevent Flameout Re-occurrence
Mos
Hrs
Enc
73 ENG2Eff: 14-Mar-1994
Also ConsiderDUE:1. RE -FUEL SYSTEM - T2 Sensor Tube and Hose Assembly and Fuel Mani...73-0016 R00ENG273
RecommendedRE (-)73-0016 R00 FUEL SYSTEM - T2 Sensor Tube and Hose Assembly and Fuel Manifolds Fuel Leak Inspection
Mos
Hrs
Enc
73 ENG1Eff: 22-Mar-1994
RecommendedRE (-)73-0016 R00 FUEL SYSTEM - T2 Sensor Tube and Hose Assembly and Fuel Manifolds Fuel Leak Inspection
Mos
Hrs
Enc
73 ENG2Eff: 22-Mar-1994
RecommendedRE (-)73-0017 R00 FUEL SYSTEM - Correction of the Nameplate on Main Fuel Controls
Mos
Hrs
Enc
73 ENG1Eff: 22-Mar-1994
Also ConsiderDUE:1. RE -FUEL SYSTEM - Replacement of the Main Fuel Control To Preven...73-0015 R01ENG173
RecommendedRE (-)73-0017 R00 FUEL SYSTEM - Correction of the Nameplate on Main Fuel Controls
Mos
Hrs
Enc
73 ENG2Eff: 22-Mar-1994
Also ConsiderDUE:1. RE -FUEL SYSTEM - Replacement of the Main Fuel Control To Preven...73-0015 R01ENG273
RecommendedRE (-)73-0019 R00 FUEL SYSTEM - Inspection for Fuel Leaks
Mos
Hrs
Enc
73 ENG1Eff: 29-Sep-1994
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM379/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)73-0019 R00 FUEL SYSTEM - Inspection for Fuel Leaks
Mos
Hrs
Enc
73 ENG2Eff: 29-Sep-1994
RecommendedRE (-)73-0020 R01 FUEL SYSTEM - Deletion of the Thermal Valve Assembly
Mos
Hrs
Enc
73 ENG1Eff: 27-May-1998
RecommendedRE (-)73-0020 R01 FUEL SYSTEM - Deletion of the Thermal Valve Assembly
Mos
Hrs
Enc
73 ENG2Eff: 27-May-1998
RecommendedRE (-)73-0021 R00 FUEL SYSTEM - Inspection and Retorque of Coupling Clamp PN 4024T95P01 and PN 4024T95P03
Mos
Hrs
Enc
73 ENG1Eff: 02-Jun-1995
RecommendedRE (-)73-0021 R00 FUEL SYSTEM - Inspection and Retorque of Coupling Clamp PN 4024T95P01 and PN 4024T95P03
Mos
Hrs
Enc
73 ENG2Eff: 02-Jun-1995
RecommendedRE (-)73-0023 R00 FUEL AND OIL SYSTEM - Inspection/Replacement of Specific Fuel and Lube Hoses and Hose/Tubes Manufactured Between January 1995 and May 1995
Mos
Hrs
Enc
73 ENG1Eff: 26-Nov-1996
RecommendedRE (-)73-0023 R00 FUEL AND OIL SYSTEM - Inspection/Replacement of Specific Fuel and Lube Hoses and Hose/Tubes Manufactured Between January 1995 and May 1995
Mos
Hrs
Enc
73 ENG2Eff: 26-Nov-1996
RecommendedRE (-)73-0026 R01 FUEL SYSTEM - Introduction of Main Fuel Control PNs 6078T55P08/P09/ P10 With Improved VG Cable Bracket
Mos
Hrs
Enc
73 ENG1Eff: 23-Oct-1997
Also ConsiderDUE:1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0044 R03ENG173
Also ConsiderDUE:1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0045 R02ENG173
RecommendedRE (-)73-0026 R01 FUEL SYSTEM - Introduction of Main Fuel Control PNs 6078T55P08/P09/ P10 With Improved VG Cable Bracket
Mos
Hrs
Enc
73 ENG2Eff: 23-Oct-1997
Also ConsiderDUE:1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0044 R03ENG273
Also ConsiderDUE:1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0045 R02ENG273
RecommendedRE (-)73-0027 R00 FUEL SYSTEM - Replacement of Fuel Filter Assembly (PN 5071T70P01)
Mos
Hrs
Enc
73 ENG1Eff: 10-Oct-1995
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM380/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)73-0027 R00 FUEL SYSTEM - Replacement of Fuel Filter Assembly (PN 5071T70P01)
Mos
Hrs
Enc
73 ENG2Eff: 10-Oct-1995
RecommendedRE (-)73-0028 R01 FUEL SYSTEM - Replacement of Fuel Filter Housing
Mos
Hrs
Enc
73 ENG1Eff: 04-Dec-1995
(NOTE: Engines that are in compliance with GE Field Engineering Instruction (FEI) CF34-65, as recorded in the Engine Service Record Book are
considered in compliance with this Service Bulletin and no further action is required.
If an engine has a filter assembly marked with a "R" (for reworked) immediately after the serial number, the filter assembly has been retrofitted
with the correct packings and does not require replacement For all
affected engines with over 3000 hours: Replace filter assembly at next 300 hour inspection, or no later than next scheduled filter replacement.If
filter assembly replacement is not possible or desirable at this time, inspect for fuel leakage, and continue to inspect at each subsequent 300
hour inspection until replacement is accomplished. Suspect leak area is shown in figure 1. The leak check of suspect area should be conducted
within 15 minutes of engine shutdown.For affected engines with less than 3000 hours: Replace the filter assembly at first 3000 hour inspection
interval.)
RecommendedRE (-)73-0028 R01 FUEL SYSTEM - Replacement of Fuel Filter Housing
Mos
Hrs
Enc
73 ENG2Eff: 04-Dec-1995
(NOTE: Engines that are in compliance with GE Field Engineering Instruction (FEI) CF34-65, as recorded in the Engine Service Record Book are
considered in compliance with this Service Bulletin and no further action is required.
If an engine has a filter assembly marked with a "R" (for reworked) immediately after the serial number, the filter assembly has been retrofitted
with the correct packings and does not require replacement For all
affected engines with over 3000 hours: Replace filter assembly at next 300 hour inspection, or no later than next scheduled filter replacement.If
filter assembly replacement is not possible or desirable at this time, inspect for fuel leakage, and continue to inspect at each subsequent 300
hour inspection until replacement is accomplished. Suspect leak area is shown in figure 1. The leak check of suspect area should be conducted
within 15 minutes of engine shutdown.For affected engines with less than 3000 hours: Replace the filter assembly at first 3000 hour inspection
interval.)
Category 9RE (-)73-0029 R00 FUEL SYSTEM Main Fuel Pump PN 6052T06P03/P05, Pulsation Elimination (Cancelled)
Mos
Hrs
Enc
73 ENG1
Category 9RE (-)73-0029 R00 FUEL SYSTEM Main Fuel Pump PN 6052T06P03/P05, Pulsation Elimination (Cancelled)
Mos
Hrs
Enc
73 ENG2
Category 9RE (-)73-0029 R01 FUEL SYSTEM Main Fuel Pump PN 6052T06P03/P05, Pulsation Elimination (Cancelled)
Mos
Hrs
Enc
73 ENG1
Category 9RE (-)73-0029 R01 FUEL SYSTEM Main Fuel Pump PN 6052T06P03/P05, Pulsation Elimination (Cancelled)
Mos
Hrs
Enc
73 ENG2
Cat. 9 - InformationalT (A/R)73-0029 R02 FUEL SYSTEM - Main Fuel Pump PN 6052T06P03/P05 Pulsation Elimination (Cancelled)
Mos
Hrs
Enc
73 ENG1Eff: 21-Mar-2005
(NOTE: Revision 2 is issued to advise overhaul and maintenance facilities and aircraft owners that CF34-BJ S/B 73-0029 is no longer valid. GE is
requesting that operators not comply with this Service Bulletin.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM381/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 9 - InformationalT (A/R)73-0029 R02 FUEL SYSTEM - Main Fuel Pump PN 6052T06P03/P05 Pulsation Elimination (Cancelled)
Mos
Hrs
Enc
73 ENG2Eff: 21-Mar-2005
(NOTE: Revision 2 is issued to advise overhaul and maintenance facilities and aircraft owners that CF34-BJ S/B 73-0029 is no longer valid. GE is
requesting that operators not comply with this Service Bulletin.)
RecommendedRE (-)73-0030 R00 FUEL SYSTEM - Removal and Cleaning of the Main Fuel Control To Improve Cold Soak Throttle Response
Mos
Hrs
Enc
73 ENG1Eff: 11-Jul-1996
RecommendedRE (-)73-0030 R00 FUEL SYSTEM - Removal and Cleaning of the Main Fuel Control To Improve Cold Soak Throttle Response
Mos
Hrs
Enc
73 ENG2Eff: 11-Jul-1996
T (A/R)73-0031 R01 FUEL SYSTEM - Service Introduction Program for Operation of General Electric CF34 Engines Using CIS Fuels and Additives
Mos
Hrs
Enc
73 ENG1Eff: 24-Jan-2002
(NOTE: This Service Bulletin is revised to notify users that this Service Bulletin has been superseded by CF34-BJ 73-0047.)
T (A/R)73-0031 R01 FUEL SYSTEM - Service Introduction Program for Operation of General Electric CF34 Engines Using CIS Fuels and Additives
Mos
Hrs
Enc
73 ENG2Eff: 24-Jan-2002
(NOTE: This Service Bulletin is revised to notify users that this Service Bulletin has been superseded by CF34-BJ 73-0047.)
T (A/R)73-0032 R03 ENGINE FUEL AND CONTROL - Rework of Main Fuel Control to Add Forward Flange Vent Groove
Mos
Hrs
Enc
73 ENG1Eff: 30-Aug-1999
T (A/R)73-0032 R03 ENGINE FUEL AND CONTROL - Rework of Main Fuel Control to Add Forward Flange Vent Groove
Mos
Hrs
Enc
73 ENG2Eff: 30-Aug-1999
RecommendedT (A/R)73-0034 R00 FUEL SYSTEM - Improved Preformed Packings on the Main Fuel Control-to-Fuel Pump Interface
Mos
Hrs
Enc
73 ENG1Eff: 12-Jan-1998
Also ConsiderDUE:1. T - | 2. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspectio...73-A0050 R08ENG173
RecommendedT (A/R)73-0034 R00 FUEL SYSTEM - Improved Preformed Packings on the Main Fuel Control-to-Fuel Pump Interface
Mos
Hrs
Enc
73 ENG2Eff: 12-Jan-1998
Also ConsiderDUE:1. T - | 2. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspectio...73-A0050 R08ENG273
RecommendedRE (-)73-0036 R00 FUEL SYSTEM - Inspection of Main Fuel Filter for Non-Torqued Filter Bowl
Mos
Hrs
Enc
73 ENG1Eff: 03-Dec-1998
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM382/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)73-0036 R00 FUEL SYSTEM - Inspection of Main Fuel Filter for Non-Torqued Filter Bowl
Mos
Hrs
Enc
73 ENG2Eff: 03-Dec-1998
RecommendedT (A/R)73-0038 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of Improved AGB-to-Fuel Pump Clamp Coupling
Mos
Hrs
Enc
73 ENG1Eff: 20-Aug-1999
RecommendedT (A/R)73-0038 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of Improved AGB-to-Fuel Pump Clamp Coupling
Mos
Hrs
Enc
73 ENG2Eff: 20-Aug-1999
Category 5RE (-)73-0041 R00 ENGINE FUEL AND CONTROL Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Relocated PressureRelief Groove
Mos
Hrs
Enc
73 ENG1Eff: 12-Aug-1999
Category 5RE (-)73-0041 R00 ENGINE FUEL AND CONTROL Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Relocated PressureRelief Groove
Mos
Hrs
Enc
73 ENG2Eff: 12-Aug-1999
Cat. 5 - RecommendedRE (-)73-0041 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Relocated Pressure-Relief Groove
Mos
Hrs
Enc
73 ENG1Eff: 01-Nov-1999
Cat. 5 - RecommendedRE (-)73-0041 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Relocated Pressure-Relief Groove
Mos
Hrs
Enc
73 ENG2Eff: 01-Nov-1999
Cat. 5 - RecommendedT (A/R)73-0041 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Relocated Pressure-Relief Groove
Mos
Hrs
Enc
73 ENG1Eff: 06-Dec-2013
Also ConsiderDUE:1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0044 R03ENG173
Also ConsiderDUE:1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0045 R02ENG173
Cat. 5 - RecommendedT (A/R)73-0041 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Relocated Pressure-Relief Groove
Mos
Hrs
Enc
73 ENG2Eff: 06-Dec-2013
Also ConsiderDUE:1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0044 R03ENG273
Also ConsiderDUE:1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0045 R02ENG273
Cat. 6 - RecommendedRE (-)73-0043 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Variable Geometry Actuator PN 5050T37G01
Mos
Hrs
Enc
73 ENG1Eff: 31-Oct-2002
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM383/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 6 - RecommendedRE (-)73-0043 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Variable Geometry Actuator PN 5050T37G01
Mos
Hrs
Enc
73 ENG2Eff: 31-Oct-2002
Cat. 6 - RecommendedRE (-)73-0043 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Variable Geometry Actuator PN 5050T37G01
Mos
Hrs
Enc
73 ENG1Eff: 11-Mar-2003
Cat. 6 - RecommendedRE (-)73-0043 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Variable Geometry Actuator PN 5050T37G01
Mos
Hrs
Enc
73 ENG2Eff: 11-Mar-2003
Cat. 6 - RecommendedRE (-)73-0043 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Variable Geometry Actuator PN 5050T37G01
Mos
Hrs
Enc
73 ENG1Eff: 17-Apr-2003
Cat. 6 - RecommendedRE (-)73-0043 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Variable Geometry Actuator PN 5050T37G01
Mos
Hrs
Enc
73 ENG2Eff: 17-Apr-2003
Cat. 6 - RecommendedT (A/R)73-0043 R03 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Variable Geometry Actuator PN 5050T37G01
Mos
Hrs
Enc
73 ENG1Eff: 07-Apr-2010
Cat. 6 - RecommendedT (A/R)73-0043 R03 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Variable Geometry Actuator PN 5050T37G01
Mos
Hrs
Enc
73 ENG2Eff: 07-Apr-2010
Cat. 6 - RecommendedRE (-)73-0044 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Product Improvement Package
Mos
Hrs
Enc
73 ENG1Eff: 09-Mar-2001
Cat. 6 - RecommendedRE (-)73-0044 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Product Improvement Package
Mos
Hrs
Enc
73 ENG2Eff: 09-Mar-2001
Cat. 6 - RecommendedRE (-)73-0044 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Product Improvement Package
Mos
Hrs
Enc
73 ENG1Eff: 21-Feb-2002
Cat. 6 - RecommendedRE (-)73-0044 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Product Improvement Package
Mos
Hrs
Enc
73 ENG2Eff: 21-Feb-2002
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM384/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 6 - RecommendedRE (-)73-0044 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Product Improvement Package
Mos
Hrs
Enc
73 ENG1Eff: 13-Dec-2012
Cat. 6 - RecommendedRE (-)73-0044 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Product Improvement Package
Mos
Hrs
Enc
73 ENG2Eff: 13-Dec-2012
Cat. 6 - RecommendedRE (-)73-0044 R03 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Product Improvement Package
Mos
Hrs
Enc
73 ENG1Eff: 08-Nov-2013
Cat. 6 - RecommendedRE (-)73-0044 R03 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of CF34 Main Fuel Controls with Product Improvement Package
Mos
Hrs
Enc
73 ENG2Eff: 08-Nov-2013
Cat. 6 - RecommendedRE (-)73-0045 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of Modified Fuel Valve Bushing into MFC
Mos
Hrs
Enc
73 ENG1Eff: 31-Jan-2001
Cat. 6 - RecommendedRE (-)73-0045 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of Modified Fuel Valve Bushing into MFC
Mos
Hrs
Enc
73 ENG2Eff: 31-Jan-2001
Cat. 6 - RecommendedRE (-)73-0045 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of Modified Fuel Valve Bushing into MFC
Mos
Hrs
Enc
73 ENG1Eff: 05-Jul-2001
Cat. 6 - RecommendedRE (-)73-0045 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of Modified Fuel Valve Bushing into MFC
Mos
Hrs
Enc
73 ENG2Eff: 05-Jul-2001
Cat. 6 - RecommendedRE (-)73-0045 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of Modified Fuel Valve Bushing into MFC
Mos
Hrs
Enc
73 ENG1Eff: 06-Dec-2013
Cat. 6 - RecommendedRE (-)73-0045 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduction of Modified Fuel Valve Bushing into MFC
Mos
Hrs
Enc
73 ENG2Eff: 06-Dec-2013
Cat. 2 - RecommendedRE (-)73-0046 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Controls for Throttle Body Leakage
Mos
Hrs
Enc
73 ENG1Eff: 13-Jun-2001
(NOTE: This Service Bulletin is applicable to these CF34 turbofan engines that have the following serial numbers and that have main fuel
controls (MFC) that have not previously complied with CF34-BJ Service Bulletins 73-0042 and 73-0044, or 73-0045)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM385/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 2 - RecommendedRE (-)73-0046 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Controls for Throttle Body Leakage
Mos
Hrs
Enc
73 ENG2Eff: 13-Jun-2001
(NOTE: This Service Bulletin is applicable to these CF34 turbofan engines that have the following serial numbers and that have main fuel
controls (MFC) that have not previously complied with CF34-BJ Service Bulletins 73-0042 and 73-0044, or 73-0045)
Category 9RE (-)73-0047 R00 ENGINE FUEL AND CONTROL Fuel System (730000) CF341A/3A/3A1/3A2/3B TS1 Fuels Fleet Leader Sampling Program (Cancelled)
Mos
Hrs
Enc
73 ENG1Eff: 24-Jan-2002
Category 9RE (-)73-0047 R00 ENGINE FUEL AND CONTROL Fuel System (730000) CF341A/3A/3A1/3A2/3B TS1 Fuels Fleet Leader Sampling Program (Cancelled)
Mos
Hrs
Enc
73 ENG2Eff: 24-Jan-2002
Cat. 7 - OptionalRE (-)73-0047 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - CF34-1A/-3A/-3A1/-3A2/-3B TS-1 Fuels Fleet Leader Sampling Program (Cancelled)
Mos
Hrs
Enc
73 ENG1Eff: 30-Mar-2006
(NOTE: This Service Bulletin is superseded by CF34-BJ S/B 73-0060.)
