Modification Control Report 13237 23.Oct - · PDF file1974-08-09 ad 03 mandatory a/c lavatory...

Document-Number Type Rev Compliance A|C Subject Status1974-08-09 AD 03 MANDATORY A/C LAVATORY WASTE RECEPTACLES ACCESS DOOR INSPECTION Taskcard Controlled

AD §a.(1): No smoking sign inst. on or beside lav door. Complied withat build.AD §a.(2): No cigarette disposal plackard at waste disposal door.Complied with at build.AD §b: No smoking sign extuinguish in cabin after take off. Internaloperativ procedure.AD §c: Ashtray at Lav door. Complied with at build.AD §d: MEL, NAS MEL, FAA MMEL. NAS Follows FAA MMEL which is morestringent than AD.AD §e, (1) og (2): Repetitive requirement to inspect waste disposalbin function. Ref MPD task.

Task controlled:CL:25-040-00-01NG: 25-120-00-01, 25-130-00-012010-NM-018-AD25-040-00-01 (TASK CL)25-130-00-01 (TASK NG)

NPRMMPDMPD

000000

Carried out on the following Taskcards25-040-00-01 (for A/C-Type: '733')Carried out on the following TaskcardsTaskcard: 25-040-00-01 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks12.02.2015 74'319/H 998:01/H Interval:1000/HPerf Dim1 (D) Perf Dim2 Perf Dim311.10.2014 73319:36/H 44494/CThis Document SUPERSEDES 1974-08-09/AD Rev.02Reason for this StatusAUTO ASSIGNED

Document-Number Type Rev Compliance A|C Subject Status

For Aircraft `LN-KKM` (S/N: 24676, Act.TAH: 73322, Act.TAC: 44495)Selection: AIRWORTHINESS DIRECTIVE

produced by www.swiss-as.comAMOS

Modification Control Report 13237 17:07

23.Oct.2014Page 1/429


1974-08-09 AD 02 MANDATORY A/C LAVATORY WASTE RECEPTACLES ACCESS DOOR INSPECTION Superseded (Superseded)AD §a.(1): No smoking sign inst. on or beside lav door. Complied withat build.AD §a.(2): No cigarette disposal plackard at waste disposal door.Complied with at build.AD §b: No smoking sign extuinguish in cabin after take off. Internaloperativ procedure.AD §c: Ashtray at Lav door. Complied with at build.AD §d: MEL, NAS MELAD §e, (1) og (2): Repetitive requirement to inspect waste disposalbin function. Ref MPD task.

Task controlled:CL:25-040-00-01NG: 25-120-00-01, 25-130-00-012010-NM-018-AD NPRM 00This Document SUPERSEDES 1974-08-09/AD Rev.01This Document has been SUPERSEDED BY 1974-08-09/AD Rev.03Reason for this StatusAUTO ASSIGNED

1974-08-09 AD 00 MANDATORY A/C LAVATORY WASTE RECEPTACLES ACCESS DOOR INSPECTION Superseded (Superseded)1974-08-09-R2 (ACTIVE)37-25-040-00-01(REPETITIVE-CL)87-BI-WEEKLY (REPETITIVE-NG)

ADTATA

This Document has been SUPERSEDED BY 1974-08-09/AD Rev.01


For Aircraft `LN-KKM` (S/N: 24676, Act.TAH: 73322, Act.TAC: 44495)Selection: AIRWORTHINESS DIRECTIVE For Aircraft `LN-KKM` (S/N: 24676, Act.TAH: 73322, Act.TAC: 44495)Selection: AIRWORTHINESS DIRECTIVE



23.Oct.2014Page 2/429

Document-Number Type Rev Compliance A|C Subject Status1974-08-09 AD 01 MANDATORY A/C LAVATORY WASTE RECEPTACLES ACCESS DOOR INSPECTION Superseded (Superseded)

1974-08-09-R2 (ACTIVE)37-25-040-00-01(REPETITIVE-CL)87-BI-WEEKLY (REPETITIVE-NG)

ADTATA

This Document SUPERSEDES 1974-08-09/AD Rev.00This Document has been SUPERSEDED BY 1974-08-09/AD Rev.02

1979-18-12 AD 00 MANDATORY COMP *AD* TO PREVENT THE RELEASE OF HIGH ENERGY TURBINE WHEEL BLADEFRAGMENTS

Not Applicable

NA for GTCP85-129 i.a.w. Honeywell SB 49-A5078 R1.85-49A5078 SB 01Perform within an unlimited threshold.

1979-18-12/AD Rev.00 *AD* TO PREVENT THE RELEASE OF HIGH ENERGY TURBINE WHEEL BLADEFRAGMENTS

Not Applicable

> 85-49A5078/SB* Rev.01 REPLACE/REWORK EXHAUST PIPE ASSEMBLY FOR IMPROVED TURBINE WHEELBLADE CONTAINMENT

Not Applicable

Affected Rotables (Part No/Serial No/Position) Status

380428-10-1 / P-60280C Pos=APU (KKM)Not Applicable / Reason: AUTOASSIGNED

1984-18-07 AD 00 MANDATORY COMP DISCHARGE CARTRIDGES PART NUMBER (P/N) 873571, 876296, Not Applicable by Serial NumberCompliance:AD § (a) is Not Applicable to NAS AC. We do not have the affected PNinstalled.1985-18-07 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 3/429

Document-Number Type Rev Compliance A|C Subject Status1985-11-52 AD 00 MANDATORY A/C *AD* TO PREVENT ENGINE FLAMEOUTS DURING CLIMB Superseded (Superseded)

1985-11-52-R1 (ACTIVE) ADThis Document has been SUPERSEDED BY 1985-11-52/AD Rev.01

1985-11-52 AD 01 MANDATORY A/C *AD* TO PREVENT ENGINE FLAMEOUTS DURING CLIMB Not ApplicableCompleted during Manufacture.Refer to Boeing document of FAA AD status at build.1985-11-52-R1 (ACTIVE) ADThis Document SUPERSEDES 1985-11-52/AD Rev.00

1985-19-01 AD 00 MANDATORY COMP REPLACE ROSEMOUNT AOA SENSORS S/N 00001 THROUGH 00173 Not Applicable by Serial NumberThe AD is also registered as performed on all B737-CL ref BOEING ADDOC R-6744-X.

Compliance:AD § (b) is Not Applicable to NAS, affected PN not installed.737-27A1126 SB 01Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

1985-19-04 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 1985-25-04 Superseded (Not Applicable bySerial Number)

1985-19-04 (SUPERSEDED)1985-25-04 (ACTIVE)737-25A1182-R4 (ACTIVE)

ADADSB


1985-21-01 AD 00 MANDATORY A/C *AD* TO DETECT LOOSE CONE BOLTS - FWD ENGINE MOUNT Not Applicable by Serial Number1985-21-01 (ACTIVE)BOEING TELEX M-7272-2396

ADSL





23.Oct.2014Page 4/429

Document-Number Type Rev Compliance A|C Subject Status1985-22-10 AD 00 MANDATORY A/C FLIGHT DIRECTOR INDICATORS AND HORIZONTAL SITUATION IND Not Applicable

Compliance:AD § (a) through (d) is not applicable, Effected PN not installed onNAS AC.1985-22-10 (ACTIVE) ADReason for this StatusAUTO ASSIGNED

1985-25-04 AD 00 MANDATORY A/C *AD* ESCAPE SLIDE INSPECTION / MODIFICATION Not ApplicableThis document is applicable to LN# 1-1170.1985-25-04 (ACTIVE)737-25A1182-R2 (ACTIVEPRR 34041

ADSBPRR 00

This Document SUPERSEDES 1985-19-04/AD Rev.001985-25-04/AD Rev.00 *AD* ESCAPE SLIDE INSPECTION / MODIFICATION Not Applicable

This Document SUPERSEDES 1985-19-04/AD Rev.00> 737-25A1182/SB* Rev.00 *AD* EVACUATION SLIDE COMPARTMENT LATCH ASSEMBLY REPLACEMENT Not Applicable by Serial Number

1986-05-02 AD 00 MANDATORY COMP UNITED INSTRUMENTS, INC. ALTIMETER PART NUMBERS 5934 Not Applicable by Serial NumberCompliance:AD § (a) through (d) is Not Applicable, Effected PN not installed onNAS AC.1986-05-02 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 5/429

Document-Number Type Rev Compliance A|C Subject Status1986-05-04 AD 00 MANDATORY A/C *AD* ESCAPE SLIDE COVER STRAPS Not Applicable

Mod appl: LN#: 1-11701986-05-04 (ACTIVE)737-25A1182-R2 (ACTIVEPRR 34041

ADSBPRR 00

1986-05-04/AD Rev.00 *AD* ESCAPE SLIDE COVER STRAPS Not Applicable> 737-25A1182/SB* Rev.00 *AD* EVACUATION SLIDE COMPARTMENT LATCH ASSEMBLY REPLACEMENT Not Applicable by Serial Number

1986-08-05 AD 00 MANDATORY COMP *AD* SPIROLOCK AND OIL DISTRIBUTOR INSP. Superseded (Superseded)This AD 1986-08-05 is applicable for CFM56-3B/3B2 in SN range 720000to 720190 engines only.1986-08-053-72-0205

ADSB

0105

This Document has been SUPERSEDED BY 1986-08-05/AD Rev.01Affected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 724473 Pos=LH (KKM) SupersededCFM56-3B2 / 725495 Pos=RH (KKM) Superseded





23.Oct.2014Page 6/429

Document-Number Type Rev Compliance A|C Subject Status1986-08-05 AD 01 MANDATORY COMP SPIROLOCK AND OIL DISTRIBUTOR INSP. Not Applicable

This AD 1986-08-05 is applicable for CFM56-3B/3B2 in SN range 720000to 720190 engines only.Status apply for EASA AD 1986-066.1986-08-053-72-0205

ADSB

0105

This Document SUPERSEDES 1986-08-05/AD Rev.001986-08-05/AD Rev.01 SPIROLOCK AND OIL DISTRIBUTOR INSP. Not Applicable

This Document SUPERSEDES 1986-08-05/AD Rev.00> 3-72-0205/SB* Rev.05 OIL DISTRIBUTOR, INSPECTION AND SERVICE OF Not Applicable by Serial Number

This Document SUPERSEDES 3-72-0205/SB Rev.04Affected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 725495 Pos=RH (KKM) Not ApplicableCFM56-3B2 / 724473 Pos=LH (KKM) Not Applicable

1986-18-04 AD 00 MANDATORY A/C *AD* TO DETECT INSUFFICIENT SELF-LOCKING NUTS Not Applicable by Serial Number1986-18-04 (ACTIVE)737-SL-27-38-A (ACTIVE)

ADSL

1986-19-03 AD 00 MANDATORY A/C *AD* HTL FIRE EXTINGUISHER DISCHARGE OUTLETS Not ApplicableMod appl. LN#: 1-10621986-19-03 (ACTIVE)737-26A1029 (ACTIVE)

ADSB

1986-19-03/AD Rev.00 *AD* HTL FIRE EXTINGUISHER DISCHARGE OUTLETS Not Applicable> 737-26A1029/SB* Rev.03 *AD* HTL FIRE EXTINGUISHER DISCHARGE OUTLETS Not Applicable by Serial Number





23.Oct.2014Page 7/429

Document-Number Type Rev Compliance A|C Subject Status1986-19-06 AD 00 MANDATORY A/C *AD* TO ENSURE AIR DUCTS HAVE ADEQUATE FLAMMABILITY CHARACT. Not Applicable

Mod appl.: LN#: 1-11931986-19-06 (ACTIVE)737-21-1085 (ACTIVEPRODUCTION LINE PRR33656

ADSBPRR

1986-19-06/AD Rev.00 *AD* TO ENSURE AIR DUCTS HAVE ADEQUATE FLAMMABILITY CHARACT. Not Applicable> 737-21-1085/SB* Rev.01 *AD* TO ENSURE AIR DUCTS HAVE ADEQUATE FLAMMABILITY CHARACT. Not Applicable by Serial Number

1986-22-03 AD 00 MANDATORY A/C *AD* MINIMIZE FIRE HAZARD DUE TO FUEL FEED TUBE ASSY CHAFING Not ApplicableMod appl: LN# 1-1193737-28A1062 SB 02

1986-22-03/AD Rev.00 *AD* MINIMIZE FIRE HAZARD DUE TO FUEL FEED TUBE ASSY CHAFING Not Applicable> 737-28A1062/SB* Rev.02 *AD* MINIMIZE FIRE HAZARD DUE TO FUEL FEED TUBE ASSY CHAFING Not Applicable by Serial Number

1986-22-10 AD 00 MANDATORY COMP COLLINS MODEL DME-42, P/N 622-6263-002, DISTANCE MEASUR Not Applicable by Serial NumberCompliance:AD § (a), (b) is Not Applicable, Effected PN not installed on NAS AC.1986-22-10 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

1986-25-01 AD 00 MANDATORY COMP VOR-ILS NAVIGATION RECEIVERS, PART NUMBER 622-3255-XXX Not Applicable by Serial NumberCompliance:AD § (a), (b) is Not Applicable, Effected PN not installed on NAS AC.1986-25-01 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 8/429

Document-Number Type Rev Compliance A|C Subject Status1987-06-02 AD 00 MANDATORY COMP SPERRY ELECTRONICS FLIGHT INSTRUMENT SYSTEMS (EFIS) SYM Not Applicable by Serial Number

Compliance:AD § (a), (b) is Not Applicable, Effected PN not installed on NAS AC.1987-06-02 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 9/429

Document-Number Type Rev Compliance A|C Subject Status1987-08-09 AD 00 MANDATORY A/C PROCEDURE TO ELIMINATE THE POSSIBILITY OF TIRE EXPLOSION Taskcard Controlled

Compliance:737-300:AD § 1 and 2 is covered by MPD task 12-015-51-01.

737-800:The 737-800 is discussed in Boeing Letter B-T113-98-0589 and FAALetter 98-103S-83.This letter includes all AD incorperated via type design, the 737-800complies with FAR.25.733(e) amendment 78 at build.The AMM ensurecontinued compliance.Continued compliance is also covered by application of a Decal.AD § 1) is covered by TO 738-32-001.AD § 2) is covered by MPD task 32-350-00-01, this task is performedat every S-check (every 72 clock hour).12-015-51-01 (TASK-CL)1987-08-09 (ACTIVE)32-350-00-01 (TASK-NG)98-103S-83BOEING LETTER B-T113-98-0589

AMMADAMMAMOCBM

0000000000

Carried out on the following TaskcardsTaskcard: 12-015-51-01 Maint. Progr.: AMP 737-CLPerf Dim1 (D) Perf Dim2 Perf Dim308.10.2010 62555:00/H 36241/CReason for this StatusAUTO ASSIGNED

1987-08-09/AD* Rev.00 PROCEDURE TO ELIMINATE THE POSSIBILITY OF TIRE EXPLOSION Taskcard ControlledCarried out on the following TaskcardsTaskcard: 12-015-51-01 Maint. Progr.: AMP 737-CLPerf Dim1 (D) Perf Dim2 Perf Dim3





23.Oct.2014Page 10/429

Document-Number Type Rev Compliance A|C Subject Status08.10.2010 62555:00/H 36241/CReason for this StatusAUTO ASSIGNED

1987-16-07 AD 00 MANDATORY COMP APPLIES TO ALL DIGITAL AND ANALOG ELECTRONIC FLIGHT INS ERRONEOUSDISPLAY OF THE ANGLE OF ATTACK FAST/SLOW PRESENTATION

Not Applicable by Serial Number

Compliance:AD § (a) and (b) is Not Applicable, affected PN is not installed onNAS aircraft.1987-16-07 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

1987-17-06 AD 00 MANDATORY A/C *AD* AM-SAFE, INCORPORATED AM-SAFE, INC., OCCUPANT RESTRAINT Not ApplicableNot applicable due to; NAS does not install AMSAFE PN:501825-403,501907-401, 501907-403, 501907-405, 502061-401, 502147-401, and502147-403.1987-17-06 (ACTIVE) ADReason for this StatusAUTO ASSIGNED

1987-20-05 AD 00 MANDATORY A/C PACIFIC LAP BELT ASSY P/N 1107177 Not ApplicableCompliance:AD § (a) is Not applicable due to; NAS does not install PN:1107177-XXX seat belts.1987-20-05 (ACTIVE) ADReason for this StatusAUTO ASSIGNED





23.Oct.2014Page 11/429

Document-Number Type Rev Compliance A|C Subject Status1987-24-11 AD 00 MANDATORY COMP *AD* INSTALLATION OF AUGMENTATION CONTAINMENT RING Not Applicable

Applies to Garrett Model GTCP 85 series Auxiliary Power Unitsequipped with one-piece cast turbine wheels, Part Nos. 968095-X,3604604-X, 3606982-1, and 3842072-1.1987-24-1185-49-568985-49-570085-49-570085-49-570085-49-5700

ADSBSBSBSBSB

000000010203

Perform BEFORE 13.Jul.19891987-24-11/AD Rev.00 *AD* INSTALLATION OF AUGMENTATION CONTAINMENT RING Not Applicable> 85-49-5700/SB* Rev.03 INCORP. OF HASTELLOY "S" TURBINE WHEEL SHROUD, PN 3611904-1 Not Applicable



> 85-49A7189/SB* Rev.02 TURBINE WHEEL SHROUD CONT. AUGMENTATION RING - INCORP. OF Not Applicable by Serial NumberAffected Rotables (Part No/Serial No/Position) Status380428-10-1 / P-60280C Pos=APU (KKM) Not Applicable

1987-26-03 AD 00 MANDATORY A/C *AD* MINIMIZE POSSIBILITY OF MISLEADING LOCALIZER DEVIATION Not ApplicableMod appl.: LN# 993-14271987-26-03 (ACTIVE)737-34A1208-R1 (ACTIVE)

ADSB

Perform within an unlimited threshold.1987-26-03/AD Rev.00 *AD* MINIMIZE POSSIBILITY OF MISLEADING LOCALIZER DEVIATION Not Applicable> 737-34A1208/SB* Rev.02 LOCALIZER ANTENNA - CABLE REPLACEMENT AND ATTENUATOR INSTALLATION Not Applicable by Serial Number

This Document SUPERSEDES 737-34A1208/SB Rev.01





23.Oct.2014Page 12/429

Document-Number Type Rev Compliance A|C Subject Status1988-01-06 AD 01 MANDATORY A/C *AD* FUEL - FUEL BOOST PUMP BYPASS VALVE PERIODOC TEST/REPLT Superseded (Not Applicable)

1990-15-17 (ACTIVE)737-28A1072-R0 (REF)737-28A1072-R1 (REF)737-28A1072-R2 (REF)737-28A1072-R3 (REF)737-28A1072-R4 (REF)737-28A1072-R5 (ACTIVE)PRODUCTION LINE PRR34394

ADSBSBSBSBSBSBPRR

This Document has been SUPERSEDED BY 1990-15-17/AD Rev.00Perform BEFORE 27.Aug.1991

1988-01-06/AD Rev.01 *AD* FUEL - FUEL BOOST PUMP BYPASS VALVE PERIODOC TEST/REPLT Not ApplicableThis Document has been SUPERSEDED BY 1990-15-17/AD Rev.00

> 737-28A1072/SB* Rev.05 *AD* FUEL - FUEL BOOST PUMP BYPASS VALVE PERIODOC TEST/REPLT Not Applicable by Serial Number

1988-01-09 AD 00 MANDATORY A/C *AD* PREVENT LOSS OF THE PRIMARY ELEC. FLIGHT INSTRUMENT SYS Not ApplicableMod appl.: LN# 1125-13701988-01-09 (ACTIVE)737-34-1220-RO (ACTIVE)PRODUCTION LINE PRR34359

ADSBPRR





23.Oct.2014Page 13/429

Document-Number Type Rev Compliance A|C Subject Status1988-03-03 AD 00 MANDATORY A/C *AD* FUSELAGE - FWD SERVICE DOORWAY AFT FRAME INSP. & REPAIR Superseded (Superseded)

1998-22-10 (ACTIVE)737-53-1108-R0 (REF)737-53-1108-R1 (REF)737-53-1108-R2 (REF)737-53-1108-R3 (REF)737-53-1108-R4 (REF)737-53-1108-R5 (ACTIVE)PRODUCTION PRR34320R

ADSBSBSBSBSBSBPRR


1988-07-07 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 1991-24-04 Superseded (Not Applicable)103-25-19-R8 (REF)1988-07-07 (SUPERSEDED)1991-24-04 (SUPERSEDED)1996-18-04 (ACTIVE)737-25A1221 (REF)737-25A1221-R1 (ACTIVE)

SBADADADSBSB

This Document has been SUPERSEDED BY 1991-24-04/AD Rev.00This Document has been SUPERSEDED BY 1996-18-04/AD Rev.00Reason for this StatusSUPERSEDED BY AD 1991-24-04





23.Oct.2014Page 14/429

Document-Number Type Rev Compliance A|C Subject Status1988-11-01 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 1991-20-03 Superseded (Not Applicable)

1988-11-01 (SUPERSEDED)1991-20-03 (SUPERSEDED)1992-24-05 (ACTIVE)737-71A1208-R2 (ACTIVE)

ADADADSB

This Document has been SUPERSEDED BY 1991-20-03/AD Rev.00This Document has been SUPERSEDED BY 1992-24-05/AD Rev.00Reason for this StatusSUPERSEDED BY AD 1991-20-03

1988-11-08 AD 00 MANDATORY A/C BRUCE INDUSTRIES, INC.: APPLIES TO ALL BALLASTS, PN 05241-1 Not ApplicableCompliance:AD § (a) is Not applicable due to; NAS has NO aircraft modified inaccordance with Supplemental Type Certificate (STC) Numbers SA1081NW,SA1315NM, SA1952NM, SA3144NM, and SA4042WE; and Civil AviationAuthority Airworthiness Approval Note No. 17027, Issue 2.1988-11-08 (ACTIVE)A9000203-33-20-01

ADSB

0000

Reason for this StatusAUTO ASSIGNED

1988-13-51 AD 01 MANDATORY A/C *AD* TO PREVENT ENGINE FLAMEOUT DURING AIRPLANE DESCENT Superseded (Superseded)1993-05-05 (ACTIVE)737-77-1031-R1 (ACTIVE)PRODUCTION PRR34633-10

ADSBPRR






23.Oct.2014Page 15/429

Document-Number Type Rev Compliance A|C Subject Status1988-14-07 AD 00 MANDATORY A/C *AD* NON-MODULAR LAVATORIES - SHROUDS Not Applicable

Mod appl.: LN# 1-1425. NA for NAS per LN#.1988-14-07 (ACTIVE) ADReason for this StatusCOMPLIANCE: N/A BY LINE NUMBER

1988-19-04 AD 00 MANDATORY A/C *AD* CABIN PRESSURE SAFETY RELIEF VALVES Not ApplicableNot Applicable due to All NAS AC certified to 35000 feet max, ref PRR34407.1989-19-04 (ACTIVE)737-21-1096 (REF)PRR34407

ADSBPRR

000100

Reason for this StatusAIRCRAFT IS NOT APPLICABLE DUE TO PRR34407.

1988-21-03 AD 00 MANDATORY A/C *AD* PREVENT FAILURE OF THE FUEL CROSSFEED VALVE Superseded (Not Applicable)NAS does not operate B737-300 on ETOPS routes.1988-21-03-R1 (ACTIVE) ADThis Document has been SUPERSEDED BY 1988-21-03/AD Rev.01

1988-21-03 AD 01 MANDATORY A/C *AD* PREVENT FAILURE OF THE FUEL CROSSFEED VALVE Not ApplicableNAS does not operate B737-300 on ETOPS routes.1988-21-03-R1 (ACTIVE) ADThis Document SUPERSEDES 1988-21-03/AD Rev.00Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 16/429

Document-Number Type Rev Compliance A|C Subject Status1988-22-09 AD 00 MANDATORY A/C TAKEOFF WARNING CONFIGURATION CHECK Taskcard Controlled

Compliance:737-800:AD § (a) AD IS NOT APPLICABLE FOR BOEING 737-700/800/900PER BOEINGLETTER B-T113-98-0589

737-300:AD § (a) is complied with through MPD Task 31-026-02-01.31-026-02-01 (737-300)93-103S-83BOEING LETTER B-T113-98-0589

TAAMOCBM

000000

Carried out on the following TaskcardsTaskcard: 31-026-02-01 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks14.11.2014 73'519/H 198:01/H Interval:200/HPerf Dim1 (D) Perf Dim2 Perf Dim312.10.2014 73319:36/H 44494/CReason for this StatusAUTO ASSIGNED

1988-25-01 AD 00 MANDATORY COMP MODEL KDM 7000B DISTANCE MEASURING EQUIPMENT (DME) Not Applicable by Serial NumberCompliance:AD § (a) is Not Applicable, affected PN not installed on NAS aircraft.1988-25-01 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 17/429

Document-Number Type Rev Compliance A|C Subject Status1989-02-05 AD 00 MANDATORY A/C BF GOODRICH (SARGENT IND., PICO DIV.), APPL. 7 MAN-LIFE P/N 100102-( ). Not Applicable

Compliance:AD § (a) is Not applicable due to; NAS does not install Life Rafts onthe aircraft.1989-02-05 (ACTIVE) ADReason for this StatusAUTO ASSIGNED

1989-02-10 AD 01 MANDATORY COMP FMZ-800 FLIGHT MANAGEMENT SYSTEM (FMS) NAVIGATION COMPU Not Applicable by Serial NumberCompliance:AD § (a) and (b) is Not Applicable, affected PN not installed on NASaircraft.1989-02-10 (ACTIVE) ADThis Document SUPERSEDES 1989-02-10/AD Rev.00Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

1989-02-10 AD 00 MANDATORY COMP FMZ-800 FLIGHT MANAGEMENT SYSTEM (FMS) NAVIGATION COMPU Superseded (Not Applicable bySerial Number)

Compliance:AD § (a) and (b) is Not Applicable, affected PN not installed on NASaircraft.1989-02-10 (ACTIVE) ADThis Document has been SUPERSEDED BY 1989-02-10/AD Rev.01Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 18/429

Document-Number Type Rev Compliance A|C Subject Status1989-03-01 AD 00 MANDATORY A/C GOODYEAR 2X8.8R16, 10PR, P/N 328Q08G2 RADIAL TIRES Superseded (Superseded)

Compliance:AD § (a), (b) is Not applicable due to; PN 328Q08G2 wheels can not beinstalled on B737.1989-03-01-R1 (ACTIVE) ADThis Document has been SUPERSEDED BY 1989-03-01/AD Rev.01

1989-03-01 AD 01 MANDATORY A/C GOODYEAR 2X8.8R16, 10PR, P/N 328Q08G2 RADIAL TIRES Not ApplicableCompliance:AD § (a), (b) is Not applicable due to; PN 328Q08G2 wheels can not beinstalled on B737.1989-03-01-R1 (ACTIVE) ADThis Document SUPERSEDES 1989-03-01/AD Rev.00Reason for this StatusAUTO ASSIGNED

1989-03-51 AD 00 MANDATORY A/C *AD* DETECT INCORRECTLY INSTALLED FIRE SYST. PLUMBING/WIRING Ex FactoryComplied with at build. Refer to AD list supplied by Boeing at build.T89-03-51 (SUPERSEDED) AD 00Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 19/429

Document-Number Type Rev Compliance A|C Subject Status1989-04-03 AD 00 MANDATORY A/C *AD* DOORS - CTRL CABIN DOOR BLOWOUT PANELS,INSP. OF SEALANT Not Applicable

Mod appl.: LN# 1-15871989-04-03 (ACTIVE)737-52A1105-R0 (REF)737-52A1105-R1 (REF)737-52A1105-R2 (ACTIVE)SBB 737-52A1105(MOD-TASK)

ADSBSBSBTA

1989-04-03/AD Rev.00 *AD* DOORS - CTRL CABIN DOOR BLOWOUT PANELS,INSP. OF SEALANT Not Applicable> 737-52A1105/SB* Rev.02 *AD* DOORS - CTRL CABIN DOOR BLOWOUT PANELS,INSP. OF SEALANT Not Applicable by Serial Number

1989-06-01 AD 00 MANDATORY A/C SWITLIK PARACHUTE LIFE PRESERVER INFLATORS Not ApplicableCompliance:AD § (a) is Not applicable due to; affected PN not installed on NASAircraft.1989-06-01 (ACTIVE) ADReason for this StatusAUTO ASSIGNED

1989-07-13 AD 00 MANDATORY A/C *AD* GENERATOR CONTROL UNIT FILTER MODULE REPLACEMENT Not ApplicableModification incorperated in production.1989-07-13 (ACTIVE)87-101 WESTINGHOUSE

ADSB





23.Oct.2014Page 20/429

Document-Number Type Rev Compliance A|C Subject Status1989-08-11 AD 00 MANDATORY A/C ONE-TIME INSPECTION OF THE APU EXHAUST FLANGE AND THE EXHAUST

MUFFLER HEAT SHIELD SKINSuperseded (Not Applicable)

AD 89-08-11, superseded by AD 92-03-07.1989-08-111990-05-021992-03-07737-SL-49-014

ADADADSL

00000002

This Document has been SUPERSEDED BY 1990-05-02/AD Rev.00This Document has been SUPERSEDED BY 1992-03-07/AD Rev.00This Document has been SUPERSEDED BY 1992-07-10/AD Rev.00

1989-08-12 AD 01 MANDATORY A/C *AD* ENGINE FIRE/OVERHEAT DETECTION SYSTEM-WARNING SYS.TEST Not ApplicablePRODUCTION PRR34741 PRRThis Document SUPERSEDES 1989-08-12/AD Rev.00

1989-08-12/AD Rev.01 *AD* ENGINE FIRE/OVERHEAT DETECTION SYSTEM-WARNING SYS.TEST Not ApplicableThis Document SUPERSEDES 1989-08-12/AD Rev.00

> 737-26-1063/SB* Rev.00 *AD* ENG AND APU FIRE DETECTION ACCESSORY UNIT REPLACEMENT Not Applicable by Serial Number

1989-08-12 AD 00 MANDATORY A/C *AD* ENGINE FIRE/OVERHEAT DETECTION SYSTEM-WARNING SYS.TEST Superseded (Not Applicable bySerial Number)

1989-08-12 (SUPERSEDED)1989-08-12-R1 (ACTIVE)737-26-1063-R0 (ACTIVE)PRODUCTION PRR34741

ADADSBPRR






23.Oct.2014Page 21/429

Document-Number Type Rev Compliance A|C Subject Status1989-09-02 AD 00 MANDATORY A/C DAVIS AIRCRAFT PRODUCTS CO., INC.: APPLICABILITY/SAFETY Not Applicable

Compliance:AD § (a), (b) is Not Applicable, affected PN not installed on NASaircraft. NAS installs AMSAFE seat belts.1989-09-02 (ACTIVE) ADReason for this StatusAUTO ASSIGNED

1989-10-01 AD 00 MANDATORY A/C *AD* ENGINE FUEL FEED SYSTEM, CLEARANCE INSPECTION Not ApplicableMod appl.: LN# 1001-1435,1437,14961989-10-01 (ACTIVE)737-28A1077 (ACTIVE)

ADSB

1989-10-01/AD Rev.00 *AD* ENGINE FUEL FEED SYSTEM, CLEARANCE INSPECTION Not Applicable> 737-28A1077/SB* Rev.00 *AD* ENGINE FUEL FEED SYSTEM, CLEARANCE INSPECTION Not Applicable by Serial Number

1989-11-01 AD 00 MANDATORY COMP *AD* PN AND MOD STATUS OF IRU UNITS, DETERMINATION OF Not Applicable by Serial NumberNA due to effected part not installed.1989-11-01 (ACTIVE)AD 1989-11-01 (MAINT TASK)

ADTA

Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

1989-11-03 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 2004-06-18 Superseded (Not Applicable)1989-11-03 (SUPERSEDED2004-06-18 (ACTIVE)

ADAD






23.Oct.2014Page 22/429

Document-Number Type Rev Compliance A|C Subject Status1989-12-02 AD 00 MANDATORY A/C *AD* LAVATORIES - AFT LAVATORY PARTITION BEAM, SAW CUT INSP. Not Applicable

Mod appl.: LN# 91-13281989-12-02 (ACTIVE)737-25-1231 (REF)737-25-1231-R1 (ACTIVE)

ADSBSB

1989-12-02/AD Rev.00 *AD* LAVATORIES - AFT LAVATORY PARTITION BEAM, SAW CUT INSP. Not Applicable> 737-25-1231/SB* Rev.01 *AD* LAVATORIES - AFT LAVATORY PARTITION BEAM, SAW CUT INSP. Not Applicable by Serial Number

This Document SUPERSEDES 737-25-1231/SB Rev.00

1989-13-05 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 1991-21-13 Superseded (Not Applicable)1989-13-05 SUPERSEDED)1991-21-13 (ACTIVE)

ADAD


1989-13-06 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 1991-05-11 Superseded (Not Applicable)1989-13-05 SUPERSEDED)1991-05-11 (ACTIVE)

ADAD






23.Oct.2014Page 23/429

Document-Number Type Rev Compliance A|C Subject Status1989-13-51 AD 00 MANDATORY COMP TO PREVENT FAN BLADE FAILURE AND COMPLETE LOS OF PWR Superseded (Cancelled)

1989-13-511996-25-113-72-0543

ADADSB

000008

This Document has been SUPERSEDED BY 1996-25-11/AD Rev.00Perform BEFORE 29.Jan.1997

1989-13-51/AD Rev.00 TO PREVENT FAN BLADE FAILURE AND COMPLETE LOS OF PWR CancelledThis Document has been SUPERSEDED BY 1996-25-11/AD Rev.00

> 3-72-0473/SB* Rev.02 FAN DISK P/N 335-014-511-0 AND FAN BLADES P/N 9527M99P09, 9527M99P08 AND1285M39P01 - REPLACEMENT OF

Cancelled

This Document has been SUPERSEDED BY 1996-25-11/AD Rev.00Affected Rotables (Part No/Serial No/Position) Status

335-014-511-0 / BC610516 Pos=RH (KKM)Cancelled / Reason: Manually deassignedafter Document Cancelled or Superseded

335-014-511-0 / DC778241 Pos=LH (KKM)Cancelled / Reason: Manually deassignedafter Document Cancelled or Superseded

1989-14-11 AD 00 MANDATORY A/C AD* PREVENT POSSIBLE FAILURE OF FLIGHT ATTENDANT SEATS Not ApplicableNot applicable due to affected P/N not installed.1989-14-11-R2 (ACTIVE)737-SL-25-070TRANS AERO SB NO. 113

ADSLSB





23.Oct.2014Page 24/429

Document-Number Type Rev Compliance A|C Subject Status1989-15-08 AD 00 MANDATORY A/C *AD* SECOND OBSERVER S SEAT MOUNTING Not Applicable

1989-15-08 (ACTIVE)737-SL-25-41 (REF)737-SL-25-41-A (REF)737-SL-25-41-B (ACTIVE)SLB 737-SL-25-041 (MOD-TASK)

ADSLSLSLTA

1989-15-08/AD Rev.00 *AD* SECOND OBSERVER S SEAT MOUNTING Not Applicable> 737-SL-25-041/SL* Rev.NOTE *AD* SECOND OBSERVER S SEAT MOUNTING Not Applicable by Serial Number

1989-17-04 AD 00 MANDATORY COMP INLET GEARBOX - NO. 3 BEARING IMPROVEMENT PROGRAM Superseded (Superseded)Superceded by 1989-23-061989-23-063-72-0530

ADSB

0003

This Document has been SUPERSEDED BY 1989-23-06/AD Rev.01Affected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 725495 Pos=RH (KKM) SupersededCFM56-3B2 / 724473 Pos=LH (KKM) Superseded


1989-08-51 (SUPERSEDED)1990-14-04 (SUPERSEDED)1991-09-17 (ACTIVE)737-57A1202-R1 (ACTIVE

ADADADSB






23.Oct.2014Page 25/429

Document-Number Type Rev Compliance A|C Subject Status1989-20-06 AD 00 MANDATORY COMP SPERRY FMZ-800 FLIGHT MANAGEMENT SYSTEMS (FMS), MODEL Not Applicable by Serial Number

Compliance:AD § (a) is Not applicable due to the system is not installed on NASB737.1989-20-06 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 26/429

Document-Number Type Rev Compliance A|C Subject Status1989-23-06 AD 01 MANDATORY COMP INLET GEARBOX - NO. 3 BEARING IMPROVEMENT PROGRAM Not Applicable





23.Oct.2014Page 27/429

Document-Number Type Rev Compliance A|C Subject StatusCategory 1Engines equipped with No.3 bearing, PIN 9732MI0P12 (havingserial numbers that begin with FAF D or FAF E only),PIN 9732MI0P18, or PIN 1362M76P02, must have the bearing removed atnext 1GB exposure, or December 31, 1997, whichever occurs first.

Category 21 Engines equipped with No. 3 bearing, PIN 9732MIOP12 (havingserial numbers that begin with FAF Dor FAF E only), shouldhave the MCD inspected at intervals not to exceed 50 EngineFlight Hours (EFH), up to 6,000 hours time in service ofthe bearing. If the bearing has more than 6,000 hours timein service the MCD may be inspected at normal intervals.

2 Engines equipped with No.3 bearing, PIN 9732MIOP18 orPIN 1362M76P02, should have the MCD inspected at intervalsnot to exceed 50 EFH. This inspection interval of 50 EFHshould continue until the bearing is replaced.

3 Engines equipped with No.3 bearing, PIN 9732MI0P12(beginning with serial numbers other than FAF D or FAF E),PIN 9732MI0PI0, or PIN 9732MI0P17, should have the MCDinspected at intervals not to exceed 75 EFH up to 6,000hours time in service of the bearings. If the bearing hasmore than 6,000 hours time in service the MCD may beinspected at normal intervals.

Category 3Engines equipped with No.3 bearing, PIN 9732M10Pl2 (beginningwith serial numbers other than FAF D or FAF E), PIN 9732M10P10,or PIN 9732M10P17, should have the bearing removed at next





23.Oct.2014Page 28/429

Document-Number Type Rev Compliance A|C Subject Statusengine shop visit, but no later than next 1GB exposure.1989-23-063-72-0530

ADSB

0003

This Document SUPERSEDES 1989-17-04/AD Rev.00This Document SUPERSEDES 1989-23-06/AD Rev.00Perform BEFORE 28.Jan.1989

1989-23-06/AD Rev.01 INLET GEARBOX - NO. 3 BEARING IMPROVEMENT PROGRAM Not ApplicableThis Document SUPERSEDES 1989-17-04/AD Rev.00This Document SUPERSEDES 1989-23-06/AD Rev.00

> 3-72-0530/SB* Rev.03 INLET GEARBOX - NO. 3 BEARING IMPROVEMENT PROGRAM Not ApplicableThis Document SUPERSEDES 3-72-0445/SB Rev.03Affected Rotables (Part No/Serial No/Position) Status

CFM56-3B2 / 724473 Pos=LH (KKM)Not Applicable / Reason: NA DUE TO PNSHOP VISIT 05

CFM56-3B2 / 725495 Pos=RH (KKM)Not Applicable / Reason: DEL DOCMSN:224676

1989-23-06 AD 00 MANDATORY COMP INLET GEARBOX - NO. 3 BEARING IMPROVEMENT PROGRAM Superseded (Superseded)1989-23-063-72-0530

ADSB

0003

This Document has been SUPERSEDED BY 1989-23-06/AD Rev.01Affected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 725495 Pos=RH (KKM) SupersededCFM56-3B2 / 724473 Pos=LH (KKM) Superseded





23.Oct.2014Page 29/429

Document-Number Type Rev Compliance A|C Subject Status1989-23-10 AD 00 MANDATORY A/C *AD* AOM REV CONTINUED SAFE FLT/LD DUE TO ENG ICE BUILDUP Closed 06.Mar.1990

All AFM revisions performed by previous operator.1989-23-10 (ACTIVE)AD 1989-23-10 (MAINT TASK)

ADTA

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

06.Mar.1990 00:00/H 0/C

Was due at: 14.Dec.1989 PerfRev.:'00' /Reason: Incorporated by Boeing atmanufacture Incorporated by Boeing atmanufacture

Reason for this StatusIncorporated by Boeing at manufacture

1989-23-52 AD 00 MANDATORY A/C *AD* AFM REVISION Not Applicable by Serial Number

1989-25-02 AD 00 MANDATORY A/C *AD* ENGINE INDICATING - POWER - WIRING MODIFICATION Not ApplicableMod appl.: LN# 1001-17621989-25-02 (ACTIVE)737-77A1026-R0 (REF)737-77A1026-R1 (REF)737-77A1026-R2 (REF)737-77A1026-R3 (REF)737-77A1026-R4 (ACTIVE)

ADSBSBSBSBSB

1989-25-02/AD Rev.00 *AD* ENGINE INDICATING - POWER - WIRING MODIFICATION Not Applicable> 737-77A1026/SB* Rev.04 *AD* ENGINE INDICATING - POWER - WIRING MODIFICATION Not Applicable by Serial Number





23.Oct.2014Page 30/429

Document-Number Type Rev Compliance A|C Subject Status1989-26-06 AD 01 MANDATORY A/C O2 MASK LANYARD RINGS AND O2 GENERATORS, REPLACEMENT OF Not Applicable

Mod appl.: LN# 1121-1482 (with exceptions)737-35A1029 SB 03This Document SUPERSEDES 1989-26-06/AD Rev.00

1989-26-06/AD Rev.01 O2 MASK LANYARD RINGS AND O2 GENERATORS, REPLACEMENT OF Not ApplicableThis Document SUPERSEDES 1989-26-06/AD Rev.00

> 737-35A1029/SB* Rev.03 O2 MASK LANYARD RINGS AND O2 GENERATORS, REPLACEMENT OF Not Applicable by Serial NumberThis Document SUPERSEDES 737-35A1029/SB Rev.00This Document SUPERSEDES 737-35A1029/SB Rev.01This Document SUPERSEDES 737-35A1029/SB Rev.02

1989-26-06 AD 00 MANDATORY A/C O2 MASK LANYARD RINGS AND O2 GENERATORS, REPLACEMENT OF Superseded (Not Applicable bySerial Number)


1990-01-03 AD 00 MANDATORY COMP HONEYWELL AH-600 ATTITUDE AND HEADING REFERENCE SYSTEM Not Applicable by Serial NumberCompliance:AD § (a), (b) is Not Applicable, affected PN not installed on NASAircraft.1990-01-037003360-34-32

ADSB

0000






23.Oct.2014Page 31/429


AD 90-05-02 superseded by AD 92-03-071989-08-111990-05-021992-03-07737-SL-49-014

ADADADSL

00000002


1990-05-09 AD 00 MANDATORY COMP TRACOR AEROSPACE, INCORPORATED TA-7800 OMEGA/VLF NAV Not Applicable by Serial NumberCompliance:AD § (a), (b) is Not Applicable, affected PN not installed on NASAircraft.138000-00-011990-05-09

SBAD

0000


1990-06-04 AD 00 MANDATORY A/C AD* INSP. OF AIRPLANES EQUIPPED WITH WALTER KIDDE FIRE DETEC Not Applicable1990-06-04 (ACTIVE)M-72-72-90-0735 (REF)

ADBM

1990-06-13 AD 00 MANDATORY COMP HONEYWELL VERTICAL GYRO, P/N 7000622-901 Not Applicable by Serial NumberCompliance:AD § (a) is Not Applicable, Effected PN not installed on NAS AC.1990-06-13 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 32/429


1990-07-02 (SUPERSEDED)1992-07-09 (ACTIVE)

ADAD


1990-09-05 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 1990-23-12 Superseded (Not Applicable)1990-09-05 (SUPERSEDED)1990-23-12 (ACTIVE)

ADAD


1990-09-08 AD 00 MANDATORY COMP *AD* IPECO TSO-C39A CREW SEATS Not Applicable by Serial Number1990-09-08 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

1990-09-11 AD 00 MANDATORY A/C AIRCRUISERS FWD DOOR EVACUATION SLIDE,MOD OF Not ApplicableNo affected rotable installed.103-25-17 (AIR CRUISER SB)1990-09-11

SBAD

0000


1990-10-51 AD 00 MANDATORY A/C *AD* CONTROL WHEELS - INSPECT FOR MISSING COTTER PINS Closed 18.May.19901990-10-5127-11-00

ADAMM


18.May.1990PerfRev.:'NOTE' / Reason: DELIVERYDOC.

Reason for this StatusDELIVERY DOC.





23.Oct.2014Page 33/429

Document-Number Type Rev Compliance A|C Subject Status1990-12-11 AD 00 MANDATORY A/C *AD* ESCAPE SLIDE RELEASE LATCH CABLE INSPECTION Superseded (Superseded)

1990-12-11 R1 XB (ACTIVE)37-B25-61-35-A (INSP-TASK)

ADTA


1990-12-11 AD 01 MANDATORY A/C ESCAPE SLIDE RELEASE LATCH CABLE INSPECTION Taskcard ControlledReptitive inspection covered by B737 MPD task 25-061-36-01.1990-12-11 R1 XB (ACTIVE)37-B25-61-35-A (INSP-TASK)

ADTA

Carried out on the following TaskcardsTaskcard: 25-061-36-01 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks28.04.2015 75'021/H 1700:15/H Interval:2000/HPerf Dim1 (D) Perf Dim2 Perf Dim322.08.2014 73021:50/H 44271/CThis Document SUPERSEDES 1990-12-11/AD Rev.00Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 34/429

Document-Number Type Rev Compliance A|C Subject Status1990-14-02 AD 00 MANDATORY A/C *AD* RUDDER TRIM CONTROL KNOB, REPLACEMENT OF Closed 19.Apr.1991

This document is applicable to LN# 1001-1865. The following LN# areNot Applicable per PRR33890-71.1990-14-02 (ACTIVE)AD 1990-14-02 (MOD TASK)PRODUCTION LINE PRR 33890-72

ADTAPRR

Perform within an unlimited threshold.1990-14-02/AD Rev.00 *AD* RUDDER TRIM CONTROL KNOB, REPLACEMENT OF Closed 19.Apr.1991> 737-27-1165/SB* Rev.01 RUDDER TRIM KNOB & GUARD REPLACEMENT Closed 19.Apr.1991

This Document SUPERSEDES 737-27-1165/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

19.Apr.1991PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:

Reason for this StatusDELIVERY DOC WO:


1989-18-51 (SUPERSEDED)1990-14-04 (SUPERSEDED)1991-09-17 (ACTIVE)737-57A1202-R0 (REF)737-57A1202-R1 (ACTIVE)

ADADADSBSB






23.Oct.2014Page 35/429

Document-Number Type Rev Compliance A|C Subject Status1990-14-06 AD 00 MANDATORY A/C AEROSPACE LIGHTING CORPORATION POWER UNITS AND POWER Superseded (Superseded)

Compliance:AD § (a), (b) is Not applicable due to system not installed. NAS usesphotoluminescent emergency lighting.1990-14-06 (SUPERSEDED)1995-22-01 (ACTIVE)

ADAD


1990-15-03 AD 00 MANDATORY A/C *AD* FUEL TUBE ASSEMBLY CHAFING AGAINST WING/STRUT STRUCTURE Not ApplicableThe AD is applicable for LN: 1001-17171990-15-03 (ACTIVE)737-28-1055-R1 (REF)737-28-1084 (ACTIVE)

ADSBSB

1990-15-03/AD Rev.00 *AD* FUEL TUBE ASSEMBLY CHAFING AGAINST WING/STRUT STRUCTURE Not Applicable> 737-28-1084/SB* Rev.03 *AD* FUEL FEED TUBE ASSEMBLY MOD. Not Applicable by Serial Number

1990-15-14 AD 00 MANDATORY A/C *AD* FIRE PROTECTION - ENGINE FIRE DETECTOR REPLACEMENT Not ApplicableMod appl is LN# 1037 - 1717.The following LN# are Not Applicable per PRR33890-48.1990-15-14 (ACTIVE)737-26-1055-R0 (REF)737-26-1055-R1 (REF)737-26-1055-R2 (ACTIVE)PRODUCTION LINE PRR 33890-48

ADSBSBSBPRR

Perform within an unlimited threshold.1990-15-14/AD Rev.00 *AD* FIRE PROTECTION - ENGINE FIRE DETECTOR REPLACEMENT Not Applicable> 737-26-1055/SB* Rev.02 *AD* FIRE PROTECTION - ENGINE FIRE DETECTOR REPLACEMENT Not Applicable by Serial Number






23.Oct.2014Page 36/429

Document-Number Type Rev Compliance A|C Subject Status1990-15-17 AD 00 MANDATORY A/C *AD* FUEL - FUEL BOOST PUMP BYPASS VALVE PERIODOC TEST/REPLT Not Applicable

This mod is applicable for LN# 1001-1523. The following LN# are Notapplicable Per PRR34394.1990-15-17 (ACTIVE)737-28A1072-R0 (REF)737-28A1072-R1 (REF)737-28A1072-R2 (REF)737-28A1072-R3 (REF)737-28A1072-R4 (REF)737-28A1072-R5 (ACTIVE)PRODUCTION LINE PRR34394

ADSBSBSBSBSBSBPRR

This Document SUPERSEDES 1988-01-06/AD Rev.011990-15-17/AD Rev.00 *AD* FUEL - FUEL BOOST PUMP BYPASS VALVE PERIODOC TEST/REPLT Not Applicable

This Document SUPERSEDES 1988-01-06/AD Rev.01> 737-28A1072/SB* Rev.05 *AD* FUEL - FUEL BOOST PUMP BYPASS VALVE PERIODOC TEST/REPLT Not Applicable by Serial Number

1990-17-20 AD 00 MANDATORY A/C *AD* WINGS - FLAP TRACK SUPPORT FITTING ATTACH BOLTS REPLCT. Not ApplicableMod appl.: LN# 1-3241990-17-20737-57A1079737-57A1079 R1737-57A1079 R2737-57A1079 R3737-57A1079 R4

ADSBSBSBSBSB

1990-17-20/AD Rev.00 *AD* WINGS - FLAP TRACK SUPPORT FITTING ATTACH BOLTS REPLCT. Not Applicable> 737-57A1079/SB* Rev.04 *AD* WINGS - FLAP TRACK SUPPORT FITTING ATTACH BOLTS REPLCT. Not Applicable by Serial Number






23.Oct.2014Page 37/429

Document-Number Type Rev Compliance A|C Subject Status1990-20-13 AD 00 MANDATORY COMP FAN MODULE ASSY, MODIFICATION OF Closed 17.Jan.2005

Status applies to EASA AD 1990-031.1990-20-133-72-0494

ADSB

0004

Perform BEFORE 14.Dec.19901990-20-13/AD Rev.00 FAN MODULE ASSY, MODIFICATION OF Closed 17.Jan.2005> 3-72-0494/SB* Rev.04 *AD* FAN MODULE ASSY, MODIFICATION OF Closed 17.Jan.2005


CFM56-3B2 / 724473 Pos=LH (KKM)

Closed / Reason: POST SB 72-543 SHOPVISIT 05 39729 / LastPerformed:17.Jan.2005 42076:00/H 21463/CRefDocument: Rev.NOTE

CFM56-3B2 / 725495 Pos=RH (KKM)

Closed / Reason: FOUND EMBODIEDSHOP VISIT 03 39730 / LastPerformed:11.Mar.2003 RefDocument:Rev.NOTE

1990-20-22 AD 00 MANDATORY A/C *AD* WINGS L.E. - LDG. LIGHT CAVITY VAPOR BARRIER SEAL INSTL Not ApplicableMod appl.: LN# 1-16421990-20-22 (ACTIVE)737-57A1197 (ACTIVE)

ADSB

1990-20-22/AD Rev.00 *AD* WINGS L.E. - LDG. LIGHT CAVITY VAPOR BARRIER SEAL INSTL Not Applicable> 737-57A1197/SB* Rev.00 *AD* WINGS L.E. - LDG. LIGHT CAVITY VAPOR BARRIER SEAL INSTL Not Applicable by Serial Number





23.Oct.2014Page 38/429

Document-Number Type Rev Compliance A|C Subject Status1990-23-12 AD 00 MANDATORY A/C *AD* APU / EXHAUST GAS TEMPERATURE GAGE-WIRE MODIFICATION Not Applicable

This mod is applicable for LN# 1001-1823. The following LN# are Notapplicable Per PRR34787.1990-09-05 (SUPERSEDED)1990-23-12 (ACTIVE)737-49-1071-R0 (REF)737-49-1071-R1 (ACTIVE)PRR 34787 (PRODUCTION)

ADADSBSBPRR

This Document SUPERSEDES 1990-09-05/AD Rev.001990-23-12/AD Rev.00 *AD* APU / EXHAUST GAS TEMPERATURE GAGE-WIRE MODIFICATION Not Applicable

This Document SUPERSEDES 1990-09-05/AD Rev.00> 737-49-1071/SB* Rev.01 *AD* APU / EXHAUST GAS TEMPERATURE GAGE-WIRE MODIFICATION Not Applicable by Serial Number

1990-24-04 AD 00 MANDATORY A/C *AD* OUTBOARD FLAP SUPPORT FITTING ATTACH BOLTS - INSP./REPL Not ApplicableThis mod is applicable for LN# 1001-1762. The following LN# are Notapplicable Per MRR3579-644.1990-24-04 (ACTIVE)737-57A1208 (ACTIVE)PRODUCTION MRR3579-644

ADSBPRR SB

Perform BEFORE 5000/H1990-24-04/AD Rev.00 *AD* OUTBOARD FLAP SUPPORT FITTING ATTACH BOLTS - INSP./REPL Not Applicable> 737-57A1208/SB* Rev.00 *AD* OUTBOARD FLAP SUPPORT FITTING ATTACH BOLTS - INSP./REPL Not Applicable by Serial Number





23.Oct.2014Page 39/429

Document-Number Type Rev Compliance A|C Subject Status1990-25-01 AD 00 MANDATORY A/C AGING AIRPLANE CORROSION PREVENTION AND CONTROL PROGRAM Closed 16.Nov.2006

For 737-800 FAA letter 120S-09-687: Maintenance Program based onMSG-3 REV2 or higher (MPD) is AMOC to AD 90-25-01. NAS AMP is basedon Boeing MPD D626A001.

For 737-300 FAA letter 120S-06-633: Structural Maintenance ProgramMPD section 10 is AMOC to AD 90-25-01. NAS AMP is based in BoeingMPD.120S-09-687 (ACTIVE)1990-25-01 (ACTIVE)CORROSION CONTROL D6-38528RA

AMOC

AD

DOCR


16.Nov.2006Reason: COMPLIED WITH IAW MPDREF AMOC 120S-06-633

Reason for this StatusCOMPLIED WITH IAW MPD REF AMOC 120S-06-633

1990-25-12 AD 00 MANDATORY A/C *AD* OXYGEN SYSTEMS - CREW OXYGEN SYSTEM TUBE INSP/REPLACEM Not ApplicableMod appl.: LN# 1066-17591990-25-12 (ACTIVE)737-35-1033-R0 (ACTIVE)

ADSB

1990-25-12/AD Rev.00 *AD* OXYGEN SYSTEMS - CREW OXYGEN SYSTEM TUBE INSP/REPLACEM Not Applicable> 737-35-1033/SB* Rev.00 OXYGEN SYSTEMS/CREW OXYGEN SYSTEM TUBE INSP/REPLACEMENT Not Applicable by Serial Number





23.Oct.2014Page 40/429

Document-Number Type Rev Compliance A|C Subject Status1990-25-14 AD 00 MANDATORY A/C *AD* INSPECTION & REWORK OF FORWAD LOWERED CEILING PANEL Closed 03.May.1994

Mod appl.: LN# 1001-2089 The following LN# are Not Applicable refPRR34963.1990-25-14 (ACTIVE)737-25-1274 R4 (ACTIVE)737-25-1274-R0 (REF)737-25-1274-R1 (REF)737-25-1274-R2 (REF)737-25-1274-R3 (REF)

ADSBSBSBSBSB

Perform within an unlimited threshold.1990-25-14/AD Rev.00 *AD* INSPECTION & REWORK OF FORWAD LOWERED CEILING PANEL Closed 03.May.1994> 737-25-1274/SB* Rev.04 *AD* INSPECTION & REWORK OF FORWAD LOWERED CEILING PANEL Closed 03.May.1994




1990-26-05 AD 00 MANDATORY A/C *AD* TRANSAERO DOUBLE CA SEATPAN, INSP OF Closed 16.Jul.19911990-26-05 ADPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

16.Jul.1991 00:00/H 0/C

AD

1990-26-05

(2).pdf

Was due at: 16.Jan.1991 PerfRev.:'00' /Reason: Performed by previous operator16.07.91 ref DFP Performed by previousoperator 16.07.91 ref DFP

Reason for this StatusPerformed by previous operator 16.07.91 ref DFP





23.Oct.2014Page 41/429

Document-Number Type Rev Compliance A|C Subject Status1991-02-10 AD 00 MANDATORY COMP FAN STAGE 1 VANE ASSY & SPLITTER FAIRING, REPL. OF Closed 27.Jun.2012

CFM International (CFMI) CFM56-3, -3B, -3C series turbofan engines.CFM SB 3-72-0450 will be introduced on the following engines:724295, 724297, 724298, 724315 thru 724319, 724321 and up.725305 thru 725310, 725312, 725313, 725335 and up.Status apply for EASA AD 1991-030.1991-02-103-72-0450

ADSB

0004

1991-02-10/AD Rev.00 FAN STAGE 1 VANE ASSY & SPLITTER FAIRING, REPL. OF Closed 27.Jun.2012> 3-72-0450/SB* Rev.04 FAN STAGE 1 VANE ASSY & SPLITTER FAIRING, REPL. OF Closed 27.Jun.2012


CFM56-3B2 / 725495 Pos=RH (KKM)

Closed / Reason: PE: PREVIOUSLYEMBODIED / Last Performed:27.Jun.201264007:00/H 38431/C RefDocument:MTURECORDED MOD STATUS WO51734400 Rev.04

CFM56-3B2 / 724473 Pos=LH (KKM) Not Applicable





23.Oct.2014Page 42/429

Document-Number Type Rev Compliance A|C Subject Status1991-030 AD B MANDATORY COMP FAN STAGE 1 VANE ASSY & SPLITTER FAIRING - REPL. OF Not Applicable

CFM International (CFMI) CFM56-3, -3B, -3C series turbofan engines.CFM SB 3-72-0450 will be introduced on the following engines:724295, 724297, 724298, 724315 thru 724319, 724321 and up.725305 thru 725310, 725312, 725313, 725335 and up.Status apply for EASA AD 1991-030.

1991-030/AD Rev.B FAN STAGE 1 VANE ASSY & SPLITTER FAIRING - REPL. OF Not Applicable> 3-72-0450/SB* Rev.04 FAN STAGE 1 VANE ASSY & SPLITTER FAIRING, REPL. OF Closed 27.Jun.2012


CFM56-3B2 / 725495 Pos=RH (KKM)

Closed / Reason: PE: PREVIOUSLYEMBODIED / Last Performed:27.Jun.201264007:00/H 38431/C RefDocument:MTURECORDED MOD STATUS WO51734400 Rev.04

CFM56-3B2 / 724473 Pos=LH (KKM) Not Applicable

1991-05-08 AD 00 MANDATORY A/C *AD* INSPECTION OF ENGINE CONTROL CABLE SYSTEM FOR CORROSION Not Applicable / Special Text: ThisAircraft is complied with at Build,ref Boeing AD list.

1991-05-08 (ACTIVE) AD





23.Oct.2014Page 43/429

Document-Number Type Rev Compliance A|C Subject Status1991-05-11 AD 00 MANDATORY A/C *AD* REDUCE RISK OF ENG THRUST LOSS DURING ETOPS, AFM REV Performed by prev. Operator

IMPLEMENTED IN MAINTENANCE SYSTEM PER BOEING DOC D6-38123RANAS does not operate any B737-300 under ETOPS rules.1989-13-06 (SUPERSEDED)1991-05-11 (ACTIVE)BOEING DOCUMENT D6-38123 RA

ADADDOCR

This Document SUPERSEDES 1989-13-06/AD Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks26.Mar.1991Reason for this StatusBOEING DOCUMENT D6-38123 RA

1991-05-16 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 1999-10-12 Superseded (Closed 08.Jul.2005)1991-05-16 (SUPERSEDED)1999-10-12 (ACTIVE)

ADAD

This Document has been SUPERSEDED BY 1999-10-12/AD Rev.00Perform within an unlimited threshold.

1991-05-16/AD Rev.00 *AD* SUPERSEDED BY AD 1999-10-12 Closed 08.Jul.2005This Document has been SUPERSEDED BY 1999-10-12/AD Rev.00

> 737-32A1224/SB* Rev.03 *AD* MLG TRUNNION PIN, ACTUATOR BEAM ARM, AND ACTUATOR BOLT Closed 08.Jul.2005Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

08.Jul.2005 27979/CPCW PER OHSR-TECHREPORT 2005

PerfRev.:'03'

1991-07-01 AD 00 MANDATORY A/C *AD* TO PREVENT BLANKING OF EITHER PILOT`S EFIS DISPLAY Not Applicable by Serial NumberEFIP-701E-34-03 (ACTIVE) SB 00





23.Oct.2014Page 44/429

Document-Number Type Rev Compliance A|C Subject Status1991-07-04 AD 00 RECOMMENDED A/C INSPECT WINDOW BELT DOUBLERTO PREVENT RAPID DECOMPRESSION OF THE

AIRPLANENot Applicable by Serial Number

Modification is applicable to LN# 1-519 and B737-100/-200.737-53-1078 SB 04

1991-07-14 AD 00 MANDATORY A/C *AD* EQUIPMENT FURNISHING - MAG. STBY COMPASS LINER, REPLACE Not Applicable1991-07-14-R0 (ACTIVE)737-25-1266-R0 (ACTIVE)

ADSB

1991-07-14/AD Rev.00 *AD* EQUIPMENT FURNISHING - MAG. STBY COMPASS LINER, REPLACE Not Applicable> 737-25-1266/SB* Rev.00 *AD* EQUIPMENT FURNISHING - MAG. STBY COMPASS LINER, REPLACE Not Applicable by Serial Number

1991-08-51 AD 00 MANDATORY A/C HONEYWELL FLIGHT MANAGEMENT SYSTEM (FMS) ONE MILLION WO Superseded (Superseded)This AD is rescinded by AD 2005-30-21.1991-08-51 (ACTIVE) ADThis Document has been SUPERSEDED BY 2005-20-31/AD Rev.00





23.Oct.2014Page 45/429

Document-Number Type Rev Compliance A|C Subject Status1991-09-05 AD 00 MANDATORY A/C *AD* COMMUNICATIONS - CREW CALL HORN CIRCUIT BREAKER INST. Closed 18.Sep.1991

This mod is applicable to LN# 1-1999. The following LN# are NotApplicab ref PRR34954.1991-09-05 (ACTIVE)737-23-1059-R0 (REF)737-23-1059-R1 (ACTIVE)PRODUCTION LINE PRR34954SBB 737-23-1059 (MOD-TASK)

ADSBSBPRRTA

Perform BEFORE 23.Nov.19911991-09-05/AD Rev.00 *AD* COMMUNICATIONS - CREW CALL HORN CIRCUIT BREAKER INST. Closed 18.Sep.1991> 737-23-1059/SB* Rev.01 *AD* COMMUNICATIONS - CREW CALL HORN CIRCUIT BREAKER INST. Closed 18.Sep.1991


18.Sep.1991PerfRev.:'NOTE' / Reason: DELIVERYDOC.






23.Oct.2014Page 46/429

Document-Number Type Rev Compliance A|C Subject Status1991-09-12 AD 00 MANDATORY A/C *AD* MODIFICATION OF ENGINE FIRE EXTINGUISHING SYSTEM WIRING Closed 27.Feb.1992

This document is applicable to LN# 1001-1889. THe following LN# areNot Applicable per PRR34774.1991-09-12 (ACTIVE)PRODUCTION LINE PRR34774SBB 737-26-1067-R1 (ACTIVE)

ADPRRSB

Perform BEFORE 28.May.19941991-09-12/AD Rev.00 *AD* MODIFICATION OF ENGINE FIRE EXTINGUISHING SYSTEM WIRING Closed 27.Feb.1992> 737-26-1067/SB* Rev.01 *AD* MODIFICATION OF ENGINE FIRE EXTINGUISHING SYSTEM WIRING Closed 27.Feb.1992


27.Feb.1992PerfRev.:'NOTE' / Reason: DELIVERYDOC

Reason for this StatusDELIVERY DOC

1991-09-17 AD 00 MANDATORY A/C *AD* SUPPORT FITTING ATTACH BOLT & NUT INSP./REPLACEMENT. Not Applicable1990-14-04 (SUPERSEDED)1991-09-17 (ACTIVE)737-57A1202-R0 (REF)737-57A1202-R1 (ACTIVE)SBB 737-57A1202 (MOD TASK)

ADADSBSBTA

This Document SUPERSEDES 1990-14-04/AD Rev.001991-09-17/AD Rev.00 *AD* SUPPORT FITTING ATTACH BOLT & NUT INSP./REPLACEMENT. Not Applicable

This Document SUPERSEDES 1990-14-04/AD Rev.00> 737-57A1202/SB* Rev.01 *AD* SUPPORT FITTING ATTACH BOLT & NUT INSP./REPLACEMENT. Not Applicable by Serial Number





23.Oct.2014Page 47/429

Document-Number Type Rev Compliance A|C Subject Status1991-10-01 AD 00 MANDATORY A/C TRAFFIC ALERT AND COLLISION AVOIDANCE (TCAS) II (OR 94) Not Applicable

Compliance:AD § (a), (b) and (c) are Not applicable due to the affected systemnot installed on NAS B737.1991-10-01 (ACTIVE) ADReason for this StatusAUTO ASSIGNED

1991-10-02 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 1993-07-15 Superseded (Not Applicable)1989-18-12-R1 (SUPERSEDED)1991-10-02 (SUPERSEDED)1993-07-15 (ACTIVE)

ADADAD


1991-10-05 AD 00 MANDATORY A/C O2 CORP. OXYGEN MASK PRESENTATION UNIT Not ApplicableCompliance:AD § (a), (b) and (c) are Not applicable due to affected PN notinstalled in NAS B737.1991-10-05 (ACTIVE) ADReason for this StatusAUTO ASSIGNED

1991-15-15 AD 00 MANDATORY COMP *AD* CREWMEMBER PROTECTIVE BREATHING EQUIPMENT MODEL 4566M37 Not Applicable by Line NumberNot applicable due to affected PN not installed on NAS B737.1991-15-15 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 48/429

Document-Number Type Rev Compliance A|C Subject Status1991-16-08 AD 00 MANDATORY A/C *AD* FUEL - AUX. FUEL TANK & SUPPORT STRUCTURE, INSP. OF Not Applicable

Not applicable due to no aux fuel tanks fitted.1991-16-08 (ACTIVE)737-28-1088 (REF)737-28A1034-R2 (ACTIVE)PRODUCTION PRR33063-R

ADSBSBPRR

1991-20-03 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 1992-24-05 Superseded (Not Applicable)1988-11-01 (SUPERSEDED)1991-20-03 (SUPERSEDED)1992-24-05 (ACTIVE)737-71A1208-R0 (REF)737-71A1208-R1 (REF)737-71A1208-R2 (ACTIVE)

ADADADSBSBSB

This Document SUPERSEDES 1988-11-01/AD Rev.00This Document has been SUPERSEDED BY 1992-24-05/AD Rev.00This Document has been SUPERSEDED BY 1992-25-04/AD Rev.00Reason for this StatusSUPERSEDED BY AD 1992-24-05





23.Oct.2014Page 49/429

Document-Number Type Rev Compliance A|C Subject Status1991-20-04 AD 00 MANDATORY A/C *AD* HORIZONTAL STAB. TRIM CONTROL SYSTEM-AUX. BRAKE REPLACE Closed 26.Feb.1992

1991-20-04 (ACTIVE)37-SBB-27-1161 (MOD-TASK)737-27-1161-R0 (REF)737-27-1161-R1 (REF)737-27-1161-R2 (ACTIVE

ADTASBSBSB

Perform within an unlimited threshold.1991-20-04/AD Rev.00 *AD* HORIZONTAL STAB. TRIM CONTROL SYSTEM-AUX. BRAKE REPLACE Closed 26.Feb.1992> 737-27-1161/SB* Rev.02 *AD* HORIZONTAL STAB. TRIM CONTROL SYSTEM-AUX. BRAKE REPLACE Closed 26.Feb.1992


26.Feb.1992PerfRev.:'NOTE' / Reason: PREVIOUSOPERATOR DOC.

Reason for this StatusPREVIOUS OPERATOR DOC.

1991-20-11 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 1993-17-02 Superseded (Not Applicable)1991-20-11 (SUPERSEDED)1993-17-02 (ACTIVE)737-SL-28-036 (REF)737-SL-28-042-A (ACTIVE)

ADADSLSL


1991-21-12 AD 00 MANDATORY COMP *AD* RADIO CONTROL PANEL REPLACEMENT Not Applicable by Serial NumberNAS controlls this AD as a component modification.Also refer to Boeing delivery doc R-6744-XX-XXX (AD status atdelivery)1991-21-12 ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 50/429

Document-Number Type Rev Compliance A|C Subject Status1991-21-13 AD 00 MANDATORY A/C *AD* ENG.CONT.SYSTEM-REPL. OF ENG. THROTTLE. CTRL. CABLES Closed 28.Feb.1992

1991-21-13 (ACTIVE)737-76-1023 (ACTIVE)SBB 737-76-1023 (MOD TASK)

ADSBTA

This Document SUPERSEDES 1989-13-05/AD Rev.00Perform within an unlimited threshold.

1991-21-13/AD Rev.00 *AD* ENG.CONT.SYSTEM-REPL. OF ENG. THROTTLE. CTRL. CABLES Closed 28.Feb.1992This Document SUPERSEDES 1989-13-05/AD Rev.00

> 737-76-1023/SB* Rev.NOTE *AD* ENG.CONT.SYSTEM-REPL. OF ENG. THROTTLE. CTRL. CABLES Closed 28.Feb.1992Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks28.Feb.1992 PerfRev.:'NOTE' / Reason: MALEV DOC.Reason for this StatusMALEV DOC.

