DA FORM 2408-15 E, OCT 91 HISTORICAL RECORD … FORM 2408-15 E, OCT 91 HISTORICAL RECORD FOR...

NUMBERLOCATIONPIDENTRYORGANIZATION

8.7.DATE

6.REMARKS

4. 5.

UH-60A 7923273HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL

Report Date: Page 1 of 4217-Jan-2016

(NO ORGANIZATION)AIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG 70400-00003REV. B SYSTEMS CONTROLS HAVE BEENBIASED IN ACCORD. A. LATERAL CONTROLSERVO INPUT ROD P/N 70400-02258-046 HASBEEN SHORTENED 1/4 TURN. B. AFTCONTROL SERVO INPUT ROD P/N 70400-02258-045 HAS BEEN LENGTHENED 1/2 TURN. C.FORWARD CONTROL SERVO INPUT ROD P/N70400-02258-047 HAS BEEN SHORTENED 1/2TURN. NOTE: WHEN ACFT RIGGING IS BIASEDRIGGING PIN HOLES ARE TEMPORARILYLOST AT THE ABOVE POINTS. G. NATTER (NOPID)

13-Sep-1980 1

(NO LOCATION)

QC000000

(NO ORGANIZATION)ONE TIME INSPECTION OF AIRCRAFT INLETANTI-ICING VALVE PER MSG. NO UH-60A-79-2.G NATTER (NO PID)

27-Sep-1980 1

(NO LOCATION)

QC000000

(NO ORGANIZATION)INSPECTED XMSN MAIN MODULE OIL DIPSTICK P/N 70351-08164 FOR BOTTOMING OUTPER MAIN ADVISORY MSG NO UH-60A-80-20 G.NATTER (NO PID)

27-Sep-1980 2

(NO LOCATION)

QC000000

B CO 158TH AVN BNONE TIME INSP OF ENG/APU FUEL SHUT OFFVALVE 9PN-70307-03024-101 FOR SN 1-75I/A/W TWX PO31500Z NOV 80 (NO PID)

05-Nov-1980 1

FT CAMPBELL, KY42223

QC000000

B CO 158TH AVN BNONE TIME INSPE OF INPUT MODULES FOR SNA264-00027 0307-03024-101 FOR SN 1-75 I/A/WTWX PO31500Z NOV 80 (NO PID)

21-Nov-1980 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF CARGO DOOR STOPSREQUIRED I/A/W SOF MSG UH-60A-81-4 DTDMAR81 COMPLETED (NO PID)

23-Mar-1981 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF TROOP CARGO LOWERDOOR STOPS REQUIRED I/A/W SOF MSG UH-60A-81-7 DTD APR81 COMPLETED AT 163.6ACFT HRS. (NO PID)

13-Apr-1981 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF OIL COOLER FANREQUIRED I/A/W SOF MSG UH-60A-81-8 DTDAPR 81 COMPLETED AT 196.6 ACFT HRS (NOPID)

13-Apr-1981 2


QC000000

B CO 158TH AVN BNONE TIME INSP OF ENGINE OUTPUT SHAFTCOMPLETED I/A/W SOF MSG UH-60A-81-12DTD 14 MAY 81 (NO PID)

15-May-1981 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF AIRCRAFT AXIAL FAN ANDSHAFT ASSY COMPLETED I/A/W SOF MSG UH-60A-81-13 DTD 15MAY81 (NO PID)

19-May-1981 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF MAIN MODULE OUTERSHAFT COMPLETED I/A/W SOF MSG UH-60A-81-18 DTD JUL 81 (NO PID)

24-Jul-1981 1


QC000000

BLACK HAWK MODTEAM

ONE TIME INSPECTION OF UH-60A GEARBOXMAIN MODULE OUTERSHAFT I/A/W TWX231600 COMPLIED WITH BY BLACK HAWKMOD TEAM AT 220.3 ACFT HRS. (NO PID)

28-Jul-1981 1


QC000000

For use of this form, see DA PAM 738-751; the proponent agency is DCSLOGEDITION OF JAN 64 IS OBSOLETEHISTORICAL RECORD FOR AIRCRAFTDA FORM 2408-15 E, OCT 91


8.7.DATE

6.REMARKS

4. 5.



BLACK HAWK MODTEAM

MOD 99-122-1 INSTALLATION OF CREW DOORGROUNDING SEALS COMPLIED WITH BYBLACK HAWK MOD TEAM (NO PID)

28-Jul-1981 2


QC000000

BLACK HAWK MODTEAM

MOD 99-124 EXTEND SHELF SUPPORT ZEEMEMBERS TO FORM A BARRIER AND DIRECTMGB OIL COOLER EXHAUST AIR AFT ANDAWAY FROM THE APU AIR INLETS COMPLIED(NO PID)

28-Jul-1981 3


QC000000

BLACK HAWK MODTEAM

MOD 99-130-6 INSTALLATION OF BOOTS TOFLIGHT CONTROL TUBES PASSAGEWAYS INCABIN CEILING TO IMPROVE WATERINTEGGRITY COMPLIED WITH (NO PID)

28-Jul-1981 4


QC000000

BLACK HAWK MODTEAM

MOD 99-099 CHANGE MAIN LANDING GERARSTRUTS TO REDUCE STRUT STIFFNESSCOMPLIED WITH (NO PID)

28-Jul-1981 5


QC000000

BLACK HAWK MODTEAM

MOD 99-ECP117-011 CHANGE OF TROOP SEATCLEVIS TO IMPROVED TYPE COMPLIED WITH(NO PID)

28-Jul-1981 6


QC000000

BLACK HAWK MODTEAM

MOD 99-ECP117-007 REPLACEMENT OFCOCKPIT DOOR HEATER DUCT GASKET FORIMPROVED FIT COMPLIED WITH (NO PID)

28-Jul-1981 7


QC000000

B CO 158TH AVN BNONE TIME INSPECTION COMPLETED I/A/WMSG UH-60A-81-17 DTD JUL81 REACTIVATIONOF PANEL LIGHT DIMMING SWITCH NVGDIMMING MODE (NO PID)

05-Aug-1981 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF M/R BLADE TIP CAPSCOMPLETED I/A/W SOF MSG UH-60A-81-20DTD AUG81 (NO PID)

11-Aug-1981 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF ENG OUT PUT SHAFTASSEMBLIES COMPLETED I/A/W SOF MSG UH-60A-81-127 DTD OCT 81 (NO PID)

06-Oct-1981 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF DESWIREL DUCT & CLAMPCOMPLETED I/A/W SOF MSG UH-60A-81-28 (NOPID)

28-Oct-1981 1


QC000000

B CO 158TH AVN BNINSTALLATION OF PART 1 OF NWL ECO#81192 INSTALLATION OF 4 SPRINGS CLIPSON INPUT LINKS OF T/R SERVO ASSYCOMPLETED (NO PID)

03-Dec-1981 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF UPPER RESTRAINTSYSTEM RUBBING BAR COMPLETED I/A/WSOF MSG UH-60A-82-6 DTD APR82 (NO PID)

07-May-1982 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF MAIN ROTOR SERVOSCREW COMPLETED I/A/W SOF MSG UH-60A-82-11 DTD 4AUG82 (NO PID)

07-Aug-1982 1


QC000000



8.7.DATE

6.REMARKS

4. 5.