Cat. 7 - OptionalRE (-)73-0047 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - CF34-1A/-3A/-3A1/-3A2/-3B TS-1 Fuels Fleet Leader Sampling Program (Cancelled)
Mos
Hrs
Enc
73 ENG2Eff: 30-Mar-2006
(NOTE: This Service Bulletin is superseded by CF34-BJ S/B 73-0060.)
Cat. 9 - InformationalT (A/R)73-0047 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - CF34-1A/-3A/-3A1/-3A2/-3B TS-1 Fuels Fleet Leader Sampling Program (Cancelled)
Mos
Hrs
Enc
73 ENG1Eff: 30-Aug-2007
(NOTE: This Service Bulletin is superseded by CF34-BJ S/B 73-0060.)
Cat. 9 - InformationalT (A/R)73-0047 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - CF34-1A/-3A/-3A1/-3A2/-3B TS-1 Fuels Fleet Leader Sampling Program (Cancelled)
Mos
Hrs
Enc
73 ENG2Eff: 30-Aug-2007
(NOTE: This Service Bulletin is superseded by CF34-BJ S/B 73-0060.)
Cat. 8 - InformationalT (A/R)73-0048 R00 ENGINE FUEL AND CONTROL - Variable Geometry Actuation System (73-00-00) - Spare Parts Release for Variable Geometry Actuator Repair Kit
Mos
Hrs
Enc
73 ENG1Eff: 31-Jul-2002
Cat. 8 - InformationalT (A/R)73-0048 R00 ENGINE FUEL AND CONTROL - Variable Geometry Actuation System (73-00-00) - Spare Parts Release for Variable Geometry Actuator Repair Kit
Mos
Hrs
Enc
73 ENG2Eff: 31-Jul-2002
Cat. 2 - RecommendedRE (-)73-0049 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Selected CF34 Main Fuel Controls
Mos
Hrs
Enc
73 ENG1Eff: 21-Feb-2003
Cat. 2 - RecommendedRE (-)73-0049 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Selected CF34 Main Fuel Controls
Mos
Hrs
Enc
73 ENG2Eff: 21-Feb-2003
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM386/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 8 - InformationalRE (-)73-0049 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Selected CF34 Main Fuel Controls
Mos
Hrs
Enc
73 ENG1Eff: 29-May-2003
Cat. 8 - InformationalRE (-)73-0049 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Selected CF34 Main Fuel Controls
Mos
Hrs
Enc
73 ENG2Eff: 29-May-2003
Cat. 2 - RecommendedRE (-)73-0049 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Selected CF34 Main Fuel Controls
Mos
Hrs
Enc
73 ENG1Eff: 02-Apr-2004
Cat. 2 - RecommendedRE (-)73-0049 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Selected CF34 Main Fuel Controls
Mos
Hrs
Enc
73 ENG2Eff: 02-Apr-2004
Cat. 2 - RecommendedRE (-)73-0049 R03 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Selected CF34 Main Fuel Controls
Mos
Hrs
Enc
73 ENG1Eff: 06-Dec-2013
Cat. 2 - RecommendedRE (-)73-0049 R03 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Selected CF34 Main Fuel Controls
Mos
Hrs
Enc
73 ENG2Eff: 06-Dec-2013
Cat. 7 - OptionalRE (-)73-0051 R00 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 6078T63P07 and PN 6078T64P07
Mos
Hrs
Enc
73 ENG1Eff: 15-Jun-2004
(NOTE: GE recommends you do this Service Bulletin at next shop visit field or overhaul, beyond 10,000 hours, of the engine.)
Cat. 7 - OptionalRE (-)73-0051 R00 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 6078T63P07 and PN 6078T64P07
Mos
Hrs
Enc
73 ENG2Eff: 15-Jun-2004
(NOTE: GE recommends you do this Service Bulletin at next shop visit field or overhaul, beyond 10,000 hours, of the engine.)
Cat. 7 - OptionalRE (-)73-0051 R01 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 6078T63P07 and PN 6078T64P07
Mos
Hrs
Enc
73 ENG1Eff: 15-Dec-2005
(NOTE: GE recommends you do this Service Bulletin at next shop visit field or overhaul, beyond 10,000 hours, of the engine.)
Cat. 7 - OptionalRE (-)73-0051 R01 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 6078T63P07 and PN 6078T64P07
Mos
Hrs
Enc
73 ENG2Eff: 15-Dec-2005
(NOTE: GE recommends you do this Service Bulletin at next shop visit field or overhaul, beyond 10,000 hours, of the engine.)
Cat. 7 - OptionalRE (-)73-0051 R02 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 5083T10P03 PN 5083T11P03 PN 5083T12P03 PN 6078T63P07 and PN 6078T64P07
Mos
Hrs
Enc
73 ENG1Eff: 02-Nov-2006
(NOTE: GE recommends you do this Service Bulletin at next shop visit field or overhaul, beyond 10,000 hours, of the engine.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM387/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 7 - OptionalRE (-)73-0051 R02 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 5083T10P03 PN 5083T11P03 PN 5083T12P03 PN 6078T63P07 and PN 6078T64P07
Mos
Hrs
Enc
73 ENG2Eff: 02-Nov-2006
(NOTE: GE recommends you do this Service Bulletin at next shop visit field or overhaul, beyond 10,000 hours, of the engine.)
Cat. 5 - RecommendedRE (-)73-0051 R03 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 5083T10P03 PN 5083T11P03 PN 5083T12P03 PN 6078T63P07 and PN 6078T64P07
Mos
Hrs
Enc
73 ENG1Eff: 23-May-2008
(NOTE: GE recommends you do this Service Bulletin at next shop visit field or overhaul, beyond 10,000 hours, of the engine.)
Cat. 5 - RecommendedRE (-)73-0051 R03 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 5083T10P03 PN 5083T11P03 PN 5083T12P03 PN 6078T63P07 and PN 6078T64P07
Mos
Hrs
Enc
73 ENG2Eff: 23-May-2008
(NOTE: GE recommends you do this Service Bulletin at next shop visit field or overhaul, beyond 10,000 hours, of the engine.)
Cat. 3 - RecommendedT (ESV)73-0051 R04 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 5083T10P03 PN 5083T11P03 PN 5083T12P03 PN 6078T63P07 and PN 6078T64P07
Mos
Hrs
Enc
73 ENG1Eff: 22-Jun-2009
(NOTE: GE recommends you do this Service Bulletin at next shop visit field or overhaul, beyond 10,000 hours, of the engine.)
Cat. 3 - RecommendedT (ESV)73-0051 R04 FUEL SYSTEM - Fuel Manifold (73-00-00) - Introduction of Fuel Injectors PN 5083T10P03 PN 5083T11P03 PN 5083T12P03 PN 6078T63P07 and PN 6078T64P07
Mos
Hrs
Enc
73 ENG2Eff: 22-Jun-2009
(NOTE: GE recommends you do this Service Bulletin at next shop visit field or overhaul, beyond 10,000 hours, of the engine.)
Cat. 5 - RecommendedRE (-)73-0055 R00 FUEL SYSTEM - (73-00-00) - Actuator Hose Fire Sleeve Improvement
Mos
Hrs
Enc
73 ENG1Eff: 25-Oct-2006
(NOTE: Revision 01 is to inform aircraft owners that Service Bulletin CF34-BJ S/B 73-0055 has been superseded by CF34-BJ S/B 73-0056)
Cat. 5 - RecommendedRE (-)73-0055 R00 FUEL SYSTEM - (73-00-00) - Actuator Hose Fire Sleeve Improvement
Mos
Hrs
Enc
73 ENG2Eff: 25-Oct-2006
(NOTE: Revision 01 is to inform aircraft owners that Service Bulletin CF34-BJ S/B 73-0055 has been superseded by CF34-BJ S/B 73-0056)
Cat. 5 - RecommendedRE (-)73-0055 R01 FUEL SYSTEM - (73-00-00) - Actuator Hose Fire Sleeve Improvement
Mos
Hrs
Enc
73 ENG1Eff: 06-Feb-2007
(NOTE: Revision 01 is to inform aircraft owners that Service Bulletin CF34-BJ S/B 73-0055 has been superseded by CF34-BJ S/B 73-0056)
Cat. 5 - RecommendedT (A/R)73-0055 R01 FUEL SYSTEM - (73-00-00) - Actuator Hose Fire Sleeve Improvement
Mos
Hrs
Enc
73 ENG2Eff: 06-Feb-2007
(NOTE: Revision 01 is to inform aircraft owners that Service Bulletin CF34-BJ S/B 73-0055 has been superseded by CF34-BJ S/B 73-0056)
Cat. 3 - RecommendedRE (-)73-0056 R00 FUEL SYSTEM - (73-00-00) - Introduction of Improved VG Actuator Hose (Final Fix)
Mos
Hrs
Enc
73 ENG1Eff: 06-Feb-2007
Cat. 3 - RecommendedRE (-)73-0056 R00 FUEL SYSTEM - (73-00-00) - Introduction of Improved VG Actuator Hose (Final Fix)
Mos
Hrs
Enc
73 ENG2Eff: 06-Feb-2007
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM388/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 3 - RecommendedRE (-)73-0056 R01 FUEL SYSTEM - (73-00-00) - Introduction of Improved VG Actuator Hose (Final Fix)
Mos
Hrs
Enc
73 ENG1Eff: 02-Aug-2007
Cat. 3 - RecommendedT (A/R)73-0056 R01 FUEL SYSTEM - (73-00-00) - Introduction of Improved VG Actuator Hose (Final Fix)
Mos
Hrs
Enc
73 ENG2Eff: 02-Aug-2007
Cat. 9 - InformationalRE (-)73-0060 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Fuel and Additives - Requirements for and Approval of
Mos
Hrs
Enc
73 ENG1Eff: 30-Aug-2007
Cat. 9 - InformationalRE (-)73-0060 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Fuel and Additives - Requirements for and Approval of
Mos
Hrs
Enc
73 ENG2Eff: 30-Aug-2007
Cat. 9 - InformationalRE (-)73-0060 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Fuel and Additives - Requirements for and Approval of
Mos
Hrs
Enc
73 ENG1Eff: 14-Jul-2011
Cat. 9 - InformationalRE (-)73-0060 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Fuel and Additives - Requirements for and Approval of
Mos
Hrs
Enc
73 ENG2Eff: 14-Jul-2011
Cat. 9 - InformationalT (-)73-0060 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Fuel and Additives - Requirements for and Approval of
Mos
Hrs
Enc
73 ENG1Eff: 22-Jun-2012
Cat. 9 - InformationalT (-)73-0060 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Fuel and Additives - Requirements for and Approval of
Mos
Hrs
Enc
73 ENG2Eff: 22-Jun-2012
Category 9T (A/R)73-0060 R03 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Fuel and Additives - Requirements for and Approval of
Mos
Hrs
Enc
73 ENG1Eff: 20-Nov-2015
Category 9T (A/R)73-0060 R03 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Fuel and Additives - Requirements for and Approval of
Mos
Hrs
Enc
73 ENG2Eff: 20-Nov-2015
Cat. 2 - RecommendedRE (-)73-0062 R00 ENGINE - Fuel System (73-00-00) - Inspection of Connection Orientation Between the Aft Actuator Head Hose Assembly and the Main Fuel Control
Mos
Hrs
Enc
73 ENG1Eff: 01-Apr-2008
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM389/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 2 - RecommendedRE (-)73-0062 R00 ENGINE - Fuel System (73-00-00) - Inspection of Connection Orientation Between the Aft Actuator Head Hose Assembly and the Main Fuel Control
Mos
Hrs
Enc
73 ENG2Eff: 01-Apr-2008
Cat. 2 - RecommendedRE (-)73-0062 R01 ENGINE - Fuel System (73-00-00) - Inspection of Connection Orientation Between the Aft Actuator Head Hose Assembly and the Main Fuel Control
Mos
Hrs
Enc
73 ENG1Eff: 01-Jul-2008
Cat. 2 - RecommendedRE (-)73-0062 R01 ENGINE - Fuel System (73-00-00) - Inspection of Connection Orientation Between the Aft Actuator Head Hose Assembly and the Main Fuel Control
Mos
Hrs
Enc
73 ENG2Eff: 01-Jul-2008
Cat. 2 - RecommendedRE (-)73-0062 R02 ENGINE - Fuel System (73-00-00) - Inspection of Connection Orientation Between the Aft Actuator Head Hose Assembly and the Main Fuel Control
Mos
Hrs
Enc
73 ENG1Eff: 27-Aug-2008
Cat. 2 - RecommendedRE (-)73-0062 R02 ENGINE - Fuel System (73-00-00) - Inspection of Connection Orientation Between the Aft Actuator Head Hose Assembly and the Main Fuel Control
Mos
Hrs
Enc
73 ENG2Eff: 27-Aug-2008
Cat. 2 - RecommendedRE (-)73-0063 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of High Time Fuel Valve Thrust Bushing and Clip
Mos
Hrs
Enc
73 ENG1Eff: 09-Feb-2012
(NOTE: Based on field event history, it is recommended that this Service Bulletin be accomplished before the MFC thrust bushing and clip have
accumulated more than 10,000 hours of field service. If utilization history (hours) of the bushing and clip are unknown, it is recommended that
this Service Bulletin be incorporated at the next MFC shop visit.Design improvements introduced per CF34-BJ S/B 73-0044 are available for
some models and would eliminate the need for this Service Bulletin. If CF34-BJ S/B 73-0044 is not accomplished or is not applicable, this
Service Bulletin should continue to be repeated per the described compliance recommendation.)