1991-24-04 AD 00 MANDATORY A/C INSPECTION OF GIRT RESTRAINT STRAPS Superseded (Not Applicable)103-25-19-R8 (REF)1988-07-07 (SUPERSEDED)1991-24-04 (SUPERSEDED)1996-18-04 (ACTIVE)737-25A1221 (REF)737-25A1221-R1 (ACTIVE)

SBADADADSBSB

This Document SUPERSEDES 1988-07-07/AD Rev.00This Document has been SUPERSEDED BY 1996-18-04/AD Rev.00Reason for this StatusSUPERSEDED BY AD 1996-18-04





23.Oct.2014Page 51/429

Document-Number Type Rev Compliance A|C Subject Status1991-24-07 AD 00 MANDATORY COMP AIR CRUISERS COMPANY EMERGENCY EVACUATION SLIDE SYSTEM Not Applicable by Serial Number

Compliance:AD § (a), (b) are Not applicable due to PN not installed on NAS B737.1991-24-07 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

1991-25-06 AD 00 MANDATORY A/C *AD* PREVENT THRUST REVERSER TRANSLATING SLEEVE SEPARATION Not Applicable737-78A1048-R0 (REF)737-78A1048-R1 (REF)737-78A1048-R2 (REF)737-78A1048-R3 (REF)737-78A1048-R4 (REF)737-78A1048-R5 (REF)737-78A1048-R6 (REF)737-78A1048-R7 (REF)737-78A1048-R8 (ACTIVE)PRODUCTION LINE PRR34553

SBSBSBSBSBSBSBSBSBPRR

Perform within an unlimited threshold.1991-25-06/AD Rev.00 *AD* PREVENT THRUST REVERSER TRANSLATING SLEEVE SEPARATION Not Applicable> 737-78A1048/SB* Rev.08 *AD* PREVENT THRUST REVERSER TRANSLATING SLEEVE SEPARATION Not Applicable by Serial Number





23.Oct.2014Page 52/429

Document-Number Type Rev Compliance A|C Subject Status1992-03-07 AD 00 MANDATORY A/C APU SHROUD PLENUM AND COMBUSTOR DRAIN LINES, INPSECTION OF Closed 05.May.1993

Wiring harness rerouting (in support of SBB 737-49-1073)EFFECTIVITYLine number 737 0001 through 2060 i.a.w. PRR 33890-86.33890-86737-49-1073737-SL-49-14

PRRSBSL

0000B

This Document SUPERSEDES 1989-08-11/AD Rev.00This Document SUPERSEDES 1990-05-02/AD Rev.00Perform BEFORE 16.Mar.1995

1992-03-07/AD Rev.00 APU SHROUD PLENUM AND COMBUSTOR DRAIN LINES, INPSECTION OF Closed 05.May.1993This Document SUPERSEDES 1989-08-11/AD Rev.00This Document SUPERSEDES 1990-05-02/AD Rev.00

> 737-49-1073/SB* Rev.00 *AD* AIRBORNE AUXILIARY POWER - FUEL DRAIN SYSTEM CHANGES Closed 05.May.1993Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 85-49-6547/SB* Rev.01 *AD* WIRING HARNESS REROUT. (IN SUPPORT OF SBB 737-49-1073) Not Applicable by Serial NumberAffected Rotables (Part No/Serial No/Position) Status380428-10-1 / P-60280C Pos=APU (KKM) Not Applicable





23.Oct.2014Page 53/429

Document-Number Type Rev Compliance A|C Subject Status1992-04-07 AD 00 MANDATORY A/C *AD* INSPECTION AND PROTECTION OF WIRE BUNDLES ABOVE COCKPIT Closed 31.Mar.1993

This document is applicable to LN# 1001-2256.1992-04-07 (ACTIVE)37-AD-1992-04-07 (REPETITIVE)737-25A1299 NSC 2 (REF)737-25A1299-R0 (REF)737-25A1299-R1 (ACTIVE)SBB 737-25A1299 (MOD-TASK

ADTASBSBSBTA

Perform within an unlimited threshold.1992-04-07/AD Rev.00 *AD* INSPECTION AND PROTECTION OF WIRE BUNDLES ABOVE COCKPIT Closed 31.Mar.1993> 737-25A1299/SB Rev.00 *AD* COCKPIT WIRE BUNDLES DOOR HEADER SUPPORT BRACKET ASSEM Closed 31.Mar.1993> > 737-25A1299-01/EO* Rev.00 *AD* COCKPIT WIRE BUNDLES DOOR HEADER SUPPORT BRACKET ASSEM Closed 31.Mar.1993


31.Mar.1993PerfRev.:'NOTE' / Reason: DELIVERYDOC.


> > AD-1992-04-07/EO* Rev.00 *AD* *AD*WIREBUNDLE INSTALLATION ABOVE COCKPIT-TO-CABIN DOO Not Applicable by Serial Number

1992-07-02 AD 00 MANDATORY A/C *AD* PYLON NACELLE STRUT - FIREWALL SEALANT INSP./INST. Not Applicable737-54-1028 (REF)737-54-1028 R1 (ACTIVE)

SBSB

1992-07-02/AD Rev.00 *AD* PYLON NACELLE STRUT - FIREWALL SEALANT INSP./INST. Not Applicable> 737-54-1028/SB* Rev.01 *AD* PYLON NACELLE STRUT - FIREWALL SEALANT INSP./INST. Not Applicable by Serial Number





23.Oct.2014Page 54/429

Document-Number Type Rev Compliance A|C Subject Status1992-07-09 AD 00 MANDATORY A/C *AD* AUTOPILOT MODE CONTROL PANLE REPL. Performed by prev. Operator

This document is applicable to LN# 1001-2008.1992-07-09A4051601-22-17A4051601-22-18

ADSBSB

000000

This Document SUPERSEDES 1990-07-02/AD Rev.00Perform WITHIN 540/D (effective from 04.May.1992)

1992-07-09/AD Rev.00 *AD* AUTOPILOT MODE CONTROL PANLE REPL. Performed by prev. OperatorThis Document SUPERSEDES 1990-07-02/AD Rev.00

> 737-22A1098/SB* Rev.00 *AD* AUTOPILOT MODE CONTROL PANLE REPL. Performed by prev. OperatorPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

26.Oct.1993LHT EO007019

PerfRev.:'00'

Reason for this StatusPERFORMED BY LUFTHANSA





23.Oct.2014Page 55/429

Document-Number Type Rev Compliance A|C Subject Status1992-07-10 AD 00 MANDATORY A/C *AD* ELEC. LOAD DISTRIBUTION - WIRE BUNDLE INSP. & PANEL MOD Closed 19.Sep.1992

1989-08-11 (SUPERSEDED)1992-07-10 (ACTIVE)737-24-1077-R0 (REF)737-24-1077-R1 (REF)737-24-1077-R2 (REF)737-24-1077-R3 (REF)737-24-1077-R4 (ACTIVE)737-24-1084-R1 (ACTIVE)

ADADSBSBSBSBSBSB

This Document SUPERSEDES 1989-08-11/AD Rev.00Perform BEFORE 03.Nov.1992

1992-07-10/AD Rev.00 *AD* ELEC. LOAD DISTRIBUTION - WIRE BUNDLE INSP. & PANEL MOD Closed 19.Sep.1992This Document SUPERSEDES 1989-08-11/AD Rev.00

> 737-24-1077/SB* Rev.04 *AD* ELEC. LOAD DISTRIBUTION - WIRE BUNDLE INSP & PANEL MOD. Closed 19.Sep.1992Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-24-1084/SB* Rev.01 *AD* ELEC. LOAD DISTRIBUTION - BATTERY BUS WIRE REPLACEMENT Closed 18.Sep.1992Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







23.Oct.2014Page 56/429

Document-Number Type Rev Compliance A|C Subject Status1992-08-06 AD 00 MANDATORY A/C *AD* AFM CHANGES TO AUTOPILOT SPERRY MODEL SP177 Not Applicable

Not applicable to 737-300.1988-19-01 (SUPERSEDED)1989-18-01 (SUPERSEDED)1992-08-06 (ACTIVE)

ADADAD


1992-08-11 AD 00 MANDATORY A/C *AD* FLIGHT ATTENDANT SEATS - PREVENT FAILURE OF SEAT PANS Closed 09.Jan.1992Affected Attendant seat PN not installed.1992-08-11 (ACTIVE)SL 737-25-58-ATRANSAERO SB 192 (REF)

ADSLSB

000


09.Jan.1992 00:00/H 0/C

Was due at: UNDEFINED PerfRev.:'00' /Reason: MALEV DFP shows closed1992-01-09 MALEV DFP shows closed1992-01-09

Reason for this StatusMALEV DFP shows closed 1992-01-09





23.Oct.2014Page 57/429

Document-Number Type Rev Compliance A|C Subject Status1992-10-06 AD 00 MANDATORY COMP AIR CRUISERS COMPANY EMERGENCY EVACUATION SLIDE SYSTEM Not Applicable by Serial Number /

Special Text: Aircraft is NotApplicable due to IFE Halon bottlesnot installed.

Compliance:AD § (a), (b) are Not Applicable due to the PN not installed on NASB737001-25-81992-10-06

SBAD

0400


1992-11-09 AD 00 MANDATORY A/C *AD* ROCKWELL/COLLINS TRP-720 TRANSPONDERS Not ApplicableThis AD is applicable to Rockwell Collins PN: 622-7878-020/-120 ModeS transponders. NAS have not installed Mode S transponders with thisPN.1992-11-09 (ACTIVE)737-34-1343-R1

ADSB

1992-15-03 AD 00 MANDATORY A/C *AD* INCORPORATION OF MAXIMUM BRAKE WEAR LIMITS INTO THE AMM Repetitive1992-15-03 (ACTIVE)B32-41-41-6A (REF)

ADTA


18.Aug.1992PerfRev.:'NOTE' / Reason: AMM TASKB32-41-41-6A

Reason for this StatusAMM TASK B32-41-41-6A





23.Oct.2014Page 58/429

Document-Number Type Rev Compliance A|C Subject Status1992-16-01 AD 00 MANDATORY A/C *AD* FUSELAGE-SIDE OF BODY FLOOR PANEL INSERTS-INSP./REP Not Applicable

Not applicable per SB effectivity.1992-16-01 (ACTIVE)737-53A1152-R1 (ACTIVE)

ADSB

Perform within an unlimited threshold.1992-16-01/AD Rev.00 *AD* FUSELAGE-SIDE OF BODY FLOOR PANEL INSERTS-INSP./REP Not Applicable> 737-53A1152/SB* Rev.01 *AD* FUSELAGE-SIDE OF BODY FLOOR PANEL INSERTS-INSP./REP Not Applicable

This Document SUPERSEDES 737-53A1152/SB Rev.00Reason for this StatusNA DUE TO SB EFFECTIVITY





23.Oct.2014Page 59/429

Document-Number Type Rev Compliance A|C Subject Status1992-16-06 AD 00 MANDATORY A/C ALL AIRCRAFT EQUIPPED WITH GARRETT AIRRESEARCH AIRCRAFT Not Applicable

Compliance:AD § (a), (b) and (c) are Not applicable due to; NAS does not havethese PN installed:355290-1-1355740-1-1355760-3-1356364-1-1, 356364-8-2, and 356364-8-3356564-3-1383042-4-1383152-1-2, 383152-16-1, and 383152-19-1383222-1-1 and 383222-4-1383342-1-1, 383342-2-1, and 383342-4-1383350-1-1383370-1-1, 383370-2-1, 383370-3-1, 383370-4-1, 383370-5-1,383370-6-1, 383370-7-1,and 383370-8-1383642-1-1383780-1-1384022-5-1 and 380422 (all dash numbers)1992-16-06 (ACTIVE) ADReason for this StatusAUTO ASSIGNED





23.Oct.2014Page 60/429

Document-Number Type Rev Compliance A|C Subject Status1992-16-15 AD 00 MANDATORY A/C SCOTT AVIATION OXYGEN MASK PLUG-IN CONNECTORS, P/N SERIES 289-57 Not Applicable

Compliance:AD § (a), (b) and (c) are Not applicable as NAS does not install289-series oxygen cylinders.1992-16-15 (ACTIVE)289-35-15 (REF)

ADSB


1992-19-16 AD 00 MANDATORY A/C *AD* PREVENT OVERHEAD STOWAGE BINS FROM SEPARATING FROM ATT. Closed 31.Mar.1993This mod is applicable to LN# 991-2095. The following LN# are NotApplicable per PRR35041-2R.1992-19-16 (ACTIVE)737-25-1291 (REF)737-25-1294 (REF)737-25A1283-R1 (REF)PRODUCTION PRR35041-2R

ADSBSBSBPRR

Perform within an unlimited threshold.1992-19-16/AD Rev.00 *AD* PREVENT OVERHEAD STOWAGE BINS FROM SEPARATING FROM ATT. Closed 31.Mar.1993> 737-25-1294/SB* Rev.00 *AD* CHANGE OF FORTY-FIVE INCH OVERHEAD STOWAGE COMPARTMENT Not Applicable by Serial Number> 737-25A1283/SB* Rev.02 *AD* MODIFICATION OF OVERHEAD STOWAGE COMPARTMENT Closed 31.Mar.1993


31.Mar.1993PerfRev.:'NOTE' / Reason: DELIVERYDOCS

Reason for this StatusDELIVERY DOCS





23.Oct.2014Page 61/429

Document-Number Type Rev Compliance A|C Subject Status1992-24-04 AD 00 MANDATORY A/C *AD* T/R CTRL SYSTEM - MOD. OF TEE & RESTRICT. FITTING ON TR Closed 26.Oct.1993

1992-24-04 (ACTIVE)737-78A1055-R0 (REF)737-78A1055-R1 (REF)737-78A1055-R2 (REF)737-78A1055-R3 (ACTIVE)SBB 737-78A1055 (MOD TASK)

ADSBSBSBSBTA

Perform within an unlimited threshold.1992-24-04/AD Rev.00 *AD* T/R CTRL SYSTEM - MOD. OF TEE & RESTRICT. FITTING ON TR Closed 26.Oct.1993> 737-78A1055/SB* Rev.00 *AD* T/R CTRL SYSTEM - MOD. OF TEE & RESTRICT. FITTING ON TR Closed 26.Oct.1993

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks26.Oct.1993 PerfRev.:'NOTE' / Reason: MALEVReason for this StatusMALEV

1992-24-05 AD 00 MANDATORY A/C *AD* POWER PLANT GEN. - NACELLE HW & FUEL LINE INTERFERENCE Not Applicable1988-11-01 (SUPERSEDED)1991-20-03 (SUPERSEDED)1992-24-05 (ACTIVE)737-71A1208737-71A1208-R0 (REF)737-71A1208-R1 (REF)

ADADADSBSBSB

000000020001

This Document SUPERSEDES 1988-11-01/AD Rev.00This Document SUPERSEDES 1991-20-03/AD Rev.00

1992-24-05/AD Rev.00 *AD* POWER PLANT GEN. - NACELLE HW & FUEL LINE INTERFERENCE Not ApplicableThis Document SUPERSEDES 1988-11-01/AD Rev.00This Document SUPERSEDES 1991-20-03/AD Rev.00

> 737-71A1208/SB* Rev.02 *AD* POWER PLANT GEN. - NACELLE HW & FUEL LINE INTERFERENCE Not Applicable by Serial Number





23.Oct.2014Page 62/429

Document-Number Type Rev Compliance A|C Subject Status1992-25-04 AD 00 MANDATORY A/C *AD* PAX OXYGEN SYSTEM - TEST STOP PLUNGERS MODIFICATION Closed 27.Mar.1992

1992-25-04 (ACTIVE)737-35A1037 (REF)737-35A1037-R1 (ACTIVE)737-35A1038-R0 (ACTIVE)SBB 737-35A1037 (MOD-TASK)

ADSBSBSBTA


1992-25-04/AD Rev.00 *AD* PAX OXYGEN SYSTEM - TEST STOP PLUNGERS MODIFICATION Closed 27.Mar.1992This Document SUPERSEDES 1991-20-03/AD Rev.00

> 737-35A1037/SB* Rev.00 PAX OXYGEN SYSTEM - TEST STOP PLUNGERS MODIFICATION Closed 27.Mar.1992Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

27.Mar.1992SUNEXPRESS EO007856

> 737-35A1038/SB* Rev.00 PAX OXYGEN SYSTEM - OXYGEN BOX ASSEMBLY MODIFICATION Not Applicable by Serial Number





23.Oct.2014Page 63/429

Document-Number Type Rev Compliance A|C Subject Status1993-01-27 AD 00 MANDATORY A/C *AD* FLIGHT CONTROLS - CONTROL CABLES GUARD REPLACEMENT Closed 08.Dec.1995

1993-01-27 (ACTIVE)737-27A1164-R1 (REF)737-27A1164-R2 (ACTIVE)737-27A1164-RO (REF)PRODUCTION LINE PRR33890-67SBB 737-27A1164 (MOD-TASK)

ADSBSBSBPRRTA

Perform BEFORE 09.Mar.19971993-01-27/AD Rev.00 *AD* FLIGHT CONTROLS - CONTROL CABLES GUARD REPLACEMENT Closed 08.Dec.1995> 737-27A1164/SB* Rev.01 FLIGHT CONTROLS - CONTROL CABLES GUARD REPLACEMENT Superseded

This Document SUPERSEDES 737-27A1164/SB Rev.00This Document has been SUPERSEDED BY 737-27A1164/SB Rev.02

> 737-27A1164/SB* Rev.02 FLIGHT CONTROLS - CONTROL CABLES GUARD REPLACEMENT Closed 08.Dec.1995This Document SUPERSEDES 737-27A1164/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

08.Dec.1995LHT EO006425

> 737-27A1164/SB* Rev.00 FLIGHT CONTROLS - CONTROL CABLES GUARD REPLACEMENT SupersededThis Document has been SUPERSEDED BY 737-27A1164/SB Rev.01

1993-04-02 AD 00 MANDATORY COMP ROCKWELL INTERNATIONAL/COLLINS AVIATION DIVISION TDR-94 Not Applicable by Line NumberCompliance:AD § (a), (b) and (c) are Not applicable due to PN not installed onNAS B7371993-04-02 (ACTIVE)TDR-94/94D-34-6-R2

ADSB






23.Oct.2014Page 64/429

Document-Number Type Rev Compliance A|C Subject Status1993-05-05 AD 00 MANDATORY A/C *AD* TO PREVENT ENGINE FLAMEOUT DURING AIRPLANE DESCENT Information Only

1993-05-05 (ACTIVE)737-77-1031-R1 (ACTIVE)PRODUCTION PRR34633-10

ADSBPRR

This Document SUPERSEDES 1988-13-51/AD Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

29.Apr.1993PerfRev.:'NOTE' / Reason: COPY OF ADINTO AFM


1993-05-05SUB1 AD 00 MANDATORY A/C *AD* TO PREVENT ENGINE FLAMEOUT DURING AIRPLANE DESCENT Closed 03.Jan.19941988-13-51-R1 (SUPERSEDED)1993-05-05 (ACTIVE)737-77-1031-R1 (ACTIVE)PRODUCTION PRR34633-10

ADADSBPRR

Perform within an unlimited threshold.1993-05-05SUB1/AD Rev.00 *AD* TO PREVENT ENGINE FLAMEOUT DURING AIRPLANE DESCENT Closed 03.Jan.1994> 737-77-1031/SB* Rev.00 *AD* MOD FOR INCREASED CAPABILITY IN HAIL, RAIN AND SLEET Closed 03.Jan.1994


03.Jan.1994PerfRev.:'NOTE' / Reason: SUNEXPRESSEO: 737-77-1031

Reason for this StatusSUNEXPRESS EO: 737-77-1031





23.Oct.2014Page 65/429

Document-Number Type Rev Compliance A|C Subject Status1993-07-05 AD 00 MANDATORY A/C AMI PILOT AND CO-PILOT SEATS, MODEL 1108, S/N 004-189 Not Applicable

Compliance:AD § (a)is Not applicable due to PN not installed in NAS B737.1993-07-05 AD 00Reason for this StatusAUTO ASSIGNED

1993-07-13 AD 00 MANDATORY COMP APU EQUIPPED WITH ONE-PIECE CAST TURBINE WHEELS. Superseded (Not Applicable by LineNumber)

Compliance:AD § (a) and (b) are Not applicable, affected PN not installed on NASAircraft.1993-07-131997-04-04

ADAD

0000

This Document has been SUPERSEDED BY 1997-04-04/AD Rev.00Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

1993-07-15 AD 00 MANDATORY A/C *AD* AC WITH CLASS B MAIN DECK CARGO COMPARTMENT Not ApplicableNot applicable due to no Main deck cargo compartment.1989-18-12-R1 (SUPERSEDED)1991-10-02 (SUPERSEDED)1993-07-15 (ACTIVE)

ADADAD

This Document SUPERSEDES 1991-10-02/AD Rev.00Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 66/429

Document-Number Type Rev Compliance A|C Subject Status1993-14-10 AD 00 MANDATORY A/C *AD* FUSELAGE - AFT LOWER CARGO DOORWAY FRAME INSP/MOD/REP Not Applicable

1993-14-10 (ACTIVE)737-53-1096 (REF)737-53-1096 R1 (REF)737-53-1096 R2 (REF)737-53-1096 R3 (REF)737-53-1096 R4 (REF)737-53-1096 R5 (ACTIVE)SBB 737-53-1096 (MAINT TASK)

ADSBSBSBSBSBSBTA

1993-14-10/AD Rev.00 *AD* FUSELAGE - AFT LOWER CARGO DOORWAY FRAME INSP/MOD/REP Not Applicable> 737-53-1096/SB* Rev.05 *AD* FUSELAGE - AFT LOWER CARGO DOORWAY FRAME INSP/MOD/REP Not Applicable by Serial Number

1993-14-12 AD 00 MANDATORY COMP CREWMEMBER PROTECTIVE BREATHING EQUIPMENT (PBE) UNITS PELS MODEL4566M37B


Compliance:AD § (a) is Not applicable due to PN not installed on NAS B737. NASinstalls Draeger PBE.1993-14-12 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

1993-15-08 AD 01 MANDATORY A/C *AD* SUPERSEDED BY AD 1997-19-03 Superseded (Not Applicable)1993-15-08 R1 (SUPERSEDED)1997-19-03 (ACTIVE)IPECO SB A001-25-74 R2 (REF)IPECO SB A001-25-92-R2 (REF)SB A001-25-92 (MOD-TASK)

ADADSBSBTA






23.Oct.2014Page 67/429

Document-Number Type Rev Compliance A|C Subject Status1993-17-02 AD 00 MANDATORY A/C *AD* WING FUEL TANK FLOAT SWITCH CONDUIT CRACKING Closed 31.Mar.1993

1991-20-11 (SUPERSEDED)1993-17-02 (ACTIVE)37-SLB-28-036 (REPETITIVE)737-SL-28-036 (REF)737-SL-28-042-A (ACTIVE)

ADADTASLSL


1993-17-02/AD Rev.00 *AD* WING FUEL TANK FLOAT SWITCH CONDUIT CRACKING Closed 31.Mar.1993This Document SUPERSEDES 1991-20-11/AD Rev.00

> 737-SL-28-042/SL Rev.A WING FUEL TANK FLOAT SWITCH CONDUIT CRACKING Closed 31.Mar.1993> > 737-SL-28-042-01/EO*Rev.00

*AD* WING FUEL TANK FLOAT SWITCH CONDUIT CRACKING Closed 31.Mar.1993

This Document terminates SLB-28-036/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

31.Mar.1993 00:00/H 0/C

PerfRev.:'00' / Reason: DELIVERY DOC.Performed by LHT on Eo 008718. Thisterminates repetitive insp. as grease isintroduced in conduit.

Reason for this StatusPerformed by LHT on Eo 008718. This terminates repetitive insp. as grease is introduced in conduit.

> > SLB-28-036/EO* Rev.00 *AD* WING FUEL TANK FLOAT SWITCH CONDUIT CRACKING Closed 31.Mar.1993This Document is terminated with implementation of 737-SL-28-042-01/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

31.Mar.1993 00:00/H 0/C

Was due at: 90000/H PerfRev.:'00' Thuisdocument is terminated by EO737-SL-28-042-01, that Eo introduces greasein conduit.

Reason for this StatusThuis document is terminated by EO 737-SL-28-042-01, that Eo introduces grease in conduit.





23.Oct.2014Page 68/429

Document-Number Type Rev Compliance A|C Subject Status1993-17-03 AD 00 MANDATORY A/C *AD* EVACUATION ESCAPE SLIDE MODIFICATION Not Applicable

BFGoodrich slides not installed on NAS Aircraft.1993-17-03 (ACTIVE)SB101658/659/660-25-257

ADSB

1993-17-51 AD 00 MANDATORY A/C *AD* HORIZONTAL STABILIZER - HINGE FITTING INSPECTION Not Applicable by Serial Number1993-17-51-R0 (ACTIVE) AD

1993-23-01 AD 00 MANDATORY A/C NORDSKOG IND, INC. WATER HEATERS AND COFFEE MAKERS Not ApplicableCompliance:AD § (a) and (b) is Not applicable due to the affected PN notinstalled on NAS B737.1993-23-01SB-93-34

ADSB

0000


1993-24-16 AD 00 MANDATORY COMP PURITAN BENNETT AERO SYSTEMS CREWMEMBER PROTECTIVE BREATHINGEQUIPMENT (PBE) 119003 AND 119003-01 UNITS

Not Applicable by Line Number

Compliance:AD § (a) is Not applicable due to the affected PN not installed onNAS B737. NAS installs Draeger PBE.1993-24-16 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 69/429

Document-Number Type Rev Compliance A|C Subject Status1994-01-04 AD 00 MANDATORY COMP TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) II Not Applicable by Line Number

Compliance:AD § (a) and (b) are Not applicable due to PN not installed in NASB737.1994-01-04 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

1994-01-05 AD 00 MANDATORY A/C TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM II PROCESS Not ApplicableCompliance:AD § (a) is Not applicable due to PN not installed on NAS B737.1994-01-05 (ACTIVE) ADReason for this StatusAUTO ASSIGNED

1994-01-06 AD 00 MANDATORY A/C TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM II PROCESS Not ApplicableCompliance:AD § (a) is Not appliacble due to PN not installed on NAS B737.1994-01-06 (ACTIVE) ADReason for this StatusAUTO ASSIGNED

1994-01-07 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 1997-14-04 Superseded (Not Applicable)1994-01-07 (SUPERSEDED)1997-14-04 (ACTIVE)

ADAD






23.Oct.2014Page 70/429

Document-Number Type Rev Compliance A|C Subject Status1994-02-02 AD 00 MANDATORY COMP COLLINS AIR TRANSPORT DIVISION DME-700 DISTANCE MEASURI Not Applicable by Line Number

Compliance:AD § (a), (b) and (c) are Not applicable to due to PN not installedon NAS B737.1994-02-02 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

1994-06-04 AD 00 MANDATORY COMP *AD* EROS SERIES MF10-[ ]-[ ] FULL FACE QUICK DONNING MASK REGULATORS Not Applicable by Line NumberNot applicable due to all masks have AD incorperated at production ormainteained by CMM 35-13-61 Rev.:3 or later (SB MF10-35-44 andMF10-35-46 incorperated.)1994-06-04 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 71/429

Document-Number Type Rev Compliance A|C Subject Status1994-06-11 AD 00 MANDATORY A/C *AD* LEADING EDGE PANEL SEALING AND DRAIN HOLE PLUGGING TO PREVENT

DRAINAGE FROM FUEL LINE LEAK INTO TURBINE EXHAUST AREAClosed 08.Dec.1995

1994-06-11 (ACTIVE)737-57-1221-R0 (REF)737-57-1221-R1 (REF)737-57-1221-R2 (ACTIVE)

ADSBSBSB

Perform BEFORE 03.Feb.19961994-06-11/AD Rev.00 *AD* LEADING EDGE PANEL SEALING AND DRAIN HOLE PLUGGING TO PREVENT

DRAINAGE FROM FUEL LINE LEAK INTO TURBINE EXHAUST AREAClosed 08.Dec.1995

> 737-57-1221/SB* Rev.00 *AD* LEADING EDGE PANEL SEALING AND DRAIN HOLE PLUGGING Closed 08.Dec.1995Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

08.Dec.1995PerfRev.:'NOTE' / Reason: PREVIOUSOPERATOR DOC.


1994-12-12 AD 00 MANDATORY A/C *AD* MAIN CARGO DOOR - HINGE SHIMS/FAIRINGS REPLACEMENT Not ApplicableNot applicable due to no Main deck cargo door installed.1994-12-12PEMCO AEROPLEX SB 737-52-0012SB 737-52-0012 (MOD-TASK)

ADSBTA

1994-14-03 AD 00 MANDATORY A/C *AD* NORDSKOG WATER HEATERS AND COFFEE MAKERS AS INSTALLED Not ApplicableNot applicable per PN installed.1994-14-03 (ACTIVE)SB-93-35

ADSB

0000






23.Oct.2014Page 72/429

Document-Number Type Rev Compliance A|C Subject Status1994-19-06 AD 00 MANDATORY A/C PURITAN BENNETT SWEEP-ON MODEL 2000 CREW MASKS Not Applicable

Compliance:AD § (a) is Not applicable due to affected PN not installed on NASB737.174250-35-11994-19-06

SBAD

0000


1994-21-05 AD 00 MANDATORY A/C *AD* TRUST REVERSER SYNC LOCK INSTALLATION - CFM56 ENGINES Superseded (Superseded)1994-21-05 (SUPERSEDED)1994-21-05-R1 (ACTIVE)37-78-31-04-01 (REP TASK)37-78-31-04-02 (REP TASK)737-78-1053-R0 (REF)737-78-1053-R1 (REF)737-78-1053-R2 (REF)737-78-1053-R3 (REF)737-78-1053-R4 (REF)737-78-1053-R5 (REF)737-78-1053-R6 (ACTIVE)AD 1994-21-05SUB1 (REPETITIVE)PRODUCTION PRR35105

ADADTATASBSBSBSBSBSBSBADPRR






23.Oct.2014Page 73/429

Document-Number Type Rev Compliance A|C Subject Status1994-21-05 AD 01 MANDATORY A/C *AD* TRUST REVERSER SYNC LOCK INSTALLATION - CFM56 ENGINES Repetitive

1994-21-05 (SUPERSEDED)1994-21-05-R1 (ACTIVE)37-78-31-04-01 (REP TASK)37-78-31-04-02 (REP TASK)737-78-1053-R0 (REF)737-78-1053-R1 (REF)737-78-1053-R2 (REF)737-78-1053-R3 (REF)737-78-1053-R4 (REF)737-78-1053-R5 (REF)737-78-1053-R6 (ACTIVE)AD 1994-21-05SUB1 (REPETITIVE)PRODUCTION PRR35105


This Document SUPERSEDES 1994-21-05/AD Rev.00Perform BEFORE 25.Nov.1999

1994-21-05/AD Rev.01 *AD* TRUST REVERSER SYNC LOCK INSTALLATION - CFM56 ENGINES RepetitiveThis Document SUPERSEDES 1994-21-05/AD Rev.00

> 737-78-1053/SB* Rev.06 *AD* TRUST REVERSER SYNC LOCK INSTALLATION - CFM56 ENGINES RepetitivePerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

12.Apr.1997PerfRev.:'NOTE' / Reason: DELIVERYDOC.






23.Oct.2014Page 74/429

Document-Number Type Rev Compliance A|C Subject Status1994-21-05SUB1 AD 01 MANDATORY A/C *AD* TRUST REVERSER SYNC LOCK REPETITIVE TEST - CFM56 ENG Taskcard Controlled

1994-21-05 (SUPERSEDED)1994-21-05-R1 (ACTIVE)37-78-031-04-01 (REPEAT TASK)37-78-031-04-02 (REPEAT TASK)737-78-1053-R0 (REF)737-78-1053-R1 (REF)737-78-1053-R2 (REF)737-78-1053-R3 (REF)737-78-1053-R4 (REF)737-78-1053-R5 (REF)737-78-1053-R6 (ACTIVE)AD 1994-21-05SUB1 (REPETITIVE)PRODUCTION PRR35105


Carried out on the following TaskcardsTaskcard: 78-031-04-02 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks26.06.2015 75'572/H 2250:25/H Interval:4000/HPerf Dim1 (D) Perf Dim2 Perf Dim326.02.2014 71572:00/H 43151/CCarried out on the following TaskcardsTaskcard: 78-031-04-01 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks26.06.2015 75'572/H 2250:25/H Interval:4000/HPerf Dim1 (D) Perf Dim2 Perf Dim305.03.2014 71572:00/H 43151/CPerform within an unlimited threshold.

1994-21-05SUB1/AD Rev.01 *AD* TRUST REVERSER SYNC LOCK REPETITIVE TEST - CFM56 ENG Taskcard ControlledCarried out on the following TaskcardsTaskcard: 78-031-04-02 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks





23.Oct.2014Page 75/429

Document-Number Type Rev Compliance A|C Subject Status26.06.2015 75'572/H 2250:25/H Interval:4000/HPerf Dim1 (D) Perf Dim2 Perf Dim326.02.2014 71572:00/H 43151/CCarried out on the following TaskcardsTaskcard: 78-031-04-01 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks26.06.2015 75'572/H 2250:25/H Interval:4000/HPerf Dim1 (D) Perf Dim2 Perf Dim305.03.2014 71572:00/H 43151/C

> 1994-21-05SUB1MPD/EO*Rev.00

1994-21-05SUB1MPD CONTROLLED BY MPD TASKS Taskcard Controlled

Carried out on the following TaskcardsTaskcard: 78-031-04-02 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks26.06.2015 75'572/H 2250:25/H Interval:4000/HPerf Dim1 (D) Perf Dim2 Perf Dim326.02.2014 71572:00/H 43151/CCarried out on the following TaskcardsTaskcard: 78-031-04-01 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks26.06.2015 75'572/H 2250:25/H Interval:4000/HPerf Dim1 (D) Perf Dim2 Perf Dim305.03.2014 71572:00/H 43151/CReason for this StatusAUTO ASSIGNED





23.Oct.2014Page 76/429

Document-Number Type Rev Compliance A|C Subject Status1994-21-06 AD 00 MANDATORY A/C PACIFIC SCIENTIFIC COMPANY, HTL/KIN-TECH DIVISION, LAP BELT ASSEMBLIES AND

RESTRAINT SYSTEMSNot Applicable

Compliance:AD § (a) and (b) are Not applicable due to the affected PN notinstalled on NAS B737.1108435-25-011108460-25-011994-21-06

SBSBAD

000000


1994-25-05 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 1997-22-07 Superseded (Not Applicable)1994-25-05 (SUPERSEDED)1997-22-07 (SUPERSEDED)2002-07-10 (ACTIVE)737-53A1177-R6 (REF)737-SL-53-063-A (REF)737-SL-53-063-B (REF)

ADADADSBSLSL

This Document has been SUPERSEDED BY 1997-22-07/AD Rev.00Reason for this StatusSUPERSEDED BY AD 1997-22-07





23.Oct.2014Page 77/429

Document-Number Type Rev Compliance A|C Subject Status1994-26-13 AD 00 MANDATORY A/C *AD* LEADING EDGE PANEL SEALING AND DRAIN HOLE PLUGGING TO PREVENT

DRAINAGE FROM FUEL LINE LEAK INTO TURBINE EXHAUST AREANot Applicable by Serial Number

This directive is applicable to LN# 2184, 2187, 2194-2197 and 2199.All other LN# are Not Applicable per AD.1994-06-11 (REF)1994-26-13 (ACTIVE)737-57-1221-R0 (REF)737-57-1221-R1 (REF)737-57-1221-R2 (ACTIVE)

ADADSBSBSB

1995-01-01 AD 00 MANDATORY COMP TERRA CORPORATION TRT 250 SERIES TRANSPONDERS Not Applicable by Serial NumberCompliance:AD § (a) through (d) is Not Applicable; affected PN not installed onNAS Aircraft.1995-01-01SB-104

ADSB

0001


1995-01-06 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 2001-09-15 Superseded (Not Applicable)1995-01-06R1 (SUPERSEDED)2001-09-15 (ACTIVE)737-53-0003-R5 (PEMCO)

ADADSB






23.Oct.2014Page 78/429


1995-02-08-R1 (SUPERSEDED)2004-23-07 (ACTIVE)737-53-1154-R2 (REF)

ADADSB


1995-02-08/AD Rev.01 *AD* SUPERSEDED BY AD 2004-23-07 Not ApplicableThis Document has been SUPERSEDED BY 2004-23-07/AD Rev.00

> 737-53-1154/SB* Rev.02 *AD* FUSELAGE, GALLEY NO 2 UPPER ATTACHMENT SUPPORT Not ApplicableReason for this StatusN/A - SB EFFECTIVITY

1995-04-01 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 1996-02-06 Superseded (Not Applicable)1995-04-01 (SUPERSDED)1996-02-06 (ACTIVE)

ADAD


1995-06-05 AD 00 MANDATORY A/C *AD* PREVENT RAPID DECOMPRESSION DUE TO CRACKING OF FUSELAGE INSP. OFMAIN DECK CARGO DOOR PER STC SA2969SO

Not Applicable

NAS does not operate any Aircraft with main deck cargo door. STCSA2969SO not performed.1995-06-05 (ACTIVE)PEMCO ALERT SB 737-53-0004

ADSB





23.Oct.2014Page 79/429

Document-Number Type Rev Compliance A|C Subject Status1995-06-53 AD 00 MANDATORY A/C TEST OF MAIN RUDDER POWER CONTROL UNIT - SECONDARY SLIDE Superseded (Superseded)


ADAD


1995-07-03 AD 00 MANDATORY COMP *AD* TO PREVENT AN AXIALLY UNCONTAINED APU FAILURE Not ApplicableNA to GCTP85-129 i.a.w. Honeywell SB 49-6919 R2. Applicabilitydeleted.85-49-6919 SB 02Perform within an unlimited threshold.

1995-07-03/AD Rev.00 *AD* TO PREVENT AN AXIALLY UNCONTAINED APU FAILURE Not Applicable> 85-49-6919/SB* Rev.02 REPLACE/REWORK EXHAUST PIPE Not Applicable



1995-09-01 AD 00 MANDATORY A/C *AD* THRUST REVERSER - APPL. OF A TOPCOAT TO THE T/R FIREWAL Not ApplicableThis document is applicable to LN# 2137-2171. All other LN# are NotApplicable per Boeing SB.1995-09-01 (ACTIVE)737-78A1056-R0 (REF)737-78A1056-R1 (ACTIVE)

ADSBSB

1995-09-01/AD Rev.00 *AD* THRUST REVERSER - APPL. OF A TOPCOAT TO THE T/R FIREWAL Not Applicable> 737-78A1056/SB* Rev.01 *AD* THRUST REVERSER - APPL. OF A TOPCOAT TO THE T/R FIREWAL Not Applicable by Serial Number





23.Oct.2014Page 80/429

Document-Number Type Rev Compliance A|C Subject Status1995-10-05 AD 00 MANDATORY A/C *AD* HORIZONTAL STABILIZER - REPL. OF THE HORIZONTAL STABILIZER ELECTRIC

TRIM ACTUATORPerformed by prev. Operator

Perform BEFORE 12.Jun.19961995-10-05/AD Rev.00 *AD* HORIZONTAL STABILIZER - REPL. OF THE HORIZONTAL STABILIZER ELECTRIC

TRIM ACTUATORPerformed by prev. Operator

> 737-27A1191/SB* Rev.01 *AD* HORIZONTAL STABILIZER - REPL. OF THE HORIZONTAL STABILIZER ELECTRICTRIM ACTUATOR

Performed by prev. Operator

This Document SUPERSEDES 737-27A1191/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

25.Nov.1994DELIVERYDOC

PerfRev.:'01'

1995-15-06 AD 00 MANDATORY A/C REPLACEMENT OF FUEL SHUT OFF ACTUATOR VALVES Closed 08.Dec.19951998-18-20J.C. CARTER SB 61163-28-08

ADSB

00

Perform within an unlimited threshold.1995-15-06/AD Rev.00 REPLACEMENT OF FUEL SHUT OFF ACTUATOR VALVES Closed 08.Dec.1995> 61163-28-08/SB* Rev.00 *AD* ENG. FUEL SHUTOFF/SYSTEM XFEED VALVES - REPLACEMENT OF Closed 08.Dec.1995


08.Dec.1995PerfRev.:'NOTE' / Reason: DELIVERYDOC.






23.Oct.2014Page 81/429

Document-Number Type Rev Compliance A|C Subject Status1995-22-01 AD 00 MANDATORY A/C AEROSPACE LIGHTING CORPORATION POWER UNITS/POWER SUPPLIES Not Applicable

Compliance:AD § (a) and (b) are Not applicable to NAS due to; affected PN notinstalled.1995-01-01 (ACTIVE) ADThis Document SUPERSEDES 1990-14-06/AD Rev.00Reason for this StatusAUTO ASSIGNED

1995-23-10 AD 00 MANDATORY A/C AIRPLANE FLIGHT MANUAL REVISION - APU SHUTDOWN Performed by prev. Operator737-800 had its AFM revised at build. ref FCOM bulletin FUA-411995-23-10 (ACTIVE) ADPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks01.Sep.2002Reason for this StatusAFM REVISED

1995-25-08 AD 00 MANDATORY A/C ROYAL INVENTUM COMPANY DR1 AND DR6 SERIES GALLEY WATER HEATERS Not ApplicableCompliance:AD § (a) is Not applicable due to Royal Inventum Company DR1 and DR6series galley water heaters not installed on NAS B737.1995-25-08 AD 00Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 82/429

Document-Number Type Rev Compliance A|C Subject Status1995-26-15 AD 00 MANDATORY A/C ALLIED SIGNAL COM. AVIONICS SYSTEMS CAS-81 TRAFFIC AL.R Superseded (Superseded)

Compliance:AD § (a), (b) and (c) are Not applicable due to PN: CAS-81 TCAS notinstalled on NAS B737.1995-26-15 (ACTIVE) ADThis Document has been SUPERSEDED BY 1995-26-15/AD Rev.01

1995-26-15 AD 01 MANDATORY A/C ALLIED SIGNAL COM. AVIONICS SYSTEMS CAS-81 TRAFFIC AL.R Not ApplicableCompliance:AD § (a), (b) and (c) are Not applicable due to PN: CAS-81 TCAS notinstalled on NAS B737.1995-26-15 (ACTIVE) ADThis Document SUPERSEDES 1995-26-15/AD Rev.00Reason for this StatusAUTO ASSIGNED

1996-02-06 AD 00 MANDATORY A/C *AD* AIRPLANE FLIGHT MANUAL REVISION - WINDSHEAR Not ApplicableApplicable to 737-300 equiped with Standard Windshear (Honeywell STC)P/N 4068060-901.AD is NA to NAS. Affcted PN not installed.1995-04-01 (SUPERSDED)1996-02-06 (ACTIVE)

ADAD

This Document SUPERSEDES 1995-04-01/AD Rev.00Reason for this StatusAFFECTED EQUIPMENT NOT INSTAL





23.Oct.2014Page 83/429

Document-Number Type Rev Compliance A|C Subject Status1996-10-06 AD 00 MANDATORY A/C *AD* FWD GALLEY SERVICE DOOR - LWR GATE HINGE REPLACEMENT Not Applicable

This document is applicable to LN# 241-1727. The following LN# areNot Applicable per PRR 34473.1996-10-06 (ACTIVE)2004-225 (REF)737-52-1097 (REF)737-52A1124 (ACTIVE)PRODUCTION LINE PRR34473SBB 737-52A1124 (MOD -TASK)

ADADSBSBPRRTA

1996-10-06/AD Rev.00 *AD* FWD GALLEY SERVICE DOOR - LWR GATE HINGE REPLACEMENT Not Applicable> 737-52A1124/SB* Rev.00 AD* FWD GALLEY SERVICE DOOR - LWR GATE HINGE REPLACEMENT Not Applicable by Serial Number

1996-10-08 AD 00 MANDATORY A/C *AD* LOWER 43 SECTION WIRE CHAFING Not Applicable1996-10-08 (ACTIVE)737-SL-24-106

ADSL

1996-10-08/AD Rev.00 *AD* LOWER 43 SECTION WIRE CHAFING Not Applicable> 737-SL-24-106/SL* Rev.04 *AD* LOWER 43 SECTION WIRE CHAFING Not Applicable by Serial Number

1996-12-09 AD 00 MANDATORY A/C PTC SEATING PRODUCTS DIVISION, B/E AEROSPACE, MODEL 950 SERIES PASSENGERSEATS EQUIPPED WITH FOOTREST ASSEMBLY

Not Applicable

Compliance:AD § (a) is Not applicable due to affected PN: B/E Aerospace (PTC)Model 950 series passenger seat not installed on NAS B737.1996-12-09 (ACTIVE) ADReason for this StatusAUTO ASSIGNED





23.Oct.2014Page 84/429

Document-Number Type Rev Compliance A|C Subject Status1996-18-04 AD 00 MANDATORY A/C *AD*FWD SERVICE & ENTRY DOOR ESCAPE SLIDE GIRT RETENTION MOD Closed 05.Jul.2012

103-25-19-R8 (REF)1988-07-07 (SUPERSEDED)1991-24-04 (SUPERSEDED)1996-18-04 (ACTIVE)737-25A1221 (REF)737-25A1221-R1 (ACTIVE)PRODUCTION LINE PRR34388SBB 737-25A1221 (MOD-TASK)

SBADADADSBSBPRRTA

This Document SUPERSEDES 1988-07-07/AD Rev.00This Document SUPERSEDES 1991-24-04/AD Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

13.Jan.1994SUNEXPRESSEO008305

Reason: EMERGENCY ESCAPE SLIDE

REPLACED

Reason for this StatusEMERGENCY ESCAPE SLIDE REPLACED

1996-18-04/AD* Rev.00 *AD*FWD SERVICE & ENTRY DOOR ESCAPE SLIDE GIRT RETENTION MOD Closed 05.Jul.2012This Document SUPERSEDES 1988-07-07/AD Rev.00This Document SUPERSEDES 1991-24-04/AD Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

13.Jan.1994SUNEXPRESSEO008305

Reason: EMERGENCY ESCAPE SLIDE

REPLACED

Reason for this StatusEMERGENCY ESCAPE SLIDE REPLACED

> 737-25A1221/SB* Rev.01 *AD* FWD SERVICE/ENTRY DOOR ESCAPE SLIDE GIRT RETENTION MOD Not ApplicableReason for this StatusAUTO ASSIGNED





23.Oct.2014Page 85/429

Document-Number Type Rev Compliance A|C Subject Status1996-18-16 AD 00 MANDATORY COMP LPTR STUB SHAFT & CONICAL SUPPORT, REIDENTIFICATION OF Closed 26.Jun.2012

Status apply for EASA AD 1997-010.1996-18-163-72-0695CFMI-TP.SM.5

ADSBESM

0001LAST

Perform within an unlimited threshold.1996-18-16/AD Rev.00 LPTR STUB SHAFT & CONICAL SUPPORT, REIDENTIFICATION OF Closed 26.Jun.2012> 3-72-0695/SB* Rev.01 LPTR STUB SHAFT & CONICAL SUPPORT, REIDENTIFICATION OF Closed 26.Jun.2012

This Document SUPERSEDES 3-72-0695/SB Rev.00Affected Rotables (Part No/Serial No/Position) Status

CFM56-3B2 / 724473 Pos=LH (KKM)

Closed / Last Performed:21.Aug.201062274:00/H 37501/C RefDocument:ESNNOT AFFECTED MTU WO 51.715.400Rev.01

CFM56-3B2 / 725495 Pos=RH (KKM)Closed / Last Performed:26.Jun.201264007:00/H 38431/C RefDocument:NAPER INST PN 301-330-626-0 Rev.01

1996-21-13 AD 00 MANDATORY A/C LITEF ATTITUDE AND HEADING REF SYS MODEL LCR-92 Not ApplicableCompliance:AD § (a) is Not applicable due to affected Attitude and HeadingReference System (AHRS) Model LCR-92, not installed on NAS B737.Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 86/429

Document-Number Type Rev Compliance A|C Subject Status1996-25-11 AD 00 MANDATORY COMP TO PREVENT FAN BLADE FAILURE AND COMPLETE LOS OF PWR Closed 27.Jun.2012

Status apply for EASA AD 1990-031.1989-13-511996-25-113-72-0543

ADADSB

000008

This Document SUPERSEDES 1989-13-51/AD Rev.00This Document SUPERSEDES 3-72-0473/SB Rev.02Perform BEFORE 29.Jan.1997

1996-25-11/AD Rev.00 TO PREVENT FAN BLADE FAILURE AND COMPLETE LOS OF PWR Closed 27.Jun.2012This Document SUPERSEDES 1989-13-51/AD Rev.00This Document SUPERSEDES 3-72-0473/SB Rev.02

> 3-72-0543/SB* Rev.08 TO PREVENT FAN BLADE FAILURE AND COMPLETE LOS OF PWR Closed 27.Jun.2012Affected Rotables (Part No/Serial No/Position) Status

CFM56-3B2 / 725495 Pos=RH (KKM)

Closed / Reason: PE: PREVIOUSLYEMBODIED / Last Performed:27.Jun.201264007:00/H 38431/C RefDocument:MTURECORDED MOD SHEET Rev.07

CFM56-3B2 / 724473 Pos=LH (KKM)Not Applicable / Reason: NA IAWMALEV 22.04.2003





23.Oct.2014Page 87/429

Document-Number Type Rev Compliance A|C Subject Status1996-25-17 AD 00 MANDATORY A/C *AD* FLIGHT CONTROLS - INSP/MOD OF THE FEEL & CENTERING UNIT Closed 19.Nov.1996

1996-25-17 (ACTIVE)737-27A1194-R0 (REF)737-27A1194-R1 (REF)737-27A1194-R2 (ACTIVE)

ADSBSBSB

Perform BEFORE 03.Aug.19971996-25-17/AD Rev.00 *AD* FLIGHT CONTROLS - INSP/MOD OF THE FEEL & CENTERING UNIT Closed 19.Nov.1996> 737-27A1194/SB* Rev.02 *AD* FLIGHT CONTROLS - INSP/MOD OF THE FEEL & CENTERING UNIT Closed 19.Nov.1996


19.Nov.1996PerfRev.:'NOTE' / Reason: PREVIOUSOPERATOR DOC.


1996-26-07 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 2007-03-07 Superseded (Not Applicable)1996-26-07 (SUPERSEDED)2000-22-02 (SUPERSEDED)2002-20-07 (SUPERSEDED)2007-03-07 (ACTIVE)

ADADADAD


1997-01-12 AD 00 MANDATORY A/C AIRTELL CENTAURUS MODEL C3-100 GROUND PROXIMITY WARNING Not ApplicableCompliance:AD § (a) is Not applicable due to affected Centaurus Model C3-100GPWS not installed on NAS B737.Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 88/429

Document-Number Type Rev Compliance A|C Subject Status1997-02-16 AD 00 MANDATORY A/C *AD* FLAPS - MOD. OF FLAP CTRL. CABLE FAILURE DETECTION SYS. Closed 08.Apr.1997

1997-02-16 (ACTIVE)737-27A1199 (ACTIVE)

ADSB

Perform BEFORE 3200/HPerform BEFORE 04.Sep.1998

1997-02-16/AD Rev.00 *AD* FLAPS - MOD. OF FLAP CTRL. CABLE FAILURE DETECTION SYS. Closed 08.Apr.1997> 737-27A1199/SB* Rev.00 *AD* FLAPS - MOD. OF FLAP CTRL. CABLE FAILURE DETECTION SYS. Closed 08.Apr.1997


08.Apr.1997PerfRev.:'NOTE' / Reason: PREVIOUSOPERATOR DOC.


1997-03-14 AD 00 MANDATORY A/C *AD* FLIGHT CTRLS - AILERON CTRL CABLE PULLLEY BRACKET INSP. Not ApplicableThis document is applicable to LN# 1-1388. The following LN# are NotApplicable per Boeing SB.1997-03-14 (ACTIVE)737-27-1154-RO (ACTIVE)

ADSB

1997-03-14/AD Rev.00 *AD* FLIGHT CTRLS - AILERON CTRL CABLE PULLLEY BRACKET INSP. Not Applicable> 737-27-1154/SB* Rev.00 *AD* FLIGHT CTRLS - AILERON CTRL CABLE PULLLEY BRACKET INSP. Not Applicable by Serial Number





23.Oct.2014Page 89/429

Document-Number Type Rev Compliance A|C Subject Status1997-04-01 AD 00 MANDATORY A/C *AD* AILERON - CENTERING SPRING AND TRIM MECHANISM MOD. Not Applicable

This mod is applicable to LN# 1-1742. The following LN# are NotApplicable due to PRR34533737-27-1155 NSC-01737-27-1155 NSC-02737-27-1155 NSC-03PRODUCTION LINE PRR34533

SBSBSBPRR

00000000

Perform within an unlimited threshold.1997-04-01/AD Rev.00 *AD* AILERON - CENTERING SPRING AND TRIM MECHANISM MOD. Not Applicable> 737-27-1155/SB* Rev.00 *AD AILERON - CENTERING SPRING AND TRIM MECHANISM MOD. Not Applicable by Serial Number





23.Oct.2014Page 90/429

Document-Number Type Rev Compliance A|C Subject Status1997-04-04 AD 00 MANDATORY COMP INSTALLATION OF CONTAINMENT AUGMENTATION RING ON ALLIEDSIGNAL INC.

GTCP85 SERIES AUXILIARY POWER UNITSNot Applicable

Compliance:AD § (Ref. Honeywell SB 49-A7189 Rev. 2, 08 Oct. 1996 for GTCP85-129.GTCP85-129CK - P/N 380428-9 **GTCP85-129H - P/N 380428-10 - S/N P-100756*GTCP85-129J - P/N 380428-11 **GTCP85-129K - P/N 380428-12 - S/N P-175*GTCP85-129CKA - P/N 380428-13 **GTCP85-129CKB - P/N 380428-14 **

* First unit production point** No production unit have been delivered with this improvement1997-04-0485-49A670685-49A7189

ADSBSB

000202

This Document SUPERSEDES 1993-07-13/AD Rev.00Perform BEFORE 24.Mar.1999

1997-04-04/AD Rev.00 INSTALLATION OF CONTAINMENT AUGMENTATION RING ON ALLIEDSIGNAL INC.GTCP85 SERIES AUXILIARY POWER UNITS

Not Applicable

This Document SUPERSEDES 1993-07-13/AD Rev.00> 85-49A7189/SB* Rev.02 TURBINE WHEEL SHROUD CONT. AUGMENTATION RING - INCORP. OF Not Applicable by Serial Number

Affected Rotables (Part No/Serial No/Position) Status380428-10-1 / P-60280C Pos=APU (KKM) Not Applicable





23.Oct.2014Page 91/429

Document-Number Type Rev Compliance A|C Subject Status1997-04-15 AD 00 MANDATORY COMP PACIFIC FIRE EXTINGUISHER BOTTLE CARTRIDGES Not Applicable by Serial Number

Compliance:AD § (a) and (b) are Not Applicable, affected PN not installed on NASAircraft.Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

1997-05-09 AD 00 MANDATORY A/C *AD* AILERON/ELEV. PCU FLOW RESTRICTOR FILTER SCREEN CONTAM. Closed 17.Aug.2001Previous operators controlled this AD on an Aircraft leveleffectivity. NAS has moved to component effectivity on laterrevisions. The original SL (Rev 00) is attached for historicalreasons only.1997-05-09737-SL-27-071

ADSL

Perform BEFORE 15000/HPerform BEFORE 09.Apr.2002

1997-05-09/AD Rev.00 *AD* AILERON/ELEV. PCU FLOW RESTRICTOR FILTER SCREEN CONTAM. Closed 17.Aug.2001> 737-SL-27-071/SL* Rev.B *AD* AILERON/ELEV. PCU FLOW RESTRICTOR FILTER SCREEN CONTAM. Not Applicable by Serial Number

This Document SUPERSEDES 737-SL-27-071/SL Rev.AAffected Rotables (Part No/Serial No/Position) Status65-44761-21 / 6895A Pos=AFT (KKM) Not Applicable65-44761-21 / 9311AB Pos=AFT (KKM) Not Applicable65-44761-21 / 7418A Pos=LH (KKM) Not Applicable

> 737-SL-27-071/SL* Rev.00 *AD* AILERON/ELEV. PCU FLOW RESTRICTOR FILTER SCREEN CONTAM. Closed 17.Aug.2001Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

17.Aug.2001PerfRev.:'NOTE' / Reason: DELIVERYDOC.






23.Oct.2014Page 92/429


1997-05-10 (SUPERSEDED)2002-20-07 (SUPERSEDED)2007-03-07 (ACTIVE)

ADADAD


1997-06-09 AD 00 MANDATORY A/C *AD* AILERON/RUDDER TRIM CONTROL MODULE REPLACEMENT Closed 13.Jun.1997This document is applicable to LN# 1001-2311,2316,2349. All other LN#are Not Applicable per Boeing SB.1997-06-09 (ACTIVE)737-27A1198-R0 (ACTIVE)

ADSB

Perform within an unlimited threshold.1997-06-09/AD Rev.00 *AD* AILERON/RUDDER TRIM CONTROL MODULE REPLACEMENT Closed 13.Jun.1997> 737-27A1198/SB* Rev.00 *AD* AILERON/RUDDER TRIM CONTROL MODULE REPLACEMENT Closed 13.Jun.1997


13.Jun.1997PerfRev.:'NOTE' / Reason: PREVIOUSOPERATOR DOC.






23.Oct.2014Page 93/429

Document-Number Type Rev Compliance A|C Subject Status1997-08-01 AD 00 MANDATORY COMP FAN DISK INSPECTION, TO PREVENT LCF FAILURE Not Applicable

AD not apllicable, NAS engines operating in Cat B only.Status apply for EASA AD 1994-195.1997-08-01CFMI-TP.SM5

ADESM

00LAST


CFM56-3B2 / 724473 Pos=LH (KKM)Not Applicable / Reason: AUTOASSIGNED

335-014-511-0 / DC778241 Pos=LH (KKM)Not Applicable / Reason: OPERATING INCAT B ONLY

CFM56-3B2 / 725495 Pos=RH (KKM)Not Applicable / Reason: AUTOASSIGNED

335-014-511-0 / BC610516 Pos=RH (KKM)Not Applicable / Reason: OPERATING INCAT B ONLY

1997-09-14 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 2000-02-18 Superseded (Not Applicable)1997-09-14 (SUPERSEDED)2000-02-18 (ACTIVE)737-SL-27-030 (ACTIVE)

ADADSL


1997-09-15 AD 00 MANDATORY A/C *AD* ENGAGE SOLENOID VALVE OF THE YAW DAMPER - INSPECTION Superseded (Superseded)1997-09-15R1 (ACTIVE)AD 1997-09-15R1 (INSP)

ADTA






23.Oct.2014Page 94/429

Document-Number Type Rev Compliance A|C Subject Status1997-09-15 AD 01 MANDATORY A/C *AD* ENGAGE SOLENOID VALVE OF THE YAW DAMPER - INSPECTION Closed 21.Feb.1998

1997-09-15R1 (ACTIVE) ADThis Document SUPERSEDES 1997-09-15/AD Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

21.Feb.1998PerfRev.:'NOTE' / Reason: DELIVERYDOC.


1997-11-10 AD 00 MANDATORY A/C SERIES 174290 CONSTANT FLOW AIRL. PORTABLE OXYGEN MASK Not ApplicableCompliance:AD § (a) and (b) is Not applicable due to the affected PN notinstalled on NAS B737.174290-35-1 (PURITAN BENNETT)1997-11-10 (ACTIVE)

SBAD






23.Oct.2014Page 95/429

Document-Number Type Rev Compliance A|C Subject Status1997-14-03 AD 00 MANDATORY A/C *AD* RUDDER PRESSURE REDUCER AND YAW DAMPER COUPLER INSTALL. Closed 26.Jul.2000

1997-14-03 ITEM A2 (ACTIVE)1998-02-01 (ACTIVE)2007-03-07 (ACTIVE)737-22-1124 R1 (ACTIVE)737-27A1206 R0 (REF)737-27A1206 R1 (REF)737-27A1206 R2 (REF)737-27A1206 R3 (ACTIVE)737-SL-27-119-C (REF)SBB 737-27A1206 (MAINT TASK)

ADADADSBSBSBSBSBSLTA

Perform BEFORE 01.Aug.20001997-14-03/AD Rev.00 *AD* RUDDER PRESSURE REDUCER AND YAW DAMPER COUPLER INSTALL. Closed 26.Jul.2000> 737-22-1124/SB* Rev.01 AUTOFLIGHT - AUTOPILOT - YAW DAMPER SYSTEM - YAW DAMPER COUPLER AND

RUDDER POWER CONTROL UNIT (PCU) WIRING CHANGEClosed 11.Feb.1999


11.Feb.1999PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:


> 737-22-1124/SB* Rev.00 *AD* Y/D SYSTEM COUPLER & RUDDER POWER CONTROL WIRING CHANGE SupersededThis Document has been SUPERSEDED BY 737-22-1124/SB Rev.01

> 737-27A1206/SB* Rev.03 *AD* RUDDER PRESSURE REDUCER AND YAW DAMPER COUPLER INST. Closed 26.Jul.2000Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

26.Jul.2000PerfRev.:'NOTE' / Reason: DELIVERYDOCS.

Reason for this StatusDELIVERY DOCS.





23.Oct.2014Page 96/429

Document-Number Type Rev Compliance A|C Subject Status1997-14-04 AD 00 MANDATORY A/C *AD* RUD. PCU DUAL SERVO VALVE AND DUAL LOADPATH BOLT REPL. Closed 21.Feb.1998

AMOC approves the use of SL 737-27-119 for leak test.The leak test is mandated by AD§a

SB 737-27A1202:This modification is applicable to LN# 1-2914. The following LN# areNot Applicable per PRR35365 and PRR38060-6.

This modification is mandated by AD 1997-14-04 §c.

SB 737-27-1185:This modification is applicable for LN# 1-2453. The following LN# areNot Applicable ref PRR35153.

This modification is mandated by AD 1997-14-04 §b.

Incorperating the mandated modifications per AD 2007-03-07 ends therequirement of this AD. Ref AD 2007-03-07 § (b).130S-03-04411994-01-07 (SUPERSEEDED)1996-23-51 (SUPERSEEDED)1997-14-04 (ACTIVE)35365 (PRODUCTION)38060-6 (PRODUCTION)737-27A1202 R0 (REF)737-27A1202 R1 (REF)737-27A1202 R2 (REF)737-27A1202 R3 (REF)737-SL-27-119-B (ACTIVE)99-130S-0367

AMOCADADADPRRPRRSBSBSBSBSLAMOC

00

00This Document SUPERSEDES 1994-01-07/AD Rev.00





23.Oct.2014Page 97/429

Document-Number Type Rev Compliance A|C Subject StatusPerform BEFORE 04.Aug.1999

1997-14-04/AD Rev.00 *AD* RUD. PCU DUAL SERVO VALVE AND DUAL LOADPATH BOLT REPL. Closed 21.Feb.1998This Document SUPERSEDES 1994-01-07/AD Rev.00

> 737-27-1185/SB* Rev.00 RUDDER POWER CONTROL UNIT-SERVO VALVE REPLACEMENT Not Applicable / Special Text: ThisAircraft is Not Applicable due toPRODUCTION LINE PRR35153

This Document has been SUPERSEDED BY 737-27-1185/SB Rev.01Reason for this StatusSBB 737-27A1202

> 737-27A1202/SB* Rev.02 *AD* RUDDER PCU DUAL SERVO VALVE AND DUAL LOADPATH BOLT REPL Closed 21.Feb.1998Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-SL-27-119/SL Rev.C *AD* RUDDER POWER CONTROL UNIT (PCU) INTERNAL LEAK TEST Not Applicable> > SLB-27-119/EO* Rev.00 RUDDER POWER CONTROL UNIT (PCU) INTERNAL LEAK TEST Not Applicable


1997-15-06 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 1998-03-10 Superseded (Not Applicable)1997-15-06 (SUPERSEDED)1998-03-10 (ACTIVE)737-25A1334-R1 (ACTIVE)PRODUCTION PRR35005-158R

ADADSBPRR






23.Oct.2014Page 98/429

Document-Number Type Rev Compliance A|C Subject Status1997-18-03 AD 00 MANDATORY A/C PURITAN-BENNETT AERO SYSTEMS CO., CONE AND SEAL ASSEMBL Not Applicable

Compliance:AD § (a) is Not applicable due to the affected PN not installed onNAS B737.1997-18-03 (ACTIVE)3500-97-14 (REF)

ADSB


1997-18-06 AD 00 MANDATORY A/C *AD* AIRPLANE MAINTENANCE PROGRAM REVISION - MAIN WHEEL WELL Information OnlyAMM has been revised refer to AMM task 12-40-00-102-001, specificallyPara G.1997-18-06 ADReason for this StatusAUTO ASSIGNED





23.Oct.2014Page 99/429

Document-Number Type Rev Compliance A|C Subject Status1997-19-03 AD 00 MANDATORY A/C *AD* CAPTAIN & F/O CREW SEATS - INSPECTION/MODIFICATION Closed 12.Dec.1997

1997-19-03 (ACTIVE)93-15-08 R1 (SUPERSEDED)IPECO SB A001-25-74 R2 (REF)IPECO SB A001-25-92-R2 (REF)SB A001-25-92 (MOD-TASK)

ADADSBSBTA


1997-19-03/AD Rev.00 *AD* CAPTAIN & F/O CREW SEATS - INSPECTION/MODIFICATION Closed 12.Dec.1997This Document SUPERSEDES 1993-15-08/AD Rev.01

> A001-25-92/SB* Rev.00 *AD* CAPTAIN & F/O CREW SEATS - INSPECTION/MODIFICATION Closed 12.Dec.1997Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

12.Dec.1997PerfRev.:'NOTE' / Reason: MALEVENGINEERING DOC.

Reason for this StatusMALEV ENGINEERING DOC.

1997-22-07 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 2002-07-08 Superseded (Not Applicable)1997-22-07 (SUPERSEDED)2002-07-08 (ACTIVE)737-53A1177-R6 (REF)737-SL-53-063-A (REF)737-SL-53-063-B (REF)

ADADSBSLSL

This Document SUPERSEDES 1994-25-05/AD Rev.00This Document has been SUPERSEDED BY 2002-07-08/AD Rev.00Reason for this StatusSUPERSEDED BY AD 2002-07-08





23.Oct.2014Page 100/429

Document-Number Type Rev Compliance A|C Subject Status1997-25-51 AD 00 MANDATORY COMP STARTER GEARSHAFT REPLACEMENT/TO PREVENT INFL SHUTDOWNS Superseded (Not Applicable by

Serial Number)1998-10-113-72-08633-72-08653-72-08733-72A0861CFMI-TP.PC.8CFMI-TP.SM.5T97-25-51

ADSBSBSBSBIPCESMAD

0001LAST0103LASTLASTLAST

This Document has been SUPERSEDED BY 1998-10-11/AD Rev.00Affected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 724473 Pos=LH (KKM) Not ApplicableCFM56-3B2 / 725495 Pos=RH (KKM) Not Applicable

1997-26-01 AD 00 MANDATORY A/C *AD* AUX RUDDER POWER CONTROL UNIT INSP., TEST & REPLACEMENT Closed 08.Feb.2000Applicable to LN#: 1-2814

L/N 1729 (LN-KKS) addressed on seperate effectivity line to allow forlink to DFP (Added by 14083)1997-26-01 (ACTIVE)AD-1997-26-01 (MOD-TASK)DOWTY (SMITHS) SB 1150-27-04

ADTASB


08.Feb.2000PerfRev.:'NOTE' / Reason: DELIVERYDOCS

Reason for this StatusDELIVERY DOCS





23.Oct.2014Page 101/429



ADAD


1998-02-01 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 2007-03-07 Superseded (Not Applicable)1998-02-01 (SUPERSEDED)2002-20-07 (SUPERSEDED)2007-03-07 (ACTIVE)737-27A1206-R1 (ACTIVE)

ADADADSB


1998-02-51 AD 00 MANDATORY A/C *AD* HORIZON. STABILIZER - INSP. FOR LOOSE/MISSING FASTENERS Not ApplicableThis document is applicable to LN# 2765-2980. All other LN# are NotApplicable per Boeing SB.1998-02-51 (ACTIVE)737-55A1060-R0 (REF)737-55A1060-R1 (ACTIVE)SBB 737-55A1060 (MOD-TASK)

ADSBSBTA

1998-02-51/AD Rev.00 *AD* HORIZON. STABILIZER - INSP. FOR LOOSE/MISSING FASTENERS Not Applicable> 737-55A1060/SB* Rev.01 *AD* HORIZON. STABILIZER - INSP. FOR LOOSE/MISSING FASTENERS Not Applicable by Serial Number

1998-03-09 AD 00 MANDATORY A/C AILERON - INSPECTION AND REPLACEMENT Not ApplicableThis Document SUPERSEDES 1997-26-04/AD Rev.00Reason for this StatusNOT APPLICABLE DUE TO CONFIG./PART NOT INSTALLED, REF DELIVERY DOC





23.Oct.2014Page 102/429

Document-Number Type Rev Compliance A|C Subject Status1998-03-10 AD 00 MANDATORY A/C *AD* OPERATIONAL TEST OF THE PILOT SEAT AND THE SEAT LOCKS Closed 24.Jul.1997

1997-15-06 (SUPERSEDED)1998-03-10 (ACTIVE)737-25A1334-R1 (ACTIVE)PRODUCTION PRR35005-158R

ADADSBPRR


1998-03-10/AD Rev.00 *AD* OPERATIONAL TEST OF THE PILOT SEAT AND THE SEAT LOCKS Closed 24.Jul.1997This Document SUPERSEDES 1997-15-06/AD Rev.00

> 737-25-1334/SB* Rev.00 *AD* FLIGHT COM. EQUIPMENT - EXAMINE SEAT TRACK ALIGNMENT Closed 24.Jul.1997Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

24.Jul.1997PerfRev.:'NOTE' / Reason: DELIVERYDOC.


> 737-25-1334/SB* Rev.01 FLIGHT COMPARTMENT EQUIPMENT - EXAMINE SEAT TRACK ALIGNMENT Closed 24.Jul.1997Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks24.Jul.1997 PerfRev.:'NOTE' / Reason: DEL DOCSReason for this StatusDEL DOCS

1998-04-41 AD 00 MANDATORY A/C *AD* MAIN DECK CARGO DOOR - HINGE INSPECTION Not ApplicableAD not effective for NAS. No cargo AC in fleet.1998-04-41 AD





23.Oct.2014Page 103/429

Document-Number Type Rev Compliance A|C Subject Status1998-07-02 AD 00 MANDATORY COMP HPC STG 1 & 2 SPOOLS - REM. FROM SERVICE Not Applicable

Status apply for EASA AD 1998-080.3-72-0856CFMI-TP.PC.8CFMI-TP.SM.5

SBIPCESM

00LASTLAST

Perform within an unlimited threshold.1998-07-02/AD Rev.00 HPC STG 1 & 2 SPOOLS - REM. FROM SERVICE Not Applicable> 3-72-0856/SB* Rev.00 HPCR STAGE 1-2 HPC STG 1 & 2 SPOOLS - REM. FROM SERVICE Not Applicable by Serial Number

Affected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 724473 Pos=LH (KKM) Not Applicable1589M66G02 / GWN0AJ7J Pos=RH (KKM) Not ApplicableCFM56-3B2 / 725495 Pos=RH (KKM) Not Applicable





23.Oct.2014Page 104/429

Document-Number Type Rev Compliance A|C Subject Status1998-07-16 AD 00 MANDATORY A/C *AD* STDB HYDRAULIC SYSTEM MODIFICATIONS Closed 23.Feb.2000

SB 737-29-1070:This modification is applicable to LN# 1001-2720. The following LN#are Not Applicable per PRR35005-109.