B CO 158TH AVN BNONE TIME INSP OF MAIN ROTOR SERVOINPUT LINK BEARINGS COMPLETED I/A/W SOFMSG 82-13 (NO PID)

12-Aug-1982 1


QC000000

B CO 158TH AVN BNONE TIME INSPECTION OF TAIL ROTORSERVO BOLTS COMPLETED I/A/W SOF MSGUH-60A-82-14 DTD SEP 82 (NO PID)

08-Sep-1982 1


QC000000

B CO 158TH AVN BNONE TIME INSPECTION OF MIXER ASSYCOMPLETED I/A/W SOF MSG UH-60A-82-16DTD SP 82 (NO PID)

23-Sep-1982 1


QC000000

B CO 158TH AVN BNONE TIME INSPECTION OF YAW AND ROLLTRIM SERVOS COMPLETED I/A/W SOF UH-60A-82-19 DTD OCT82 (NO PID)

26-Oct-1982 1


QC000000

B CO 158TH AVN BNONE TIME INSPECTION OF MAIN ROTORFOWARD INPUT SERVO ROD END ASSYCOMPLETED I/W/A D.F. MSG FROM D.A.M.ODTD 14OCT82 (NO PID)

09-Nov-1982 1


QC000000

B CO 158TH AVN BNONE TIME INSPECTION OF MAIN ROTORPITCH CHANGE ROD END ASSY COMPLETEDI/A/W D.F. MSG FROM D.A.M.O DTD 30 SEP 82(NO PID)

09-Nov-1982 2


QC000000

B CO 158TH AVN BNONE TIME INSPECTION OF DRAG BEAM ASSYCOMPLETED I/A/W SOF MSG UH-60A-82-21DTD NOV 82 (NO PID)

17-Nov-1982 1


QC000000

B CO 158TH AVN BNONE TIME INSPECTION OF FLIGHT CONTROLSDIRECTIONAL CONTROL LEVER COMPLETEDI/A/W SOF MSG UH-60A-83-02 DTD MAR 83 (NOPID)

05-Apr-1983 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF AIR INLET DUCTS ANDALIGNMENT PIN BRACKETS COMPLETEDI/A/W SOF MSG UH-60A-83-04 APR 83 (NO PID)

11-Apr-1983 1


QC000000

OCM/ACE TEAMOCM/ACE PERFORMED AT 996 A/C HRS AT FTCAMPBELL KY BY ACE TEAM MEMBER NTSARCOM OCM SEC. ST. LOUIS MO (NO PID)

12-Apr-1983 1


QC000000

B CO 158TH AVN BNONE TIME INSPECTION OF STABILATORAMPLIFIERS COMPLETED IAW SOF MSG UH-60A-83-09 (NO PID)

26-Oct-1983 1


QC000000

B CO 158TH AVN BNONE TIME INSPECTION AND REPLACEMENTOF COLLECTIVE BIAS TUBE ASSY WASHERSI/A/W SOF MSG UH-60A-83-10 (NO PID)

26-Oct-1983 2


QC000000

B CO 158TH AVN BNINSPECTION OF TAIL ROTOR SERVO VALVESTEMS COMPLETED I/A/W SOF MSG UH-60A-83-12 (NO PID)

08-Nov-1983 1


QC000000

B CO 158TH AVN BNINSPECTION OF ACCESSORY MODULERETURN SCREENS COMPLETED I/A/W SOFMSG UH-60A-83-11 (NO PID)

22-Nov-1983 1


QC000000

B CO 158TH AVN BNINSPECTION OF ACFT HISTORICAL RECORDSCOMPLETED I/A/W SOF MSG UH-60A-84-01 (NOPID)

23-Jan-1984 1


QC000000



8.7.DATE

6.REMARKS

4. 5.



SIKORSKY ACFTONE TIME ULTRASONIC INSP OF MAINMODULE SHAFT COMPLETED I/A/W SOF MSGUH-60A-84-01 DTD 19JAN84 (NO PID)

05-Feb-1984 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF T/R PYLON HINGEBRACKET COMPLETED I/A/W SOF MSG UH-60A-84-03 (NO PID)

06-Apr-1984 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF OIL LEVELS ON I/G/B &T/R/G/B I/A/W SOF MSG UH-60A-84-06 DTD23APR84 (NO PID)

27-Apr-1984 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF ENGINE OUT PUT DRIVESHAFT BOLTS DUE I/A/W SOF MSG UH-60A-84-07 PRIOR TO NEXT 14 DAY 10 HRS INSP DTD10MAY84 (NO PID)

14-May-1984 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF CARGO HOOK SQUIB REQI/A/W SOF MSG UH-60A-84-08 DTD 29 MAY 84(NO PID)

30-May-1984 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF LOGITUDINAL ANDLATERAL LINK ASSY REQ I/A/W SOF MSG UH-60A-84-11 DTD 2JUL84 (NO PID)

06-Jul-1984 1


QC000000

OCM/ACE TEAMOCM/ACE PERFORMED AT 911 A/C HRS AT FTCAMPBELL, KY BY ACE TEAM MEMBER RAVSCOM OCM SEC.ST LOUIS MO. (NO PID)

20-Jul-1984 1


QC000000

B CO 158TH AVN BNSOF ONE TIME INSP T/R CABLES UH-60A-84-14TB 55-1520-237-20-58 COMPLETED AT 946.4ACFT HRS.TED AT 946.4 ACFT HRS. (NO PID)

02-Nov-1984 1


QC000000

B CO 158TH AVN BNONE TIME INSP ON LIFE LIMITS OF STAGE#1,#2 GAS GENRATORS TURBINE ROTORDISK COMPLETED I/A/W TB 55-2840-248-20-16DTD 7APR84 (NO PID)

07-Jan-1985 1


QC000000

B CO 158TH AVN BNSOF INSP UH-60A-84-17 TB 55-1520-237-20-59MAIN GEAR DOWEL PIN COMPLETED (NO PID)

07-Jan-1985 2


QC000000

B CO 158TH AVN BNONE TIME INSP OF STABILATOR AMPLIFIERFOR NO-LOCKING TYPE POTEINTOMETERI/A/W SOF MSG UH-60A-85-01 COMPLETED 13FEB 85 (NO PID)

13-Feb-1985 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF STABILATOR AMPS BY SNCOMPLETED I/A/W UH-60A-85-03 AT 980.4ACFT HRS. (NO PID)

07-Mar-1985 1

FT. CAMPBELL, KY42223-5000

QC000000

B CO 158TH AVN BNONE TIME INSP OF SOF MSG TO CHANGEAUTOROTATION LIMITS IAW UH60A-85-02COMPLETED (NO PID)

12-Mar-1985 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF AND REPLACEMENT OFSTAB AMPLI- FIERS IAW UH60A-85-04COMPLETED (NO PID)

14-Mar-1985 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF ECU LOCKOUT ISPROHIBITED IAW SOF MSG UH60A-85-05COMP (NO PID)

18-Mar-1985 1


QC000000



8.7.DATE

6.REMARKS

4. 5.



B CO 158TH AVN BNONE TIME INSPECTION OF PRIMARY SERVOINPUT RODS FOR RETAINERS ON CERTAINSERIAL NUMBERED SERVOS IAW SOF MSGUH60A-85-06 (TB 55-1520-20-01) COMP 21 MAR85 (NO PID)

21-Mar-1985 1


QC000000

B CO 158TH AVN BNONE TIME INSPECTION OF FLT CONTROLSDONE IAW SOF MSG UH60A-85-07COMPLETED AT 988.3 ACFT HOURS (NO PID)

10-Apr-1985 1


QC000000

B CO 158TH AVN BNONE TIME INSPECTION OF ACFT M/R SPINDLEDONE IAW SOF MSG UH60A-85-11 & TB 55-1520-237-20-65 COMP AT 988.3 ACFT HOURS(NO PID)

30-Apr-1985 1


QC000000

B CO 158TH AVN BNONE TIME INSPECTION OF ACFT DONE IAWSOF UH60A- 85-10 & TB 55-1520-237-20-64COMP AT 988.3 A/C HRS (NO PID)

02-May-1985 1


QC000000

B CO 158TH AVN BNONE TIME INSPECTION OF T-700 ENG POWERTURBINE CASE IAW SOF MSG UH60A-85-12DTD MAY 85 COMPLETED AT 988.3 ACFTHOURS (NO PID)

13-May-1985 1


QC000000

B CO 158TH AVN BNONE TIME INSPECTION OF M/R SPINDLE IAWSOF MSG UH60A-85-13 (TB 55-1520-237-20-66)COMPLETED AT 988.3 ACFT HOURS (NO PID)

17-May-1985 1


QC000000

B CO 158TH AVN BNONE TIME INSPECTION OF MAIN ROTORSHAFT IAW SOF MSG UH60A-85-14 DTD 2 JUN85 (NO PID)

03-Jun-1985 1


QC000000

B CO 158TH AVN BNONE TIME RECORD INSP FOR HUB S/N & P/NIAW SOF MSG UH60A-85-15 (TB 55-1520-237-20-69) COMPLETED AT 988.3 ACFT HOURS (NOPID)

03-Jun-1985 2


QC000000

B CO 158TH AVN BNOCM/ACE PERFORMED AT 0988 ACFT HOURSAT FT. CAMPBELL, KY BY ACE TEAMMEMBER, AVSCOM OCMSEC, ST. LOUIS, MO(NO PID)