Cat. 2 - RecommendedRE (-)73-0063 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of High Time Fuel Valve Thrust Bushing and Clip
Mos
Hrs
Enc
73 ENG2Eff: 09-Feb-2012
(NOTE: Based on field event history, it is recommended that this Service Bulletin be accomplished before the MFC thrust bushing and clip have
accumulated more than 10,000 hours of field service. If utilization history (hours) of the bushing and clip are unknown, it is recommended that
this Service Bulletin be incorporated at the next MFC shop visit.Design improvements introduced per CF34-BJ S/B 73-0044 are available for
some models and would eliminate the need for this Service Bulletin. If CF34-BJ S/B 73-0044 is not accomplished or is not applicable, this
Service Bulletin should continue to be repeated per the described compliance recommendation.)
Cat. 3 - RecommendedRE (-)73-0063 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of High Time Fuel Valve Thrust Bushing and Clip
Mos
Hrs
Enc
73 ENG1Eff: 31-May-2013
Cat. 3 - RecommendedRE (-)73-0063 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of High Time Fuel Valve Thrust Bushing and Clip
Mos
Hrs
Enc
73 ENG2Eff: 31-May-2013
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM390/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Category 6RE (-)73-0064 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Min Speed Adjustment Lever
Mos
Hrs
Enc
73 ENG1Eff: 04-Aug-2015
(AVG MAN HRS: 2)
Category 6RE (-)73-0064 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Min Speed Adjustment Lever
Mos
Hrs
Enc
73 ENG2Eff: 04-Aug-2015
(AVG MAN HRS: 2)
MRB ≈24-Nov-2019RE73-10-11-204 Fuel Pump Assembly - General Visual Inspection of the engine fuel pump assembly
27-Jun-2005Mos
1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs
Enc
(PKG 3000 Eng Hour)
73 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈24-Nov-2019RE73-10-11-204 Fuel Pump Assembly - General Visual Inspection of the engine fuel pump assembly
31-May-2005Mos
1,818.6 Hrs (+40)13,956-/+403,00010,956Hrs
Enc
(PKG 3000 Eng Hour)
73 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈25-Sep-2016RE73-10-16-208 Fuel Heater Assembly - Check for evidence of leakage from fuel heater
10-Feb-2016Mos
300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs
6,769Enc
(PKG 300 Eng Hour)
73 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈25-Sep-2016RE73-10-16-208 Fuel Heater Assembly - Check for evidence of leakage from fuel heater
10-Feb-2016Mos
300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs
6,728Enc
(PKG 300 Eng Hour)
73 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈25-Sep-2016RE73-10-21-202 Fuel Filter Assembly - Check bypass indicator and carry out a visual check of mounting bracket
10-Feb-2016Mos
300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs
6,728Enc
(PKG 300 Eng Hour)
73 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15) (NOTE: If bypass indicator is protruding check fuel filter element.)
MRB ≈25-Sep-2016RE73-10-21-202 Fuel Filter Assembly - Check bypass indicator and carry out a visual check of mounting bracket
10-Feb-2016Mos
300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs
6,769Enc
(PKG 300 Eng Hour)
73 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15) (NOTE: If bypass indicator is protruding check fuel filter element.)
MRB ≈10-May-2017RE73-10-21-203 Fuel Filter Assembly - Check Fuel filter element
10-Feb-2016Mos
600 Hrs (+40)(12,737.4)-/+4060012,137.4Hrs
6,769Enc
(PKG 600 Eng Hour)
73 ENG1
(SOURCE: TLMC 05-20-15) (NOTE: Install new fuel filter element.)
MRB ≈03-May-2017RE73-10-21-203 Fuel Filter Assembly - Check Fuel filter element
10-Feb-2016Mos
590.8 Hrs (+40)(12,611.2)-/+4060012,020.4Hrs
6,728Enc
(PKG 600 Eng Hour)
73 ENG2
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15) (NOTE: Install new fuel filter element.)
MRB ≈22-Feb-2021RE73-20-11-206 Fuel Control Unit - General Visual Inspection of main fuel control assembly
05-Jun-2009Mos
2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs
Enc
(PKG 3000 Eng Hour)
73 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM391/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈24-Nov-2019RE73-20-11-206 Fuel Control Unit - General Visual Inspection of main fuel control assembly
28-Jul-2005Mos
1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs
Enc
(PKG 3000 Eng Hour)
73 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈25-Sep-2016RE73-20-16-210 N1 Speed Control Amplifier - Visual Check of control amplifier isolators
10-Feb-2016Mos
300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs
6,769Enc
(PKG 300 Eng Hour)
73 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈25-Sep-2016RE73-20-16-210 N1 Speed Control Amplifier - Visual Check of control amplifier isolators
10-Feb-2016Mos
300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs
6,728Enc
(PKG 300 Eng Hour)
73 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
Recommended - AlertRE (-)73-A0032 REV 2 ENGINE FUEL AND CONTROL - Rework of Main Fuel Control to Add Forward Flange Vent Groove
Mos
Hrs
Enc
73 ENG1
Recommended - AlertRE (-)73-A0032 REV 2 ENGINE FUEL AND CONTROL - Rework of Main Fuel Control to Add Forward Flange Vent Groove
Mos
Hrs
Enc
73 ENG2
AlertRE (-)73-A0033 R00 ENGINE FUEL AND CONTROL Fuel System (730000) Rework of Main Fuel Control for Overspeed Protection
Mos
Hrs
Enc
73 ENG1Eff: 21-Nov-1997
AlertRE (-)73-A0033 R00 ENGINE FUEL AND CONTROL Fuel System (730000) Rework of Main Fuel Control for Overspeed Protection
Mos
Hrs
Enc
73 ENG2Eff: 21-Nov-1997
AlertRE (-)73-A0033 R01 ENGINE FUEL AND CONTROL Fuel System (730000) Rework of Main Fuel Control for Overspeed Protection
Mos
Hrs
Enc
73 ENG1Eff: 29-May-1998
AlertRE (-)73-A0033 R01 ENGINE FUEL AND CONTROL Fuel System (730000) Rework of Main Fuel Control for Overspeed Protection
Mos
Hrs
Enc
73 ENG2Eff: 29-May-1998
AlertRE (-)73-A0033 R02 ENGINE FUEL AND CONTROL Fuel System (730000) Rework of Main Fuel Control for Overspeed Protection
Mos
Hrs
Enc
73 ENG1Eff: 09-Mar-1999
AlertRE (-)73-A0033 R02 ENGINE FUEL AND CONTROL Fuel System (730000) Rework of Main Fuel Control for Overspeed Protection
Mos
Hrs
Enc
73 ENG2Eff: 09-Mar-1999
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM392/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AlertRE (-)73-A0033 R03 ENGINE FUEL AND CONTROL Fuel System (730000) Rework of Main Fuel Control for Overspeed Protection
Mos
Hrs
Enc
73 ENG1Eff: 09-Sep-1999
AlertRE (-)73-A0033 R03 ENGINE FUEL AND CONTROL Fuel System (730000) Rework of Main Fuel Control for Overspeed Protection
Mos
Hrs
Enc
73 ENG2Eff: 09-Sep-1999
Cat. 1 - RecommendedRE (-)73-A0033 R04 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Main Fuel Control for Overspeed Protection
Mos
Hrs
Enc
73 ENG1Eff: 01-Nov-1999
Cat. 1 - RecommendedRE (-)73-A0033 R04 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Main Fuel Control for Overspeed Protection
Mos
Hrs
Enc
73 ENG2Eff: 01-Nov-1999
Cat. 1 - RecommendedRE (-)73-A0033 R05 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Main Fuel Control for Overspeed Protection
Mos
Hrs
Enc
73 ENG1Eff: 13-Sep-2004
Cat. 1 - RecommendedRE (-)73-A0033 R05 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Main Fuel Control for Overspeed Protection
Mos
Hrs
Enc
73 ENG2Eff: 13-Sep-2004
Cat. 1 - RecommendedRE (-)73-A0033 R06 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Main Fuel Control for Overspeed Protection
Mos
Hrs
Enc
73 ENG1Eff: 02-Dec-2004
Cat. 1 - RecommendedRE (-)73-A0033 R06 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Main Fuel Control for Overspeed Protection
Mos
Hrs
Enc
73 ENG2Eff: 02-Dec-2004
Cat. 1 - RecommendedRE (-)73-A0033 R07 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Main Fuel Control for Overspeed Protection
OVD[06-May-2014]Mos
2,537.4 Hrs[14,674.8]Hrs
Enc
73 ENG1Eff: 06-May-2009
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0041 R02ENG173
Also ConsiderDUE:1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0044 R03ENG173
Also ConsiderDUE:1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0045 R02ENG173
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM393/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 1 - RecommendedRE (-)73-A0033 R07 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Rework of Main Fuel Control for Overspeed Protection
Mos
Hrs
Enc
73 ENG2Eff: 06-May-2009
Also ConsiderDUE:1. T A/R | 2. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0041 R02ENG273
Also ConsiderDUE:1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0044 R03ENG273
Also ConsiderDUE:1. RE -ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Introduct...73-0045 R02ENG273
RecommendedRE (-)73-A0035 R01 FUEL SYSTEM - Inspection for Possible Missing Fuel Filter Plug
Mos
Hrs
Enc
73 ENG1Eff: 02-Dec-1998
(NOTE: Main fuel filters PN 5050T60P01 are of two different configurations. One configuration has two filter housing ports that are plugged
and safety-wired and the other configuration does not have ports that require plugs and safety wire. This Service Bulletin applies to these CF34
turbofan engines that have a main fuel filter PN 5050T60P01 that is equipped with filter housing ports and plugs)
RecommendedRE (-)73-A0035 R01 FUEL SYSTEM - Inspection for Possible Missing Fuel Filter Plug
Mos
Hrs
Enc
73 ENG2Eff: 02-Dec-1998
(NOTE: Main fuel filters PN 5050T60P01 are of two different configurations. One configuration has two filter housing ports that are plugged
and safety-wired and the other configuration does not have ports that require plugs and safety wire. This Service Bulletin applies to these CF34
turbofan engines that have a main fuel filter PN 5050T60P01 that is equipped with filter housing ports and plugs)
RecommendedRE (-)73-A0037 R00 FUEL SYSTEM - Replacement of Selected CF34 Main Fuel Controls
Mos
Hrs
Enc
73 ENG1Eff: 22-Jan-1999
RecommendedRE (-)73-A0037 R00 FUEL SYSTEM - Replacement of Selected CF34 Main Fuel Controls
Mos
Hrs
Enc
73 ENG2Eff: 22-Jan-1999
RecommendedRE (-)73-A0039 R00 FUEL SYSTEM - Inspection and Replacement of Main Fuel Filter PN 4106T62P01
Mos
Hrs
Enc
73 ENG1Eff: 26-Mar-1999
RecommendedRE (-)73-A0039 R00 FUEL SYSTEM - Inspection and Replacement of Main Fuel Filter PN 4106T62P01
Mos
Hrs
Enc
73 ENG2Eff: 26-Mar-1999
Cat. 2 - RecommendedRE (-)73-A0040 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Buna-N Material Preformed Packing
Mos
Hrs
Enc
73 ENG1Eff: 07-Jul-1999
(NOTE: The improvement described in this Service Bulletin has been introduced on these CF34 turbofan production engines. However, if the
main fuel control was replaced in the field using Buna-N material preformed packings, the packings must be replaced. CF34-3A1 engines,
serial numbers 807515 and up CF34-3B engines, serial numbers 872272 and up.)
Cat. 2 - RecommendedRE (-)73-A0040 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Replacement of Buna-N Material Preformed Packing
Mos
Hrs
Enc
73 ENG2Eff: 07-Jul-1999
(NOTE: The improvement described in this Service Bulletin has been introduced on these CF34 turbofan production engines. However, if the
main fuel control was replaced in the field using Buna-N material preformed packings, the packings must be replaced. CF34-3A1 engines,
serial numbers 807515 and up CF34-3B engines, serial numbers 872272 and up.)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM394/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 2 - RecommendedRE (-)73-A0050 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG1Eff: 26-Jul-2004
Cat. 2 - RecommendedRE (-)73-A0050 R00 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG2Eff: 26-Jul-2004
Cat. 2 - RecommendedRE (-)73-A0050 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG1Eff: 02-Dec-2004
Cat. 2 - RecommendedRE (-)73-A0050 R01 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG2Eff: 02-Dec-2004
Cat. 2 - RecommendedRE (-)73-A0050 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG1Eff: 20-Jan-2006
Cat. 2 - RecommendedRE (-)73-A0050 R02 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG2Eff: 20-Jan-2006
Cat. 2 - RecommendedRE (-)73-A0050 R03 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG1Eff: 10-Oct-2007
Cat. 2 - RecommendedRE (-)73-A0050 R03 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG2Eff: 10-Oct-2007
Cat. 2 - RecommendedRE (-)73-A0050 R04 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG1Eff: 25-Apr-2008
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM395/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 2 - RecommendedRE (-)73-A0050 R04 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG2Eff: 25-Apr-2008
Cat. 2 - RecommendedRE (-)73-A0050 R05 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG1Eff: 05-Jan-2011
(NOTE: This Alert Service Bulletin is applicable to all CF34-1A, -3A, -3A1, -3A2, -3B, turbofan engine main fuel controls (MFCs) and main fuel
pumps (MFPs).
These regions apply to operators re-fueling in that region more than 50 percent of the time. For MFCs that have already accumulated the
operating hours bellow, do within 500 operating hours from the issue date of this Alert Service Bulletin. (b) Repeat this Service Bulletin
inspection procedure at intervals shown bellow. Region/Country Inspection Interval of MFC Asia (1) 4,000 operating hours- China (2, 3, 4)
Shop visit or 20,000 operating hours- India (2, 3, 4) Shop visit or 20,000 operating hours- Japan 1,500 operating hours Middle East (2) 10,000
operating hours Commonwealth of Independent States (CIS) (2) 10,000 operating hours Africa (2) 10,000 operating hours North America (2, 3,
4) Shop visit or 20,000 operating hours Central America and the Caribbean (1) 10,000 operating hours- US Virgin Islands 4,000 operating
hours South America (2) 10,000 operating hours Europe (2) 10,000 operating hours Australia (2) 10,000 operating hours Unknown 1,500
operating hours 1 Exceptions to the Asian, Central American and the Caribbean regions are provided below. 2 If the aircraft is re-fueled in
the Asian region more than 50 percent of the time since the initial Service Bulletin inspection, re-inspect per the Asian region inspection
intervals. 3 If the aircraft is re-fueled outside this region since the initial Service Bulletin inspection, and has not been operated in the Asian
region, re-inspect every 10,000 operating hours. 4 Inspect at every shop visit or 20,000 operating hours, whichever occurs later.)
Cat. 2 - RecommendedRE (-)73-A0050 R05 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG2Eff: 05-Jan-2011
(NOTE: This Alert Service Bulletin is applicable to all CF34-1A, -3A, -3A1, -3A2, -3B, turbofan engine main fuel controls (MFCs) and main fuel
pumps (MFPs).
These regions apply to operators re-fueling in that region more than 50 percent of the time. For MFCs that have already accumulated the
operating hours bellow, do within 500 operating hours from the issue date of this Alert Service Bulletin. (b) Repeat this Service Bulletin
inspection procedure at intervals shown bellow. Region/Country Inspection Interval of MFC Asia (1) 4,000 operating hours- China (2, 3, 4)
Shop visit or 20,000 operating hours- India (2, 3, 4) Shop visit or 20,000 operating hours- Japan 1,500 operating hours Middle East (2) 10,000
operating hours Commonwealth of Independent States (CIS) (2) 10,000 operating hours Africa (2) 10,000 operating hours North America (2, 3,
4) Shop visit or 20,000 operating hours Central America and the Caribbean (1) 10,000 operating hours- US Virgin Islands 4,000 operating
hours South America (2) 10,000 operating hours Europe (2) 10,000 operating hours Australia (2) 10,000 operating hours Unknown 1,500
operating hours 1 Exceptions to the Asian, Central American and the Caribbean regions are provided below. 2 If the aircraft is re-fueled in
the Asian region more than 50 percent of the time since the initial Service Bulletin inspection, re-inspect per the Asian region inspection
intervals. 3 If the aircraft is re-fueled outside this region since the initial Service Bulletin inspection, and has not been operated in the Asian
region, re-inspect every 10,000 operating hours. 4 Inspect at every shop visit or 20,000 operating hours, whichever occurs later.)