SB 737-29-1071:This modification is applicable to LN# 1001-2791. The following LN#are Not Applicable per PRR35005-109.1998-07-16 (ACTIVE)737-29-1070 (REF)737-29-1070 NSC 1 (ACTIVE)PRODUCTION PRR35005-109SBB 737-29-1070 (MANIT TASK)SBB 737-29-1071 (ACTIVE)SBB 737-29-1071 (MAINT TASK)

ADSBSBPRRTASBTA

Perform BEFORE 4000/H1998-07-16/AD Rev.00 *AD* STDB HYDRAULIC SYSTEM MODIFICATIONS Closed 23.Feb.2000> 737-29-1070/SB* Rev.00 *AD* REV OF THE STDB SYS HYDR LEADING EDGE FLOW RESTRICTOR Closed 23.Feb.2000




> 737-29-1071/SB* Rev.00 *AD* HYDRAULIC FUSES IN THE STANDBY SYSTEM REPLACEMENT Closed 13.Mar.1999Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







23.Oct.2014Page 105/429

Document-Number Type Rev Compliance A|C Subject Status1998-096 AD B MANDATORY COMP ACCESSORY GEAR BOX (AGB) AND TRANSFER GEAR BOX (TGB) Not Applicable

3-72-08613-72-08633-72-08653-72-0873

SBSBSBSB

LAST01LAST01

Perform within an unlimited threshold.1998-096/AD Rev.B ACCESSORY GEAR BOX (AGB) AND TRANSFER GEAR BOX (TGB) Not Applicable> 1998-096-01/EO* Rev.B ACCESSORY GEAR BOX (AGB) AND TRANSFER GEAR BOX (TGB) Not Applicable by Serial Number

Affected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 724473 Pos=LH (KKM) Not ApplicableCFM56-3B2 / 725495 Pos=RH (KKM) Not Applicable

> 1998-096-02/EO* Rev.B ACCESSORY GEAR BOX (AGB) AND TRANSFER GEAR BOX (TGB) Not Applicable by Serial NumberAffected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 724473 Pos=LH (KKM) Not ApplicableCFM56-3B2 / 725495 Pos=RH (KKM) Not Applicable

> 1998-096-03/EO* Rev.B ACCESSORY GEAR BOX (AGB) AND TRANSFER GEAR BOX (TGB) Not Applicable by Serial NumberAffected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 725495 Pos=RH (KKM) Not ApplicableCFM56-3B2 / 724473 Pos=LH (KKM) Not Applicable

> 1998-096-04/EO* Rev.B ACCESSORY GEAR BOX (AGB) AND TRANSFER GEAR BOX (TGB) Not Applicable by Serial NumberAffected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 724473 Pos=LH (KKM) Not ApplicableCFM56-3B2 / 725495 Pos=RH (KKM) Not Applicable

> 1998-096-05/EO* Rev.B ACCESSORY GEAR BOX (AGB) AND TRANSFER GEAR BOX (TGB) Not Applicable by Serial NumberAffected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 725495 Pos=RH (KKM) Not ApplicableCFM56-3B2 / 724473 Pos=LH (KKM) Not Applicable





23.Oct.2014Page 106/429

Document-Number Type Rev Compliance A|C Subject Status1998-10-11 AD 00 MANDATORY COMP STARTER GEARSHAFT REPLACEMENT/TO PREVENT INFL SHUTDOWNS Not Applicable

Status apply for EASA AD 1998-096.1998-10-113-72-08633-72-08653-72-08733-72A0861CFMI-TP.PC.8CFMI-TP.SM.5T97-25-51

ADSBSBSBSBIPCESMAD

0001LAST0103LASTLASTLAST

This Document SUPERSEDES 1997-25-51/AD Rev.001998-10-11/AD Rev.00 STARTER GEARSHAFT REPLACEMENT/TO PREVENT INFL SHUTDOWNS Not Applicable

This Document SUPERSEDES 1997-25-51/AD Rev.00> 3-72-0863/SB* Rev.01 STARTER GEARSHAFT REPLACEMENT Not Applicable by Serial Number

Affected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 725495 Pos=RH (KKM) Not ApplicableCFM56-3B2 / 724473 Pos=LH (KKM) Not Applicable

> 3-72-0867/SB* Rev.00 ENGINE TRANSFER GEARBOX BEVEL GEAR REPLACEMENT Not Applicable by Serial NumberAffected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 725495 Pos=RH (KKM) Not ApplicableCFM56-3B2 / 724473 Pos=LH (KKM) Not Applicable

1998-11-51 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 1999-21-15 Superseded (Not Applicable)1998-11-52 (SUPERSEDED)1999-21-15 (ACTIVE)737-28A1120-R0 (REF)AD 1998-11-51 (SUPERSEDED)

ADADSBAD






23.Oct.2014Page 107/429

Document-Number Type Rev Compliance A|C Subject Status1998-11-52 AD 00 MANDATORY A/C *AD* FUEL PUMP WIRING (SUPERSEDED BY AD 99-21-15) Superseded (Not Applicable)

1998-11-52 (SUPERSEDED)1999-21-15 (ACTIVE)737-28A1120-R0 (REF)

ADADSB


1998-12-32 AD 00 MANDATORY COMP HPTR DISK INSPECTION Closed 14.Mar.2008Status apply for EASA AD 1997-327.1998-12-323-72-0843

ADSB

0001

Perform BEFORE 03.Sep.19981998-12-32/AD Rev.00 HPTR DISK INSPECTION Closed 14.Mar.2008> 3-72-0843/SB* Rev.01 HPTR DISK INSPECTION Closed 14.Mar.2008


CFM56-3B2 / 725495 Pos=RH (KKM)Closed / Last Performed:14.Mar.200853354:00/H 29781/C RefDocument:NA,MTU WO 51 .684.400 Rev.01

CFM56-3B2 / 724473 Pos=LH (KKM)Closed / Last Performed:17.Jan.200542076:00/H 21463/C RefDocument:NA,NEC WO E724473-02 Rev.01





23.Oct.2014Page 108/429

Document-Number Type Rev Compliance A|C Subject Status1998-13-12 AD 01 MANDATORY A/C *AD* RUDDER PEDAL PUSHROD FASTENES, INSP FOR CORRECT INST. Closed 14.Jul.1998

1998-13-12 (SUPERSEDED)1998-13-12-R1 (ACTIVE)737-27A1212-R0 (REF)737-27A1212-R1 (ACTIVE)

ADADSBSB

Perform BEFORE 04.Oct.19981998-13-12/AD Rev.01 *AD* RUDDER PEDAL PUSHROD FASTENES, INSP FOR CORRECT INST. Closed 14.Jul.1998> 737-27A1212/SB* Rev.01 *AD* RUDDER PEDAL PUSHROD FASTENES, INSP FOR CORRECT INSTALL Closed 14.Jul.1998




1998-18-20 AD 00 MANDATORY COMP *AD* REPLM. OF ACTUATOR ON FUEL SYSTEM ENG/CROSSFEED VALVE Not Applicable by Serial NumberNot applicable per SB effectivity.AD only applicable to PN 40574-2 and -5.

SB 61163-28-09 required to be performed by AD was incorporated intoCMM 28-20-33 on May 1st 1996. All valves installed by NAS have beenmaintained by CMM revisions after this date.1995-15-06 (SUPERSEDED)1998-18-20 (ACTIVE)28-20-33J.C. CARTER 6113-28-09 (REF)

ADADCMMSB

3

Affected Rotables (Part No/Serial No/Position) Status40574-4 / 4694 Pos=CTR (KKM) Not Applicable40574-4 / 6929 Pos=LH (KKM) Not Applicable40574-4 / 6509 Pos=RH (KKM) Not Applicable





23.Oct.2014Page 109/429

Document-Number Type Rev Compliance A|C Subject Status1998-19-09 AD 00 MANDATORY A/C *AD* FUEL PUMP WIRING (SUPERSEDED BY AD 99-21-15) Superseded (Not Applicable)

1998-19-09 (SUPERSEDED)1999-21-15 (ACTIVE)737-28A1120-R0 (REF)

ADADSB


1998-19-10 AD 00 MANDATORY COMP ACCESSORY GEARBOX STARTER GEAR SHAFT FAILURE. Not ApplicableStatus apply for EASA AD 1998-198.3-72-0877 SB 03Perform within an unlimited threshold.

1998-19-10/AD Rev.00 ACCESSORY GEARBOX STARTER GEAR SHAFT FAILURE. Not Applicable> 3-72-0877/SB* Rev.01 ACCESSORY GEARBOX STARTER GEAR SHAFT FAILURE. Not Applicable


CFM56-3B2 / 725495 Pos=RH (KKM)Not Applicable / Reason: NA PER ESN,DELIVERY MSN:24676 39730

CFM56-3B2 / 724473 Pos=LH (KKM)Not Applicable / Reason: NA PER ESN,SHOP VISIT 2005 39729





23.Oct.2014Page 110/429

Document-Number Type Rev Compliance A|C Subject Status1998-22-10 AD 00 MANDATORY A/C *AD* FUSELAGE - FWD SERVICE DOORWAY AFT FRAME INSP. & REPAIR Not Applicable

This document is applicable to LN# 1-1426. The following LN# are NotApplicable per PRR34320R.1998-22-10 (ACTIVE)737-53-1108-R0 (REF)737-53-1108-R1 (REF)737-53-1108-R2 (REF)737-53-1108-R3 (REF)737-53-1108-R4 (REF)737-53-1108-R5 (ACTIVE)PRODUCTION PRR34320R

ADSBSBSBSBSBSBPRR

This Document SUPERSEDES 1988-03-03/AD Rev.001998-22-10/AD Rev.00 *AD* FUSELAGE - FWD SERVICE DOORWAY AFT FRAME INSP. & REPAIR Not Applicable

This Document SUPERSEDES 1988-03-03/AD Rev.00> 737-53A1108/SB* Rev.05 *AD* FUSELAGE - FWD SERVICE DOORWAY AFT FRAME INSP. & REPAIR Not Applicable by Serial Number

This Document has been SUPERSEDED BY 737-53A1108/SB Rev.06

1998-24-27 AD 00 MANDATORY A/C *AD* TOILET COMPARTMENT FIRE EXTINGUISHERS Not ApplicableNot applicable due to affected First Technology Fire and Safety Ltd.toilet compartment fire extinguisher not installed on NAS B737.1998-24-27 (ACTIVE)26-110 (REF)

ADSB






23.Oct.2014Page 111/429

Document-Number Type Rev Compliance A|C Subject Status1998-25-06 AD 00 MANDATORY A/C *AD* CARGO DOOR AFT - FRAME & BEAM INSPECTION, REPAIR & MOD (SUPERSEDED

BY AD 2000-06-13)Superseded (Not Applicable bySerial Number)

mandated by AD 1998-25-06 (SUPERSEDED)1998-25-06 (SUPERSEDED)2000-06-13 (SUPERSEDED)2000-06-13-R1 (ACTIVE)737-52A1079-R0 (REF)737-52A1079-R1 (REF)737-52A1079-R2 (REF)737-52A1079-R3 (REF)737-52A1079-R4 (REF)737-52A1079-R5 (REF)737-52A1079-R6 (REF)

ADADADSBSBSBSBSBSBSB

000100010203040506


1998-25-10 AD 00 MANDATORY A/C *AD* AIRCRAFT BELTS, INC. Superseded (Superseded)Not applicable to NAS due to; affected PN not installed.1998-25-10-R1 (ACTIVE) ADThis Document has been SUPERSEDED BY 1998-25-10/AD Rev.01

1998-25-10 AD 01 MANDATORY A/C *AD* AIRCRAFT BELTS, INC. Not ApplicableNot applicable to NAS due to; affected PN not installed.1998-25-10-R1 (ACTIVE) ADThis Document SUPERSEDES 1998-25-10/AD Rev.00Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 112/429

Document-Number Type Rev Compliance A|C Subject Status1999-01-16 AD 00 MANDATORY A/C *AD* PASSENGER WATER SYSTEM - IN FLIGHT POTABLE WATER CHANGE Closed 31.Jan.2002

1999-01-16 (ACTIVE)1999-01-16 XA (ACTIVE)1999-01-16 XB (ACTIVE)737-38-1043-R0 (REF)737-38-1043-R1 (REF)737-38-1043-R2 (ACTIVE)PRODUCTION PRR35005-182SBB 737-38-1043WP1 (MOD-TASK)

ADADADSBSBSBPRRTA

Perform within an unlimited threshold.1999-01-16/AD Rev.00 *AD* PASSENGER WATER SYSTEM - IN FLIGHT POTABLE WATER CHANGE Closed 31.Jan.2002> 737-38-1043WP1/SB* Rev.00 *AD* POTABLE WATER DRAINAGE - INSTRUCTION PLACKARD INSTALL Closed 28.Jul.1998

This Document has been SUPERSEDED BY 737-38-1043WP1/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-38-1043WP1/SB* Rev.01 *AD* POTABLE WATER DRAINAGE - INSTRUCTION PLACKARD INSTALL See prev. DocstatusThis Document SUPERSEDES 737-38-1043WP1/SB Rev.00This Document has been SUPERSEDED BY 737-38-1043WP1/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks28.Jul.1998 PerfRev.:'NOTE'Reason for this StatusDELIVERY DOC.

> 737-38-1043WP1/SB* Rev.02 *AD* POTABLE WATER DRAINAGE - INSTRUCTION PLACKARD INSTALL See prev. DocstatusThis Document SUPERSEDES 737-38-1043WP1/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks28.Jul.1998 PerfRev.:'NOTE'Reason for this StatusDELIVERY DOC.





23.Oct.2014Page 113/429

Document-Number Type Rev Compliance A|C Subject Status> 737-38-1043WP2/SB* Rev.01 *AD* POTABLE WATER DRAINAGE - VALVE INSTALLATION Closed 31.Jan.2002

This Document SUPERSEDES 737-38-1043WP2/SB Rev.00This Document has been SUPERSEDED BY 737-38-1043WP2/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

31.Jan.2002PerfRev.:'NOTE' / Reason: DELIVERYDOC.


> 737-38-1043WP2/SB* Rev.00 *AD* POTABLE WATER DRAINAGE - VALVE INSTALLATION SupersededThis Document has been SUPERSEDED BY 737-38-1043WP2/SB Rev.01

> 737-38-1043WP2/SB* Rev.02 *AD* POTABLE WATER DRAINAGE - VALVE INSTALLATION See prev. DocstatusThis Document SUPERSEDES 737-38-1043WP2/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks31.Jan.2002 PerfRev.:'NOTE'Reason for this StatusDELIVERY DOC.

1999-01-16 XA AD 00 MANDATORY A/C POTABLE WATER DRAINAGE - INSTRUCTION PLACKARD INSTALLATION Closed 28.Jul.19981999-01-16 (ACTIVE)35005-182 (PRODUCTION)737-38-1043 (REF)737-38-1043 R1 (REF)737-38-1043 R2 (REF)SBB 737-38-1043WP1 (MAINT TASK

ADPRRSBSBSBTA


28.Jul.1998PerfRev.:'NOTE' / Reason: DELIVERYDOC






23.Oct.2014Page 114/429

Document-Number Type Rev Compliance A|C Subject Status1999-01-16 XB AD 00 MANDATORY A/C POTABLE WATER DRAINAGE - ISOLATION VALVE INSTALATTION Closed 31.Jan.2002

1999-01-16 (REF)35005-182 (PRODUCTION)737-38-1043 (REF)737-38-1043 R1 (REF)737-38-1043 R2 (REF)AD 1999-01-16 XB (ACTIVE)SBB 737-38-1043WP2 (MAINT TASK

ADPRRSBSBSBADTA


31.Jan.2002PerfRev.:'NOTE' / Reason: DELIVERYDOC






23.Oct.2014Page 115/429

Document-Number Type Rev Compliance A|C Subject Status1999-03-04 XA AD 00 MANDATORY A/C *AD* FUEL QTY SYSTEM PROVIDE SHIELDING AND WIRE SEPARATION Taskcard Controlled

FAA AMOC letter informs that STC ST00127BO is an AMOC to AD 1999-03-0405-1032 (ACTIVE)130S-00-0632737-28-1156-R1 (ACTIVE)737-28-1157-R0 (ACTIVE)737-28-1186-R2 (ACTIVE)ST00146BO (ACTIVE)ST00847SE (ACTIVE)T3031-0012-0101 (ACTIVE)

TDAMOCSBSBSBSTCSTCDWG

0000010202000000

Perform BEFORE 09.Mar.20031999-03-04 XA/AD Rev.00 *AD* FUEL QTY SYSTEM PROVIDE SHIELDING AND WIRE SEPARATION Taskcard Controlled> 737-28-1156/SB* Rev.01 *AD* SMITHS TRANSIENT SUPPRESSION UNIT (TSU) INSTALLATION Not Applicable

Reason for this StatusSBB 737-28-1157

> 737-28-1157/SB Rev.00 *AD* BF GOODRICH TRANSIENT SUPPRESION DEVICE (TST) INSTALL. Taskcard Controlled> > 737-28-1157-01/EO* Rev.01 *AD* BF GOODRICH TRANSIENT SUPPRESION DEVICE (TST) INSTALL. Closed 14.Mar.2003


14.Mar.2003 42144:00/H 19904/CMALEVEO:737-28-0043/SB28-1157

> > 737-28-1157MPD/EO*Rev.00

737-28-1157MPD CONTROLLED BY MPD TASKS Taskcard Controlled

Carried out on the following TaskcardsTaskcard: NAS-2841-006 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks05.04.2019 88'534/H 15212:25/H Interval:24000/HPerf Dim1 (D) Perf Dim2 Perf Dim306.07.2011 64534:00/H 37798/CCarried out on the following TaskcardsTaskcard: NAS-2841-007 Maint. Progr.: AMP 737-CL





23.Oct.2014Page 116/429

Document-Number Type Rev Compliance A|C Subject StatusExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks10.02.2017 81'168/H 7846:25/H Interval:39000/HCarried out on the following TaskcardsTaskcard: NAS-2841-005 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks04.02.2015 04.Feb.2015104d, 6h Interval:365/DPerf Dim1 (D) Perf Dim2 Perf Dim304.02.2014 71572:00/H 43151/CReason for this StatusAUTO ASSIGNED

> 737-28-1186/SB* Rev.02 *AD* INST OF GOODRICH CORPORATION ISOLATED FUEL QUANTITY TX Not ApplicableReason for this StatusSBB 737-28-1157/STC ST00127BO





23.Oct.2014Page 117/429

Document-Number Type Rev Compliance A|C Subject Status1999-03-04 XB AD 00 MANDATORY A/C *AD* REPL OF THE FUEL VENT DOOR TO ADD A FLAME ARRESTOR Closed 28.Mar.2001

FAA AMOC letter informs that STC ST00127BO is an AMOC to AD 1999-03-04130S-00-0632 (ACTIVE)1999-03-04 (ACTIVE)1999-03-04 XB (ACTIVE)737-28-1026 (REF)737-28-1131-R3 (ACTIVE)PRODUCTION LINE PRR 35389-1R

AMOCADADSBSBPRR

Perform BEFORE 09.Mar.20021999-03-04 XB/AD Rev.00 *AD* REPL OF THE FUEL VENT DOOR TO ADD A FLAME ARRESTOR Closed 28.Mar.2001> 737-28-1131/SB* Rev.03 *AD* REPL OF THE FUEL VENT DOOR TO ADD A FLAME ARRESTOR Closed 28.Mar.2001


28.Mar.2001PerfRev.:'NOTE' / Reason: DELIVERYDOCS.

Reason for this StatusDELIVERY DOCS.

> SA00859SE/STC* Rev.00 FUEL - FUEL VENT SYSTEM - ADD FLAME ARRESTOR & PRESSURE RELI Not Applicable

1999-04-10 AD 00 MANDATORY A/C INSPECTION TO DETERMINE TYPE OF FLUORESCENT BALLASTS Not ApplicableAffected PN/Equipment not Installed on NAS Aircraft.1999-04-10 (ACTIVE) ADReason for this StatusAUTO ASSIGNED





23.Oct.2014Page 118/429

Document-Number Type Rev Compliance A|C Subject Status1999-04-23 AD 00 MANDATORY A/C *AD* FUSELAGE - FIN AFT, BOLT INSP. & REPLACEMENT Not Applicable

This document is Applicable to LN#: 1-1485. All other LN# are NotApplicable per Boeing SB.1999-04-23 (ACTIVE)737-53-1107 (REF)737-53-1107 R1 (REF)737-53-1107 R2 (REF)737-53-1107 R3 (REF)737-53-1107 R4 (ACTIVE)

ADSBSBSBSBSB

1999-04-23/AD Rev.00 *AD* FUSELAGE - FIN AFT, BOLT INSP. & REPLACEMENT Not Applicable> 737-53-1107/SB* Rev.00 *AD* FUSELAGE - FIN AFT, BOLT INSP. & REPLACEMENT Not Applicable by Serial Number

1999-05-12 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 2004-15-04 Superseded (Not Applicable)1999-05-12 (SUPERSEDED)2004-15-04 (ACTIVE)737-28A1132-R0 (REF)737-28A1132-R1 (REF)737-28A1132-R2 (ACTIVE)SBB 737-28A1132 (MOD-TASK)

ADADSBSBSBTA






23.Oct.2014Page 119/429


1999-05-15 (SUPERSEDED)2000-19-05 (ACTIVE)737-27A1205 (ACTIVE)737-SL-27-118-D (REF)

ADADSBSL


1999-08-16 AD 00 MANDATORY COMP SUPERSEDED BY AD 2000-12-01 Superseded (Superseded)SUPERSEDE BY 2000-12-01This Document has been SUPERSEDED BY 2000-12-01/AD Rev.00Affected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 725495 Pos=RH (KKM) SupersededCFM56-3B2 / 724473 Pos=LH (KKM) Superseded

1999-08-21 AD 00 MANDATORY A/C PREVENTION OF REDUCED OXYGEN CONSUMPTION ON PURITAN-BENNETTC351-2000 SERIES PASSENGER OXYGEN MASKS

Not Applicable

Compliance:Per AD § (a) Not applicable due to the affected Puritan-BennettC351-2000 seriespassenger oxygen masks and portable oxygen masks notinstalled on NAS B737.1999-08-21 (ACTIVE)C-351-2000-35-1 (REF)

ADSB






23.Oct.2014Page 120/429

Document-Number Type Rev Compliance A|C Subject Status1999-08-23 AD 00 MANDATORY A/C *AD* BS 1016 AFT PRESS. BULKHEAD - INSPECTION FOR WEB CRACK Superseded (Closed 13.Nov.2012)

1999-08-23 (ACTIVE)37-SBB-53A1214-1A (REP TASK)37-SBB-53A1214-1F (REP TASK)37-SBB-53A1214-3 (REP TASK)737-53A1214 (REF)737-53A1214 R1 (REF)737-53A1214 R2 (REF)SBB 737-53A1214 (MAINT TASK)

ADTATATASBSBSBTA

This Document has been SUPERSEDED BY 2012-18-13/AD Rev.00Perform BEFORE 25750/C

1999-08-23/AD Rev.00 *AD* BS 1016 AFT PRESS. BULKHEAD - INSPECTION FOR WEB CRACK Closed 13.Nov.2012This Document has been SUPERSEDED BY 2012-18-13/AD Rev.00

> 737-53A1214/SB Rev.02 *AD* BS 10016 AFT PRESS. BULKHEAD - INSPECTION FOR WEB CRACK Closed 13.Nov.2012This Document has been SUPERSEDED BY 737-53A1214/SB Rev.03

> > 737-53A1214-01/EO* Rev.00 BS 1016 AFT PRESS. BULKHEAD - INSPECTION FOR WEB CRACK Closed 16.Feb.2002Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

16.Feb.2002DELIVERYDOC.

> > 737-53A1214-1A/EO* Rev.00 NDT INSPECTION OF WEB AT "Y" CHORD - ABOVE S-15L/R AFT *** MANDATORYREPETITIVE NDT INSPECTION AFT SIDE ***

Cancelled

This Document has been SUPERSEDED BY 737-53A1214-1A1/EO Rev.00This Document has been SUPERSEDED BY 737-53A1214-1A2/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks08.Nov.2012 68139:00/H 40570/C 354128, N/A Was due at: 41126/C PerfRev.:'00'Reason for this StatusManually deassigned after Document Cancelled or Superseded

> > 737-53A1214-1F/EO* Rev.00 NDT INSPECTION OF WEB AT "Y" CHORD - ABOVE S-15L/R FWD *** MANDATORYREPETITIVE NDT INSPECTION FWD SIDE ***

Cancelled

This Document has been SUPERSEDED BY 737-53A1214-1F1/EO Rev.00This Document has been SUPERSEDED BY 737-53A1214-1F2/EO Rev.00





23.Oct.2014Page 121/429

Document-Number Type Rev Compliance A|C Subject StatusPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

24.Mar.2010 60867:00/H 35008/CPerfRev.:'NOTE' / Reason: AMICOS WO510114 2-INSPHEAVY-SERV-12YR/SI/CPCP.NA

Reason for this StatusManually deassigned after Document Cancelled or Superseded

> > 737-53A1214-3/EO* Rev.00 NDT INSPECTION OF WEB AT "Y" CHORD - BELOW S-15L/R *** MANDATORYREPETITIVE NDT INSPECTION AFT SIDE ***

Cancelled

This Document has been SUPERSEDED BY 737-53A1214-3A/EO Rev.00This Document has been SUPERSEDED BY 737-53A1214-3F/EO Rev.00Reason for this StatusManually deassigned after Document Cancelled or Superseded





23.Oct.2014Page 122/429

Document-Number Type Rev Compliance A|C Subject Status1999-10-12 AD 00 MANDATORY COMP *AD* MLG - ACTUATOR BEAM ARM INSPECTION/OVERHAUL/REWORK/REPL Repetitive

FAA AMOC letter approves the use of Rev 01 of SB 737-32A1314 as anAMOC to AD 1999-10-12.120S-10-531 (ACTICE)1991-05-16 (SUPERSEDED)1999-10-12 (ACTIVE)37-SBB-32A1314 (REPETITIVE)37-SBB-32A1314-1(REPETITIVE)37-SBB-32A1314-2 (OVERHAUL)737-32A1224-R3 (REF)737-32A1314 IN 01737-32A1314-R1 (ACTIVE)737-SRP-32-0094 (REF)

AMOCADADTATATASBSBSBSRP

NA


1999-10-12/AD Rev.00 *AD* MLG - ACTUATOR BEAM ARM INSPECTION/OVERHAUL/REWORK/REPL RepetitiveThis Document SUPERSEDES 1991-05-16/AD Rev.00

> 737-32A1314-04/EO* Rev.01 *AD* MLG - ACTUATOR BEAM ARM INSPECTION/OVERHAUL/REWORK/REPL Closed 08.Jul.2005 / Special Text:Component first OH per SB737A1314


65-46109-38 / SI10668 Pos=RH (KKM)

Closed / Special Text: Component first OHper SB737A1314 / Reason: LN-KKMEO403522 C/E04432 44495 / LastPerformed:08.Jul.2005 46143:00/H 23575/CRefDocument: Rev.NOTE

65-46109-38 / SI-10386 Pos=LH (KKM)

Closed / Special Text: Component first OHper SB737A1314 / Reason: LN-KKMEO403521 C/E0443275 44494 / LastPerformed:08.Jul.2005 46143:00/H 23575/CRefDocument: Rev.NOTE

> 737-32A1314-1/EO* Rev.01 MLG ACTUATOR BEAM ARM VISUAL AND AN NDT/ULTRASONIC INSP Repetitive





23.Oct.2014Page 123/429

Document-Number Type Rev Compliance A|C Subject StatusAffected Rotables (Part No/Serial No/Position) Status

65-46109-38 / SI10668 Pos=RH (KKM)Repetitive / Next Due:19.Jul.2019 / LastPerformed:05.Feb.2013 65993:00/H27014/C W/O:401271 Rev.01

65-46109-38 / SI-10386 Pos=LH (KKM)Repetitive / Next Due:30.Aug.2019 / LastPerformed:05.Feb.2013 58099:00/H32874/C W/O:401272 Rev.01

> 737-32A1314-2/EO* Rev.01 *AD*MLG ACTUATOR BEAM ARM REMOVE FOR OVERHAUL/RESTORA ** REPETITIVEOVERHAUL EVERY 10 YEARS **

Repetitive


65-46109-38 / SI10668 Pos=RH (KKM)

Repetitive / Next Due:17.Aug.2023 / LastPerformed:19.Aug.2013 27014/CRefDocument:FORM 20134302 OH SVRev.01

65-46109-38 / SI-10386 Pos=LH (KKM)

Repetitive / Next Due:28.Aug.2023 / LastPerformed:30.Aug.2013 27014/CRefDocument:FORM 20134473 OH SVRev.01





23.Oct.2014Page 124/429

Document-Number Type Rev Compliance A|C Subject Status1999-10-13 AD 00 MANDATORY A/C S245 FLAP LIMIT SWITCH INSPECTION AND R850 RELAY INST. Not Applicable

Apllicability:CL:This document is Applicable to LN#: 2997-3108. All other LN# are NotApplicable per PRR 38030-31.

NG:This document is Applicable to LN#: 1-268.

Compliance:AD § (a) is complied with through SB 737-27A1227 (CL) and SB737-27A1228 (NG).1999-10-13 (ACTIVE)737-27A1227-R3 (ACTIVE-CL)737-27A1228-R3 (ACTIVE-NG)737-SRP-27-0114 (REF)FAA LETTER 99-130S-496PRODUCTION LINE PRR38060-31

ADSBSBSRPAMOCPRR

000303000000

1999-10-13/AD Rev.00 S245 FLAP LIMIT SWITCH INSPECTION AND R850 RELAY INST. Not Applicable> 737-27A1227/SB* Rev.03 *AD* FLIGHT CONTROLS - FLAP LIMIT SWITCH INSP. & RELAY INST Not Applicable by Serial Number

This Document SUPERSEDES 737-27A1227/SB Rev.02> 737-27A1227/SB* Rev.02 *AD* FLIGHT CONTROLS - FLAP LIMIT SWITCH INSP. & RELAY INST Not Applicable by Serial Number

This Document has been SUPERSEDED BY 737-27A1227/SB Rev.03





23.Oct.2014Page 125/429

Document-Number Type Rev Compliance A|C Subject Status1999-11-05 AD 00 MANDATORY A/C *AD* MAIN RUDDER POWER CONTROL UNIT - SECONDARY SLIDE Closed 17.Mar.2005

Per AD 2007-03-07:If AD 2007-03-07 is done, the requirements of AD 1999-11-05 areended. The requirem ent for repetitive testing is therefore ended.1999-11-05 (SUPERSEDED)2002-20-07 (SUPERSEDED)2007-03-07 (ACTIVE)737-27A1221-R1 (ACTIVE-CL)737-27A1222-R1 (ACTIVE-NG)PRODUCTION LINEPRR35005-224-R (CL)PRODUCTION LINE PRR38357-R(NG)

AD

AD

AD

SB

SB

PRR

PRR

00

00


1999-11-05/AD Rev.00 *AD* MAIN RUDDER POWER CONTROL UNIT - SECONDARY SLIDE Closed 17.Mar.2005This Document SUPERSEDES 1995-06-53/AD Rev.00

> 737-27A1221/SB Rev.01 *AD* RUDDER PCU SECONDARY SLIDE - DISPLACEMENT TEST Closed 17.Mar.2005> > 737-27A1221/EO* Rev.00 *AD* RUDDER PCU SECONDARY SLIDE - DISPLACEMENT TEST Not Applicable by Serial Number> > 737-27A1221-01/EO* Rev.00 *AD* RUDDER PCU SECONDARY SLIDE - DISPLACEMENT TEST Closed 17.Mar.2005

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Mar.2005 PerfRev.:'NOTE' / Reason: KKM 150404Reason for this StatusKKM 150404





23.Oct.2014Page 126/429

Document-Number Type Rev Compliance A|C Subject Status1999-12-06 AD 00 MANDATORY A/C ALLIED SIGNAL NAV RECEIVER, PREVENT INTERFERENCE OF FM Not Applicable

Compliance:

AD § (a) is Not applicable due to the affected PN not installed on NASB737.Reason for this StatusAUTO ASSIGNED

1999-18-17 AD 00 MANDATORY COMP *AD* SUPERSEDED BY AD 1999-24-08 Superseded (Not Applicable bySerial Number)


ADAD

This Document has been SUPERSEDED BY 1999-24-08/AD Rev.00Affected Rotables (Part No/Serial No/Position) Status

948F458-5 / TT7773 Pos=AFT (KKM)Not Applicable / Reason: AUTOASSIGNED

948F458-3 / WG491 Pos=LH (KKM) Superseded

948F458-5 / ZI1747 Pos=RH (KKM)Not Applicable / Reason: AUTOASSIGNED

40176-7 / S02551 Pos=E&E (KKM) Superseded

1999-19-27 AD 00 MANDATORY COMP *AD* MLG WHEEL ASSEMBLY - TIE BOLTS INSP. & REPLACEMENT Not Applicable by Serial NumberBFGOODRICH SB 3-1398-32-16BFGOODRICH SB 3-1439-32-13

SBSB

0000






23.Oct.2014Page 127/429


1999-21-15 (SUPERSEDED)2007-11-07 (SUPERSEDED)2007-24-02 (ACTIVE)737-28A1120-R4 (REPLACED)737-28A1263-R2 (ACTIVE)

ADADADSBSB

This Document SUPERSEDES 1998-11-51/AD Rev.00This Document SUPERSEDES 1998-11-52/AD Rev.00This Document SUPERSEDES 1998-19-09/AD Rev.00This Document has been SUPERSEDED BY 2007-24-02/AD Rev.00Reason for this StatusSUPERSEDED BY AD 2007-24-02





23.Oct.2014Page 128/429

Document-Number Type Rev Compliance A|C Subject Status1999-22-16 AD 00 MANDATORY A/C *AD* DOORS-CONTROL CABIN DOOR-EMERGENCY EXIT PANEL-INSPECT. Closed 21.Feb.2001

Compliance:AD 1999-22-16 § (a) and (b). is complied with through SB 737-521128and SB 737-52-1137.

This document is effective for737CL:LN# 1717-3028.737NG: LN# 1-91.1999-22-16-R0 (ACTIVE)737-52-1128737-52-1128-R1737-52-1137-R0 (ACTIVE)PRODUCTION LINE (PRR 38060-24)

ADSBSBSBPRR

Perform within an unlimited threshold.1999-22-16/AD Rev.00 *AD* DOORS-CONTROL CABIN DOOR-EMERGENCY EXIT PANEL-INSPECT. Closed 21.Feb.2001> 737-52-1128/SB* Rev.00 CONTROL CABIN DOOR - EMERGENCY EXIT PANEL INSPECTION Closed 21.Feb.2001

This Document has been SUPERSEDED BY 737-52-1128/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







23.Oct.2014Page 129/429

Document-Number Type Rev Compliance A|C Subject Status1999-23-20 AD 00 MANDATORY A/C *AD* REFUEL VALVE ACTUATOR SUPPRESSION DIODES REPLACEMENT Closed 19.Nov.2000

1999-23-20 (ACTIVE)38060-19 (PRODUCTION)737-28-1115 (REF)737-28-1115 IN 01 (REF)737-28-1115 R1 (ACTIVE)SBB 737-28-1115 (MAINT TASK)

ADPRRSBSBSBTA

Perform BEFORE 27.Dec.20001999-23-20/AD Rev.00 *AD* REFUEL VALVE ACTUATOR SUPPRESSION DIODES REPLACEMENT Closed 19.Nov.2000> 737-28-1115/SB* Rev.01 *AD* REFUEL VALVE ACTUATOR SUPPRESSION DIODES REPLACEMENT. Closed 19.Nov.2000


19.Nov.2000PerfRev.:'NOTE' / Reason: DELIVERYDOC.


1999-23-22 AD 02 MANDATORY A/C *AD* MODE `E` TRANSPONDER WITH SINGLEGILHAM CODE ALT. IN PUT Not ApplicableNot applicable due to that NAS does not install Mode "C" transponderwith single Gillham code altitude input.1999-23-22 (ACTIVE) ADReason for this StatusAUTO ASSIGNED

1999-23-24 AD 00 MANDATORY COMP *AD* ALLIED SIGNAL, ILS RECEIVER Not Applicable by Line Number1999-23-24 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 130/429

Document-Number Type Rev Compliance A|C Subject Status1999-24-06 AD 00 MANDATORY A/C *AD* FUEL - ENGINE FUEL FEED SYSTEM - FUEL BOOST PUMP INSP. Not Applicable

The modification is for fuel pumps installed on AUX fule tanks. NASdoes not have any auxiliary fuel tanks installed.1999-24-06 (ACTIVE)737-28A1134 (REF)737-28A1134 R1 (ACTIVE)SBB 737-28A1134 (ACTIVE)

ADSBSBTA

Perform BEFORE 03.Jul.20001999-24-06/AD Rev.00 *AD* FUEL - ENGINE FUEL FEED SYSTEM - FUEL BOOST PUMP INSP. Not Applicable> 737-28A1134/SB* Rev.01 *AD* FUEL - ENGINE FUEL FEED SYSTEM - FUEL BOOST PUMP INSP. Not Applicable by Serial Number





23.Oct.2014Page 131/429

Document-Number Type Rev Compliance A|C Subject Status1999-24-08 AD 00 MANDATORY COMP *AD* A/C BATTERY REPLACEMENT & GEN. CONTROL UNIT DIODE TEST Open

1999-18-17 (SUPERSEDED)1999-24-08 (ACTIVE)37-24-031-11-01 (REPETITIVE)37-AD-1999-24-08 (REPETITIVE)737-24A1136M-7200-99-01528

ADADTATASBBM

02


1999-24-08/AD Rev.00 *AD* A/C BATTERY REPLACEMENT & GEN. CONTROL UNIT DIODE TEST OpenThis Document SUPERSEDES 1999-18-17/AD Rev.00

> 1999-24-08MPD/EO* Rev.00 1999-24-08MPD CONTROLLED BY MPD TASKS Taskcard ControlledCarried out on the following TaskcardsTaskcard: 24-031-11-01 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks14.12.2014 73'771/H 450:15/H Interval:750/HAffected Rotables (Part No/Serial No/Position) Status

40176-7 / S02551 Pos=E&E (KKM)Taskcard Controlled / Reason: AUTOASSIGNED

> AD-1999-24-08/EO* Rev.00 *AD* ELECTRICAL POWER - GCU DIODE CR910 TESTING ON AIRCRAFT ***MANDATORY REPETITIVE DIODE TEST ***

Repetitive


948F458-3 / WG491 Pos=LH (KKM)Repetitive / Next Due: 56438:36/H / LastPerformed:03.Oct.2014 55838:36/H42528/C W/O:15751334 Rev.00





23.Oct.2014Page 132/429

Document-Number Type Rev Compliance A|C Subject Status1999-245 AD 01 MANDATORY COMP INSPECTION OF FUEL FILTER COVER ATTACHMENT PARTS Not Applicable

2000-15-013-73-A129

ADSB

0000

Perform within an unlimited threshold.1999-245/AD Rev.01 INSPECTION OF FUEL FILTER COVER ATTACHMENT PARTS Not Applicable> 3-73-A129/SB* Rev.00 FUEL PUMP WITH NEW FILTER COVER ATTACHM. - INTRODUCTION OF NEW Not Applicable


1999-25-02 AD 00 MANDATORY A/C *AD*INSPECTION OF THE SPOILER MIXER FOR CORRECT INSTALLATION Closed 10.Oct.1998This modification is applicable to LN 1-2681.1999-25-02 (ACTIVE)737-27A1213 (REF)737-27A1213 R1 (ACTIVE)SBB 737-27A1213 (MAINT TASK)

ADSBSBTA

Perform BEFORE 14.Mar.20001999-25-02/AD Rev.00 *AD*INSPECTION OF THE SPOILER MIXER FOR CORRECT INSTALLATION Closed 10.Oct.1998> 737-27A1213/SB* Rev.01 *AD* INSPECTION OF THE SPOILER MIXER FOR CORRECT INSTALL. Closed 10.Oct.1998


10.Oct.1998PerfRev.:'NOTE' / Reason: DELIVERYDOC.






23.Oct.2014Page 133/429

Document-Number Type Rev Compliance A|C Subject Status1999-26-21 AD 00 MANDATORY A/C PRESSURE HOSE AND WIRE BUNDLE INSPECTION AND CLAMP INST Closed 23.Mar.2000

Compliance:AD § (a) and (b) are complied with through SB 737-29A1076.AD § (c) and (d) are complied with through SB 737-29A1077.1999-26-21 (ACTIVE)737-29A1076-R1 (ACTIVE737-29A1077-R2 (ACTIVE)

ADSBSB

Perform within an unlimited threshold.1999-26-21/AD Rev.00 PRESSURE HOSE AND WIRE BUNDLE INSPECTION AND CLAMP INST Closed 23.Mar.2000> 737-29A1076/SB* Rev.01 *AD* HYD SYS B MOTOR DRIVEN PUMP WIRE BUNDLE INSP/CLAMP INST Closed 23.Mar.2000




2000-018 AD B MANDATORY COMP INSPECTION OF HIGH PRESSURE TURBINE FRONT ROTATING AIR SEAL Not ApplicableStatus apply for FAA AD 2000-05-22.3-72-0922 SB 00

2000-018/AD Rev.B INSPECTION OF HIGH PRESSURE TURBINE FRONT ROTATING AIR SEAL Not Applicable> 3-72-0922/SB* Rev.00 *AD* HPT FRONT ROTATING AIR SEALS BOLT HOLES ONE TIME INSP. Not Applicable


CFM56-3B2 / 724473 Pos=LH (KKM)Not Applicable / Reason: SEAL SN NA,SHOP VISIT 2005

CFM56-3B2 / 725495 Pos=RH (KKM)Not Applicable / Reason: SEAL SN NA,DELIVERY DOCS





23.Oct.2014Page 134/429

Document-Number Type Rev Compliance A|C Subject Status2000-02-03 AD 00 MANDATORY A/C *AD* SUPERSEDED BY 2003-03-05 Superseded (Closed 18.Dec.2001)

2000-02-03 (SUPERSEDED)2003-03-05 (ACTIVE)737-27-1174 (REF)737-27A1243-R2 (ACTIVE)737-SRP-27-0138 (REF)PRODUCTION LINE PRR35005-175SBB-737-27A1243 (MOD-TASK)

ADADSBSBSRPPRRTA


2000-02-03/AD Rev.00 *AD* SUPERSEDED BY 2003-03-05 Closed 18.Dec.2001This Document has been SUPERSEDED BY 2003-03-05/AD Rev.00

> 737-27-1211/SB* Rev.00 *AD* REPL OF THE ROD ENDS FOR THE LEADING EDGE SLAT ACTUATOR Closed 08.Dec.2001This Document has been SUPERSEDED BY 737-27A1211/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

08.Dec.2001PerfRev.:'NOTE' / Reason: REPLACED BY737-27A1243

Reason for this StatusREPLACED BY 737-27A1243

> 737-27A1211/SB* Rev.02 *AD* REPLACEMENT OF ROD ENDS FOR LEADING EDGE SLAT ACTUATORS Closed 18.Dec.2001This Document SUPERSEDES 737-27A1211/SB Rev.01This Document has been SUPERSEDED BY 737-27A1211/SB Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







23.Oct.2014Page 135/429

Document-Number Type Rev Compliance A|C Subject Status2000-02-18 AD 00 MANDATORY COMP *AD* AILERON/ELEVATOR AND RUDDER PCU CYLINDER BORE REWORK Not Applicable

1997-09-142000-02-18737-SL-27-030

ADADSL

000000

This Document SUPERSEDES 1997-09-14/AD Rev.002000-02-18/AD Rev.00 *AD* AILERON/ELEVATOR AND RUDDER PCU CYLINDER BORE REWORK Not Applicable

This Document SUPERSEDES 1997-09-14/AD Rev.00> 737-SL-27-030/SL* Rev.00 *AD* RUDDER PCU, INSPECTION & REPLACEMENT Not Applicable by Serial Number

Affected Rotables (Part No/Serial No/Position) Status65-44761-21 / 9311AB Pos=AFT (KKM) Not Applicable65-44761-21 / 6895A Pos=AFT (KKM) Not Applicable65-44761-22 / 12765A Pos=RH (KKM) Not Applicable65-44761-21 / 7418A Pos=LH (KKM) Not Applicable





23.Oct.2014Page 136/429

Document-Number Type Rev Compliance A|C Subject Status2000-0294 AD 00 MANDATORY COMP REVISION OF ENGINE SHOP MANUAL/SUPERSED.BY AD2002-13-03 Superseded (Superseded)

2000-12-012002-13-03

ADAD

0000

This Document has been SUPERSEDED BY 2002-13-03/AD Rev.002000-0294/AD Rev.00 REVISION OF ENGINE SHOP MANUAL/SUPERSED.BY AD2002-13-03 Superseded

This Document has been SUPERSEDED BY 2002-13-03/AD Rev.00> 2000-12-01/AD* Rev.00 REVISION OF ENGINE SHOP MANUAL/SUPERSED.BY AD2002-13-03 Superseded

This Document SUPERSEDES 1999-08-16/AD Rev.00This Document has been SUPERSEDED BY 2002-13-03/AD Rev.00This Document has been SUPERSEDED BY F-2002-390/AD Rev.00Affected Rotables (Part No/Serial No/Position) Status

CFM56-3B2 / 725495 Pos=RH (KKM)

Repetitive / Reason: SET BYEFFECTIVE-FROM ON MOD 39730 /Last Performed:11.Dec.2000 RefDocument:Rev.NOTE

CFM56-3B2 / 724473 Pos=LH (KKM)






23.Oct.2014Page 137/429

Document-Number Type Rev Compliance A|C Subject Status2000-04-02 AD 00 MANDATORY A/C *AD* FUEL LOW PRESS. SWITCHES REPL/INSP. OF FUEL BOOST PUMPS Closed 25.Nov.1998

2000-04-02 (ACTIVE)35005-218 (PRODUCTION)37-SBB-28A1114 (REP TASK)737-28A1114 (REF)737-28A1114 R1 (REF)737-28A1114 R2 (REF)737-28A1114 R3 (REF)SBB 737-28A1114 (MAINT TASK)

ADPRRTASBSBSBSBTA

Perform BEFORE 29.Mar.20022000-04-02/AD Rev.00 *AD* FUEL LOW PRESS. SWITCHES REPL/INSP. OF FUEL BOOST PUMPS Closed 25.Nov.1998> 737-28A1114/SB Rev.03 *AD* FUEL LOW PRESS SWITCHES REPL./INSP. OF FUEL BOOST PUMPS Closed 25.Nov.1998> > 737-28A1114/EO* Rev.03 *AD* FUEL BOOST PUMPS INSPECTION Not Applicable

Reason for this StatusREPETITIVE INSPECTION TERMINATED BY MODIFICATION

> > 737-28A1114-01/EO* Rev.03 *AD* FUEL LOW PRESS SWITCHES REPL./INSP. OF FUEL BOOST PUMPS Closed 25.Nov.1998Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

25.Nov.1998PerfRev.:'NOTE' / Reason: DELIVERYDOC.


2000-04-24 AD 00 MANDATORY A/C *AD* PREVENT AN UNCONTAINED APU FAILURE AND DAMAGE TO A/C Not ApplicableNot applicable due to Honeywell International (formerly AlliedSignalInc.) 36-300(A), 36-280(B), and 36-280(D) series Auxiliary PowerUnits (APUs) not installed on NAS B737.2000-04-24 (ACTIVE) ADReason for this StatusAUTO ASSIGNED





23.Oct.2014Page 138/429

Document-Number Type Rev Compliance A|C Subject Status2000-05-13 AD 00 MANDATORY A/C LANDING GEAR - WHEEL AND BRAKES - BRAKE MOUNTING GASKET REPLACEMENT

WITH ALUMINIUM-NICKEL-BRONZE GASKET.Closed 19.Nov.2000

This document is Applicable to LN#: 502-2135. All other LN# are NotApplicable per Boeing SB.

references:/A/: SB 737-32-1253 NSC-1/B/: SB 737-32-1253 NSC-2Perform WITHIN 1500/C (effective from 19.Mar.2000)Perform WITHIN 200/D (effective from 19.Mar.2000)

2000-05-13/AD Rev.00 LANDING GEAR - WHEEL AND BRAKES - BRAKE MOUNTING GASKET REPLACEMENTWITH ALUMINIUM-NICKEL-BRONZE GASKET.

Closed 19.Nov.2000

> 737-32-1253/SB* Rev.00 LANDING GEAR - WHEEL AND BRAKES - BRAKE MOUNTING GASKET REPLACEMENTWITH ALUMINIUM-NICKEL-BRONZE GASKET.

Closed 19.Nov.2000


19.Nov.200043995 ITEM704

PerfRev.:'00' / Reason: PERFORMED BYAEROPLEX

Reason for this StatusPERFORMED BY AEROPLEX





23.Oct.2014Page 139/429

Document-Number Type Rev Compliance A|C Subject Status2000-05-22 AD 00 MANDATORY COMP HPT FRONT ROTATING AIR SEALS BOLT HOLES ONE TIME INSP. Not Applicable

Category 2 - CampaignThe high pressure turbine (HPT) front rotating air seal 1282M72P03,with a serial number beginning with NCE is affected.NOTE: The change in this Service Bulletin can be accomplishedin-shop.Status apply for EASA AD 2000-018.3-72-0922 SB 00Perform within an unlimited threshold.

2000-05-22/AD Rev.00 HPT FRONT ROTATING AIR SEALS BOLT HOLES ONE TIME INSP. Not Applicable> 3-72-0922/SB* Rev.00 *AD* HPT FRONT ROTATING AIR SEALS BOLT HOLES ONE TIME INSP. Not Applicable


CFM56-3B2 / 724473 Pos=LH (KKM)Not Applicable / Reason: SEAL SN NA,SHOP VISIT 2005

CFM56-3B2 / 725495 Pos=RH (KKM)Not Applicable / Reason: SEAL SN NA,DELIVERY DOCS





23.Oct.2014Page 140/429

Document-Number Type Rev Compliance A|C Subject Status2000-05-29 AD 00 MANDATORY A/C *AD* FUSELAGE - BODY STATION 178 BULKHEAD - INSPECTION Closed 21.Feb.2008

Applicable to LN#: 1-27372000-05-29 (ACTIVE)37-SBB-53A1173 (REPETITIVE)737-53-1173 IN 06 (REF)737-53A1173-R0 (REF)737-53A1173-R1 (REF)737-53A1173-R2 (REF)737-53A1173-R3 (REF)737-53A1173-R4 (ACTIVE)SBB 737-53A1173 (MOD TASK)

ADTASBSBSBSBSBSBTA

Perform BEFORE 50000/C2000-05-29/AD Rev.00 *AD* FUSELAGE - BODY STATION 178 BULKHEAD - INSPECTION Closed 21.Feb.2008> 737-53A1173/SB Rev.04 FUSELAGE - BODY STATION 178 BULKHEAD - INSPECTION, REPAIR AND PREVENTIVE

MODIFICATIONClosed 21.Feb.2008

> > 737-53A1173/EO* Rev.04 FUSELAGE - BODY STATION 178 BULKHEAD - INSPECTION CancelledPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

05.Sep.2006 50494:00/H 27176/CPerfRev.:'NOTE' / Reason: AMICOS WO150725 KKM 37-SBB-53A1173 BS 178BULKHEA

Reason for this StatusPREVENTIVE MODIFICATION PERFORMED ON EO 737-53A1173-01

> > 737-53A1173-01/EO* Rev.04 *AD* FUSELAGE - BODY STATION 178 BULKHEAD - INSPECTION Closed 21.Feb.2008Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

21.Feb.2008 54541:00/H 30316/CPerfRev.:'NOTE' / Reason: KKM 151384ITEM: 1

Reason for this StatusKKM 151384 ITEM: 1





23.Oct.2014Page 141/429

Document-Number Type Rev Compliance A|C Subject Status2000-06-13 AD 01 MANDATORY A/C *AD* CARGO DOOR AFT - FRAME & BEAM INSPECTION, REPAIR & MOD Superseded (Not Applicable)

This mod is applicable to LN# 1-1642. All other LN# are NotApplicable per Boeing SB.1998-25-06 (SUPERSEDED)2000-06-13 (SUPERSEDED)2000-06-13-R1 (ACTIVE)737-52A1079-R0 (REF)737-52A1079-R1 (REF)737-52A1079-R2 (REF)737-52A1079-R3 (REF)737-52A1079-R4 (REF)737-52A1079-R5 (REF)737-52A1079-R6 (ACTIVE)SBB 737-52A1079 (MOD TASK)

ADADADSBSBSBSBSBSBSBTA


2000-06-13/AD Rev.01 *AD* CARGO DOOR AFT - FRAME & BEAM INSPECTION, REPAIR & MOD Not ApplicableThis Document SUPERSEDES 2000-06-13/AD Rev.00This Document has been SUPERSEDED BY 2013-13-12/AD Rev.00

> 737-52A1079/SB* Rev.07 DOORS - AFT CARGO - FRAME AND BEAM INSPECTION, REPAIR AND MODIFICATION Not Applicable by Serial NumberThis Document SUPERSEDES 737-52A1079/SB Rev.00

> 737-52A1079/SB* Rev.00 *AD* CARGO DOOR AFT - FRAME & BEAM INSPECTION, REPAIR & MOD Not Applicable by Serial NumberThis Document has been SUPERSEDED BY 737-52A1079/SB Rev.07





23.Oct.2014Page 142/429

Document-Number Type Rev Compliance A|C Subject Status2000-06-13 AD 00 MANDATORY A/C *AD* CARGO DOOR AFT - FRAME & BEAM INSPECTION, REPAIR & MOD (SUPERSEDED

BY AD 2006-06-13 R1)Superseded (Not Applicable)

This mod is applicable to LN# 1-16421998-25-06 (SUPERSEDED)2000-06-13 (SUPERSEDED)2000-06-13-R1 (ACTIVE)737-52A1079-R0 (REF)737-52A1079-R1 (REF)737-52A1079-R2 (REF)737-52A1079-R3 (REF)737-52A1079-R4 (REF)737-52A1079-R5 (REF)737-52A1079-R6 (ACTIVE)SBB 737-52A1079 (MOD TASK)



2000-06-13/AD Rev.00 *AD* CARGO DOOR AFT - FRAME & BEAM INSPECTION, REPAIR & MOD (SUPERSEDEDBY AD 2006-06-13 R1)

Not Applicable


> 737-52A1079/SB* Rev.00 *AD* CARGO DOOR AFT - FRAME & BEAM INSPECTION, REPAIR & MOD Not Applicable by Serial NumberThis Document has been SUPERSEDED BY 737-52A1079/SB Rev.07





23.Oct.2014Page 143/429

Document-Number Type Rev Compliance A|C Subject Status2000-07-06 AD 00 MANDATORY A/C *AD* FWD CARGO-LOWER FWD AND AFT CORNER INSP,MOD AND REPL Superseded (Closed 08.Mar.2005)

2000-07-06 (ACTIVE)737-52A1100737-52A1100 IN 07737-52A1100 IN 09737-52A1100 R1737-52A1100 R2737-52A1100 R3737-52A1100 R4

ADSBSBSBSBSBSBSB

This Document has been SUPERSEDED BY 2013-09-10/AD Rev.00Perform BEFORE 12000/CPerform BEFORE 16.May.2004

2000-07-06/AD Rev.00 *AD* FWD CARGO-LOWER FWD AND AFT CORNER INSP,MOD AND REPL Closed 08.Mar.2005This Document has been SUPERSEDED BY 2013-09-10/AD Rev.00

> 737-52A1100/SB Rev.04 *AD* FWD CARGO DOORS, LOWER FWD/AFT CORNER INSP MOD/REPL. Closed 08.Mar.2005> > 737-52A1100/EO* Rev.04 *AD* FWD CARGO DOORS, LOWER FWD AND AFT CORNER INSP, MOD AN Not Applicable by Serial Number

This Document is terminated with implementation of 737-52A1100-01/EO Rev.04> > 737-52A1100-01/EO* Rev.04 *AD* FWD CARGO DOORS, LOWER FWD/AFT CORNER INSP MOD/REPL. Closed 08.Mar.2005

This Document terminates 737-52A1100/EO Rev.04Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

08.Mar.2005 46130:00/H 23575/CPerfRev.:'NOTE' / Reason: KKM 150399ITEM: 1






23.Oct.2014Page 144/429

Document-Number Type Rev Compliance A|C Subject Status2000-08-17 AD 00 MANDATORY A/C *AD* TAXI LIGHT ASSEMBLY - INSPECTION & REPLACEMENT Not Applicable / Special Text: This

Aircraft is Not Applicable due toVAR#.

This document is applicable to LN# 16-2374.2000-08-17 (ACTIVE)737-33-1129-R0 (ACTIVE)SBB 737-33-1129 (MOD-TASK)

ADSBTA

Perform BEFORE 30.Jul.20002000-08-17/AD Rev.00 *AD* TAXI LIGHT ASSEMBLY - INSPECTION & REPLACEMENT Not Applicable / Special Text: This

Aircraft is Not Applicable due toVAR#.

> 737-33-1129/SB* Rev.00 *AD* TAXI LIGHT ASSEMBLY - INSPECTION & REPLACEMENT Not Applicable / Special Text: Thisaircraft is Not Applicable due toVAR#.


2000-10-21 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 2004-04-03 Superseded (Not Applicable)2000-10-21 (SUPERSEEDED)2004-04-03 (ACTIVE)737-25A1363-R2 (ACTIVE)IPECO A001-25-47PRODUCTION LINE MRR3257-1156

ADADSBSBPRR






23.Oct.2014Page 145/429

Document-Number Type Rev Compliance A|C Subject Status2000-12-01 AD 00 MANDATORY COMP REVISION OF ENGINE SHOP MANUAL/SUPERSED.BY AD2002-13-03 Superseded (Superseded)

2000-12-012002-13-03

ADAD

0000

This Document SUPERSEDES 1999-08-16/AD Rev.00This Document has been SUPERSEDED BY 2002-13-03/AD Rev.00This Document has been SUPERSEDED BY F-2002-390/AD Rev.00Affected Rotables (Part No/Serial No/Position) Status

CFM56-3B2 / 725495 Pos=RH (KKM)


CFM56-3B2 / 724473 Pos=LH (KKM)






23.Oct.2014Page 146/429

Document-Number Type Rev Compliance A|C Subject Status2000-14-13 AD 00 MANDATORY A/C *AD* DOOR HANDLE MOUNTING HUB ASSEMBLY REPLACEMENT. Closed 08.Dec.1995

This mod is applicable to LN# 1001-26502000-14-13 (ACTIVE)737-25-1322-R0 (REF)737-25-1322-R1 (REF)737-25-1322-R2 (ACTIVE)SBB 737-25-1322 (MOD TASK)

ADSBSBSBTA

Perform BEFORE 23.Feb.20022000-14-13/AD Rev.00 *AD* DOOR HANDLE MOUNTING HUB ASSEMBLY REPLACEMENT. Closed 08.Dec.1995> 737-25-1322/SB* Rev.02 *AD* DOOR HANDLE MOUNTING HUB ASSEMBLY REPLACEMENT. Closed 08.Dec.1995








23.Oct.2014Page 147/429

Document-Number Type Rev Compliance A|C Subject Status2000-15-01 AD 00 MANDATORY COMP FUEL PUMP FILTER COVER HELICOIL INSERT, INSP./REPL. OF Not Applicable

Ref. CFM SB 3-73-0129/A129 applicability.

CFM56-3/3B/3C ESN86X136 and higher

Main Fuel Pump SN YA021001 and higher

Appl. to the old fuel pump PN 301-778-801-0, 301-778-802-0,301-779-001-0 and 301-779-002-0 from engine,if installed. Refer tothe BOEING Maintenance Manual (BMM),73-11-01.

New fuel pumps to be installed PN 301-778-804-0, 301-778-805-0,301-779-005-0 and 301-779-006-0. Refer to the BMM,73-11-012.Apply for EASA ADStatus apply for EASA AD 1999-245.1999-2452000-15-013-73-01253-73-01263-73-0129

DGACADSBSBSB

0100010100

2000-15-01/AD Rev.00 FUEL PUMP FILTER COVER HELICOIL INSERT, INSP./REPL. OF Not Applicable> 3-73-0125/SB* Rev.01 ENGINE FUEL AND CONTROL - MAIN FUEL PUMP REPLACEMENT OF THE

ATTACHMENT PARTS OF THE FUEL FILTER COVERNot Applicable


> 3-73-0126/SB* Rev.01 ENGINE - FUEL AND CONTROL - MAIN FUEL PUMP INSPECTION OF FUEL FILTERCOVER ATTACHMENT PARTS

Not Applicable


> 3-73-0129/SB* Rev.00 FUEL PUMP WITH NEW FILTER COVER ATTACHM. - INTRODUCTION OF NEW Not ApplicableAffected Rotables (Part No/Serial No/Position) Status





23.Oct.2014Page 148/429

Document-Number Type Rev Compliance A|C Subject StatusNo affected rotable installed

> 3-73-A129/SB* Rev.00 FUEL PUMP WITH NEW FILTER COVER ATTACHM. - INTRODUCTION OF NEW Not ApplicableAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

2000-15-16 AD 00 MANDATORY A/C *AD* PASSENGER & ATTENDANT OXYGEN MASK LANDYARD REPLACEMENT Closed 17.Mar.2005This document is applicable to LN# 1-2984.737-35-1049737-35-1049B/E AEROSPACE 3500-98-07B/E AEROSPACE 3500-98-07 A01PRODUCTION LINE PRR38060-9

SBSBSBSBPRR

0001000100

Perform BEFORE 12.Sep.20052000-15-16/AD Rev.00 *AD* PASSENGER & ATTENDANT OXYGEN MASK LANDYARD REPLACEMENT Closed 17.Mar.2005> 737-35-1049/SB* Rev.00 PASSENGER & ATTENDANT OXYGEN MASK LANDYARD REPLACEMENT Superseded

This Document has been SUPERSEDED BY 737-35-1049/SB Rev.01> 737-35-1049/SB* Rev.01 PASSENGER & ATTENDANT OXYGEN MASK LANDYARD REPLACEMENT Closed 17.Mar.2005








23.Oct.2014Page 149/429


2000-17-51 (SUPERSEDED2001-08-07 (SUPERSEDED)2004-03-23 (ACTIVE)737-52-0037-R2 (PEMCO)

ADADADSB


2000-18-04 AD 00 MANDATORY A/C *AD* PREVENT LOSS OF STRUCT. INTEGRITY OF SEAT Superseded (Superseded)Not applicable due to the affected Aviointeriors S.p.A. (formerlyALVEN), model 312 seats not installed on NAS B737.2000-18-04 (ACTIVE) ADThis Document has been SUPERSEDED BY 2005-07-27/AD Rev.00





23.Oct.2014Page 150/429

Document-Number Type Rev Compliance A|C Subject Status2000-19-05 AD 00 MANDATORY A/C *AD* ELEVATOR TAB ROD ATTACHMENT NUT INSPECTION Closed 31.Oct.2000

This mod is applicable to LN# 1-2939. The following LN# are NotApplicable due to MRR 3277-1146.1999-05-15 (SUPERSEDED)2000-19-05 (ACTIVE)2000-19-05 XA (REF)737-27A1205-R0 (ACTIVE)737-SL-27-118/A/B/C/D (REF)SBB 737-27A1205 (MOD-TASK)

ADADADSBSLTA

This Document SUPERSEDES 1999-05-15/AD Rev.00Perform BEFORE 25.Oct.2002

2000-19-05/AD Rev.00 *AD* ELEVATOR TAB ROD ATTACHMENT NUT INSPECTION Closed 31.Oct.2000This Document SUPERSEDES 1999-05-15/AD Rev.00

> 737-27A1205/SB* Rev.00 ELEVATOR TAB ROD ATTACHMENT NUT INSPECTION Closed 09.Feb.1999Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-SL-27-118/SL* Rev.E ELEVATOR TAB PUSH ROD INST. - NEW BOLTS AND CASTELLARED NUTS Closed 31.Oct.2000Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

31.Oct.2000PerfRev.:'NOTE' / Reason: DELIVERYDOC.






23.Oct.2014Page 151/429

Document-Number Type Rev Compliance A|C Subject Status2000-22-02 AD 00 MANDATORY A/C MODIFICATION OF THE RUDDER PCU, INTRODUCTION OF RESP PROGRAM Superseded (Not Applicable)

1996-26-07 (SUPERSEDED)2000-22-02-R1 (SUPERSEDED)2002-20-07 (SUPERSEDED)2007-03-07 (ACTIVE)

ADADADAD


2000-23-34 AD 00 MANDATORY A/C *AD* AUTOPILOT MODE CONTROL PANLE REPL. Performed by prev. Operator1992-07-09A4051601-22-17A4051601-22-18

ADSBSB

000000

Perform WITHIN 540/D (effective from 08.Jan.2001)2000-23-34/AD Rev.00 *AD* AUTOPILOT MODE CONTROL PANLE REPL. Performed by prev. Operator> 737-22A1130/SB Rev.00 AUTOFLIGHT - AUTOTHROTTLE COMPUTER - REPLACEMENT OF THE

AUTOTHROTTLE COMPUTERPerformed by prev. Operator

> > 737-22A1130-01/EO* Rev.00 AUTOFLIGHT - AUTOTHROTTLE COMPUTER - REPLACEMENT OF THEAUTOTHROTTLE COMPUTER

Performed by prev. Operator


03.Mar.2000DELIVERYDOC

PerfRev.:'00'

> > 737-22A1130-02/EO* Rev.00 AUTOFLIGHT - AUTOTHROTTLE COMPUTER - REPLACEMENT OF THEAUTOTHROTTLE COMPUTER

Not Applicable


755SUE2-4 / 6448 Pos=E&E (KKM)Not Applicable / Reason: AUTOASSIGNED





23.Oct.2014Page 152/429

Document-Number Type Rev Compliance A|C Subject Status2000-26-05 AD 00 MANDATORY A/C *AD* AIR CONDITIONING-DISTRIBUTION - DUCT INSULATION REPL. Not Applicable

This document is applicable to airplanes line numbers 2591,2601,2720, 2723, 2730, 2733, 2734, 2736 through 2850, 2852 through 3126,divided into four groups. All other LN# are Not Applicable per PRR35--05-231R.2000-26-05 (ACTIVE)737-21A1129 IN 01 (REF)737-21A1129-R0 (ACTIVE)737-SRP-21-0125 (REF)PRODUCTION PRR 35005-231RSBB 737-21A1129 (MOD-TASK)

ADSBSBSRPPRRTA

2000-26-05/AD Rev.00 *AD* AIR CONDITIONING-DISTRIBUTION - DUCT INSULATION REPL. Not Applicable> 737-21A1129/SB* Rev.00 *AD* AIR CONDITIONING-DISTRIBUTION - DUCT INSULATION REPL. Not Applicable by Serial Number





23.Oct.2014Page 153/429

Document-Number Type Rev Compliance A|C Subject Status2001-01-13 AD 00 MANDATORY A/C FUEL QTY IND SYST/INSP OF WIRING HARNESS IN WING TANK Closed 02.Apr.2001

This document is effective for LN# 1001-3132.

Compliance:AD § (b/(c)) is complied with via SB 737-28A1168.2001-01-13 (ACTIVE)737-28A1168-R0 (REF)737-28A1168-R1 (REF)737-28A1168-R2 (ACTIVE)

ADSBSBSB

Perform BEFORE 28.Aug.20022001-01-13/AD Rev.00 FUEL QTY IND SYST/INSP OF WIRING HARNESS IN WING TANK Closed 02.Apr.2001> 737-28A1168/SB* Rev.02 FUEL QTY IND SYST/INSP OF WIRING HARNESS IN WING TANK Closed 02.Apr.2001


02.Apr.2001PerfRev.:'NOTE' / Reason: DELIVERYDOC.






23.Oct.2014Page 154/429

Document-Number Type Rev Compliance A|C Subject Status2001-02-01 AD 00 MANDATORY A/C FUSELAGE/BODY STATION 178 BULKHEAD INSPECTION/REPAIR Not Applicable

This document is applicable to LN# 2738-3071. All other LN# are NotApplicable per Boeing SB.

Compliance:AD § (a) and (b) is covered by EO 737-53A1208AD § (c) is covered by EO 737-53A1208-012001-02-01737-53A1208737-53A1208737-53A1208-01

ADEOSBEO

00010101

2001-02-01/AD Rev.00 FUSELAGE/BODY STATION 178 BULKHEAD INSPECTION/REPAIR Not Applicable> 737-53A1208/SB Rev.01 *FUSELAGE/BODY STATION 178 BULKHEAD INSPECTION/REPAIR Not Applicable> > 737-53A1208/EO* Rev.01 FUSELAGE - BODY STATION 178 BULKHEAD INSPECTION AND RE Not Applicable by Serial Number

This Document is terminated with implementation of 737-53A1208-01/EO Rev.01> > 737-53A1208-01/EO* Rev.01 FUSELAGE/BODY STATION 178 BULKHEAD INSPECTION/REPAIR Not Applicable by Serial Number

This Document terminates 737-53A1208/EO Rev.01





23.Oct.2014Page 155/429

Document-Number Type Rev Compliance A|C Subject Status2001-04-06 AD 00 MANDATORY COMP FAN DISK DOVETAIL, WEAR MEASUREMENT OF Closed 26.Jun.2012

Ref. SB CFM56-3/-3B/-3C 72-0854

Compliance:AD § (a) through (f) is complied with through SB 3-72-0854.2001-04-063-72-0854

ADSB

0005

Perform within an unlimited threshold.2001-04-06/AD Rev.00 FAN DISK DOVETAIL, WEAR MEASUREMENT OF Closed 26.Jun.2012> 3-72-0854/SB* Rev.05 FAN DISK DOVETAIL, WEAR MEASUREMENT OF Closed 26.Jun.2012


CFM56-3B2 / 725495 Pos=RH (KKM)

Closed / Last Performed:26.Jun.201264007:00/H 38431/C RefDocument:MTURECORDED MOD SHEET WO 51734400Rev.05

CFM56-3B2 / 724473 Pos=LH (KKM)

Closed / Reason: NEW DISK INST. ONSHOP VISIT 39729 / LastPerformed:17.Jan.2005 42076:00/H 21463/CRefDocument: Rev.NOTE

2001-08-07 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 2004-03-23 Superseded (Not Applicable)2001-08-07 (SUPERSEDED)2004-03-23 (ACTIVE)737-52-0037-R2 (PEMCO)

ADADSB






23.Oct.2014Page 156/429

Document-Number Type Rev Compliance A|C Subject Status2001-08-24 AD 00 MANDATORY A/C *AD* AIRPLANE FLIGHT MANUAL REVISION - FUEL PUMP OPERATION Closed 01.Sep.2002

FAA AMOC letter approves the installation of fuel pump Auto Shut Off,as installled from LN# 1494 and on as an AMOC to this AD.

Boeing SB 737-28A1206 is approved as an AMOC to §A.2001-08-24 (ACTIVE)38545-20S (PRODUCTION)FAA LETTER 140S-06-275

ADPRRAMOC

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks01.Sep.2002 Reason: AD INSERTED IN AFMReason for this StatusAD INSERTED IN AFM

2001-08-24/AD* Rev.00 *AD* AIRPLANE FLIGHT MANUAL REVISION - FUEL PUMP OPERATION Closed 01.Sep.2002Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks01.Sep.2002 Reason: AD INSERTED IN AFMReason for this StatusAD INSERTED IN AFM

2001-09-15 AD 00 MANDATORY A/C *AD* INSPECTION OF MAIN DECK CARGO DOOR FOR CRAKING Not ApplicableNAS has no Aircraft with main deck cargo door installed.1995-01-06R1 (SUPERSEDED)2001-09-15-R0 (ACTIVE)737-53-0003-R5 (PEMCO)

ADADSB

This Document SUPERSEDES 1995-01-06/AD Rev.00

2001-10-13 AD 00 MANDATORY A/C *AD* BRITAX SELL GMBH & CO OHG - WATER BOILERS, COFFEE MAKER Superseded (Superseded)Not applicable due to the affected PN not isntalled on NAS B737.This Document has been SUPERSEDED BY 2002-21-01/AD Rev.00





23.Oct.2014Page 157/429

Document-Number Type Rev Compliance A|C Subject Status2001-10-14 AD 00 MANDATORY A/C *AD* INSPECTION OF THE RELEASE PIN LOCATION IN OXYGEN GEN. Repetitive

AMOC letter gives permission to use one of two options to comply withAD. NAS will use "Option 2" of the AMOC. NAS performs repetitivinspections of the AC oxygen generators and uses the improved AMMreferences for Removal/Installation.130S-01-334737-35-1076737-35-1077PRODUCTION MRR3350-1422S

AMOCSBSBPRR

000000

Perform within an unlimited threshold.2001-10-14/AD Rev.00 *AD* INSPECTION OF THE RELEASE PIN LOCATION IN OXYGEN GEN. Repetitive> 737-35-1076/SB Rev.00 OXYGEN GENERATOR, INSPECTION OF RELEASE PIN LOCATION Repetitive> > 737-35-1076-01/EO* Rev.00 OXYGEN GENERATOR, INSPECTION OF RELEASE PIN LOCATION See prev. Docstatus

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Aug.2001 45757:00/H 23244/C PerfRev.:'NOTE'Reason for this StatusDEL DOCS

> > 737-35-1076-02/EO* Rev.00 OXYGEN GENERATOR, INSPECTION OF RELEASE PIN LOCATION RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

31.Jul.2015Perform initially within (effective from08.Jun.2001) (F) 540/D / Interval(F):540/D

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks06.Feb.2014 71572:00/H 43151/C 489224, N/A Was due at: 19.Apr.2014 PerfRev.:'00'





23.Oct.2014Page 158/429

Document-Number Type Rev Compliance A|C Subject Status2001-11-05 AD 00 MANDATORY COMP NO. 4 BEARING - SUSPECT BEARING SN Not Applicable by Serial Number

Appl. to No. 4 Bearings:PN 305-355-717-0SN DB387608-F, DB387612-8, DB387614-4, DB387625-H, DB387647-Y,DB387650-6, DB387651-5, DB387661-K, DB387609-Y, DB387611-7,DB387615-3, DB387601-N, DB387594-1, DB387592-3, DB387610-8,DB387600-P, B387649-V, DB387678-C, DB387652-4, DB387659-C,DB387655-1, DB387684-F, DB387588-V, DB387657-E, DB387653-3,DB387597-D, DB387602-M, DB387589-U, DB387656-O, DB387671-4.