01-Jul-1985 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF SEQUENCE VALVE &OPERATION IN ECU LOCK OUT COMPLETEDIAW SOF MSG UH60A-85-22 AT 988.3 ACFTHOURS (NO PID)

22-Jul-1985 1


QC000000

B CO 158TH AVN BNONE TIME RECORDS INSP FOR M/R SPINDLE &TIE ROD RET LIFE COMPLETED IAW SOF MSGUH60A-85-21 AT 988.3 ACFT HOURS (NO PID)

22-Jul-1985 2


QC000000

B CO 158TH AVN BNONE TIME RECORDS INSP FOR M/R SPINDLEW/TIE ROD RET LIFE TO 1400 HRS IAW SOFMSG UH60A-85-20 COMPLETED AT 988.3 ACFTHOURS (NO PID)

22-Jul-1985 3


QC000000

B CO 158TH AVN BNONE TIME RECORDS INSP FOR MAIN ROTORSHAFT NSN CHG COMPLETED IAW SOF MSGUH60A-85-19 & TB 55-1520-237-70 AT 988.3ACFT HOURS (NO PID)

22-Jul-1985 4


QC000000

B CO 158TH AVN BNONE TIME INSP FOR UNGROUNDINGREQUIREMENTS COMPLETED IAW SOF MSGUH60A-85-18 & TB 55-1520-237-70 AT 988.3ACFT HOURS (NO PID)

22-Jul-1985 5


QC000000



8.7.DATE

6.REMARKS

4. 5.



B CO 158TH AVN BNONE TIME RECORD INSP FOR HIGH SPEEDSHFT VIBRATION LEVELS IAW SOF MSGUH60A-85-17 & TB 55-1520-237-20-67COMPLETED AT 988.3 ACFT HOURS (NO PID)

22-Jul-1985 6


QC000000

B CO 158TH AVN BNONE TIME RECORD INSP OF MAIN ROTORHUB COMPLETED IAW SOF MSG UH60A-85-16& TB 55-1520-237-20-69 AT 988.3 ACFT HOURS(NO PID)

22-Jul-1985 7


QC000000

B CO 158TH AVN BNSOF MSG UH-60A-85-23/TB 55-1520-237-20-71,T/R D/S BEARING CRITERIA COMPLETED AT988.3 ACFT HRS (NO PID)

26-Jul-1985 1


QC000000

B CO 158TH AVN BNSOF MSG UH-60A-85-24 (TB 55-1520-237-20-72)UNGROUNDING CRITERIA FOR T/R D/SBEARINGS AND ADDITION OF D/S BEARINGSTO ACFT CONDITION CHANGE DA FORM 2408-16 COMPLETED 2 AUG 85 AT 988.3 ACFTHOURS (NO PID)

02-Aug-1985 1


QC000000

B CO 158TH AVN BNSOF MSG UH-60A-85-9 & 18 COMPLETED AT988.3 ACFT HRS (NO PID)

10-Sep-1985 1


QC000000

B CO 158TH AVN BNAT 988.3 ACFT HOURS RIGGING CKCOMPLETED WITH THE FOLLOWINGADJUSTMENTS MADE: YAW BOOST SERVOINPUT CONTROL ROD 1 1/2 TURN, ROLLOUTPUT SHORTENED 2 TURNS, LATERALPRIMARY SERVO SHORTENED 1/2 TURN (NOPID)

16-Sep-1985 1


QC000000

B CO 158TH AVN BNSOF UH60A-85-25 TORQUE STABILIZATION OFM/R PITCH HORN BOLTS ENTERED AT 1062.4ACFT HOURS (NO PID)

01-Nov-1985 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF T/R IAW SOF MSG UH60A-86-02 & -03(TB 55-1520-237-20-74) COMPLETEDAT 1184.9 A/C HRS (NO PID)

18-Mar-1986 1


QC000000

B CO 158TH AVN BNONE TIME INSP OF T/R D/S BEARINGS IAWSOF MSG UH6086-01 (TB 55O-1520-237-23-1)COMPLETED AT 1180.8 ACFT HOURS (NO PID)

18-Mar-1986 2


QC000000

B CO 158TH AVN BNACFT GROUNDED IAW SOF MSG UH60A-86-05,DECLARED GROUNDED UNTIL FURTHERNOTICE (NO PID)

25-Mar-1986 1


QC000000

C CO 24TH CABSOF MSG UH-60A-86-06 STAB/AUTO FLTCONTROL PANEL RETROFIT COMPLETED 19APR 86 (NO PID)

18-Apr-1986 1

HAAF GA 31409

QC000000

B CO 158TH AVN BNSOF MSG UH60A-86-07 REQUIREMENTS FORUNGROUNDING (TB 55-1520-237-20-75) MWO55-1520-237-20-1 (NO PID)

30-Apr-1986 1


QC000000

B CO 158TH AVN BNSOF MSG UH60A-86-08 (TB 55-1520-237-20-77)REPLACEMENT OF STABILATOR ACTUATORS(NO PID)

09-May-1986 1


QC000000

B CO 158TH AVN BNSOF MSG UH60A-86-09 INSP OF ENG OILCOOLER ASSY (TB 55-2840-248-50-43)COMPLETED 30 MAY 86 (NO PID)

29-May-1986 1


QC000000



8.7.DATE

6.REMARKS

4. 5.



B CO 158TH AVN BNSOF MSG UH-60A-86-10 ONE TIME INSP OFYAW LEVER BEARINGS COMPLETED 9 JUL 86(NO PID)

08-Jul-1986 1


QC000000

B CO 158TH AVN BNOCM/ACE PERFORMED AT 1213 A/C HOURSAT FT.CAMPBELL KY BY ACE TEAM MEMBER,AVSCOM OCM SEC, ST. LOUIS, MO (NO PID)

17-Jul-1986 1


QC000000

B CO 158TH AVN BNSOF MSG UH-60A-86-13 REPLACEMENT OFAN310-8 NUTS COMPLETED. (NO PID)

29-Jul-1986 1


QC000000

B CO 158TH AVN BNSOF MSG UH-60A-86-12 LOCATION & CHANGEOUT OF SERIAL NUMBERED YAW & BOOSTSERVO*S COMPLETED 30 JUL 86 (NO PID)

30-Jul-1986 1


QC000000

174TH AVN COSOF MSG UH-60A-86-16 UH60A BLACKHAWKLEVER ASSY P/N 70400-02623-041COMPLETED 30 OCT 86 (NO PID)

14-Oct-1986 1

HAAF GA 31409

QC000000

174TH AVN COSOF MSG UH-60A-86-17 CONTRACTOR INSPOF XMSN OIL COOLER FAN SPLINES & T/RDRIVESHAFT COMPLETED 22 OCT 86 (NO PID)

22-Oct-1986 1

HAAF GA 31409

QC000000

174TH AVN COSOF MSG UH-60A-86-19 REPETITIVE INSP OFEYEBOLT P/N 70209-02136-102 COMPLETED 03NOV 86 (NO PID)

31-Oct-1986 1

HAAF GA 31409

QC000000

174TH AVN COSOF MSG UH-60A-86-20 FIELD INSP OF THE1ST THREE T/R,DRIVESHAFT SPLINECOUPLINGS & REMOVAL OF MATERIALUNDER CREW SEATS COMPLETED 7 NOV 86AT 1263.7 ACFT HOURS (NO PID)

07-Nov-1986 1

HAAF GA 31409

QC000000

174TH AVN COSOF MSG UH-60A-86-21 ONE TIME INSP OFCREW SEATS FOR "ARA" MANUFAC DUECOMPLETED 01 DEC 86 (NO PID)

04-Dec-1986 1

HAAF GA 31409

QC000000

174TH AVN COSOF MSG UH-60A-86-02 ONE TIME INSP OF T/4DRIVE SHAFT FLEX COUPLING NUTSCOMPLETED 20 FEB 87 COMPLETED 14 MAR87 (NO PID)

25-Feb-1987 1

HAAF GA 31409

QC000000

174TH AVN COSOF MSG UH-60A-87-03 ONE TIME &RECURRING INSP OF FIRST THREE T/R DRIVESHAFT SPLINE COUPLINGS COMPLETED 14MAR 87 (NO PID)

14-Mar-1987 1

HAAF GA 31409

QC000000

174TH AVN COSOF MSG UH-60A-87-04 REVISION TO INSP OFEYEBOLT P/N 70209-02136-102 COMPLETED 25MAR 87 (NO PID)

25-Mar-1987 1

HAAF GA 31409

QC000000

174TH AVN COSOF MSG UH-60A-87-06 ONE TIME INSP &RECURRING INSP OF OIL COOLER SPLINESCOMPLETED 14 MAY 87 (NO PID)

15-May-1987 1

HAAF GA 31409

QC000000

174TH AVN COSOF MSG UH-60A-87-07 ONE TIME INSP &RECURRING INSP OF LAT/LONG LINK ASSYCOMPLETED 15 MAY 87 (NO PID)

19-May-1987 1

HAAF GA 31409

QC000000

174TH AVN COSOF MSG UH-60A-87-05 STABILATOROPERATIONAL PROCE-DURES COMPLETED(NO PID)

28-May-1987 1

HAAF GA 31409

QC000000



8.7.DATE

6.REMARKS

4. 5.