Cat. 2 - RecommendedRE (-)73-A0050 R06 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG1Eff: 28-Sep-2011
Cat. 2 - RecommendedRE (-)73-A0050 R06 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG2Eff: 28-Sep-2011
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM396/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 2 - RecommendedRE (-)73-A0050 R07 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG1Eff: 05-Dec-2011
Cat. 2 - RecommendedRE (-)73-A0050 R07 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG2Eff: 05-Dec-2011
Cat. 2 - RecommendedT (-)73-A0050 R08 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG1Eff: 26-Jul-2004
(NOTE: This Alert Service Bulletin is applicable to all CF34-1A, -3A, -3A1, -3A2, -3B, turbofan engine main fuel controls (MFCs) and main fuel
pumps (MFPs).
These regions apply to operators re-fueling in that region more than 50 percent of the time. For MFCs that have already accumulated the
operating hours bellow, do within 500 operating hours from the issue date of this Alert Service Bulletin. (b) Repeat this Service Bulletin
inspection procedure at intervals shown bellow. Region/Country Inspection Interval of MFC Asia (1) 4,000 operating hours- China (2, 3, 4)
Shop visit or 20,000 operating hours- India (2, 3, 4) Shop visit or 20,000 operating hours- Japan 1,500 operating hours Middle East (2) 10,000
operating hours Commonwealth of Independent States (CIS) (2) 10,000 operating hours Africa (2) 10,000 operating hours North America (2, 3,
4) Shop visit or 20,000 operating hours Central America and the Caribbean (1) 10,000 operating hours- US Virgin Islands 4,000 operating
hours South America (2) 10,000 operating hours Europe (2) 10,000 operating hours Australia (2) 10,000 operating hours Unknown 1,500
operating hours 1 Exceptions to the Asian, Central American and the Caribbean regions are provided below. 2 If the aircraft is re-fueled in
the Asian region more than 50 percent of the time since the initial Service Bulletin inspection, re-inspect per the Asian region inspection
intervals. 3 If the aircraft is re-fueled outside this region since the initial Service Bulletin inspection, and has not been operated in the Asian
region, re-inspect every 10,000 operating hours. 4 Inspect at every shop visit or 20,000 operating hours, whichever occurs later.)
Cat. 2 - RecommendedT (-)73-A0050 R08 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
Hrs
Enc
73 ENG2Eff: 26-Jul-2004
(NOTE: This Alert Service Bulletin is applicable to all CF34-1A, -3A, -3A1, -3A2, -3B, turbofan engine main fuel controls (MFCs) and main fuel
pumps (MFPs).
These regions apply to operators re-fueling in that region more than 50 percent of the time. For MFCs that have already accumulated the
operating hours bellow, do within 500 operating hours from the issue date of this Alert Service Bulletin. (b) Repeat this Service Bulletin
inspection procedure at intervals shown bellow. Region/Country Inspection Interval of MFC Asia (1) 4,000 operating hours- China (2, 3, 4)
Shop visit or 20,000 operating hours- India (2, 3, 4) Shop visit or 20,000 operating hours- Japan 1,500 operating hours Middle East (2) 10,000
operating hours Commonwealth of Independent States (CIS) (2) 10,000 operating hours Africa (2) 10,000 operating hours North America (2, 3,
4) Shop visit or 20,000 operating hours Central America and the Caribbean (1) 10,000 operating hours- US Virgin Islands 4,000 operating
hours South America (2) 10,000 operating hours Europe (2) 10,000 operating hours Australia (2) 10,000 operating hours Unknown 1,500
operating hours 1 Exceptions to the Asian, Central American and the Caribbean regions are provided below. 2 If the aircraft is re-fueled in
the Asian region more than 50 percent of the time since the initial Service Bulletin inspection, re-inspect per the Asian region inspection
intervals. 3 If the aircraft is re-fueled outside this region since the initial Service Bulletin inspection, and has not been operated in the Asian
region, re-inspect every 10,000 operating hours. 4 Inspect at every shop visit or 20,000 operating hours, whichever occurs later.)
Alert, Cat. 2 - Recommended ≈21-Jun-2016T73-A0050 R09 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
174.27 Hrs≈12,311.67500Hrs
Enc
73 ENG1Eff: 29-Mar-2015
Also ConsiderDUE:1. T A/R | 2. RE -FUEL SYSTEM - Improved Preformed Packings on the Main Fuel C...73-0034 R00ENG173
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM397/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Alert, Cat. 2 - Recommended ≈21-Jun-2016T73-A0050 R09 ENGINE FUEL AND CONTROL - Fuel System (73-00-00) - Inspection of Main Fuel Control Input Drive Shaft Spline Main Fuel Pump Control Drive Shaft Spline and Main
Fuel Pump Secondary Drive Shaft Spline
Mos
174.27 Hrs≈12,194.67500Hrs
Enc
73 ENG2Eff: 29-Mar-2015
Also ConsiderDUE:1. T A/R | 2. RE -FUEL SYSTEM - Improved Preformed Packings on the Main Fuel C...73-0034 R00ENG273
MandatoryRE (-)99-23-26 Main Fuel Control (MFC)
Mos
Hrs
Enc
73 ENG1Eff: 05-Nov-1999
MandatoryRE (-)99-23-26 Main Fuel Control (MFC)
Mos
Hrs
Enc
73 ENG2Eff: 05-Nov-1999
MandatoryRE (-)99-23-26 R1 Main Fuel Control (MFC)
27-Dec-1999Mos
Hrs
Enc
73 ENG1FOUND P/C/WEff: 17-Feb-2000 Complied
With
MandatoryRE (-)99-23-26 R1 Main Fuel Control (MFC)
27-Dec-1999Mos
Hrs
Enc
73 ENG2FOUND P/C/WEff: 17-Feb-2000 Complied
With
AlertRE (-)A601-0144 Modification - Fuel Temperature Indicator - Decal Addition
18-Sep-1984Mos
Hrs
Ldg
73 A/FEff: 21-May-1985 Complied With
AlertRE (-)A601-1049 Modification - Fuel Temperature Bulb - Seal Replacement
Mos
Hrs
Ldg
73 A/F
AlertT (A/R)A601-1049 Rev 1 Modification - Fuel Temperature Bulb - Seal Replacement
Mos
Hrs
Ldg
73 A/FEff: 15-Sep-1985
▼ 74 - IGNITION
RE (O/C)Fan Inlet Temperature Sensor
27-Jun-2005Mos
10,839Hrs10,839
5,949Enc5,949
74 ENG2Overhauled4033T65P03
UNKNOWN
RE (O/C)Fan Inlet Temperature Sensor
31-May-2005Mos
10,956Hrs
5,990Enc
74 ENG14033T65P03EGN10383
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM398/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Igniter Plug
15-Sep-2007Mos
11,280.5Hrs
Enc
No.174 ENG14048T30P06CSP52897
RE (O/C)Igniter Plug
15-Sep-2007Mos
11,163.5Hrs
Enc
No.174 ENG24048T30P06CSP56214
RE (O/C)Igniter Plug
15-Sep-2007Mos
11,280.5Hrs
Enc
No.274 ENG14048T30P06TDG00869
RE (O/C)Igniter Plug
15-Sep-2007Mos
11,163.5Hrs
Enc
No.274 ENG24048T30P06TDG00868
RE (O/C)Ignition Exciter
27-Jun-2005Mos
10,839Hrs
5,949Enc
No.174 ENG25027T49P02SNT4234R
RE (O/C)Ignition Exciter
31-May-2005Mos
10,956Hrs10,956
5,990Enc5,999
No.174 ENG1Overhauled5027T49P02
4600
RE (O/C)Ignition Exciter
20-Sep-1983Mos
0Hrs
0Enc
No.274 ENG1UnknownUnknown
RE (O/C)Ignition Exciter
20-Sep-1983Mos
0Hrs
0Enc
No.274 ENG2UnknownUnknown
RE (O/C)Static Ignition Inverter
20-Sep-1983Mos
0Hrs0
0Ldg0
74 A/FNewASH671-2
UNKNOWN
MRB ≈03-May-2017RE74-00-00-204 (Left) Ignition System Operational Test - Ignition System
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
74 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE74-00-00-204 (Right) Ignition System Operational Test - Ignition System
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
74 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM399/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)74-0002 R02 ELECTRICAL SYSTEM - Installation of N2 Electrical Filter
Mos
Hrs
Enc
74 ENG1Eff: 12-Sep-1989
RecommendedRE (-)74-0002 R02 ELECTRICAL SYSTEM - Installation of N2 Electrical Filter
Mos
Hrs
Enc
74 ENG2Eff: 12-Sep-1989
RecommendedRE (-)74-0004 R01 ELECTRICAL SYSTEM - N1 Control Amplifier Adjustment
Mos
Hrs
Enc
74 ENG1Eff: 10-Mar-1989
RecommendedRE (-)74-0004 R01 ELECTRICAL SYSTEM - N1 Control Amplifier Adjustment
Mos
Hrs
Enc
74 ENG2Eff: 10-Mar-1989
RecommendedT (A/R)74-0006 R00 ELECTRICAL SYSTEM - Verification of Ignition Leads for Correct Installation
Mos
Hrs
Enc
74 ENG1Eff: 26-Feb-1993
RecommendedT (A/R)74-0006 R00 ELECTRICAL SYSTEM - Verification of Ignition Leads for Correct Installation
Mos
Hrs
Enc
74 ENG2Eff: 26-Feb-1993
RecommendedRE (-)74-0007 R00 ELECTRICAL SYSTEM - Upgrade of the Engine Ignition Leads
Mos
Hrs
Enc
74 ENG1Eff: 15-Dec-1993
RecommendedRE (-)74-0007 R00 ELECTRICAL SYSTEM - Upgrade of the Engine Ignition Leads
Mos
Hrs
Enc
74 ENG2Eff: 15-Dec-1993
RecommendedRE (-)74-0008 R00 ELECTRICAL SYSTEM - Replacement of the Green Jumper Cable on CF34-3A2 Engines
Mos
Hrs
Enc
74 ENG1Eff: 27-Jul-1994
(NOTE: All CF34-3A2 engines with green jumper cable PN 5085T35P01)
RecommendedRE (-)74-0008 R00 ELECTRICAL SYSTEM - Replacement of the Green Jumper Cable on CF34-3A2 Engines
Mos
Hrs
Enc
74 ENG2Eff: 27-Jul-1994
(NOTE: All CF34-3A2 engines with green jumper cable PN 5085T35P01)
RecommendedRE (-)74-0009 R00 ELECTRICAL SYSTEM - Ignition Exciter Replacement
Mos
Hrs
Enc
74 ENG1Eff: 21-Oct-1994
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM400/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)74-0009 R00 ELECTRICAL SYSTEM - Ignition Exciter Replacement
Mos
Hrs
Enc
74 ENG2Eff: 21-Oct-1994
OptionalRE (-)74-0010 R00 ELECTRICAL INFORMATION - Upgrade Program for Control Amplifier PN 5071T98P01
Mos
Hrs
Enc
74 ENG1Eff: 29-Apr-1997
OptionalRE (-)74-0010 R00 ELECTRICAL INFORMATION - Upgrade Program for Control Amplifier PN 5071T98P01
Mos
Hrs
Enc
74 ENG2Eff: 29-Apr-1997
Cat. 6 - RecommendedRE (-)74-0015 R00 IGNITION - Electrical System (74-00-00) - Ignition Exciter P/N 9238M66P08 Inspection
Mos
Hrs
Enc
74 ENG1Eff: 21-Apr-2010
Cat. 6 - RecommendedRE (-)74-0015 R00 IGNITION - Electrical System (74-00-00) - Ignition Exciter P/N 9238M66P08 Inspection
Mos
Hrs
Enc
74 ENG2Eff: 21-Apr-2010
Cat. 7 - OptionalRE (-)74-0016 R00 IGNITION - Electrical System (74-00-00) - Introduction of New Ignition Exciter VIN 10-631045-3 (P/N 9238M66P11)
Mos
Hrs
Enc
74 ENG1Eff: 07-Oct-2010
Cat. 7 - OptionalRE (-)74-0016 R00 IGNITION - Electrical System (74-00-00) - Introduction of New Ignition Exciter VIN 10-631045-3 (P/N 9238M66P11)
Mos
Hrs
Enc
74 ENG2Eff: 07-Oct-2010
Cat. 7 - OptionalRE (-)74-0016 R01 IGNITION - Electrical System (74-00-00) - Introduction of New Ignition Exciter VIN 10-631045-3 (P/N 9238M66P11)
Mos
Hrs
Enc
74 ENG1Eff: 26-Jul-2011
Cat. 7 - OptionalRE (-)74-0016 R01 IGNITION - Electrical System (74-00-00) - Introduction of New Ignition Exciter VIN 10-631045-3 (P/N 9238M66P11)
Mos
Hrs
Enc
74 ENG2Eff: 26-Jul-2011
MRB ≈25-Sep-2016RE74-10-11-203 Ignition Exciter - Visual Check
10-Feb-2016Mos
300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs
6,728Enc
(PKG 300 Eng Hour)
74 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈25-Sep-2016RE74-10-11-203 Ignition Exciter - Visual Check
10-Feb-2016Mos
300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs
6,769Enc
(PKG 300 Eng Hour)
74 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM401/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈25-Sep-2016RE74-10-16-202 Igniter Plug - Inspect Igniter plugs
10-Feb-2016Mos
300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs
6,769Enc
(PKG 300 Eng Hour)
74 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈25-Sep-2016RE74-10-16-202 Igniter Plug - Inspect Igniter plugs
10-Feb-2016Mos
300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs
6,728Enc
(PKG 300 Eng Hour)
74 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
AlertRE (-)A601-0131 Modification - Start Relays - Additional Diodes
18-Sep-1985Mos
Hrs
Ldg
74 A/FEff: 30-Jun-1985 Complied With
▼ 75 - BLEED AIR
RE (O/C)B-Sump Regulator Valve
20-Sep-1983Mos
0Hrs0
0Enc0
75 ENG2New4060T81G03
UNKNOWN
RE (O/C)B-Sump Vent Regulator Valve
20-Sep-1983Mos
0Hrs
0Enc
75 ENG1UnknownUnknown
RE (O/C)B-Sump Vent Regulator Valve
20-Sep-1983Mos
0Hrs
0Enc
75 ENG2UnknownUnknown
RE (O/C)Pressure Regulating Valve
29-Jan-2005Mos
10,580.3Hrs
5,376Enc
75 ENG1601-97097-71767
RE (O/C)Pressure Regulating Valve
20-Sep-1983Mos
0Hrs0
0Enc0
75 ENG2New4020T35G04
UNKNOWN
RE (O/C)Vaiable Geometry Actuator
20-Sep-1983Mos
0Hrs
0Enc
No.475 ENG1UnknownUnknown