Appl. to CFM56-3:ESN 725109, 720493, 721253, 720383, 857594, 721237, 726245, 856671.

Appl. to CFM56-7B:ESN 876395, 876399, 876400, 876401, 876403, 876405, 876406, 876410,876421, 876423, 876424, 876429, 876431, 876432, 876434, 876727,876729, 876730, 877404, 877408, 877427, 875232, 874219.2001-11-05 AD 00Affected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 725495 Pos=RH (KKM) Not ApplicableCFM56-3B2 / 724473 Pos=LH (KKM) Not Applicable





23.Oct.2014Page 159/429

Document-Number Type Rev Compliance A|C Subject Status2001-11-07 AD 00 MANDATORY A/C HYDRAULIC POWER - DC MOTOR OPERATED SHUTOFF VALVE INSP. Closed 21.Feb.1998

2001-11-07 (ACTIVE)737-29A1073-R2 (ACTIVE CL)737-29A1081-R1 (ACTIVE NG)PRODUCTION LINE PRR35005-223

ADSBSBPRR

Perform within an unlimited threshold.2001-11-07/AD Rev.00 HYDRAULIC POWER - DC MOTOR OPERATED SHUTOFF VALVE INSP. Closed 21.Feb.1998> 737-29A1073/SB* Rev.04 HYDRAULIC POWER - DC MOTOR OPERATED SHUTOFF VALVE INSPECTION Closed 21.Feb.1998


21.Feb.1998PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:


> 737-29A1078/SB* Rev.02 REPLACEMENT OF DC MOTOR OPERATED SHUTOFF VALVE Not ApplicableReason for this StatusNOT APPLICABLE DUE TO EFFECTED PARTS NOT INSTALLED

2001-11-11 AD 00 MANDATORY A/C PASS. SEATS. AVIO INTERIORS SEAT TRACK FITTING REPLACEM Not ApplicableNot applicable due to Variable Number.2001-11-11 (ACTIVE)737-25-1371-R0 (REF)737-25-1371-R1 (REF)737-25-1371-R2 (REF)737-25-1371-R3 (ACTIVE)AVIO INT 180/A184-01AVIO INT 184/E23-01 R1

ADSBSBSBSBSBSB

2001-11-11/AD Rev.00 PASS. SEATS. AVIO INTERIORS SEAT TRACK FITTING REPLACEM Not Applicable> 737-25-1371/SB* Rev.03 PASS. SEATS. AVIO INTERIORS SEAT TRACK FITTING REPLACEM Not Applicable by Serial Number






23.Oct.2014Page 160/429

Document-Number Type Rev Compliance A|C Subject Status2001-13-07 AD 00 MANDATORY A/C *AD* TEST OF ELECTR. CIRCUITS THAT CLOSE FUEL SHUTOFF VALVE Closed 27.Mar.2001

2001-13-07 (ACTIVE)737-28-1160-R1 (ACTIVE-NG)737-28-1164-R1 (ACTIVE-CL)

ADSBSB

Perform within an unlimited threshold.2001-13-07/AD Rev.00 *AD* TEST OF ELECTR. CIRCUITS THAT CLOSE FUEL SHUTOFF VALVE Closed 27.Mar.2001> 737-28-1164/SB* Rev.01 *AD* TEST OF ELECTR. CIRCUITS THAT CLOSE FUEL SHUTOFF VALVE Closed 27.Mar.2001




2001-14-06 AD 00 MANDATORY A/C *AD* AD SUPERSEDED BY 2005-10-11 Superseded (Closed 24.Jan.2004)2001-14-06 (SUPERSEDED)2004-5395 (REF)2005-10-11 (ACTIVE)737-28-1196-R3 (ACTIVE)737-SL-24-138 (REF)PRODUCTION LINE MRR3282-1516

ADADADSBSLPRR

This Document has been SUPERSEDED BY 2005-10-11/AD Rev.002001-14-06/AD* Rev.00 *AD* AD SUPERSEDED BY 2005-10-11 Closed 24.Jan.2004

This Document has been SUPERSEDED BY 2005-10-11/AD Rev.00> 737-28-1196/SB* Rev.03 *AD* ENG FUEL SHUTOFF VALVE, WIRING CHANGES IN MWW Closed 24.Jan.2004


24.Jan.2004 43499:00/H 21327/CPerfRev.:'NOTE' / Reason: KKM 150052ITEM: 2






23.Oct.2014Page 161/429

Document-Number Type Rev Compliance A|C Subject Status2001-14-10 AD 00 MANDATORY A/C *AD* AIRPLANE FLIGHT MANUAL REVISION - IFE SYSTEM Not Applicable

NAS has no Aircraft with STC ST00171SE installed.2001-14-10 (ACTIVE)ST00171SE (REF)

ADSTC

Reason for this StatusSTC NOT INSTALLED

2001-15-01 AD 00 MANDATORY A/C *AD* INFLATION CYLINDER TRIGGER HOUSING COVER INSTALLATION Closed 28.Aug.20042001-15-01 (ACTIVE)PRODUCTION LINE PRR38275-10PRODUCTION LINE PRR38395SBB 737-25-1403-R1 (737-NG)SBB 737-25-1404-R1 (737-NGSBB 737-25-1405-R1 (737-CL)

ADPRRPRRSBSBSB

Perform within an unlimited threshold.2001-15-01/AD Rev.00 *AD* INFLATION CYLINDER TRIGGER HOUSING COVER INSTALLATION Closed 28.Aug.2004> 737-25-1405/SB* Rev.01 *AD* ESCAPE SLIDE (DOOR-MOUNTED) LATCH ASSEMBLY MODIFICATION Closed 28.Aug.2004


28.Aug.2004 44948:00/H 22546/CPerfRev.:'NOTE' / Reason: KKM 150238ITEM: 1


2001-15-17 AD 00 MANDATORY A/C *AD* ROCKWELL COLLINS - CTL-92 TRANSPONDER CONTROL PANEL Not ApplicableNot applicable. CTL-92 transponder control panel not installed onNAS B737.2001-15-17 (ACTIVE) ADReason for this StatusAUTO ASSIGNED





23.Oct.2014Page 162/429

Document-Number Type Rev Compliance A|C Subject Status2001-20-10 AD 00 MANDATORY A/C *AD* WIRE BUNDLES IN FOUR JUNCTION BOXES IN THE MAIN WHEEL W Closed 25.Oct.2003

2001-20-10 (ACTIVE)737-SL-24-111-E (REF)737-SL-24-111-F (REF)

ADSLSL F

Perform within an unlimited threshold.2001-20-10/AD Rev.00 *AD* WIRE BUNDLES IN FOUR JUNCTION BOXES IN THE MAIN WHEEL W Closed 25.Oct.2003> 737-SL-24-111/SL* Rev.D *AD* JUNCTION BOX IN MAIN WHEEL WELL, WIRE CHAFING Closed 25.Oct.2003


25.Oct.2003 42985:00/H 20792/CPerfRev.:'NOTE' / Reason: KKM 150052ITEM: 1


2001-22-13 AD 00 MANDATORY A/C *AD* RUDDER & TAB-RUDDER PEDAL PUSHROD FASTENER RPL Closed 23.Oct.20022001-22-13 (ACTIVE)737-27A1214 (REF)737-27A1214-R1 (ACTIVE)PRODUCTION PRR35404

ADSBSBPRR

Perform within an unlimited threshold.2001-22-13/AD Rev.00 *AD* RUDDER & TAB-RUDDER PEDAL PUSHROD FASTENER RPL Closed 23.Oct.2002> 737-27A1214/SB* Rev.01 *AD* RUDDER & TAB-RUDDER PEDAL PUSHROD FASTENER REPLACEMENT Closed 23.Oct.2002


23.Oct.2002PerfRev.:'NOTE' / Reason: DELIVERYDOC






23.Oct.2014Page 163/429


This mod is applicable to LN# 1-3110.2001-24-02 (SUPERSEDED)2003-20-08 (SUPERSEDED)2006-26-13 (ACTIVE)737-25-1412-R3 (ACTIVE)PRODUCTION MRR3259-1295

ADADADSBPRR

This Document has been SUPERSEDED BY 2006-26-13/AD Rev.002001-24-02/AD Rev.00 *AD* SUPERSEDED BY AD 2006-26-13 Not Applicable

This Document has been SUPERSEDED BY 2006-26-13/AD Rev.00> 737-25-1412/SB* Rev.03 **AD* OBSERVER/ATTENDANT SHOULDER RESTRAINT SYSTEM ATTACHMEN Not Applicable by Serial Number

2002-01-01 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 2006-12-23 Superseded (Superseded)2002-01-01 (SUPERSEDED)2006-12-23 (ACTIVE)737-55A1070 (REF)737-55A1070-R1 (ACTIVE)

ADADSBSB






23.Oct.2014Page 164/429

Document-Number Type Rev Compliance A|C Subject Status2002-02-08 AD 00 MANDATORY A/C *AD* MLG SUPPORT BEAM RETAINING PIN - BOLT & NUT REPLACEMENT Closed 30.Mar.2001

Per AD § (a) SB 737-57A1260 is to be performed.

NOTE 1 of the AD is not applicable to NAS. Some 737-200 may have alocknut installed, that is not actually covered by effectivity in SB737-57A1260. NAS does not operate B737-200.2002-02-08 (ACTIVE)737-57-1216-R2 (ACTIVE)737-57A1260-R1 (REF)737-57A1260-R2 (ACTIVE)737-57A1260-RO (REF)SBB 737-57A1260 (REF)

ADSBSBSBSBTA

Perform within an unlimited threshold.2002-02-08/AD Rev.00 *AD* MLG SUPPORT BEAM RETAINING PIN - BOLT & NUT REPLACEMENT Closed 30.Mar.2001> 737-57A1260/SB* Rev.02 MLG SUPPORT BEAM RETAINING PIN - BOLT & NUT REPLACEMENT Closed 30.Mar.2001








23.Oct.2014Page 165/429

Document-Number Type Rev Compliance A|C Subject Status2002-05-07 AD 00 RECOMMENDED A/C *AD* WINGS - TRAILING EDGE FLAP TRACK REPLACEMENT Superseded (Superseded / Special

Text: PRR 34707 (Prod. equivalentto SB 737-57-1203) OR SB737-57A1271)

This modification is applicable to LN# 1001-1910. The following LN#are Not Applicable due to PRR34707.2002-05-07 (ACTIVE)34707 (PRODUCTION)737-57-1203 (REF)737-57-1203 R1 (REF)737-57-1203 R2 (REF)737-57-1203 R3 (REF)737-57-1203 R4 (REF)737-57-1203 R5 (ACTIVE)

ADPRRSBSBSBSBSBSB


2002-06-05 AD 00 MANDATORY COMP *AD* ROCKWELL COLLINS ATC TRANSPONDERS P/N 522-2703-XXXX Not Applicable by Line Number /Special Text: PRR 34707 (Prod.equivalent to SB 737-57-1203) ORSB 737-57A1271

Transport category airplanes, certificated in any category, equippedwith Rockwell Collins Mode C 621A-3 Air Traffic Control (ATC)transponder(s), part number (P/N) 522-2703-XXX (where XXX is anyseries number).2002-06-05 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 166/429

Document-Number Type Rev Compliance A|C Subject Status2002-06-06 AD 00 MANDATORY COMP *AD* TDR-94 MODE S TRANSPONDERS Not Applicable by Line Number /

Special Text: PRR 34707 (Prod.equivalent to SB 737-57-1203) ORSB 737-57A1271

2002-06-06 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 167/429

Document-Number Type Rev Compliance A|C Subject Status2002-07-08 AD 00 MANDATORY A/C *AD* FIND AND FIX CRACKING OF CERTAIN FUSELAGE LAP JOINT REP Open

This mod is applicable to LN# 6-2565. The following LN# are NotApplicable per Boeing SB.1997-22-07 (SUPERSEDED)2002-07-08 (ACTIVE)37-SBB-53A1177P1 (REPETTITIVE)37-SBB-53A1177P2 (REPETTITIVE)37-SBB-53A1177P5 (REPETTITIVE)737-53A1177-R6 (ACTIVE)737-SL-53-063-A (REF)737-SL-53-063-B (REF)SBB 737-53A1177 (TASK)

ADADTATATASBSLSLTA


2002-07-08/AD Rev.00 *AD* FIND AND FIX CRACKING OF CERTAIN FUSELAGE LAP JOINT REP OpenThis Document SUPERSEDES 1997-22-07/AD Rev.00

> 737-53A1177/SB Rev.07 FUSELAGE - SKIN - REPAIR METHODS FOR CRACKS IN LOWER SKINS AT LAP JOINTSAND WINDOW CORNERS

Open

This Document SUPERSEDES 737-53A1177/SB Rev.06> > 737-53A1177-01/EO* Rev.01 FUSELAGE - SKIN - LAP JOINTS MODIFICATION (REPAIR) Open

This Document SUPERSEDES 737-53A1177-01/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

50000/C Perform initially before(F) 50000/C> > 737-53A1177-02/EO* Rev.00 FUSELAGE - SKIN - REPETITIVE LFEC INSP FOR AREAS OUTSIDE CROWN AREA Open

Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

70000/CPerform initially before(F) 70000/C /Interval(F):5000/C

> > 737-53A1177-03/EO* Rev.00 FUSELAGE - SKIN - FOLLOW ON LFEC LAP JOINT INSPECTIONS OpenDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT> > 737-53A1177-04/EO* Rev.00 FUSELAGE - SKIN - INSPECTION -- WINDOW CORNERS Open





23.Oct.2014Page 168/429

Document-Number Type Rev Compliance A|C Subject StatusDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document


> > 737-53A1177-05/EO* Rev.00 FUSELAGE - SKIN - SB 737-53A1177 TABLE 10 WINDOW CORNERS INSPECTION OpenDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document


> > 737-53A1177-06/EO* Rev.00 FUSELAGE - SKIN - SB 737-53A1177 TABLE 11 WINDOW CORNERS INSPECTION OpenDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document


> > 737-53A1177-07/EO* Rev.00 FUSELAGE - SKIN - SB 737-53A1177 TABLE 16-18 BUTT JOINT INSPECTION OpenDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT> > 737-53A1177-08/EO* Rev.00 FUSELAGE - SKIN - INSPECTION -- WINDOW CORNERS PROVENTIVE MODIFICATION Open

Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document60000/C Perform initially before(F) 60000/C

2002-07-10 AD 00 MANDATORY A/C *AD* FIND AND FIX CRACKING OF CERTAIN FUS. LAP JOINT REPAIRS Closed 01.Sep.2004This document is applicable to LN# 292-2565.2002-07-10 (ACTIVE)737-53A1177-R6 (ACTIVE)737-SL-53-063-A (REF)737-SL-53-063-B (REF)

ADSBSLSL


01.Sep.2004 44971:00/H 22565/CPerfRev.:'NOTE' / Reason: KKM 150273ITEM: 1






23.Oct.2014Page 169/429

Document-Number Type Rev Compliance A|C Subject Status2002-10-11 AD 00 MANDATORY A/C *AD* AFT PRESSURE BULKHEAD INSPECTION Superseded (Repetitive)

1984-20-03-R1 (SUPERSEDED)2002-10-11 (ACTIVE)37-SBB-53A1075 (REPETITIVE)737-53A1075 (REF)737-53A1075-R1 (REF)737-53A1075-R2 (REF)737-53A1075-R3 (ACTIVE)

ADADTASBSBSBSB

This Document has been SUPERSEDED BY 2014-05-02/AD Rev.R0

Thereafter perform in an interval of 1460/D2002-10-11/AD Rev.00 *AD* AFT PRESSURE BULKHEAD INSPECTION Repetitive

This Document has been SUPERSEDED BY 2014-05-02/AD Rev.R0> 737-53A1075/SB Rev.03 *AD* AFT PRESSURE BULKHEAD INSPECTION Repetitive> > 737-53A1075-01/EO* Rev.00 *AD* AFT PRESSURE BULKHEAD INSPECTION/MOD AND REP *** MANDATORY

REPETITIVE DETAILED VISUAL INSPECTION ***Repetitive

This Document SUPERSEDES 737-53A1075/EO Rev.03NOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

25.Feb.2016Perform initially within (effective from08.Apr.2014) (L) 120/D / Interval(F):730/D


25.Feb.2014 71572:00/H 43151/C N/APerfRev.:'03' / Reason: Initialized: Last perf.with 737-53A1075/EO/03





23.Oct.2014Page 170/429

Document-Number Type Rev Compliance A|C Subject Status2002-10-12 AD 00 MANDATORY A/C *AD* INSPECTION & REPLACEMENT OF AILERON TAB CONTROL ROD Closed 03.Apr.2001

2002-10-12 (ACTIVE)37-SBB-27-1223 (REPETITIVE)737-27-1223 (ACTIVE)737-27-1223 IN01PRODUCTION LINE PRR38275-2SBB 737-27-1223 (MOD-TASK)

ADTASBSBPRRTA

Perform BEFORE 20000/C2002-10-12/AD Rev.00 *AD* INSPECTION & REPLACEMENT OF AILERON TAB CONTROL ROD Closed 03.Apr.2001> 737-27-1223/SB Rev.00 *AD* INSP. & REPL. OF AILERON TAB CONTROL ROD Not Applicable> > 737-27-1223/EO* Rev.00 *AD* *AD* 2002-10-12 REPL. OF AILERON TAB CONTROL ROD Not Applicable by Serial Number

This Document is terminated with implementation of 737-27-1223-01/EO Rev.00> > 737-27-1223-01/EO* Rev.00 *AD* INSP. & REPL. OF AILERON TAB CONTROL ROD Closed 03.Apr.2001

This Document terminates 737-27-1223/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

03.Apr.2001PerfRev.:'NOTE' / Reason: DELEVIERYDOCS

Reason for this StatusDELEVIERY DOCS





23.Oct.2014Page 171/429

Document-Number Type Rev Compliance A|C Subject Status2002-13-03 AD 00 MANDATORY COMP REVISION OF ENGINE SHOP MANUAL. Information Only

Perform inspections of the parts at each piece-part opportunity inaccordance with the Inspection/Check section instructions.

Inspection at next piece-parts-exposure.2000-12-012002-13-03

ADAD

0000

This Document SUPERSEDES 2000-0294/AD Rev.00This Document SUPERSEDES 2000-12-01/AD Rev.00Affected Rotables (Part No/Serial No/Position) Status

CFM56-3B2 / 724473 Pos=LH (KKM)Information Only / Reason: AUTOASSIGNED

CFM56-3B2 / 725495 Pos=RH (KKM)Information Only / Reason: AUTOASSIGNED

2002-13-07 AD 00 MANDATORY COMP *AD* HONEYWELL IRU P/N HG1075AB05 AND HG1075GB05 SERIES Not Applicable by Serial Number2002-13-07 (ACTIVE)HG1075AB-34-A0013 (REF)HG1075GB-34-A0005 (REF)

ADSBSB






23.Oct.2014Page 172/429

Document-Number Type Rev Compliance A|C Subject Status2002-18-02 AD 00 MANDATORY A/C *AD* INSPECTION OF LOWER BEARING SUPPORT OF AIL TRANSFER MEC Closed 30.Mar.2001

2002-18-02 (ACTIVE)737-27A1238-R0 (ACTIVE)

ADSB

Perform within an unlimited threshold.2002-18-02/AD Rev.00 *AD* INSPECTION OF LOWER BEARING SUPPORT OF AIL TRANSFER MEC Closed 30.Mar.2001> 737-27A1238/SB* Rev.00 *AD* LATERAL TRANSFER MECH, LOWER BEARING SUPPORT INSP/MOD Closed 30.Mar.2001




2002-19-51 AD 01 MANDATORY A/C *AD* FLIGHT CONTROL MODULE INSPECTION FOR SUSPECT FCM Not ApplicableAD § j and k are covered by Remarks on the PN. This will avoidinstalling incorrect PN/SN.

SB 737-27-1261 is an AMOC to AD 2002-19-51R1. This SB definesapproved PN/SN.This Document SUPERSEDES 2002-19-51/AD Rev.00Perform BEFORE 17.Oct.2002

2002-19-51/AD Rev.01 *AD* FLIGHT CONTROL MODULE INSPECTION FOR SUSPECT FCM Not ApplicableThis Document SUPERSEDES 2002-19-51/AD Rev.00

> 2002-19-51-01/EO* Rev.00 *AD* FLIGHT CONTROL MODULE INSPECTION FOR SUSPECT FCM Not ApplicableReason for this StatusAFFECTED PN NOT INSTALLED.

> 2002-19-51-02/EO* Rev.00 *AD* FLIGHT CONTROL MODULE INSPECTION FOR SUSPECT FCM Not ApplicableAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 173/429

Document-Number Type Rev Compliance A|C Subject Status2002-19-51 AD 00 MANDATORY A/C *AD* FLIGHT CONTROL MODULE INSPECTION FOR SUSPECT FCM Superseded (Superseded)






23.Oct.2014Page 174/429

Document-Number Type Rev Compliance A|C Subject Status2002-20-07 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 2007-03-07 Superseded (Closed 17.Mar.2005)

FAA AMOC letter approves the modifications performed duringproduction, AFM entries and maintenance program as an AMOC to this ADfrom LN# 1268 and on.130S-03-191999-11-05 (SUPERSEDED)2002-20-07 (SUPERSEDED)2007-03-07 (ACTIVE)737-27-1246-01 (737-CL)737-27-1247-R1 (REF)737-27-1253-R3 (REF)737-27-1264-R0 (737-CL)737-27A1221-R1 (REF)PRODUCTION LINE PRR38275-140S

AMOCADADADSBSBSBSBSBPRR

00


2002-20-07/AD Rev.00 *AD* SUPERSEDED BY AD 2007-03-07 Closed 17.Mar.2005This Document has been SUPERSEDED BY 2007-03-07/AD Rev.00

> 737-27-1255/SB* Rev.02 *AD* RUDDER CONTROL SYSTEM; INSTALLATION OF NEW RUDDER SYS. Closed 17.Mar.2005This Document SUPERSEDES 737-27-1255/SB Rev.01This Document has been SUPERSEDED BY 737-27-1255/SB Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-27-1255/SB* Rev.00 *AD* RUDDER CONTROL SYSTEM; INSTALLATION OF NEW RUDDER SYS. SupersededThis Document has been SUPERSEDED BY 737-27-1255/SB Rev.01

> 737-27-1255/SB* Rev.01 *AD* RUDDER CONTROL SYSTEM; INSTALLATION OF NEW RUDDER SYS. SupersededThis Document SUPERSEDES 737-27-1255/SB Rev.00This Document has been SUPERSEDED BY 737-27-1255/SB Rev.02





23.Oct.2014Page 175/429

Document-Number Type Rev Compliance A|C Subject Status> 737-27-1264/SB* Rev.02 *AD* RUDDER & RUD. TRIM CTRL SYST. REPLACEMENT OF P5-3 PANEL Closed 17.Mar.2005




> 737-55-1052/SB* Rev.01 *AD* VERTICAL STAB, TRAILING EDGE BEAM INSPECTION & REWORK Closed 10.Mar.2005Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



2002-20-09 AD 00 MANDATORY COMP *AD* MODEL AFD-3010 FLIGHT DISPLAY UNIT Not Applicable by Serial Number2002-20-09 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

2002-21-01 AD 00 MANDATORY A/C *AD* BRITAX SELL GMBH & CO OHG - WATER BOILERS, COFFEE MAKER Not ApplicableNot applicable due to the affected PN not installed on NAS B737.This Document SUPERSEDES 2001-10-13/AD Rev.00Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 176/429

Document-Number Type Rev Compliance A|C Subject Status2003-03-05 AD 00 MANDATORY A/C *AD* LEADING EDGE SLATS/INSP. FOR VIBRO-ENGRAVED ROD ENDS Closed 18.Dec.2001

2000-02-03 (SUPERSEDED)2003-03-05 (ACTIVE)737-27-1174-RO (REF)737-27A1243-R0 (ACTIVE)737-SRP-27-0138 (REF)SBB-737-27A1243 (MOD-TASK)

ADADSBSBSRPTA


2003-03-05/AD Rev.00 *AD* LEADING EDGE SLATS/INSP. FOR VIBRO-ENGRAVED ROD ENDS Closed 18.Dec.2001This Document SUPERSEDES 2000-02-03/AD Rev.00

> 737-27A1211/SB* Rev.03 FLIGHT CONTROLS - LIFT AUGMENTATION - LEADING EDGE FLAPS AND SLATSREPLACEMENT OF THE ROD ENDS FOR THE LEADING EDGE SLAT ACTUATORS

See prev. Docstatus / Special Text:This aircraft is Not Applicable due toPRODUCTION LINE PRR35005-175

This Document SUPERSEDES 737-27A1211/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks18.Dec.2001 PerfRev.:'NOTE'Reason for this StatusDELIVERY DOC.

> 737-27A1243/SB* Rev.03 *AD* LEADING EDGE SLATS-INSPECT. FOR VIBRO-ENGRAVED ROD ENDS Closed 06.Dec.2001Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







23.Oct.2014Page 177/429

Document-Number Type Rev Compliance A|C Subject Status2003-03-11 AD 00 MANDATORY COMP *AD* AIR CRUISERS COMPANY - EMERGENCY EVACUATION SLIDE/RAFT Superseded (Not Applicable by

Serial Number)2003-03-11 (ACTIVE) ADThis Document has been SUPERSEDED BY 2004-03-01/AD Rev.00Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

2003-03-15 AD 01 MANDATORY A/C *AD* REVISION OF AIRPLANE FLIGHT MANUAL Closed 07.Mar.20032003-03-15-R1 (ACTIVE)AD 2003-03-15 (TASK)

ADTA


07.Mar.2003PerfRev.:'NOTE' / Reason: AIRPLANEFLIGHT MANUAL REVISED

Reason for this StatusAIRPLANE FLIGHT MANUAL REVISED

2003-03-15 AD 00 MANDATORY A/C *AD* REVISION OF AIRPLANE FLIGHT MANUAL Superseded (Information Only)2003-03-15-R1 (ACTIVE)AD 2003-03-15 (TASK)

ADTA

This Document has been SUPERSEDED BY 2003-03-15/AD Rev.01Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 178/429

Document-Number Type Rev Compliance A|C Subject Status2003-04-06 AD 00 MANDATORY COMP *AD* HONEYWELL PRIMUS II RNZ-850/-851 INTEGRATED NAVIGATION Superseded (Not Applicable by

Serial Number / Special Text: NASonly opearates AC in group 2 and 4.)

2003-04-06 (ACTIVE) ADThis Document has been SUPERSEDED BY 2006-22-05/AD Rev.00Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

2003-07-12 AD 00 MANDATORY COMP *AD* MLG/NLG LIFE LIMITED COMPONENTS TRACKING & S/N ADDITION Closed 11.Sep.20062003-07-12 (ACTIVE)737-32-1322-R1 (ACTIVE)737-32-1322-RO (REF)737-SRP-32-0058 (REF)AD 2003-07-12 (INSP-TASK)SBB 737-32-1322P1 (REPET)SBB 737-32-1322P2 (INSP-TASK)

ADSBSBSRPTATATA

Perform BEFORE 20.May.20132003-07-12/AD Rev.00 *AD* MLG/NLG LIFE LIMITED COMPONENTS TRACKING & S/N ADDITION Closed 11.Sep.2006> 737-32-1322/SB* Rev.01 *AD* MLG/NLG LIFE LIMITED COMPONENTS TRACKING & S/N ADDITION Closed 11.Sep.2006


65-73762-21 / T3011 Pos=FWD (KKM)Closed / Last Performed:11.Sep.200627172/C RefDocument:SRT E0553431 OH2006 Rev.01

65-73761-127 / MC03525 Pos=LH (KKM)Closed / Last Performed:08.Jul.200527929/C RefDocument:PCW SRTE0403521 OH 2005 Rev.01

65-73761-128 / MC03526 Pos=RH (KKM)Closed / Last Performed:08.Jul.200527979/C RefDocument:PCW SRTE0403522 OH 2005 Rev.01





23.Oct.2014Page 179/429

Document-Number Type Rev Compliance A|C Subject Status2003-08-15 AD 00 MANDATORY A/C *AD* FUSELAGE, CROWN SKIN LAP JOINT INSPECTION FOR CRACKING Superseded (Cancelled)

This mod is applicable to LN# 1-2552. The following LN# are notapplicabel.2003-08-15 (ACTIVE)737-53A1255 (ACTIVE)

ADSB

This Document has been SUPERSEDED BY 2013-09-01/AD Rev.00Perform BEFORE 45000/C

2003-08-15/AD Rev.00 *AD* FUSELAGE, CROWN SKIN LAP JOINT INSPECTION FOR CRACKING CancelledThis Document has been SUPERSEDED BY 2013-09-01/AD Rev.00

> 737-53A1255/SB* Rev.00 FUSELAGE, CROWN SKIN LAP JOINT INSPECTION FOR CRACKING CancelledThis Document has been SUPERSEDED BY 737-53A1255/SB Rev.01Reason for this StatusManually deassigned after Document Cancelled or Superseded

2003-14-04 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 2005-12-05 Superseded (Cancelled)2003-14-04 (SUPERSEDED)2005-12-05 (SUPERSEDED)2007-10-12 (ACTIVE)C&D B221001-52-03-R3 (REF)ST01335LA (REF)

ADADADSBSTC






23.Oct.2014Page 180/429

Document-Number Type Rev Compliance A|C Subject Status2003-14-06 AD 00 MANDATORY A/C *AD* DETECT/CORRECT FATIGUE CRACKS IN THE LAP JOINTS Closed 07.Feb.2008

This mod is applicable to LN# 292-2947.2004-7997 (REF)737-53-1179 IN-03AMOC 120S-03-732AMOC 120S-05-312M-7200-03-01505

ADSBADADDOCR

0000000000

Perform within an unlimited threshold.2003-14-06/AD Rev.00 *AD* DETECT/CORRECT FATIGUE CRACKS IN THE LAP JOINTS Closed 07.Feb.2008> 737-53-1179/SB* Rev.02 BONDED SKIN DOUBLERS (TEAR STRAPS) DELAMINATION INSPECTION Closed 07.Feb.2008

This Document terminates AD-2003-14-06-1/EO Rev.00This Document terminates AD-2003-14-06-2/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> AD-2003-14-06-1/EO* Rev.00 *AD* *AD* DETECT AND CORRECT FATIGUE CRACKS IN LAP JOINTS.E CancelledThis Document is terminated with implementation of 737-53-1179/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

15.Nov.2004 45537:00/H 23037/CWas due at: 23537/C PerfRev.:'NOTE' /Reason: AMICOS WO 150316 KKM LAPJOINT CRACK INSP.-

Reason for this StatusTERMINATED BY SB 737-53-1179

> AD-2003-14-06-2/EO* Rev.00 *AD* NDT INSP TO DETECT AND CORRECT FATIGUE CRACKS IN LAP JOINTS. CancelledThis Document is terminated with implementation of 737-53-1179/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

07.Feb.2008 54542:00/H 30315/CPerfRev.:'NOTE' / Reason: AMICOS WO151166 KKM37-AD-2003-14-06-2*AD*LAP JOI





23.Oct.2014Page 181/429

Document-Number Type Rev Compliance A|C Subject StatusReason for this StatusTERMINATED BY SB 737-53-1179

2003-20-08 AD 00 MANDATORY A/C *AD* ATTENDANT SEAT - CHANGE ATTACHMENT OF SHOULDER RESTRAIN Superseded (Not Applicable)This mod is applicable to LN# 1-3110.2001-24-02 (SUPERSEDED)2003-20-08 (SUPERSEDED)2006-26-13 (ACTIVE)737-25-1412-R3 (ACTIVE)PRODUCTION MRR3259-1295

ADADADSBPRR


2003-20-08/AD Rev.00 *AD* ATTENDANT SEAT - CHANGE ATTACHMENT OF SHOULDER RESTRAIN Not ApplicableThis Document has been SUPERSEDED BY 2006-26-13/AD Rev.00

> 737-25-1412/SB* Rev.03 **AD* OBSERVER/ATTENDANT SHOULDER RESTRAINT SYSTEM ATTACHMEN Not Applicable by Serial Number





23.Oct.2014Page 182/429

Document-Number Type Rev Compliance A|C Subject Status2003-23-05 AD 00 MANDATORY A/C *AD* MANUFACTURE DATE CODE ON TITEFLEX HOSES - INSPECTION OF Closed 10.Aug.2004

2003-23-05 (ACTIVE)737-26A1082-R0 (REF)737-26A1108-R1 (ACTIVE-CL)737-26A1109-R3 (ACTIVE-NG)737-SRP-73-0028 (REF)SBB-737-26A1108 (MOD-TASK)

ADSBSBSBSRPTA

Perform BEFORE 24.Dec.20052003-23-05/AD Rev.00 *AD* MANUFACTURE DATE CODE ON TITEFLEX HOSES - INSPECTION OF Closed 10.Aug.2004> 737-26A1108/SB* Rev.01 *AD* ENGINE & CARGO COMPT FIRE EXT BOTTLE HOSES INSPECTION Closed 10.Aug.2004 / Special Text:

GROUP 4 OR 5 AIRPLANEPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



2003-24-08->2002-22-05/AD

AD 00 MANDATORY A/C *AD* WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSP FOR CRACKS. & FLAP GAPCHECK

Superseded (Superseded)






23.Oct.2014Page 183/429

Document-Number Type Rev Compliance A|C Subject Status2003-26-01 AD 00 MANDATORY A/C *AD* RUDDER, ACTUATOR, LOOSE BOLTS ON ATTACH FITTINGS Repetitive

FAA AMOC letter approves performing Stage 2 and Stage 3 inspectionsin liu of Stage 1 inspections as an AMOC to this AD.120S-04-174 (ACTIVE)2003-26-01 (ACTIVE)737-55A1087 (REF)737-55A1087 IN 01 (REF)737-55A1087 IN 02 (REF)737-55A1087 IN 03 (ACTIVE)

AMOCADSBSBSBSB

Perform BEFORE 4500/CPerform BEFORE 6000/H

2003-26-01/AD Rev.00 *AD* RUDDER, ACTUATOR, LOOSE BOLTS ON ATTACH FITTINGS Repetitive> 737-55A1087/SB Rev.00 *AD* RUDDER, ACTUATOR, LOOSE BOLTS ON ATTACH FITTINGS Repetitive> > 737-55A1087-01/EO* Rev.00 *AD* RUDDER, ACTUATOR, LOOSE BOLTS ON ATTACH FITTINGS Closed 10.Mar.2005




> > 737-55A1087-1/EO* Rev.00 *AD* RUDDER, ACTUATOR ATTACH FITTINGS, INSP FOR LOOSE Not Applicable by Serial Number> > 737-55A1087-3/EO* Rev.00 *AD* RUDDER-MAIN & AUX ACTUATOR ATTACH FITTINGS TORQUE CHECK **

STAGE 3 - REPEAT TORQUE CHECK/REWORK **Repetitive


77572:00/H 47651/CPerform initially before(F) 52130/H or28075/C / Interval(F):6000/H or 4500/C


14.Feb.2014 71572:00/H 43151/C 489492, N/AWas due at: 45070/C and 4448340/HPerfRev.:'00'





23.Oct.2014Page 184/429

Document-Number Type Rev Compliance A|C Subject Status2003-26-08 AD 00 MANDATORY A/C *AD* PRESSURE RELIEF VALVE REPLACM. ON WATER TANK PRESS SYST Not Applicable

Effectivity logic:Sb 737-38-1029:This modification is applicable for Specific Var#. The Other VAR#are Not Applicable Per PRR34978.

SB 737-38A1038:This modification is applicable for LN# 2524-2696. The Other LN#are Not Applicable Per PRR35005-98.

SB 737-38A1047:This modification is applicable for LN# 1629-2478.737-38-1029737-38A1038737-38A1047737-38A1047737-38A1047PRODUCTION PRR34978PRODUCTION PRR35005-98

SBSBSBSBSBPRRPRR

01020001020000

2003-26-08/AD Rev.00 *AD* PRESSURE RELIEF VALVE REPLACM. ON WATER TANK PRESS SYST Not Applicable> 737-38-1029/SB* Rev.01 *AD* PRESS/RELIEF VALVE IN THE POTABLE WATER PNEU/PRESS/SYST Not Applicable

This Document SUPERSEDES 737-38-1029/SB Rev.00> 737-38A1038/SB* Rev.02 *AD* PRESSURE RELIEF VALVE REPLACEMENT Not Applicable by Serial Number> 737-38A1047/SB* Rev.02 *AD* PRESSURE RELIEF VALVE REPLACM. ON WATER TANK PRESS SYST Closed 21.Dec.2000








23.Oct.2014Page 185/429

Document-Number Type Rev Compliance A|C Subject Status2003-26-14 AD 00 MANDATORY COMP *AD* WALTER KIDDE HAND-HELD HALON FIRE EXTINGUISHER CERTAIN Not Applicable

2003-26-14 (ACTIVE)737-SL-26-043 (REF)W.K.898052-26-449 (ACTIVE)

ADSLSB

Affected Rotables (Part No/Serial No/Position) Status898052 / X-655307 Pos=FWD#2 (KKM) Not Applicable898052 / Y-172221 Pos=AFT (KKM) Not Applicable898052 / W-567324 Pos=AFT (KKM) Not Applicable

2003-26-14/AD* Rev.00 *AD* WALTER KIDDE HAND-HELD HALON FIRE EXTINGUISHER CERTAIN Not Applicable by Serial NumberAffected Rotables (Part No/Serial No/Position) Status898052 / X-655307 Pos=FWD#2 (KKM) Not Applicable898052 / Y-172221 Pos=AFT (KKM) Not Applicable898052 / W-567324 Pos=AFT (KKM) Not Applicable

> 737-SL-26-043/SL* Rev.00 EMERGENCY EQUIPMENT - PORTABLE HALON EXTINGUISHERS PN: 898052 RECALLOF


Affected Rotables (Part No/Serial No/Position) Status898052 / X-655307 Pos=FWD#2 (KKM) Not Applicable898052 / Y-172221 Pos=AFT (KKM) Not Applicable898052 / W-567324 Pos=AFT (KKM) Not Applicable





23.Oct.2014Page 186/429

Document-Number Type Rev Compliance A|C Subject Status2004-02-08 AD 00 MANDATORY A/C *AD* ESCAPE SLIDE COMPARTMENT HINGE ASSEMBLY REPLACEMENT Closed 08.Mar.2005

This document is applicable to LN# 1-3132.2004-02-08737-25-1430

ADSB

0001

Perform BEFORE 04.Mar.20072004-02-08/AD Rev.00 *AD* ESCAPE SLIDE COMPARTMENT HINGE ASSEMBLY REPLACEMENT Closed 08.Mar.2005> 737-25-1430/SB* Rev.01 ESCAPE SLIDE COMPARTMENT HINGE ASSEMBLY REPLACEMENT Closed 08.Mar.2005




2004-03-01 AD 00 MANDATORY COMP *AD* AIR CRUISERS COMPANY EMERGENCY EVACUATION SLIDE/RAFT Not Applicable by Line Number2004-03-01 (ACTIVE) ADThis Document SUPERSEDES 2003-03-11/AD Rev.00Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

2004-03-23 AD 00 MANDATORY A/C *AD* MAIN DECK CARGO DOOR FRAMES, TO DETECT/CORRECT CRACKING Not ApplicableNAS does not operate Aircraft with Main Deck Cargo door.2001-08-07 (SUPERSEDED)2004-03-23 (ACTIVE)737-52-0037 (PEMCO)

ADADSB

This Document SUPERSEDES 2000-17-51/AD Rev.00This Document SUPERSEDES 2001-08-07/AD Rev.00Reason for this StatusNO MAIN DECK CARGO DOOR





23.Oct.2014Page 187/429

Document-Number Type Rev Compliance A|C Subject Status2004-03-34 AD 00 MANDATORY A/C *AD* ESCAPE SLIDE AFT LATCH CABLE ASSY MOUNTING FASTENERS Superseded (Superseded)

2004-03-34 (SUPERSEDED)2004-03-34-R1 (ACTIVE)737-25-1434-R0 (ACTIVE)SBB 737-25-1434 (MOD-TASK)

ADADSBTA


2004-03-34 AD 01 MANDATORY A/C *AD* ESCAPE SLIDE AFT LATCH CABLE ASSY MOUNTING FASTENERS Closed 08.Mar.20052004-03-34737-25-1434

ADSB

0000

This Document SUPERSEDES 2004-03-34/AD Rev.00Perform BEFORE 21.Jul.2007

2004-03-34/AD Rev.01 *AD* ESCAPE SLIDE AFT LATCH CABLE ASSY MOUNTING FASTENERS Closed 08.Mar.2005This Document SUPERSEDES 2004-03-34/AD Rev.00

> 737-25-1434/SB* Rev.00 *AD* ESCAPE SLIDE AFT LATCH CABLE ASSY MOUNTING FASTENERS Closed 08.Mar.2005Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







23.Oct.2014Page 188/429

Document-Number Type Rev Compliance A|C Subject Status2004-04-03 AD 02 MANDATORY A/C CREW SEATS - REAR TRACK LOCK BRACKET BOLTS INSPECTION Closed 12.Jun.2004

This Document SUPERSEDES 2000-10-21/AD Rev.00Perform WITHIN 90/D (effective from 24.Mar.2004)

2004-04-03/AD Rev.02 CREW SEATS - REAR TRACK LOCK BRACKET BOLTS INSPECTION Closed 12.Jun.2004This Document SUPERSEDES 2000-10-21/AD Rev.00

> 737-25A1363/SB* Rev.00 *AD* CREW SEATS, REAR TRACK LOCK BRACKET BOLTS INSPECTION SupersededThis Document has been SUPERSEDED BY 737-25A1363/SB Rev.01

> 737-25A1363/SB* Rev.02 *AD* CREW SEATS, REAR TRACK LOCK BRACKET BOLTS INSPECTION See prev. DocstatusThis Document SUPERSEDES 737-25A1363/SB Rev.01This Document has been SUPERSEDED BY 737-25A1363/SB Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks12.Jun.2004 44399:00/H 22146/C PerfRev.:'NOTE'Reason for this StatusKKM 150228 ITEM: 1

> 737-25A1363/SB* Rev.01 *AD* CREW SEATS, REAR TRACK LOCK BRACKET BOLTS INSPECTION Closed 12.Jun.2004This Document SUPERSEDES 737-25A1363/SB Rev.00This Document has been SUPERSEDED BY 737-25A1363/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

12.Jun.2004 44399:00/H 22146/CPerfRev.:'NOTE' / Reason: KKM 150228ITEM: 1






23.Oct.2014Page 189/429

Document-Number Type Rev Compliance A|C Subject Status2004-06-18 AD 00 MANDATORY A/C *AD* REPLACING VALVE SEALS AND PERFORMING LEAK TESTS Closed 17.Mar.2005

2004-06-18 (ACTIVE)37-AD-2004-06-18-1 (REPET)37-AD-2004-06-18-2 (REPET)37-AD-2004-06-18-3 (REPET)37-AD-2004-06-18-4 (REPET)37-AD-2004-06-18-5 (REPET)AD 2004-06-18 (TASK)

ADTATATATATATA








23.Oct.2014Page 190/429

Document-Number Type Rev Compliance A|C Subject Status2004-06-18-2 AD 00 MANDATORY A/C *AD* LAVATORY FLUSH/FILL LINES - LEVER/LOCK CAP REPLACEMENT Closed 17.Mar.2005 / Special Text:

Inital seal repl. and leak test only.Repetitive insp: 2004-06-18SUB1

AD 2004-06-18 Paragraph (f) gives instructions to, before 5000 fhfrom eff date of AD, perform one of the following options:1) Install an FAA-approved lever/lock cap on the flush/fill linesfor all lavatories,or,2) Install a vacuum break check valve having Monogram p/n series3765-190, Shaw Aero Devices p/n series 301-0009, or otherFAA-approved vacuum break check valve in the flush/fill lines forall lavatories,or,3) Install a flush/fill ball valve Kaiser Electroprecision p/nseries 0062-0009 on the flush/fill lines for all lavatories,or,4) Install an FAA-approved shut-off valve that uses a mechanical orelectrical device on the flush/fill lines for all lavatories.2004-06-18 (ACTIVE)AD 2004-06-18-2 (MOD-TASK)

ADTA

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Mar.2005 46134:00/H 23577/C PerfRev.:'NOTE' / Reason: WO#150387Reason for this StatusWO#150387





23.Oct.2014Page 191/429

Document-Number Type Rev Compliance A|C Subject Status2004-06-18SUB1 AD 00 MANDATORY A/C *AD* TO PREVENT DAMAGE TO AIRCRAFT AS A RESULT OF BLUE ICE Repetitive

2004-06-18 (ACTIVE)37-AD-2004-06-18-1 (REPET)37-AD-2004-06-18-2 (REPET)37-AD-2004-06-18-3 (REPET)37-AD-2004-06-18-4 (REPET)37-AD-2004-06-18-5 (REPET)AD 2004-06-18 (TASK)

ADTATATATATATA

Perform within an unlimited threshold.2004-06-18SUB1/AD Rev.00 *AD* TO PREVENT DAMAGE TO AIRCRAFT AS A RESULT OF BLUE ICE Repetitive> AD-2004-06-18-1/EO* Rev.00 *AD* *AD* LEAK CHECK OF FWD TOILET SERVICE SYSTEM Repetitive


74319:36/HPerform initially before(F) 0/H /Interval(F):1000/H

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks14.Oct.2014 73319:36/H 44494/C 15696656, Was due at: 4411657/H PerfRev.:'00'

> AD-2004-06-18-2/EO* Rev.00 *AD* *AD* LEAK CHECK OF AFT TOILET SERVICE SYSTEM RepetitiveNOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentNOTE: 'Whichever comes later' calculation logic applicable for the intervalDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

24.Feb.2015 74057:59/H

Perform initially before(L) 0/H Performinitially within (effective from ManufacturerDate 13.Mar.1990) (L) 0/D /Interval(L):1000/H or 180/D


28.Aug.2014 73057:59/H 44302/C 554392,Was due at: 31.Aug.2014 and 4354320/HPerfRev.:'00'

> AD-2004-06-18-3/EO* Rev.00 *AD* FWD & AFT LAVATORY FLUSH/FILL LINES RepetitiveNOTE: 'Whichever comes later' calculation logic applicable for the intervalDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document





23.Oct.2014Page 192/429


28.Feb.2018 76572:00/H

Perform initially before(F) 0/H Performinitially within (effective from ManufacturerDate 13.Mar.1990) (F) 0/D /Interval(L):5000/H or 1460/D


01.Mar.2014 71572:00/H 43151/C 489215, N/AWas due at: 07.Nov.2016 and 4388340/HPerfRev.:'00'

> AD-2004-06-18-4/EO* Rev.00 FORWARD LAVATORY DRAIN SYSTEM, SEAL CHANGE RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

01.Aug.2015Perform initially within (effective fromManufacturer Date 13.Mar.1990) (F) 0/D /Interval(F):540/D


> AD-2004-06-18-5/EO* Rev.00 AFT LAVATORY DRAIN SYSTEM, SEAL CHANGE RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

30.Jul.2015Perform initially within (effective fromManufacturer Date 13.Mar.1990) (F) 0/D /Interval(F):540/D


2004-08-16 AD 00 MANDATORY COMP *AD* NARCO AVIONICS INC . AT150 TRANSPONDERS Not Applicable by Serial Number2004-08-16 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 193/429

Document-Number Type Rev Compliance A|C Subject Status2004-10-06 AD 00 MANDATORY A/C *AD* HYD HEAT EXCHANGER, ELECT. BONDING AT FITTING INTO TANK Closed 19.May.2002

2004-10-06 (ACTIVE)737-29A1096-R0 (REF)737-29A1096-R1 (REF)737-29A1096-R2 (ACTIVE)SBB 737-29A1096 (MOD-TASK)

ADSBSBSBTA

Perform BEFORE 21.Jun.20092004-10-06/AD Rev.00 *AD* HYD HEAT EXCHANGER, ELECT. BONDING AT FITTING INTO TANK Closed 19.May.2002> 737-29A1096/SB* Rev.02 *AD* HYD HEAT EXCHANGER, ELECT. BONDING AT FITTING INTO TANK Closed 19.May.2002




2004-10-13 AD 00 MANDATORY COMP MAIN FUEL PUMPS EQUIP. WITH SOLID BRONZE BEARING - REPL. Closed 27.Jun.20122004-10-133-73-01043-73-0120

ADSBSB

000306

Perform BEFORE 01.Jan.20072004-10-13/AD Rev.00 MAIN FUEL PUMPS EQUIP. WITH SOLID BRONZE BEARING - REPL. Closed 27.Jun.2012> 3-73-0120/SB* Rev.06 MAIN FUEL PUMPS EQUIP. WITH SOLID BRONZE BEARING - REPL. Closed 27.Jun.2012

Affected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 724473 Pos=LH (KKM) Not Applicable / Reason: 39729

CFM56-3B2 / 725495 Pos=RH (KKM)

Closed / Reason: PB: PREVIOUSLYEMBODIED / Last Performed:27.Jun.201264007:00/H 38431/C RefDocument:MTURECORDED MOD SHEET WO 51734400Rev.06





23.Oct.2014Page 194/429

Document-Number Type Rev Compliance A|C Subject Status2004-13-20 AD 00 MANDATORY A/C *AD* GARMIN AT,APOLLO GX SERIES GPS NAV UNITS Not Applicable

Not applicable due to the PN not installed on NAS B737.2004-12-20 (ACTIVE) ADReason for this StatusAUTO ASSIGNED





23.Oct.2014Page 195/429

Document-Number Type Rev Compliance A|C Subject Status2004-15-04 AD 00 MANDATORY A/C *AD* FUEL/PRESSURE FUELING SYSTEM/ADD SLEEVES TO THE WIRES Closed 17.Mar.2005

1999-05-12 (SUPERSEDED)2004-15-04 (ACTIVE)737-28A1132-R0 (REF)737-28A1132-R1 (REF)737-28A1132-R2 (REPLACED)737-28A1141-R4 (ACTIVE)SBB 737-28A1132 (MOD-TASK)

ADADSBSBSBSBTA


2004-15-04/AD Rev.00 *AD* FUEL/PRESSURE FUELING SYSTEM/ADD SLEEVES TO THE WIRES Closed 17.Mar.2005This Document SUPERSEDES 1999-05-12/AD Rev.00

> 737-28A1132/SB* Rev.02 *AD* FUEL/PRESSURE FUELING SYSTEM/ADD SLEEVES TO THE WIRES Not ApplicableThis Document has been CANCELLED BY 737-28A1141/SB Rev.02Reason for this StatusSB REPLACED BY 737-28A1141

> 737-28A1141/SB* Rev.04 *AD* PRESSURE FUELING SYSTEM - IMPR. FUELING FLOAT SWITCH See prev. DocstatusThis Document SUPERSEDES 737-28A1141/SB Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Mar.2005 46130:00/H 23575/C PerfRev.:'NOTE'Reason for this StatusKKM 150398 ITEM: 1

> 737-28A1141/SB* Rev.02 *AD* PRESSURE FUELING SYSTEM - IMPR. FUELING FLOAT SWITCH SupersededThis Document CANCELS 737-28A1132/SB Rev.02This Document SUPERSEDES 737-28A1141/SB Rev.01This Document has been SUPERSEDED BY 737-28A1141/SB Rev.03

> 737-28A1141/SB* Rev.03 *AD* PRESSURE FUELING SYSTEM - IMPR. FUELING FLOAT SWITCH Closed 17.Mar.2005This Document SUPERSEDES 737-28A1141/SB Rev.02This Document has been SUPERSEDED BY 737-28A1141/SB Rev.04Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks





23.Oct.2014Page 196/429




2004-18-06 AD 00 MANDATORY A/C *AD* FUSELAGE SKIN CHEM-MILL LINE CRACK INSPECTION/REPAIR Superseded (Superseded)This mod is applicable to LN# 292-2565.2004-18-06 (ACTIVE)737-53A1210-R0 (REF)737-53A1210-R1 (ACTIVE)

ADSBSB






23.Oct.2014Page 197/429

Document-Number Type Rev Compliance A|C Subject Status2004-19-10 AD 00 MANDATORY A/C *AD* HORIZONTAL STABILIZER HINGE PIN INSP. & CORROSION PREV. Repetitive

2004-19-10 (ACTIVE)37-SBB-55A1077-P1 (REPETITIVE)37-SBB-55A1077-P2 (REPETITIVE)37-SBB-55A1077-P3 (REPETITIVE)737-55A1077 IN01 (REF)737-55A1077-RO (ACTIVE)

ADTATATASBSB

Perform within an unlimited threshold.2004-19-10/AD Rev.00 *AD* HORIZONTAL STABILIZER HINGE PIN INSP. & CORROSION PREV. Repetitive> 737-55A1077/SB Rev.00 *AD* HORIZONTAL STABILIZER HINGE PIN INSP. & CORROSION PREV. Repetitive> > 737-55A1077-P1/EO* Rev.00 *AD* *AD* HORIZONTAL STAB. - DET. VISUAL INSP OF HINGE PIN Not Applicable by Serial Number> > 737-55A1077-P2/EO* Rev.00 *AD* HORIZONTAL STAB. - INNER & OUTER HINGE PIN INSPECTION ***

MANDATORY REPETITIVE VISUAL INSPECTION ***Repetitive


01.Nov.2016 76139:00/HPerform initially within (effective fromManufacturer Date 13.Mar.1990) (F) 0/D or0/H / Interval(F):1460/D or 8000/H


02.Nov.2012 68139:00/H 40570/C 273609, N/AWas due at: 23.Mar.2014 and 4132020/HPerfRev.:'00'

> > 737-55A1077-P3/EO* Rev.00 *AD* HORIZONTAL STAB. - INNER & OUTER HINGE PIN INSPECTION ***MANDATORY REPETITIVE VISUAL INSPECTION ***

Repetitive


31.Oct.2020 84139:00/H

Perform initially before(F) 61435/H Performinitially within (effective from ManufacturerDate 13.Mar.1990) (F) 8269/D /Interval(F):16000/H or 2920/D


02.Nov.2012 68139:00/H 40570/C 273647, N/AWas due at: 05.Feb.2016 and 4232520/HPerfRev.:'00'





23.Oct.2014Page 198/429

Document-Number Type Rev Compliance A|C Subject Status2004-22-01 AD 00 MANDATORY A/C *AD* CARGO RESTRAINT STRAP ASSEMBLIES Not Applicable

NAS has no Aircraft with STC ST01004NY installed.ST01004NY STC 00Reason for this StatusAUTO ASSIGNED

2004-22-05 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 2009-07-11 Superseded (Closed 13.Feb.1999)The AMOC letter approves SRM repairs as an AMOC to the SB repair.120S-04-485 (ACTIVE)2004-22-05 (SUPERSEDED)2009-07-11 (ACTIVE)37-SBB-53A1266 (DELETED)37-SBB-55-1057P1 (REPLACED)737-55-1057-R0 (REPLACED)737-55-1057-R1 (REPLACED)

AMOCADADTATASBSB


2004-22-05/AD Rev.00 *AD* SUPERSEDED BY AD 2009-07-11 Closed 13.Feb.1999This Document has been SUPERSEDED BY 2009-07-11/AD Rev.00

> 737-55-1057/SB* Rev.00 *AD* VERTICAL STAB. AUX STRUC., DORSAL FIN AY INSP/PREV MOD Closed 13.Feb.1999Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

13.Feb.1999PerfRev.:'NOTE' / Reason: REPLACED BYSB737-53A1266

Reason for this StatusREPLACED BY SB737-53A1266





23.Oct.2014Page 199/429

Document-Number Type Rev Compliance A|C Subject Status2004-23-07 AD 00 MANDATORY A/C *AD* FUSELAGE, GALLEY NO 2 UPPER ATTACHMENT SUPPORT. Not Applicable

AC that have status Not Applicable are either NA per SB effectivityor have reduced Galley weight.PRODUCTION PRR34961 PRRThis Document SUPERSEDES 1995-02-08/AD Rev.01Perform within an unlimited threshold.

2004-23-07/AD Rev.00 *AD* FUSELAGE, GALLEY NO 2 UPPER ATTACHMENT SUPPORT. Not ApplicableThis Document SUPERSEDES 1995-02-08/AD Rev.01

> 737-53-1154/SB* Rev.02 *AD* FUSELAGE, GALLEY NO 2 UPPER ATTACHMENT SUPPORT Not ApplicableReason for this StatusN/A - SB EFFECTIVITY





23.Oct.2014Page 200/429

Document-Number Type Rev Compliance A|C Subject Status2005-03-02 AD 00 MANDATORY A/C *AD* AIR CONDITION OVERHEAD DUCT LANYARD INSTALLATION Closed 07.Feb.2008

This mod is applicable to LN# 1001-2813.2005-03-02 (ACTIVE)737-21-1131 (REF)737-21-1131-R1 (REF)737-21-1131-R2 (ACTIVE)AD 2005-03-02(SECONDARY-TASK)SBB 737-21-1131 (MOD-TASK)

ADSBSBSBTATA

Perform BEFORE 09.Mar.20112005-03-02/AD Rev.00 *AD* AIR CONDITION OVERHEAD DUCT LANYARD INSTALLATION Closed 07.Feb.2008> 737-21-1131/SB* Rev.04 *AD* AIR CONDITION OVERHEAD DUCT LANYARD INSTALLATION See prev. Docstatus / Special Text:

This Aircraft is NA to this LN# due toPRODUCTION LINE PRR35426-R

This Document SUPERSEDES 737-21-1131/SB Rev.02Reason for this StatusPERFORMED ON PREVIOUS REVISION

> 737-21-1131/SB* Rev.02 *AD* AIR CONDITION OVERHEAD DUCT LANYARD INSTALLATION Closed 07.Feb.2008This Document has been SUPERSEDED BY 737-21-1131/SB Rev.04Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







23.Oct.2014Page 201/429

Document-Number Type Rev Compliance A|C Subject Status2005-04-01 AD 00 MANDATORY A/C *AD* BONDING BTW. ENG FUEL FEED LINE FITTING/WING FRONT SPAR Closed 20.Feb.2008

2005-04-01 (ACTIVE)737-28A1174 (REF)737-28A1174 IN 01 (REF)737-28A1174 R1 (REF)737-28A1174 R2 (ACTIVE)SBB 737-28A1174 (MAINT TASK)

ADSBSBSBSBTA

Perform BEFORE 22.Mar.20102005-04-01/AD Rev.00 *AD* BONDING BTW. ENG FUEL FEED LINE FITTING/WING FRONT SPAR Closed 20.Feb.2008> 737-28A1174/SB* Rev.02 *AD* BONDING BTW. ENG FUEL FEED LINE FITTING/WING FRONT SPAR Closed 20.Feb.2008

This Document SUPERSEDES 737-28A1174/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



2005-04-01SUB1 AD 00 MANDATORY A/C *AD* BONDING BTW. ENG FUEL FEED LINE FITTING/WING FRONT SPAR Not Applicable2005-04-01 (ACTIVE)737-28A1174 (REF)737-28A1174 IN 01 (REF)737-28A1174 R1 (REF)737-28A1174 R2 (ACTIVE)SBB 737-28A1174 (MAINT TASK)

ADSBSBSBSBTA





23.Oct.2014Page 202/429

Document-Number Type Rev Compliance A|C Subject Status2005-05-17 AD 00 MANDATORY A/C *AD* FUEL QUANTITY - ADD BONDING STRAPS TO SAFE SIDE HARNESS Not Applicable

2005-05-17 (ACTIVE)BFG 737-300766-28-2 REV6BFG V-1520 (REF)SB 737-300766-28-2 (MOD-TASK)

ADSBSBTA

2005-05-17/AD Rev.00 *AD* FUEL QUANTITY - ADD BONDING STRAPS TO SAFE SIDE HARNESS Not Applicable> 737-300766-28-2/SB* Rev.06 *AD* FUEL QUANTITY - ADD BONDING STRAPS TO SAFE SIDE HARNESS Closed 08.Apr.2006


08.Apr.2006 49237:00/H 26198/CPerfRev.:'NOTE' / Reason: KKM 150651ITEM: 1






23.Oct.2014Page 203/429

Document-Number Type Rev Compliance A|C Subject Status2005-07-12 AD 00 MANDATORY A/C *AD* FWD GALLEY DOOR CUTOUT FR. INSP. STA 291.5, STRING.16R Open

2005-07-12 (ACTIVE)37-SBB-53A1241 (REPETITIVE)737-53A1241-R0 (ACTIVE)

ADTASB

Perform within an unlimited threshold.2005-07-12/AD Rev.00 *AD* FWD GALLEY DOOR CUTOUT FR. INSP. STA 291.5, STRING.16R Open> 737-53A1241/SB Rev.01 FUSELAGE - FRAMES AND BULKHEADS - STA 277 TO STA 328 FRAME INSPECTIONS

STRINGER 7R TO 17R - FORWARD GALLEY DOOR CUTOUTOpen

This Document SUPERSEDES 737-53A1241/SB Rev.00> > 737-53A1241-01/EO* Rev.00 FUSELAGE - FRAMES AND BULKHEADS - STA 291.5 FRAME WEB INSPECTIONS

AROUND STR 16R - FORWARD GALLEY DOOR CUTOUTRepetitive

This Document SUPERSEDES 737-53A1241/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

47651/C Interval(F):4500/CPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks06.Feb.2014 71572:00/H 43151/C 489487, N/A Was due at: 45070/C PerfRev.:'00'

> > 737-53A1241-02/EO* Rev.00 FUSELAGE - FRAMES AND BULKHEADS - STA 277 TO STA 291.5 FRAME INSPECTIONSSTRINGER 7R TO 17R - FORWARD GALLEY DOOR CUTOUT

Open

NOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

46238/CPerform initially before(L) 30000/C Performinitially within (effective from 11.Jun.2013)(L) 4500/C / Interval(F):9000/C

> > 737-53A1241-03/EO* Rev.00 FUSELAGE - FRAMES AND BULKHEADS - STA 277 TO STA 328 FRAME INSPECTIONSSTRINGER 7R TO 17R - FORWARD GALLEY DOOR CUTOUT

Open

NOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

46238/CPerform initially before(L) 30000/C Performinitially within (effective from 11.Jun.2013)(L) 4500/C / Interval(F):9000/C

> 737-53A1241/SB Rev.00 *AD* FWD GALLEY DOOR CUTOUT FR. INSP. STA 291.5, STRING.16R Cancelled





23.Oct.2014Page 204/429

Document-Number Type Rev Compliance A|C Subject StatusThis Document has been SUPERSEDED BY 737-53A1241/SB Rev.01

> > 737-53A1241/EO* Rev.00 *AD*FWD GALLEY DOOR COUTOUT, STA 291.5 FRAME INSP AT STR 16R ***MANDATORY REPETITIVE DETAILED & NDT INSPECTION ***

Cancelled

This Document has been SUPERSEDED BY 737-53A1241-01/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks02.Nov.2012 68139:00/H 40570/C 273627, N/A Was due at: 42298/C PerfRev.:'00'Reason for this StatusManually deassigned after Document Cancelled or Superseded





23.Oct.2014Page 205/429

Document-Number Type Rev Compliance A|C Subject Status2005-07-19 AD 00 MANDATORY A/C *AD* CARGO DOOR CUTOUT, SKIN, BEARSTRAP AND FRAME INSPECTION Open

2005-07-19 (ACTIVE)37-NAS-5313-001 (REPETITIVE)37-NAS-5313-002 (REPETITIVE)37-NAS-5313-003 (REPETITIVE)37-SBB-53A1228-1 (REPETITIVE)37-SBB-53A1228-2 (REPETITIVE)737-53A1228 IN01 (REF)737-53A1228-R0 (ACTIVE)

ADTATATATATASBSB

Perform within an unlimited threshold.2005-07-19/AD Rev.00 *AD* CARGO DOOR CUTOUT, SKIN, BEARSTRAP AND FRAME INSPECTION Open> 737-53A1228/SB Rev.00 *AD* CARGO DOOR CUTOUT, SKIN, BEARSTRAP AND FRAME INSPECTION Open> > 737-53A1228-1/EO* Rev.00 *AD* FORWARD CARGO CUTOUT/DOORWAY - SKIN, BEARSTRAP & FRAME IAW SB

COMPLIANCE TABLE 1 & 2.Repetitive



Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks14.Feb.2014 71572:00/H 43151/C 489239, N/A Was due at: 44570/C PerfRev.:'00'

> > 737-53A1228-2/EO* Rev.00 *AD* AFT CARGO CUTOUT/DOORWAY - SKIN, BEARSTRAP & FRAME INS IAW SBCOMPLIANCE TABLES 1 & 3.

Repetitive




> > 737-53A1228MPD/EO*Rev.00

ADDITIONAL INSPECTION CONTROLLED BY MAINTENANCE TASK Taskcard Controlled / Special Text:Repaired after findings from SB -Additional inspection required.

Carried out on the following TaskcardsTaskcard: NAS-5313-006 Maint. Progr.: AMP 737-CL





23.Oct.2014Page 206/429

Document-Number Type Rev Compliance A|C Subject StatusExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks21.10.2015 47151/C 2'656/C Interval:4000/CPerf Dim1 (D) Perf Dim2 Perf Dim313.02.2014 71572:00/H 43151/CReason for this StatusAUTO ASSIGNED

2005-07-27 AD 00 MANDATORY A/C *AD* PREVENT LOSS OF STRUCT. INTEGRITY OF SEAT SERIE 312 Not ApplicableNot applicable due to the affected Aviointeriors S.p.A. (formerlyALVEN), model 312 seats not installed on NAS B737.2005-07-27 (ACTIVE) ADThis Document SUPERSEDES 2000-18-04/AD Rev.00Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 207/429

Document-Number Type Rev Compliance A|C Subject Status2005-10-11 AD 00 MANDATORY A/C *AD* INSPECTION OF CONNECTORS LINKED TO FUEL SHUT-OF VALVES Closed 24.Jan.2004

130S-04-183 (REF)2001-14-06 (SUPERSEDED)2004-5395 (REF)2005-10-11 (ACTIVE)737-28-1196-R3 (ACTIVE)737-SL-24-138 (REF)PRODUCTION LINE MRR3282-1516

AMOCADADADSBSLPRR


2005-10-11/AD Rev.00 *AD* INSPECTION OF CONNECTORS LINKED TO FUEL SHUT-OF VALVES Closed 24.Jan.2004This Document SUPERSEDES 2001-14-06/AD Rev.00

> 737-28-1196/SB* Rev.03 *AD* ENG FUEL SHUTOFF VALVE, WIRING CHANGES IN MWW Closed 24.Jan.2004Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

24.Jan.2004 43499:00/H 21327/CPerfRev.:'NOTE' / Reason: KKM 150052ITEM: 2






23.Oct.2014Page 208/429


2003-14-04 (SUPERSEDED)2005-12-05 (SUPERSEDED)2007-10-12 (ACTIVE)37-B52-51-00-5C (REPETITIVE)37-NAS-5200-002 (REPETITIVE)87-52-360-00-01 (REPETITIVE)B221001-52-03 (REF)B221001-52-03 R3 (REF)SB B221001-52-03 (REF)

ADADADTATATASBSBTA






23.Oct.2014Page 209/429

Document-Number Type Rev Compliance A|C Subject Status2005-13-15 AD 00 MANDATORY A/C *AD* APPLICATION OF THE SECONDARY FUEL VAPOR-BARRIER Closed 07.Mar.2005

Applicablility:NG:This document is applicable to LN# 1-1134. The other LN# are NotApplicable per MRR3288-1221.

CL:This document is applicable to LN# 311-3132.2005-13-15 (ACTIVE)737-57-1250-R2 (ACTIVE-NG)737-57-1261-R1 (ACTIVE-CL)PRODUCTION LINE MRR3288-1221

ADSBSBPRR

Perform within an unlimited threshold.2005-13-15/AD Rev.00 *AD* APPLICATION OF THE SECONDARY FUEL VAPOR-BARRIER Closed 07.Mar.2005> 737-57-1261/SB* Rev.01 *AD* CENTER WING BOX, INSP. OF SECONDARY FUEL VAPOR BARRIER Closed 07.Mar.2005








23.Oct.2014Page 210/429

Document-Number Type Rev Compliance A|C Subject Status2005-13-27 AD 00 MANDATORY A/C FUSELAGE SKIN INSP/REP OF CRACKS AT CHEM-MILLED STEPS Superseded (Not Applicable)

Service Bulletin 737-53A1234-R2.F. ApprovalThis service bulletin was examined by the Federal AviationAdministration (FAA). The changes specified in this service bulletincomply with the applicable regulations and are FAA approved, as wellas European Aviation Safety Agency (EASA)/Joint Aviation Authorities(JAA) approved for all EASA/JAA approved airplanes listed in theservice bulletin effectivity. This service bulletin and its approvalwere based on the airplane in its original Boeing deliveryconfiguration or as modified by other approved Boeing changes.

If an airplane has a non-Boeing modification or repair that affects acomponent or system also affected by this service bulletin, theoperator is responsible for obtaining appropriate regulatory agencyapproval before incorporating this service bulletin.