174TH AVN COSOF MSG UH-60A-87-02 REVISION TOMESSAGE ON T-700 ENG FUEL DIFFERENTIALPRESSURE INDICATOR COMPLETED 24 FEB87 (NO PID)

28-May-1987 2

HAAF GA 31409

QC000000

174TH AVN COSOF MSG UH-60A-887-01 ONE TIME INSP &VALIDATION OF T-700 ENG FUELDIFFERENTIAL PRESSURE INDICATORCOMPLETED 23 FEB 87 (NO PID)

28-May-1987 3

HAAF GA 31409

QC000000

ASF #157SOF GEN 87-02 ONE TIME INSP FOR LOCALPURCHASED ACFT TIME CHANGECOMPONENTS/PARTS C/W AT 1364.2 ACFTHOURS (NO PID)

13-Jul-1987 1

FT. RUCKER, AL

QC000000

ASF #157SOF UH-60A-87-08 ONE TIME INSP OFMIDSECTION BELL CRANK ASSY C/W AT1379.2 ACFT HRS (NO PID)

15-Jul-1987 1

FT. RUCKER, AL

QC000000

ASF #157TB 55-1520-237-20-104 NEWOVERHAUL/RETIREMENT LIFE SCHEDULEFOR H-60 RETIREMENT COMPONENTS C/W AT1670.9 A/C HRS (NO PID)

25-Aug-1987 1

FT. RUCKER, AL 36362

QC000000

ASF #157TB 55-1520-237-20-86 ELECTGRICALDISCONNECTION OF THE PITCH BIASACTUATOR C/W AT 1397.5 ACFT HRS (NO PID)

31-Aug-1987 1

FT. RUCKER, AL

QC000000

ASF #157SOF UH-60-87-10 ONE TIME INSP OF L/H & R/HINPUT MODULE FLANGES C/W AT 1405.1 ACFTHRS (NO PID)

15-Oct-1987 1

FT. RUCKER, AL

QC000000

ASF #157SOF UH-60-87-11 ONE TIME INSP OF CARGODOOR UPPER & LOWER ROLLER SUPPORTASSY C/W AT 1410.5 ACFT HRS (NO PID)

05-Nov-1987 1

FT. RUCKER, AL

QC000000

ASF #157MIM UH-60-87-XSOF-02 TB 55-1520-237-20-93,ONE TIME INSP & RECURRING INSP OF ENGCOWLINGS C/W AT 1410.5 ACFT HOURS (NOPID)

16-Nov-1987 1

FT. RUCKER, AL

QC000000

ASF #157SOF UH60-87-12 ONE TIME INSP FORDEFECTIVE POWER TURBINE MODULES C/WAT 1423.7 ACFT HOURS (NO PID)

03-Dec-1987 1

FT. RUCKER, AL

QC000000

ASF #157SOF UH60-87-09, UH60A/EH-60A SERIES ACFT,CYCLIC STABILATOR SLEW SWITCH & MWO55-1520-237-50-46 C/WAT 1429 ACFT HOURSBY PROJECT OLR, FT. CAMPBELL, KY (NOPID)

12-Jan-1988 1

FT. RUCKER, AL

QC000000

ASF #157SOF UH60-88-01 INSP FOR CERTAIN SERIALNUMBER T/R BLADE ASSY C/W 1429.1 ACFTHRS (NO PID)

16-Feb-1988 1

FT. RUCKER, AL

QC000000

ASF #157SOF UH60-88-03 EXTENTION TO RETIREMENTLIFE OF M/R SHAFT C/W 1488.5 ACFT HRS (NOPID)

19-May-1988 1

FT. RUCKER, AL

QC000000

ASF #157SOF UH60-88-05 INITIATION OF APU MOAT C/WAT 1488.5 ACFT HRS (NO PID)

13-Jun-1988 1

FT. RUCKER, AL

QC000000

ASF #157SOF UH60A-88-06 OVERHAUL LIFE FOR XMSNOIL COOLER BLOWER C/W AT 1488.5 ACFTHRS (NO PID)

11-Jul-1988 1

FT. RUCKER, AL

QC000000

ASF #157SOF UH60A-88-07 REVISION TO SOF UH60A-88-05 C/W AT 1488.5 ACFT HOURS (NO PID)

05-Aug-1988 1

FT. RUCKER, AL

QC000000



8.7.DATE

6.REMARKS

4. 5.



ASF #157SOF UH-60-88-09 ONE TIME INSP OF ARACREW SEATS C/W AT 1488.5 ACFT HOURS (NOPID)

08-Aug-1988 1

FT. RUCKER, AL

QC000000

ASF #157SOF UH-60-88-08 REVISION TO SOF UH60A-88-06 C/W AT 1488.5 ACFT HOURS (NO PID)

08-Aug-1988 2

FT. RUCKER, AL

QC000000

ASF #157SOF UH-60-88-04 REVISION TO SOF UH-60-88-02 C/W BY SIKORSKY ACFT SUPPORTSERVICES (NO PID)

12-Aug-1988 1

FT. RUCKER, AL

QC000000

ASF #157TB 55-1520-237-20-96 (UH-60-88-02) ONE TIMEINSP OF TR GEARBOX OUTPUT SHAFT, C/W,CIV, USAAVNDTA (NO PID)

12-Aug-1988 2

FT. RUCKER, AL

QC000000

ASF #157PERIODIC INSPECTION #3 COMPLETED AT1488.5 A/C HRS (NO PID)

21-Aug-1988 1

FT. RUCKER, AL

QC000000

ASF #157SOF GEN 88-02 INSP FOR INSTALLATION OFCORRECT PORTABLE FIRE EXTINGUISHERSC/W AT 1496.6 A/C HRS (NO PID)

23-Sep-1988 1

FT. RUCKER, AL

QC000000

ASF #157SOF GEN 88-03 REVISION TO SOF GEN 88-02INSP FOR CORRECT PORTABLE FIREEXTINGUISHERS C/W AT 1511.3 A/C HOURS(NO PID)

11-Oct-1988 1

FT. RUCKER, AL

QC000000

ASF #157SOF UH-60-88-11 IMMEDIATE RESTRICTION OFREAPPELL-ING OPERATIONS C/W AT 1524.7A/C HOURS (NO PID)

27-Oct-1988 1

FT. RUCKER, AL

QC000000

ASF #157SOF UH-60-88-12 REVISION TO UH-60-88-10C/W AT 1538.5 A/C HOURS (NO PID)

07-Nov-1988 1

FT. RUCKER, AL

QC000000

ASF #157SOF UH-60-88-10 ONE TIME INSP OFTROOP/GUNNER SEAT UPPER SUPPORTINSTALLATION C/W AT 1538.5 A/C HOURS (NOPID)

07-Nov-1988 2

FT. RUCKER, AL

QC000000

ASF #157SOF UH-60-88-13 ONE TIME INSP OF M/RBLADE PINS C/W AT 1541.9 A/C HOURS (NOPID)

18-Nov-1988 1

FT. RUCKER, AL

QC000000

ASF #17OCM/ACE PERFORMED AT 1563 A/C HOURSBY ACE TEAM MEMBER, AVSCOM OCMSEC,ST. LOUIS. MO (NO PID)

01-Feb-1989 1

FT. BENNING, GA

QC000000

ASF #17UH-60-89-01 ONE TIME INSP OF T700-GE-700GAS ENG STATOR SHROUDS C/W AT 1573.3A/C HRS (NO PID)