RE (O/C)Vaiable Geometry Actuator
20-Sep-1983Mos
0Hrs
0Enc
No.475 ENG2UnknownUnknown
RE (O/C)Variable Geometry Actuator
20-Sep-1983Mos
0Hrs
0Enc
No.175 ENG1UnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM402/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Variable Geometry Actuator
20-Sep-1983Mos
0Hrs
0Enc
No.175 ENG2UnknownUnknown
RE (O/C)Variable Geometry Actuator
20-Sep-1983Mos
0Hrs
0Enc
No.275 ENG1UnknownUnknown
RE (O/C)Variable Geometry Actuator
20-Sep-1983Mos
0Hrs
0Enc
No.275 ENG2UnknownUnknown
RE (O/C)Variable Geometry Actuator
20-Sep-1983Mos
0Hrs
0Enc
No.375 ENG1UnknownUnknown
RE (O/C)Variable Geometry Actuator
20-Sep-1983Mos
0Hrs
0Enc
No.375 ENG2UnknownUnknown
RecommendedRE (-)601-1007 Modification - Cooling - Inlet Guide Vane (IGV) Control
Mos
Hrs
Ldg
75 A/F
RecommendedT (A/R)601-1007 Rev 1 Modification - Cooling - Inlet Guide Vane (IGV) Control
Mos
Hrs
Ldg
75 A/FEff: 18-Dec-1984
RecommendedT (A/R)601-1034 Modification - Engine Bleed Air Duct - Hardware
Mos
Hrs
Ldg
75 A/FEff: 22-Oct-1984
Cat. 6 - RecommendedRE (-)74-0011 R00 IGNITION - Electrical System (74-00-00) - Introduction of Improved W2 Blue Cable Assembly
Mos
Hrs
Enc
75 ENG1Eff: 06-Jun-2001
Cat. 6 - RecommendedRE (-)74-0011 R00 IGNITION - Electrical System (74-00-00) - Introduction of Improved W2 Blue Cable Assembly
Mos
Hrs
Enc
75 ENG2Eff: 06-Jun-2001
RecommendedRE (-)75-0001 R01 AIR SYSTEM - Rework B-Sump Regulator Valve
Mos
Hrs
Enc
75 ENG1Eff: 11-Aug-1995
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM403/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)75-0001 R01 AIR SYSTEM - Rework B-Sump Regulator Valve
Mos
Hrs
Enc
75 ENG2Eff: 11-Aug-1995
RecommendedRE (-)75-0002 R04 AIR - Introduction of New and Reworked B-Sump Vent Regulator Valves
Mos
Hrs
Enc
75 ENG1Eff: 28-Jun-2000
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
RecommendedRE (-)75-0002 R04 AIR - Introduction of New and Reworked B-Sump Vent Regulator Valves
Mos
Hrs
Enc
75 ENG2Eff: 28-Jun-2000
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
RecommendedRE (-)75-0003 R00 ENGINE - Air System - Introduction of Air Tube Spacer PN 3049T28P01
Mos
Hrs
Enc
75 ENG1Eff: 03-Dec-1998
RecommendedRE (-)75-0003 R00 ENGINE - Air System - Introduction of Air Tube Spacer PN 3049T28P01
Mos
Hrs
Enc
75 ENG2Eff: 03-Dec-1998
MRB ≈25-Sep-2016RE75-30-00-201 Variable Geometry Control - Visual Check of VG system, paying particular attention to rod end bushings, actuator shaft bearings, lever arms, feedback cable, actuator
attachment points, turnbuckles, actuator ring and torque shaft forward bearing for migration / Lubricate VG rod end bearings (24 locations)
10-Feb-2016Mos
300 Hrs (+40)(12,320.4)-/+4030012,020.4Hrs
6,728Enc
(PKG 300 Eng Hour)
75 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈25-Sep-2016RE75-30-00-201 Variable Geometry Control - Visual Check of VG system, paying particular attention to rod end bushings, actuator shaft bearings, lever arms, feedback cable, actuator
attachment points, turnbuckles, actuator ring and torque shaft forward bearing for migration / Lubricate VG rod end bearings (24 locations)
10-Feb-2016Mos
300 Hrs (+40)(12,437.4)-/+4030012,137.4Hrs
6,769Enc
(PKG 300 Eng Hour)
75 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
▼ 76 - ENGINE CONTROLS
AWL - Life LimitRE (O/C)Auto-Throttle Retard System Clevis Pin
27-Jan-1987Mos
1,267Hrs
470Ldg
Left76 A/FNOT APPLICABLE
AWL - Life LimitRE (O/C)Auto-Throttle Retard System Clevis Pin
27-Jan-1987Mos
1,267Hrs
470Ldg
Right76 A/FNOT APPLICABLE
RE (O/C)Clevis Assy, Auto-Throttle
20-Sep-1983Mos
0Hrs
0Ldg
Left76 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM404/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Clevis Assy, Auto-Throttle
20-Sep-1983Mos
0Hrs
0Ldg
Right76 A/FUnknownUnknown
RE (O/C)Engine Throttle Quadrant
20-Sep-1983Mos
0Hrs
0Ldg
76 A/FUnknownUnknown
RE (O/C)Throttle Control Gearbox Assembly
20-Sep-1983Mos
0Hrs
0Ldg
Left76 A/FUnknownUnknown
Component Inspection SimpleDUE: 12,035.4 Hrs1. T 1600 Hrs | 2. RA 1600 Hrs | 3. RA 1600 Hrs | 4. RE
1000 HrsThrottle Control Gearbox - Functional Test of the Throttle C...76-10-00-101 *A/F76
RE (O/C)Throttle Control Gearbox Assembly
20-Sep-1983Mos
0Hrs
0Ldg
Right76 A/FUnknownUnknown
Component Inspection SimpleDUE: 12,035.4 Hrs1. T 1600 Hrs | 2. RA 1600 Hrs | 3. RA 1600 Hrs | 4. RE
1000 HrsThrottle Control Gearbox - Functional Test of the Throttle C...76-10-00-101 *A/F76
MandatoryRE (-)2009-24-18 Engine controls.
26-Jan-2011Mos
11,460.7Hrs
5,905Ldg
76 A/FFOUND P/C/WEff: 08-Jan-2010 Complied
With
RecommendedRE (-)601-0086 Special Check/Modification - Throttle Quadrant - Anti-Torque Shaft Retention
Mos
Hrs
Ldg
76 A/F
RecommendedRE (-)601-0086 Rev 1 Special Check/Modification - Throttle Quadrant - Anti-Torque Shaft Retention
21-Nov-1984Mos
Hrs
Ldg
76 A/FEff: 13-Mar-1985 Complied With
RecommendedRE (-)601-0106 Special Check/Replacement - Controlex Cable - Seal Nut
06-Sep-1985Mos
607Hrs
261Ldg
76 A/FEff: 20-Sep-1984 Complied With
OptionalT (A/R)601-0317 Modification - Controlex Throttle Control Cables - Routing
Mos
Hrs
Ldg
76 A/FEff: 31-Oct-1990
RecommendedRE (-)601-0410 Special Check/Modification - Throttle Quadrant - Inadvertent Shut-off
05-Apr-1994Mos
Hrs
Ldg
76 A/FEff: 01-Nov-1993 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM405/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-0538 Special Check/Modification - Engine Controls - Possible Failure of Engine Throttle Push/Pull Control-Assembly
05-Aug-2003Mos
9,585.6Hrs
4,797Ldg
76 A/FEff: 30-Sep-2002 Complied With
RecommendedT (A/R)601-0583 Special Check/Modification - Throttle Controls - Inspection/Replacement of the Throttle Gear Box Part No. 2100140-003, 2100140-005 and 2100140-007
Mos
Hrs
Ldg
76 A/FEff: 31-May-2006
RecommendedRE (-)601-1018 Modification - Throttle Controls - Auto-Throttle Retarder System
02-Nov-1992Mos
1,267Hrs
480Ldg
76 A/FComplied With
RecommendedT (A/R)601-1018 Rev 1 Modification - Throttle Controls - Auto-Throttle Retarder System
Mos
Hrs
Ldg
76 A/FEff: 24-Aug-1984
RecommendedRE (-)601-1020 Modification - Throttle Controls - Replacement of Throttle Rod End Assemblies
Mos
Hrs
Ldg
76 A/F
RecommendedT (A/R)601-1020 Rev 1 Modification - Throttle Controls - Replacement of Throttle Rod End Assemblies
Mos
Hrs
Ldg
76 A/FEff: 09-Apr-1984
RecommendedRE (-)601-1044 Modification - ATR Control - Clevis Assembly
16-Jul-1986Mos
952Hrs
403Ldg
76 A/FEff: 10-Oct-1985 Complied With
RecommendedRE (-)601-1054 Special Check/Modification - Throttle Controls - Auto Throttle Retarder Cable Assembly
02-May-1988Mos
1,995Hrs
756Ldg
76 A/FEff: 02-Apr-1987 Complied With
RecommendedRE (-)601-1074 Special Check/Modification - Controlex Cable - Tang Wear and Spiral Wrap Addition
20-Nov-2000Mos
Hrs
Ldg
76 A/FEff: 13-Jul-1990 Complied With
OptionalT (A/R)601-1076 Throttle Control Rod Assembly - Adjustment Facility
Mos
Hrs
Ldg
76 A/FEff: 18-Mar-1991
AWL ≈06-Feb-2016RE76-10-00-101 * Throttle Control Gearbox - Functional Test of the Throttle Control Gearbox Assembly Part Numbers 2100140-003/-005/-007
22-Mar-2007Mos
OVD12,035.41,00011,035.4Hrs
Ldg
Left76 A/FUnknownUnknown
(SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM406/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈06-Feb-2016RE76-10-00-101 * Throttle Control Gearbox - Functional Test of the Throttle Control Gearbox Assembly Part Numbers 2100140-003/-005/-007
22-Mar-2007Mos
OVD12,035.41,00011,035.4Hrs
Ldg
Right76 A/FUnknownUnknown
(SOURCE: TLMC 05-10-30)
MandatoryRE (-)95-03-06 Engine Throttle Quadrant
28-Apr-1995Mos
4,555Hrs
1,824Ldg
76 A/FSI 601-0410Eff: 31-Mar-1995 Complied
With
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Modification - Throttle Quadrant - Inadvertent...601-0410A/F76
Compliance Share DoubleDUE:1. T A/R | 2. RE -Special Check/Modification - Throttle Quadrant - Idle Stop P...A601-0374 Rev 1A/F76
RecommendedRE (-)A601-0374 Special Check/Modification - Throttle Quadrant - Idle Stop Pawl
Mos
Hrs
Ldg
76 A/F
RecommendedRE (-)A601-0374 Rev 1 Special Check/Modification - Throttle Quadrant - Idle Stop Pawl
31-Oct-1993Mos
Hrs
Ldg
76 A/FEff: 30-Sep-1992 Complied With
▼ 77 - ENGINE INDICATING
RE (O/C)Engine Apr Control Amplifier
31-May-2005Mos
10,956Hrs
5,990Enc
77 ENG14074T27G01UNKNOWN
RE (O/C)Engine Apr Control Amplifier
20-Sep-1983Mos
0Hrs
0Enc
77 ENG2UnknownUnknown
RE (O/C)Engine Instrument Control Panel
20-Sep-1983Mos
0Hrs
0Ldg
77 A/FUnknownUnknown
RE (O/C)Engine Vibration Accelerometer
20-Sep-1983Mos
0Hrs
0Ldg
Left77 A/FUnknownUnknown
RE (O/C)Engine Vibration Accelerometer
20-Sep-1983Mos
0Hrs
0Ldg
Right77 A/FUnknownUnknown
RE (O/C)Engine Vibration Indicator
20-Sep-1983Mos
0Hrs0
0Ldg0
77 A/FNew124-497-1
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM407/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Engine Vibration Monitor
18-Oct-2003Mos
9,808.2Hrs
4,927Ldg
77 A/F6632M1438718
RE (O/C)Inlet Turbine Temperature Indicator
20-Sep-1983Mos
0Hrs
0Ldg
77 A/FUnknownUnknown
RE (O/C)N1 Fan Rpm Indicator
21-Aug-2004Mos
10,458.3Hrs
5,306Ldg
77 A/F418-098-119776
RE (O/C)N2 Speed Sensor
20-Sep-1983Mos
0Hrs
0Enc
77 ENG1UnknownUnknown
RE (O/C)N2 Speed Sensor(Right)
24-Feb-2003Mos
9,253.9Hrs9,253.9
4,606Enc4,606
77 ENG2418-098-12829
RE (O/C)N2 Turbine Rpm Indicator
20-Sep-1983Mos
0Hrs
0Ldg
77 A/FUnknownUnknown
RE (O/C)Signal Data Converter
20-Sep-1983Mos
0Hrs
0Ldg
77 A/FUnknownUnknown
RecommendedRE (-)601-0057 Modification - Engine Vibration Monitoring System - Shield Ground
26-Jan-1987Mos
1,267Hrs
470Ldg
77 A/FEff: 16-Apr-1984 Complied With
OptionalRE (-)601-0238 Modification – Inter Turbine Temperature Indicating – Use of CF34-3A Engines at -3A Power Settings on CL-601 Aircraft
26-Aug-2002Mos
8,743.6Hrs
4,289Ldg
77 A/FEff: 08-Feb-1988 Complied With
▼ 78 - EXHAUST
AWL - Life Limit ≈04-Aug-2016RE10 O'Clock Actuator Rod End
20-Sep-1983Mos
0Hrs0
174 Ldg6,5006,5000Ldg0
Left78 A/FNew3233445-1
UNKNOWN
(NOTE: Note: For P/N 3236757-1 applicable only if ever operated with PDI P/N 126758-3 or lower dash number)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM408/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL - Life Limit ≈04-Aug-2016RE10 O'Clock Actuator Rod End
20-Sep-1983Mos
0Hrs0
174 Ldg6,5006,5000Ldg0
Right78 A/FNew3233445-1
UNKNOWN
(NOTE: Note: For P/N 3236757-1 applicable only if ever operated with PDI P/N 126758-3 or lower dash number)
AWL - Life Limit ≈04-Aug-2016RE10 O'Clock Anti-Rotation Tang
20-Sep-1983Mos
0Hrs0
174 Ldg6,5006,5000Ldg0
Left78 A/FNew3233586-1
UNKNOWN
(NOTE: Note: Applicable only if ever operated with PDI P/N 126758-3 or lower dash number)
AWL - Life Limit ≈04-Aug-2016RE10 O'Clock Anti-Rotation Tang
20-Sep-1983Mos
0Hrs0
174 Ldg6,5006,5000Ldg0
Right78 A/FNew3233586-1
UNKNOWN
(NOTE: Note: Applicable only if ever operated with PDI P/N 126758-3 or lower dash number)
AWL - Life Limit ≈04-Aug-2016RE2 O'Clock Actuator Rod End
20-Sep-1983Mos
0Hrs0
174 Ldg6,5006,5000Ldg0
Left78 A/FNew3233445-1
UNKNOWN
(NOTE: Note: For P/N 3236757-1 applicable only if ever operated with PDI P/N 126758-3 or lower dash number)
AWL - Life Limit ≈04-Aug-2016RE2 O'Clock Actuator Rod End
20-Sep-1983Mos
0Hrs0
174 Ldg6,5006,5000Ldg0
Right78 A/FNew3233445-1
UNKNOWN
(NOTE: Note: For P/N 3236757-1 applicable only if ever operated with PDI P/N 126758-3 or lower dash number)
AWL - Life Limit ≈04-Aug-2016RE2 O'Clock Anti-Rotation Tang
20-Sep-1983Mos
0Hrs0
174 Ldg6,5006,5000Ldg0
Left78 A/FNew3233586-1
UNKNOWN
(NOTE: Note: Applicable only if ever operated with PDI P/N 126758-3 or lower dash number)
AWL - Life Limit ≈04-Aug-2016RE2 O'Clock Anti-Rotation Tang
20-Sep-1983Mos
0Hrs0
174 Ldg6,5006,5000Ldg0
Right78 A/FNew3233586-1
UNKNOWN
(NOTE: Note: Applicable only if ever operated with PDI P/N 126758-3 or lower dash number)
AWL - Life Limit ≈04-Aug-2016RE4 O'Clock Actuator Rod End
20-Sep-1983Mos
0Hrs0
174 Ldg6,5006,5000Ldg0
Left78 A/FNew3233445-1
UNKNOWN
(NOTE: Note: For P/N 3236757-1 applicable only if ever operated with PDI P/N 126758-3 or lower dash number)