In addition, the Manager of the FAA Seattle Aircraft CertificationOffice approves the inspections and repairs defined in this servicebulletin as an alternative method of compliance to the inspections andrepairs required by paragraphs (g), (h) and (i) of FAA AD 2005-13-27.All provisions of FAA AD 2005-13-27 that are not specificallyreferenced in the above statement remain fully applicable and mustbe complied with.2005-13-27 (ACTIVE)37-SBB-53-1234-P1A (REPET)37-SBB-53-1234-P1B (REPET)737-53-1234-R0 (REF)737-53-1234-R1 (ACTIVE)

ADTATASBSB

This Document has been SUPERSEDED BY 2012-26-02/AD Rev.002005-13-27/AD Rev.00 FUSELAGE SKIN INSP/REP OF CRACKS AT CHEM-MILLED STEPS Not Applicable





23.Oct.2014Page 211/429

Document-Number Type Rev Compliance A|C Subject StatusThis Document has been SUPERSEDED BY 2012-26-02/AD Rev.00

> 737-53-1234/SB Rev.01 FUSELAGE SKIN - NDT INSP OF CRACKS AT CHEM-MILLED STEPS Not ApplicableThis Document has been SUPERSEDED BY 737-53A1234/SB Rev.02

> > 737-53-1234-P1A/EO* Rev.01 *AD* FUSELAGE SKIN - NDT INSP - CRACKS AT CHEM MILLED STEPS Not Applicable by Serial NumberThis Document SUPERSEDES 737-53-1234-P1A/EO Rev.00This Document has been SUPERSEDED BY 737-53A1234-01/EO Rev.00

> > 737-53-1234-P1A/EO* Rev.00 *AD* FUSELAGE SKIN - NDT INSP - CRACKS AT CHEM MILLED STEPS Not Applicable by Serial NumberThis Document has been SUPERSEDED BY 737-53-1234-P1A/EO Rev.01

> > 737-53-1234-P1B/EO* Rev.00 *AD* FUSELAGE SKIN - NDT INSP - CRACKS AT CHEM MILLED STEPS. Not Applicable by Serial NumberThis Document has been SUPERSEDED BY 737-53A1234-01/EO Rev.00

2005-18-08 AD 00 MANDATORY A/C *AD* MAIN LANDING GEAR BEAM FITTING INSPECTION AND REPLACEMT Not Applicable by Serial NumberThis mod is applicable to LN# 1001-1670.2005-18-08 (ACTIVE)737-57-1216-R2 (ACTIVE)737-57-1267-R0 (ACTIVE)737-57A1260-R2 (ACTIVE)737-SRP-57-0126 (REF)

ADSBSBSBSRP





23.Oct.2014Page 212/429

Document-Number Type Rev Compliance A|C Subject Status2005-18-08SUB1 AD 00 MANDATORY A/C *AD* MLG BEAM - L AND R - FITTING INSPECTION AND REPLACEMENT Not Applicable

Replacement of the fitting iaw. SB 737-57-1216 R2, Part III andinstallation a retaining bolt, castellated nut, and cotter pin iaw.SB 737-57A1260 R2 constitutes t/a for AD 2005-18-08.2005-18-08 XG (2)37-SBB-57-1216-L (REPETITIVE)37-SBB-57-1316-R (REPETITIVE)737-57-1216 IN 04737-57-1216-R0737-57-1216-R1737-57-1216-R2SBB 737-57-1216-L (MOD TASK)SBB 737-57-1216-R (MOD TASK)

ADTATASBSBSBSBTATA

Perform within an unlimited threshold.2005-18-08SUB1/AD Rev.00 *AD* MLG BEAM - L AND R - FITTING INSPECTION AND REPLACEMENT Not Applicable> 737-57-1267-L/SB Rev.00 L/H MLG BEAM SUPPORT FITTING RETAINING PIN LUG FRACTURE Not Applicable> > 737-57-1267-L/EO* Rev.00 *AD* MLG BEAM SUPPORT FITTNG RETAINING PIN LUG FRACTURE INS Not Applicable by Serial Number

This Document is terminated with implementation of 737-57-1267-L-01/EO Rev.00> > 737-57-1267-L-01/EO*Rev.00

L/H MLG BEAM SUPPORT FITTING RETAINING PIN LUG FRACTURE Not Applicable by Serial Number

This Document terminates 737-57-1267-L/EO Rev.00> 737-57-1267-R/SB Rev.00 R/H MLG BEAM SUPPORT FITTING RETAINING PIN LUG FRACTURE Not Applicable> > 737-57-1267-R/EO* Rev.00 *AD* MLG BEAM SUPPORT FITTNG RETAINING PIN LUG FRACTURE INS Not Applicable by Serial Number> > 737-57-1267-R-01/EO*Rev.00

R/H MLG BEAM SUPPORT FITTING RETAINING PIN LUG FRACTURE Not Applicable by Serial Number





23.Oct.2014Page 213/429

Document-Number Type Rev Compliance A|C Subject Status2005-19-19 AD 00 MANDATORY A/C *AD* FMC CHANGE THE OPERATIONAL PROGRAM SOFTWARE 10.5A Closed 13.Aug.2005

2005-19-19 (ACTIVE)737-34A1801 (ACTIVE-NG)737-34A1821 (ACTIVE-CL)PRODUCTION LINEMRR3344-1581SPRODUCTION LINE PRR38275-67S

AD

SB

SB

PRR

PRR

Perform BEFORE 26.Apr.20062005-19-19/AD Rev.00 *AD* FMC CHANGE THE OPERATIONAL PROGRAM SOFTWARE 10.5A Closed 13.Aug.2005> 737-34A1821/SB* Rev.00 *AD* FMC: CHANGE THE OPERATIONAL SOFTWARE TO VERSION 10,5A Closed 13.Aug.2005








23.Oct.2014Page 214/429

Document-Number Type Rev Compliance A|C Subject Status2005-19-25 AD 00 MANDATORY A/C *AD* FUSELAGE, SKIN - RADIO ALTIMETER ANTENNA CUTOUT Closed 04.Sep.2006

Modification performed via SB 737-53-1230 is terminating action forrepetitive inspection.2005-19-25 (ACTIVE)37-SBB-53-1230P1(REPETITIVE)737-53-1230-R0 (ACTIVE)SBB 737-53-1230 (MOD TASK)

ADTASBTA

Perform within an unlimited threshold.2005-19-25/AD Rev.00 *AD* FUSELAGE, SKIN - RADIO ALTIMETER ANTENNA CUTOUT Closed 04.Sep.2006> 737-53-1230/SB Rev.00 *AD* FUSELAGE, SKIN - RADIO ALTIMETER ANTENNA CUTOUT Closed 04.Sep.2006> > 737-53-1230-01/EO* Rev.00 *AD* FUSELAGE, SKIN - RADIO ALTIMETER ANTENNA CUTOUT Closed 04.Sep.2006

This Document terminates 737-53-1230P1/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

04.Sep.2006 50494:00/H 27176/CPerfRev.:'NOTE' / Reason: KKM 150738ITEM: 2


> > 737-53-1230P1/EO* Rev.00 *AD* FUSELAGE, SKIN - RADIO ALTIMETER ANTENNA CUTOUT INSPEC CancelledThis Document is terminated with implementation of 737-53-1230-01/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

04.Sep.2006 50494:00/H 27176/CPerfRev.:'NOTE' / Reason: AMICOS WO150738 KKM SBB 737-53-1230*AD*ANTENNA C

Reason for this StatusPREVENTIVE MODIFIACTION PERF. ON EO 737-53-1230-01





23.Oct.2014Page 215/429

Document-Number Type Rev Compliance A|C Subject Status2005-20-01 AD 00 MANDATORY A/C *AD* WINGS CENTER SECTION REAR SPAR. STIFFNERS INSP & REPL. Open

This Document is applicable to all 737CL.

SB 737-57A1269 IN-03 introduces SB 737-47-1007 as an AMOC to AD2005-20-01. SB 737-47-1007 is rejected due to cost.737-57A1269737-57A1269 IN-01737-57A1269 IN-02737-57A1269 IN-03737-57A1269-01737-57A1269P1

SBSBSBSBEOEO

000000000101

Perform within an unlimited threshold.2005-20-01/AD Rev.00 *AD* WINGS CENTER SECTION REAR SPAR. STIFFNERS INSP & REPL. Open> 737-57A1269/SB Rev.01 *AD* WINGS CENTER SECTION REAR SPAR. STIFFNERS INSP & REPL. Open

This Document SUPERSEDES 737-57A1269/SB Rev.00> > 737-57A1269-01/EO* Rev.01 *AD* WINGS CENTER SECTION REAR SPAR. STIFFNERS INSP & REPL. Term.Action open

Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of DocumentNO LIMIT

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks01.Apr.2006 49193:00/H 26146/C PerfRev.:'NOTE'

> > 737-57A1269P1/EO* Rev.01 *AD* WINGS CNTR SECT. REAR SPAR. STIFFNER L/H & R/H BBL 6.1 *** MANDATORYREPETITIVE INSPECTION ***

Repetitive








23.Oct.2014Page 216/429

Document-Number Type Rev Compliance A|C Subject Status2005-20-03 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 2009-16-14 Superseded (Cancelled)

2005-20-03 (SUPERSEDED)2009-16-14 (ACTIVE)37-SBB-53A1204 (REP TASK)737-53-1204-R0 (REF)737-53-1204-R1 (ACTIVE)PRODUCTION LINE MRR3537-1153

ADADTASBSBPRR

This Document has been SUPERSEDED BY 2009-16-14/AD Rev.NOTEPerform within an unlimited threshold.

2005-20-03/AD Rev.00 *AD* SUPERSEDED BY AD 2009-16-14 CancelledThis Document has been SUPERSEDED BY 2009-16-14/AD Rev.NOTE

> 737-53A1204/SB Rev.01 *AD* INTERCOASTALS - BS360 & 294.5 S-6/17L - NDT INSPECTION Cancelled> > 737-53A1204/EO* Rev.01 NDT - INTERCOASTALS - BS360 & 294.5 S-6/17L - INTERNAL NDT INSPECTION

REPETITIVE INSPECTIONCancelled

This Document has been SUPERSEDED BY 737-53A1204-01/EO Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks05.Jul.2011 64534:00/H 37798/C 205164, N/A Was due at: 38852/C PerfRev.:'01'Reason for this StatusManually deassigned after Document Cancelled or Superseded

2005-20-31 AD 00 MANDATORY A/C *AD* HONEYWELL FLIGHT MANAGMENT SYSTEM Not ApplicableThis AD rescinds AD 91-08-51.2005-20-31 ADThis Document SUPERSEDES 1991-08-51/AD Rev.00Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 217/429

Document-Number Type Rev Compliance A|C Subject Status2005-20-39 AD 00 MANDATORY A/C *AD* MLG, TRUNION PIN, ACT. BEAM BOLT/TEE-FITTING BOLT INSP Closed 16.Mar.2005

2005-20-39 (ACTIVE)37-32-001(TECHNICAL DIRECTIVE)737-32A1367-R1 (ACTIVE)737-32A1367-RO (REF)DE#74320PRODUCTION LINE MRR3323-1546SBB 737-32A1367 (INSP-TASK)

ADTDSBSBDOCRPRRTA

Perform within an unlimited threshold.2005-20-39/AD Rev.00 *AD* MLG, TRUNION PIN, ACT. BEAM BOLT/TEE-FITTING BOLT INSP Closed 16.Mar.2005> 737-32A1367/SB* Rev.00 *AD* MLG, TRUNION PIN, ACT. BEAM BOLT/TEE-FITTING BOLT INSP Closed 16.Mar.2005








23.Oct.2014Page 218/429

Document-Number Type Rev Compliance A|C Subject Status2005-23-17 AD 00 MANDATORY A/C *AD* FUEL-POSSIBLE WIRE CHAFING BEHIND P15 PANEL. Closed 17.Mar.2005

2005-23-17 (ACTIVE)737-28-1193-R1 (ACTIVE CL)737-28-1200 (REVISED)737-28-1200 IN02 (ACTIVE)737-28-1200 R1 (ACTIVE)PRODUCTION MRR3282-1519SSBB-737-28-1200 (MAINT TASK)

ADSBSBSBSBPRRTA

Perform BEFORE 21.Jun.20062005-23-17/AD Rev.00 *AD* FUEL-POSSIBLE WIRE CHAFING BEHIND P15 PANEL. Closed 17.Mar.2005> 737-28-1193/SB* Rev.01 *AD* PRESSURE FUELING SYSTEM - INSPECTION FOR WIRE CHAFING Closed 17.Mar.2005




2005-23-17SUB1 AD 00 MANDATORY A/C *AD* FUEL-POSSIBLE WIRE CHAFING BEHIND P15 PANEL. Not Applicable by Serial Number2005-23-17 (ACTIVE)737-28-1193-R1 (ACTIVE CL)737-28-1200 (REVISED)737-28-1200 IN02 (ACTIVE)737-28-1200 R1 (ACTIVE)PRODUCTION MRR3282-1519SSBB-737-28-1200 (MAINT TASK)

ADSBSBSBSBPRRTA





23.Oct.2014Page 219/429

Document-Number Type Rev Compliance A|C Subject Status2005-26-03 AD 00 MANDATORY A/C *AD* ELEVATOR INPUT TORQUE TUBE - MODIFICATION Closed 18.Feb.2008

This modification is applicable to all B737 classic and B737 NG forLine number interval 1-1412.737-27A1271737-27A1271737-27A1274PRODUCTION LINE PRR38275-55S

SBSBSBPRR

000101

Perform BEFORE 18.Jan.20112005-26-03/AD Rev.00 *AD* ELEVATOR INPUT TORQUE TUBE - MODIFICATION Closed 18.Feb.2008> 737-27A1274/SB* Rev.01 FLIGHT CONTROLS - ELEVATOR AND TAB - ELEVATOR INPUT TORQUE TUBE

MODIFICATIONSee prev. Docstatus

This Document SUPERSEDES 737-27A1274/SB Rev.00Reason for this StatusAIRCRAFT MODIFIED VIA SB 737-27A1274 REV.:00

> 737-27A1274/SB* Rev.00 FLIGHT CONTROLS - ELEVATOR AND TAB - ELEVATOR INPUT TORQUE TUBEMODIFICATION

Closed 18.Feb.2008

This Document has been SUPERSEDED BY 737-27A1274/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

18.Feb.2008 54542:00/H 30315/CKKM 151344ITEM: 1

PerfRev.:'00'





23.Oct.2014Page 220/429

Document-Number Type Rev Compliance A|C Subject Status2006-0140 AD 00 MANDATORY A/C *AD* AIR CONDITIONING - ZONAL DRYING SYSTEM DEACTIVATION Superseded (Not Applicable)

2006-0118R1-E (SUPERSEDED)2006-0140-E (SUPERSEDED)2006-0140R1 (SUPERSEDED)2006-0140R2 (ACTIVE)EASA NUMBER 2004-4416LBA.21E2.TA0636

ADADADADSTCSTC

This Document has been SUPERSEDED BY 2006-0140R4/AD Rev.04Reason for this StatusCOMPLIANCE: N/A EQUIPMENT NOT INSTALLED

2006-0140R4 AD 04 MANDATORY A/C *AD* AIR CONDITIONING - ZONAL DRYING SYSTEM DEACTIVATION Not Applicable2006-0118R1-E (SUPERSEDED)2006-0140-E (SUPERSEDED)2006-0140R1 (SUPERSEDED)2006-0140R2 (ACTIVE)EASA NUMBER 2004-4416LBA.21E2.TA0636

ADADADADSTCSTC

This Document SUPERSEDES 2006-0140/AD Rev.00This Document SUPERSEDES 2006-0140R1/AD Rev.00This Document SUPERSEDES 2006-0140R2/AD Rev.00Reason for this StatusCOMPLIANCE: N/A EQUIPMENT NOT INSTALLED





23.Oct.2014Page 221/429

Document-Number Type Rev Compliance A|C Subject Status2006-0220 AD 00 MANDATORY A/C *AD* EQUIPMENT-PASS. SEATS-INSPECTION OF SEATBELT SHACKLE Not Applicable

NAS have Recaro Type 3510B (on the 737-800) and Type 3510D (on the737-300) installed.Not Applicable due to:All NAS Reacro seats were installed in 2009 (new shipset) or later,all seats are excluded from the MFG date interval. Only seats MFGbetween 1st Nov 2005 and 5th May 2006 are applicable.2006-0220 (ACTIVE)2006-17-13 (ACTIVE)

ADAD

2006-0264 AD 00 MANDATORY A/C *AD* REPLACEMENT OF ALL SEAT TRACK FITTINGS ON ALL PAX SEATS Not Applicable2001-11-11 REF)2006-0264 (ACTIVE)SB 737-25-1371-R2 (REF)

ADADSB

Reason for this StatusCOMPLIANCE: EQUIPMENT NOT INSTALLED

2006-0265 AD 00 MANDATORY A/C *AD* MODE `C` AND MODE `S TRANSPONDER SYSTEM UTILISING GILH Not Applicable*AD* MODE `C` AND MODE `S TRANSPONDER SYSTEM UTILISINGGILHAM Aircraft NOT equipped with one or more Mode `C` or Mode `S`transponder systems which utilise Gilham code altitude input I.E.2006-0265 (EQUIPMENT NOT INST) ADReason for this StatusCOMPLIANCE: N/A SUPJECTED TRANSPONDER NOT INSTALLE





23.Oct.2014Page 222/429

Document-Number Type Rev Compliance A|C Subject Status2006-03-12 AD 00 MANDATORY A/C *AD* WINGS CENTER TANK WIRE BUNDLES INSP & CLAMPS CHANGE Taskcard Controlled

As per AD §f all action per SB 737-28-1208 rev.:01 is to beperoformed.NAS has modified some AC per rev.: 00 and then performed thedifference from Rev.:00 to 01 via TO 37-28-001.The remaining NAS Aircraft has been modified via SB rev.: 01.SB rev.:02 was issued after AD compliance date and therefore notperformed by NAS.2006-03-12 (ACTIVE)37-28-001 (REF)37-B28-11-00-6A (REPETITIVE)737-28-1208 IN 01 (REF)737-28-1208-R0 (REF)737-28-1208-R1 (ACTIVE)

ADEODTASBSBSB

Perform BEFORE 15.Mar.20112006-03-12/AD Rev.00 *AD* WINGS CENTER TANK WIRE BUNDLES INSP & CLAMPS CHANGE Taskcard Controlled> 737-28-1208/SB Rev.00 *AD* WINGS CENTER TANK WIRE BUNDLES INSP & CLAMPS CHANGE Taskcard Controlled

This Document has been SUPERSEDED BY 737-28-1208/SB Rev.01> > 37-28-001/TO* Rev.00 WINGS CENTER TANK WIRE BUNDLES INSPECTION & CLAMP CANGE Closed 21.Feb.2008




> > 737-28-1208-01/EO* Rev.00 *AD* WINGS CENTER TANK WIRE BUNDLES INSP & CLAMPS CHANGE Closed 14.Mar.2005This Document has been SUPERSEDED BY 737-28-1208-01/EO Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







23.Oct.2014Page 223/429

Document-Number Type Rev Compliance A|C Subject Status> > 737-28-1208MPD/EO*Rev.01


Carried out on the following TaskcardsTaskcard: 28-011-00-01 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks12.03.2015 12.Mar.2015140d, 6h Interval:10/YRPerf Dim1 (D) Perf Dim2 Perf Dim314.03.2005 00:00/H 23575/CReason for this StatusAUTO ASSIGNED

> 737-28-1208/SB Rev.01 *AD* WINGS CENTER TANK WIRE BUNDLES INSP & CLAMPS CHANGE Taskcard ControlledThis Document SUPERSEDES 737-28-1208/SB Rev.00This Document has been SUPERSEDED BY 737-28-1208/SB Rev.02

> > 737-28-1208-01/EO* Rev.01 WINGS CENTER TANK WIRE BUNDLES INSP & CLAMPS CHANGE See prev. DocstatusThis Document SUPERSEDES 737-28-1208-01/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks14.Mar.2005 46130:00/H 23575/C PerfRev.:'NOTE'Reason for this StatusKKM 150408 ITEM: 1

> > 737-28-1208MPD/EO*Rev.01



> 737-28-1208/SB* Rev.02 FUEL - INDICATING - WING CENTER TANK WIRE BUNDLES INSPECTION AND CLAMPSCHANGE

See prev. Docstatus





23.Oct.2014Page 224/429

Document-Number Type Rev Compliance A|C Subject StatusThis Document SUPERSEDES 737-28-1208/SB Rev.01Reason for this StatusALL NAS AIRCRAFT MODIFIED VIA SB REV.:00+TO 37-28-001 OR SB REV.:01

> 737-28-1208R1/SB* Rev.01 *AD* WINGS CENTER TANK WIRE BUNDLES INSP & CLAMPS CHANGE Not Applicable by Serial Number

2006-03-12SUB1 AD 00 MANDATORY A/C *AD* WINGS CENTER TANK WIRE BUNDLES INSP & CLAMPS CHANGE Not Applicable by Serial Number2006-03-12 (ACTIVE)37-28-001 (REF)37-B28-11-00-6A (REPETITIVE)737-28-1208 IN 01 (REF)737-28-1208-R0 (REF)737-28-1208-R1 (ACTIVE)SBB 737-28-1208 (MOD-TASK)

ADEODTASBSBSBTA

2006-0334 AD 01 MANDATORY COMP *AD* COMMUNICATION - THALES VHF DATA RADIO, MODIFICATION OF Not Applicable by Serial Number2006-0334 (SUPERSEDED)2006-0334R1 (ACTIVE)

ADAD


2006-04-04 AD 00 MANDATORY COMP *AD* MEGGITT MODEL 602 SMOKE DETECTOR Not Applicable by Serial NumberThis AD is applicable to Meggit Model 602 Smoke detectors.Per AD § (c) Smoke detectors listed in "Current PN" are effected.Per AD § (f) the effected PN must be replaced with modified detectorsas detailed in Meggitt SIL.2006-04-04 (ACTIVE)MEGGITT 8930-26-01

ADSIL C






23.Oct.2014Page 225/429


2006-07-12 (SUPERSEDED)2010-05-23 (ACTIVE)PRODUCTION LINEPRR35005-262RSSBB 737-53A1262-1 (SUB-MOD)SBB 737-53A1262-2 (SUB-MOD)SBB 737-53A1262-3 (SUB-MOD)SBB 737-53A1262-4 (SUB-MOD)SBB 737-53A1262-5 (SUB-MOD)SBB 737-53A1262-R3 (ACTIVE)

ADADPRRSBSBSBSBSBSB

This Document has been SUPERSEDED BY 2010-05-13SUB1/AD Rev.00This Document has been SUPERSEDED BY 2010-05-13SUB2/AD Rev.00This Document has been SUPERSEDED BY 2010-05-13SUB3/AD Rev.00This Document has been SUPERSEDED BY 2010-05-13SUB4/AD Rev.02Reason for this StatusSUPERSEDED BY AD 2010-05-23





23.Oct.2014Page 226/429

Document-Number Type Rev Compliance A|C Subject Status2006-12-06 AD 00 MANDATORY A/C *AD* GALLEY WIRE BUNDLE PROTECTIVE WRAP REPLACEMENT Not Applicable

AC that are Not Applicable, does not have the affected Galleyinstalled.737-25-1438-R4 (ACTIVE,CL)737-25-1439-R4 (ACTIVE,NG)PRODUCTION LINE MRR3250-1417

SBSBPRR

040400

2006-12-06/AD Rev.00 *AD* GALLEY WIRE BUNDLE PROTECTIVE WRAP REPLACEMENT Not Applicable> 737-25-1438/SB* Rev.01 *AD* GALLEY WIRE BUNDLE PROTECTIVE WRAP REPLACEMENT Not Applicable

This Document SUPERSEDES 737-25-1438/SB Rev.00This Document has been SUPERSEDED BY 737-25-1438/SB Rev.02Reason for this StatusAFFECTED EQIPMENT NOT INSTALL

> 737-25-1438/SB* Rev.02 *AD* GALLEY WIRE BUNDLE PROTECTIVE WRAP REPLACEMENT Not ApplicableThis Document SUPERSEDES 737-25-1438/SB Rev.01This Document has been SUPERSEDED BY 737-25-1438/SB Rev.03Reason for this StatusAFFECTED EQIPMENT NOT INSTALL

> 737-25-1438/SB* Rev.03 *AD* GALLEY WIRE BUNDLE PROTECTIVE WRAP REPLACEMENT Not ApplicableThis Document SUPERSEDES 737-25-1438/SB Rev.02This Document has been SUPERSEDED BY 737-25-1438/SB Rev.04Reason for this StatusAFFECTED EQIPMENT NOT INSTALL

> 737-25-1438/SB* Rev.04 *AD* GALLEY WIRE BUNDLE PROTECTIVE WRAP REPLACEMENT Not ApplicableThis Document SUPERSEDES 737-25-1438/SB Rev.03Reason for this StatusAFFECTED EQIPMENT NOT INSTALL





23.Oct.2014Page 227/429

Document-Number Type Rev Compliance A|C Subject Status2006-12-23 AD 00 MANDATORY A/C *AD* INSPECTION OF ELEVATOR TAB HINGE AND ELEVATOR TAB CONTR Repetitive

2002-01-01 (SUPERSEDED)2006-12-23 (ACTIVE)37-SBB-55A1070P1+P2(REPEAT)37-SBB-55A1070P3 (REPEAT)737-55A1070-R0 (REF)737-55A1070-R3 (ACTIVE)

ADADTATASBSB


2006-12-23/AD Rev.00 *AD* INSPECTION OF ELEVATOR TAB HINGE AND ELEVATOR TAB CONTR RepetitiveThis Document SUPERSEDES 2002-01-01/AD Rev.00

> 737-55A1070/SB Rev.03 *AD* ELEVATOR TAB FREE-PLAY REPEAT INSPECTION Repetitive> > 737-55A1070P1+2/EO*Rev.00

*AD* HINGE DETAIL, FREE-PLAY AND CLAMPED HINGE PUTTY INSPEC AD 2006-12-23 -SBB 737-55A1070 PART 1, PART 2 AND PART 10

Repetitive


75319:36/H 45994/CPerform initially before(F) 28394/C or52066/H / Interval(F):1500/C or 2000/H


06.Oct.2014 73319:36/H 44494/C 554152,Was due at: 44651/C and 4414320/HPerfRev.:'00'

> > 737-55A1070P3/EO* Rev.00 *AD* ELEVATOR TAB CONTROL INSPECTION AD 2006-12-23 - SBB 737-55A1070, REV 2,PART 3

Repetitive


77572:00/H 47651/CPerform initially before(F) 31394/C or56066/H / Interval(F):4500/C or 6000/H







23.Oct.2014Page 228/429

Document-Number Type Rev Compliance A|C Subject Status2006-12-23P4 AD 00 MANDATORY A/C *AD* ELEVATOR / TAB DETERMINATION OF CONFIGURATION Closed 10.Jul.2006

2006-12-23 (ACTIVE)2006-12-23P4 (ACTIVE)737-55A1070-R2 (REF)737-55A1070-R3 (ACTIVE)SBB 737-55A1070P4 (INSPECTION)SBB 737-55A1070P4 (INSPECTION)

ADADSBSBSBTA

Perform BEFORE 03.Oct.20062006-12-23P4/AD Rev.00 *AD* ELEVATOR / TAB DETERMINATION OF CONFIGURATION Closed 10.Jul.2006> 737-55A1070P4/SB Rev.03 *AD* ELEVATOR / TAB DETERMINATION OF CONFIGURATION Closed 10.Jul.2006> > 737-55A1070-2/SB* Rev.03 *AD* ELEVATOR & TAB, INITIAL INSPECTIONS & PUTTY APPLICATION Closed 10.Jul.2006


10.Jul.2006 50066:00/H 26894/CPerfRev.:'NOTE' / Reason: KKM 150759ITEM: 1


2006-13-13 AD 00 MANDATORY A/C AIRPLANE FLIGHT MANUAL REVISION CABIN PRESSURIZATION PROCEDURES Closed 07.Jul.20062006-13-13 (ACTIVE) ADPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

07.Jul.2006Reason: IMPLEMENTED IN AFM, AFMREVISED

Reason for this StatusIMPLEMENTED IN AFM, AFM REVISED





23.Oct.2014Page 229/429

Document-Number Type Rev Compliance A|C Subject Status2006-15-05 AD 00 MANDATORY A/C *AD* AUXILIARY FUEL TANKS - IMPROVED FUELING FLOAT SWITCH Not Applicable

NAS has no Auxiliary fuel tanks installed.2006-15-05 (ACTIVE)737-28A1192-R0 (REF)737-28A1192-R1 (REF)737-28A1192-R2 (ACTIVE)SBB 737-28A1192 (MOD-TASK)

ADSBSBSBTA

Perform BEFORE 24.Aug.20082006-15-05/AD Rev.00 *AD* AUXILIARY FUEL TANKS - IMPROVED FUELING FLOAT SWITCH Not Applicable> 737-28A1192/SB* Rev.02 *AD* AUXILIARY FUEL TANKS - IMPROVED FUELING FLOAT SWITCH Not Applicable

Reason for this StatusAUX. FUEL TANKS NOT INST.





23.Oct.2014Page 230/429

Document-Number Type Rev Compliance A|C Subject Status2006-15-18 AD 00 MANDATORY A/C *AD* LIGHTS - SUPPLY TEST GROUND SIGNAL WIRING SEPARATION Closed 17.Mar.2005

2006-15-18 (ACTIVE)737-33-1133 R3 (ACTIVE)AD 2006-15-18 (TASK)SBB 737-33-1132 (MOD-TASK-CL)SBB 737-33-1133 (MOD-TASK-NG)

ADSBTATATA

Perform BEFORE 05.Sep.20102006-15-18/AD Rev.00 *AD* LIGHTS - SUPPLY TEST GROUND SIGNAL WIRING SEPARATION Closed 17.Mar.2005> 737-33-1132/SB* Rev.00 LIGHTS - SUPPLY TEST GROUND SIGNAL WIRING SEPARATION Closed 17.Mar.2005

This Document has been SUPERSEDED BY 737-33-1132/SB Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-33-1132/SB* Rev.01 LIGHTS - SUPPLY TEST GROUND SIGNAL WIRING SEPARATION See prev. DocstatusThis Document SUPERSEDES 737-33-1132/SB Rev.00This Document has been SUPERSEDED BY 737-33-1132/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-33-1132/SB* Rev.02 LIGHTS - SUPPLY TEST GROUND SIGNAL WIRING SEPARATION See prev. DocstatusThis Document SUPERSEDES 737-33-1132/SB Rev.01This Document has been SUPERSEDED BY 737-33-1132/SB Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Mar.2005 46130:00/H 23575/C PerfRev.:'NOTE'Reason for this StatusKKM 150147 ITEM: 1

> 737-33-1132/SB* Rev.03 LIGHTS - SUPPLY TEST GROUND SIGNAL WIRING SEPARATION See prev. Docstatus





23.Oct.2014Page 231/429

Document-Number Type Rev Compliance A|C Subject StatusThis Document SUPERSEDES 737-33-1132/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Mar.2005 46130:00/H 23575/C PerfRev.:'NOTE'Reason for this StatusKKM 150147 ITEM: 1

2006-16-18 AD 00 MANDATORY COMP *AD* TO PREVENT A BEARING ERROR LEADING TO DEPARTED FLIGHT Superseded (Not Applicable bySerial Number)

Not applicable due to Sandel Avionics Incorporated (Sandel) ModelST3400 terrain awareness warning system/radio magnetic indicator(TAWS/RMI) units not installed on NAS B737.2006-16-18-R1 (ACTIVE)3400-1 (ACTIVE)TAWS/RMI MODEL SR3400 UNITS

ADSBIPC

This Document has been SUPERSEDED BY 2006-16-18/AD Rev.01Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

2006-16-18 AD 01 MANDATORY COMP *AD* TO PREVENT A BEARING ERROR LEADING TO DEPARTED FLIGHT Not Applicable by Serial NumberNot applicable due to Sandel Avionics Incorporated (Sandel) ModelST3400 terrain awareness warning system/radio magnetic indicator(TAWS/RMI) units not installed on NAS B737.2006-16-18-R1 (ACTIVE)3400-1 (ACTIVE)TAWS/RMI MODEL SR3400 UNITS

ADSBIPC

This Document SUPERSEDES 2006-16-18/AD Rev.00Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 232/429

Document-Number Type Rev Compliance A|C Subject Status2006-17-13 AD 00 MANDATORY COMP *AD* RECARO SEATS MODEL 3410 - PREVENT A SEAT BELT FROM DET. Not Applicable by Serial Number

NSB does not have Recaro Series effected by the AD installed. Pleaserefer to LOPA.2006-0220 (ACTIVE)2006-17-13 (ACTIVE)

ADAD


2006-18-08 AD 00 MANDATORY COMP *AD* GOODYEAR AVIATION TIRES Not Applicable by Serial NumberNAS does not have effected PN installed.2006-18-08 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

2006-18-11 AD 00 MANDATORY A/C *AD* AUXILIARY FUEL SYSTEM - DEACTIVATION AND VENTING Not ApplicableNAS has no Auxiliary fuel tanks installed.2006-18-11SA725NE

ADSTC

Reason for this StatusAUX. FUEL TANKS NOT INST.

2006-19-04 AD 00 MANDATORY COMP *AD* TRANSPONDER - TO PREVENT THE TRANSPONDER GOING INTO STD Not Applicable by Serial NumberNot applicable due to; affected PN not installed on NAS AC.2006-19-04 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 233/429

Document-Number Type Rev Compliance A|C Subject Status2006-21-01 AD 00 MANDATORY A/C *AD* AILERON BALANCE TAB FREEPLAY CHECK AND LUBRICATION Repetitive

27-026-01-01 (REPETITIVE)27-026-02-01 (REPETITIVE)27-033-00-01 (REPETITIVE)27-033-00-02 (REPETITIVE)737-27-1272 (ACTIVE-CL)737-27-1273R2 (ACTIVE-NG)

TATATATASBSB

000000000000

Perform BEFORE 14.Apr.20082006-21-01/AD Rev.00 *AD* AILERON BALANCE TAB FREEPLAY CHECK AND LUBRICATION Repetitive> 737-27-1272/SB Rev.00 *AD * AILERON BALANCE TAB FREEPLAY CHECK AND LUBRICATION Repetitive> > 737-27-1272P1/EO* Rev.00 *AD* AILERON BALANCE TAB FREEPLAY CHECK Repetitive


07.Feb.2016 79572:00/HPerform initially within (effective fromManufacturer Date 13.Mar.1990) (F) 0/D or0/H / Interval(F):730/D or 8000/H


07.Feb.2014 71572:00/H 43151/C 489495, N/AWas due at: 30.Oct.2014 and 4568340/HPerfRev.:'00'

> > 737-27-1272P2/EO* Rev.00 *AD* AILERON BALANCE TAB BEARING LUBRICATION *** MANDATORY REPETITIVELUBRICATION ***

Repetitive


24.Feb.2015 75572:00/H



24.Feb.2014 71572:00/H 43151/C 489223, N/AWas due at: 12.Apr.2014 and 4388100/HPerfRev.:'00'





23.Oct.2014Page 234/429

Document-Number Type Rev Compliance A|C Subject Status2006-22-05 AD 00 MANDATORY COMP *AD* HONEYWELL PRIMUS II RNZ-850/-851 INTEGRATED NAVIGATION Superseded (Not Applicable by

Serial Number)2003-04-06 (ACTIVE) ADThis Document SUPERSEDES 2003-04-06/AD Rev.00This Document has been SUPERSEDED BY 2010-07-02/AD Rev.00Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

2006-26-01 AD 00 MANDATORY COMP FUEL FILTER REPLACEMENT Closed 27.Nov.2007 / Special Text:PN WF337661, WF337017,7595983-101 and 7588133 no longerin stock.

2006-26-01TD 06-1036

ADTD


CFM56-3B2 / 725495 Pos=RH (KKM)

Closed / Special Text: PN WF337661,WF337017, 7595983-101 and 7588133 nolonger in stock. / Reason: KKS 220704ITEM: 1 39730 / LastPerformed:25.Sep.2007 52419:00/H29081/C RefDocument: Rev.NOTE

CFM56-3B2 / 724473 Pos=LH (KKM)

Closed / Special Text: PN WF337661,WF337017, 7595983-101 and 7588133 nolonger in stock. / Reason: KKM 151141ITEM: 1 39729 / LastPerformed:27.Nov.2007 50472:00/H28170/C RefDocument: Rev.NOTE





23.Oct.2014Page 235/429

Document-Number Type Rev Compliance A|C Subject Status2006-26-09 AD 00 MANDATORY A/C *AD* AIR-COND. BRACKET ATTACHMENTS INSPECTION MOD & REAIR Closed 07.Feb.2008

2006-26-09 (ACTIVE)37-SBB-53-1216 (REPETITIVE)737-53-1216-R0 (REF)737-53-1216-R1 (AVTIVE)SBB 737-53-1216-1 (INP-TASK)

ADTASBSBTA

Perform BEFORE 40000/C2006-26-09/AD Rev.00 *AD* AIR-COND. BRACKET ATTACHMENTS INSPECTION MOD & REAIR Closed 07.Feb.2008> 737-53-1216/SB Rev.01 *AD* AIR-COND. BRACKET ATTACHMENTS INSPECTION MOD & REAIR Closed 07.Feb.2008> > 737-53-1216/EO* Rev.01 *AD* AIRCONDITIONING BRACKET ATTACHMENTS ST 360 - 907, INSP Cancelled

This Document is terminated with implementation of 737-53-1216-01/EO Rev.01Reason for this StatusCANCELLED DUE TO EO 737-53-1216-01 PERFORMED

> > 737-53-1216-01/EO* Rev.01 *AD* AIR-COND. BRACKET ATTACHMENTS INSPECTION MOD & REAIR Closed 07.Feb.2008This Document terminates 737-53-1216/EO Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







23.Oct.2014Page 236/429

Document-Number Type Rev Compliance A|C Subject Status2006-26-09SUB1 AD 00 MANDATORY A/C *AD* AIR-COND. BRACKET ATTACHMENTS POST MOD / REPAIR INSP. Open

2006-26-09 PARAGRAPH K737-53-1216 R1, PART 4737-53-1216-R0 (REF)AD 2006-26-09SUB1 (SEC-TASK)SBB 737-53-1216-2 (INSP-TASK)

ADSBSBTATA

Perform BEFORE 54315/C2006-26-09SUB1/AD Rev.00 *AD* AIR-COND. BRACKET ATTACHMENTS POST MOD / REPAIR INSP. Open> 737-53-1216-2/SB* Rev.01 *AD* AIR-COND. BRACKET ATTACHMENTS POST MOD / REPAIR INSP. Open


2006-26-13 AD 00 MANDATORY A/C *AD* ATTENDANT SEAT - CHANGE ATTACHMENT OF SHOULDER RESTRAIN Not ApplicableThis mod is applicable to LN# 596-3110. The following LN# are NotApplicable per MRR3259-1295.2001-24-02 (SUPERSEDED)2003-20-08 (SUPERSEDED)2006-26-13 (ACTIVE)737-25-1412-R3 (ACTIVE)PRODUCTION MRR3259-1295

ADADADSBPRR

This Document SUPERSEDES 2001-24-02/AD Rev.00This Document SUPERSEDES 2003-20-08/AD Rev.00Perform within an unlimited threshold.

2006-26-13/AD Rev.00 *AD* ATTENDANT SEAT - CHANGE ATTACHMENT OF SHOULDER RESTRAIN Not ApplicableThis Document SUPERSEDES 2001-24-02/AD Rev.00This Document SUPERSEDES 2003-20-08/AD Rev.00

> 737-25-1412/SB* Rev.03 **AD* OBSERVER/ATTENDANT SHOULDER RESTRAINT SYSTEM ATTACHMEN Not Applicable by Serial Number





23.Oct.2014Page 237/429

Document-Number Type Rev Compliance A|C Subject Status2007-03-03 AD 00 MANDATORY A/C *AD* VERTICAL BEAM WEBS AT STA 178 PRESSURE BULKHEAD/CRACKS Repetitive

2007-03-03 (ACTIVE)37-SBB-53A1225 (REPETITIVE)737-53A1225-R0 (REF)737-53A1225-R1 (ACTIVE)SBB 737-53A1225 (MOD-TASK)

ADTASBSBTA

Perform BEFORE 50000/C2007-03-03/AD Rev.00 *AD* VERTICAL BEAM WEBS AT STA 178 PRESSURE BULKHEAD/CRACKS Repetitive> 737-53A1225/SB Rev.01 *AD* VERTICAL BEAM WEBS AT STA 178 PRESSURE BULKHEAD/CRACKS Repetitive> > 737-53A1225/EO* Rev.01 *AD* VERTICAL BEAM WEBS AT STA 178 PRESSURE BULKHEAD - CRAC Repetitive

This Document is terminated with implementation of 737-53A1225-01/EO Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

05.Sep.2006 50494:00/H 27176/CPerfRev.:'NOTE' / Reason: AMICOS WO150786 KKM 37-SBB-53A1225 STA 178BEAM I

Reason for this StatusAMICOS WO 150786 KKM 37-SBB-53A1225 STA 178 BEAM INSP -ATC

> > 737-53A1225-01/EO* Rev.01 *AD* VERTICAL BEAM WEBS AT STA 178 PRESSURE BULKHEAD/CRACKS Closed 21.Feb.2008This Document terminates 737-53A1225/EO Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> > 737-53A1225-1/EO* Rev.01 *AD* VERTICAL BEAM WEBS AT STA 178 PRESSURE BULKHEAD/REPAIR CancelledReason for this StatusPERMANENT MODIFICATION PERFORMED, REF EO 737-53A1225-01





23.Oct.2014Page 238/429

Document-Number Type Rev Compliance A|C Subject Status2007-03-07 AD 00 MANDATORY A/C *AD* INSTALL. OF AN ENHANCED RUDDER CONTROL SYSTEM (RSEP) Closed 21.Feb.2008

2002-20-07-R1 (SUPERSEDED)2007-03-07 (ACTIVE)737-27-1246-R1 CL (REF)737-27-1247-R2 NG (REF)737-27-1253-R3 NG (REF)737-27-1255-R3 CL (REF)737-27-1262-R1 NG (REF)737-27-1264-R2 CL (REF)737-27A1279-R1 NG (REF)737-27A1280-R1 NG (REF)737-27A1281-R0 CL (REF)737-55-1052-R1 CL (REF)

ADADSBSBSBSBSBSBSBSBSBSB

This Document SUPERSEDES 1997-05-10/AD Rev.00This Document SUPERSEDES 1998-02-01/AD Rev.00This Document SUPERSEDES 2000-22-02/AD Rev.00This Document SUPERSEDES 2002-20-07/AD Rev.00Perform within an unlimited threshold.

2007-03-07/AD Rev.00 *AD* INSTALL. OF AN ENHANCED RUDDER CONTROL SYSTEM (RSEP) Closed 21.Feb.2008This Document SUPERSEDES 1997-05-10/AD Rev.00This Document SUPERSEDES 1998-02-01/AD Rev.00This Document SUPERSEDES 2000-22-02/AD Rev.00This Document SUPERSEDES 2002-20-07/AD Rev.00

> 737-1150-27-05/SB* Rev.A *AD* AUX RUDDER POWER CONTROL PACAGE - REPL OF INPUT LEVER Not Applicable by Serial NumberAffected Rotables (Part No/Serial No/Position) Status1U1150-4 / 0962 Pos=#0 (KKM) Not Applicable

> 737-27-1246/SB* Rev.01 *AD* RUDDER & RUDDER TRIM CONTROL SYSTEM, WIRE PROVISIONS Closed 14.Mar.2005Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks


Reason for this Status





23.Oct.2014Page 239/429

Document-Number Type Rev Compliance A|C Subject StatusKKM 150405 ITEM: 1

> 737-27-1255/SB* Rev.02 *AD* RUDDER CONTROL SYSTEM; INSTALLATION OF NEW RUDDER SYS. Closed 17.Mar.2005This Document SUPERSEDES 737-27-1255/SB Rev.01This Document has been SUPERSEDED BY 737-27-1255/SB Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-27-1255/SB* Rev.03 *AD* RUDDER CONTROL SYSTEM; INSTALLATION OF NEW RUDDER SYS. See prev. DocstatusThis Document SUPERSEDES 737-27-1255/SB Rev.02This Document has been SUPERSEDED BY 737-27-1255/SB Rev.04Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Mar.2005 46130:00/H 23575/C PerfRev.:'NOTE'Reason for this StatusKKM 150404 ITEM: 1

> 737-27-1255/SB* Rev.00 *AD* RUDDER CONTROL SYSTEM; INSTALLATION OF NEW RUDDER SYS. SupersededThis Document has been SUPERSEDED BY 737-27-1255/SB Rev.01

> 737-27-1255/SB* Rev.01 *AD* RUDDER CONTROL SYSTEM; INSTALLATION OF NEW RUDDER SYS. SupersededThis Document SUPERSEDES 737-27-1255/SB Rev.00This Document has been SUPERSEDED BY 737-27-1255/SB Rev.02

> 737-27-1255/SB* Rev.04 *AD* RUDDER CONTROL SYSTEM; INSTALLATION OF NEW RUDDER SYS. See prev. DocstatusThis Document SUPERSEDES 737-27-1255/SB Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Mar.2005 46130:00/H 23575/C PerfRev.:'NOTE'Reason for this StatusKKM 150404 ITEM: 1

> 737-27-1255P2/SB* Rev.03 *AD* RUDDER CONTROL SYSTEM; INSTALLATION OF NEW. Closed 21.Feb.2008Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks






23.Oct.2014Page 240/429

Document-Number Type Rev Compliance A|C Subject StatusReason for this StatusKKM 151289 ITEM: 1

> 737-27-1264/SB* Rev.02 *AD* RUDDER & RUD. TRIM CTRL SYST. REPLACEMENT OF P5-3 PANEL Closed 17.Mar.2005Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-55-1052/SB* Rev.01 *AD* VERTICAL STAB, TRAILING EDGE BEAM INSPECTION & REWORK Closed 10.Mar.2005Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



2007-04-15 AD 00 MANDATORY A/C *AD* SICMA AERO SEAT - PAX SEATS - MODIFY AFT TRACK FITTINGS Not ApplicableNot applicable due to; SICMA Aeroseats not installed in NAS fleet.2007-04-15 (ACTIVE)90-25-005-R0 (REF)

ADSB






23.Oct.2014Page 241/429

Document-Number Type Rev Compliance A|C Subject Status2007-07-02 AD 00 MANDATORY A/C MODIFICATION OF THE OXYGEN ACTIVATION MECHANISM Not Applicable

Compliance:

AD § (f) is complied with through SB 737-25-1545 for NAS B737-800 andthrough SB 737-25-1548 for NAS B737-300.

AMOC 150S-12-128 was issued allowing extension of AD compliance time.It was not required for NAS to use AMOC, parts available.150S-12-128 (NOT USED)737-25-1545737-25-1548PRODUCTION LINE MRR3254-1596PRODUCTION LINE PRR38275-77

AMOCSBSIBPRRPRR

0001010000

2007-07-02/AD Rev.00 MODIFICATION OF THE OXYGEN ACTIVATION MECHANISM Not Applicable> 737-25-1548/SB* Rev.01 EQUIPMENT AND FURNISHINGS - PASSENGER COMPARTMENT - MODIFICATION OF

THE OXYGEN ACTIVATION MECHANISMNot Applicable by Serial Number

This Document CANCELS 737-25-1394/SB Rev.02This Document SUPERSEDES 737-25-1548/SB Rev.00

> 737-25-1548/SB* Rev.00 MOD OF THE PSU OXYGEN ACTIVATION MECHANISM Not Applicable by Serial NumberThis Document has been SUPERSEDED BY 737-25-1548/SB Rev.01

2007-07-12 AD 00 MANDATORY COMP HONEYWELL FLIGHT MANAGEMENT SYSTEMS (FMSS) Superseded (Not Applicable bySerial Number)

2007-07-12 (ACTIVE) ADThis Document has been SUPERSEDED BY 2009-08-01/AD Rev.00Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 242/429

Document-Number Type Rev Compliance A|C Subject Status2007-10-12 AD 00 MANDATORY A/C INSTALLATION OF REINFORCED FLIGHT DECK DOOR Closed 28.Nov.2003

2003-14-04 (SUPERSEDED)2005-12-05 (SUPERSEDED)2007-10-12 (ACTIVE)B22-1-18-R17 (ACTIVE)ST01335LA (ACTIVE)

ADADADSBSTC


28.Nov.2003 43180:00/H 21008/CPerfRev.:'NOTE' / Reason: KKM 150081ITEM: 1






23.Oct.2014Page 243/429

Document-Number Type Rev Compliance A|C Subject Status2007-10-12SUB1 AD 00 MANDATORY A/C INADVERTENT RELEASE OF COCKPIT DOOR DECOMPRESSION PANEL Taskcard Controlled

2003-14-04 (SUPERSEDED)2005-12-05 (SUPERSEDED)2007-10-12 (F) (ACTIVE)37-B52-51-00-5C (REPETITIVE)37-NAS-5200-002 (REPETITIVE)87-52-360-00-01 (REPETITIVE)B221001-52-03 (REF)B221001-52-03-R3 (ACTIVE)CDRB22-69 (REF)SB B221001-52-03 (REF)ST01335LA (REF)

ADADADTATATASBSBMPDTASTC

Perform within an unlimited threshold.2007-10-12SUB1/AD Rev.00 INADVERTENT RELEASE OF COCKPIT DOOR DECOMPRESSION PANEL Taskcard Controlled> 2007-10-12SUB1MPD/EO*Rev.00

2007-10-12SUB1MPD CONTROLLED BY MPD TASKS Taskcard Controlled

Carried out on the following TaskcardsTaskcard: NAS-5200-002 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks11.03.2015 74'572/H 1250:25/H Interval:3000/HPerf Dim1 (D) Perf Dim2 Perf Dim314.02.2014 71572:00/H 43151/CReason for this StatusAUTO ASSIGNED





23.Oct.2014Page 244/429

Document-Number Type Rev Compliance A|C Subject Status2007-10-12SUB2 AD 00 MANDATORY A/C GVI INSPECTION TO DETECT AND CORRECT WIRE CHAFING Closed 29.Apr.2008

2003-14-04 (SUPERSEDED)2005-12-05 (SUPERSEDED)2007-10-12 (O) (ACTIVE)B221001-52A02 (ACTIVE)SB B221001-52A02 (MOD TASK)ST01335LA (REF)

ADADADSBTASTC

Perform within an unlimited threshold.2007-10-12SUB2/AD Rev.00 GVI INSPECTION TO DETECT AND CORRECT WIRE CHAFING Closed 29.Apr.2008> B221001-52A02/SB* Rev.00 *AD* COCKPIT DOOR WIRING INSPECTION AND REWORK Closed 29.Apr.2008


B221200BM631 / 810571 Pos=#1 (KKM)

Closed / Reason: KKM 151279 ITEM: 146873 / Last Performed:29.Apr.200811951:00/H 9776/C RefDocument:Rev.NOTE

2007-10-12SUB3 AD 00 MANDATORY A/C REVISE MAINTENANCE PROGRAM FOR THE COCKPIT DOOR Closed 19.Dec.20052003-14-04 (SUPERSEDED)2005-12-05 (SUPERSEDED)2007-10-12 (ACTIVE)CDRB22-69 (REF)ST01335LA (REF)

ADADADMPDSTC


19.Dec.2005Reason: C&D AEROSPACE REPORTCDRB22-69

Reason for this StatusC&D AEROSPACE REPORT CDRB22-69





23.Oct.2014Page 245/429

Document-Number Type Rev Compliance A|C Subject Status2007-10-12SUB4 AD 00 MANDATORY A/C MODIFY THE REINFORCED FLIGHT DECK DOOR Not Applicable

2003-14-04 (SUPERSEDED)2005-12-05 (SUPERSEDED)2007-10-12 (J) (ACTIVE)B221001-52-03-R3 (ACTIVE)B221200-52-01-R1 (ACTIVE)ST01335LA (REF)

ADADADSBSBSTC

Perform within an unlimited threshold.2007-10-12SUB4/AD Rev.00 MODIFY THE REINFORCED FLIGHT DECK DOOR Not Applicable> B221001-52-03/SB* Rev.03 *AD* COCKPIT DOOR ASSY. PRESSURE RELIEF LATCH REPLACEMENT Not Applicable

This Document SUPERSEDES B221001-52-03/SB Rev.02Affected Rotables (Part No/Serial No/Position) Status

B221200BM631 / 810571 Pos=#1 (KKM)Not Applicable / Reason: N/AACCORDING TO SB

> B221001-52-03/SB* Rev.02 *AD* COCKPIT DOOR ASSY. PRESSURE RELIEF LATCH REPLACEMENT SupersededThis Document has been SUPERSEDED BY B221001-52-03/SB Rev.03Affected Rotables (Part No/Serial No/Position) StatusB221200BM631 / 810571 Pos=#1 (KKM) Superseded

> B221200-52-01/SB* Rev.01 *AD* COCKPIT DOOR ASSY. DEADBOLT ARMOUR PLATE INSTALLATION Not ApplicableAffected Rotables (Part No/Serial No/Position) Status

B221200BM631 / 810571 Pos=#1 (KKM)Not Applicable / Reason: IMPLEMENTEDBEFORE INSTALL.





23.Oct.2014Page 246/429

Document-Number Type Rev Compliance A|C Subject Status2007-11-07 AD 00 MANDATORY A/C *AD* FUEL BOOST PUMP ELECTRICAL WIRES AND SLEEVE INSP./REPL. Superseded (Not Applicable)

1998-19-09 (SUPERSEDED)1999-21-15 (SUPERSEDED)2007-11-07 (SUPERSEDED)2007-24-02 (ACTIVE)737-28A1120-R4 (REF)

ADADADADSB


2007-16-05 AD 00 MANDATORY A/C *AD* INSP. OF ELEVATOR CONTROL TAB RODS AND CTR ROD JAM NUTS Repetitive2007-16-05 (ACTIVE)37-SBB-27A1266 (REPETITIVE)737-27A1266-R0 (REF)737-27A1266-R1 (ACTIVE)

ADTASBSB

Perform within an unlimited threshold.2007-16-05/AD Rev.00 *AD* INSP. OF ELEVATOR CONTROL TAB RODS AND CTR ROD JAM NUTS Repetitive> 737-27A1266/SB Rev.01 *AD* INSP. OF ELEVATOR CONTROL TAB RODS AND CTR ROD JAM NUTS Repetitive> > 737-27A1266/EO* Rev.00 *AD* INSP. OF ELEVATOR CTR. TAB RODS AND CTR. ROD JAM NUTS *** REPETITIVE

INSPECTIONS***Repetitive


77572:00/H 47651/CPerform initially before(F) 0/H or 0/C /Interval(F):6000/H or 4500/C







23.Oct.2014Page 247/429

Document-Number Type Rev Compliance A|C Subject Status2007-18-03 AD 00 MANDATORY A/C *AD* SEAT TRACKS - VISUAL INSP. OF FLIGHT CREW SEAT LOCKS Not Applicable by Serial Number

This mod is applicable to VAR# PT187-PT188, PS971-PS978.2007-18-03 (ACTIVE)737-25A1363-R2 (ACTIVE)AD 2007-18-03 (MOD TASK)IPECO A001-25-47 (REF)PRODUCTION LINE MRR3257-1156

ADSBTASBPRR





23.Oct.2014Page 248/429

Document-Number Type Rev Compliance A|C Subject Status2007-24-02 AD 00 MANDATORY A/C AD* FUEL BOOST PUMP ELECTRICAL WIRES AND SLEEVE INSP./REPL. Repetitive

2007-11-07 (SUPERSEDED)2007-24-02 (ACTIVE)37-SBB-28A1263 (REPETITIVE)737-28A1263-R0 (REF)737-28A1263-R1 (REF)737-28A1263-R2 (ACTIVE)737-SRP-28-0113 (REF)

ADADTASBSBSBSRP

This Document SUPERSEDES 1999-21-15/AD Rev.00This Document SUPERSEDES 2007-11-07/AD Rev.00Perform within an unlimited threshold.

2007-24-02/AD Rev.00 AD* FUEL BOOST PUMP ELECTRICAL WIRES AND SLEEVE INSP./REPL. RepetitiveThis Document SUPERSEDES 1999-21-15/AD Rev.00This Document SUPERSEDES 2007-11-07/AD Rev.00

> 737-28A1263/SB Rev.02 *AD* FUEL BOOST PUMP ELECTRICAL WIRES AND SLEEVE INSP./REPL. RepetitiveThis Document CANCELS 737-28A1120/SB Rev.04

> > 737-28A1263/EO* Rev.02 FUEL BOOST PUMP ELECTRICAL WIRES AND SLEEVE INSP. *** MANDATORYREPETITIVE INSPECTION ***

Repetitive

This Document SUPERSEDES 737-28A1263/SB Rev.01Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

79536:00/HPerform initially before(F) 0/H /Interval(F):15000/H

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks06.Jul.2011 64536:00/H 37799/C 205193, N/A Was due at: 4055700/H PerfRev.:'02'





23.Oct.2014Page 249/429

Document-Number Type Rev Compliance A|C Subject Status2007-26-04 AD 00 MANDATORY A/C *AD* FUSELAGE SKIN - CIRCUMFERENTIAL BUTT SPLICE - MOD Open

This mod is applicable to LN# 1-2565.2007-26-04 (ACTIVE)737-53-1267-R0 (ACTIVE)

ADSB

Perform BEFORE 75000/C2007-26-04/AD Rev.00 *AD* FUSELAGE SKIN - CIRCUMFERENTIAL BUTT SPLICE - MOD Open> 737-53-1267/SB Rev.00 *AD* FUSELAGE SKIN - CIRCUMFERENTIAL BUTT SPLICE - MOD Open> > 737-53-1267/EO* Rev.00 *AD* FUSELAGE - SKIN - CIRCUMFERENTIAL BUTT SPLICE - MODIFI Open

This Document is terminated with implementation of 737-53-1267-01/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document


> > 737-53-1267-01/EO* Rev.00 *AD* FUSELAGE SKIN - CIRCUMFERENTIAL BUTT SPLICE - MOD OpenThis Document terminates 737-53-1267/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

75000/C Perform initially before(F) 75000/C

2008-01-01 AD 00 MANDATORY A/C RECTIFICATION OF FLIGHT DECK DOOR INST. PER STC ST01143SE Not ApplicableNAS has not implemented STC ST01143ST.2008-01-0152-2295 REV 1.(VENDOR SB)

ADSB





23.Oct.2014Page 250/429

Document-Number Type Rev Compliance A|C Subject Status2008-03-20 AD 00 MANDATORY A/C *AD* SLIDE COMPARTMENT MODIFICATION, FWD SERVICE DOOR Closed 02.Nov.2012 W/O:273620

This document is applicable to all 737CL.

Compliance:AD § (f) is complied with through SB 737-25-1567.

AD § (g) is complied with through SB 737-25-1430.737-25-1567 SB 01Perform BEFORE 16.Mar.2013

2008-03-20/AD Rev.00 *AD* SLIDE COMPARTMENT MODIFICATION, FWD SERVICE DOOR Closed 02.Nov.2012 W/O:273620> 737-25-1430/SB* Rev.01 ESCAPE SLIDE COMPARTMENT HINGE ASSEMBLY REPLACEMENT Closed 08.Mar.2005




> 737-25-1567/SB* Rev.01 SLIDE COMPARTMENT MODIFICATION, FWD SERVICE DOOR Closed 02.Nov.2012 W/O:273620This Document SUPERSEDES 737-25-1567/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks02.Nov.2012 68139:00/H 40570/C 273620, N/A Was due at: 15.Mar.2013 PerfRev.:'01'

> 737-25-1567/SB* Rev.00 SLIDE COMPARTMENT MODIFICATION, FWD SERVICE DOOR CancelledThis Document has been SUPERSEDED BY 737-25-1567/SB Rev.01Reason for this StatusManually deassigned after Document Cancelled/Superseeded





23.Oct.2014Page 251/429

Document-Number Type Rev Compliance A|C Subject Status2008-04-21 AD 00 MANDATORY A/C *AD* WINGS - CENTER WING BOX - FLOOR BEAM INSP/MOD/REPAIR Closed 07.Feb.2008

Compliance:This AD is complied with through Sb 737-57-1210, specifically;

EO 737-57-1210-01: Covers the preventive modification and terminatesthe repetitive inspections. Ref AD 2008-04-21 § (g) and (h).

EO 737-57-1210-02: Covers the repetitive inspection mandated by AD2008-04-21 § (f).2001-14-20737-57-1210737-57-1210 IN-01

ADSBSB

000200

Perform BEFORE 48000/H2008-04-21/AD Rev.00 *AD* WINGS - CENTER WING BOX - FLOOR BEAM INSP/MOD/REPAIR Closed 07.Feb.2008> 737-57-1210/SB Rev.03 WINGS - CENTER WING BOX - FLOOR BEAM INSPECTION, MODIFICATION AND

REPAIRClosed 07.Feb.2008

This Document SUPERSEDES 737-57-1210/SB Rev.02> > 737-57-1210-01/EO* Rev.02 *AD* WINGS - CENTER WING BOX - FLOOR BEAM INSP/MOD/REPAIR Closed 07.Feb.2008

This Document terminates 737-57-1210/EO Rev.02This Document has been SUPERSEDED BY 737-57-1210-01/EO Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> > 737-57-1210-01/EO* Rev.03 WINGS - CENTER WING BOX - FLOOR BEAM INSP/MOD/REPAIR See prev. DocstatusThis Document SUPERSEDES 737-57-1210-01/EO Rev.02This Document terminates 737-57-1210-02/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks07.Feb.2008 54539:00/H 30315/C PerfRev.:'NOTE'Reason for this Status





23.Oct.2014Page 252/429

Document-Number Type Rev Compliance A|C Subject StatusKKM 151394 ITEM: 1

> > 737-57-1210-02/EO* Rev.00 FLOOR BEAM - CENTER WING BOX - DETAILED INSPECTION. *** MANDATORYINTERNAL REPETITIVE DVI INSPECTION ***

Not Applicable

This Document SUPERSEDES 737-57-1210/EO Rev.02This Document is terminated with implementation of 737-57-1210-01/EO Rev.03Reason for this StatusNOT APPLICABLE DUE TO TERMINATING ACTION PERF. ON EO 737-57-1210-01

2008-05-06 AD 00 MANDATORY A/C *AD* FLOOR BEAM, LONGITUNINAL INSPECTION, BETWEEN BS 656/727 Repetitive2008-05-06 (ACTIVE)737-57-1296 (ACTIVE)SBB 737-57-1296 (MAINT TASK)

ADSBTA

Perform BEFORE 20000/C for the first timeThereafter perform in an interval of 7000/C

2008-05-06/AD Rev.00 *AD* FLOOR BEAM, LONGITUNINAL INSPECTION, BETWEEN BS 656/727 Repetitive> 737-57-1296/SB Rev.00 WINGS - CENTER WING BOX - LONGITUDINAL FLOOR BEAM INSPECTION BETWEEN

BODY STATION 656 AND BODY STATION 727Repetitive

> > 737-57-1296/EO* Rev.00 NDT/DVI INSP. CTR. WING BOX - LONGITUDINAL FLOOR BEAM INSPECTION. **MANDATORY REPETITIVE INSP. BTW BODY STA 656 & STA 727 **

Repetitive

Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document47570/C

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks01.Nov.2012 68139:00/H 40570/C 273618, N/A Was due at: 42008/C PerfRev.:'00'





23.Oct.2014Page 253/429


2008-06-24 (SUPERSEDED)2010-14-06 (ACTIVE)B/E AEROSPACE 174080-35-01SBB 737-35-1099-R1 (ACTIVE)

ADADSBSB


2008-06-27 AD 00 MANDATORY COMP BF-GOODRICH EVACUATION SYSTEM - GVI/REPL OF SHEAR-PIN Not Applicable25-343 SB 03Perform within an unlimited threshold.

2008-06-27/AD Rev.00 BF-GOODRICH EVACUATION SYSTEM - GVI/REPL OF SHEAR-PIN Not Applicable> 25-343/SB* Rev.03 GOODRICH EVACUATION SYSTEM - SLIDES - SHEAR PIN RESTRAINT INSPECTION OF Not Applicable






23.Oct.2014Page 254/429

Document-Number Type Rev Compliance A|C Subject Status2008-06-29 AD 00 MANDATORY A/C LE SLATS, MAIN TRACK DOWNSTOP ASSEMBLY INSPECTION Superseded (Superseded)

The repetitive inspection is made mandatory by AD §(f).All NAS Aircraft are group 2 AC.

AMOC in SB 737-57A1301 rev.:03:This service bulletin has been approved by the FAA. In addition, theManager of the FAA Seattle Aircraft Certification Office approves theaccomplishment of the applicable inspections, and investigative andcorrective actions specified in Table 1 of SB 737-57A1301, Revision3, as an alternative method of compliance (AMOC) to the inspections,and investigative and corrective actions required by paragraph(f) of AD 2008-06-29.2011-NM-071-AD737-57A1301737-57A1301737-57A1301737-57A1301737-57A1301 IN-01737-SRP-57-0208 (REF)

NPRMSBSBSBSBSBSRP

000001020300






23.Oct.2014Page 255/429

Document-Number Type Rev Compliance A|C Subject Status2008-08-10 AD 00 MANDATORY A/C *AD* MLG BEAM OUTBOARD STABILIZING FITTING REPLACEMENT Open

All NAS AC are group 8 AC. Per SB it is not neccesary to replacebolts, existing bolts may be re-used. NAS has not replaced bolts.Therefore there is no requirement to NDT inspect bolts attaching theFWD Fitting.

The requirement to comply with the SB is covered by AD para g and h.

Para g states that SB part II must be complied with within 36 monthsof effective date. Then 120 month GVI. NAS complies with AD para gand SB Part II.

Para h states that an alternate compliance is approved. In line 3,the AD states that the actions in para h are in liu of para g. para hof the AD covers Part I of the SB.

Since NAS performs para g of the AD. Para h is not applicable to NASaircraft.2008-08-10 (ACTIVE)37-SBB-57A1266 (REPETITIVE)737-57A1266 (REF)737-57A1266 IN 01 (REF)737-57A1266 R1 (ACTIVE)AD 2008-08-10 (SECONDARYTASK)

ADTASBSBSBTA

Perform BEFORE 18.May.20112008-08-10/AD Rev.00 *AD* MLG BEAM OUTBOARD STABILIZING FITTING REPLACEMENT Open> 737-57A1266/SB Rev.02 WINGS - ATTACH FITTINGS - LANDING GEAR ATTACH FITTINGS, MLG BEAM

OUTBOARD STABILIZING FITTING REPLACEMENTOpen






23.Oct.2014Page 256/429

Document-Number Type Rev Compliance A|C Subject Status> > 11-1072/TD* Rev.00 INSTALLATION OF FREEZEPLUG IN REAR SPAR, MSN 27285 FINAL REPAIR OF ONE

HOLE WHILE PERFORMING SB 737-57A1266Not Applicable by Serial Number

> > 737-57A1266/EO* Rev.01 *AD* VISUAL INSP. OF THE OUTB STABILIZING FITTING, WALKING B HANGER, ANDREAR SPAR ATTACH FITTING

Cancelled

This Document has been SUPERSEDED BY 737-57A1266-02/EO Rev.00Reason for this StatusManually deassigned after Document Cancelled or Superseded

> > 737-57A1266-01/EO* Rev.02 *AD* MLG BEAM OUTBOARD STABILIZING FITTING REPLACEMENT See prev. DocstatusThis Document SUPERSEDES 737-57A1266-01/EO Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks11.Mar.2005 46130:00/H 23575/C PerfRev.:'NOTE'Reason for this StatusKKM 150397 ITEM: 1

> > 737-57A1266-02/EO* Rev.00 VISUAL INSP. OF THE OUTB STABILIZING FITTING, WALKING B HANGER, AND REARSPAR ATTACH FITTING

Open


11.Mar.2015 489501Perform initially within (effective fromManufacturer Date 13.Mar.1990) (F) 0/D /Interval(F):3650/D

> 737-57A1266/SB Rev.00 *AD* MLG BEAM OUTBOARD STABILIZING FITTING REPLACEMENT Closed 11.Mar.2005This Document has been SUPERSEDED BY 737-57A1266/SB Rev.01


Cancelled


> > 737-57A1266-01/EO* Rev.00 *AD* MLG BEAM OUTBOARD STABILIZING FITTING REPLACEMENT Closed 11.Mar.2005This Document has been SUPERSEDED BY 737-57A1266-01/EO Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks





23.Oct.2014Page 257/429


11.Mar.2005 46130:00/H 23575/CKKM 150397ITEM: 1

> 737-57A1266/SB Rev.01 *AD* MLG BEAM OUTBOARD STABILIZING FITTING REPLACEMENT CancelledThis Document SUPERSEDES 737-57A1266/SB Rev.00This Document has been SUPERSEDED BY 737-57A1266/SB Rev.02


Cancelled


> > 737-57A1266-01/EO* Rev.01 *AD* MLG BEAM OUTBOARD STABILIZING FITTING REPLACEMENT SupersededThis Document SUPERSEDES 737-57A1266-01/EO Rev.00This Document has been SUPERSEDED BY 737-57A1266-01/EO Rev.02

2008-09-13 AD 00 MANDATORY A/C *AD* STRUCTURAL SIGIFICANT ITEM INSPECTIONS INCORPORATION Repetitive2008-09-13 ADPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

24.Jun.2008 55637:00/H 31168/CPerfRev.:'NOTE' / Reason: BOEINGDOCUMENT D6-82669

Reason for this StatusBOEING DOCUMENT D6-82669





23.Oct.2014Page 258/429

Document-Number Type Rev Compliance A|C Subject Status2008-09-15 AD 00 MANDATORY A/C *AD* FLIGHT DECK NUMBER 2, 4 AND 5 WINDOWS - INSPECTION Repetitive

2008-09-15 (ACTIVE)37-SBB-56A1023 (REPETITIVE)37-SBB-56A1023P1 (REPETITIVE)737-56-1026 (REF)737-56A1023-R0 (ACTIVE)

ADTATASBSB

Perform within an unlimited threshold.2008-09-15/AD Rev.00 *AD* FLIGHT DECK NUMBER 2, 4 AND 5 WINDOWS - INSPECTION Repetitive> 737-56A1023/SB Rev.01 *AD* FLIGHT DECK NUMBER 2, 4 AND 5 WINDOWS - INSPECTION Repetitive> > 737-56A1023/EO* Rev.00 FLIGHT DECK WINDOWS NUMBER 2 REPETITIVE INSPECTION *** REPETITIVE

INSPECTION ***Repetitive


22.Jan.2017 79072:00/H



07.Feb.2014 71572:00/H 43151/C 436900, N/AWas due at: 12.Jun.2014 and 4322040/HPerfRev.:'00'

> > 737-56A1023P1/EO* Rev.00 *AD* FLIGHT DECK NO. 4+5 WINDOWS INSPECTION AND REPLACEMENT ***MANDATORY REPETITIVE INSPECTION ***






23.Oct.2014Page 259/429

Document-Number Type Rev Compliance A|C Subject Status2008-10-09 AD 01 MANDATORY A/C *AD* SFAR 88 REQUIREMENTS INCORPORATION Taskcard Controlled

FAA AMOC letter:120S-09-230 approves the change of wording in AWL tasks in the BoeingMaintenance program.140S-11-202a approves deviations to 28-AWL-05.

Refer to NAS approved maint. program.