13-Feb-1989 1

FT. BENNING, GA

QC000000

ASF #17UH-60-89-02 ONE TIME INSP OF T700-GE-700CORRECT SOF UH-60-89-01, ONE TIME INSPFO T700 ENG GAS GENSTATOR SHROUDSC/W AT 1580.4 A/C HRS (NO PID)

14-Feb-1989 1

FT. BENNING, GA

QC000000

ASF #17UH-60-89-03 ONE TIME INSP OF M/R SPINDSLEC/W AT 1624.7 A/C HR (NO PID)

31-Mar-1989 1

FT. BENNING, GA

QC000000

ASF #17UH-60-89-03 AMENDMENT UH-60-89-04,040800Z MAR 89 ONE TIME INSP OF M/RSPINDLES C/W AT 1624.7 A/C HR (NO PID)

31-Mar-1989 2

FT. BENNING, GA

QC000000

ASF #17SOF UH-60-89-05 ONE TIME INSP OF WIRESTRIKE PROTECTION SYS C/W AT 1645.3 A/CHOURS (NO PID)

07-Aug-1989 1

FT. BENNING, GA 31905

QC000000



8.7.DATE

6.REMARKS

4. 5.



ASF #157SOF UH-60-89-08 ONE TIME INSP OF FUELBOOST PUMP HOSE ATTACHMENT C/W AT1658.3 A/C HOURS (NO PID)

14-Aug-1989 1


QC000000

ASF #157SOF UH-60-89-09 CORRECTION OFRETIREMENT LIFE COMPONENT SCHEDULEC/W AT 1658.3 A/C HOURS (NO PID)

17-Aug-1989 1


QC000000

ASF #157SOF UH-60-89-10 ONE TIME INSP OF T700-GE-700 ENG GAS GEN ROTOR & STATORSHROUD HISTORICAL RECORDS C/W AT1679.7 A/C HOURS (NO PID)

20-Sep-1989 1


QC000000

ASF #17SOF UH-60-89-11 ONE TIME INSP OF OILCOOLER AXIAL FAN C/W AT 1695.3 A/CHOURS (NO PID)

14-Nov-1989 1

FT. BENNING, GA

QC000000

ASF #17SOF UH-60-89-12 ONE TIME INSP OF OILCOOLER AXIAL FAN C/W AT 1704.6 A/CHOURS (NO PID)

30-Nov-1989 1

FT. BENNING, GA

QC000000

ASF #17OCM/ACE PERFORMED AT 1712 A/C HOURSAT FT.BENNING BY ACE TEAM MEMBER,AVSCOM OCMSEC, ST. LOUIS MO (NO PID)

10-Jan-1990 1

FT. BENNING, GA

QC000000

ASF #17SOF UH-60-89-13 INSP OF TIEDOWN RINGBOLTS C/W 1713 A/C HOURS (NO PID)

23-Feb-1990 1

FT. BENNING, GA

QC000000

ASF #17SOF UH-60-90-01 ONE TIME INSP OF M/REXPANDABLE PINS C/W AT 1720.4 A/C HRS(NO PID)

11-Apr-1990 1

FT. BENNING, GA

QC000000

ASF #17TB 55-1520-237-20-113 ONE TIME INSP OF ICERATE INDICATOR C/W AT 1781.4 ACFT HRS(NO PID)

15-Jun-1990 1

FT. BENNING, GA

QC000000

ASF #17TB 55-1520-237-20-111 ONE TIME INSP OFUPPER PRESSURE PLATE & SPINDLE TO HUBATTACHMENT BOLTS C/W AT 1785.3 ACFTHRS (NO PID)

02-Jul-1990 1

FT. BENNING, GA

QC000000

ASF #17SOF-UH-60-90-02 ONE TIME INSP OF TAILROTOR PITCH BEAM RETAINING WASHERAND NUT C/W AT 1796.3 A/C HR (NO PID)

13-Aug-1990 1

FT. BENNING, GA

QC000000

ASF #17TB 55-1520-237-20-114 ONE TIME INSP OFMEDEVAC PROVISION POWER RECEPTACLEC/W AT 1851.9 A/C HRS (NO PID)

09-Nov-1990 1

FT. BENNING, GA

QC000000

ASF #17OCM/ACE PERFORMED AT 1878 A/C HRS ATCOLUMBIA, GA BY ACE TEAM MEMBER,AVSCOM OCMSEC, ST. LOUIS MO (NO PID)

19-Dec-1990 1

FT. BENNING, GA

QC000000

ASF #17UH-60-91-ASAM-01 REPLACEMENT OF T/RPITCH BEAM RETAINER WASHER C/W AT 1910A/C HOURS (NO PID)

13-Feb-1991 1

FT. BENNING, GA

QC000000

ASF #17UH-60-91-ASAM-05 INSP OF M/R SPINDLE C/WAT 1914.7A/C HOURS (NO PID)

26-Feb-1991 1

FT. BENNING, GA

QC000000

ASF #17UH-60-91-ASAM-06 INSP OF CARGO HOOK C/WAT 1936.0 A/C HOURS (NO PID)

01-Apr-1991 1

FT. BENNING, GA

QC000000

ASF #17UH-60-91-ASAM-08 INSP OF FIREEXTINGUISHER SYSTEM C/W AT 1962 A/CHOURS (NO PID)

05-Apr-1991 1

FT. BENNING, GA

QC000000



8.7.DATE

6.REMARKS

4. 5.



ASF #17PMS-2 #4 C/W AT 1988.6 A/C HOURS (NO PID) 02-May-1991 1

FT. BENNING, GA

QC000000

ASF #17UH-60-91-ASAM-09 INSP OF ELASTOMERICBEARINGS C/W AT 1989 A/C HOURS (NO PID)

06-Jun-1991 1

FT. BENNING, GA

QC000000

ASF #17UH-60-91-ASAM'S-02, 03, & 04 N/A THIS ACFT S(NO PID)

06-Jun-1991 2

FT. BENNING, GA

QC000000

ASF #17UH-60-91-ASAM-10 ONE TIME INSP OF MAINLANDING GEAR BRAKE ASSY, PISTONINSULATOR C/W AT 1991.0 A/C HOURS (NOPID)

25-Jul-1991 1

FT. BENNING, GA

QC000000

ASF #17UH-60-92-ASAM-01 INSP FOR 3UNSERVICEABLE SPINDLE ASSY C/W AT 2078A/C HRS (NO PID)

15-Jan-1992 1

FT. BENNING, GA

QC000000

ASF #17OCM/ACE PERFORMED AT 2103 A/C HRS ATFT. BENNING, GA BY ACE TEAM MEMBER,AVSCOM OCMSEC, ST. LOUIS, MO (NO PID)

14-Feb-1992 1

FT. BENNING, GA

QC000000

ASF #17UH-60-92-ASAM-05 INSP & REPLACEMENT OFTHE M/R EXPANDABLE PIN C/W AT 2168 A/CHOURS (NO PID)

14-Oct-1992 1

FT. BENNING, GA

QC000000

ASF #17UH-60-92-ASAM-06 ONE TIME INSP OF PEDALADJUSTOR ASSEMBLY C/W AT 2168 (NO PID)

20-Oct-1992 1

FT. BENNING, GA

QC000000

ASF #17UH-60-93-ASAM-01 PERFORMANCE OF ANOPERATIONAL CHECK ON ALL CHIPDETECTORS C/W AT 2168 A/C HRS (NO PID)

22-Oct-1992 1

FT. BENNING, GA

QC000000

ASF #17OCM/ACE PERFORMED AT 2186 A/C HOURSBY ACE TEAM MEMBER, TSARCOM OCMSECTION, ST. LOUIS, MO (NO PID)

14-Jan-1993 1

FT. BENNING, GA

QC000000

ASF #17UH-60-93-ASAM-08 RIGGING OF THE RAILROTOR IAW UH-60-93-ASAM-08 C/W AT 2193.3ACFT HOURS (NO PID)

27-Jan-1993 1

FT. BENNING, GA

QC000000

ASF #17UH-60-93-ASAM-06 ONE TIME INSP TOREMOVE SUSPECT TAIL ROTOR PITCHBEAMS C/W AT 2193.3 ACFT HOURS (NO PID)