AWL - Life Limit ≈04-Aug-2016RE4 O'Clock Actuator Rod End
20-Sep-1983Mos
0Hrs0
174 Ldg6,5006,5000Ldg0
Right78 A/FNew3233445-1
UNKNOWN
(NOTE: Note: For P/N 3236757-1 applicable only if ever operated with PDI P/N 126758-3 or lower dash number)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM409/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL - Life Limit ≈02-Jul-2021RE4 O'Clock Anti-Rotation Tang
30-Sep-2004Mos
4,399Hrs0
1,942 Ldg8,2686,5001,768Ldg0
Left78 A/FNew3233586-1
UNKNOWN
(NOTE: Note: Applicable only if ever operated with PDI P/N 126758-3 or lower dash number)
AWL - Life Limit ≈04-Aug-2016RE4 O'Clock Anti-Rotation Tang
20-Sep-1983Mos
0Hrs0
174 Ldg6,5006,5000Ldg0
Right78 A/FNew3233586-1
UNKNOWN
(NOTE: Note: Applicable only if ever operated with PDI P/N 126758-3 or lower dash number)
AWL - Life Limit ≈04-Aug-2016RE8 O'Clock Actuator Rod End
20-Sep-1983Mos
0Hrs0
174 Ldg6,5006,5000Ldg0
Left78 A/FNew3233445-1
UNKNOWN
(NOTE: Note: For P/N 3236757-1 applicable only if ever operated with PDI P/N 126758-3 or lower dash number)
AWL - Life Limit ≈04-Aug-2016RE8 O'Clock Actuator Rod End
20-Sep-1983Mos
0Hrs0
174 Ldg6,5006,5000Ldg0
Right78 A/FNew3233445-1
UNKNOWN
(NOTE: Note: For P/N 3236757-1 applicable only if ever operated with PDI P/N 126758-3 or lower dash number)
AWL - Life Limit ≈28-Aug-2033RE8 O'Clock Anti-Rotation Tang
17-May-2013Mos
11,788.8Hrs0
6,317 Ldg12,6436,5006,143Ldg0
Left78 A/FNew3233586-1
UNKNOWN
(NOTE: Note: Applicable only if ever operated with PDI P/N 126758-3 or lower dash number)
AWL - Life Limit ≈04-Aug-2016RE8 O'Clock Anti-Rotation Tang
20-Sep-1983Mos
0Hrs0
174 Ldg6,5006,5000Ldg0
Right78 A/FNew3233586-1
UNKNOWN
(NOTE: Note: Applicable only if ever operated with PDI P/N 126758-3 or lower dash number)
AWL - Life Limit ≈24-Dec-2042REBallscrew Actuator
20-Sep-1983Mos
0Hrs0
9,674 Ldg16,00016,0000Ldg0
Left No.178 A/FNew3272570-2
UNKNOWN
(NOTE: Note: With Gimbal (P/N 3235452) and Housing (P/N 3233436) only)
AWL - Life Limit ≈24-Dec-2042REBallscrew Actuator
20-Sep-1983Mos
0Hrs0
9,674 Ldg16,00016,0000Ldg0
Left No.278 A/FNew3272570-2
UNKNOWN
(NOTE: Note: With Gimbal (P/N 3235452) and Housing (P/N 3233436) only)
AWL - Life Limit ≈24-Dec-2042REBallscrew Actuator
20-Sep-1983Mos
0Hrs0
9,674 Ldg16,00016,0000Ldg0
Left No.378 A/FNew3272570-2
UNKNOWN
(NOTE: Note: With Gimbal (P/N 3235452) and Housing (P/N 3233436) only)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM410/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL - Life Limit ≈24-Dec-2042REBallscrew Actuator
20-Sep-1983Mos
0Hrs0
9,674 Ldg16,00016,0000Ldg0
Left No.478 A/FNew3272570-2
UNKNOWN
(NOTE: Note: With Gimbal (P/N 3235452) and Housing (P/N 3233436) only)
AWL - Life Limit ≈24-Dec-2042REBallscrew Actuator
20-Sep-1983Mos
0Hrs0
9,674 Ldg16,00016,0000Ldg0
Right No.178 A/FNew3272570-2
UNKNOWN
(NOTE: Note: With Gimbal (P/N 3235452) and Housing (P/N 3233436) only)
AWL - Life Limit ≈24-Dec-2042REBallscrew Actuator
20-Sep-1983Mos
0Hrs0
9,674 Ldg16,00016,0000Ldg0
Right No.278 A/FNew3272570-2
UNKNOWN
(NOTE: Note: With Gimbal (P/N 3235452) and Housing (P/N 3233436) only)
AWL - Life Limit ≈27-Feb-2050REBallscrew Actuator
27-Feb-1999Mos
5,912Hrs0
12,258 Ldg18,58416,0002,584Ldg0
Right No.378 A/FNew3272570-2
UNKNOWN
(NOTE: Note: With Gimbal (P/N 3235452) and Housing (P/N 3233436) only)
AWL - Life Limit ≈01-May-2054REBallscrew Actuator
11-May-2002Mos
8,425.9Hrs0
13,761 Ldg20,08716,0004,087Ldg0
Right No.478 A/FNew3272570-2
UNKNOWN
(NOTE: Note: With Gimbal (P/N 3235452) and Housing (P/N 3233436) only)
RE (O/C)Stow Thrust Reverser Switch
20-Sep-1983Mos
0Hrs
0Ldg
Left78 A/FUnknownUnknown
RE (O/C)Stow Thrust Reverser Switch
20-Sep-1983Mos
0Hrs
0Ldg
Right78 A/FUnknownUnknown
AWL - Life LimitRE (O/C)T/R Latch Interlock Fittings
20-Sep-1983Mos
0Hrs0
0Ldg0
Left78 A/FNew228-50790-113
NOT APPLICABLE
(NOTE: N/A per report furnished)
AWL - Life LimitRE (O/C)T/R Latch Interlock Fittings
20-Sep-1983Mos
0Hrs0
0Ldg0
Right78 A/FNew228-50790-113
NOT APPLICABLE
RE (O/C)Thrust Reverser (PDU)
20-Sep-1983Mos
0Hrs
0Ldg
No.178 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM411/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Thrust Reverser (PDU)
12-Sep-2008Mos
11,455.7Hrs
5,898Ldg
No.278 A/F126758-6-2P-188C
RE (O/C)Thrust Reverser Interlock Fittings
20-Sep-1983Mos
0Hrs
0Ldg
Left78 A/FUnknownUnknown
RE (O/C)Thrust Reverser Interlock Fittings
20-Sep-1983Mos
0Hrs
0Ldg
Right78 A/FUnknownUnknown
RecommendedRE (-)601-0045 Modification - Thrust Reverser - Anti-Ice/Wheel Spin-up
Mos
Hrs
Ldg
78 A/F
RecommendedRE (-)601-0045 Rev 1 Modification - Thrust Reverser - Anti-Ice/Wheel Spin-up
Mos
Hrs
Ldg
78 A/FEff: 23-Apr-1984
RecommendedRE (-)601-0046 Modification - Thrust Reverser - Activation
Mos
Hrs
Ldg
78 A/F
RecommendedT (A/R)601-0046 Rev 1 Modification - Thrust Reverser - Activation
Mos
Hrs
Ldg
78 A/FEff: 10-Jul-1984
RecommendedRE (-)601-0047 Modification - 14th Stage Bleed Air - Control System
Mos
Hrs
Ldg
78 A/F
RecommendedRE (-)601-0047 Rev 1 Modification - 14th Stage Bleed Air - Control System
Mos
Hrs
Ldg
78 A/FEff: 05-Jun-1984
RecommendedRE (-)601-0050 Modification - Thrust Reverser - EMI Suppression
Mos
Hrs
Ldg
78 A/F
RecommendedRE (-)601-0050 Rev 1 Modification - Thrust Reverser - EMI Suppression
Mos
Hrs
Ldg
78 A/FEff: 09-Apr-1984
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM412/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalRE (-)601-0400 Modification - Thrust Reverser - Prevent Power Interruption and Relocate Stow and Throttle Lockout Microswitches
Mos
Hrs
Ldg
78 A/F
OptionalT (A/R)601-0400 Rev 1 Modification - Thrust Reverser - Prevent Power Interruption and Relocate Stow and Throttle Lockout Microswitches
Mos
Hrs
Ldg
78 A/FEff: 29-Feb-2000
OptionalRE (-)601-0409 Modification - Thrust Reverser Unlocked Annunciation Wiring Change
Mos
Hrs
Ldg
78 A/FEff: 15-May-1995
OptionalT (A/R)601-0578 Modification - Thrust Reverser - Replacement of PDU Engine Nose Cowl Internal Pockets
Mos
Hrs
Ldg
78 A/FEff: 30-Jan-2007
Recommended ≈05-Jan-2022T (A/R)601-0582 Modification - Exhaust Nozzle Assembly - Replacement of the Exhaust Nozzle and Tail Pipe Attachment Bolts
Mos
2,833.8 Hrs[14,875]Hrs
Ldg
78 A/FEff: 28-Aug-2006
RecommendedRE (-)601-1013 Modification - Thrust Reverser - Stowed and Throttle Lockout Microswitches
Mos
Hrs
Ldg
78 A/F
RecommendedRE (-)601-1013 Rev 1 Modification - Thrust Reverser - Stowed and Throttle Lockout Microswitches
07-Aug-1985Mos
Hrs
Ldg
78 A/FEff: 24-Aug-1984 Complied With
RecommendedRE (-)601-1015 Modification - Thrust Reverser - Blocker Door Numbers 8 and 9
Mos
Hrs
Ldg
78 A/F
RecommendedRE (-)601-1015 Rev 1 Modification - Thrust Reverser - Blocker Door Numbers 8 and 9
26-Jan-1987Mos
1,267Hrs
480Ldg
78 A/FEff: 28-Aug-1984 Complied With
RecommendedRE (-)601-1017 Modification - Thrust Reverser - Upper Pylon Cascade and Upper Center Cascade
Mos
Hrs
Ldg
78 A/F
RecommendedT (A/R)601-1017 Rev 1 Modification - Thrust Reverser - Upper Pylon Cascade and Upper Center Cascade
Mos
Hrs
Ldg
78 A/FEff: 09-Apr-1984
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM413/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-1019 Modification - Thrust Reverser - Power Drive Unit Actuator
Mos
Hrs
Ldg
78 A/F
RecommendedT (A/R)601-1019 Rev 1 Modification - Thrust Reverser - Power Drive Unit Actuator
Mos
Hrs
Ldg
78 A/FEff: 07-Jun-1984
RecommendedRE (-)601-1021 Modification - Thrust Reverser - Systems
Mos
Hrs
Ldg
78 A/F
RecommendedT (A/R)601-1021 Rev 1 Modification - Thrust Reverser - Systems
Mos
Hrs
Ldg
78 A/FEff: 02-Apr-1984
RecommendedRE (-)601-1023 Modification - Thrust Reverser - Air Tube Installation
Mos
Hrs
Ldg
78 A/F
RecommendedT (A/R)601-1023 Rev 1 Modification - Thrust Reverser - Air Tube Installation
Mos
Hrs
Ldg
78 A/FEff: 18-May-1984
RecommendedRE (-)601-1024 Modification - Thrust Reverser - Replacement of Interlock Latch Fittings
Mos
Hrs
Ldg
78 A/F
RecommendedRE (-)601-1024 Rev 1 Modification - Thrust Reverser - Replacement of Interlock Latch Fittings
18-Sep-1985Mos
607Hrs
261Ldg
78 A/FEff: 14-Dec-1985 Complied With
RecommendedRE (-)601-1026 Modification - Thrust Reverser - Replacement of Blocker Door Stops and Bumpers
21-Mar-1991Mos
3,182Hrs
1,266Ldg
78 A/FComplied With
RecommendedRE (-)601-1026 Rev 1 Modification - Thrust Reverser - Replacement of Blocker Door Stops and Bumpers
Mos
Hrs
Ldg
78 A/F
RecommendedRE (-)601-1026 Rev 2 Modification - Thrust Reverser - Replacement of Blocker Door Stops and Bumpers
Mos
Hrs
Ldg
78 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM414/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedT (A/R)601-1026 Rev 3 Modification - Thrust Reverser - Replacement of Blocker Door Stops and Bumpers
Mos
Hrs
Ldg
78 A/FEff: 04-Feb-1986
RecommendedRE (-)601-1038 Modification - Thrust Reverser Diverter Fairing - Addition of Drain Hole
02-May-1988Mos
1,995Hrs
756Ldg
78 A/FEff: 18-Mar-1985 Complied With
RecommendedRE (-)601-1042 Special Check/Replacement - Thrust Reverser - Blocker Doors
Mos
Hrs
Ldg
78 A/F
RecommendedRE (-)601-1042 Rev 1 Special Check/Replacement - Thrust Reverser - Blocker Doors
02-May-1988Mos
1,995Hrs
756Ldg
78 A/FEff: 28-Jan-1986 Complied With
RecommendedRE (-)601-1056 Modification - Exhaust Nozzle Fairing - Installation of New Bolts and Bushings
13-Oct-1992Mos
3,754Hrs
1,519Ldg
78 A/FEff: 19-Sep-1988 Complied With
RecommendedRE (-)601-1057 Modification - Thrust Reverser Main Tracks - Slider Block Assemblies
Mos
Hrs
Ldg
78 A/F
RecommendedRE (-)601-1057 Rev 1 Modification - Thrust Reverser Main Tracks - Slider Block Assemblies
Mos
Hrs
Ldg
78 A/F
RecommendedRE (-)601-1057 Rev 2 Modification - Thrust Reverser Main Tracks - Slider Block Assemblies
23-Mar-1992Mos
3,584Hrs
1,446Ldg
78 A/FEff: 25-Jun-1993 Complied With
RecommendedRE (-)601-1058 Modification - Thrust Reverser - Deploy Microswitch Target
Mos
Hrs
Ldg
78 A/F
RecommendedRE (-)601-1058 Rev 1 Modification - Thrust Reverser - Deploy Microswitch Target
Mos
Hrs
Ldg
78 A/F
RecommendedRE (-)601-1058 Rev 2 Modification - Thrust Reverser - Deploy Microswitch Target
23-Mar-1992Mos
3,584Hrs
1,446Ldg
78 A/FEff: 16-Oct-1989 Complied With
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM415/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)601-1061 Modification - Thrust Reverser Blocker Doors - Improved Retention
Mos
Hrs
Ldg
78 A/F
RecommendedRE (-)601-1061 Rev 1 Modification - Thrust Reverser Blocker Doors - Improved Retention
25-Mar-1991Mos
3,182Hrs
1,266Ldg
78 A/FEff: 02-Nov-1990 Complied With
RecommendedRE (-)601-1065 Modification - Auto-Throttle Retarder Control - Cable Protection
23-Feb-1990Mos
2,687Hrs
1,034Ldg
78 A/FEff: 25-Oct-1989 Complied With
RecommendedRE (-)601-1066 Modification - Thrust Reverser Torque Box - DrainageThrust Reverser Torque Box - Drainage
Mos
Hrs
Ldg
78 A/F
RecommendedRE (-)601-1066 Rev 1 Modification - Thrust Reverser Torque Box - DrainageThrust Reverser Torque Box - Drainage
21-Feb-1991Mos
3,142Hrs
1,250Ldg
78 A/FEff: 04-Dec-1990 Complied With
RecommendedRE (-)601-1069 Modification - Thrust Reverser - Introduction of -6 PDU
Mos
Hrs
Ldg
78 A/F
RecommendedT (A/R)601-1069 Rev 1 Modification - Thrust Reverser - Introduction of -6 PDU
Mos
Hrs
Ldg
78 A/FEff: 10-Jan-1990
RecommendedRE (-)601-1070 Special Check/Modification/Rework - Thrust Reverser - Upper Pylon Cascades
25-Mar-1991Mos
3,182Hrs
1,266Ldg
78 A/F2BEff: 31-Aug-1990 Complied
With
RecommendedRE (-)601-1071 Rework -Thrust Reverser - Interlocking Latch Fitting Attach Rivets
Mos
Hrs
Ldg
78 A/F
RecommendedRE (-)601-1071 Rev 1 Rework -Thrust Reverser - Interlocking Latch Fitting Attach Rivets
Mos
Hrs
Ldg
78 A/FEff: 15-Apr-1993
OptionalT (A/R)601-1073 Modification - Thrust Reverser - No. 7 Blocker Door Link Housing Replacement
Mos
Hrs
Ldg
78 A/FEff: 06-Mar-1991
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM416/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
OptionalT (A/R)601-1075 Modification - Thrust Reverser - Blocker Door Link Housing Covers