NAS has not inmplemented any of the FAA AMOC.120S-09-230 (ACTIVE)140S-11-202A140S-14-892008-10-09 (SUPERSEDED)2008-10-09-R1 (ACTIVE)28-011-00-01 (28-AWL-01)28-022-04-01 (28-AWL-20)28-028-23-01 (28-AWL-23)28-AWL-02 &-24 (NA TO NAS)28-AWL-04 TO -19 (NA TO NAS)28-AWL-0528-AWL-21, SB NOT INCORP.NAS-2841-001 (28-AWL-03)NAS-2841-002 (28-AWL-22)

AMOCAMOCAMOCADADTATATATATATATATATA

0000000000000000000000000000






23.Oct.2014Page 260/429

Document-Number Type Rev Compliance A|C Subject StatusDocument-Number Type Rev Compliance A|C Subject Status




23.Oct.2014Page 261/429

Document-Number Type Rev Compliance A|C Subject Status2008-11-04 AD 00 MANDATORY A/C *AD* ENTRY & GALLEY DOORWAY, FWD. UPPET & LOWER HINGE CUTOUT Superseded (Open)

2008-11-04 (ACTIVE)37-NAS-5312-001 (REPETITIVE)737-53A1200737-53A1200-1737-53A1200-2737-53A1200-3737-53A1200-4737-53A1200-5737-SRP-53-0134 (REF)

ADTASBEOEOEOEOEOSRP

000001000000000000


2008-11-04/AD Rev.00 *AD* ENTRY & GALLEY DOORWAY, FWD. UPPET & LOWER HINGE CUTOUT OpenThis Document has been SUPERSEDED BY 2014-05-21/AD Rev.0

> 737-53A1200/SB Rev.00 *AD* ENTRY & GALLEY DOORWAY, FWD. UPPET & LOWER HINGE CUTOUT Taskcard ControlledThis Document has been SUPERSEDED BY 737-53A1200/SB Rev.02

> > 737-53A1200-1/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD ENTRY DOORWAY UPPER &LOWER HINGE CUTOUT INSPECTION. GROUP 2 AIRPLANES

Superseded

This Document has been SUPERSEDED BY 737-53A1200-01/EO Rev.00This Document has been SUPERSEDED BY 737-53A1200-02/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

07.Feb.2008 54542:00/H 30315/CPerfRev.:'NOTE' / Reason: AMICOS WO151169 KKM 37-SBB-53A1200-1 HINGECUTOUT

Reason for this StatusAMICOS WO 151169 KKM 37-SBB-53A1200-1 HINGE CUTOUT INSP, ATCL REF MRC

> > 737-53A1200-2/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD ENTRY DOORWAY UPPER &LOWER HINGE CUTOUT INSPECTION. GROUP 3 AIRPLANES


This Document has been SUPERSEDED BY 737-53A1200-03/EO Rev.00This Document has been SUPERSEDED BY 737-53A1200-04/EO Rev.00





23.Oct.2014Page 262/429

Document-Number Type Rev Compliance A|C Subject Status> > 737-53A1200-3/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD ENTRY DOORWAY UPPER &

LOWER HINGE CUTOUT INSPECTION. GROUP 4 AIRPLANESNot Applicable by Serial Number


> > 737-53A1200-4/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD GALLEY DOORWAY UPPER &LOWER HINGE CUTOUT INSPECTION. GROUP 2 AIRPLANES

Cancelled

This Document has been SUPERSEDED BY 737-53A1200-07/EO Rev.00This Document has been SUPERSEDED BY 737-53A1200-08/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks


Reason for this StatusManually deassigned after Document Cancelled or Superseded

> > 737-53A1200-5/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD GALLEY DOORWAY UPPER &LOWER HINGE CUTOUT INSPECTION. GROUP 3 & 4 AIRPLANES



> > 737-53A1200MPD/EO*Rev.00

737-53A1200MPD CONTROLLED BY MPD TASKS Taskcard Controlled


> 737-53A1200/SB Rev.02 FUSELAGE - STRUCTURE AROUND OPENINGS - FORWARD ENTRY AND FORWARDGALLEY SERVICE DOORWAY UPPER AND LOWER HINGE CUTOUT

Repetitive

This Document SUPERSEDES 737-53A1200/SB Rev.00This Document SUPERSEDES 737-53A1200/SB Rev.01

> > 737-53A1200-01/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD ENTRY DOORWAY UPPERHINGE CUTOUT INSPECTION. GROUP 2 AIRPLANES

Closed 07.Jul.2011

This Document SUPERSEDES 737-53A1200-1/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks





23.Oct.2014Page 263/429


07.Jul.2011 54542:00/H 30315/C

Was due at: 48315/C PerfRev.:'00' PERFPERMANENT REP ON FWD ENTRYDOOR UPPER HINGE ACC SR1-748133531 AND FAA 8100-9

Reason for this StatusPERF PERMANENT REP ON FWD ENTRY DOOR UPPER HINGE ACC SR 1-748133531 ANDFAA 8100-9

> > 737-53A1200-02/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD ENTRY DOORWAY LOWERHINGE CUTOUT INSPECTION. GROUP 2 AIRPLANES

Repetitive

This Document SUPERSEDES 737-53A1200-1/EO Rev.00NOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

48315/C

Perform initially within (effective from25.Jun.2008) (L) 3000/C Perform initiallywithin (effective from 25.Jun.2008) (L)20000/C / Interval(F):18000/C





This Document SUPERSEDES 737-53A1200-2/EO Rev.00> > 737-53A1200-04/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD ENTRY DOORWAY LOWER

HINGE CUTOUT INSPECTION. GROUP 3 AIRPLANESNot Applicable by Serial Number

This Document SUPERSEDES 737-53A1200-2/EO Rev.00> > 737-53A1200-05/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD ENTRY DOORWAY UPPER








23.Oct.2014Page 264/429

Document-Number Type Rev Compliance A|C Subject StatusThis Document SUPERSEDES 737-53A1200-3/EO Rev.00

> > 737-53A1200-07/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD GALLEY DOORWAY UPPERHINGE CUTOUT INSPECTION. GROUP 2 AIRPLANES

Repetitive


48315/C

Perform initially within (effective from22.Apr.2014) (L) 3000/C Perform initiallywithin (effective from 22.Apr.2014) (L)20000/C / Interval(F):18000/C



> > 737-53A1200-08/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD GALLEY DOORWAY LOWERHINGE CUTOUT INSPECTION. GROUP 2 AIRPLANES

Repetitive


48315/C




> > 737-53A1200-09/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD GALLEY DOORWAY UPPERHINGE CUTOUT INSPECTION. GROUP 3 & 4 AIRPLANES


This Document SUPERSEDES 737-53A1200-5/EO Rev.00





23.Oct.2014Page 265/429

Document-Number Type Rev Compliance A|C Subject Status> > 737-53A1200-10/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD GALLEY DOORWAY LOWER

HINGE CUTOUT INSPECTION. GROUP 3 & 4 AIRPLANESNot Applicable by Serial Number


2008-12-03 AD 00 MANDATORY A/C *AD* AUXILIARY FUEL TANKS INSTALLED IN ACC. WITH SPEC. STC Not ApplicableNAS has no auxiliary fuel tanks installed2008-12-03 (ACTIVE)SA3992NM, SA3980NM (REF)

ADSTC

2008-13-12 AD 01 MANDATORY A/C AD* FRAME & BULK:UPPER FRAME TO SIDE FRAME SPLICE INSP & MOD OpenThis mod is applicable to LN# 1-1919.2008-13-12 (REF)2008-13-12 R1 (ACTIVE)737-53A1261737-53A1261737-53A1261-01

ADADEOSBEO

0000000000

Perform within an unlimited threshold.2008-13-12/AD Rev.01 AD* FRAME & BULK:UPPER FRAME TO SIDE FRAME SPLICE INSP & MOD Open> 737-53A1261/SB Rev.00 *AD* FRAME&BULK:UPPER FRAME TO SIDE FRAME SPLICE INSP & MOD Open> > 737-53A1261/EO* Rev.00 FRAMES AND BULKHEAD - UPPER FRAME TO SIDE FRAME SPLICE INSP REPETITIVE

INSP.Repetitive




> > 737-53A1261-01/EO* Rev.00 *AD* FRAME&BULK:UPPER FRAME TO SIDE FRAME SPLICE MODIFICATION. Term.Action openDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT





23.Oct.2014Page 266/429

Document-Number Type Rev Compliance A|C Subject Status2008-13-25 AD 00 MANDATORY A/C *AD* WEB INSPECTION - MAIN WHEEL WELL PRESSURE DECK Not Applicable

This mod is applicable to LN# 2587,2594.2008-13-25 (ACTIVE)737-57-0199 (REF)737-57-1289-R0 (ACTIVE)

ADSRPSB

2008-13-25/AD Rev.00 *AD* WEB INSPECTION - MAIN WHEEL WELL PRESSURE DECK Not Applicable> 737-57-1289/SB* Rev.00 *AD* WEB INSPECTION - MAIN WHEEL WELL PRESSURE DECK Not Applicable by Serial Number

2008-15-05 AD 00 MANDATORY A/C *AD* OUTBOARD FLAP CARRIAGE SPINDLE CORROSION, INSPECTION Superseded (Superseded)This Document has been SUPERSEDED BY 2009-23-10/AD Rev.00

2008-15-05 XF AD 00 MANDATORY A/C *AD* OUTBOARD FLAP CARRIAGE SPINDLE CORROSION, PN/SN READ OF Superseded (Closed 05.Jun.2008)2008-15-05 (SUPERSEDED)2009-23-10 (ACTIVE)37-SBB-57A1304P2 (REPETITIVE)737-57A1218 (REF)737-57A1277 (REF)737-57A1304 (ACTIVE)737-SRP-57-0221 (REF)SBB 737-57A1304 (MAINT TASK)

ADADTASBSBSBSRPTA

This Document has been SUPERSEDED BY 2009-23-10/AD Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

05.Jun.2008 55459:00/H 31034/CPerfRev.:'NOTE' / Reason:ACCOMPLISHED ON WO:151472

Reason for this StatusACCOMPLISHED ON WO:151472





23.Oct.2014Page 267/429

Document-Number Type Rev Compliance A|C Subject Status2008-17-03 AD 00 MANDATORY A/C *AD* FR BS303.9,WEB CRACKS, HOLES FOR DOOR STOP FITT STRAP Closed 18.Feb.2008

This mod is applicable to LN# 1-2765.

Compliance:

(f) For airplanes identified in Boeing Alert Service Bulletin737-53A1188, Revision 2, dated May 9, 2007, including airplanesmodified by the repair/preventive change specified in the originalversion, dated April 9, 1998; or Revision 1, dated March 18, 1999; ofthe service bulletin: Do detailed and high frequency eddy current(HFEC) inspections in the web and doubler around the slotted holesin the frame web at stringers 15L and 16L, in accordance with theAccomplishment Instructions of Revision 2 of the service bulletin.

(g) For airplanes identified in Boeing Alert Service Bulletin737-53A1197, dated August 25, 2006: Do an ultrasound inspection ofthe slot-shaped cutout in the web for the door stop strap atstringer 16L, an HFEC inspection of the web along the upper and loweredges of the doubler around the doorstop strap at stringer 16L, and adetailed inspection of the web around the doubler for thecutout at stringer 16L, in accordance with the AccomplishmentInstructions of the service bulletin. Do the inspections at theapplicable time specified in paragraph 1.E. of the service bulletin,except as provided by paragraph (h) of this AD. Do all applicablecorrective actions before further flight in accordance with theservice bulletin, except as provided by paragraph (i) of this AD.Repeat the inspections at intervals not to exceed 4,500 flightcycles, until accomplishment of the repair/preventive change inaccordance with the service bulletin, which terminates the repetitiveinspections.





23.Oct.2014Page 268/429

Document-Number Type Rev Compliance A|C Subject Status737-53-1188737-53-1188737-53A1188737-53A1188 IN-02737-SRP-53-149 (REF)

SBSBSBSBSRP

00010200

Perform within an unlimited threshold.2008-17-03/AD Rev.00 *AD* FR BS303.9,WEB CRACKS, HOLES FOR DOOR STOP FITT STRAP Closed 18.Feb.2008> 737-53A1188/SB* Rev.02 *AD* FR BS303.9,WEB CRACKS, HOLES FOR DOOR STOP FITT STRAP Not Applicable by Serial Number

This Document has been SUPERSEDED BY 737-53A1188/SB Rev.03> 737-53A1188/SB Rev.03 FUSELAGE - BODY STATION 303.9 FRAME - WEB CRACKS AT HOLES FOR DOOR STOP

INTERCOSTAL STRAP AT STRINGERS 15 AND 16 LEFT -Not Applicable

This Document SUPERSEDES 737-53A1188/SB Rev.02> > 737-53A1188-01/EO* Rev.00 FUSELAGE - BODY STATION 303.9 FRAME - WEB CRACKS AT HOLES FOR DOOR STOP

INTERCOSTAL STRAP AT STRINGERS 15 AND 16 LEFT -Not Applicable by Serial Number

> 737-53A1197/SB Rev.02 *AD* FUSE, BS303.9 CRACKS AT HOLE FOR DOOR STOP AT STR 16 Closed 18.Feb.2008> > 737-53A1197/EO* Rev.00 FUSELAGE, BS303.9 CRACKS AT HOLE FOR DOOR STOP AT STR 16 L/H Cancelled


18.Feb.2008 54542:00/H 30315/CPerfRev.:'NOTE' / Reason: AMICOS WO151168 KKM 37-SBB-53A1197 BS303.9FRAME

Reason for this StatusPREVENTIVE MODIFICATION PERFORMED ON EO 737-53A1197-01

> > 737-53A1197-01/EO* Rev.00 *AD* FUSE, BS303.9 CRACKS AT HOLE FOR DOOR STOP AT STR 16 Closed 07.Feb.2008Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







23.Oct.2014Page 269/429

Document-Number Type Rev Compliance A|C Subject Status2008-17-13 AD 00 MANDATORY A/C *AD* LAVATORY A STREIGHT TO 90DEG HOSE ASSY, REPLACEMENT OF Closed 08.Nov.2012 W/O:273644

SB Item F Approval:This service bulletin has been approved by the FAA. In addition, theManager of the FAA Seattle Aircraft Certification Office approves theaction (i.e. inspection or modification) defined in this servicebulletin as an alternative method of compliance to the requirementsof paragraph (f) of AD 2008-17-13. All provisions of AD 2008-17-13that are not specifically referenced in the above statement remainfully applicable and must be complied with.2008-17-13 (ACTIVE)737-38A1054 (ACTIVE)AD 2008-17-13 (TASK)SBB 737-38A1054 (MOD-TASK)

ADSBTATA

Perform BEFORE 05.Nov.20132008-17-13/AD Rev.00 *AD* LAVATORY A STREIGHT TO 90DEG HOSE ASSY, REPLACEMENT OF Closed 08.Nov.2012 W/O:273644> 737-38A1054/SB* Rev.00 *AD* LAVATORY A STREIGHT TO 90DEG HOSE ASSY, REPLACEMENT OF Cancelled

This Document has been SUPERSEDED BY 737-38A1054/SB Rev.01Reason for this StatusManually deassigned after Document Cancelled/Superseeded

> 737-38A1054/SB* Rev.01 WATER/WASTE - PASSENGER WATER SYSTEM, LAVATORY A STRAIGHT TO 90 DEGREEHOSE ASSEMBLY REPLACEMENT

Closed 08.Nov.2012 W/O:273644

This Document SUPERSEDES 737-38A1054/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks08.Nov.2012 68139:00/H 40570/C 273644, N/A Was due at: 04.Nov.2013 PerfRev.:'01'





23.Oct.2014Page 270/429

Document-Number Type Rev Compliance A|C Subject Status2008-19-03 AD 00 MANDATORY A/C *AD* FUSELAGE SKIN-STR S-1/2R, STA 400-460 DVI INSPECTION Superseded (Superseded)

Faa AMOC letter approves certain repairs as AMOC for this AD andterminates the need for further repetitive inspections for therepaired area.2008-19-03 (ACTIVE)737-53A1293 (ACTIVE)737-SRP-53-0334 (REF)FAA LETTER 120S-09-460

ADSBSRPAMOC


2008-21-03 AD 00 MANDATORY A/C *AD* NACELLE STRUT - MID SPAR FUSE PIN - INSPECT/REPAIR/MOD Superseded (Superseded)2008-21-03 (ACTIVE)37-SBB-54A1044 (REPETITIVE)737-54-1044-R0 (REF)737-54A1044-R2 (ACTIVE)737-SRP-54-0115 (REF)PRODUCTION LINEPRR35005-273RS

ADTASBSBSRPPRR


2008-22-01 AD 00 MANDATORY A/C AUXILIARY FUEL TANKS PER SPEC STC, DEACTIVATION OF. Not ApplicableNAS has no auxiliary fuel tanks installed.2008-22-01 (ACTIVE) ADReason for this StatusAUTO ASSIGNED





23.Oct.2014Page 271/429

Document-Number Type Rev Compliance A|C Subject Status2008-23-07 AD 00 MANDATORY A/C AIRPLANE FLIGHT MANUAL REVISION Closed 25.Nov.2008

2008-23-07 (ACTIVE)AD2008-23-07 (MAINT TASK)

ADTA


25.Nov.2008Reason: AFM REVISED BY INSERTINGAD

Reason for this StatusAFM REVISED BY INSERTING AD

2008-23-09 AD 00 MANDATORY A/C *AD* EQUIPMENT/FURNISHINGS - INSULATION BLANKETS, REPL OF Not ApplicableOnly MSN: 24256 in NAS fleet is applicable.All other AC are Not Applicable per Boeing SB.737-25-1572 SB 00

2008-23-09/AD Rev.00 *AD* EQUIPMENT/FURNISHINGS - INSULATION BLANKETS, REPL OF Not Applicable> 737-25-1572/SB* Rev.00 *AD* EQUIPMENT/FURNISHINGS - INSULATION BLANKETS, REPL OF Not Applicable

Reason for this StatusNOT APPLICABLE BY VARIABLE NUMBER. AFFECTED INSULATION TYPE NOT INST.





23.Oct.2014Page 272/429

Document-Number Type Rev Compliance A|C Subject Status2008-24-05 AD 00 MANDATORY A/C WINDSHIELD WIPER MOTORS - REPLACEMENT OF Not Applicable

737-30A1057 IN-01 SB 00Perform within an unlimited threshold.

2008-24-05/AD Rev.00 WINDSHIELD WIPER MOTORS - REPLACEMENT OF Not Applicable> 737-30A1059/SB* Rev.02 ICE AND RAIN PROTECTION - WINDSHIELD WIPER SYSTEM - CHANGE THE

WINDSHIELD WIPER MOTORNot Applicable

This Document SUPERSEDES 737-30A1059/SB Rev.01Reason for this StatusAUTO ASSIGNED

> 737-30A1059/SB* Rev.01 ICE AND RAIN PROTECTION - WINDSHIELD WIPER SYSTEM - CHANGE THEWINDSHIELD WIPER MOTOR

Not Applicable / Special Text: Thisaicraft is Not Applicable by AircraftModel.

This Document has been SUPERSEDED BY 737-30A1059/SB Rev.02Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 273/429

Document-Number Type Rev Compliance A|C Subject Status2009-0036 AD 00 MANDATORY COMP FAN BLADES - 25 DEGREE MID-SPAN SHROUDS INSP. Not Applicable

Repetitive Inspection of the Platform Underside of the 25 DegreesMidspan Shroud Fan Blades2009-00362010-12-033-72-10673-72-1067NAS-7221-001

ADADSBSBTA

0000000100

Perform BEFORE 20.May.20092009-0036/AD Rev.00 FAN BLADES - 25 DEGREE MID-SPAN SHROUDS INSP. Not Applicable> 3-72-1067/SB* Rev.01 FAN BLADES - 25 DEGREE MID-SPAN SHROUDS INSP. Not Applicable


CFM56-3B2 / 724473 Pos=LH (KKM)Not Applicable / Reason: NA - 37DEGREES MIDSPAN SHROUD FANBLADES INST.

CFM56-3B2 / 725495 Pos=RH (KKM)Not Applicable / Reason: NA - 37DEGREES MIDSPAN SHROUD FANBLADES INST.

2009-02-06 AD 01 MANDATORY A/C *AD* FUSELAGE FRAMES-WIRE PENETRATION HOLE-INSP/REPAIR & MOD Superseded (Superseded)2009-02-06R1 (ACTIVE)37-SBB-53A1279 (REPETITIVE)737-53A1279-R0 (ACTIVE)737-SRP-53-0289 (REF)AD 2009-02-06 (SUPERSEDED)SBB 737-53A1279 (TERMINATING)

ADTASBSRPADTA






23.Oct.2014Page 274/429

Document-Number Type Rev Compliance A|C Subject Status2009-02-06 AD 00 MANDATORY A/C *AD* SUPERSEDED BY AD 2009-02-06R1 Superseded (Not Applicable)

2009-02-06 (SUPERSEDED)2009-02-06R1 (ACTIVE)37-SBB-53A1279 (REPETITIVE)737-53A1279-R0 (ACTIVE)737-SRP-53-0289 (REF)SBB 737-53A1279 (TERMINATING)

ADADTASBSRPTA

This Document has been SUPERSEDED BY 2009-02-06/AD Rev.01Reason for this StatusSUPERSEDED BY AD 2009-02-06R1

2009-0251-E AD 00 MANDATORY A/C HALON PORTABLE FIRE EXT - INSPECTION OF Not ApplicableHalon bottles with poor quality of halon.

NAS does not install FFE Halon bottles.2010-01-03 (REF ONLY)AD 2009-0251-EAD 2009-0251-E (ACTIVE)AD 2009-0262 (REF ONLY)

ADTAADAD






23.Oct.2014Page 275/429

Document-Number Type Rev Compliance A|C Subject Status2009-0262 AD 00 MANDATORY A/C HALON PORTABLE FIRE EXT - INSPECTION OF Superseded (Superseded)

Halon bottles with poor quality of halon. Further PN/SN found to becontaminated, ref FFE ASB.

NAS does not install FFE Halon extinguishers.2010-01-03 (REF ONLY)AD 2009-0251-E (REF ONLY)AD 2009-0262AD 2009-0262 (SUPERCEEDED)AD 2009-0262R1 (ACTIVE)ASB 26-115-C (FFE SB)

ADADTAADADSB

This Document has been SUPERSEDED BY 2009-0262/AD Rev.01

2009-0262 AD 01 MANDATORY A/C HALON PORTABLE FIRE EXT - INSPECTION OF Not ApplicableHalon bottles with poor quality of halon. Further PN/SN found to becontaminated, ref FFE ASB.

NAS does not install FFE Halon extinguishers.2010-01-03 (REF ONLY)AD 2009-0251-E (REF ONLY)AD 2009-0262AD 2009-0262 (SUPERCEEDED)AD 2009-0262R1 (ACTIVE)ASB 26-115-C (FFE SB)

ADADTAADADSB

This Document SUPERSEDES 2009-0262/AD Rev.00Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 276/429

Document-Number Type Rev Compliance A|C Subject Status2009-0278 AD 00 MANDATORY A/C HALON PORTABLE FIRE EXT - INSPECTION OF Not Applicable

Halon bottles with poor quality of halon.

NAS does not install SICLI Halon extinguishers.AD 2009-0278 (ACTIVE) ADReason for this StatusAUTO ASSIGNED

2009-04-15 AD 00 MANDATORY A/C *AD* STRINGER TIE CLIPS - STA 360 TO 907, S10R/L INSP/REPAIR Repetitive1993-08-04 (REF)2009-04-15 (ACTIVE)37-SBB-53-1268-A (REPETITIVE)737-53-1085-R1 (REF)737-53-1268-R0 (ACTIVE)737-SRP-53-0212 (REF)NPRM 2007-NM-085-AD (REF)PRODUCTION LINEMRR3534-1595S

ADADTASBSBSRPADPRR

Perform within an unlimited threshold.2009-04-15/AD Rev.00 *AD* STRINGER TIE CLIPS - STA 360 TO 907, S10R/L INSP/REPAIR Repetitive> 737-53-1268/SB Rev.00 *AD* STRINGER TIE CLIPS - STA 360 TO 907, S10R/L INSP/REPAIR Repetitive> > 737-53-1268-A/EO* Rev.00 *AD* FUSELAGE - STRINGER TIE CLIPS - STA 360 TO 907, S10R/L *** MANDATORY

REPETITIVE NDT AND DETAILED INSPECTION ***Repetitive




07.Feb.2008 54542:00/H 30315/CPerfRev.:'NOTE' / Reason: AMICOS WO151295 KKM 37-SBB-53-1268-ASTRINGER TIE





23.Oct.2014Page 277/429

Document-Number Type Rev Compliance A|C Subject Status2009-05-08 AD 00 MANDATORY COMP TRIMBLE OR FREEFLIGHT SYSTEMS, SOFWARE UPDATE Not Applicable by Serial Number

2009-05-08 (ACTIVE) ADAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

2009-07-11 AD 00 MANDATORY A/C *AD* VERTICAL STAB. AUX STRUC., DORSAL FIN AY INSP/PREV MOD Closed 27.Jun.2011 W/O:2051742004-22-05737-53A1266737-55-1057

ADSBSB

000000

This Document SUPERSEDES 2004-22-05/AD Rev.00Perform BEFORE 30.Aug.2013

2009-07-11/AD Rev.00 *AD* VERTICAL STAB. AUX STRUC., DORSAL FIN AY INSP/PREV MOD Closed 27.Jun.2011 W/O:205174This Document SUPERSEDES 2004-22-05/AD Rev.00

> 737-53A1266/SB* Rev.00 *AD* FUSELAGE - DORSAL FIN NOSE CAP MODIFICATION Closed 27.Jun.2011 W/O:205174Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks27.Jun.2011 64534:00/H 37798/C 205174, N/A Was due at: 39315/C PerfRev.:'00'

> 737-55-1057/SB* Rev.00 *AD* VERTICAL STAB. AUX STRUC., DORSAL FIN AY INSP/PREV MOD Closed 13.Feb.1999Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

13.Feb.1999PerfRev.:'NOTE' / Reason: REPLACED BYSB737-53A1266

Reason for this StatusREPLACED BY SB737-53A1266

2009-08-01 AD 00 MANDATORY COMP HONEYWELL FLIGHT MANAGEMENT SYSTEMS (FMSS) Not Applicable by Serial Number2007-07-12 (ACTIVE) ADThis Document SUPERSEDES 2007-07-12/AD Rev.00Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 278/429

Document-Number Type Rev Compliance A|C Subject Status2009-09-06 AD 00 MANDATORY A/C *AD* AIRSTAIR DOOR CUTOUT - WEB & INTERCOASTAL INSP./MOD. Closed 07.Feb.2008

2009-09-06 (ACTIVE)737-53A1269-RO (ACTIVE)737-SRP-53-0249 (REF)AD 2009-09-06 (REF TASK)SBB 737-53A1269 (INSP-TASK)

ADSBSRPTATA

Perform BEFORE 45000/C2009-09-06/AD Rev.00 *AD* AIRSTAIR DOOR CUTOUT - WEB & INTERCOASTAL INSP./MOD. Closed 07.Feb.2008> 737-53A1269/SB* Rev.00 *AD* AIRSTAIR DOOR CUTOUT - WEB & INTERCOASTAL INSP./MOD. Closed 07.Feb.2008








23.Oct.2014Page 279/429

Document-Number Type Rev Compliance A|C Subject Status2009-09-07 AD 00 MANDATORY COMP *AD* MLG RETRACT ACTUATOR BEAM INSPECTION AND REWORK Open

AD 2009-09-07 mandate a repetetive overhaul interval of 10 years.Note that serials that have performed SB 737-32A1355 Rev.1 or Rev.2might show with status "open" if performed prior to AD issue date.

EO 737-32A1355-01 covers the initial overhaul requirement, before22.apr.2011.

EO 737-32A1355P1 covers repeat inspection (2 years interval).EO 737-32A1355P2 covers repeat inspection (10 years interval)2009-09-07 (ACTIVE)37-SBB-32A1355P1 (REPEAT-TASK)37-SBB-32A1355P2 (REPEAT-TASK)737-32A1355-R1 (REF)737-32A1355-R2 (ACTIVE)737-32A1355-RO (REF)AD 2009-09-07 (SCONDARY TASK)PRODUCTION LINEPRR35005-245RSSBB 737-32A1355 (MOD-TASK)

ADTATASBSBSBTAPRRTA

Perform BEFORE 31.Dec.20102009-09-07/AD Rev.00 *AD* MLG RETRACT ACTUATOR BEAM INSPECTION AND REWORK Open> 737-32A1355/SB Rev.02 LANDING GEAR - MAIN GEAR EXTENSION AND RETRACTION - RETRACT ACTUATOR

BEAM INSPECTION AND REWORKOpen

> > 737-32A1355-01/EO* Rev.00 *AD* MLG RETRACT ACTUATOR BEAM INSPECTION/REWORK/OVERHAUL Closed 10.Sep.2008Affected Rotables (Part No/Serial No/Position) Status

65-46108-19 / 1051 Pos=RH (KKM)Closed / Reason: EO403526 44610 / LastPerformed:27.Jun.2005 46143:00/H23575/C RefDocument: Rev.NOTE





23.Oct.2014Page 280/429


65-46108-17 / 75 Pos=LH (KKM)Closed / Reason: WO EO662798 44611 /Last Performed:10.Sep.2008 54036:00/H29925/C RefDocument: Rev.NOTE

> > 737-32A1355P1/EO* Rev.00 *AD* *AD* MLG RETRACT ACTUATOR BEAM REPEAT INSPECTION Not ApplicableAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

> > 737-32A1355P2/EO* Rev.00 *AD* *AD* MLG RETRACT ACTUATOR BEAM REPEAT OVERHAUL OpenAffected Rotables (Part No/Serial No/Position) Status65-46108-17 / 75 Pos=LH (KKM) Open / Next Due:08.Sep.201865-46108-19 / 1051 Pos=RH (KKM) Open / Next Due:25.Jun.2015





23.Oct.2014Page 281/429

Document-Number Type Rev Compliance A|C Subject Status2009-11-02 AD 00 MANDATORY COMP HPC SPOOL 4-9 - REPLACEMENT OF CERTAIN P/N AND S/N Not Applicable

Applicable to:HPC 4-9 Spools by PN and SN

9513M93G08 MPON16411590M29G01 GWN0087D1590M29G01 GWN00MG21590M29G01 GWN011LG1590M29G01 GWN012851590M29G01 GWN021JC1590M29G01 GWNFY9231590M29G01 GWNFY9241590M29G01 GWNPA7561590M29G01 GWNPG0151590M29G01 GWNWC5151590M29G01 GWNWR5231590M29G01 GWNWT6311590M29G01 GWNYC4951588M89G03 GWN03K1R1588M89G03 GWN03N611588M89G03 GWN03N6C1588M89G03 GWN040L91588M89G03 GWN0468N1588M89G03 GWN05AM01277M97G02 GWNE12981277M97G02 GWNE15641277M97G02 GWNJ78911277M97G02 GWNT41879513M93G11 GWNB33731358M94G01 GWNU0169

2009-11-02/AD Rev.00 HPC SPOOL 4-9 - REPLACEMENT OF CERTAIN P/N AND S/N Not Applicable





23.Oct.2014Page 282/429

Document-Number Type Rev Compliance A|C Subject Status> 2009-11-02-01/EO* Rev.00 HPC SPOOL 4-9 - REPLACEMENT OF CERTAIN P/N AND S/N - CFM56-7B Not Applicable by Serial Number

Affected Rotables (Part No/Serial No/Position) Status1590M29G01 / GWNYN282 Pos=RH (KKM) Not Applicable1588M89G03 / GWN094F0 Pos=LH (KKM) Not Applicable

> 2009-11-02-02/EO* Rev.00 HPC SPOOL 4-9 - REPLACEMENT OF CERTAIN P/N AND S/N - CFM56-3 Not Applicable by Serial NumberAffected Rotables (Part No/Serial No/Position) Status1588M89G03 / GWN094F0 Pos=LH (KKM) Not Applicable1590M29G01 / GWNYN282 Pos=RH (KKM) Not Applicable

2009-12-05 AD 00 MANDATORY A/C *AD* EFIS COOLING SUPPLY OFF LIGHT WIRING, MODIFICATION OF Closed 27.Jun.2011 W/O:2051512009-12-05 (ACTIVE)737-21A1156-R0 (REF)737-21A1156-R1 (REF)737-21A1156-R2 (ACTIVE)737-SRP-24-0122 (REF)

ADSBSBSBSRP

Perform BEFORE 16.Jul.20112009-12-05/AD Rev.00 *AD* EFIS COOLING SUPPLY OFF LIGHT WIRING, MODIFICATION OF Closed 27.Jun.2011 W/O:205151> 737-21A1156/SB* Rev.02 *AD* EFIS COOLING SUPPLY OFF LIGHT WIRING, MODIFICATION OF Closed 27.Jun.2011 W/O:205151

This Document has been SUPERSEDED BY 737-21A1156/SB Rev.03Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks27.Jun.2011 64534:00/H 37798/C 205151, N/A Was due at: 16.Jul.2011 PerfRev.:'02'

> 737-21A1156/SB* Rev.03 EQUIPMENT COOLING SYSTEM - ELECTRONIC FLIGHT INSTRUMENT SYSTEMCOOLING SUPPLY OFF LIGHT WIRING CHANGE

See prev. Docstatus

This Document SUPERSEDES 737-21A1156/SB Rev.02Reason for this StatusPERFORMED ON REV 2





23.Oct.2014Page 283/429

Document-Number Type Rev Compliance A|C Subject Status2009-12-06 AD 00 MANDATORY A/C INST. OF IN-FLIGHT. ENT SYSTEM CB, RELAY AND WIRING Not Applicable

This mod is applicable to LN# 1-1615.2009-12-06 (ACTIVE)737-24-1145 (ACTIVE-CL)737-24-1147-R0 (REF)737-24-1147-R1 (ACTIVE- NG)737-SRP-24-0093 (REF)PRR35428-R (PRODUCTION)PRR38454 (PRODUCTION)

ADSBSBSBSRPPRRPRR

Perform BEFORE 16.Jul.20142009-12-06/AD Rev.00 INST. OF IN-FLIGHT. ENT SYSTEM CB, RELAY AND WIRING Not Applicable> 737-24-1145/SB* Rev.00 AD* INST. OF IN-FLIGHT. ENT SYSTEM CB, RELAY AND WIRING Not Applicable by Serial Number





23.Oct.2014Page 284/429

Document-Number Type Rev Compliance A|C Subject Status2009-14-04-1 AD 00 MANDATORY A/C LIGHTS - OUTBOARD LANDING LIGHTS - ISOLATE OR ADD NEW WIRES Closed 21.Feb.2008

LIGHTS - OUTBOARD LANDING LIGHTS - ISOLATE OR ADD NEW WIRESParagraph f) f AD 2009-14-04 pertains directly to this SB.Part 1 of SB results in MMEL restrictions.Part 2 of SB has no restrictions.Performing paragraph g) of AD 2009-14-04, is terminating para f)requirements.2009-14-04 (ACTIVE)2009-14-04-1 (ACTIVE, PARA F)2009-14-04-2 (REF, PARA G)737-33A1140-R0 (ACTIVE)PRODUCTION LINEMRR3335-1627S

AD

AD

AD

SB

PRR

Perform BEFORE 08.Feb.20102009-14-04-1/AD Rev.00 LIGHTS - OUTBOARD LANDING LIGHTS - ISOLATE OR ADD NEW WIRES Closed 21.Feb.2008> 2009-14-04-2/AD Rev.00 ENGINE FUEL SHUTOFF VALVE - WIRE REPL-CONNECTOR REPL, INSP Closed 21.Feb.2008> > 737-28-1241P1/SB* Rev.01 *AD* ENGINE FUEL SHUTOFF VALVE - WIRE BUNDLE REPLACEMENT Closed 21.Feb.2008

This Document SUPERSEDES 737-28-1241P1/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> > 737-28-1241P2/SB* Rev.01 *AD* ENG FUEL SHUTOFF VALVE-INSP. OF GROMMETS AND FAIRLEADS Closed 07.Feb.2008This Document SUPERSEDES 737-28-1241P2/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> > 737-28-1241P3/SB* Rev.01 ENGINE FUEL SHUTOFF VALVE - REPLACEMENT OF ELEC. CONNECTORS Not Applicable





23.Oct.2014Page 285/429

Document-Number Type Rev Compliance A|C Subject StatusThis Document SUPERSEDES 737-28-1241P3/SB Rev.00Reason for this StatusNEW KIT P/N TO BE INSTALLED

> 737-33A1140/SB* Rev.00 *AD* OUTBOARD LANDING LIGHTS - ISOLATE OR ADD NEW WIRES CancelledThis Document has been SUPERSEDED BY 737-33A1140/SB Rev.01Reason for this StatusSB 737-28-1241 PERFORMED, SB COVERS REQ. OF SB 737-33A1140

> 737-33A1140/SB* Rev.01 *AD* OUTBOARD LANDING LIGHTS - ISOLATE OR ADD NEW WIRES CancelledThis Document SUPERSEDES 737-33A1140/SB Rev.00Reason for this StatusSB 737-28-1241 PERFORMED, SB COVERS REQ. OF SB 737-33A1140





23.Oct.2014Page 286/429

Document-Number Type Rev Compliance A|C Subject Status2009-14-04-2 AD 00 MANDATORY A/C ENGINE FUEL SHUTOFF VALVE - WIRE REPL-CONNECTOR REPL, INSP Closed 21.Feb.2008

2009-14-04 (ACTIVE)2009-14-04-01 (REF, PARA F)2009-14-04-02 (ACTIVE, PARA G)737-28-1241-R0 (REF)737-28-1241-R1 (ACTIVE)737-SRP-28-0104 (REF)SBB 737-28-1241P1 (MOD TASK)SBB 737-28-1241P2 (MOD TASK)SBB 737-28-1241P3 (MOD TASK)

ADTATASBSBSRPTATATA

Perform BEFORE 12.Aug.20142009-14-04-2/AD Rev.00 ENGINE FUEL SHUTOFF VALVE - WIRE REPL-CONNECTOR REPL, INSP Closed 21.Feb.2008> 737-28-1241P1/SB* Rev.01 *AD* ENGINE FUEL SHUTOFF VALVE - WIRE BUNDLE REPLACEMENT Closed 21.Feb.2008

This Document SUPERSEDES 737-28-1241P1/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-28-1241P2/SB* Rev.01 *AD* ENG FUEL SHUTOFF VALVE-INSP. OF GROMMETS AND FAIRLEADS Closed 07.Feb.2008This Document SUPERSEDES 737-28-1241P2/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> 737-28-1241P3/SB* Rev.01 ENGINE FUEL SHUTOFF VALVE - REPLACEMENT OF ELEC. CONNECTORS Not ApplicableThis Document SUPERSEDES 737-28-1241P3/SB Rev.00Reason for this StatusNEW KIT P/N TO BE INSTALLED





23.Oct.2014Page 287/429

Document-Number Type Rev Compliance A|C Subject Status2009-16-14 AD NO

TEMANDATORY A/C *AD* INTERCOASTALS - BS360 & 294.5 S-6/17L - INSPECTION Superseded (Cancelled)

2005-20-03 (SUPERSEDED)2009-16-14 (ACTIVE)37-SBB-53A1204 (REP TASK)737-53-1204 IN 01 (REF)737-53-1204-R0 (REF)737-53-1204-R1 (ACTIVE)

ADADTASBSBSB

This Document SUPERSEDES 2005-20-03/AD Rev.00This Document has been SUPERSEDED BY 2012-12-05/AD Rev.00Perform within an unlimited threshold.

2009-16-14/AD Rev.NOTE *AD* INTERCOASTALS - BS360 & 294.5 S-6/17L - INSPECTION CancelledThis Document SUPERSEDES 2005-20-03/AD Rev.00This Document has been SUPERSEDED BY 2012-12-05/AD Rev.00








23.Oct.2014Page 288/429

Document-Number Type Rev Compliance A|C Subject Status2009-20-11 AD 00 MANDATORY A/C *AD* BF GOODRICH TRANSIENT SUPPRESION DEVICE (TST) INSTALL. Taskcard Controlled

This AD is applicable to AC with STC ST00127BO installed.AC that have status "Not Applicable" does not have FQIS via this STC.1999-03-04 XA737-28-1157NAS-2841-005 (INSP TASK)NAS-2841-006 (INSP TASK)NAS-2841-007 (INSP TASK)PRODUCTION PRR35423-RST00127BO (ACTIVE)T2007-0010-0101 (ACTIVE)

ADSBTATATAPRRSTCDOCR

NOTE00000000000000

Perform BEFORE 05.Dec.20092009-20-11/AD Rev.00 *AD* BF GOODRICH TRANSIENT SUPPRESION DEVICE (TST) INSTALL. Taskcard Controlled> ST00127BO/STC Rev.00 *AD* BF GOODRICH TRANSIENT SUPPRESION DEVICE (TST) INSTALL. Taskcard Controlled> > 737-28-1157/SB Rev.00 *AD* BF GOODRICH TRANSIENT SUPPRESION DEVICE (TST) INSTALL. Taskcard Controlled> > > 737-28-1157-01/EO* Rev.01 *AD* BF GOODRICH TRANSIENT SUPPRESION DEVICE (TST) INSTALL. Closed 14.Mar.2003


14.Mar.2003 42144:00/H 19904/CMALEVEO:737-28-0043/SB28-1157

> > > 737-28-1157MPD/EO*Rev.00


Carried out on the following TaskcardsTaskcard: NAS-2841-006 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks05.04.2019 88'534/H 15212:25/H Interval:24000/HPerf Dim1 (D) Perf Dim2 Perf Dim306.07.2011 64534:00/H 37798/CCarried out on the following TaskcardsTaskcard: NAS-2841-007 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks





23.Oct.2014Page 289/429

Document-Number Type Rev Compliance A|C Subject Status10.02.2017 81'168/H 7846:25/H Interval:39000/HCarried out on the following TaskcardsTaskcard: NAS-2841-005 Maint. Progr.: AMP 737-CLExp Dim1 (D) Exp Dim2 Exp Dim3 Togo Remarks04.02.2015 04.Feb.2015104d, 6h Interval:365/DPerf Dim1 (D) Perf Dim2 Perf Dim304.02.2014 71572:00/H 43151/CReason for this StatusAUTO ASSIGNED





23.Oct.2014Page 290/429

Document-Number Type Rev Compliance A|C Subject Status2009-21-01 AD 00 MANDATORY A/C *AD* FUSELAGE AFT SKIN - INSPECTION, MOD AND REPLACEMENT Open

This Mod is applicable to LN# 1001-2565. The following LN# are NotApplicable per PRR35040.2009-21-01 (ACTIVE)37-SBB-53-1168 (REPETITIVE)6-1151-737-PGM-108 (REF)737-53-1168-R3 (ACTIVE)737-SRP-53-0131 (REF)PRODUCTION PRR 35040

ADTABMSBSRPPRR

Perform within an unlimited threshold.2009-21-01/AD Rev.00 *AD* FUSELAGE AFT SKIN - INSPECTION, MOD AND REPLACEMENT Open> 737-53-1168/SB Rev.03 FUSELAGE SKIN BS 727-1016 S-14/25 L/R - INSPECTION, MOD, REPLACEMENT Open> > 737-53-1168/EO* Rev.00 FUSELAGE SKIN BS 727-1016 S-14/25 L/R - INSPECTION *** REPETITIVE MANDATORY

INSPECTION ***Repetitive




> > 737-53-1168-01/EO* Rev.00 FUSELAGE SKIN BS 727-1016 S-14/25 L/R - MOD, REPLACEMENT (NO SKIN CHANGECARRIED OUT)

Term.Action open






23.Oct.2014Page 291/429

Document-Number Type Rev Compliance A|C Subject Status2009-21-10 AD 01 MANDATORY COMP OXYGEN - CREW OXYGEN CYLINDER DISCARD OF Not Applicable by Serial Number

2009-21-10 (SUPERSEEDED)2009-21-10-R1 (ACTIVE)AD 2009-21-10 (MAINT TASK)

ADADTA

This Document SUPERSEDES 2009-21-10/AD Rev.00Affected Rotables (Part No/Serial No/Position) Status801307-00 / 599240 Pos=#1 (KKM) Not Applicable

2009-21-10 AD 00 MANDATORY COMP OXYGEN - CREW OXYGEN CYLINDER DISCARD OF Superseded (Not Applicable bySerial Number)

2009-21-10 (SUPERSEEDED)2009-21-10-R1 (ACTIVE)AD 2009-21-10 (MAINT TASK)

ADADTA

This Document has been SUPERSEDED BY 2009-21-10/AD Rev.01Affected Rotables (Part No/Serial No/Position) Status801307-00 / 599240 Pos=#1 (KKM) Not Applicable

2009-23-10 AD 00 MANDATORY A/C *AD* OUTBOARD FLAP CARRIAGE SPINDLE CORROSION, INSPECTION Superseded (Superseded)This Document SUPERSEDES 2008-15-05/AD Rev.00This Document SUPERSEDES 2008-15-05 XF/AD Rev.00This Document has been SUPERSEDED BY 2011-04-10/AD Rev.00





23.Oct.2014Page 292/429

Document-Number Type Rev Compliance A|C Subject Status2009-26-03 AD 00 MANDATORY A/C *AD* REMOVAL AND REPLACEMENT OF THE STATIC INVERTER MODULE Not Applicable

This document is applicable to:

737CL: All LN#.737NG: LN# 1-1735.The following LN are Not Applicable due toPRR38275-80S.PRR35005-265RS (CL)PRR38275-80S (NG)

PRRPRR

0000

Perform within an unlimited threshold.2009-26-03/AD Rev.00 *AD* REMOVAL AND REPLACEMENT OF THE STATIC INVERTER MODULE Not Applicable> 737-24A1166/SB Rev.04 *AD* ELECTRICAL POWER - STANDBY POWER SYSTEM - REMOVAL AND

REPLACEMENT OF THE STATIC INVERTER MODULENot Applicable

This Document SUPERSEDES 737-24A1166/SB Rev.03> > 737-24A1166-01/EO* Rev.00 *AD* ELECTRICAL POWER - STANDBY POWER SYSTEM - REMOVAL AND

REPLACEMENT OF THE STATIC INVERTER MODULENot Applicable


39B168-1-C / 3427 Pos=E&E (KKM)Not Applicable / Reason: AUTOASSIGNED

> > 737-24A1166-02/EO* Rev.00 *AD* ELECTRICAL POWER - STANDBY POWER SYSTEM - REMOVAL ANDREPLACEMENT OF THE STATIC INVERTER MODULE

Not Applicable / Special Text: Notapplicable due to SB effectivity.

Reason for this StatusNOT APPLIC DUE TO PART NOT INST.





23.Oct.2014Page 293/429

Document-Number Type Rev Compliance A|C Subject Status2010-0062 AD 01 MANDATORY A/C HALON PORTABLE FIRE EXT - INSPECTION OF Not Applicable / Special Text:

Aircraft is Not Applicable due to IFEHalon bottles not installed.

NAS does not have IFE Halon bottles installed.2010-01-03 (REF ONLY)AD 2009-0251-E (REF ONLY)AD 2009-0262 (REF ONLY)AD 2010-0062 (SUPERSEEDED)AD 2010-0062-R1 (ACTIVE)ASB 26-115-C (FFE SB)ASB 26-116-B (FFE SB)

ADADADADADSBSB

This Document SUPERSEDES 2010-0062/AD Rev.00Reason for this StatusAUTO ASSIGNED

2010-0062 AD 00 MANDATORY A/C HALON PORTABLE FIRE EXT - INSPECTION OF Superseded (Not Applicable /Special Text: Aircraft is NotApplicable due to IFE Halon bottlesnot installed.)

NAS does not have IFE Halon bottles installed.2010-01-03 (REF ONLY)AD 2009-0251-E (REF ONLY)AD 2009-0262 (REF ONLY)AD 2010-0062 (SUPERSEEDED)AD 2010-0062-R1 (ACTIVE)ASB 26-115-C (FFE SB)ASB 26-116-B (FFE SB)

ADADADADADSBSB

This Document has been SUPERSEDED BY 2010-0062/AD Rev.01Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 294/429

Document-Number Type Rev Compliance A|C Subject Status2010-01-03 AD 00 MANDATORY A/C HALON PORTABLE FIRE EXT - INSPECTION OF Not Applicable / Special Text:

Aircraft is Not Applicable due to IFEHalon bottles not installed.

Not applicable due to; NAS has not installed any Halon Firesuppression deviced manufactured by FFE.2010-01-03 (ACTIVE)AD 2009-0251-E (REF ONLY)AD 2009-0262 (REF ONLY)AD 2010-01-03ASB 26-115 (FFE SB)

ADADADTASB






23.Oct.2014Page 295/429

Document-Number Type Rev Compliance A|C Subject Status2010-01-09 AD 00 MANDATORY A/C *AD* FUSELAGE SKIN-CRACKS AT CHEM-MILLED STEPS CROWN SKINS Superseded (Repetitive)





23.Oct.2014Page 296/429

Document-Number Type Rev Compliance A|C Subject StatusBOEING SERVICE BULLETIN 737-53A1301-R2.

F. ApprovalThis service bulletin was examined by the Federal AviationAdministration (FAA). The changes specified in this service bulletincomply with the applicable regulations and are FAA approved, as wellas European Aviation Safety Agency (EASA)/Joint Aviation Authorities(JAA) approved for all EASA/JAA approved airplanes listed in theservice bulletin effectivity. This service bulletin and its approvalwere based on the airplane in its original Boeing deliveryconfiguration or as modified by other approved Boeing changes.


In addition, the Manager of the FAA Seattle Aircraft CertificationOffice (ACO) approves the inspections with the correspondingcompliance times specified in Tables 1 through 4, under paragraph1.E., "Compliance," of Service Bulletin 737-53A1301 Revision 2 as anAMOC to the inspections with the corresponding compliance timesspecified in Table 1 under paragraph 1.E., "Compliance," of ServiceBulletin 737-53A1301, dated September 3, 2009, required by paragraph(g) of AD 2010-01-09.

When this service bulletin specifies contacting Boeing for repairinstructions, the repair instructions must be approved by the FAA isaccordance with the AD. All provisions of AD 2010-01-09 that are notspecifically referenced in the above statement remain fullyapplicable and must be complied with.





23.Oct.2014Page 297/429

Document-Number Type Rev Compliance A|C Subject Status1-14658921652010-01-09 (ACTIVE)37-SBB-53A1301 (REPETITIVE)737-53A1301 R1 (ACTIVE)

SRADTASB


2010-01-09/AD Rev.00 *AD* FUSELAGE SKIN-CRACKS AT CHEM-MILLED STEPS CROWN SKINS RepetitiveThis Document has been SUPERSEDED BY 2011-24-12/AD Rev.00

> 737-53A1301/EO* Rev.01 FUSELAGE CROWN SKINS SPEC LOC - EXTERN NDT/UTPA INSP CRACKS ATCHEM-MILLED STEPS.

Cancelled

This Document has been SUPERSEDED BY 737-53A1301/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks11.Mar.2011 63756:00/H 37193/C 148913, N/A Was due at: 37261/C PerfRev.:'01'Reason for this StatusManually deassigned after Document Cancelled/Superseeded

> 737-53A1301/SB Rev.02 FUSELAGE - SKIN - CRACKS AT CHEM-MILLED STEPS IN CROWN SKINS AT SPECIFIEDLOCATIONS - INSPECTION

Repetitive

This Document SUPERSEDES 737-53A1301/EO Rev.01This Document SUPERSEDES 737-53A1301/SB Rev.01

> > 737-53A1301/EO* Rev.02 FUSELAGE CROWN SKINS -NDT AT SPECIFIEC LOCATIONS- EXTERNAL UTPAINSPECTION FOR CRACKS AT CHEM-MILLED STEPS.

Repetitive




> > 737-53A1301-1/EO* Rev.02 FUSELAGE CROWN SKINS - NDT AT SPECIFIEC LOCATIONS - MFEC INSPECTION FORCRACKS AT CHEM-MILLED STEPS.






23.Oct.2014Page 298/429

Document-Number Type Rev Compliance A|C Subject Status2010-04-16 AD 00 MANDATORY COMP REPLACE SICLI HALON FIRE EXTINGUISHERS Not Applicable by Serial Number

This AD applies to Type H1-10 AIR Halon 1211 (BCF) portable fireextinguishers manufactured by SICLI, having part number (P/N)1708337B4. Replace effected SN with serviceable extinguisher.Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 299/429

Document-Number Type Rev Compliance A|C Subject Status2010-05-13SUB1 AD 00 MANDATORY A/C FUSELAGE SKIN - INSPECTION FOR SCRIBE MARKS - ZONE 1 Closed 20.Feb.2008

Service Bulletin 737-53A1262-R3.F. ApprovalThis service bulletin was examined by the Federal AviationAdministration (FAA). The changes specified in this service bulletincomply with the applicable regulations and are FAA approved, as wellas European Aviation Safety Agency (EASA)/Joint Aviation Authorities(JAA) approved for all EASA/ JAA approved airplanes listed in theservice bulletin effectivity. This service bulletin and its approvalwere based on the airplane in its original Boeing deliveryconfiguration or as modified by other approved Boeing changes.


This service bulletin has been reviewed with respect to therequirements of AD 98-11-04 R1, Paragraph (g), and the inspections donot affect a SSI. However, any repair that results from theinspection findings of this service bulletin, should be assessed withrespect to the requirements of AD 98-11-04 R1, paragraph (g), todetermine if it affects or creates a SSI.

This service bulletin has been approved by the FAA. In addition, theManager of the FAA Seattle Aircraft Certification Office approves theinspections defined in this service bulletin as an alternativemethod of compliance to the requirements of paragraph (f), (g), (j),(l), (m), (n) and (q) of AD 2006-07-12. All provisions of AD2006-07-12 that are not specifically referenced in the abovestatement remain fully applicable and must be complied with.





23.Oct.2014Page 300/429

Document-Number Type Rev Compliance A|C Subject Status2006-07-12 (SUPERSEDED)2010-05-13 (ACTIVE)737-53A1262 IN 01 (REF)737-53A1262 IN 02 (REF)737-53A1262-R1 (REF)737-53A1262-R2 (ACTIVE)737-53A1262-RO (REF)AD 2010-05-13SUB1 (ACTIVE)SBB-737-53A1262-1

ADADSBSBSBSBSBADTA

This Document SUPERSEDES 2006-07-12/AD Rev.00Perform BEFORE 32174/C

2010-05-13SUB1/AD Rev.00 FUSELAGE SKIN - INSPECTION FOR SCRIBE MARKS - ZONE 1 Closed 20.Feb.2008This Document SUPERSEDES 2006-07-12/AD Rev.00

> 737-53A1262-1/SB* Rev.03 FUSELAGE SKIN - INSPECTION FOR SCRIBE LINES - ZONE 1 Closed 20.Feb.2008Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks



> > 737-53A1262-1-01/EO*Rev.00

LN-KKB. FUSELAGE SKIN - LAP JOINT S-4L & 4R BS 360-1016. REPEAT EXTERNAL NDTINSPECTION OF SCRIBE LINES. UT PHASED ARRAY.


This Document is terminated with implementation of 737-53A1262-1-02/EO Rev.00> > 737-53A1262-1-02/EO*Rev.00

LN-KKB. FUSELAGE SKIN - LAP JOINT S-4L & 4R BS 360-1016. REPEAT EXTERNAL NDTINSPECTION OF SCRIBE LINES. UT PHASED ARRAY.


This Document terminates 737-53A1262-1-01/EO Rev.00> > 737-53A1262-1-03/EO*Rev.00

LN-KKB. FUSELAGE SKIN - BUTT JOINT BS360 & 907 S-10L-10R. REPEAT EXTERNALNDT INSPECTION OF SCRIBE LINES.


> > 737-53A1262-1-04/EO*Rev.00

LN-KKB. FUSELAGE SKIN - WING TO BODY FAIRINGS - S-14L BS 907-1016 EXTERNALREPAIR AT BS 920 S-19L. REPEAT NDT INSPECTION OF SCRIBE LINES


> > 737-53A1262-1-05/EO*Rev.00

LN-KKB. FUSELAGE SKIN LAP JOINT S4L & 4R BS 360-1016. ONE TIME INTERNAL NDTINSPECTION






23.Oct.2014Page 301/429

Document-Number Type Rev Compliance A|C Subject Status> > 737-53A1262-1-06/EO*Rev.00

LN-KKB. FUSELAGE SKIN LAP JOINT S-4L & 4R SCRIBE LINES REPAIR Not Applicable by Serial Number

2010-05-13SUB2 AD 00 MANDATORY A/C FUSELAGE SKIN - INSPECTION FOR SCRIBE MARKS - ZONE 2 Open2006-07-12 (SUPERSEDED)2010-05-13SUB2 (ACTIVE)737-53A1262 IN 01 (REF)737-53A1262 IN 02 (REF)737-53A1262-R0 (REF)737-53A1262-R1 (REF)737-53A1262-R2 (REF)737-53A1262-R3 (ACTIVE)AD 2010-05-13 (ACTIVE)SBB 737-53A1262-2 (ACTIVE)SBB 737-53A1262-2 (MAIN-TASK)

ADADSBSBSBSBSBSBADSBTA


2010-05-13SUB2/AD Rev.00 FUSELAGE SKIN - INSPECTION FOR SCRIBE MARKS - ZONE 2 OpenThis Document SUPERSEDES 2006-07-12/AD Rev.00

> 737-53A1262-2/SB* Rev.03 FUSELAGE SKIN - INSPECTION FOR SCRIBE MARKS - ZONE 2 OpenDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document






23.Oct.2014Page 302/429

Document-Number Type Rev Compliance A|C Subject Status2010-05-13SUB3 AD 00 MANDATORY A/C *AD* FUSELAGE SKIN - INSPECTION FOR SCRIBE MARKS - ZONE 3 Open

2006-07-12 (SUPERSEDED)2010-05-13 (ACTIVE)2010-05-13SUB3 (ACTIVE)737-53A1262 IN 01 (REF)737-53A1262 IN 02 (REF)737-53A1262-R0 (REF)737-53A1262-R1 (REF)737-53A1262-R2 (REF)737-53A1262-R3 (ACTIVE)SBB 737-53A1262-3 (ACTIVE)SBB 737-53A1262-3 (MAIN-TASK)



2010-05-13SUB3/AD Rev.00 *AD* FUSELAGE SKIN - INSPECTION FOR SCRIBE MARKS - ZONE 3 OpenThis Document SUPERSEDES 2006-07-12/AD Rev.00

> 737-53A1262-3/SB* Rev.02 *AD* FUSELAGE SKIN - INSPECTION FOR SCRIBE MARKS - ZONE 3 OpenDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document






23.Oct.2014Page 303/429


2006-07-12 (SUPERSEDED)2010-05-13 (ACTIVE2010-05-13SUB4 (ACTIVE)737-53A1262 IN 01 (REF)737-53A1262 IN 02 (REF)737-53A1262-R0 (REF)737-53A1262-R1 (REF)737-53A1262-R2 (REF)737-53A1262-R3 (ACTIVE)AD 2006-07-12SUB4 (REF-TASK)SBB 737-53A1262-4 (ACTIVE)SBB 737-53A1262-4 (MAIN-TASK)

ADADADSBSBSBSBSBSBTASBSB


2010-05-13SUB4/AD Rev.02 *AD* FUSELAGE SKIN - INSPECTION FOR SCRIBE MARKS - ZONE 4 OpenThis Document SUPERSEDES 2006-07-12/AD Rev.00

> 737-53A1262-4/SB* Rev.03 *AD* FUSELAGE SKIN - INSPECTION FOR SCRIBE MARKS - ZONE 4 OpenDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document






23.Oct.2014Page 304/429


2006-07-12 (SUPERSEDED)2010-05-13 (ACTIVE)2010-05-13SUB5 (ACTIVE)737-53A1262 IN 01 (REF)737-53A1262 IN 02 (REF)737-53A1262-R0 (REF)737-53A1262-R1 (REF)737-53A1262-R2 (REF)737-53A1262-R3AD 2010-05-13SUB5 (SEC-TASK)SBB 737-53A1262-5 (INSP-TASK)

ADADADSBSBSBSBSBSBTATA

Perform BEFORE 65000/C2010-05-13SUB5/AD Rev.00 *AD* FUSELAGE SKIN - INSPECTION FOR SCRIBE MARKS - ZONE 5 Open> 737-53A1262-5/SB* Rev.03 *AD* FUSELAGE SKIN - INSPECTION FOR SCRIBE MARKS - ZONE 5 Open


2010-07-02 AD 00 MANDATORY COMP *AD* HONEYWELL PRIMUS II RNZ-850/-851 INTEGRATED NAVIGATION Not Applicable by Serial Number2003-04-06 (ACTIVE) ADThis Document SUPERSEDES 2006-22-05/AD Rev.00Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 305/429

Document-Number Type Rev Compliance A|C Subject Status2010-11-05 AD 00 MANDATORY COMP OXYGEN - CREW AND PASSENGER O2 SYS. - INSP. OF CYLINDER Not Applicable by Serial Number

176000-35-01 (BAE SB)6084-34-35-01-R1 (AVOX SB)737-35A1124 R00 (ACTIVE)737-35A1126 R00 (ACTIVE)SBB 737-35A1124 (INSP TASK)SBB 737-35A1126 (INSP TASK)

SBSBSBSBTATA

Affected Rotables (Part No/Serial No/Position) Status801307-00 / 599240 Pos=#1 (KKM) Not Applicable

2010-12-03 AD 00 MANDATORY COMP 25 DEGR. MIDSPAN SHROUD FAN BLADES Not ApplicableRepetitive Inspection of the Platform Underside of the 25 DegreesMidspan Shroud Fan Blades.Applicable to CFM56-3B1 and -3B2 only.2009-00362010-12-033-72-10673-72-1067NAS-7221-001

ADADSBSBTA

000100

Perform BEFORE 15.Aug.20072010-12-03/AD Rev.00 25 DEGR. MIDSPAN SHROUD FAN BLADES Not Applicable> 3-72-1067/SB* Rev.01 FAN BLADES - 25 DEGREE MID-SPAN SHROUDS INSP. Not Applicable


CFM56-3B2 / 724473 Pos=LH (KKM)Not Applicable / Reason: NA - 37DEGREES MIDSPAN SHROUD FANBLADES INST.

CFM56-3B2 / 725495 Pos=RH (KKM)Not Applicable / Reason: NA - 37DEGREES MIDSPAN SHROUD FANBLADES INST.





23.Oct.2014Page 306/429

Document-Number Type Rev Compliance A|C Subject Status2010-14-06 AD 00 MANDATORY A/C *AD* OXYGEN MASK ASSEMBLY INSPECTION AND MODIFICATION Closed 28.Oct.2012 W/O:273634

2008-06-24 (SUPERSEDED)2010-14-06 (ACTIVE)AD 2010-14-06 (SECONDARYTASK)B/E AEROSPACE 174080-35-01SBB 737-35-1099 (MAINT TASK)SBB 737-35-1099-R1 (ACTIVE)

ADADTASBTASB

This Document SUPERSEDES 2008-06-24/AD Rev.00Perform BEFORE 23.Apr.2013

2010-14-06/AD Rev.00 *AD* OXYGEN MASK ASSEMBLY INSPECTION AND MODIFICATION Closed 28.Oct.2012 W/O:273634This Document SUPERSEDES 2008-06-24/AD Rev.00

> 737-35-1099/SB* Rev.01 OXYGEN MASK ASSEMBLY INSPECTION AND MODIFICATION Closed 28.Oct.2012 W/O:273634This Document SUPERSEDES 737-35-1099/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks28.Oct.2012 68139:00/H 40570/C 273634, N/A Was due at: 22.Apr.2013 PerfRev.:'01'





23.Oct.2014Page 307/429

Document-Number Type Rev Compliance A|C Subject Status2010-15-08->2002-22-05/AD

AD 00 MANDATORY A/C *AD* WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSP FOR CRACKS. & FLAP GAPCHECK

Superseded (Open)

This AD mandates the NDT inspections, OH and life limit of the FlapCarriag

Compliance:

AD § (g) through (n) is complied with through SB 737-57A1277 andspecifically:EO 737-57A1277-01: NDT inspectionEO 737-57A1277-02: GAP check

AD § (o)through (s) (§ (p) is NA to NAS, NAS does not operate737-100/-200) is complied with through SB 737-57A1218 andspecifically:EO 737-57A1218-01: Overhaul requirementEO 737-57A1218-02: Carriage spindle life limit for known historyEO 737-57A1218-03: Carriage spindle life limit for unknown historyThis Document SUPERSEDES 2003-24-08/AD Rev.00This Document has been SUPERSEDED BY 2014-05-12/AD Rev.00Perform within an unlimited threshold.

2010-15-08/AD Rev.00 *AD* WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSP FOR CRACKS. & FLAP GAPCHECK

Open


> 737-57A1218/SB Rev.06 WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSPECTION/OVERHAUL & LIFELIMITING

Open

This Document SUPERSEDES 737-57A1218/SB Rev.05> > 737-57A1218-01/EO* Rev.00 WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSPECTION/OVERHAUL Open






23.Oct.2014Page 308/429


65-46481-116 / 1783 Pos=#8 (KKM)Repetitive / Next Due:11.Jan.2022 38297/C/ Last Performed:13.Jan.2014 0/CRefDocument:FAA 8130-3 026010 Rev.00

65-46481-145 / B5121 Pos=#1 (KKM) Open / Next Due:14.May.2021 22077/C

65-46481-119 / B3554 Pos=#2 (KKM)

Repetitive / Next Due:05.Oct.2020 22073/C/ Last Performed:07.Oct.2012 0/CRefDocument:FAA 8130-3 024128-2Rev.00

65-46481-106 / 4914WG Pos=#7 (KKM)

Repetitive / Next Due:05.Feb.2019 37305/C/ Last Performed:07.Feb.2011 35283:00/H25305/C RefDocument:EASA F1001282424 Rev.00

> > 737-57A1218-02/EO* Rev.01 WINGS- TE OUTB FLAP CARRIAGE SPINDELS LIFE LIMIT FOR FLAP CARRIAGES WITHDOCUMENTED HISTORY

Open

This Document SUPERSEDES 737-57A1218-02/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status65-46481-119 / B3554 Pos=#2 (KKM) Open / Next Due: 40000/C65-46481-106 / 4914WG Pos=#7 (KKM) Open / Next Due: 40000/C65-46481-145 / B5121 Pos=#1 (KKM) Open / Next Due: 40000/C65-46481-116 / 1783 Pos=#8 (KKM) Open / Next Due: 40000/C

> > 737-57A1218-03/EO* Rev.00 WINGS- TE OUTB FLAP CARRIAGE SPINDELS LIFE LIMIT FOR FLAP CARRIAGES WITHUN-DOCUMENTED HISTORY

Not Applicable / Special Text: Thiscomp.is Not Applicable due toKNOWN history,ref EO737-57A1218-02


65-46481-116 / 1783 Pos=#8 (KKM)

Not Applicable / Special Text: This comp.isNot Applicable due to KNOWN history,refEO 737-57A1218-02 / Reason: THISCOMP.IS NOT APPLICABLE DUE TOKNOWN HISTORY,REF EO737-57A1218-02





23.Oct.2014Page 309/429


65-46481-145 / B5121 Pos=#1 (KKM)

Not Applicable / Special Text: This comp.isNot Applicable due to KNOWN history,refEO 737-57A1218-02 / Reason: EO737-57A1218-02 COVER CARRIAGESWITH KNOWN HISTORY

65-46481-119 / B3554 Pos=#2 (KKM)

Not Applicable / Special Text: This comp.isNot Applicable due to KNOWN history,refEO 737-57A1218-02 / Reason: NA DUETO KNOWN HISTORY, REFER TO EO737-57A1218-02

65-46481-106 / 4914WG Pos=#7 (KKM)

Not Applicable / Special Text: This comp.isNot Applicable due to KNOWN history,refEO 737-57A1218-02 / Reason: NOTAPPLICABLE SINCE HISTORY ISKNOWN, REF EO 737-57A1218-02

> 737-57A1277/SB Rev.01 WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSP FOR CRACKS. & FLAP GAP CHECK SupersededThis Document SUPERSEDES 737-57A1277/SB Rev.00This Document has been SUPERSEDED BY 737-57A1277/SB Rev.03

> > 737-57A1277-01/EO* Rev.00 NDT OF TE OUTB FLAP CARRIAGE SPINDELS INSP FOR CRACKS. SupersededThis Document has been SUPERSEDED BY 737-57A1277-01/EO Rev.01Affected Rotables (Part No/Serial No/Position) Status

65-46481-145 / B5121 Pos=#1 (KKM)Superseded / Reason: Manually deassignedafter Document Cancelled or Superseded

65-46481-119 / B3554 Pos=#2 (KKM)Superseded / Reason: Manually deassignedafter Document Cancelled or Superseded

65-46481-116 / 1783 Pos=#8 (KKM)Superseded / Reason: Manually deassignedafter Document Cancelled or Superseded

65-46481-106 / 4914WG Pos=#7 (KKM)Superseded / Reason: Manually deassignedafter Document Cancelled or Superseded

> > 737-57A1277-02/EO* Rev.00 WINGS- TE OUTB FLAP GAP CHECK & CARRIAGE SPINDELS INSP FOR CRACKS. SupersededThis Document has been SUPERSEDED BY 737-57A1277-02/EO Rev.01





23.Oct.2014Page 310/429

Document-Number Type Rev Compliance A|C Subject StatusReason for this StatusManually deassigned after Document Cancelled or Superseded





23.Oct.2014Page 311/429

Document-Number Type Rev Compliance A|C Subject Status2010-16-06 AD 00 MANDATORY A/C CREW OXYGEN SYSTEM LOW PRESSURE FLEX HOSE REPL. Closed 10.May.2012

Applicability:CL:This document is applicable to All 737CL.

NG:This document is applicable to LN# 1-348

AD compliance:AD § (g); compliance is covered by performing SB 737-35A1053 and737-35A1058.

AD § (h); compliance is covered by entering PN into AMOS SuspiciousParts module.

AD § (i) is used by NAS as some aircraft have been modified per Rev00 of SB 737-35A1053.737-35A1053737-35A1058PRODUCTION LINE PRR38275-1

SBSBPRR

010100

Perform BEFORE 10.Sep.20132010-16-06/AD Rev.00 CREW OXYGEN SYSTEM LOW PRESSURE FLEX HOSE REPL. Closed 10.May.2012> 737-35A1053/SB Rev.02 OXYGEN - CREW OXYGEN - CREW OXYGEN SYSTEM LOW PRESSURE FLEX HOSE

REPLACEMENTNot Applicable / Special Text: ThisAircraft is not applicable due to PRR38275-1

This Document SUPERSEDES 737-35A1053/SB Rev.01> > 737-35A1053-01/EO* Rev.00 OXYGEN - CREW OXYGEN - CREW OXYGEN SYSTEM LOW PRESSURE FLEX HOSE

REPLACEMENTNot Applicable / Special Text: ThisAircraft is not applicable due to PRR38275-1

Reason for this StatusNA DUE TO HAVING PERFORMED REV 00 OR 01 OF SB, GROUP 1 CONFIG 2.





23.Oct.2014Page 312/429

Document-Number Type Rev Compliance A|C Subject Status> 737-35A1053/SB* Rev.00 CREW OXYGEN SYSTEM LOW PRESSURE FLEX HOSE REPL. Cancelled

This Document has been SUPERSEDED BY 737-35A1053/SB Rev.01Reason for this StatusManually deassigned after Document Cancelled or Superseded

> 737-35A1053/SB* Rev.01 CREW OXYGEN SYSTEM LOW PRESSURE FLEX HOSE REPL. Closed 18.Jan.2001This Document SUPERSEDES 737-35A1053/SB Rev.00This Document has been SUPERSEDED BY 737-35A1053/SB Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

18.Jan.2001PerfRev.:'NOTE' / Reason: DELIVERYDOC WO:






23.Oct.2014Page 313/429

Document-Number Type Rev Compliance A|C Subject Status2010-25-06 AD 00 MANDATORY A/C BODY FRAME AND OVERWING STUB BEAM INSPECTION - BS 616 TO 639 Repetitive

737-53A1254737-53A1254NAS-5311-001 (MSN 24256)NAS-5311-002 (MSN 28658)NAS-5311-003 (MSN 28654)

SBSBMPDMPDMPD

0102000000

Perform BEFORE 15000/C for the first timeThereafter perform in an interval of 4500/C

2010-25-06/AD Rev.00 BODY FRAME AND OVERWING STUB BEAM INSPECTION - BS 616 TO 639 Repetitive> 737-53A1254/SB Rev.01 FUSELAGE - BODY FRAME AND OVERWING STUB BEAM INSPECTION AND REPAIR

BODY STATIONS 597 TO 639Cancelled


> > 737-53A1254/EO* Rev.01 BODY FRAME AND OVERWING STUB BEAM INSPECTION - BS 597 TO 639 CancelledThis Document SUPERSEDES 737-53A1254/EO Rev.00This Document has been SUPERSEDED BY 737-53A1254-01/EO Rev.02Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks31.Oct.2012 68139:00/H 40570/C 273628, N/A Was due at: 42298/C PerfRev.:'01'Reason for this StatusManually deassigned after Document Cancelled or Superseded

> 737-53A1254/SB Rev.02 FUSELAGE - BODY FRAME AND OVERWING STUB BEAM INSPECTION AND REPAIRBODY STATIONS 597 TO 639

Repetitive

This Document SUPERSEDES 737-53-1182/SB Rev.02This Document SUPERSEDES 737-53A1254/SB Rev.01

> > 737-53A1254-01/EO* Rev.02 BODY FRAME AND OVERWING STUB BEAM INSPECTION - BS 597 TO 639 RepetitiveThis Document SUPERSEDES 737-53A1254/EO Rev.01Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document







23.Oct.2014Page 314/429


2011-0043 AD 00 MANDATORY COMP NAVIGATION SYSTEMS - MODE-S TRANSPONDER CONTROL PANELS - MODIFICATION Not ApplicableNot aplicable to NAS 737-800.Only aplicable to NAS 737-300 LN-KKA (G7490-12), which has beenphased out.G7490 ( )-34-01G7492 ( )-34-01G7493 ( )-34-01

SBSBSB

000100

Perform BEFORE 31.Jan.20142011-0043/AD Rev.00 NAVIGATION SYSTEMS - MODE-S TRANSPONDER CONTROL PANELS - MODIFICATION Not Applicable> G7490( )-34-01/SB* Rev.00 FLIGHT ID/ATC/TCAS CONTROL PANEL - DIGITAL BOARD ASSEMBLY PC2 AND PC4

REPLACEMENTNot Applicable






23.Oct.2014Page 315/429

Document-Number Type Rev Compliance A|C Subject Status2011-0090 AD 01 MANDATORY COMP IDENTIFICATION / REPLACEMENT OXYGEN MASK REGULATOR INFLATABLE

HARNESSOpen

EASA AD requires the inspection of crew oxygen masks perIntertechnique SB MXH-35-240 Revision 2 dated 10 May 2011.Intertechnique SB MXH-35-241 dated 06 April 2011.(or later revision).NAS performs a partial fleet inspection thus complying with RequiredAction item 1 and 2. On newly deliverd Aircraft (Jan 11 and on) arecord review has been performed to check for repalced harness ormask. This is also in compliance with Item 2.Item 3 is covered by Reciving information.Item 4 is Not Applicable, only applicable to Bombardier Aircraft.737-SL-35-022SB MXH-35-240

SLSB

A03

This Document SUPERSEDES 2011-0090/AD Rev.00Affected Rotables (Part No/Serial No/Position) Status

MC10-25-104 / 32839 Pos=#1 (KKM)Closed / Reason: SB MXH-35-240 REV.:07/ Last Performed:25.Nov.2011RefDocument:EASAS F1 WO: 14259303

MC10-25-104 / 33047 Pos=FWD (KKM)Closed / Reason: REF SB MXH-35-240REV.:07 / Last Performed:19.Oct.2012RefDocument:EASA F1 WO: 14646590

MC10-25-124 / 49059 Pos=#2 (KKM)

Closed / Reason: REF SBMXH-35-240REV.:07 / LastPerformed:15.Oct.2012 72703:00/H17053/C RefDocument:EASA F1 WO:14669688

2011-0090/AD* Rev.01 IDENTIFICATION / REPLACEMENT OXYGEN MASK REGULATOR INFLATABLEHARNESS

Open

This Document SUPERSEDES 2011-0090/AD Rev.00Affected Rotables (Part No/Serial No/Position) Status





23.Oct.2014Page 316/429


MC10-25-104 / 32839 Pos=#1 (KKM)Closed / Reason: SB MXH-35-240 REV.:07/ Last Performed:25.Nov.2011RefDocument:EASAS F1 WO: 14259303

MC10-25-104 / 33047 Pos=FWD (KKM)Closed / Reason: REF SB MXH-35-240REV.:07 / Last Performed:19.Oct.2012RefDocument:EASA F1 WO: 14646590

MC10-25-124 / 49059 Pos=#2 (KKM)

Closed / Reason: REF SBMXH-35-240REV.:07 / LastPerformed:15.Oct.2012 72703:00/H17053/C RefDocument:EASA F1 WO:14669688

> MXH-35-240/SB* Rev.07 IDENTIFICATION / REPLACEMENT OXYGEN MASK REGULATOR INFLATABLEHARNESS

Open (Next Shop Visit)

Affected Rotables (Part No/Serial No/Position) StatusMC10-25-104 / 32839 Pos=#1 (KKM) Open / NO LIMITMC10-25-124 / 49059 Pos=#2 (KKM) Open / NO LIMITMC10-25-104 / 33047 Pos=FWD (KKM) Open / NO LIMIT





23.Oct.2014Page 317/429

Document-Number Type Rev Compliance A|C Subject Status2011-0090 AD 00 MANDATORY A/C IDENTIFICATION / REPLACEMENT OXYGEN MASK REGULATOR INFLATABLE

HARNESSSuperseded (Closed 05.Nov.2012W/O:273635)

EASA AD requires the inspection of crew oxygen masks perIntertechnique SB MXH-35-240 Revision 2 dated 10 May 2011.Intertechnique SB MXH-35-241 dated 06 April 2011.(or later revision).NAS performs a partial fleet inspection thus complying with RequiredAction item 1 and 2. On newly deliverd Aircraft (Jan 11 and on) arecord review has been performed to check for repalced harness ormask. This is also in compliance with Item 2.Item 3 is covered by Reciving information.Item 4 is Not Applicable, only applicable to Bombardier Aircraft.737-SL-35-022SB MXH-35-240

SLSB

A02

This Document has been SUPERSEDED BY 2011-0090/AD Rev.01Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks05.Nov.2012 68139:00/H 40570/C 273635, N/A Was due at: 31.May.2013 PerfRev.:'00'

2011-0094 AD 00 MANDATORY COMP EQUIPMENT AND FURNISHING - LIFE JACKET VACUUM BAG - MODIFICATION(VENDOR: AERAZUR)



2011-0098 AD 00 MANDATORY A/C TEST/REPLACEMENT OF KOITO INDUSTRIES PASSANGER SEATS Not Applicable / Special Text: Thisaircraft is Not Applicable due toKoito Seats Not installed.