27-Jan-1993 2

FT. BENNING, GA

QC000000

ASF #17TB 1-1520-237-20-128 ELECTRICALDISCONNECTION OF THE PITCH BIASACTUATOR C/W AT 2193.3 ACFT HOURS (NOPID)

27-Jan-1993 3

FT. BENNING, GA

QC000000

ASF #17UH-60-93-ASAM-12 ABRUPT CHANGE IN MAINROTOR TRACK/VIBRATION TO ADVISE PILOTSC/W (NO PID)

07-Jun-1993 1

FT. BENNING, GA

QC000000

ASF #17UH-60-93-ASAM-13 ESSS AND ERFS MISSIONKITS INSTALLED TM 237-10 PROCEDURECHANGE C/W (NO PID)

07-Jun-1993 2

FT. BENNING, GA

QC000000

ASF #17UH-660-93-ASAM-15 ESSS AND ERFSAMENDMENT TO UH-60-93-ASAM-14 NOTREQUIRED THIS ACFT (NO PID)

23-Jun-1993 1

FT. BENNING, GA

QC000000

ASF #17UH-660-93-ASAM-14 ESSS AND ERFSCLEANING AND INSP OF BRU-22A/A EJECTORRACK NOT REQUIRED THIS ACFT (NO PID)

23-Jun-1993 2

FT. BENNING, GA

QC000000



8.7.DATE

6.REMARKS

4. 5.



ASF #17UH-60-93-ASAM-10 ONE TIME INSP &RECURRING INSP/ CLEANING OF ESSSVALVES & PNUE LINES N/A THIS A/C (NO PID)

01-Jul-1993 1

FT. BENNING, GA

QC000000

ASF #17UH-60-93-ASAM-11 INSPECT & REPLACE ARACREW RESTRAINT, BUCKLE/CROTCH ASSYC/W (NO PID)

01-Jul-1993 2

FT. BENNING, GA

QC000000

ASF #17UH-60-93-ASAM-09 ONE TIME INSP TODETERMINE COM- PLIANCE WITH SYSTEMMWO'S COMPLIED WITH (NO PID)

01-Jul-1993 3

FT. BENNING, GA

QC000000

ASF #17UH-60-93-ASAM-16 HYDRAULIC PUMPMODULE KNURLED KNOB INSP COMPLIEDWITH - C/W (NO PID)

10-Aug-1993 1

FT. BENNING, GA

QC000000

ASF #17UH-60-94-ASAM-01 ONE TIME INSP OFMASTER WARNING PANEL FOR P/N 70550-01101 C/W (NO PID)

21-Dec-1993 1

FT. BENNING, GA

QC000000

ASF #17UH-60-94-ASAM-03 ONE TIME INSPECTION OFM/R SPINDLE ASSY & ELASTOMERIC THRUSTBEARINGS, 2397.6 A/C HOURS (NO PID)

20-Jan-1994 1

FT. BENNING, GA

QC000000

AVSCOM OCMSECTION,ACE TEAM

OCM/ACE PERFORMED AT 2412 A/C HOURSAT FT. BENNIN G,GA (NO PID)

04-Feb-1994 1

FT. BENNING, GA

QC000000

ASF #17UH60-94-ASAM-06 ONE TIME INSP OF PILOTS'& CO-PIL 0T'S RESTRAINT SYSTEM TO INSUREBOTH ARE LIFT LEVER OR ROTARY RELEASE- C/W (NO PID)

11-Feb-1994 1

FT. BENNING, GA

QC000000

ASF #17UH-60-94-ASAM-05 ONE TIME INSP OF TAILG/B WITH TAIL G/B OUTPUT SHAFT P/N 70358-06620-101 (NO PID)

11-Feb-1994 2

FT. BENNING, GA

QC000000

ASF #17UH-60-94-ASAM-04 ONE TIME INSP OF PITCHBEAM FOR SUSPECTED S/N - CW (NO PID)

11-Feb-1994 3

FT. BENNING, GA

QC000000

ASF #17UH-60-94-ASAM-07 RETIREMENT LIFE TIMECHANGE TO OVERHAUL AND RETIREMENTTABLE - C/W 2461.7 A/C HOURS (NO PID)

06-Apr-1994 1

FT. BENNING, GA

QC000000

ASF #17UH-60-94-ASAM-09 ONE TIME INSP OFPRIMARY SERVOS COMPLIED WITH AT 2459.3A/C HOURS C/W (NO PID)

06-Apr-1994 2

FT. BENNING, GA

QC000000

ASF #17UH-60-94-ASAM-10 REVISION TO UH-60 94-ASAM-03 2487.6 ACFT HRS - CW (NO PID)

18-Apr-1994 1

FT. BENNING, GA

QC000000

ASF #17UH-60-94-ASAM-11 INFO ON M/R BLADE DE-ICE TEST (NO PID)

09-May-1994 1

FT. BENNING, GA

QC000000

CCADUH-60-95-ASAM-05 - CHANGE IN RETIREMENTLIFE FOR SERVO BEAM RAILS - CW (NO PID)

03-Mar-1995 1

CORPUS CHRISTI, TX

QC000000

CCADUH-60-95-ASAM-04 (TB 1-1520-237-20-160) -REDUCTION OF TORQUE OF SELF-RETAININGPIVOT BOLTS - CW (NO PID)

03-Mar-1995 2

CORPUS CHRISTI, TX

QC000000

CCADUH-60-95-ASAM-03 (TB 1-1520-237-20-158) -REQ RE- SHIM OF TR PIVOT BRG PERREVISED PROCEDURES & CERTAIN BLADEASSY WILL BE INSP FOR SPECIFIED SN'SWHICH CONTAIN COMPOSITE PIVOT BRGRETAINER - CW (NO PID)

03-Mar-1995 3

CORPUS CHRISTI, TX

QC000000



8.7.DATE

6.REMARKS

4. 5.



CCADTB 1-2835-214-20-1 - ONE TIME INSP OFFORMS AND RECORDS FOR H-60 APU'S - CW(NO PID)

03-Mar-1995 4

CORPUS CHRISTI, TX

QC000000

CCADUH-60-94-ASAM-07/08 (TB 1-1520-237-20-154)CHG TO UH-60 OVERHAUL & RETIREMENTLIFE TABLE - CW (NO PID)

03-Mar-1995 5

CORPUS CHRISTI, TX

QC000000

CCADUH-60-93-ASAM-10 (TB 1-1520-237-20-141) ONE-TIME RECURRING INSP/CLEANING OF ESSSVALVES & PNEUMATIC LINES - PCW (NO PID)

03-Mar-1995 6

CORPUS CHRISTI, TX

QC000000

CCADUH-60-93-ASAM-03 (TB 1-1520-237-20-130)REVISION TO M/R BLADE EXP PINS UH-60-92-ASAM-05 ON 101 PINS - CW (NO PID)

03-Mar-1995 7

CORPUS CHRISTI, TX

QC000000

CCADTB 1-1520-237-20-128 - DISCONNECTION OFTHE PITCH BIAS ACTUATOR - CW - CW (NOPID)

03-Mar-1995 8

CORPUS CHRISTI, TX

QC000000

CCADUH-60-92-ASAM-02 (TB 1-1520-237-20-132) ONE-TIME INSP FOR ENG OUTPUT SHAFT BOLTTORQUE & VIBRATION LEVEL - CW (NO PID)

03-Mar-1995 9

CORPUS CHRISTI, TX

QC000000

CCADACFT SIX-MONTHS FILE WILL BE RETAINEDAT CCAD IAW TDS NO. AGEN-X0363, CH 1,DTD 13JAN84. (NO PID)

03-Mar-1995 10

CORPUS CHRISTI, TX

QC000000

CCADACFT EXTERIOR PAINTED WITH LOW-REFLECTIVE POLYURETHANE ACFT GREEN,MIL-C-46168 IAW TM 55-1500-345-23DTD12JUN86, & ECP# 0245. (NO PID)

03-Mar-1995 11

CORPUS CHRISTI, TX

QC000000

CCADNEXT PMS-2 #6 DUE AT 2994.3 ACFT HOURS.(NO PID)

03-Mar-1995 12

CORPUS CHRISTI, TX

QC000000

CCADACFT COMPLETEDREFURBISHMENT/STANDARDIZATIONPROGRAM 03MAR95 BY CCAD AT 2494.3 ACFTHOURS IAW ATCOM SOW DTD 05AUG93WHICH INCLUDED MW01-1520-237-55/7 ANDPMS-2 #5. (NO PID)