Mos
Hrs
Ldg
78 A/FEff: 30-Apr-1990
RecommendedRE (-)601-1079 Special Check/Modification - Thrust Reverser - Pneumatic Drive Unit Flexshaft Bolts
21-Feb-1991Mos
3,142Hrs
1,250Ldg
78 A/FEff: 14-Sep-1990 Complied With
RecommendedRE (-)601-1084 Special Check/Modification - Thrust Reverser - Blocker Doors and Sound Attenuating Material (SAM) Panels
Mos
Hrs
Ldg
78 A/F
RecommendedRE (-)601-1084 Rev 1 Special Check/Modification - Thrust Reverser - Blocker Doors and Sound Attenuating Material (SAM) Panels
26-Jan-1996Mos
4,785Hrs
1,932Ldg
78 A/FEff: 15-Dec-1999 Complied With
OptionalRE (-)601-1089 Modification - Translating Cowl Doors Support Struts - Addition of Dampening Pad and Retention Bracket
Mos
Hrs
Ldg
78 A/F
OptionalT (A/R)601-1089 Rev 1 Modification - Translating Cowl Doors Support Struts - Addition of Dampening Pad and Retention Bracket
Mos
Hrs
Ldg
78 A/FEff: 15-Apr-1997
OptionalT (A/R)601-1094 Modification - Thrust Reverser Main Track - Repl Eccentric Bushings With Concentric
Mos
Hrs
Ldg
78 A/FEff: 28-Nov-1997
RecommendedRE (-)601-1100 Special Check/Rework - Thrust Reverser - Examine Condition of Actuator Attachment Fittings
Mos
Hrs
Ldg
78 A/F
RecommendedT (A/R)601-1100 Rev 1 Special Check/Rework - Thrust Reverser - Examine Condition of Actuator Attachment Fittings
Mos
Hrs
Ldg
78 A/FEff: 19-Oct-2001
MRB ≈20-Oct-2017RE78-10-00-211 (Left) Exhaust Nozzle Assembly Remove exhaust nozzle fairing and carry out a visual check off airing, nozzle, stiffeners, attachment links and brackets. Reinstall fairing
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE78-10-00-211 (Right) Exhaust Nozzle Assembly Remove exhaust nozzle fairing and carry out a visual check off airing, nozzle, stiffeners, attachment links and brackets. Reinstall fairing
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM417/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈23-May-2017RE78-30-00-101 * (Left) Thrust Reverser - Main Track - Aft Lugs - NDT Check
20-May-2009Mos
617.4 Hrs12,658.61,20011,458.6Hrs
Ldg
78 A/F
Ref.:PSP 612 Part 6 ET-78-30-01 (SOURCE: TLMC 05-10-30) (NOTE: With PDU Part Number 126758-3 Installed)
AWL ≈23-May-2017RE78-30-00-101 * (Right) Thrust Reverser - Main Track - Aft Lugs - NDT Check
20-May-2009Mos
617.4 Hrs12,658.61,20011,458.6Hrs
Ldg
78 A/F
Ref.:PSP 612 Part 6 ET-78-30-01 (SOURCE: TLMC 05-10-30) (NOTE: With PDU Part Number 126758-3 Installed)
AWL ≈24-Aug-2023RE78-30-00-102 * (Left) Thrust Reverser - Main Upper and Lower Pylon Tracks - NDT Check
08-Aug-2005Mos
3,618.6 Hrs15,659.84,80010,859.8Hrs
Ldg
78 A/F
Ref.:PSP 612 Part 6 ET-78-30-02 (SOURCE: TLMC 05-10-30)
AWL ≈24-Aug-2023RE78-30-00-102 * (Right) Thrust Reverser - Main Upper and Lower Pylon Tracks - NDT Check
08-Aug-2005Mos
3,618.6 Hrs15,659.84,80010,859.8Hrs
Ldg
78 A/F
Ref.:PSP 612 Part 6 ET-78-30-02 (SOURCE: TLMC 05-10-30)
AWL ≈23-Jul-2016RE78-30-00-103 * (Left) Thrust Reverser - Main Track Attachment Fittings - NDT Check
22-Jul-2004Mos
217.1 Hrs12,258.31,80010,458.3Hrs
Ldg
78 A/F
Ref.:PSP 612 Part 6 ET-78-30-05 (SOURCE: TLMC 05-10-30) (NOTE: With PDU Part Number 126758-3 Installed)
AWL ≈23-Jul-2016RE78-30-00-103 * (Right) Thrust Reverser - Main Track Attachment Fittings - NDT Check
22-Jul-2004Mos
217.1 Hrs12,258.31,80010,458.3Hrs
Ldg
78 A/F
Ref.:PSP 612 Part 6 ET-78-30-05 (SOURCE: TLMC 05-10-30) (NOTE: With PDU Part Number 126758-3 Installed)
AWL ≈06-Jul-2018RE78-30-00-104 * (Left) Thrust Reverser - Main Tracks - Lower Flange - NDT Check
21-Apr-2000Mos
1,155.2 Hrs13,196.46,6006,596.4Hrs
Ldg
78 A/F
Ref.:PSP 612 Part 6 ET-78-30-03 (SOURCE: TLMC 05-10-30)
AWL ≈06-Jul-2018RE78-30-00-104 * (Right) Thrust Reverser - Main Tracks - Lower Flange - NDT Check
21-Apr-2000Mos
1,155.2 Hrs13,196.46,6006,596.4Hrs
Ldg
78 A/F
Ref.:PSP 612 Part 6 ET-78-30-03 (SOURCE: TLMC 05-10-30)
AWL ≈17-Oct-2020RE78-30-00-105 * (Left) Thrust Reverser - Service Pylon Support Rail - NDT Check
14-Nov-2000Mos
2,248.7 Hrs14,289.97,2007,089.9Hrs
Ldg
78 A/F
Ref.:PSP 612 Part 6 ET-78-30-04 (SOURCE: TLMC 05-10-30)
AWL ≈17-Oct-2020RE78-30-00-105 * (Right) Thrust Reverser - Service Pylon Support Rail - NDT Check
14-Nov-2000Mos
2,248.7 Hrs14,289.97,2007,089.9Hrs
Ldg
78 A/F
Ref.:PSP 612 Part 6 ET-78-30-04 (SOURCE: TLMC 05-10-30)
AWL ≈09-Apr-2022T78-30-00-106 * (Left) Service Pylon - Upper and Lower Pylon Track Support Bed - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
78 A/F
Ref.:PSP 612 Part 9 VC-78-30-01 (SOURCE: TLMC 05-10-30)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM418/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
AWL ≈09-Apr-2022T78-30-00-106 * (Right) Service Pylon - Upper and Lower Pylon Track Support Bed - Visual Check
Mos
2,958.8 Hrs15,00015,000Hrs
Ldg
78 A/F
Ref.:PSP 612 Part 9 VC-78-30-01 (SOURCE: TLMC 05-10-30)
MRB ≈20-Oct-2017RE78-30-00-202 (Left) Thrust Reverser Functional Test of auto stow system
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE78-30-00-202 (Right) Thrust Reverser Functional Test of auto stow system
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE78-30-00-208 Thrust Reverser With thrust reversers manually deployed, visual check of blockerdoors, actuators, links and hinges - With thrust reversers stowed, carry out a visual
check to ensure that blocker doors are closed and faired
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈08-May-2018RE78-30-00-212 Thrust Reverser General Visual Check of the torque box, torque box molded seal,fittings, inner and outer skin panels, rib assemblies, ringsegments and attaching
cascades
05-Apr-2005Mos
1,076.8 Hrs (+40)13,118-/+402,40010,718Hrs
Ldg
(PKG 2400 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈13-Jul-2017RE78-30-00-215 Thrust Reverser Thrust Reverser Warning Circuit Functional Test
04-May-2004Mos
684 Hrs (+30)(12,725.2)-/+402,40010,325.2Hrs
Ldg
(PKG 2400 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE78-30-00-216 (Left) Thrust Reverser Thrust Reverser Unlocked Light Functional Test
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE78-30-00-216 (Right) Thrust Reverser Thrust Reverser Unlocked Light Functional Test
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE78-30-00-218 Ballscrew Actuators Lubrication of Ballscrew Actuators and Mounts
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
78 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
≈09-Apr-2022RE78-30-00-403 T/R MAIN TRACK UPPER FLANGE NDT
20-Sep-1983Mos
2,958.8 Hrs15,00015,0000Hrs
Ldg
78 A/F
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM419/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
≈06-Jun-2016RE78-30-00-407 T/R MAIN TRACK ACT FIT ATT HOLE NDT
07-Jun-2004Mos
155 Hrs12,196.21,80010,396.2Hrs
Ldg
78 A/F
MRB ≈03-May-2017RE78-30-11-209 Cascades/Pylon Tracks Visual Check
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
78 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈18-Sep-2016RE78-30-16-219 Thrust Reverser (Pre SB 601-1084) Detailed Inspection of the 6 o’clock SAM Panel and Underlying Brackets
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈08-May-2018RE78-30-26-204 Blocker Doors Special Detailed Inspection of Blocker Door Bushings
05-Apr-2005Mos
1,076.8 Hrs (+40)13,118-/+402,40010,718Hrs
Ldg
(PKG 2400 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE78-30-31-210 Main Tracks Visual Check of the main track and attachments
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
78 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE78-30-41-201 (Left) Main and Pylon Track Slider Blocks Detailed Inspection of slider block
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE78-30-41-201 (Right) Main and Pylon Track Slider Blocks Detailed Inspection of slider block
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE78-30-46-206 Pneumatic Drive/Flexshaft Lock Unit (Pre Allied Signal SB 126758-78-1487) - Remove filter from flexshaft lock, check and reinstall
10-Feb-2016Mos
590.8 Hrs (+40)12,611.2-/+4060012,020.4Hrs
6,728Enc
(PKG 600 Eng Hour)
78 ENG2
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15) (NOTE: (Pre Allied Signal SB 126758-78-1487))
MRB ≈03-May-2017RE78-30-46-206 Pneumatic Drive/Flexshaft Lock Unit (Pre Allied Signal SB 126758-78-1487) - Remove filter from flexshaft lock, check and reinstall
10-Feb-2016Mos
590.8 Hrs (+40)12,728.2-/+4060012,137.4Hrs
6,769Enc
(PKG 600 Eng Hour)
78 ENG1
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15) (NOTE: (Pre Allied Signal SB 126758-78-1487))
MRB ≈08-May-2018RE78-30-51-217 Flexshafts Special Detailed Inspection of Flexshaft
05-Apr-2005Mos
1,076.8 Hrs (+40)13,118-/+402,40010,718Hrs
Ldg
(PKG 2400 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈08-May-2018RE78-30-56-214 Ballscrew Actuators Inspection Detailed Inspection of Ballscrew Actuator
05-Apr-2005Mos
1,076.8 Hrs (+40)13,118-/+402,40010,718Hrs
Ldg
(PKG 2400 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM420/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈20-Oct-2017RE78-30-61-213 (Left) Auto-Throttle Retarder Control Functional Test of Auto-Throttle Retarder and Throttle Lock
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈20-Oct-2017RE78-30-61-213 (Right) Auto-Throttle Retarder Control Functional Test of Auto-Throttle Retarder and Throttle Lock
29-Oct-2012Mos
812.3 Hrs (+40)(12,853.5)-/+401,20011,653.5Hrs
Ldg
(PKG 1200 Hour)
78 A/F
(SOURCE: TLMC 05-20-15)
CPCPREC78-00-801 Thrust Reverser - CPCP Check including the following items: (1) Pylon / (2) Pylon track and support rail / (3) Main tracks with attachment fitiings
5.8 Months (+30
Days)(26-Sep-2016)-/+16026-Sep-2011Mos
Hrs
Ldg
(PKG 60 Month)
78 A/F
(SOURCE: TLMC 05-30-20)
▼ 79 - OIL
RE (O/C)A-Sump Scavenge Pump
27-Jun-2005Mos
10,839Hrs
5,949Enc
79 ENG24018T11P02LJA39980
RE (O/C)A-Sump Scavenge Pump
20-Sep-1983Mos
0Hrs0
0Enc0
79 ENG1New4018T11P02
LJA11682
RE (O/C)Engine Oil Filter
04-May-2004Mos
10,325.2Hrs
5,223Enc
79 ENG24012373-81282063649
RE (O/C)Engine Oil Filter
20-Sep-1983Mos
0Hrs
0Enc
79 ENG1UnknownUnknown
RE (O/C)Engine Oil Level Control
20-Sep-1983Mos
0Hrs
0Ldg
79 A/FUnknownUnknown
RE (O/C)Engine Oil Pressure Switch
20-Sep-1983Mos
0Hrs
0Ldg
No.179 A/FUnknownUnknown
RE (O/C)Engine Oil Pressure Switch
20-Sep-1983Mos
0Hrs
0Ldg
No.279 A/FUnknownUnknown
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM421/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Engine Oil Pressure Transducer
20-Sep-1983Mos
0Hrs
0Ldg
Left79 A/FUnknownUnknown
RE (O/C)Engine Oil Pressure Transducer
20-Sep-1983Mos
0Hrs
0Ldg
Right79 A/FUnknownUnknown
RE (O/C)Lube & Scavenge Pump
15-Sep-2007Mos
11,073.6Hrs
6,114Enc
79 ENG24022T27G22NMAA0807
RE (O/C)Lube & Scavenge Pump
31-May-2005Mos
10,956Hrs10,956
5,990Enc5,990
79 ENG1Overhauled4022T27G22
NMAA0611
RE (O/C)Lubricating System Pump
20-Sep-1983Mos
0Hrs
0Ldg
79 A/FUnknownUnknown
RE (O/C)Oil Cooler
27-Jun-2005Mos
10,839Hrs10,839
5,949Enc5,949
79 ENG2Overhauled4048T39P01
AEY02609
RE (O/C)Oil Cooler
31-May-2005Mos
10,956Hrs10,956
5,990Enc5,990
79 ENG1Overhauled4048T39P01
AEY02491
RE (O/C)Oil Filter Bypass Sensor
20-Sep-1983Mos
0Hrs
0Enc
79 ENG1UnknownUnknown
RE (O/C)Oil Filter Bypass Sensor
20-Sep-1983Mos
0Hrs
0Enc
79 ENG2UnknownUnknown
RE (O/C)Oil Filter Bypass Sensor
20-Sep-1983Mos
0Hrs0
0Ldg0
Left79 A/FNew4060T64P01
UNKNOWN
RE (O/C)Oil Filter Bypass Sensor
20-Sep-1983Mos
0Hrs0
0Ldg0
Right79 A/FNew4060T64P01
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM422/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Oil Level Probe
20-Sep-1983Mos
0Hrs
0Ldg
Left79 A/FUnknownUnknown
RE (O/C)Oil Level Probe
20-Sep-1983Mos
0Hrs0
0Ldg0
Right79 A/FNew20016-0000-01
UNKNOWN
RE (O/C)Oil Pressure Indicator
02-Oct-2002Mos
8,878.7Hrs
4,374Ldg
79 A/F601-50915-1663
RE (O/C)Oil Tank
20-Sep-1983Mos
0Hrs
0Enc
79 ENG1UnknownUnknown
RE (O/C)Oil Tank
20-Sep-1983Mos
0Hrs
0Enc
79 ENG2UnknownUnknown
RE (O/C)Oil Temperature Indicator
20-Sep-1983Mos
0Hrs
0Ldg
79 A/FUnknownUnknown
RE (O/C)Selector - Oil Repl System Valve