NSB does not have any seats installed manufactured by KoitoIndustries. Please refer to LOPA.Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 318/429

Document-Number Type Rev Compliance A|C Subject Status2011-01-09 AD 00 MANDATORY A/C OXYGEN - INSPECTION OF B/E AEROSPACE PBE Not Applicable / Special Text: This

Aircraft is Not Applicable, DraegerSmoke hoods installed.

Compliance:This AD is not applicable to NAS fleet.

Per AD § (g) a review of records has been performed. NAS onlyoperates with Draeger and Scott PBE.

AD § (h) is covered by entering data into AMOS suspicious partsmodule.Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 319/429

Document-Number Type Rev Compliance A|C Subject Status2011-01-12 AD 00 MANDATORY A/C NACELLE STRUT - MIDSPAR FUSE PIN - INSPECTION, REPAIR AND REPLACEMENT Open

This AD is accomplished by two EO.EO 737-54A1044-01 covers the replacement per AD§ (h).EO 737-54A1044 covers the repetitive inspection per AD §(g).This Document SUPERSEDES 2008-21-03/AD Rev.00Perform BEFORE 09.Feb.2021

2011-01-12/AD Rev.00 NACELLE STRUT - MIDSPAR FUSE PIN - INSPECTION, REPAIR AND REPLACEMENT OpenThis Document SUPERSEDES 2008-21-03/AD Rev.00

> 737-54A1044/SB Rev.02 *AD* NACELLE STRUT - MIDSPAR FUSE PIN - INSPECT/REPAIR/MOD Open> > 737-54A1044/EO* Rev.02 *AD* NACELLE STRUT - MIDSPAR FUSE PIN - INSPECTION & REPAIR *** REPETITIVE

MANDATORY INSPECTION ***Repetitive


16.Feb.2019Perform initially within (effective fromManufacturer Date 13.Mar.1990) (F)7211/D / Interval(F):1825/D

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks17.Feb.2014 71572:00/H 43151/C 436906, N/A Was due at: 17.Mar.2014 PerfRev.:'02'

> > 737-54A1044-01/EO* Rev.02 *AD* NACELLE STRUT - MIDSPAR FUSE PIN - REPALCEMENT OF OpenDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

07.Feb.2020Perform initially within (effective from09.Feb.2010) (F) 3650/D

2011-0223 AD 00 MANDATORY A/C MAIN DECK CARGO DOOR, REPLACEMENT OR MODIFICATION Not Applicable by Serial NumberThis AD is Not Applicable to NAS, NAS does not install main deckcargo door. NAS has not embodied FAA STC SA2969SO or EASA STCEASA.IM.A.S.02424.EASA.IM.A.S.02424SA2969SO

STCSTC

0000





23.Oct.2014Page 320/429

Document-Number Type Rev Compliance A|C Subject Status2011-03-14 AD 00 MANDATORY A/C INSTALLATION OF WARNING INDICATOR LIGHTS Closed 05.Mar.2014

This document is Applicable to LN# 1-3132.

Compliance:Per AD § (c)(1) only SB 737-31A1325 is applicable to NAS.

AD § (g) is complied with by incorperating SB 737-31A1325.

AD § (h) is Not Applicable to NAS, no B737-400 in fleet.

AD § (i) is performed via SB 737-31A1325.

AD § (j) is performed via SB 737-31A1325.Perform BEFORE 14.Mar.2014

2011-03-14/AD Rev.00 INSTALLATION OF WARNING INDICATOR LIGHTS Closed 05.Mar.2014> 737-31A1325/SB* Rev.02 INDICATING / RECORDING SYSTEMS - AURAL WARNING SYSTEM - INST. OF THE

CABIN ALTITUDE WARNING SYSTEM AND TAKEOFF CONFIG.WARNING SYSTEMLIGHTS

See prev. Docstatus

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks05.Mar.2014 71572:00/H 43151/C N/A Was due at: 13.Mar.2014 PerfRev.:'01'

> 737-31A1325/SB* Rev.01 INDICATING / RECORDING SYSTEMS - AURAL WARNING SYSTEM - INST. OF THECABIN ALTITUDE WARNING SYSTEM AND TAKEOFF CONFIG.WARNING SYSTEMLIGHTS

Closed 05.Mar.2014 W/O:436905

This Document SUPERSEDES 737-31A1325/SB Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks05.Mar.2014 71572:00/H 43151/C 436905, N/A Was due at: 13.Mar.2014 PerfRev.:'01'

> 737-31A1325/SB* Rev.00 IND./RECORDING SYSTEMS - AURAL WARNING SYSTEM - INSTALLATION OF THECABIN ALT. WARNING SYS. AND TAKEOFF CONFIGURATION WARNING SYS. LIGHTS

Cancelled






23.Oct.2014Page 321/429


2011-04-09 AD 00 MANDATORY A/C OXYGEN - DEACTIVATION OF LAVATORY OXYGEN GENERATORS Superseded (Not Applicable)This AD is applicable only to-AC operating under 14 CFR FAA Part 121-US reg- AC operating under FAA Part 129

Ref EASA letter stating that this AD is not applicable for USmanufactured aircraft operating in Europe (under EASA juristiction).

During re-delivery some aircraft will be transferred to FAA Part121/129 opweration. The AD will be incorporated at that time.EASA E-MAILEASA LETTER

DOCRDOCR

0000

This Document has been SUPERSEDED BY 2012-11-09/AD Rev.00Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 322/429

Document-Number Type Rev Compliance A|C Subject Status2011-04-10 AD 00 MANDATORY A/C WINGS - TE FLAP - INSPECTION OF CARRIAGE ASSY WITH HVOF COATING Closed 05.Jun.2008

This AD introduces a terminating action per §j of the AD.This Document SUPERSEDES 2009-23-10/AD Rev.00Perform within an unlimited threshold.

2011-04-10/AD Rev.00 WINGS - TE FLAP - INSPECTION OF CARRIAGE ASSY WITH HVOF COATING Closed 05.Jun.2008This Document SUPERSEDES 2009-23-10/AD Rev.00

> 737-57A1304/SB Rev.01 OUTBOARD FLAP CARRIAGE SPINDLE CORROSION, INSPECTION Closed 05.Jun.2008> > 737-57A1304-01/EO* Rev.00 OUTBOARD FLAP CARRIAGE SPINDLE CORROSION, INSPECTION Closed 05.Jun.2008


05.Jun.2008 47535:00/H 31034/CACCOMPLISHED ONWO:151472

PerfRev.:'00'

> > 737-57A1304-02/EO* Rev.00 OUTBOARD FLAP CARRIAGE SPINDLE CORROSION, INSPECTION Not Applicable / Special Text: ThisCarriage is Not Applicable by PN/SN.


65C27409-27 / B3554 Pos=#2 (KKM)Not Applicable / Special Text: This Carriageis Not Applicable by PN/SN.

65C27409-23 / 4914WG Pos=#7 (KKM)Not Applicable / Special Text: This Carriageis Not Applicable by PN/SN. / Reason:AUTO ASSIGNED

65C27409-25 / 1783 Pos=#8 (KKM)Not Applicable / Special Text: This Carriageis Not Applicable by PN/SN. / Reason:AUTO ASSIGNED

65C27409-33 / B5121 Pos=#1 (KKM)Not Applicable / Special Text: This Carriageis Not Applicable by PN/SN. / Reason:AUTO ASSIGNED

> > 737-57A1304-03/EO* Rev.00 OUTBOARD FLAP CARRIAGE SPINDLE CORROSION, INSPECTION Not Applicable / Special Text: ThisCarriage is Not Applicable by PN/SN.


65C27409-27 / B3554 Pos=#2 (KKM)Not Applicable / Special Text: This Carriageis Not Applicable by PN/SN.





23.Oct.2014Page 323/429


65C27409-25 / 1783 Pos=#8 (KKM)Not Applicable / Special Text: This Carriageis Not Applicable by PN/SN. / Reason:AUTO ASSIGNED

65C27409-23 / 4914WG Pos=#7 (KKM)Not Applicable / Special Text: This Carriageis Not Applicable by PN/SN. / Reason:AUTO ASSIGNED

65C27409-33 / B5121 Pos=#1 (KKM)Not Applicable / Special Text: This Carriageis Not Applicable by PN/SN. / Reason:AUTO ASSIGNED





23.Oct.2014Page 324/429

Document-Number Type Rev Compliance A|C Subject Status2011-08-51 AD 00 MANDATORY A/C *AD* - NDT OF CROWN SKIN LAP JOINT - INSPECTION FOR LOWER ROW CRACKING

AT STRINGER S-4L/R, BETWEEN BS 360 AND BS 908.Not Applicable

NOTE:AD to follow compliance times given in SB 737-53A1319.

Ref SB 737-53A1319 R1:

F. ApprovalThis service bulletin was examined by the Federal AviationAdministration (FAA). The changes specified in this service bulletincomply with the applicable regulations and are FAA approved, as wellas European Aviation Safety Agency (EASA)/Joint Aviation Authorities(JAA) approved for all EASA/JAA approved airplanes listed in theservice bulletin effectivity. This service bulletin and its approvalwere based on the airplane in its original Boeing deliveryconfiguration or as modified by other approved Boeing changes.


In addition, the Manager of the FAA Seattle Aircraft CertificationOffice approves accomplishment of the inspection methods and crackconfirmation in accordance with Boeing Alert Service Bulletin737-53A1319, Revision 1, as an AMOC to accomplishment of theinspection methods and crack confirmation required by paragraphs (g)and (i) of AD 2011-08-51. All provisions of AD 2011-08-51 that arenot specifically referenced in this paragraph remain fully applicableand must be complied with accordingly.





23.Oct.2014Page 325/429

Document-Number Type Rev Compliance A|C Subject Status2011-08-51/AD Rev.00 *AD* - NDT OF CROWN SKIN LAP JOINT - INSPECTION FOR LOWER ROW CRACKING

AT STRINGER S-4L/R, BETWEEN BS 360 AND BS 908.Not Applicable

> 737-53A1319-01/EO* Rev.02 FUSE SKIN - NDT OF CROWN SKIN LAP JOINT - EXTERNAL EDDY CURRENT INSPLOWER ROW CRACKING AT STRINGER S-4L/R, BETWEEN BS 360 AND BS 908


This Document SUPERSEDES 737-53A1319-01/EO Rev.01> 737-53A1319-02/EO* Rev.00 FUSE SKIN - NDT - ONE TIME INTERNAL DETAILED AND EDDY CURRENT INSP FOR

CRACKING AT STRINGER S-4L/R, BETWEEN BS 360 AND BS 908Not Applicable by Serial Number

> 737-53A1319-03/EO* Rev.00 FUSE SKIN - ONE TIME INTERNAL GENERAL VISUAL INSP FOR CRACKING LWR SKINPANEL S-4L/R, BETWEEN BS 908 AND BS 1016


> 737-53A1319/SB Rev.00 FUSELAGE SKIN - NDT OF CROWN SKIN LAP JOINT - INSPECTION FOR LOWER ROWCRACKING AT STRINGER S-4L/R, BETWEEN BS 360 AND BS 908

Not Applicable

This Document has been SUPERSEDED BY 737-53A1319/SB Rev.01> > 737-53A1319-01/EO* Rev.00 FUSELAGE SKIN - NDT OF CROWN SKIN LAP JOINT - INSPECTION FOR LOWER ROW

CRACKING AT STRINGER S-4L/R, BETWEEN BS 360 AND BS 908Not Applicable by Serial Number

This Document has been SUPERSEDED BY 737-53A1319-01/EO Rev.01> 737-53A1319/SB Rev.01 FUSELAGE - SKIN - CROWN SKIN LAP JOINT - INSPECTION FOR LOWER ROW

CRACKING AT STRINGER S-4, BETWEEN BS 360 AND BS 908Not Applicable


> > 737-53A1319-01/EO* Rev.01 FUSELAGE SKIN - NDT OF CROWN SKIN LAP JOINT - INSPECTION FOR LOWER ROWCRACKING AT STRINGER S-4L/R, BETWEEN BS 360 AND BS 908


This Document SUPERSEDES 737-53A1319-01/EO Rev.00This Document has been SUPERSEDED BY 737-53A1319-01/EO Rev.02





23.Oct.2014Page 326/429

Document-Number Type Rev Compliance A|C Subject Status2011-12-01 AD 00 MANDATORY A/C TEST/REPLACEMENT OF KOITO INDUSTRIES PASSANGER SEATS Not Applicable / Special Text: This

aircraft is Not Applicable due toKoito Seats Not installed.

NSB does not have any seats installed manufactured by KoitoIndustries. Please refer to LOPA.NM-11-46 DOCR 00Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 327/429

Document-Number Type Rev Compliance A|C Subject Status2011-12-09 AD 00 MANDATORY A/C FUEL PUMP CONTROL GROUND FAULT INTERRUPT RELAY GFI, INST. OF Open

NSB has not performed the initial release of SB 737-28A1212. NSBoperates Group 2,4 and 13 aircraft.NSB will comply with AD by fulfilling the requirements of § (G),(1).(AD § (g).(2) is only for Group 1 and 8 aircraft.) and AD § (j) and(k). NSB will activate NAS task NAS-2841-002 upon completion of SB,thus complying with AD § (l).(2).2009-NM-228-AD65-49808-24-01 (ACTIVE)737-28A1212 IN-01NAS-2841-002 (AWL TASK)PRR35440-10RS

NPRMSBSBTAPRR

00

000000

Perform WITHIN 1800/D (effective from 15.Jul.2011)2011-12-09/AD Rev.00 FUEL PUMP CONTROL GROUND FAULT INTERRUPT RELAY GFI, INST. OF Open> 737-28A1212/SB Rev.02 FUEL - ENGINE FUEL FEED SYSTEM - FUEL PUMP CONTROL GROUND FAULT

INTERRUPTER (GFI) RELAY INSTALLATIONOpen

This Document SUPERSEDES 737-28A1212/SB Rev.01> > 737-28A1212-01/EO* Rev.00 FUEL PUMP CONTROL GROUND FAULT INTERRUPT RELAY GFI, INST. OF Open


18.Jun.2016Perform initially within (effective from15.Jul.2011) (F) 1800/D

> > 737-28A1212-02/EO* Rev.00 FUEL PUMP CONTROL GROUND FAULT INTERRUPT RELAY GFI, INST. OF Not ApplicableReason for this StatusTHIS AC IS NA DUE TO BEEING IN GROUP 2, REF EO 737-28A1212-01

> > 737-28A1212MPD/EO*Rev.00

737-28A1212MPD CONTROLLED BY MPD TASKS Taskcard Controlled






23.Oct.2014Page 328/429

Document-Number Type Rev Compliance A|C Subject Status2011-14-08 AD 00 MANDATORY A/C OXYGEN - GENERAL VISUAL INSPECTION OF PSU OXYGEN MASK ASSEMBLY Not Applicable

Per AD § (b)(5) all NAS B737-300 are adressed by AD 2010-14-06 and SB737-35-1099.

Per AD §(c) all NAS B737-300 are Not Applicable since the safetyissue is adressed i AD § (b)(5).

AD § (e) is covered by AD 2010-14-06 and SB 737-35-1099.174080-35-04 SB 000Perform WITHIN 1080/D (effective from 19.Aug.2011)Perform WITHIN 6500/H (effective from 19.Aug.2011)

2011-14-08/AD Rev.00 OXYGEN - GENERAL VISUAL INSPECTION OF PSU OXYGEN MASK ASSEMBLY Not Applicable> 174080-35-04/SB* Rev.00 OXYGEN - GENERAL VISUAL INSPECTION/MOD OF PSU OXYGEN MASK ASSEMBLY Not Applicable / Special Text: Boeing

737 are Not Applicable by AD2011-14-08 § (c)






23.Oct.2014Page 329/429

Document-Number Type Rev Compliance A|C Subject Status2011-21-08 AD 00 MANDATORY A/C INSPECTION AND REPAIR OF BACKRESTS ON SICMA AERO SEATS Not Applicable / Special Text: A

LOPA review of the AC has beenperf.by Engineering. No SICMA PNinst

NAS has conducted a LOPA review of all Aircraft. NAS has no aircraftwith Sicma seats installed.

Compliance:AD § (f) in its entirety is Not Applicable to NAS due to No Sicmaseats installed.90-25-013 ISSUE 4 SB 04Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 330/429

Document-Number Type Rev Compliance A|C Subject Status2011-23-05 AD 00 MANDATORY A/C FUSELAGE FRAMES AND BULKHEADS - FORWARD CARGO BAY STRINGER 19 TO

STRINGER 21 - FRAMES AND FRAME REINFORCEMENTS AT WIRE PENETRATIONHOLE

Open

In compliance with paragraph(g)Inspection and (h) RepetitiveInspection.This Document SUPERSEDES 2009-02-06/AD Rev.01Perform within an unlimited threshold.

2011-23-05/AD Rev.00 FUSELAGE FRAMES AND BULKHEADS - FORWARD CARGO BAY STRINGER 19 TOSTRINGER 21 - FRAMES AND FRAME REINFORCEMENTS AT WIRE PENETRATIONHOLE

Open

This Document SUPERSEDES 2009-02-06/AD Rev.01> 737-53A1279/SB Rev.01 FUSELAGE - FRAMES AND BULKHEADS - FORWARD CARGO BAY STRINGER 19 TO

STRINGER 21 - FRAMES AND FRAME REINFORCEMENTS - INSPECTION, REPAIROpen

This Document SUPERSEDES 737-53A1279/SB Rev.00> > 737-53A1279/EO* Rev.01 NDT - FUSELAGE - FRAMES AND BULKHEADS - FORWARD CARGO BAY STRINGER 19

TO STRINGER 21 - FRAMES AND FRAME REINFORCEMENTS - INSPECTIONRepetitive

This Document SUPERSEDES 737-53A1279/EO Rev.00NOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentNOTE: 'Whichever comes later' calculation logic applicable for the intervalDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

47651/C

Perform initially within (effective fromManufacturer Date 13.Mar.1990) (L)30000/C Perform initially within (effectivefrom 02.Sep.2011) (L) 90/D /Interval(L):4500/C


> > 737-53A1279-01/EO* Rev.00 *AD* FUSELAGE FRAMES-WIRE PENETRATION HOLE-INSP/REPAIR & MOD Term.Action openDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT





23.Oct.2014Page 331/429

Document-Number Type Rev Compliance A|C Subject Status2011-24-12 AD 00 MANDATORY A/C FUSELAGE - SKIN - CRACKS AT CHEM-MILLED STEPS IN CROWN SKINS AT SPECIFIED

LOCATIONS - INSPECTIONRepetitive


2011-24-12/AD Rev.00 FUSELAGE - SKIN - CRACKS AT CHEM-MILLED STEPS IN CROWN SKINS AT SPECIFIEDLOCATIONS - INSPECTION

Repetitive

This Document SUPERSEDES 2010-01-09/AD Rev.00> 737-53A1301/SB Rev.02 FUSELAGE - SKIN - CRACKS AT CHEM-MILLED STEPS IN CROWN SKINS AT SPECIFIED

LOCATIONS - INSPECTIONRepetitive

This Document SUPERSEDES 737-53A1301/EO Rev.01This Document SUPERSEDES 737-53A1301/SB Rev.01

> > 737-53A1301/EO* Rev.02 FUSELAGE CROWN SKINS -NDT AT SPECIFIEC LOCATIONS- EXTERNAL UTPAINSPECTION FOR CRACKS AT CHEM-MILLED STEPS.

Repetitive




> > 737-53A1301-1/EO* Rev.02 FUSELAGE CROWN SKINS - NDT AT SPECIFIEC LOCATIONS - MFEC INSPECTION FORCRACKS AT CHEM-MILLED STEPS.






23.Oct.2014Page 332/429

Document-Number Type Rev Compliance A|C Subject Status2011-27-03 AD 00 MANDATORY A/C TO PREVENT AN UNDETECTED FAILURE OF THE PRIMARY LOAD PATH FOR THE

BALLSCREW IN THE DRIVE MECHANISM OF THE HSTA AND SUBSEQUENT WEAROpen





23.Oct.2014Page 333/429

Document-Number Type Rev Compliance A|C Subject StatusEfectivity:There are two SB requred to be performed by this AD.

SB 737-27A1277 is for 737NG is divided into two Groups:Gr1: LN# 1-1715Gr2: LN# 1716 and on

Compliance:AD §(g) is covered by these 4 Engineering Orders:

EO 737-27A1277-01 covers detailed inspection.EO 737-27A1277-02 covers lubricationEO 737-27A1277-03 covers restoration/OHEO 737-27A1277-04 covers impementation of MFG SB on Group 1 AC.

SB 737-27A1278 is for 737-100/200/300/400/500:

Compliance:AD §(g) is covered by these 4 Engineering Orders:

EO 737-27A1278-01 covers detailed inspection.EO 737-27A1278-02 covers lubricationEO 737-27A1278-03 covers restoration/OHEO 737-27A1278-04 covers impementation of MFG SB on Group 1 AC.

AMOC:An AMOC has been issued adressing §(g) of this AD. The AMOC specifiesthat you may extract only delta information from the SB (The SBcovers both MPD and AMM requirements, thus you have a doublelubrication requirement.). NAS takes advantage of the AMOC.





23.Oct.2014Page 334/429

Document-Number Type Rev Compliance A|C Subject Status737-27A1277737-27A1277-01737-27A1277-02737-27A1277-03737-27A1277-04737-27A1278737-27A1278-01737-27A1278-02737-27A1278-03737-27A1278-04PRODUCTION LINE PRR38275-74S

SBEOEOEOEOSBEOEOEOEOPRR

0100000000010000000000

Perform within an unlimited threshold.2011-27-03/AD Rev.00 TO PREVENT AN UNDETECTED FAILURE OF THE PRIMARY LOAD PATH FOR THE

BALLSCREW IN THE DRIVE MECHANISM OF THE HSTA AND SUBSEQUENT WEAROpen

> 737-27A1278/SB Rev.01 FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM -BALLSCREW AND BALL NUT INSPECTION AND LUBRICATION

Open

This Document SUPERSEDES 737-27A1278/SB Rev.00> > 737-27A1278-01/EO* Rev.00 DETAILED INSP. OF BALLSCREW;HORIZONTAL STABILIZER TRIM CONTROL SYSTEM Repetitive


04.Aug.2015 75572:00/HPerform initially before(F) 4000/H /Interval(F):4000/H or 547/D


03.Feb.2014 71572:00/H 43151/C 436901, N/AWas due at: 07.May.2014 and 4328340/HPerfRev.:'00'

> > 737-27A1278-02/EO* Rev.00 LUBRICATION OF BALLSCREW;HORIZONTAL STABILIZER TRIM CONTROL SYSTEM RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

05.Oct.2015 75319:36/HPerform initially before(F) 2000/H /Interval(F):360/D or 2000/H


10.Oct.2014 73319:36/H 44494/C 544213,Was due at: 07.Feb.2015 and 4414320/HPerfRev.:'00'





23.Oct.2014Page 335/429

Document-Number Type Rev Compliance A|C Subject Status> > 737-27A1278-03/EO* Rev.00 FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM -

BALLSCREW AND NUT INSPECTION, LUBRICATION, AND REPAIR/OVERHAULPart-Requirem.Contr.

> > 737-27A1278-04/EO* Rev.00 FLIGHT CONTROLS - HORIZONTAL STABILIZER TRIM CONTROL SYSTEM -BALLSCREW AND NUT INSPECTION, LUBRICATION, AND REPAIR/OVERHAUL

Open (Next Shop Visit)

Affected Rotables (Part No/Serial No/Position) Status65-49970-25 / KE01031 Pos=AFT (KKM) Open / NO LIMIT





23.Oct.2014Page 336/429

Document-Number Type Rev Compliance A|C Subject Status2012-02-08 AD 00 MANDATORY COMP AVIATION COMMUNICATION & SURVEILLANCE SYSTEMS, LLC (ACSS) TRAFFIC

ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) UNITSOpen

This AD is applicable to NAS 737-300 equipped with ACSS TCAS 2000(P/N 7517900-10003 or -10004) or T2CAS (9000000-20005).

Compliance:(g) P/N 7517900-10003 or -10004: Upgrade software i.a.w. SB8008229-001 Rev.02 (ATA SB 7517900-34-6040).P/N 9000000-20005: Upgrade software i.a.w. SB 8008233-001 Rev.03 (ATASB 9000000-34-6016).733-34-005733-34-0067517900-34-60409000000-34-6016US-2012-02-08

TOTOSBSBAD

0000020300

Perform BEFORE 13.Mar.20152012-02-08/AD Rev.00 AVIATION COMMUNICATION & SURVEILLANCE SYSTEMS, LLC (ACSS) TRAFFIC

ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) UNITSOpen

> 7517900-34-6040/SB Rev.02 NAVIGATION - TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM - TCAS 2000COMPUTER UNIT - INSTALLS NEW OPERATIONAL SW PN 9001049-005

Not Applicable

> > 733-34-005/TO* Rev.00 NAVIGATION - TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM - TCAS 2000COMPUTER UNIT - INSTALL NEW OPERATIONAL SW PN 9001049-005

Not Applicable


> 9000000-34-6016/SB Rev.03 NAVIGATION - TRAFFIC AND TERRAIN COLLISION AVOIDANCE SYSTEM - T2CASCOMPUTER UNIT - INSTALLS NEW OPERATIONAL SOFTWARE PN 9001049-005

Open

> > 733-34-006/TO* Rev.00 NAVIGATION - TRAFFIC AND TERRAIN COLLISION AVOIDANCE SYSTEM - T2CASCOMPUTER UNIT - INSTALL NEW OPERATIONAL SOFTWARE

Open


9000000-20005 / 22000131 Pos=E&E (KKM)Open / Next Due:12.Mar.2015 / WO:15864598





23.Oct.2014Page 337/429


2012-02-09 AD 00 MANDATORY A/C AIR CONDITIONING - DISTRIBUTION - REPLACEMENT OF BMS 8-39 DUCTINSULATION

Not Applicable

This AD applies to The Boeing Company Model 737-100, -200, -200C, and-300 series airplanes, certificated in any category; as identified inBoeing Service Bulletin 737-21A1132, Revision 3, dated February 16,2011.

Effectivity:This document is applicable to LN# 3-1585.

Compliance:

AD § (g) is complied with through SB 737-21A1132.2011-NM-101-AD2012-02-09737-21A1132737-21A1132737-21A1132737-SRP-21-0130 (REF)PRODUCTION LINE PRR35005-235R

NPRMADSBSBSBSRPPRR

000000010200

2012-02-09/AD Rev.00 AIR CONDITIONING - DISTRIBUTION - REPLACEMENT OF BMS 8-39 DUCTINSULATION

Not Applicable

> 737-21A1132/SB* Rev.03 AIR CONDITIONING - DISTRIBUTION - REPLACEMENT OF BMS 8-39 DUCTINSULATION







23.Oct.2014Page 338/429

Document-Number Type Rev Compliance A|C Subject Status2012-0209 AD 00 MANDATORY COMP ENGINE ACCESSORY GEARBOX (AGB) HAND-CRANKING PAD - MODIFICATION On Attrition

Applicability:CFM56-3 engines all models, all serial numbers not equipped with anAGB Part Number 335-300-112-0.CFM56-7B engines not equipped with an AGB PN 340-046-508-0 or PN340-046-509-0.12-1153-72-11297B-72-05647B-72-0879

ADSBSBSB

00000101

Perform within an unlimited threshold.2012-0209/AD Rev.00 ENGINE ACCESSORY GEARBOX (AGB) HAND-CRANKING PAD - MODIFICATION On Attrition> 3-72-1129/SB* Rev.03 ACCESSORY GEARBOX ASSEMBLY (AGB) WITH A NEW STARTER DRIVE PAD AND NEW

HANDCRANKING COVER AND REWORK OF OLD AGB TO THE NEW ONEOn Attrition

Affected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 725495 Pos=RH (KKM) On Attrition / Reason: AUTO ASSIGNEDCFM56-3B2 / 724473 Pos=LH (KKM) On Attrition / Reason: AUTO ASSIGNED





23.Oct.2014Page 339/429

Document-Number Type Rev Compliance A|C Subject Status2012-0254 AD 01 MANDATORY COMP OXYGEN - FLIGHT CREW OXYGEN MASK REGULATOR - IDENTIFICATION /

OPERATIONAL PROCEDURE / REPLACEMENTNot Applicable by Serial Number

In a repair station, improper maintenance on oxygen mask regulatorswas reported to Intertechnique: during an inspection of the oxygentest bench by its manufacturer, incorrect settings were noticed. Thistest bench setting discrepancy on the oxygen mask regulator couldcause an improper mask dilution schedule.

Not applicable to NAS due to no affected SN737-SL-35-026MCF-SBU-35-001

SLSB

0000

This Document SUPERSEDES 2012-0254/AD Rev.00Affected Rotables (Part No/Serial No/Position) StatusMC10-25-104 / 32839 Pos=#1 (KKM) Not ApplicableMC10-25-124 / 49059 Pos=#2 (KKM) Not ApplicableMC10-25-104 / 33047 Pos=FWD (KKM) Not Applicable





23.Oct.2014Page 340/429

Document-Number Type Rev Compliance A|C Subject Status2012-08-17 AD 00 MANDATORY A/C FUEL-REVISION OF MAINT PROGRAM FOR FQIS INST. BY STC ST00146BO Not Applicable / Special Text: This

Aircraft is Not Applicable due toSTC ST00146BO not installed.

This AD is only applicable to B737CL with STC ST00146BO incorperated.

Compliance:EO 2012-08-17-01 ensures compliance with AD§ (g), 4000 FH interval.EO 2012-08-17-02 ensures compliance with AD§ (g), 24000FH interval.2012-08-17-012012-08-17-02ST00146BOT3044-0010-0101

EOEOSTCDOCR

000000D

Perform BEFORE 30.Nov.20132012-08-17/AD Rev.00 FUEL-REVISION OF MAINT PROGRAM FOR FQIS INST. BY STC ST00146BO Not Applicable / Special Text: This

Aircraft is Not Applicable due to STCST00146BO not installed.

> 2012-08-17-01/EO* Rev.00 FUEL-REVISION OF MAINT PROGRAM FOR FQIS INST. BY STC ST00146BO Not ApplicableReason for this StatusNOT APPLICABLE DUE TO STC ST00146BO NOT INSTALLED.

> 2012-08-17-02/EO* Rev.00 FUEL-REVISION OF MAINT PROGRAM FOR FQIS INST. BY STC ST00146BO Not ApplicableReason for this StatusNOT APPLICABLE DUE TO STC ST00146BO NOT INSTALLED.





23.Oct.2014Page 341/429

Document-Number Type Rev Compliance A|C Subject Status2012-11-09 AD 00 MANDATORY A/C OXYGEN - DEACTIVATION OF LAVATORY OXYGEN GENERATORS Not Applicable

This AD is applicable only to-AC operating under 14 CFR FAA Part 121-US reg- AC operating under FAA Part 129

Ref EASA letter stating that this AD is not applicable for USmanufactured aircraft operating in Europe (under EASA juristiction).

During re-delivery some aircraft will be transferred to FAA Part121/129 opweration. The AD will be incorporated at that timeEASA E-MAILEASA LETTER

DOCRDOCR

0000

This Document SUPERSEDES 2011-04-09/AD Rev.00Perform WITHIN 21/D (effective from 14.Mar.2011)

2012-11-09/AD Rev.00 OXYGEN - DEACTIVATION OF LAVATORY OXYGEN GENERATORS Not ApplicableThis Document SUPERSEDES 2011-04-09/AD Rev.00

> 2012-11-09-01/EO* Rev.00 OXYGEN - DEACTIVATION OF LAVATORY OXYGEN GENERATORS Not ApplicableReason for this StatusOMLY FOR AC OPEARTING UNDER 14CFR PART 121 OR US REGISTERED

> 2012-11-09-02/EO* Rev.00 OXYGEN - INSTALLATION OF SUPPLEMENTARY LAVATORY OXYGEN SYSTEM Not Applicable / Special Text: Thisaircraft is NOT to be operated under14CFR121 or 129 rules.






23.Oct.2014Page 342/429

Document-Number Type Rev Compliance A|C Subject Status2012-12-04 AD 00 MANDATORY A/C *AD* FUSELAGE SKIN-STR S-1/2R, STA 400-460 DVI INSPECTION Open

2008-19-03 (ACTIVE)737-53A1293 (ACTIVE)737-SRP-53-0334 (REF)FAA LETTER 120S-09-460

ADSBSRPAMOC


2012-12-04/AD Rev.00 *AD* FUSELAGE SKIN-STR S-1/2R, STA 400-460 DVI INSPECTION OpenThis Document SUPERSEDES 2008-19-03/AD Rev.00

> 737-53A1293/SB* Rev.02 FUSELAGE - SKIN - STRINGER S-1 AND S-2R, STATION 400 TO 460 INSPECTION ANDREPAIR

Open

This Document SUPERSEDES 737-53A1293/SB Rev.01Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

NO LIMIT> > 737-53A1293/EO* Rev.02 NDT - FUSELAGE SKIN - BS 400-460, S-1/2R - EXTERNAL UTPA INSPECTION Repetitive




> > 737-53A1293-1/EO* Rev.02 NDT - FUSELAGE SKIN - BS 400-460, S-1/2R - EXTERNAL MFEC INSPECTION Not ApplicableReason for this StatusTEMPORATY NOT APPLIC DUE TO UTPA INSP PERF ON EO 737-53A1293





23.Oct.2014Page 343/429

Document-Number Type Rev Compliance A|C Subject Status2012-12-05 AD 00 MANDATORY A/C *AD* INTERCOASTALS - BS360 & 294.5 S-6/17L - INSPECTION Repetitive

737-53-1204737-53A-1240737-53A1240US-2012-12-05

SBSBSBAD

020101N/A

This Document SUPERSEDES 2009-16-14/AD Rev.NOTEPerform within an unlimited threshold.

2012-12-05/AD Rev.00 *AD* INTERCOASTALS - BS360 & 294.5 S-6/17L - INSPECTION RepetitiveThis Document SUPERSEDES 2009-16-14/AD Rev.NOTE




> 737-53A1204/SB Rev.02 *AD* INTERCOASTALS - BS360 & 294.5 S-6/17L - NDT INSPECTION Repetitive> > 737-53A1204-01/EO* Rev.02 *AD* NDT - INTERCOASTALS - BS360 & 294.5 S-6/17L - INTERNAL NDT INSP. REPETITIVE

INSPECTIONRepetitive / Special Text: Group 1.




> 737-53A1240/SB Rev.01 *AD* FUSELAGE - FRAME BS 348.5 S-14/16L - INTERNAL NDT INSPECTION Repetitive> > 737-53A1240/EO* Rev.01 *AD* NDT - FUSELAGE - FRAME BS 348.5 S-14/16L - INTERNAL NDT INSP. Repetitive / Special Text: Group 3.







23.Oct.2014Page 344/429

Document-Number Type Rev Compliance A|C Subject StatusPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks13.Feb.2014 71572:00/H 43151/C 273642, N/A Was due at: 43798/C PerfRev.:'01'





23.Oct.2014Page 345/429

Document-Number Type Rev Compliance A|C Subject Status2012-13-07 AD 00 MANDATORY COMP WINGS - TRAILING EDGE FLAPS - OUTBOARD FLAP, CARRIAGE SPINDLE - INSPECTION

FOR CORROSIONNot Applicable / Special Text: PerAD and SB 737-57A1319, this PN isNot Applicable for inspections

Due to more reports of failed HVOF coatings, all HVOF coated carraigespindles must be inspected within 90 days, repeat insp. every 180days.

SB allows for a document review to determine which carriage spindlesto inspect. NAS treats this SB as a component SB as we have track ofall sub ASSY PN.

Compliance:AD § (g) is complied with through a document review. NAS hasregistered all carriage sub assemblies.AD § (h) is complied with through EO 737-57A1319-01AD § (i) is complied with through EO 737-57A1319-02, this EO replacesany affected carriage with finding.AD § (j) is covered through receiving/document review and/or EO737-57A1319-01 which will be called out at installation.AD § (k); Revision 00 of the SB was utilized for initial inspections,but Revision: 01 was used before the AD was issued.737-57A1319737-57A1319-01737-57A1319-02

SBEOEO

010000

Perform within an unlimited threshold.2012-13-07/AD Rev.00 WINGS - TRAILING EDGE FLAPS - OUTBOARD FLAP, CARRIAGE SPINDLE - INSPECTION

FOR CORROSIONNot Applicable / Special Text: Per ADand SB 737-57A1319, this PN is NotApplicable for inspections

> 737-57A1319/SB Rev.01 WINGS - TRAILING EDGE FLAPS - OUTBOARD FLAP, CARRIAGE SPINDLE - INSPECTIONFOR CORROSION

Not Applicable






23.Oct.2014Page 346/429

Document-Number Type Rev Compliance A|C Subject Status> > 737-57A1319-01/EO* Rev.00 WINGS - INSPECTION FOR CORROSION - OUTBOARD FLAP, CARRIAGE SPINDLE Not Applicable

This Document is terminated with implementation of 737-57A1319-02/EO Rev.00Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

> > 737-57A1319-02/EO* Rev.00 WINGS - REPLACEMENT OF OUTBOARD FLAP, CARRIAGE SPINDLE Not ApplicableThis Document terminates 737-57A1319-01/EO Rev.00Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 347/429

Document-Number Type Rev Compliance A|C Subject Status2012-18-13 AD 01 MANDATORY A/C BS 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR WEB CRACKS Open

The time requirement is controled by the time requirements of theunderlaying EO:s

2012-18-13 R1

(s) Retained Terminating Action With Revised Paragraph ReferenceThis paragraph restates the terminating action specified in paragraph(s) of AD 2012-18-13, Amendment 39-17190 (77 FR 57990, September 19,2012), with a revised paragraph reference. Accomplishment of therequirements in paragraph (k) of this AD terminates the requirementsof paragraphs (g) through (j) of this AD.

2012-18-12

(s) Terminating Action Accomplishment of the requirements ofparagraphs (k) through (q) of this AD terminates the requirements ofparagraphs (g) through (j) of this AD.





23.Oct.2014Page 348/429

Document-Number Type Rev Compliance A|C Subject Status1999-08-23737-53A1214737-53A1214737-53A1214737-53A1214737-53A1214-01737-53A1214-1A1737-53A1214-1A2737-53A1214-1F1737-53A1214-1F2737-53A1214-2737-53A1214-3A737-53A1214-3F737-53A1214-4737-53A1214-5737-53A1214-6ST01219SE

ADSBSBSBSBEOEOEOEOEOEOEOEOEOEOEOSTC

0001020304000000000000000000000000


2012-18-13/AD Rev.01 BS 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR WEB CRACKS OpenThis Document SUPERSEDES 2012-18-13/AD Rev.00

> 737-53A1214/SB Rev.04 FUSELAGE - BODY STATION 1016 AFT PRESSURE BULKHEAD WEB CRACKSINSPECTION AND REPAIR

Open

This Document SUPERSEDES 737-53A1214/SB Rev.03> > 737-53A1214-1A1/EO*Rev.00

PART I - NDT INSP OF WEB AT "Y" CHORD - S-5L TO 7L AND S-5R TO 9R FROM AFT Repetitive

This Document SUPERSEDES 737-53A1214-1A/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

46951/C 502758Perform initially before(F) 27375/C /Interval(F):1200/C






23.Oct.2014Page 349/429

Document-Number Type Rev Compliance A|C Subject Status03.Dec.2013 71211:00/H 42863/C 490746, N/A Was due at: 42940/C PerfRev.:'00'

> > 737-53A1214-1A2/EO*Rev.00

PART I - NDT INSPECTION OF WEB AT "Y" CHORD - ABOVE S-15L/R EXCEPT S-5L TO 7LAND S-5R TO 9R. FROM AFT.

Repetitive




29.Jun.2012 67212:00/H 39926/C N/APerfRev.:'00' / Reason: Initialized: Last perf.with 737-53A1214-1A/EO/00

> > 737-53A1214-1F1/EO*Rev.00

PART I - NDT INSP OF WEB AT "Y" CHORD - S-5L TO 7L AND S-5R TO 9R FROMFORWARD

Repetitive

This Document SUPERSEDES 737-53A1214-1F/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document



> > 737-53A1214-1F2/EO*Rev.00

PART I -NDT INSPECTION OF WEB AT "Y" CHORD -ABOVE S-15L/R EXCEPT S-5L TO 7LAND S-5R TO 9R. FROM FORWARD.

Repetitive




> > 737-53A1214-2/EO* Rev.00 PART II - DETAILED INSPECTION FOR OIL-CANNING FROM AFT RepetitiveNOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document





23.Oct.2014Page 350/429


47740/CPerform initially within (effective from24.Oct.2012) (L) 1200/C /Interval(F):6000/C

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks11.Jun.2013 69701:00/H 41740/C 436174, N/A Was due at: 41763/C PerfRev.:'00'

> > 737-53A1214-3A/EO* Rev.00 PART III - NDT INSPECTION OF WEB AT "Y" CHORD - BELOW S-15L/R FROM AFT OpenThis Document SUPERSEDES 737-53A1214-3/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

55151/C 489483Perform initially within (effective from24.Oct.2012) (F) 6000/C or 730/D /Interval(F):6000/C

> > 737-53A1214-3F/EO* Rev.00 PART III - NDT INSPECTION OF WEB AT "Y" CHORD - BELOW S-15L/R FROM FWD. RepetitiveThis Document SUPERSEDES 737-53A1214-3/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

55151/CPerform initially within (effective from24.Oct.2012) (F) 6000/C or 730/D /Interval(F):12000/C


14.Feb.2014 71572:00/H 43151/C 489480, N/AWas due at: 46563/C and 24.Oct.2014PerfRev.:'00'

> > 737-53A1214-4/EO* Rev.00 PART IV - NDT INSPECTION OF THE DOME CAP AT THE CENTER OF THE BULKHEADFROM AFT

Repetitive





> > 737-53A1214-5/EO* Rev.00 PART V -NDT INSP OF FWD FLANGE OF THE "Z" STIFFENERS AT THE DOME CAPFROM FWD

Repetitive





23.Oct.2014Page 351/429





> > 737-53A1214-6/EO* Rev.00 PART VI - DETAILED INSPECTION FOR EXISTING REPAIRS ON THE BULKHEAD FROMAFT

Closed 03.Feb.2014 W/O:489479






23.Oct.2014Page 352/429

Document-Number Type Rev Compliance A|C Subject Status2012-18-13 AD 00 MANDATORY A/C BS 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR WEB CRACKS Superseded (Open)

1999-08-23 (ACTIVE)37-SBB-53A1214-1A (REP TASK)37-SBB-53A1214-1F (REP TASK)37-SBB-53A1214-3 (REP TASK)737-53A1214737-53A1214 (REF)737-53A1214 R1 (REF)737-53A1214 R2 (REF)SBB 737-53A1214 (MAINT TASK)

ADTATATASBSBSBSBTA

04

This Document SUPERSEDES 1999-08-23/AD Rev.00This Document has been SUPERSEDED BY 2012-18-13/AD Rev.01Perform within an unlimited threshold.

2012-18-13/AD Rev.00 BS 1016 AFT PRESSURE BULKHEAD - INSPECTION FOR WEB CRACKS OpenThis Document SUPERSEDES 1999-08-23/AD Rev.00This Document has been SUPERSEDED BY 2012-18-13/AD Rev.01

> 737-53A1214/SB Rev.04 FUSELAGE - BODY STATION 1016 AFT PRESSURE BULKHEAD WEB CRACKSINSPECTION AND REPAIR

Open

This Document SUPERSEDES 737-53A1214/SB Rev.03> > 737-53A1214-1A1/EO*Rev.00

PART I - NDT INSP OF WEB AT "Y" CHORD - S-5L TO 7L AND S-5R TO 9R FROM AFT Repetitive



Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks03.Dec.2013 71211:00/H 42863/C 490746, N/A Was due at: 42940/C PerfRev.:'00'

> > 737-53A1214-1A2/EO*Rev.00

PART I - NDT INSPECTION OF WEB AT "Y" CHORD - ABOVE S-15L/R EXCEPT S-5L TO 7LAND S-5R TO 9R. FROM AFT.

Repetitive






23.Oct.2014Page 353/429




29.Jun.2012 67212:00/H 39926/C N/APerfRev.:'00' / Reason: Initialized: Last perf.with 737-53A1214-1A/EO/00

> > 737-53A1214-1F1/EO*Rev.00

PART I - NDT INSP OF WEB AT "Y" CHORD - S-5L TO 7L AND S-5R TO 9R FROMFORWARD

Repetitive




> > 737-53A1214-1F2/EO*Rev.00

PART I -NDT INSPECTION OF WEB AT "Y" CHORD -ABOVE S-15L/R EXCEPT S-5L TO 7LAND S-5R TO 9R. FROM FORWARD.

Repetitive




> > 737-53A1214-2/EO* Rev.00 PART II - DETAILED INSPECTION FOR OIL-CANNING FROM AFT RepetitiveNOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

47740/CPerform initially within (effective from24.Oct.2012) (L) 1200/C /Interval(F):6000/C

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks11.Jun.2013 69701:00/H 41740/C 436174, N/A Was due at: 41763/C PerfRev.:'00'

> > 737-53A1214-3A/EO* Rev.00 PART III - NDT INSPECTION OF WEB AT "Y" CHORD - BELOW S-15L/R FROM AFT OpenThis Document SUPERSEDES 737-53A1214-3/EO Rev.00





23.Oct.2014Page 354/429


55151/C 489483Perform initially within (effective from24.Oct.2012) (F) 6000/C or 730/D /Interval(F):6000/C

> > 737-53A1214-3F/EO* Rev.00 PART III - NDT INSPECTION OF WEB AT "Y" CHORD - BELOW S-15L/R FROM FWD. RepetitiveThis Document SUPERSEDES 737-53A1214-3/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document




> > 737-53A1214-4/EO* Rev.00 PART IV - NDT INSPECTION OF THE DOME CAP AT THE CENTER OF THE BULKHEADFROM AFT

Repetitive





> > 737-53A1214-5/EO* Rev.00 PART V -NDT INSP OF FWD FLANGE OF THE "Z" STIFFENERS AT THE DOME CAPFROM FWD

Repetitive









23.Oct.2014Page 355/429

Document-Number Type Rev Compliance A|C Subject Status> > 737-53A1214-6/EO* Rev.00 PART VI - DETAILED INSPECTION FOR EXISTING REPAIRS ON THE BULKHEAD FROM

AFTClosed 03.Feb.2014 W/O:489479






23.Oct.2014Page 356/429

Document-Number Type Rev Compliance A|C Subject Status2012-19-11 AD 00 MANDATORY A/C AIR CONDITIONING - CABIN PRESSURE INDICATION AND WARNING SYSTEM -

REDUNDANT PRESSURE SWITCH INSTALLATIONOpen

Compliance:

AD §(C)(1): This § is complied with through SB 737-21-1164 Rev.1AD §(C)(2): This § is complied with through SB 737-21-1165 Rev.:2AD § (d) through (g) is complied with through both SB 737-21-1164 and737-21-1165.AD § (h)is complied with through SB 737-31A1325 Rev.:00 and SB737-21A1332.AD§ (i)(1): NA to NAS, we will perform SB 737-21-1165 Rev.:02.AD§ (i)(2): NA to NAS, we have not performed SB 737-31A1332 Rev.:01AD§ (i)(3): This paragraph gives credit for NAS performing SB737-31A1332 Rev.:02 on all NAS group Aircraft. Less group 24, MSN:28620.AD§ (i)(4): NA to NAS, NAS has no Group 21 AC.737-21-1164737-21-1165737-31A1325737-31A1332737-31A1332AMM 21-33-00, 21-33-04, 24-22-00AMM 25-11-01, 31-51-00, 31-51-04AMM 34-16-00, 52-40-00BAE SB 69-78214-31-03FTD 737NG-FTD-31-07001PRR 38275-129SSRP 737-SRP-21-0172

SBSBSBSBSBAMMAMMAMMSBFTDPRRSRP

010200020300000000000000

Perform BEFORE 27.Nov.20182012-19-11/AD Rev.00 AIR CONDITIONING - CABIN PRESSURE INDICATION AND WARNING SYSTEM -

REDUNDANT PRESSURE SWITCH INSTALLATIONOpen





23.Oct.2014Page 357/429

Document-Number Type Rev Compliance A|C Subject Status> 737-21-1164/SB* Rev.01 PRESSURIZATION INDICATION AND WARNING - REDUNDANT PRESSURE SWITCH

AND AURAL WARNING MODULE INSTALLATIONCancelled

This Document SUPERSEDES 737-21-1164/SB Rev.00This Document has been SUPERSEDED BY 737-21-1164/SB Rev.02Reason for this StatusManually deassigned after Document Cancelled or Superseded

> 737-21-1164/SB* Rev.02 PRESSURIZATION INDICATION AND WARNING - REDUNDANT PRESSURE SWITCHAND AURAL WARNING MODULE INSTALLATION

Open / Special Text: SB group 6

This Document SUPERSEDES 737-21-1164/SB Rev.01Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document06.Nov.2018 Perform initially before(F) 07.Nov.2018

> 737-31A1325/SB* Rev.00 IND./RECORDING SYSTEMS - AURAL WARNING SYSTEM - INSTALLATION OF THECABIN ALT. WARNING SYS. AND TAKEOFF CONFIGURATION WARNING SYS. LIGHTS

Cancelled






23.Oct.2014Page 358/429

Document-Number Type Rev Compliance A|C Subject Status2012-23-04 AD 00 MANDATORY A/C FUSELAGE - FRAMES - BODY STATION 727 OUTBOARD CHORD AT STRINGER 18A

INSPECTION AND PREVENTIVE MODIFICATIONOpen

737-53A116695-12-17 (-100, -200)

SBAD

020

Perform within an unlimited threshold.2012-23-04/AD Rev.00 FUSELAGE - FRAMES - BODY STATION 727 OUTBOARD CHORD AT STRINGER 18A

INSPECTION AND PREVENTIVE MODIFICATIONOpen

> 737-53A1166/SB Rev.02 FUSELAGE - FRAMES - BODY STATION 727 OUTBOARD CHORD AT STRINGER 18AINSPECTION AND PREVENTIVE MODIFICATION

Open

> > 07-1040/TD* Rev.00 STA 727 FRAME OUTBOARD CHORD - REPLACEMENT OF REPAIR/MOD. Not Applicable by Serial Number> > 737-53A1166-F1/EO* Rev.01 FUSELAGE, FRAMES BST 727 OUTB CHORD AT STR 18A INSP & MOD Term.Action open


> > 737-53A1166-P1/EO* Rev.01 FUSELAGE FRAME BS727 AUX & OUTB CHORD AT STR 18A INSPECTION RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document



> > 737-53A1166-P2/EO* Rev.00 FUSELAGE FRAME BS727 STRINGER 18A OUTBOARD CHORD INSPECTION RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document



> > 737-53A1166-P3/EO* Rev.00 FUSELAGE FRAME, BS727 OUTB CHORD AT STR 18A INSPECTION OPEN HOLE EDDYCURRENT INSPECTION

Open







23.Oct.2014Page 359/429

Document-Number Type Rev Compliance A|C Subject Status2012-23-14 AD 00 MANDATORY A/C *AD* FUSELAGE - SKIN - SKIN CRACKING AT THE AFT WASTE WATER DRAIN MAST

INSPECTION/ REPAIRClosed 12.Nov.2012 W/O:273636

737-53A1318 SB 00Perform within an unlimited threshold.

2012-23-14/AD Rev.00 *AD* FUSELAGE - SKIN - SKIN CRACKING AT THE AFT WASTE WATER DRAIN MASTINSPECTION/ REPAIR

Closed 12.Nov.2012 W/O:273636

> 737-53A1318/SB* Rev.00 *AD* FUSELAGE - SKIN - SKIN CRACKING AT THE AFT WASTE WATER DRAIN MASTINSPECTION AND REPAIR

Closed 12.Nov.2012 W/O:273636

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks12.Nov.2012 68139:00/H 40570/C 273636, N/A Was due at: 43024/C PerfRev.:'00'





23.Oct.2014Page 360/429

Document-Number Type Rev Compliance A|C Subject Status2012-26-02 AD 00 MANDATORY A/C FUSELAGE - SKIN - CRACKS AT CHEM-MILLED STEPS - INSPECTION AND REPAIR Not Applicable





23.Oct.2014Page 361/429

Document-Number Type Rev Compliance A|C Subject StatusCompliance notes:(Para. = AD 2012-26-02 Paragraph)

Para.(a) through (f)Non-complience items.

Para.(g) and (h) Retained Inital and Repetitive inspectionsTerminated by Para.(m).

Para.(i) through (l) Retained Repairs, Reporting and Previousaction.Paragraph to retaint compliance with AD 2005-13-27

Para.(m) New Fuselage Skin Inspections at Chem-Mill Steps Commonto Lap JointsComplied with by EO 737-53A1234-01,-02,-03,-04,-05,-06EO 737-53A1234-01 and -02 is same insp with MFEC and UTPA.EO 737-53A1234-03 and -04 is same insp with MFEC and UTPA.EO 737-53A1234-05 and -06 is same insp with MFEC and UTPA.

Para.(n) New Permanent or Time-Limited Repair for Cracking FoundDuring Inspections Required by Paragraph (m) of This ADComplied with by Part 2 or 4 of EO 737-53A1234-01 or -02Part 2 is permanent repair.Part 4 is time limited repair.

Para. (o) New Fuselage Skin Inspections at Chem-Mill Steps Commonto Shear Wrinkle AreasComplied with by EO 737-53A1234-07 or -08EO 737-53A1234-07 and -08 is same insp with MFEC and UTPA





23.Oct.2014Page 362/429

Document-Number Type Rev Compliance A|C Subject StatusPara. (p) New Fuselage Skin Inspections at Specified VerticalChem-Mill Step LocationsComplied with by EO 737-53A1234-10 or -11EO 737-53A1234-10 and -11 is same insp with MFEC and UTPA

Para. (q) New Fuselage Skin Inspections at Chem-Mill Steps inGeneral Pocket-to-Pocket AreasComplied with by EO 737-53A1234-12/-13 and EO 737-53A1234-14/-15EO 737-53A1234-12 and -13 is same insp, at S-10L to S-10R STA 360to 1016, with MFEC and UTPAEO 737-53A1234-14 and -15 is same insp, at STA 259.5 to 360between S-4L and S-4R, with MFEC and UTPA

Para. (r) New Inspection ExceptionFor inspections required by paragraph (m) of this AD:Complied with by Note 1 in EO 737-53A1234-01,-02,-03,-04,-05,-06,-10,-11,-12,-13,-14 and -15.

Para. (s) New Repair of Cracking Found During InspectionsRequired by Para. (o) Through (q) of This AD.Paragraph to give actions per AMOC applicability.

Para. (t) New Actions for Airplanes on Which Repairs Have BeenDone Using Previous Service Information.Sub Para 1 Complied with by Part 3 of EO 737-53A1234-01 and -02Sub Para 2 and 3 is N/A due to no time-limited repairs on NAS fleetat AD effectivity.

Para. (u) New Action Not in Accomplishment Instructions ofService InformationComplied with by AD note under item 3.B.1.i in





23.Oct.2014Page 363/429

Document-Number Type Rev Compliance A|C Subject StatusEO 737-53A1234-01,-02,-03,-04,-05,-06,-10,-11,-12,-13,-14 and -15.

Para. (v) Exceptions to Boeing Alert Service Bulletin737-53A1234, Revision 2, Dated November 24, 2010All applicable EO`s have same effectivity date as AD 2012-26-02

Para.(w) through (y)Non-complience items.This Document SUPERSEDES 2005-13-27/AD Rev.00

2012-26-02/AD Rev.00 FUSELAGE - SKIN - CRACKS AT CHEM-MILLED STEPS - INSPECTION AND REPAIR Not ApplicableThis Document SUPERSEDES 2005-13-27/AD Rev.00

> 737-53A1234/SB Rev.02 FUSELAGE - SKIN - CRACKS AT CHEM-MILLED STEPS - INSPECTION AND REPAIR Not ApplicableThis Document SUPERSEDES 737-53-1234/SB Rev.01

> > 737-53A1234-01/EO* Rev.01 NDT FUSELAGE SKINS S-10L/R FIG 2 - MFEC INSP FOR CRACKS AT CHEM-MILLEDSTEPS. FIGURE 2 - THRESHOLD 25000 FC.


This Document SUPERSEDES 737-53A1234-01/EO Rev.00> > 737-53A1234-02/EO* Rev.01 NDT FUSELAGE SKINS S-10L/R FIG 2 - UTPA INSP FOR CRACKS AT CHEM-MILLED

STEPS. LAP JOINTS. - THRESHOLD 25000 FC.(NOT IN USE)Not Applicable by Serial Number

This Document SUPERSEDES 737-53A1234-02/EO Rev.00> > 737-53A1234-03/EO* Rev.01 NDT FUSELAGE SKINS S-4L/R 10L/R FIG 11 - MFEC INSP FOR CRACKS AT CHEM-MILLED

STEPS. LAP JOINTS. THRESHOLD 28000 FC.Not Applicable by Serial Number

This Document SUPERSEDES 737-53A1234-03/EO Rev.00> > 737-53A1234-04/EO* Rev.01 NDT FUSELAGE SKINS S-4L/R 10L/R FIG 11 - UTPA INSP FOR CRACKS AT CHEM-MILLED

STEPS. LAP JOINTS. THRESHOLD 28000 FC. (NOT IN USE)Not Applicable by Serial Number

This Document SUPERSEDES 737-53A1234-04/EO Rev.00> > 737-53A1234-05/EO* Rev.01 NDT FUSELAGE SKINS S-4L/R 10L/R FIG 16 - MFEC INSP FOR CRACKS AT CHEM-MILLED

STEPS LAP JOINTS. THRESHOLD 42000 FC.Not Applicable by Serial Number

This Document SUPERSEDES 737-53A1234-05/EO Rev.00> > 737-53A1234-06/EO* Rev.01 NDT FUSELAGE SKINS S-4L/R 10L/R FIG 16 - UTPA INSP FOR CRACKS AT CHEM-MILLED

STEPS LAP JOINTS. THRESHOLD 42000 FC.(NOT IN USE)Not Applicable by Serial Number






23.Oct.2014Page 364/429

Document-Number Type Rev Compliance A|C Subject Status> > 737-53A1234-07/EO* Rev.01 NDT FUSELAGE SKINS S-6/9L & 6/9R FIG 20 - MFEC INSP FOR CRACKS AT

CHEM-MILLED STEPS - SHEAR WRINKLE AREAS- - THRESHOLD 33000 FC.Not Applicable by Serial Number

This Document SUPERSEDES 737-53A1234-07/EO Rev.00> > 737-53A1234-08/EO* Rev.01 NDT FUSELAGE SKINS S-6/9L & 6/9R FIG 20 - UTPA INSP FOR CRACKS AT

CHEM-MILLED STEPS-SHEAR WRINKLE AREAS-THRESHOLD 33000 FC.(NOT IN USE)Not Applicable by Serial Number

This Document SUPERSEDES 737-53A1234-08/EO Rev.00> > 737-53A1234-09/EO* Rev.00 PERMANENT SKIN REPAIR AT S-10 ABOVE LAP SPLICE. Not Applicable by Serial Number> > 737-53A1234-10/EO* Rev.00 FUSELAGE CROWN SKINS - NDT INSP FOR VERTICAL CHEM-MILL CRACKING AT

SPECIFIED LOCATIONS- FIGURE 24 - 1800 FC/FH INTERVALNot Applicable by Serial Number

> > 737-53A1234-12/EO* Rev.00 FUSELAGE SKIN NDT INSP AT CHEM-MILL STEPS IN GEN POCKET-TO-POCKET AREAS10L TO S-10R STA 360 TO STA 1016- FIGURE 28 - 500 FC INTERVAL


> > 737-53A1234-14/EO* Rev.00 FUSELAGE SKIN NDT INSP AT CHEM-MILL STEPS IN GEN POCKET-TO-POCKET AREASTA259.5 TO STA360 S-4L TO S-4R - FIGURE 33 - 500 FC/FH INTERVAL






23.Oct.2014Page 365/429

Document-Number Type Rev Compliance A|C Subject Status2013-0020 AD 03 MANDATORY COMP SAFETY BELTS / TORSO RESTRAINT SYSTEMS - INSP/REPLACEMENT Superseded (Not Applicable)

This AD revision 3 is issued to update AmSafe and Schroth referencepublications.

As a result of an investigation on some maintenance organisations,EASA was made aware that safety belts and torso restraint systemsmanufactured by design approval holders, have been maintained orrepaired by maintenance organisations without holding approvedmaintenance data.

Ref AD:

Within 6 months after 14 February 2013 [the effective date of theoriginal issue of this AD], inspect the markings of safety beltsand/or torso restraint systems, to determine if they have beenmaintained or repaired by organisations other than the designapproval holder. A review of the applicable maintenance records isacceptable to identify the safety belts and/or torso restraintsystems as specified in this paragraph, provided those records can berelied upon for that purpose, and the affected safety belts and/ortorso restraint systems can be conclusively identified from thatreview.

NAS Action:Review of applicable maintenance records (RO at logistic dep) showsthat the seat belts are maintained at approved shop.EASA AD 2013-0020EASA AD 2013-0020EASA AD 2013-0020

ADADAD

000102

This Document SUPERSEDES 2013-0020/AD Rev.02This Document has been SUPERSEDED BY 2013-0020/AD Rev.04





23.Oct.2014Page 366/429

Document-Number Type Rev Compliance A|C Subject StatusAffected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

2013-0020/AD* Rev.03 SAFETY BELTS / TORSO RESTRAINT SYSTEMS - INSP/REPLACEMENT Not ApplicableThis Document SUPERSEDES 2013-0020/AD Rev.02This Document has been SUPERSEDED BY 2013-0020/AD Rev.04Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 367/429

Document-Number Type Rev Compliance A|C Subject Status2013-0020 AD 04 MANDATORY COMP SAFETY BELTS / TORSO RESTRAINT SYSTEMS - INSP/REPLACEMENT Not Applicable





23.Oct.2014Page 368/429

Document-Number Type Rev Compliance A|C Subject StatusCorrection of revision 4 dated 05 September 2014 state:This AD is re-published to improve the wording with regard to safetybelts and torso restraints not affected by the AD. Clarification isprovided on companies qualified to repair/overhaul safety belts andtorso restraints.

This AD revision 4 amends the "Applicability" section to clarify EPAmarkings, to update the Pasific Scientific reference publication, andto correct Appendix 1 of the AD


Ref AD:

1. Within 6 months after 14 February 2013 [the effective date of theoriginal issue of this AD], inspect the markings of safety beltsand/or torso restraint systems, to determine if they have beenmaintained or repaired by organisations other than the designapproval holder. A review of the applicable maintenance records isacceptable to identify the safety belts and/or torso restraintsystems as specified in this paragraph, provided those records can berelied upon for that purpose, and the affected safety belts and/ortorso restraint systems can be conclusively identified from thatreview.

2 If safety belts and torso restraint systems have been maintained orrepaired by an organisation other than the design approval holder,





23.Oct.2014Page 369/429

Document-Number Type Rev Compliance A|C Subject Statuswithin 1 month after the inspection required by paragraph (1) of thisAD, verify if the organisation is listed among the authorizedmaintenance or repair organisation reference documents quoted in theRef. Publications section of this AD, or alternatively contact thedesign approval holder of the safety belts and torso restraintsystems for confirmation that the maintenance or repair organisationhad been authorised by them.

3 If the safety belts and/or torso restraint systems have beenmaintained or repaired by a repair station/maintenance organizationnot authorized by the design approval holder, within 18 months afterthe inspection required by paragraph (1) of this AD, remove thesafety belts and/or torso restraint systems and replace them withserviceable parts, or make the relevant seat inoperative.

NAS Action:Review of applicable maintenance records (RO at logistic dep) showsthat the seat belts are maintained at approved shop.AMSAFE REP STN DOC E512615EASA AD 2013-0020EASA AD 2013-0020EASA AD 2013-0020EASA AD 2013-0020SIL 25-0303D

DOCRADADADADSIL

LAST00010203LAST

This Document SUPERSEDES 2013-0020/AD Rev.03Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

2013-0020/AD* Rev.04 SAFETY BELTS / TORSO RESTRAINT SYSTEMS - INSP/REPLACEMENT Not ApplicableThis Document SUPERSEDES 2013-0020/AD Rev.03Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 370/429


2013-0020 AD 00 MANDATORY COMP SAFETY BELTS / TORSO RESTRAINT SYSTEMS - INSP/REPLACEMENT Superseded (Not Applicable bySerial Number)

As a result of an investigation on some maintenance organisations,EASA was made aware that safety belts and torso restraint systemsmanufactured by design approval holders, have been maintained orrepaired by maintenance organisations without holding approvedmaintenance data.This Document has been SUPERSEDED BY 2013-0020/AD Rev.01Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 371/429

Document-Number Type Rev Compliance A|C Subject Status2013-0020 AD 01 MANDATORY COMP SAFETY BELTS / TORSO RESTRAINT SYSTEMS - INSP/REPLACEMENT Superseded (Not Applicable by

Serial Number)As a result of an investigation on some maintenance organisations,EASA was made aware that safety belts and torso restraint systemsmanufactured by design approval holders, have been maintained orrepaired by maintenance organisations without holding approvedmaintenance data.

Ref AD:


NAS Action:Review of applicable maintenance records (RO at logistic dep) showsthat the seat belts are maintained at approved shop.EASA AD 2013-0020 AD 00This Document SUPERSEDES 2013-0020/AD Rev.00This Document has been SUPERSEDED BY 2013-0020/AD Rev.02Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 372/429

Document-Number Type Rev Compliance A|C Subject Status2013-0020 AD 02 MANDATORY COMP SAFETY BELTS / TORSO RESTRAINT SYSTEMS - INSP/REPLACEMENT Superseded (Not Applicable)


Ref AD:


NAS Action:Review of applicable maintenance records (RO at logistic dep) showsthat the seat belts are maintained at approved shop.EASA AD 2013-0020EASA AD 2013-0020EASA AD 2013-0020

ADADAD

000102

This Document SUPERSEDES 2013-0020/AD Rev.01This Document has been SUPERSEDED BY 2013-0020/AD Rev.03Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

2013-0020/AD* Rev.02 SAFETY BELTS / TORSO RESTRAINT SYSTEMS - INSP/REPLACEMENT Not Applicable





23.Oct.2014Page 373/429

Document-Number Type Rev Compliance A|C Subject StatusThis Document SUPERSEDES 2013-0020/AD Rev.01This Document has been SUPERSEDED BY 2013-0020/AD Rev.03Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed

2013-01-03 AD 00 MANDATORY A/C COMMUNICATIONS - PASCOMMUNICATIONS - PASSENGER ENTERTAINMENT AUDIOENTERTAINMENT MULTIPLEXER POWER RELAY WIRING CHANGE

Not Applicable

Not applicable to NAS due to no affected SN2013-01-03/AD Rev.00 COMMUNICATIONS - PASCOMMUNICATIONS - PASSENGER ENTERTAINMENT AUDIO

ENTERTAINMENT MULTIPLEXER POWER RELAY WIRING CHANGENot Applicable

> 737-23-1302/SB* Rev.00 COMMUNICATIONS - PASSENGER ENTERTAINMENT SYSTEM - AUDIOENTERTAINMENT MULTIPLEXER POWER RELAY WIRING CHANGE






23.Oct.2014Page 374/429

Document-Number Type Rev Compliance A|C Subject Status2013-02-02 AD 00 MANDATORY COMP HPT DISKS MANUF. BY GLOBAL MATERIAL SOLUTIONS OF PRATT & WHITNEY -

REMOVAL FROM SERVICE OFNot Applicable / Special Text:Global Material of Pratt & Whitneynot inst in NAS fleet

Comply with this AD within the compliance times specified, unlessalready done.(1) For CFM56-3, CFM56-3B, and CFM56-3C turbofan engines operating to20,100 lbs maximum takeoff (MTO) thrust, remove the HPT disk fromservice on or before accumulating 8,000 cycles-since-new (CSN).(2) For CFM56-3B and CFM56-3C turbofan engines operating to 22,100lbs MTO thrust, remove the HPT disk from service on or beforeaccumulating 8,000 CSN.(3) For CFM56-3C turbofan engines operating to 23,500 lbs MTO thrust,remove the HPT disk from service on or before accumulating 4,000 CSN.(4) For HPT disks that have been used in multiple models or thrustinstallations, the formula in the ADDED DATA section of Pratt &Whitney Special Instruction 6F-12 dated December 21, 2012 must beused to calculate the remaining life on the disk.Affected Rotables (Part No/Serial No/Position) Status

CFM56-3B2 / 725495 Pos=RH (KKM)Not Applicable / Special Text: GlobalMaterial of Pratt & Whitney not inst inNAS fleet / Reason: AUTO ASSIGNED

CFM56-3B2 / 724473 Pos=LH (KKM)Not Applicable / Special Text: GlobalMaterial of Pratt & Whitney not inst inNAS fleet / Reason: AUTO ASSIGNED





23.Oct.2014Page 375/429

Document-Number Type Rev Compliance A|C Subject Status2013-04-05 AD 00 MANDATORY A/C FUSELAGE - SKIN - SKIN CRACKING UNDER THE NUMBER 3 VHF ANTENNA -

INSPECTION, REPAIR AND PREVENTIVE MODIFICATIONNot Applicable

Perform within an unlimited threshold.2013-04-05/AD Rev.00 FUSELAGE - SKIN - SKIN CRACKING UNDER THE NUMBER 3 VHF ANTENNA -

INSPECTION, REPAIR AND PREVENTIVE MODIFICATIONNot Applicable

> 737-53-1287/SB* Rev.01 FUSELAGE - SKIN - SKIN CRACKING UNDER THE NUMBER 3 VHF ANTENNA -INSPECTION, REPAIR AND PREVENTIVE MODIFICATION

Not Applicable / Special Text: ServiceBulletin not applicable for NAS fleet.