03-Mar-1995 13

CORPUS CHRISTI, TX

QC000000

CCADTHIS ACFT HAS DEVIATION INCORPORATEDBASED ON COMMODITY COMMANDENGINEERING DECISIONS REACHED ATCCAD. APPLICATION OF THIS DEVIATION ISNOT AUTHORIZED TO BE PERFORMED ATOTHER FACILITIES. THIS ATCOMENGINEERING CALL/DIRECTIVE (AEC/AED) DONOT COMPROMISE THE INTEGRITY OF THISACFT & IS DESCRIBED BELOW FORIDENTIFICATION PURPOSES ONLY: (1) R/HINTERCOASTAL, PN 70202-01009-101, AED-A1617 HAS BEEN WRITTEN TO CHG CMWR TOALLOW STANDARD ANGLE REPAIR IAWATCOM ENG CALL#A7434DTD16FEB95,SIGNED T.ISAACS (NO PID)

03-Mar-1995 14

CORPUS CHRISTI, TX

QC000000

AASF #1UH-60-95-ASAM-06 (TB 1-1520-237-20-168) ONETIME AND RECURRING INSP FOR CRACKEDMAIN TRANSMISSION BEAMS, UPPER DECKSKIN CRACKS. COMPL 2507.5 ACFT HRS (NOPID)

13-Jul-1995 1

TOPEKA, KANSAS

QC000000



8.7.DATE

6.REMARKS

4. 5.



AASF #1UH-60-96-01 SOF CHANGE IN RET. LIFE OFFOR. BELLCRANK SUP. P/N -048 MANUF. BYHMW AND REMOVAL OF SPECIFIED SN FOR.BELLCRANK SUP. ASSY C/W AT 2510A/CHOURS. (NO PID)

08-Nov-1995 1

TOPEKA, KANSAS

QC000000

AASF #1UH-60-96-SOF-02 (TB 1-1520-237-20-173) ONE-TIME INSP FOR SUSPECT TAIL ROTORINBOARD RETENTION PLATES, C/W 2510.2 A/CHOURS. (NO PID)

28-Nov-1995 1

TOPEKA, KANSAS

QC000000

AASF #1UH-60-95-ASAM-08 ONE TIME INSP OF GGROTORS WITH USED BLADES C/W AT 2510.2HOURS (NO PID)

29-Nov-1995 1

TOPEKA, KANSAS

QC000000

AASF #1UH-60-95-ASAM-07, INSP ALL GUNNER/TROOPSEATS UPPER ATTENUATION WIRES ANDATTENUATOR ROLLER ASSY, C/W 2510.2ACFT HOURS (NO PID)

30-Nov-1995 1

TOPEKA, KANSAS

QC000000

AASF #1S0F UH-60-96-03 CERTAIN M/R BLADE CUFFSHAVE REDUCED RET. LIFE C/W AT 2510.2HOURS C/W 2510.2 ACFT HOURS. (NO PID)

05-Dec-1995 1

TOPEKA, KANSAS

QC000000

AASF #1UH-60-96-ASAM-02 (TB 1-1520-237-20-171) ONE-TIME INSPECTION FOR SUSPECT MAINROTOR SHAFT NUT BOLTS. C/W 2510.2 ACFTHOURS. (NO PID)

26-Dec-1995 1

TOPEKA, KANSAS

QC000000

AASF #1UH-60-96-SOR-04 (TB 1-1520-237-20-175)REMOVAL OF SPECIFIC SERIAL NUMBEREDAFT BELLCRANK SUPT ASSYS. C/W 2510.2ACFT HOURS. (NO PID)

16-Jan-1996 1

TOPEKA, KANSAS

QC000000

AASF #1UH-60-96-ASAM-03 C/W ON UH-60-96-ASAM-02(NO PID)

17-Jan-1996 1

TOPEKA, KANSAS

QC000000

AASF #1UH-60-96-ASAM-04 (TB 1-1520-237-20-176). TOREVISE OPERATIONAL LOAD LIMITS ON FASTROPE INSERT/EXTR ACTION SYS. C/W 2510.2ACFT HOURS. (NO PID)

31-Jan-1996 1

TOPEKA, KANSAS

QC000000

AASF #1UH-60-96-ASAM-05 CHANGE CERTAIN SERIALNUM FOR BELLCRANK SUPPORT ASSY FROM500 TO 1800 HR TBO C/W AT 2519.3 ACFT HRS.(NO PID)

19-Jul-1996 1

TOPEKA, KANSAS

QC000000

AASF #1UH-60-96-ASAM-07 REPLACE CERTAIN SN#SPINDLE ASSEMBLIES WITHINREQUIREMENTS OF ASAM C/W AT 2522.7ACFT HOURS. (NO PID)

05-Sep-1996 1

TOPEKA, KANSAS

QC000000

AASF #1UH-60-96-ASAM-08 SERIAL NO. VERIFICATIONOF CERTAIN PART NO. INBOARD T/R RET.PLATE C/W AT 2522.7 ACFT HOURS. (NO PID)

06-Sep-1996 1

TOPEKA, KANSAS

QC000000

AASF #1UH-60-96-ASAM-11 (TB-1-1520-237-20-183)MAINT MANDATORY INCREASE IN FATIGUELIFE OF CERTAIN M/R BLADE CUFFS, C/W2529.1 ACFT HOURS. (NO PID)

10-Oct-1996 1

TOPEKA, KANSAS

QC000000



8.7.DATE

6.REMARKS

4. 5.



AASF #1UH-60-96-ASAM-10 (TB 1-1520-237-20-182)ESTABLISH REQUIREMENTS FORREPLACEMENT OF TEFLON SLEEVE BEARINGIN THE SPHERICAL ELASTOMERIC BEARINGASSEMBLY AT EVERY 500 HOURS PMS-2INSPECTION, C/W 2524.9 ACFT HOURS. (NOPID)

10-Oct-1996 2

TOPEKA, KANSAS

QC000000

AASF #1UH-60-97-ASAM-02 (TB-1-1520-237-20-184) ONE-TIME INSP TAIL ROTOR DRIVE FLEXCOUPLINGS, C/W 2542.0 ACFT HOURS (NOPID)

11-Dec-1996 1

TOPEKA, KANSAS

QC000000

AASF #1UH-60-97-ASAM-04 CERTAIN M/R CUFF TBOTIME TO 2400 HRS C/W AT 2552.0 ACFT HRS(MT4634)

03-Jan-1997 1

TOPEKA, KS

QC000000

AASF #1UH-60-97-01 S0F REMOVAL OF CERTAINREWORKED M/R SWASHPLATE ASSYS C/W AT2552.0 ACFT HRS (MT4634)

03-Jan-1997 2

TOPEKA, KS

QC000000

AASF #1UH-60-97-ASAM-01 (TB 1-1520-237-20-181)INSPECTION OF MAIN ROTOR HUB ASSYSFOR PROPER EDGE BREAK, C/W 2558.2 ACFTHRS. (GP9820)

06-Feb-1997 1

TOPEKA, KS

QC000000

AASF #1UH-60-97-ASAM-05 (TB 1-1520-237-23-3) ONETIME INSPECTION OF VISCOUS DAMPER BRGSUPPORT ASSEMB- LIES, C/W 2558.2 ACFTHRS. (GP9820)

08-Feb-1997 1

TOPEKA, KS

QC000000

AASF #1UH-60-97-ASAM-06 (TB 1-1520-237-20-3189)INSP LATERAL BELLCRANK ASSYS FORCERTAIN S/N'S REDUCED RETIREMENTLIFE,C/W 2558.2 ACFT HRS. (GP9820)

12-Feb-1997 1

TOPEKA, KS

QC000000

AASF #1UH-60-97-ASAM-07 (TB 1-1520-237-20-188)REMOVE FROM SERVICE ALL T/R SERVO CYLASSYS WITH CERTAIN S/N'S, C/W 2558.2 ACFTHRS. (GP9820)

13-Feb-1997 1

TOPEKA, KS

QC000000

AASF #1UH-60-97-ASAM-08 (TB 1-1520-237-20-187)CERTAIN CONNECTING LINK ASSYS MUST BEREMOVED FROM SERVICE C/W AT 2558.2ACFT HRS (GP9820)

13-Feb-1997 2

TOPEKA, KS

QC000000

AASF #1UH-60-97-ASAM-09 (TB 1-1520-237-20-190)INSPECT ALL MAIN ROTOR SHAFTEXTENSION ASSYS C/W AT 2558 ACFT HRS(GP9820)

18-Feb-1997 1

TOPEKA, KS

QC000000

AASF #1UH-60-97-ASAM-10 FATIGUE LIFE CHANGE OFCERTAIN MAIN SUPPORT BRIDGES C/W AT2558.2 ACFT HRS (GP9820)

20-Feb-1997 1

TOPEKA, KS

QC000000

AASF #1UH-60-97-ASAM-11 (TB 1-1520-237-20-192)INCREASE IN FATIGUE LIFE FOR THE M/RBLADE CUFFS C/W AT 2563.6 ACFT HRS(GP9820)

11-Mar-1997 1

TOPEKA, KS

QC000000

AASF #1UH-60-97-ASAM-13 (TB 1-1520-237-20-194) ONETIME INSP OF M/R SPINDLE SPHERICALELASTROMIC BEARING C/W AT 2593.6 ACFTHRS (GP9820)

10-Jul-1997 1

TOPEKA, KS.