14-Nov-2006Mos
10,923.5Hrs
5,578Ldg
79 A/FP194-39505-1209177
OptionalT (A/R)601-0639 Modification - Indicating - Add an On/Off Power Switch for the Engine Oil Indicating Board in Junction Box JB4
Mos
Hrs
Ldg
79 A/FEff: 15-Sep-2014
RecommendedRE (-)601-1098 Modification - Oil Storage - Replacement of Oil Tank Support Beams
30-Oct-1998Mos
Hrs
Ldg
79 A/FSB 79-9Eff: 30-Oct-1998 Complied
With
Cat. 7 - OptionalRE (-)75-0004 R00 AIR - Air System (75-00-00) - Introduction of New T2 Sensor Anti-icing Air Tube
Mos
Hrs
Enc
79 ENG1Eff: 07-Mar-2000
Cat. 7 - OptionalRE (-)75-0004 R00 AIR - Air System (75-00-00) - Introduction of New T2 Sensor Anti-icing Air Tube
Mos
Hrs
Enc
79 ENG2Eff: 07-Mar-2000
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM423/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedT (A/R)79-0002 R00 OIL SYSTEM - Increased Capacity C-sump Scavenge Lines
Mos
Hrs
Enc
79 ENG1Eff: 25-Apr-1991
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
RecommendedT (A/R)79-0002 R00 OIL SYSTEM - Increased Capacity C-sump Scavenge Lines
Mos
Hrs
Enc
79 ENG2Eff: 25-Apr-1991
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
RecommendedRE (-)79-0003 R01 OIL SYSTEM - A-Sump Scavenge Pump: Inspection of Drive Coupling (Muff Gear)
Mos
Hrs
Enc
79 ENG1Eff: 06-Nov-1991
RecommendedRE (-)79-0003 R01 OIL SYSTEM - A-Sump Scavenge Pump: Inspection of Drive Coupling (Muff Gear)
Mos
Hrs
Enc
79 ENG2Eff: 06-Nov-1991
RecommendedRE (-)79-0006 R03 OIL SYSTEM - Introduction and Field Installation of Improved Stainless Steel Oil Tank Support Beams
Mos
Hrs
Enc
79 ENG1Eff: 31-Mar-1999
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
RecommendedRE (-)79-0006 R03 OIL SYSTEM - Introduction and Field Installation of Improved Stainless Steel Oil Tank Support Beams
Mos
Hrs
Enc
79 ENG2Eff: 31-Mar-1999
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
RecommendedRE (-)79-0007 R01 OIL SYSTEM - Replacement of Lube and Scavenge Pump Spur Gear
Mos
Hrs
Enc
79 ENG1Eff: 16-Dec-1997
RecommendedRE (-)79-0007 R01 OIL SYSTEM - Replacement of Lube and Scavenge Pump Spur Gear
Mos
Hrs
Enc
79 ENG2Eff: 16-Dec-1997
RecommendedRE (-)79-0008 R01 OIL SYSTEM - Introduction of Improved (Non-Coated) Oil Tank on Fielded Engines and New Production Engines, and Elimination of A-sump Scavenge Pump on New
Production Engines
Mos
Hrs
Enc
79 ENG1Eff: 03-Mar-1999
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM424/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RecommendedRE (-)79-0008 R01 OIL SYSTEM - Introduction of Improved (Non-Coated) Oil Tank on Fielded Engines and New Production Engines, and Elimination of A-sump Scavenge Pump on New
Production Engines
Mos
Hrs
Enc
79 ENG2Eff: 03-Mar-1999
Category 3RE (-)79-0009 R00 OIL SYSTEM Introduction and Field Installation of Improved Stainless Steel Oil Tank Support Beams
Mos
Hrs
Enc
79 ENG1Eff: 31-Jan-2011
Category 3RE (-)79-0009 R00 OIL SYSTEM Introduction and Field Installation of Improved Stainless Steel Oil Tank Support Beams
Mos
Hrs
Enc
79 ENG2Eff: 31-Jan-2011
Category 3RE (-)79-0009 R01 OIL SYSTEM Introduction and Field Installation of Improved Stainless Steel Oil Tank Support Beams
Mos
Hrs
Enc
79 ENG1Eff: 14-Apr-1998
Category 3RE (-)79-0009 R01 OIL SYSTEM Introduction and Field Installation of Improved Stainless Steel Oil Tank Support Beams
Mos
Hrs
Enc
79 ENG2Eff: 14-Apr-1998
Cat. 3 - RecommendedT (A/R)79-0009 R02 OIL SYSTEM - Introduction and Field Installation of Improved Stainless Steel Oil Tank Support Beams
Mos
Hrs
Enc
79 ENG1Eff: 05-Jan-2011
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
Cat. 3 - RecommendedT (A/R)79-0009 R02 OIL SYSTEM - Introduction and Field Installation of Improved Stainless Steel Oil Tank Support Beams
Mos
Hrs
Enc
79 ENG2Eff: 05-Jan-2011
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
RecommendedT (A/R)79-0013 R00 OIL - Oil System (79-00-00) - Introduction of Flex-Metal Oil Filter Impending Bypass Hose Assemblies
Mos
Hrs
Enc
79 ENG1Eff: 03-Apr-2001
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG172
RecommendedT (A/R)79-0013 R00 OIL - Oil System (79-00-00) - Introduction of Flex-Metal Oil Filter Impending Bypass Hose Assemblies
Mos
Hrs
Enc
79 ENG2Eff: 03-Apr-2001
Also ConsiderDUE:1. RE -ENGINE - General (72-00-00) - Upgrade of CF34-1A and CF34-3A...72-0195 R08ENG272
Cat. 7 - OptionalRE (-)79-0014 R00 OIL - Service Evaluation for Lube and Scavenge Pump Assembly
Mos
Hrs
Enc
79 ENG1Eff: 10-Apr-2001
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM425/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 7 - OptionalRE (-)79-0014 R00 OIL - Service Evaluation for Lube and Scavenge Pump Assembly
Mos
Hrs
Enc
79 ENG2Eff: 10-Apr-2001
RecommendedRE (-)79-0016 R00 OIL - Lube and Scavenge Components (79-00-00) - Introduction of Improved Lube and Scavenge Pump Assembly PN 6087T04P06
Mos
Hrs
Enc
79 ENG1Eff: 18-Oct-2001
RecommendedRE (-)79-0016 R00 OIL - Lube and Scavenge Components (79-00-00) - Introduction of Improved Lube and Scavenge Pump Assembly PN 6087T04P06
Mos
Hrs
Enc
79 ENG2Eff: 18-Oct-2001
Cat. 9 - InformationalRE (-)79-0025 R00 Oil - General (79-00-00) - Approved Oils
Mos
Hrs
Enc
79 ENG1Eff: 07-Sep-2007
Cat. 9 - InformationalRE (-)79-0025 R00 Oil - General (79-00-00) - Approved Oils
Mos
Hrs
Enc
79 ENG2Eff: 07-Sep-2007
Cat. 9 - InformationalRE (-)79-0025 R01 Oil - General (79-00-00) - Approved Oils
Mos
Hrs
Enc
79 ENG1Eff: 09-Jul-2010
Cat. 9 - InformationalRE (-)79-0025 R01 Oil - General (79-00-00) - Approved Oils
Mos
Hrs
Enc
79 ENG2Eff: 09-Jul-2010
Cat. 9 - InformationalRE (-)79-0025 R02 Oil - General (79-00-00) - Approved Oils
Mos
Hrs
Enc
79 ENG1Eff: 12-Dec-2011
Cat. 9 - InformationalRE (-)79-0025 R02 Oil - General (79-00-00) - Approved Oils
Mos
Hrs
Enc
79 ENG2Eff: 12-Dec-2011
Cat. 9 - InformationalT (-)79-0025 R03 Oil - General (79-00-00) - Approved Oils
Mos
Hrs
Enc
79 ENG1Eff: 08-May-2012
Cat. 9 - InformationalT (-)79-0025 R03 Oil - General (79-00-00) - Approved Oils
Mos
Hrs
Enc
79 ENG2Eff: 08-May-2012
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM426/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
Cat. 9 - InformationalT (-)79-0025 R04 Oil - General (79-00-00) - Approved Oils
Mos
Hrs
Enc
79 ENG1Eff: 01-Dec-2014
Cat. 9 - InformationalT (-)79-0025 R04 Oil - General (79-00-00) - Approved Oils
Mos
Hrs
Enc
79 ENG2Eff: 01-Dec-2014
Category 9T (A/R)79-0025 R05 Oil - General (79-00-00) - Approved Oils
Mos
Hrs
Enc
79 ENG1Eff: 14-Oct-2015
Category 9T (A/R)79-0025 R05 Oil - General (79-00-00) - Approved Oils
Mos
Hrs
Enc
79 ENG2Eff: 14-Oct-2015
Cat. 6 - RecommendedRE (-)79-0028 R00 OIL - Oil System (79-00-00) - Introduction of Improved Oil Filter Bypass Sensor P/N 4060T64P04
Mos
Hrs
Enc
79 ENG1Eff: 29-Jun-2010
Cat. 6 - RecommendedRE (-)79-0028 R00 OIL - Oil System (79-00-00) - Introduction of Improved Oil Filter Bypass Sensor P/N 4060T64P04
Mos
Hrs
Enc
79 ENG2Eff: 29-Jun-2010
MRB ≈10-May-2017RE79-20-21-203 Oil Filter Assembly - Inspect and install new filter element
10-Feb-2016Mos
600 Hrs (+40)(12,737.4)-/+4060012,137.4Hrs
6,769Enc
(PKG 600 Eng Hour)
79 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE79-20-21-203 Oil Filter Assembly - Inspect and install new filter element
10-Feb-2016Mos
590.8 Hrs (+40)(12,611.2)-/+4060012,020.4Hrs
6,728Enc
(PKG 600 Eng Hour)
79 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
Servicing - RecommendedRE (A/R)79-20-21-301 Oil Filter Assembly - Inspect and install new filter element on new or overhauled engine
Mos
Hrs
Enc
79 ENG1
Ref.:G.E. M.M. SEI-580 Section 5-21-00 (ZONE: 410, 420) (ACCESS: 412-AB -AT, 414-AB -AT, 422-AB -AT, 424-AB -AT) (SOURCE: MPD 3.2)
(NOTE: This is a one-time item only for new or overhauled engines. Subsequent servicing is covered by item 79-20-21-203.)
Servicing - RecommendedRE (A/R)79-20-21-301 Oil Filter Assembly - Inspect and install new filter element on new or overhauled engine
Mos
Hrs
Enc
79 ENG2
Ref.:G.E. M.M. SEI-580 Section 5-21-00 (ZONE: 410, 420) (ACCESS: 412-AB -AT, 414-AB -AT, 422-AB -AT, 424-AB -AT) (SOURCE: MPD 3.2)
(NOTE: This is a one-time item only for new or overhauled engines. Subsequent servicing is covered by item 79-20-21-203.)
MRB ≈20-Oct-2017RE79-20-26-208 Oil/Fuel Heat Exchanger Assembly - Visual Check, paying particular attention for chafing of housing from loop clamp on C-Sump aft scavenge hose
29-Oct-2012Mos
812.3 Hrs (+40)(12,949.7)-/+401,20011,749.7Hrs
Enc
(PKG 1200 Eng Hour)
79 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM427/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
MRB ≈20-Oct-2017RE79-20-26-208 Oil/Fuel Heat Exchanger Assembly - Visual Check, paying particular attention for chafing of housing from loop clamp on C-Sump aft scavenge hose
29-Oct-2012Mos
812.3 Hrs (+40)(12,832.7)-/+401,20011,632.7Hrs
Enc
(PKG 1200 Eng Hour)
79 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈03-Apr-2016RE79-20-31-201 Chip Detector - Check Chip Detector (5 per engine)
11-Nov-2015Mos
71.6 Hrs12,20910012,109Hrs
Enc
79 ENG1
(SOURCE: TLMC 05-20-15)
MRB ≈03-Apr-2016RE79-20-31-201 Chip Detector - Check Chip Detector (5 per engine)
11-Nov-2015Mos
71.6 Hrs12,09210011,992Hrs
Enc
79 ENG2
(SOURCE: TLMC 05-20-15)
MRB ≈22-Feb-2021RE79-21-01-202 C-Sump Scavenge Screens - Detailed Inspection
05-Jun-2009Mos
2,417.4 Hrs (+40)(14,554.8)-/+403,00011,554.8Hrs
Enc
(PKG 3000 Eng Hour)
79 ENG1
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈24-Nov-2019RE79-21-01-202 C-Sump Scavenge Screens - Detailed Inspection
28-Jul-2005Mos
1,818.6 Hrs (+40)(13,839)-/+403,00010,839Hrs
Enc
(PKG 3000 Eng Hour)
79 ENG2
Ref.:G.E. MM SEI-580 Section 5-21-00 (SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE79-30-26-204 Oil Filter Impending Bypass Sensor - Functional Test
10-Feb-2016Mos
590.8 Hrs (+40)(12,611.2)-/+4060012,020.4Hrs
6,728Enc
(PKG 600 Eng Hour)
79 ENG2
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
MRB ≈10-May-2017RE79-30-26-204 Oil Filter Impending Bypass Sensor - Functional Test
10-Feb-2016Mos
600 Hrs (+40)(12,737.4)-/+4060012,137.4Hrs
6,769Enc
(PKG 600 Eng Hour)
79 ENG1
(SOURCE: TLMC 05-20-15)
RE (O/C)7930505 Pressure Switch (Oil)
Mos
Hrs
Ldg
Right79 A/FUnknownUnknown
▼ 80 - STARTING
RE (O/C)Engine Air Start Valve
20-Sep-1983Mos
0Hrs0
0Ldg0
Left80 A/FNew898930-3-1
UNKNOWN
RE (O/C)Engine Air Start Valve
20-Sep-1983Mos
0Hrs
0Ldg
Right80 A/FUnknownUnknown
RE (O/C)Engine Air Starter
20-Sep-1983Mos
0Hrs0
0Ldg0
Left80 A/FNew3505188-7-1
UNKNOWN
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM428/429
BOMBARDIERChallenger 601 N213TS,SN 3013
N213TS STATUS REPORT (with relations)
Owner/Operator: DuPage Aerospace Corporation DuPage
Aerospace Corporation
RemainingDUETOLREQCWTSITSRITSOITSNIMOC Note or Component StatePN/SN
TimeCategoriesDescriptionTask No
RE (O/C)Engine Air Starter
20-Sep-1983Mos
0Hrs
0Ldg
Right80 A/FUnknownUnknown
MRB ≈18-Sep-2016RE80-10-11-201 Air Turbine Starter/Air Turbine Starter Replenishing Visual Check - Check Oil level
10-Feb-2016Mos
290.8 Hrs (+40)(12,332)-/+4030012,041.2Hrs
6,326Ldg
(PKG 300 Hour)
80 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈10-May-2017RE80-10-11-202 (Left) Air Turbine Starter Air Turbine Starter (ATS) Oil change
10-Feb-2016Mos
600 Hrs (+40)12,641.2-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
80 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈10-May-2017RE80-10-11-202 (Right) Air Turbine Starter Air Turbine Starter (ATS) Oil change
10-Feb-2016Mos
600 Hrs (+40)12,641.2-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
80 A/F
(SOURCE: TLMC 05-20-15)
MRB ≈03-May-2017RE80-10-11-203 Air Turbine Starter (Part No. 3505188-9 and Subs) - Detailed Inspection of the Drain-Plug Magnetic Chip-Detector
10-Feb-2016Mos
590.8 Hrs (+40)(12,632)-/+4060012,041.2Hrs
6,326Ldg
(PKG 600 Hour)
80 A/F
(Tol. Adjustment: -9.2 Hrs) (SOURCE: TLMC 05-20-15)
[ ]: Manual entry, (): Package, ≠: Masked Due, ≈: Estimated, Δ: Deficient, OVD: Overdue, Tol: Tolerance
Generated: 6-Apr-2016 1:16 PM429/429