This Document SUPERSEDES 737-53-1287/SB Rev.00Reason for this StatusAUTO ASSIGNED





23.Oct.2014Page 376/429

Document-Number Type Rev Compliance A|C Subject Status2013-09-01 AD 00 MANDATORY A/C FUSELAGE, CROWN SKIN LAP JOINT INSPECTION FOR CRACKING Open / Special Text: Group 5

serialnumbersThis Document SUPERSEDES 2003-08-15/AD Rev.00Perform within an unlimited threshold.

2013-09-01/AD Rev.00 FUSELAGE, CROWN SKIN LAP JOINT INSPECTION FOR CRACKING Open / Special Text: Group 5serialnumbers

This Document SUPERSEDES 2003-08-15/AD Rev.00> 737-53A1255/SB Rev.02 FUSELAGE-SKIN-CROWN SKIN LAP JOINT-INSPECTION FOR LOWER ROW CRACKING

AT STRINGERS S-4, S-10, S-14 BETWEEN STA 360-540 AND STA 727-908Open / Special Text: Group 5serialnumbers

This Document SUPERSEDES 737-53A1255/SB Rev.01> > 737-53A1255-01/EO* Rev.00 FUSELAGE-SKIN-CROWN SKIN LAP JOINT-INSPECTION FOR LOWER ROW CRACKING

AT STRINGERS S-4, S-10, S-14 BETWEEN STA 360-540 AND STA 727-908Closed 12.Feb.2014 W/O:489216

This Document is terminated with implementation of 737-53A1255-03/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

12.Feb.2014 71572:00/H 43151/C 489216, N/AWas due at: 43445/C PerfRev.:'00' / Reason:Document terminated manually.

Reason for this StatusDocument terminated manually.

> > 737-53A1255-02/EO* Rev.00 FUSELAGE-SKIN-CROWN SKIN LAP JOINT-INSPECTION FOR LOWER ROW CRACKINGAT STRINGERS S-4, S-10, S-14 BETWEEN STA 360-540 AND STA 727-908


This Document is terminated with implementation of 737-53A1255-04/EO Rev.00> > 737-53A1255-03/EO* Rev.00 FUSELAGE-SKIN-CROWN SKIN LAP JOINT-INSPECTION FOR LOWER ROW CRACKING

AT STRINGERS S-4, S-10, S-14 BETWEEN STA 360-540 AND STA 727-908Closed 14.Feb.2014 W/O:489486

This Document terminates 737-53A1255-01/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks14.Feb.2014 71572:00/H 43151/C 489486, N/A Was due at: 45000/C PerfRev.:'00'



This Document terminates 737-53A1255-02/EO Rev.00> > 737-53A1255-05/EO* Rev.00 FUSELAGE-SKIN-CROWN SKIN LAP JOINT-INSPECTION FOR LOWER ROW CRACKING

AT STRINGERS S-4, S-10, S-14 BETWEEN STA 360-540 AND STA 727-908Open / Special Text: post EO737-53A1255-03





23.Oct.2014Page 377/429


45651/CPerform initially within (effective from13.Jun.2013) (F) 2500/C /Interval(F):2500/C







23.Oct.2014Page 378/429

Document-Number Type Rev Compliance A|C Subject Status2013-09-02 AD 00 MANDATORY A/C WINGS - TRAILING EDGE FLAP TRACK REPLACEMENT Repetitive





23.Oct.2014Page 379/429

Document-Number Type Rev Compliance A|C Subject StatusCompliance:Applicability for NAS is controlled by AD § (a)(1), all B737-100through 500.

AD §(g)through (i) is not applicable for NAS, as this § coversB737-100 and -200 via AD 2000-25-07.AD §(j)and (k) is applicable only for B737-100,-200, but(j) iscomplied with thorugh SB 737-57-1203 or production equivalent. Noinitial inspection required. §(k) is not applicable for NAS B737-300AC.AD §(l) and (m) is applicable only for B737-100,-200 thus notapplicable for NAS.AD §(n) is complied with through SB 737-57-1203 and also terminatedby performing SB 737-57A1271 Rev.:03.AD §(o) is not applicable to NAS, due to not operating B737-100,-200and incorperation of SB 737-57-1203.AD §(p)(1) through (4), §(q), §(r), §(s) and §(u) is complied withthrough SB 737-57A1271, specifically EO 737-57A1271-1.AD §(t) is complied with through SB 737-57A1271, specifically EO737-57A1271-2.AD §(v) requires us to use AD §(y) to obtain a repair instructions.We must apply for an AMOC.AD §(w)is complied with through an entry in AMOS Suspicious Partsmodule.AD §(x) is not used by NAS, as we control the airworthiness throughSB 737-57A1271 Rev.:03.

NOTEAD does not have a single compliance time, but is a function ofseveral underlying documents and their compliance times. But AD §(q)(2) value is used a single entry.





23.Oct.2014Page 380/429

Document-Number Type Rev Compliance A|C Subject Status2002-05-07737-57-1203737-57A1271737-57A1271-1737-57A1271-2

ADSBSBEOEO

0005030101

This Document SUPERSEDES 2002-05-07/AD Rev.00Perform WITHIN 180/D (effective from 13.Jun.2013)

2013-09-02/AD Rev.00 WINGS - TRAILING EDGE FLAP TRACK REPLACEMENT RepetitiveThis Document SUPERSEDES 2002-05-07/AD Rev.00

> 737-57-1203/SB* Rev.05 *AD* WINGS - TRAILING EDGE FLAP TRACK REPLACEMENT Closed 15.Jan.1995Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

15.Jan.1995PerfRev.:'NOTE' / Reason: DELIVERYDOC.


> 737-57A1271/SB Rev.03 WINGS - TRAILING EDGE AND TRAILING EDGE DEVICES - TRAILING EDGE FLAPSOUTBOARD FLAP, INBOARD TRACK INSPECTION/OVERHAUL/REPLACEMENT

Repetitive

This Document SUPERSEDES 737-57A1271/SB Rev.02> > 737-57A1271-1/EO* Rev.01 OUTB. TRAILING EDGE FLAPS, INB. TRACK INSPECTION AT WB 254 INSTR FOR VISUAL

AND EDDY CURRENT INSP. FLAP TRACKS (APP TO #2&#7)Repetitive


65C34812-6 / E-2487 Pos=#2 (KKM)

Repetitive / Next Due:22.Jan.2018 10000/C/ Last Performed:22.Jan.2014RefDocument:FORM 8130-3 026156Rev.01

65C34812-6 / E-3004 Pos=#7 (KKM)Repetitive / Next Due:21.Jan.2018 10000/C/ Last Performed:22.Jan.2014RefDocument:N/A Rev.01

> > 737-57A1271-2/EO* Rev.01 OUTB TRAILING EDGE FLAPS, INB TRACK,OVERHAUL/REPLM. AT WBL 254 RepetitiveAffected Rotables (Part No/Serial No/Position) Status





23.Oct.2014Page 381/429


65C34812-6 / E-2487 Pos=#2 (KKM)

Repetitive / Next Due:20.Jan.2022 20000/C/ Last Performed:22.Jan.2014 0/CRefDocument:FORM 8130-3 026156Rev.01

65C34812-6 / E-3004 Pos=#7 (KKM)Repetitive / Next Due:21.Jan.2022 20000/C/ Last Performed:22.Jan.2014 0/CRefDocument:FAA FORM 026155 Rev.01

> > 737-57A1271-3/EO* Rev.00 OUTB. TRAILING EDGE FLAPS, INB. TRACK INSPECTION AT WB 254 INSTR FOR VISUALAND EDDY CURRENT INSP. FLAP TRACKS (APP TO #2&#7)

Not Applicable


65C34812-6 / E-3004 Pos=#7 (KKM)

Not Applicable / Reason: AD §(Q)ALLOWS FOR LATE INITIALINSPECTION, NAS USECONSERVATIVE §(U)

65C34812-6 / E-2487 Pos=#2 (KKM)

Not Applicable / Reason: AD §(Q)ALLOWS FOR LATE INITIALINSPECTION, NAS USECONSERVATIVE §(U)





23.Oct.2014Page 382/429

Document-Number Type Rev Compliance A|C Subject Status2013-09-08 AD 00 MANDATORY A/C FUEL - ENGINE FUEL FEED SYSTEM - ENGINE FUEL SUCTION FEED OPERATIONAL

TESTRepetitive

Effectivity:This Document is effective for All B737-300,-400,-500 Aircraft.

Compliance:AD § (g) is complied with through SB 737-28A1307 rev.:00,specifically throughEO 737-28A1307-01: Covers testing of LH engineEO 737-28A1307-02: Covers Testing of RH engine

NOTEThis recent release of the Ref AD contains a typographical errorregarding a reference to SB 737-28A1407. The correct reference is theSB 737-28A1307. The FAA is aware of the issue and is in the processof correcting the error through the Office of the Federal Register.See the attachment of the AD that highlights the two locations of thetypographical error, along with comments that contain the correctreference.2007-NM-351-AD737-28A1307737-28A1307-01737-28A1307-02737-FTD-28-04001

NPRMSBEOEOFTD

0000000000

Perform WITHIN 7500/H (effective from 18.Jun.2013)Perform WITHIN 730/D (effective from 18.Jun.2013)

2013-09-08/AD Rev.00 FUEL - ENGINE FUEL FEED SYSTEM - ENGINE FUEL SUCTION FEED OPERATIONALTEST

Repetitive

> 737-28A1307/SB Rev.00 FUEL - ENGINE FUEL FEED SYSTEM - ENGINE FUEL SUCTION FEED OPERATIONALTEST

Repetitive





23.Oct.2014Page 383/429

Document-Number Type Rev Compliance A|C Subject Status> > 737-28A1307-01/EO* Rev.00 FUEL - ENGINE FUEL FEED SYSTEM - LH ENGINE FUEL SUCTION FEED OPERATIONAL

TESTRepetitive


22.Feb.2016 79072:00/HPerform initially within (effective from14.May.2012) (F) 720/D or 7500/H /Interval(F):720/D or 7500/H


04.Mar.2014 71572:00/H 43151/C 489226, N/AWas due at: 04.May.2014 and 4456560/HPerfRev.:'00'

> > 737-28A1307-02/EO* Rev.00 FUEL - ENGINE FUEL FEED SYSTEM - RH ENGINE FUEL SUCTION FEED OPERATIONALTEST

Repetitive


22.Feb.2016 79072:00/HPerform initially within (effective from14.May.2012) (F) 720/D or 7500/H /Interval(F):720/D or 7500/H


04.Mar.2014 71572:00/H 43151/C 489227, N/AWas due at: 04.May.2014 and 4456560/HPerfRev.:'00'





23.Oct.2014Page 384/429

Document-Number Type Rev Compliance A|C Subject Status2013-09-10 AD 00 MANDATORY A/C DOORS - FORWARD CARGO - LOWER FORWARD AND AFT CORNER INSPECTION

MODIFICATION AND REPLACEMENTOpen

This AD supersedes AD 2000-07-06, Amendment 39-11660 (65 FR 19302,April 11, 2000).

This AD applies to all The Boeing Company Model 737-100, -200, -200C,-300, -400, and - 500 series airplanes, certificated in any category.

§ 39.13 [Amended]2. The FAA amends § 39.13 by removing airworthiness directive (AD)2000-07-06, Amendment 39-11660 (65 FR 19302, April 11, 2000), andadding the following new AD:

2013-09-10 The Boeing Company: Amendment 39-17452; Docket No.FAA-2012-0855; Directorate Identifier 2011-NM-136-AD.

Compliance:AD § 39.13 is complied with through SB 737-52A1100 rev 05.Cargo Door modification pr:EO 737-52A1100-01 - *AD* FWD CARGO DOORS, LOWER FWD/AFT CORNERMOD/REPL.737-52A1100 SB 04This Document SUPERSEDES 2000-07-06/AD Rev.00Perform within an unlimited threshold.

2013-09-10/AD Rev.00 DOORS - FORWARD CARGO - LOWER FORWARD AND AFT CORNER INSPECTIONMODIFICATION AND REPLACEMENT

Open

This Document SUPERSEDES 2000-07-06/AD Rev.00> 737-52A1100/SB Rev.05 *AD* FWD CARGO DOORS, LOWER FWD/AFT CORNER INSP MOD/REPL. Open> > 737-52A1100-01/EO* Rev.05 *AD* FWD CARGO DOORS, LOWER FWD/AFT CORNER MOD/REPL. See prev. Docstatus

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks08.Mar.2005 46130:00/H 23575/C PerfRev.:'NOTE'





23.Oct.2014Page 385/429

Document-Number Type Rev Compliance A|C Subject StatusReason for this StatusKKM 150399 ITEM: 1

> > 737-52A1100-02/EO* Rev.00 FWD CARGO DOORS, LOWER FWD AND AFT CORNER INSPECTION. PART V -SUPPLEMENTAL STRUCTURAL INSPECTIONS.

Open / Special Text: Additional workper SB Rev.5, EO not amended by AD2013-09-10


46328/CPerform initially within (effective from28.Jun.2013) (F) 4500/C /Interval(F):4500/C

> 737-52A1100/SB Rev.04 *AD* FWD CARGO DOORS, LOWER FWD/AFT CORNER INSP MOD/REPL. Closed 08.Mar.2005> > 737-52A1100/EO* Rev.04 *AD* FWD CARGO DOORS, LOWER FWD AND AFT CORNER INSP, MOD AN Not Applicable by Serial Number

This Document is terminated with implementation of 737-52A1100-01/EO Rev.04> > 737-52A1100-01/EO* Rev.04 *AD* FWD CARGO DOORS, LOWER FWD/AFT CORNER INSP MOD/REPL. Closed 08.Mar.2005

This Document terminates 737-52A1100/EO Rev.04Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks







23.Oct.2014Page 386/429

Document-Number Type Rev Compliance A|C Subject Status2013-13-12 AD 00 MANDATORY A/C DOORS - AFT CARGO - FRAME AND BEAM INSPECTION, REPAIR AND MODIFICATION Open / Special Text: Repetive insp

per EO 737-52A1153-01 and -10. -10not mandated by AD

This AD applies to the aft cargo door of 737-300, all serial numbers.

Paragraph (h), (i), (j), (k), (l), (m) & (n) restates AD 2000-06-13 R1and is coverd by SB 737-52A1079 R7 wich is N/A to NSB fleet.

Paragraph (o) states: identify aft cargodoor and is covered by SB737-52A1153 (EO 737-52A1153-01)

Paragraph (p), (q) and (r): Refers to paragraph (o) and includescargo doors as applicable to SB 737-52A1079 R7.

Paragraph (s) & (t) requires accomplishment of SB 737-52A1153 & SB737-52-1154 R1.

The aft cargo door applicable P/N`s for SB 737-52A1079 R7 is also setup as suspicious parts, to highlight this AD at receiving, in the(unlikely) event of said cargo doors are to be ordered.737-52-1154737-52A1079737-52A1153

SBSBSB

010700


2013-13-12/AD Rev.00 DOORS - AFT CARGO - FRAME AND BEAM INSPECTION, REPAIR AND MODIFICATION Open / Special Text: Repetive insp perEO 737-52A1153-01 and -10. -10 notmandated by AD

This Document SUPERSEDES 2000-06-13/AD Rev.01> 737-52-1154/SB Rev.02 DOORS - CARGO COMPARTMENT DOORS - AFT CARGO DOOR - CROSS BEAM INSP. On Attrition






23.Oct.2014Page 387/429

Document-Number Type Rev Compliance A|C Subject Status> > 737-52-1154-01/EO* Rev.01 AFT CARGO DOOR - CROSS BEAM D, INSPECTION On Attrition

This Document SUPERSEDES 737-52-1154-01/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition / NO LIMIT

> > 737-52-1154-02/EO* Rev.00 AFT CARGO DOOR - CROSS BEAM D, FORWARD END REPAIR On AttritionAffected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition

> > 737-52-1154-03/EO* Rev.00 AFT CARGO DOOR - CROSS BEAM D, AFT END REPAIR On AttritionAffected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition

> > 737-52-1154-04/EO* Rev.00 AFT CARGO DOOR - CROSS BEAM D, REPETITIVE INSPECTION AFTER REPAIR On AttritionAffected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition

> 737-52A1079/SB* Rev.07 DOORS - AFT CARGO - FRAME AND BEAM INSPECTION, REPAIR AND MODIFICATION Not Applicable by Serial NumberThis Document SUPERSEDES 737-52A1079/SB Rev.00

> 737-52A1153/SB Rev.01 DOORS - AFT CARGO - CROSS BEAM E, ADJACENT LOWER CORNER FRAMES ANDREINFORCING ANGLES - INSPECTION, REPAIR AND MODIFICATION

Open

This Document SUPERSEDES 737-52A1153/SB Rev.00> > 737-52A1153-01/EO* Rev.03 AFT CARGO DOOR - CROSS BEAM E, ADJACENT LOWER CORNER FRAMES AND

REINFORCING ANGLES - INSPECTION.Open

This Document SUPERSEDES 737-52A1153-01/EO Rev.02This Document is terminated with implementation of 737-52A1153-02/EO Rev.01Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) Open / Next Due: 42971/C

> > 737-52A1153-02/EO* Rev.01 AFT CARGO DOOR - CROSS BEAM E, PREVENTATIVE MOD TO BOTH ENDS, ANDLOWER CORNER FRAME TERMINATING INSPECTION

Open

This Document terminates 737-52A1153-01/EO Rev.03This Document SUPERSEDES 737-52A1153-02/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) Open / Next Due:09.Sep.2017 46633/C

> > 737-52A1153-03/EO* Rev.01 AFT CARGO DOOR - CROSS BEAM E, FORWARD END REPAIR On Attrition





23.Oct.2014Page 388/429

Document-Number Type Rev Compliance A|C Subject StatusThis Document SUPERSEDES 737-52A1153-03/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status

65-47952-337 / 001649 Pos=AFT (KKM)On Attrition / Reason: To be performed ifcracks are found on EO-01

> > 737-52A1153-04/EO* Rev.01 AFT CARGO DOOR - CROSS BEAM E, AFT END REPAIR On AttritionThis Document SUPERSEDES 737-52A1153-04/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition

> > 737-52A1153-05/EO* Rev.01 AFT CARGO DOOR - FORWARD LOWER CORNER FRAME AND REINFORCING ANGLES -REPLACEMENT

On Attrition

This Document SUPERSEDES 737-52A1153-05/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition

> > 737-52A1153-06/EO* Rev.01 AFT CARGO DOOR - AFT LOWER CORNER FRAME AND REINFORCING ANGLES -REPLACEMENT

On Attrition

This Document SUPERSEDES 737-52A1153-06/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status65-47952-337 / 001649 Pos=AFT (KKM) On Attrition

> > 737-52A1153-10/EO* Rev.02 SUPPLEMENTAL STRUCTURAL INSPECTIONS, AFT CARGO DOOR - CROSS BEAM EAND ADJACENT LOWER CORNER FRAMES AND ANGLES.

Event-Triggered

This Document SUPERSEDES 737-52A1153-10/EO Rev.01Affected Rotables (Part No/Serial No/Position) Status

65-47952-337 / 001649 Pos=AFT (KKM)Event-Triggered / Reason: To be performed4500 CY after rep or preventative mod /Last Performed: RefDocument:





23.Oct.2014Page 389/429

Document-Number Type Rev Compliance A|C Subject Status2013-13-15 AD 00 MANDATORY A/C FUEL - INTEGRAL FUEL TANKS - ACCESS DOOR INSPECTION/REPLACEMENT Not Applicable

Compliance:AD § (g) is complied with through SB 737-28-1286AD § (f) is complied with through NAS AMP for the B737CL. 57-AWL-01is Not Applicable to the current NAS Fleet due to LN#.737-28-1286 SB 00

2013-13-15/AD Rev.00 FUEL - INTEGRAL FUEL TANKS - ACCESS DOOR INSPECTION/REPLACEMENT Not Applicable> 737-28-1286/SB* Rev.00 FUEL - INTEGRAL FUEL TANKS - ACCESS DOOR INSPECTION/REPLACEMENT Not Applicable by Serial Number





23.Oct.2014Page 390/429

Document-Number Type Rev Compliance A|C Subject Status2013-15-14 AD 00 MANDATORY A/C LE SLATS, MAIN TRACK DOWNSTOP ASSEMBLY INSPECTION Open

Compliance:AD § (g) is complied with through EO 737-57A1301-02.(Already in compliance as of AD issue date.)AD § (h) is complied with through EO 737-57A1301-03.(Already in compliance as of AD issue date.)AD § (i) is complied with through EO 737-57A1301-01. NAS does not usethe option to extend the due date to 72months/15000FC from ADeffective date, but opts to use SB effective date.

General Note on due date. As the due date is a function of the 3 EOsbelow, no due date is defined on the AD.

General Note on compliance: NAS incorperated Rev.:03 of SB737-57A1301 as soon as it was released, in Feb 8th 2008.2011-NM-071-AD737-57A1301737-57A1301737-57A1301737-57A1301737-57A1301 IN-01737-SRP-57-0208 (REF)

NPRMSBSBSBSBSBSRP

000001020300


2013-15-14/AD Rev.00 LE SLATS, MAIN TRACK DOWNSTOP ASSEMBLY INSPECTION OpenThis Document SUPERSEDES 2008-06-29/AD Rev.00

> 737-57A1301/SB Rev.03 WINGS - FLIGHT SURFACES - LEADING EDGE SLATS - MAIN TRACK DOWNSTOPASSEMBLY INSPECTION AND MODIFICATION

Open

This Document SUPERSEDES 737-57A1301/SB Rev.02> > 737-57A1301-01/EO* Rev.01 LE SLATS, MAIN TRACK DOWNSTOP ASSEMBLY MODIFICATION Open






23.Oct.2014Page 391/429


19.Sep.2019 57386/CPerform initially within (effective from20.Sep.2013) (F) 15000/C or 2190/D

> > 737-57A1301-02/EO* Rev.00 LE SLATS, MAIN TRACK DOWNSTOP ASSEMBLY INSPECTION RepetitiveThis Document SUPERSEDES 737-57A1301/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document



> > 737-57A1301-03/EO* Rev.00 LE SLATS, MAIN TRACK DOWNSTOP ASSEMBLY DET INSPECTION FOR FOD Closed 01.Nov.2012 W/O:273638Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks01.Nov.2012 68139:00/H 40570/C 273638, N/A Was due at: 31.Jul.2013 PerfRev.:'00'





23.Oct.2014Page 392/429

Document-Number Type Rev Compliance A|C Subject Status2013-18-08 AD 00 MANDATORY A/C FUSELAGE - SKIN - FUSELAGE SKIN CHEM-MILL LINE CRACK INSP AND REP Open





23.Oct.2014Page 393/429

Document-Number Type Rev Compliance A|C Subject StatusApplicable to:

LN-KKN (Group 9 in SB 737-53A1210 Rev.3)LN-KKW and LN-KKM. (Group 14 in SB 737-53A1210 Rev.3)

Paragraph (g)is superseeded by paragraph (p)

Paragraph (h)is superseeded by paragraph (s)

Paragraph (i) is covered by 737-53A1210-P7

Paragraph (j) is covered by 737-53A1210-P5 and -P6

Paragraph (k) is covered by 737-53A1210-P5 and -P6

Paragraph (L) is covered by the report back-message in 737-53A1210-P5and -P6

Paragraph (m) is N/A for current NAS-fleet as of effectivity date ofthis AD.

Paragraph (n) is N/A for current NAS-fleet as of effectivity date ofthis AD.

Paragraph (o) This is an optional exception that NAS has chosen todisregard.

Paragraph (p) is covered by 737-53A1210-P1

Paragraph (q) is N/A for current NAS-fleet as of effectivity date ofthis AD.





23.Oct.2014Page 394/429


Paragraph (r)is covered by 737-53A1210-P3

Paragraph (s)is covered by 737-53A1210-P4

Paragraph (t) is N/A for current NAS-fleet as of effectivity date ofthis AD.

Paragraph (u)is covered by 737-53A1210-P2.737-53A1210 SB 03This Document SUPERSEDES 2004-18-06/AD Rev.00Perform within an unlimited threshold.

2013-18-08/AD Rev.00 FUSELAGE - SKIN - FUSELAGE SKIN CHEM-MILL LINE CRACK INSP AND REP OpenThis Document SUPERSEDES 2004-18-06/AD Rev.00

> 737-53A1210/SB Rev.03 *AD* FUSELAGE SKIN CHEM-MILL LINE CRACK INSPECTION/REPAIR Open> > 737-53A1210-P1/EO* Rev.03 *AD* FUSELAGE SKIN - CROWN AREA SKIN INSPECTION Repetitive




> > 737-53A1210-P2/EO* Rev.03 *AD* FUSELAGE SKIN - WINDOW BELT INSPECTION RepetitiveDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

44951/C Interval(F):1800/CPerf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks07.Feb.2014 71572:00/H 43151/C 489232, N/A Was due at: 44372/C PerfRev.:'03'

> > 737-53A1210-P3/EO* Rev.03 *AD* FUSELAGE SKIN CHEM-MILL LINE- VERTICAL CRACK INSP RepetitiveNOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document





23.Oct.2014Page 395/429


44951/CPerform initially before(L) 55000/H Performinitially within (effective from 06.Nov.2013)(L) 1800/C or 55000/C / Interval(F):1800/C


> > 737-53A1210-P4/EO* Rev.03 *AD* FUSELAGE SKIN CHEM-MILL LINE - LOWER LOBE AREA SECTION 41 -INSPECTION.

Repetitive




> > 737-53A1210-P5/EO* Rev.00 *AD* FUSELAGE SKIN - PERMANENT REPAIR On Attrition> > 737-53A1210-P6/EO* Rev.00 *AD* FUSELAGE SKIN - TIME LIMITED REPAIR On Attrition> > 737-53A1210P7/EO* Rev.03 PREVENTIVE MOD: FUSELAGE SKIN CHEM-MILL LINE CRACK AFFECTS AREA AT

BS500D - BS520.Not Applicable by Serial Number





23.Oct.2014Page 396/429

Document-Number Type Rev Compliance A|C Subject Status2013-18-09 AD 00 MANDATORY COMP EMERGENCY LOCATOR TRANSMITTER - BATTERY WIRING INSTALLATION

DISCREPANCIESSuperseded (Closed 02.Aug.2013W/O:459439)

Compliance:AD § (k)(ii)For The Boeing Company Model 737-600, -700, -700C, -800, -900, and-900ER series airplanes: Boeing Multi Operator MessageMOM-MOM-13-0593-01B, dated July 28, 2013.1152682-23-A2213-107513-1075

SBTDTD

010001

This Document has been SUPERSEDED BY 2014-17-02/AD Rev.0Perform BEFORE 31.Jan.2014

2013-18-09/AD Rev.00 EMERGENCY LOCATOR TRANSMITTER - BATTERY WIRING INSTALLATIONDISCREPANCIES

Closed 02.Aug.2013 W/O:459439

This Document has been SUPERSEDED BY 2014-17-02/AD Rev.0> 13-1075/TD* Rev.00 INSPECT ELT BATTERY, BATTERY WIRING, AND ELT TO BATTERY WIRING Closed 02.Aug.2013 W/O:459439

This Document has been SUPERSEDED BY 13-1075/TD Rev.01Affected Rotables (Part No/Serial No/Position) Status

1152682-1 / 072C-256 Pos=AFT (KKM)Closed / Last Performed:02.Aug.201326536:00/H 20636/C W/O:459439 Rev.00

> 13-1075/TD* Rev.01 INSPECT ELT BATTERY, BATTERY WIRING, AND ELT TO BATTERY WIRING See prev. DocstatusThis Document SUPERSEDES 13-1075/TD Rev.00Affected Rotables (Part No/Serial No/Position) Status1152682-1 / 072C-256 Pos=AFT (KKM) See prev. Docstatus / Reason: .





23.Oct.2014Page 397/429

Document-Number Type Rev Compliance A|C Subject Status2013-24-13 AD 00 MANDATORY A/C AD - FUSELAGE - PASSENGER CABIN FLOORS - STATION 520 TO 540 - SEAT TRACK

LINK ASSEMBLIESOpen

Perform within an unlimited threshold.2013-24-13/AD Rev.00 AD - FUSELAGE - PASSENGER CABIN FLOORS - STATION 520 TO 540 - SEAT TRACK

LINK ASSEMBLIESOpen

> 737-53-1260/SB Rev.01 FUSELAGE - PASSENGER CABIN FLOORS - STATION 520 TO 540 - SEAT TRACK LINKASSEMBLIES - REPLACEMENT/MODIFICATION

Open

This Document SUPERSEDES 737-53-1260/SB Rev.00> > 737-53-1260-01/EO* Rev.00 FUSELAGE - PASSENGER CABIN FLOORS - STATION 520 TO 540 - SEAT TRACK LINK

ASSEMBLIES - REPLACEMENT/MODIFICATIONOpen


06.Jan.2019Perform initially within (effective from07.Jan.2014) (F) 1825/D

2013-25-05 AD 00 MANDATORY A/C FUEL - ENGINE FUEL FEED SYSTEM - FUEL PUMP CONTROL GROUND FAULTINTERRUPTER (GFI) RELAY INSTALLATION

Not Applicable / Special Text: NASonly opearates AC in group 2 and 4.

This AD is only applicable to AC in group 5,6,7,9 Config 1 and 2.NAN only operated AC in Group 2 and 4.2009-NM-228-AD2011-12-0965-49808-24-01 (ACTIVE)737-28A1212737-28A1212737-28A1212NAS-2841-002 (AWL TASK)PRR35440-10RS

NPRMADSBSBSBSBTAPRR

0000

0001020000






23.Oct.2014Page 398/429

Document-Number Type Rev Compliance A|C Subject Status2013-26-01 AD 00 MANDATORY COMP ACCESSORY GEARBOX (AGB) - CFM56-3 AND CFM56-7B SERIES TURBOFAN ENGINES On Attrition

Perform an Independent Inspection to verify re-installation of theAGB handcranking pad cover after any maintenance that involves theremoval and re-installation of the AGB handcranking cover.2013-26-01-012013-26-01-027B-72-05647B-72-0879

EOEOSBSB

00000001

Perform within an unlimited threshold.2013-26-01/AD Rev.00 ACCESSORY GEARBOX (AGB) - CFM56-3 AND CFM56-7B SERIES TURBOFAN ENGINES On Attrition> 2013-26-01-01/EO Rev.00 ACCESSORY GEARBOX (AGB) - CFM56-3 SERIES TURBOFAN ENGINES On Attrition> > 3-72-1129/SB* Rev.03 ACCESSORY GEARBOX ASSEMBLY (AGB) WITH A NEW STARTER DRIVE PAD AND NEW

HANDCRANKING COVER AND REWORK OF OLD AGB TO THE NEW ONEOn Attrition

Affected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 725495 Pos=RH (KKM) On Attrition / Reason: AUTO ASSIGNEDCFM56-3B2 / 724473 Pos=LH (KKM) On Attrition / Reason: AUTO ASSIGNED





23.Oct.2014Page 399/429

Document-Number Type Rev Compliance A|C Subject Status2014-01-05 AD R0 MANDATORY A/C FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 & BS 908, S-10L TO S-10R Open

This AD is controlled by SB 737-53A1322Perform within an unlimited threshold.

2014-01-05/AD Rev.R0 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 & BS 908, S-10L TO S-10R Open> 737-53A1322/SB Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 & BS 908, S-10L TO S-10R -

INSPECTION AND REPLACEMENTOpen

> > 737-53A1322-01/EO* Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 & BS 908, S-10L TO S-10R -INITIAL INSPECTION

Open

NOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentNOTE: 'Whichever comes later' calculation logic applicable for the intervalDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

50000/CPerform initially before(L) 50000/C Performinitially within (effective from 14.Mar.2014)(L) 5000/C

> > 737-53A1322-02/EO* Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 S-5L TO S-3L, S-3R TOS-5R - REPETETIVE INSPECTION

Postponed (open) / Special Text: PostEO 737-53A1322-01

Reason for this StatusTO BE TRIGGERD WHEN EO 737-53A1322-01 IS POST

> > 737-53A1322-03/EO* Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 908 S-5L TO S-3L, S-3R TOS-5R - REPETETIVE INSPECTION



> > 737-53A1322-04/EO* Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 & BS 908 S-10L TO S-5L,S-3L TO S-3R, S-5R TO S-10R - REPETETIVE INSPECTION



> > 737-53A1322-05/EO* Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 AND 908 S-5L TO S-3L,S-3R TO S-5R - FASTENER REMOVAL AND REINSTALLATION

On Attrition

> > 737-53A1322-06/EO* Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 - STRINGER SPLICEREMOVAL AND REPLACEMENT

On Attrition





23.Oct.2014Page 400/429

Document-Number Type Rev Compliance A|C Subject Status> > 737-53A1322-07/EO* Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 908 - STRINGER SPLICE

REMOVAL AND REPLACEMENTOn Attrition

> > 737-53A1322-08/EO* Rev.00 FUSELAGE - STRINGER SPLICES AND BUTT STRAPS AT BS 360 & BS 908 - POSTSTRINGER SPLICE REMOVAL AND REPLACEMENT - INSPECTION

On Attrition / Special Text: post EO737-53A1322-06 and/or737-53A1322-07





23.Oct.2014Page 401/429

Document-Number Type Rev Compliance A|C Subject Status2014-0142 AD 01 MANDATORY COMP OXYGEN - OXYGEN MASK REGULATOR INFLATABLE HARNESS / INFLATION HOSE -

IDENTIFICATION / REPLACEMENTNot Applicable

EASA AD requires the inspection of crew oxygen masks perZodiac Aerospace SB MC10-35-274R01.

None of the applicable PN in use in NAS/NAN.

Revision 1 of AD 2014-0142 only adds affected part numbers to theapplicability in the AD. The SB MC10-35-274R01 already stated correctapplicability in the first place (also mandated by AD 2014-0142R00),hence, there are still no applicable PN.

All Mask PN stated in SB MC10-35-274R01 is added with warning insuspicious parts APN: 4642014-01422014-0142

ADAD

0001

This Document SUPERSEDES 2014-0142/AD Rev.00Perform within an unlimited threshold.

2014-0142/AD Rev.01 OXYGEN - OXYGEN MASK REGULATOR INFLATABLE HARNESS / INFLATION HOSE -IDENTIFICATION / REPLACEMENT

Not Applicable

This Document SUPERSEDES 2014-0142/AD Rev.00> MC10-35-274/SB* Rev.01 OXYGEN - HARNESS ASSEMBLY - INSPECTION FOR POTENTIAL DEFECTIVE

COMPONENTNot Applicable

This Document SUPERSEDES MC10-35-274/SB Rev.00Affected Rotables (Part No/Serial No/Position) StatusNo affected rotable installed





23.Oct.2014Page 402/429

Document-Number Type Rev Compliance A|C Subject Status2014-0142 AD 00 MANDATORY COMP OXYGEN - OXYGEN MASK REGULATOR INFLATABLE HARNESS / INFLATION HOSE -

IDENTIFICATION / REPLACEMENTSuperseded (Not Applicable)

EASA AD requires the inspection of crew oxygen masks perZodiac Aerospace SB MC10-35-274.

None of the applicable PN in use in NAS2014-0142 AD 00This Document has been SUPERSEDED BY 2014-0142/AD Rev.01





23.Oct.2014Page 403/429

Document-Number Type Rev Compliance A|C Subject Status2014-03-06 AD 00 RECOMMENDED A/C WINGS - LANDING GEAR SUPPORT BEAM - REAR SPAR AND AFT SUPPORT FITTING Superseded (Superseded)

Applicable to all B737CL.

Compliance:AD §(f) is complied with through EO detailed below.AD §(g) is NA to NAS as we do not operate Group 1 AC (737-100/200)AD §(h) Group 2-7 AC inspections are complied with through EOdetailed below.

NAS only has aircraft in Group 6, Config 2 and Group 7.The SB is divided into 2 EO:737-57-1318-01: Group 6 Config 2 AC.737-57-1318-02: Group 6 Config 2 AC.737-57-1318-03: Group 7737-57-1318-04: Group 7737-57-1318-05: Group 7 AC.MSN:29072 with MLG drop May 2015.

No time limit on AD, as the time limit is differentiated, refer to EOfor time limits.120S-14-2512013-NM-131-AD2014-12-13737-57-1216737-57-1318-01737-57-1318-02737-57-1318-03737-57-1318-04737-57-1318-05

AMOCNPRMADSBEOEOEOEOEO

000000020000000000






23.Oct.2014Page 404/429

Document-Number Type Rev Compliance A|C Subject Status2014-04-05 AD 00 MANDATORY A/C AIR CONDITIONING - CONTROL CABIN CONDITIONED AIR DISTRIBUTION SYSTEM -

REMOVAL OF METAL CLAMP INST. ON HOSES TO THE AC TEMPERATURE SENSORClosed 08.Apr.2014 W/O:556884

All NAS AC performed iaw SB 737-21-1186

EO 737-21-1186-01 created to remove all metal clamps, ref AD (g)(1)2013-NM-125-ADAD 2014-04-05AMM 21-22-09, 25-11-21BOEING 737-21-1186IN01BOEING SRP 737-SRP-21-0186SAFO13006SWPM 20-10-11, 12, 13, 19

NPRMADAMMSBSRPSIBSWPM

000000IN01000000

Perform BEFORE 01.Apr.20192014-04-05/AD Rev.00 AIR CONDITIONING - CONTROL CABIN CONDITIONED AIR DISTRIBUTION SYSTEM -

REMOVAL OF METAL CLAMP INST. ON HOSES TO THE AC TEMPERATURE SENSORClosed 08.Apr.2014 W/O:556884

> 737-21-1186/SB* Rev.00 AIR CONDITIONING - CONTROL CABIN CONDITIONED AIR DISTRIBUTION SYSTEM -INSP OF METAL CLAMP INST. ON HOSES TO THE AC TEMPERATURE SENSOR

Closed 08.Apr.2014 W/O:556884

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks25.Apr.2013 69256:00/H 41420/C 431232, N/A Was due at: 31.May.2013 PerfRev.:'00'

> > 737-21-1186-01/EO* Rev.00 AIR CONDITIONING - CONTROL CABIN CONDITIONED AIR DISTRIBUTION SYSTEM -REMOVAL OF METAL CLAMP INST. ON HOSES TO THE AC TEMPERATURE SENSOR

Closed 08.Apr.2014 W/O:556884

Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks08.Apr.2014 71829:00/H 43364/C 556884, Was due at: 01.Jun.2014 PerfRev.:'00'





23.Oct.2014Page 405/429

Document-Number Type Rev Compliance A|C Subject Status2014-05-02 AD R0 MANDATORY A/C FUSELAGE - FUSELAGE AFT PRESSURE BULKHEAD INSPECTION MODIFICATION, AND

REPAIRSuperseded (Repetitive)

Paragraph (g): N/A, Applic to L/N 1-929 only.

Paragraph (h): N/A, Applic to L/N 1-929 only.

Paragraph (i): N/A, Applic to L/N 1-929 only.

Paragraph (j): N/A, Applic to L/N 1-929 only.

Paragraph (k)(3):Perf earlier per AD 2002-10-11 par (e)(3)737-53A1075/EO

Paragraph (l)(2): Covered by 737-53A1075-01/EO (Restatement of AD2002-10-11 par (f))Note: interval lowered from 4y to 2y/120days aftereff date whichever occurs later.

Paragraph (m)(2): Covered by 737-53A1075-01/EO.

Paragraph (n): New requirement,(Fig 2 step 1-6). Covered by737-53A1075-01/EO, step D.

Paragraph (o): Optional to (l)(2)Insp from Aft side only. NOT CHOSEN!

Paragraph (p): SB 737-53A1075, Fig.3 removed from EO. Engineeringmust be contacted if findings.This Document SUPERSEDES 2002-10-11/AD Rev.00This Document has been SUPERSEDED BY 2014-18-02/AD Rev.00Perform within an unlimited threshold.

2014-05-02/AD Rev.R0 FUSELAGE - FUSELAGE AFT PRESSURE BULKHEAD INSPECTION MODIFICATION, ANDREPAIR

Repetitive





23.Oct.2014Page 406/429

Document-Number Type Rev Compliance A|C Subject StatusThis Document SUPERSEDES 2002-10-11/AD Rev.00This Document has been SUPERSEDED BY 2014-18-02/AD Rev.00

> 737-53A1075/SB Rev.03 *AD* AFT PRESSURE BULKHEAD INSPECTION Repetitive> > 737-53A1075-01/EO* Rev.00 *AD* AFT PRESSURE BULKHEAD INSPECTION/MOD AND REP *** MANDATORY


This Document SUPERSEDES 737-53A1075/EO Rev.03NOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document








23.Oct.2014Page 407/429

Document-Number Type Rev Compliance A|C Subject Status2014-05-12 AD 00 MANDATORY A/C WINGS - TRAILING EDGE FLAPS - OUTBOARD FLAP CARRIAGE SPINDLE -INSPECTION

FOR CRACKINGOpen





23.Oct.2014Page 408/429

Document-Number Type Rev Compliance A|C Subject StatusThis AD is applicable to all B737-100 through -500.

Compliance:AD §(g) is comlied with throughEO 737-57A1277-01 (NDT) EO is revised to indicate SB Rev03EO 737-57A1277-02 (Gap Check) EO is revised to indicate SB Rev03

AD §(h) is complied with through:EO 737-57A1277-02 (Gap Check) EO is revised to indicate SB Rev03

AD §(i) is complied with through:EO 737-57A1277-02 (Gap Check) EO is revised to indicate SB Rev03.NAS will only use the latest rev of the SB as approved data.

AD §(j) is complied with through:EO 737-57A1277-01 (NDT) EO is revised to indicate SB Rev03

AD §(k) is complied with through:EO 737-57A1277-01 (NDT) EO is revised to indicate SB Rev03.NAS will only use the latest rev of the SB as approved data.

AD §(l) is complied with through a company policy to only installcarriages in OH condition. This is covered during receiving of part.

AD §(m) must be complied with at overhaul by approved shop. Theadherence of this § will be confirmed during receiving of part intoNorwegian stores.

AD §(n): NAS will report all findings to OEM this due to National andEASA requirements.





23.Oct.2014Page 409/429

Document-Number Type Rev Compliance A|C Subject StatusAD §(o) 2 (i) and (ii) is complied with through:EO 737-57A1281-01, refleting SB 737-57A1218 Rev:06 as approved data.Norwegian has always had an overhaul program for its OUTB Flapcarriages.

AD§ (p) is NA to NAS as we do not operate AC sub type.

AD § (q)is complied with through:EO 737-57A1218-02, reflecting SB 737-57A1218 Rev:06 as approved data.

AD § (r)is complied with through:EO 737-57A1218-03, reflecting SB 737-57A1218 Rev:06 as approved data.

AD §(s) is continously complied with through:EO 737-57A1218-02 and 03, reflecting SB 737-57A1218 Rev:06 as approveddata.

This AD contains no time limits, as the time limits are a function ofthe underlying EO.737-57A1218737-57A1218-01737-57A1218-02737-57A1218-03737-57A1277737-57A1277-01737-57A1277-02737-57A1277-03

SBEOEOEOSBEOEOEO

0600010003000000

This Document SUPERSEDES 2010-15-08/AD Rev.002014-05-12/AD Rev.00 WINGS - TRAILING EDGE FLAPS - OUTBOARD FLAP CARRIAGE SPINDLE -INSPECTION

FOR CRACKINGOpen

This Document SUPERSEDES 2010-15-08/AD Rev.00





23.Oct.2014Page 410/429

Document-Number Type Rev Compliance A|C Subject Status> 737-57A1218/SB Rev.06 WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSPECTION/OVERHAUL & LIFE

LIMITINGOpen

This Document SUPERSEDES 737-57A1218/SB Rev.05> > 737-57A1218-01/EO* Rev.00 WINGS- TE OUTB FLAP CARRIAGE SPINDELS INSPECTION/OVERHAUL Open


65-46481-116 / 1783 Pos=#8 (KKM)Repetitive / Next Due:11.Jan.2022 38297/C/ Last Performed:13.Jan.2014 0/CRefDocument:FAA 8130-3 026010 Rev.00

65-46481-145 / B5121 Pos=#1 (KKM) Open / Next Due:14.May.2021 22077/C

65-46481-119 / B3554 Pos=#2 (KKM)

Repetitive / Next Due:05.Oct.2020 22073/C/ Last Performed:07.Oct.2012 0/CRefDocument:FAA 8130-3 024128-2Rev.00

65-46481-106 / 4914WG Pos=#7 (KKM)

Repetitive / Next Due:05.Feb.2019 37305/C/ Last Performed:07.Feb.2011 35283:00/H25305/C RefDocument:EASA F1001282424 Rev.00

> > 737-57A1218-02/EO* Rev.01 WINGS- TE OUTB FLAP CARRIAGE SPINDELS LIFE LIMIT FOR FLAP CARRIAGES WITHDOCUMENTED HISTORY

Open

This Document SUPERSEDES 737-57A1218-02/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status65-46481-119 / B3554 Pos=#2 (KKM) Open / Next Due: 40000/C65-46481-106 / 4914WG Pos=#7 (KKM) Open / Next Due: 40000/C65-46481-145 / B5121 Pos=#1 (KKM) Open / Next Due: 40000/C65-46481-116 / 1783 Pos=#8 (KKM) Open / Next Due: 40000/C

> > 737-57A1218-03/EO* Rev.00 WINGS- TE OUTB FLAP CARRIAGE SPINDELS LIFE LIMIT FOR FLAP CARRIAGES WITHUN-DOCUMENTED HISTORY

Not Applicable / Special Text: Thiscomp.is Not Applicable due toKNOWN history,ref EO737-57A1218-02






23.Oct.2014Page 411/429


65-46481-116 / 1783 Pos=#8 (KKM)

Not Applicable / Special Text: This comp.isNot Applicable due to KNOWN history,refEO 737-57A1218-02 / Reason: THISCOMP.IS NOT APPLICABLE DUE TOKNOWN HISTORY,REF EO737-57A1218-02

65-46481-145 / B5121 Pos=#1 (KKM)

Not Applicable / Special Text: This comp.isNot Applicable due to KNOWN history,refEO 737-57A1218-02 / Reason: EO737-57A1218-02 COVER CARRIAGESWITH KNOWN HISTORY

65-46481-119 / B3554 Pos=#2 (KKM)

Not Applicable / Special Text: This comp.isNot Applicable due to KNOWN history,refEO 737-57A1218-02 / Reason: NA DUETO KNOWN HISTORY, REFER TO EO737-57A1218-02

65-46481-106 / 4914WG Pos=#7 (KKM)

Not Applicable / Special Text: This comp.isNot Applicable due to KNOWN history,refEO 737-57A1218-02 / Reason: NOTAPPLICABLE SINCE HISTORY ISKNOWN, REF EO 737-57A1218-02

> 737-57A1277/SB Rev.03 WINGS - TRAILING EDGE FLAPS - OUTBOARD FLAP CARRIAGE SPINDLE - INSPECTIONFOR CRACKING

Open


> > 737-57A1277-01/EO* Rev.01 NDT OF TE OUTB FLAP CARRIAGE SPINDELS INSP FOR CRACKS. OpenThis Document SUPERSEDES 737-57A1277-01/EO Rev.00Affected Rotables (Part No/Serial No/Position) Status

65-46481-106 / 4914WG Pos=#7 (KKM)Repetitive / Next Due:05.Apr.2015 33501/C/ Last Performed:07.Oct.2014 44068:36/H32001/C W/O:15483811 Rev.01





23.Oct.2014Page 412/429


65-46481-116 / 1783 Pos=#8 (KKM)Repetitive / Next Due: 29297/C / LastPerformed:13.Jan.2014 0/CRefDocument:FAA 8130-3 026010 Rev.00

65-46481-119 / B3554 Pos=#2 (KKM)Repetitive / Next Due:04.Apr.2015 15497/C/ Last Performed:06.Oct.2014 5180:36/H13997/C W/O:15483875 Rev.01

65-46481-145 / B5121 Pos=#1 (KKM) Open / Next Due: 13077/C> > 737-57A1277-02/EO* Rev.01 WINGS- TE OUTB FLAP GAP CHECK & CARRIAGE SPINDELS INSP FOR CRACKS. Repetitive

This Document SUPERSEDES 737-57A1277-02/EO Rev.00NOTE: 'Whichever comes later' calculation logic applicable for the intervalDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

21.Oct.2014 44634/CPerform initially before(F) 140/C /Interval(L):140/C or 14/D


07.Oct.2014 73319:36/H 44494/C 15665000,Was due at: 44533/C and 26.Sep.2014PerfRev.:'01'

> > 737-57A1277-03/EO* Rev.00 NDT OF TE OUTB FLAP CARRIAGE SPINDELS INSP FOR CRACKS. Not ApplicableAffected Rotables (Part No/Serial No/Position) Status

65-46481-145 / B5121 Pos=#1 (KKM)Not Applicable / Reason: Datum SN hasbeen overhauled and is controlled by EO737-57A1277-01

65-46481-119 / B3554 Pos=#2 (KKM)Not Applicable / Reason: Datum SN hasbeen overhauled and is controlled by EO737-57A1277-01

65-46481-106 / 4914WG Pos=#7 (KKM)Not Applicable / Reason: Datum SN hasbeen overhauled and is controlled by EO737-57A1277-01

65-46481-116 / 1783 Pos=#8 (KKM)Not Applicable / Reason: Datum SN hasbeen overhauled and is controlled by EO737-57A1277-01





23.Oct.2014Page 413/429

Document-Number Type Rev Compliance A|C Subject Status2014-05-21 AD 0 MANDATORY A/C FUSELAGE - STRUCTURE AROUND OPENINGS - FORWARD ENTRY AND FORWARD

GALLEY SERVICE DOORWAY UPPER AND LOWER HINGE CUTOUTRepetitive

This Document SUPERSEDES 2008-11-04/AD Rev.002014-05-21/AD Rev.0 FUSELAGE - STRUCTURE AROUND OPENINGS - FORWARD ENTRY AND FORWARD


This Document SUPERSEDES 2008-11-04/AD Rev.00> 737-53A1200/SB Rev.02 FUSELAGE - STRUCTURE AROUND OPENINGS - FORWARD ENTRY AND FORWARD




Closed 07.Jul.2011

This Document SUPERSEDES 737-53A1200-1/EO Rev.00Perf Dim1 (D) Perf Dim2 Perf Dim3 W/O, Ref.-Doc Remarks

07.Jul.2011 54542:00/H 30315/C

Was due at: 48315/C PerfRev.:'00' PERFPERMANENT REP ON FWD ENTRYDOOR UPPER HINGE ACC SR1-748133531 AND FAA 8100-9

Reason for this StatusPERF PERMANENT REP ON FWD ENTRY DOOR UPPER HINGE ACC SR 1-748133531 ANDFAA 8100-9

> > 737-53A1200-02/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD ENTRY DOORWAY LOWERHINGE CUTOUT INSPECTION. GROUP 2 AIRPLANES

Repetitive


48315/C

Perform initially within (effective from25.Jun.2008) (L) 3000/C Perform initiallywithin (effective from 25.Jun.2008) (L)20000/C / Interval(F):18000/C






23.Oct.2014Page 414/429







This Document SUPERSEDES 737-53A1200-2/EO Rev.00> > 737-53A1200-05/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD ENTRY DOORWAY UPPER




This Document SUPERSEDES 737-53A1200-3/EO Rev.00> > 737-53A1200-07/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD GALLEY DOORWAY UPPER

HINGE CUTOUT INSPECTION. GROUP 2 AIRPLANESRepetitive


48315/C




> > 737-53A1200-08/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD GALLEY DOORWAY LOWERHINGE CUTOUT INSPECTION. GROUP 2 AIRPLANES

Repetitive






23.Oct.2014Page 415/429

Document-Number Type Rev Compliance A|C Subject StatusNOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

48315/C




> > 737-53A1200-09/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD GALLEY DOORWAY UPPERHINGE CUTOUT INSPECTION. GROUP 3 & 4 AIRPLANES


This Document SUPERSEDES 737-53A1200-5/EO Rev.00> > 737-53A1200-10/EO* Rev.00 FUSELAGE. STRUCTURE AROUND OPENINGS. FORWARD GALLEY DOORWAY LOWER

HINGE CUTOUT INSPECTION. GROUP 3 & 4 AIRPLANESNot Applicable by Serial Number






23.Oct.2014Page 416/429

Document-Number Type Rev Compliance A|C Subject Status2014-08-08 AD 00 MANDATORY A/C FUSELAGE - SKIN - FORWARD ENTRY DOORWAY - LOWER CORNERS - INSPECTION

AND REPAIRNot Applicable

§(g) Repetetive inspections.KKW is applicable to § g(2) for Group 3 AC which is Part 2 of737-53A1329, dated June 4, 2013 with effective date according to AD

§(h) Repair.KKW is applicable to § g(2) for Group 3 AC which is Part 2 of737-53A1329, dated June 4, 2013

EO 737-53A1329-01 covers part 2 of SB 737-53A1329 dated 4 june, 20132014-08-08/AD Rev.00 FUSELAGE - SKIN - FORWARD ENTRY DOORWAY - LOWER CORNERS - INSPECTION

AND REPAIRNot Applicable

> 737-53A1329/SB Rev.00 FUSELAGE - SKIN - FORWARD ENTRY DOORWAY - LOWER CORNERS - INSPECTIONAND REPAIR

Not Applicable

> > 737-53A1329-01/EO* Rev.00 FUSELAGE - SKIN - FORWARD ENTRY DOORWAY - LOWER CORNERS - INSPECTIONAND REPAIR


This Document has been SUPERSEDED BY 737-53A1329-01/EO Rev.01> > 737-53A1329-01/EO* Rev.01 FUSELAGE - SKIN - FORWARD ENTRY DOORWAY - LOWER CORNERS - INSPECTION

AND REPAIRNot Applicable by Serial Number






23.Oct.2014Page 417/429

Document-Number Type Rev Compliance A|C Subject Status2014-12-13 AD 00 MANDATORY A/C WINGS - LANDING GEAR SUPPORT BEAM - REAR SPAR AND AFT SUPPORT FITTING Open

Applicable to all B737CL.

Compliance:AD §(f) is complied with through EO detailed below.AD §(g) is NA to NAS as we do not operate Group 1 AC (737-100/200)AD §(h) and § (i) Group 2-7 AC inspections are complied with throughEO detailed below.

NAS only has aircraft in Group 6, Config 2 and Group 7.The SB is divided into 2 EO:737-57-1318-01: Group 6 Config 2 AC.737-57-1318-02: Group 6 Config 2 AC.737-57-1318-03: Group 7737-57-1318-04: Group 7737-57-1318-05: Group 7 AC.MSN:29072 with MLG drop May 2015. Reject!

No time limit on AD, as the time limit is differentiated, refer to EOfor time limits.120S-14-2512013-NM-131-AD2014-03-06737-57-1216737-57-1318737-57-1318-01737-57-1318-02737-57-1318-03737-57-1318-04737-57-1318-05

AMOCNPRMADSBSBEOEOEOEOEO

00000002000000000000

This Document SUPERSEDES 2014-03-06/AD Rev.002014-12-13/AD Rev.00 WINGS - LANDING GEAR SUPPORT BEAM - REAR SPAR AND AFT SUPPORT FITTING Open





23.Oct.2014Page 418/429

Document-Number Type Rev Compliance A|C Subject StatusThis Document SUPERSEDES 2014-03-06/AD Rev.00

> 737-57-1318/SB Rev.00 WINGS - LANDING GEAR SUPPORT BEAM - REAR SPAR AND AFT SUPPORT FITTINGINSPECTION

Open

> > 737-57-1318-01/EO* Rev.00 MLG SUPPORT BEAM -NDT INSPECTION OF REAR SPAR AND AFT SUPPORT FITTINGSURFACE INSPECTION OF LH/RH FITTING

Open

This Document is terminated with implementation of 737-57-1318-02/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

47873/CPerform initially within (effective from09.Apr.2014) (F) 4500/C /Interval(F):4500/C

> > 737-57-1318-02/EO* Rev.00 MLG SUPPORT BEAM -INSPECTION OF REAR SPAR AND AFT SUPPORT FITTING OPENHOLE HFEC INSP 12 FASTENER HOLES

Open

This Document terminates 737-57-1318-01/EO Rev.00Due Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document

61373/CPerform initially within (effective from09.Apr.2014) (F) 18000/C /Interval(F):24000/C

> > 737-57-1318-03/EO* Rev.00 MLG SUPPORT BEAM -INSPECTION OF REAR SPAR AND AFT SUPPORT FITTINGSURFACE INSPECTION OF LH/RH FITTING


This Document is terminated with implementation of 737-57-1318-04/EO Rev.00> > 737-57-1318-04/EO* Rev.00 MLG SUPPORT BEAM -INSPECTION OF REAR SPAR AND AFT SUPPORT FITTING OPEN

HOLE HFEC INSP 12 FASTENER HOLESNot Applicable by Serial Number

This Document terminates 737-57-1318-03/EO Rev.00> > 737-57-1318-05/EO* Rev.00 MLG SUPPORT BEAM -INSPECTION OF REAR SPAR AND AFT SUPPORT FITTING OPEN

HOLE HFEC INSP 12 FASTENER HOLESNot Applicable by Serial Number





23.Oct.2014Page 419/429

Document-Number Type Rev Compliance A|C Subject Status2014-13-07 AD 0 MANDATORY A/C INFORMATION-LIGHT-STROBE POSITION LIGHTS-LIGHTNING OF THE TAIL STROBE

LIGHT AND WIRE BUNDLE-FAA FINAL RULENot Applicable

2014-13-07/AD Rev.0 INFORMATION-LIGHT-STROBE POSITION LIGHTS-LIGHTNING OF THE TAIL STROBELIGHT AND WIRE BUNDLE-FAA FINAL RULE

Not Applicable

> 737-33-1149/SB* Rev.00 LIGHTS - STROBE POSITION LIGHTS - LIGHTNING PROTECTION OF THE TAIL STROBELIGHT AND WIRE BUNDLE


2014-17-02 AD 0 MANDATORY COMP EMERGENCY LOCATOR TRANSMITTER BATTERY WIRING INSTALLATIONDISCREPANCIES

Closed 02.Aug.2013 W/O:459439

This Document SUPERSEDES 2013-18-09/AD Rev.002014-17-02/AD Rev.0 EMERGENCY LOCATOR TRANSMITTER BATTERY WIRING INSTALLATION

DISCREPANCIESClosed 02.Aug.2013 W/O:459439

This Document SUPERSEDES 2013-18-09/AD Rev.00> 2013-18-09/AD Rev.00 EMERGENCY LOCATOR TRANSMITTER - BATTERY WIRING INSTALLATION


This Document has been SUPERSEDED BY 2014-17-02/AD Rev.0> > 13-1075/TD* Rev.00 INSPECT ELT BATTERY, BATTERY WIRING, AND ELT TO BATTERY WIRING Closed 02.Aug.2013 W/O:459439

This Document has been SUPERSEDED BY 13-1075/TD Rev.01Affected Rotables (Part No/Serial No/Position) Status


> > 13-1075/TD* Rev.01 INSPECT ELT BATTERY, BATTERY WIRING, AND ELT TO BATTERY WIRING See prev. DocstatusThis Document SUPERSEDES 13-1075/TD Rev.00Affected Rotables (Part No/Serial No/Position) Status1152682-1 / 072C-256 Pos=AFT (KKM) See prev. Docstatus / Reason: .





23.Oct.2014Page 420/429

Document-Number Type Rev Compliance A|C Subject Status2014-18-02 AD 00 MANDATORY A/C AD- FUSELAGE - FUSELAGE AFT PRESSURE BULKHEAD INSPECTION MODIFICATION

AND REPAIRRepetitive

Paragraph (g): N/A, Applic to L/N 1-929 only.

Paragraph (h): N/A, Applic to L/N 1-929 only.

Paragraph (i): N/A, Applic to L/N 1-929 only.

Paragraph (j): N/A, Applic to L/N 1-929 only.

Paragraph (k)(3):Perf earlier per AD 2002-10-11 par (e)(3)737-53A1075/EO

Paragraph (l)(2): Covered by 737-53A1075-01/EO

Paragraph (m)(2): Covered by 737-53A1075-01/EO.

Paragraph (n): Restatement of requirement paragrapg (n) from AD2014-05-02 (Fig 2 step 1-6). Covered by 737-53A1075-01/EO, step D.

Paragraph (o): Optional to (l)(2)Insp from Aft side only. NOT CHOSEN!

Paragraph (p): SB 737-53A1075, Fig.3 removed from EO. Engineeringmust be contacted if findings.This Document SUPERSEDES 2014-05-02/AD Rev.R0

2014-18-02/AD Rev.00 AD- FUSELAGE - FUSELAGE AFT PRESSURE BULKHEAD INSPECTION MODIFICATIONAND REPAIR

Repetitive

This Document SUPERSEDES 2014-05-02/AD Rev.R0> 737-53A1075/SB Rev.03 *AD* AFT PRESSURE BULKHEAD INSPECTION Repetitive> > 737-53A1075-01/EO* Rev.00 *AD* AFT PRESSURE BULKHEAD INSPECTION/MOD AND REP *** MANDATORY






23.Oct.2014Page 421/429

Document-Number Type Rev Compliance A|C Subject StatusThis Document SUPERSEDES 737-53A1075/EO Rev.03NOTE: 'Whichever comes later' calculation logic applicable for the first accomplishmentDue Dim1 (D) Due Dim2 Due Dim3 New W/O Time-Requirement of Document




92-21-04 AD 00 RECOMMENDED A/C MAIN CARGO DOOR LOCK VISUAL AND WARNING INDICATION MODIFICATION Not Applicable by Serial NumberNot applicable to NAS B737. No aircraft with main deck cargo door.737-52-1060 SB 00

CF-2013-25 AD 00 MANDATORY COMP EMERGENCY LOCATOR TRANSMITTER - BATTERY WIRING INSTALLATIONDISCREPANCIES

Closed 02.Aug.2013 W/O:459439

1152682-23-A2213-107513-1075

SBTDTD

010001

Perform BEFORE 23.Aug.2013CF-2013-25/AD Rev.00 EMERGENCY LOCATOR TRANSMITTER - BATTERY WIRING INSTALLATION


> 13-1075/TD* Rev.00 INSPECT ELT BATTERY, BATTERY WIRING, AND ELT TO BATTERY WIRING Closed 02.Aug.2013 W/O:459439This Document has been SUPERSEDED BY 13-1075/TD Rev.01Affected Rotables (Part No/Serial No/Position) Status


> 13-1075/TD* Rev.01 INSPECT ELT BATTERY, BATTERY WIRING, AND ELT TO BATTERY WIRING See prev. DocstatusThis Document SUPERSEDES 13-1075/TD Rev.00Affected Rotables (Part No/Serial No/Position) Status1152682-1 / 072C-256 Pos=AFT (KKM) See prev. Docstatus / Reason: .





23.Oct.2014Page 422/429

Document-Number Type Rev Compliance A|C Subject StatusF-1989-181 AD 03 MANDATORY COMP INLET GEARBOX - NO. 3 BEARING IMPROVEMENT PROGRAM Not Applicable





23.Oct.2014Page 423/429

Document-Number Type Rev Compliance A|C Subject StatusTo prevent failure of number 3 bearings.

AD 1989-23-06 R01

Category 1Engines equipped with No.3 bearing, PIN 9732MI0P12 (havingserial numbers that begin with FAF D or FAF E only),PIN 9732MI0P18, or PIN 1362M76P02, must have the bearing removed atnext 1GB exposure, or December 31, 1997, whichever occurs first.

Category 21 Engines equipped with No. 3 bearing, PIN 9732MIOP12 (havingserial numbers that begin with FAF Dor FAF E only), shouldhave the MCD inspected at intervals not to exceed 50 EngineFlight Hours (EFH), up to 6,000 hours time in service ofthe bearing. If the bearing has more than 6,000 hours timein service the MCD may be inspected at normal intervals.

2 Engines equipped with No.3 bearing, PIN 9732MIOP18 orPIN 1362M76P02, should have the MCD inspected at intervalsnot to exceed 50 EFH. This inspection interval of 50 EFHshould continue until the bearing is replaced.

3 Engines equipped with No.3 bearing, PIN 9732MI0P12(beginning with serial numbers other than FAF D or FAF E),PIN 9732MI0PI0, or PIN 9732MI0P17, should have the MCDinspected at intervals not to exceed 75 EFH up to 6,000hours time in service of the bearings. If the bearing hasmore than 6,000 hours time in service the MCD may beinspected at normal intervals.





23.Oct.2014Page 424/429

Document-Number Type Rev Compliance A|C Subject StatusCategory 3Engines equipped with No.3 bearing, PIN 9732M10Pl2 (beginningwith serial numbers other than FAF D or FAF E), PIN 9732M10P10,or PIN 9732M10P17, should have the bearing removed at nextengine shop visit, but no later than next 1GB exposure.1989-23-061989-23-063-72-0530

ADADSB

000103

Perform BEFORE 28.Jan.1989F-1989-181/AD Rev.03 INLET GEARBOX - NO. 3 BEARING IMPROVEMENT PROGRAM Not Applicable> 3-72-0530/SB* Rev.03 INLET GEARBOX - NO. 3 BEARING IMPROVEMENT PROGRAM Not Applicable


CFM56-3B2 / 724473 Pos=LH (KKM)Not Applicable / Reason: NA DUE TO PNSHOP VISIT 05

CFM56-3B2 / 725495 Pos=RH (KKM)Not Applicable / Reason: DEL DOCMSN:224676





23.Oct.2014Page 425/429

Document-Number Type Rev Compliance A|C Subject StatusF-1997-298 AD 04 MANDATORY COMP FAN DISK - INSPECTION OF Closed 26.Jun.2012

Ref. Service Bulletin CFM56-3/-3B/-3C SB 72-0854 Revision 5.2001-04-063-72-0854

ADSB

0005

Perform within an unlimited threshold.F-1997-298/AD Rev.04 FAN DISK - INSPECTION OF Closed 26.Jun.2012> 3-72-0854/SB* Rev.05 FAN DISK DOVETAIL, WEAR MEASUREMENT OF Closed 26.Jun.2012


CFM56-3B2 / 725495 Pos=RH (KKM)

Closed / Last Performed:26.Jun.201264007:00/H 38431/C RefDocument:MTURECORDED MOD SHEET WO 51734400Rev.05

CFM56-3B2 / 724473 Pos=LH (KKM)

Closed / Reason: NEW DISK INST. ONSHOP VISIT 39729 / LastPerformed:17.Jan.2005 42076:00/H 21463/CRefDocument: Rev.NOTE





23.Oct.2014Page 426/429

Document-Number Type Rev Compliance A|C Subject StatusF-2001-240 AD 00 MANDATORY COMP CHIP DETECTOR INSPECTION Not Applicable

Between 50 to 75 flight hours following the effective date of thisAirworthiness Directive, inspect the aft sump Magnetic Chip Detector.Repeat the inspection every 50 to 75 flight hours as long as the No.4 bearing has not been replaced.3-72-0965 SB 00

F-2001-240/AD Rev.00 CHIP DETECTOR INSPECTION Not Applicable> 3-72-0965/SB* Rev.00 MAGNETIC CHIP DETECTOR - REDUCED INTERVAL FOR AFT SUMP Not Applicable by Serial Number

Affected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 725495 Pos=RH (KKM) Not ApplicableCFM56-3B2 / 724473 Pos=LH (KKM) Not Applicable

> 3-72-0966/SB* Rev.00 NO.4 ROLLER BEARING 305-355-717-0 - REPLACEMENT OF DEFECTIVE BATCH Not Applicable by Serial NumberAffected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 724473 Pos=LH (KKM) Not ApplicableCFM56-3B2 / 725495 Pos=RH (KKM) Not Applicable





23.Oct.2014Page 427/429

Document-Number Type Rev Compliance A|C Subject StatusF-2002-390 AD 00 MANDATORY COMP REVISION OF ENGINE SHOP MANUAL. Information Only

Perform inspections of the subjected parts at each piece-partopportunity in accordance with the Inspection/Check sectioninstructions.2000-12-012002-13-03

ADAD

0000


F-2002-390/AD Rev.00 REVISION OF ENGINE SHOP MANUAL. Information OnlyThis Document SUPERSEDES 2000-12-01/AD Rev.00

> 2002-13-03/AD* Rev.00 REVISION OF ENGINE SHOP MANUAL. Information OnlyThis Document SUPERSEDES 2000-0294/AD Rev.00This Document SUPERSEDES 2000-12-01/AD Rev.00Affected Rotables (Part No/Serial No/Position) Status

CFM56-3B2 / 724473 Pos=LH (KKM)Information Only / Reason: AUTOASSIGNED

CFM56-3B2 / 725495 Pos=RH (KKM)Information Only / Reason: AUTOASSIGNED





23.Oct.2014Page 428/429

Document-Number Type Rev Compliance A|C Subject StatusF-2004-095 AD 00 MANDATORY COMP ENGINE FUEL AND CONTROL - REPLACEMENT OF MAIN FUEL PUMPS EQUIPPED

WITH SOLID BRONZE BEARINGS WITH PUMPS EQUIPPED WITH BI-METALClosed 27.Jun.2012

Replacement of main fuel pumps equipped with solid bronze bearingswith pumps equipped with bi-metal, aluminium/bronze bearings.2004-10-133-73-0120

ADSB

0006

Perform within an unlimited threshold.F-2004-095/AD Rev.00 ENGINE FUEL AND CONTROL - REPLACEMENT OF MAIN FUEL PUMPS EQUIPPED

WITH SOLID BRONZE BEARINGS WITH PUMPS EQUIPPED WITH BI-METALClosed 27.Jun.2012

> 3-73-0120/SB* Rev.06 MAIN FUEL PUMPS EQUIP. WITH SOLID BRONZE BEARING - REPL. Closed 27.Jun.2012Affected Rotables (Part No/Serial No/Position) StatusCFM56-3B2 / 724473 Pos=LH (KKM) Not Applicable / Reason: 39729

CFM56-3B2 / 725495 Pos=RH (KKM)

Closed / Reason: PB: PREVIOUSLYEMBODIED / Last Performed:27.Jun.201264007:00/H 38431/C RefDocument:MTURECORDED MOD SHEET WO 51734400Rev.06

T1989-01-51 AD 00 MANDATORY A/C *AD* SUPERSEDED BY T1989-03-51 Not ApplicableT1989-01-51 (SUPERSEDED)T1989-03-51 (ACTIVE)

ADAD

0000

Reason for this StatusSUPERSEDED BY AD T1989-03-51

T1989-03-51 AD 00 MANDATORY A/C *AD* ENGINE AND CARGO COMPARTMENT FIRE PROTECTION SYSTEM Not ApplicableComplied with at build.T1989-01-51 (SUPERSEDED)T1989-03-51 (ACTIVE)

ADAD





23.Oct.2014Page 429/429

Date post:	18-Mar-2018
Category:	Documents
Upload:	tranlien
View:	284 times
Download:	12 times

Modification Control Report 13237 23.Oct - · PDF file1974-08-09 ad 03 mandatory a/c lavatory...

Documents