QC000000



8.7.DATE

6.REMARKS

4. 5.



AASF #1UH-60-97-ASAM-14 (TB 1-1520-237-20-195) INSPALL ACFT FOR BELLCRANK SUPPORTS FORCERTAIN P/N AND REMOVE C/W AT 2596.2ACFT HRS (GP9820)

02-Sep-1997 1

TOPEKA, KS.

QC000000

AASF #1UH-60-97-ASAM-15 (TB 1-1520-237-20-196) INSPALL ACFT FOR CERTAIN BRG ROD END P/NAND REMOVE C/W AT2596.2 ACFT HRS(GP9820)

02-Sep-1997 2

TOPEKA, KS.

QC000000

AASF #1UH-60-97-ASAM-17 (TB 1-1520-237-20-199) INSPALL ACFT WITH THE INTERNAL RESCUEHOIST BRACKET ASSY C/W AT 2596.2 ACFTHRS (GP9820)

03-Sep-1997 1

TOPEKA, KS.

QC000000

AASF #1UH-60-96-ASAM-09 (TB 1-1520-237-20-180)VISUALLY INSP ALL STABILATOR ACTUATORCLEVISES BY NEXT PMS 2 C/W AT 2596.2ACFT HRS (GP9820)

03-Sep-1997 2

TOPEKA, KS.

QC000000

AASF #1UH-60-97-ASAM-18 (TB 1-1520-237-20-201)INSPECT SWASHPLATE ASSY SN# TOREMOVE SUSPECT ASSY C/W AT 2596.2 ACFTHRS (GP9820)

11-Sep-1997 1

TOPEKA, KS.

QC000000

AASF #1UH-60-98-ASAM-03 VERIFY MANUFACTURESCAGE CODE ON THE SWASHPLATE LINK PN70400-08110-54 C/W (MT4634)

30-Oct-1997 1

TOPEKA, KS.

QC000000

AASF #2ONE TIME INSP FOR REWORKED PRIMARY,YAW & COLLECTIVE BOOST, & T/R SERVOS(XD8508)

14-Apr-1998 1

SALINA, KS. 67401

QC000000

AASF #2"JACE"/CPC PERFORMED AT 2654 ACFTHOURS BY TEAM MEMBER "N" AMCOMDLR/MWO BRANCH HUNTSVILLE, AL. (DS5651)

01-Sep-1998 1

SALINA, KS

QC000000

AASF #2UH-60-98-ASAM-07 (TB 1-1520-237-20-206) ONETIME INSPECTION OF LEFT TIE ROD P/N 70400-08115-043 FORCAGE CODE 3R021 C/W(XD8508)

30-Sep-1998 1

SALINA, KS. 67401

QC000000

AASF #2UH-60-99-ASAM-03 TB 1-2840-248-20-22 ALLUH-60A AND EH-60A SERIES HELICOPTERSONE TIME INSPECTION OF ALL T700-GE-700ENGINES RECORDS CW (XS9537)

24-Nov-1998 1

SALINA, KS

QC000000

AASFUH-60-99-ASAM-06 VISUALLY INSPECT PITCHHORNS FOR CERTAIN SERIAL NUMBERS ANDREDUCE RETIREMENT LIFE TO 2500 HRS(XF3938)

29-Dec-1998 1

LINCOLN NE

QC000000

AASFUH-60-99-ASAM-05 ONE TIME INSPECTION OFTHE SPINDLE BEARING ASSEMBLY P/N 70102-08100-044/056 FOR THE EXISTANCE OF THESLEEVE BEARING PN SB5203-202 (XF3938)

29-Dec-1998 2

LINCOLN NE

QC000000

ARMY AVIATIONSUPPORT FACILITY #2

RECURRING INSPECTION OF MAIN ROTORHUB ASSYS FOR PROPER EDGE BREAK, C/W(XD8508)

30-Mar-1999 1

SALINA, KANSAS 67401

QC000000

AASF #2UH-60-99-ASAM-07 TB 1-1520-237-20-212 INSPOF M/R HUB ASSY C/W (XS9537)

08-Apr-1999 1

SALINA, KS

QC000000



8.7.DATE

6.REMARKS

4. 5.



AASF #2UH-60-99-ASAM-08 TB 1-1520-237-20-211 ALL H-60 ACFT REVISED RETIREMENT LIFE OFBELLCRANK SUPPORT ASSY P/N 70400-08162-042/043/045 MANUFACTURED BY AIRINDUSTRIES CAGE 8L513 C/W AT 2708.3(XS9537)

11-Jun-1999 1

SALINA, KS

QC000000

AASF #2JACE/CPC PERFORMED AT 2741 ACFT HRS ATBY TEAM MEMBER N AMCOM OLR/MWOBRANCH KILLEEN, TX (DS5651)

14-Jul-1999 1

SALINA, KS. 67401

QC000000

AASF #2UH-60-99-ASAM-09 (TB1-1520-237-20-214) ONETIME INSPECTION OF THE MAIN ROTORBLADE EXPANDABLE PINS P/N 70103-08107-101/102/103 (XD8508)

29-Jul-1999 1

SALINA, KS. 67401

QC000000

AASF #2UH-60-99-ASAM-10 (TB1-1520-237-20-213)INSPECTION AND PREVENTIVE MAINTENANCEON THE NUMBER TWO CROSSFEEDBREAKAWAY VALVE, P/N 70307-03006-103(XD8508)

06-Aug-1999 1

SALINA, KS. 67401

QC000000

AASF #2UH-60-99-ASAM-11 (TB1-2840-248-20-23) ONETIME INSPECTION OF T700-GE-700/701/701CENGINES (XD8508)

06-Aug-1999 2

SALINA, KS. 67401

QC000000

AASF #2UH-60-99-ASAM-12 TB 1-2840-248- ALL UH-60A,EH-60A AND UH-60Q ACFT INSPECTIONINTERVAL CHANGE FOR HAMILTONSTANDARD HYDRO MECHANICAL UNITS HMUC/W 2753.7 ACFT HRS. #1 ENG S/N GEE306985HMU S/N J7341 #2 ENG S/N GEE307920 HMUS/N UDA96531 (XS9537)

19-Aug-1999 1

SALINA, KS

QC000000

AASF #2UH-60-00-ASAM-01 (TB 1-1520-237-20-215)RIVISION OF UH-60-99-ASAM-07 RECURRINGINSP OF M/R HUB ASSY FOR PROPER EDGEBREAK C/W AT 2788.5 ACFT HRS (XD8508)

22-Nov-1999 1

SALINA, KS. 67401

QC000000

AASF #2UH-60-00-ASAM-02 (TB 1-1520-237-20-216) ALLH-60,SONE TIME INSPECTION OF CYCLICSTICK WIRE BUNDLES FOR CLEARANCE ANDCHAFFING. (XD8508)

15-Dec-1999 1

SALINA, KS. 67401

QC000000

AASF #2UH-60-99-ASAM-10 (TB 1-1520-237-20-213) #2CROSSFEED BREAKAWAY VALVE REPLACEDAT 2794.4 ACFT HRS 16 DEC 99 (XS9537)

16-Dec-1999 1

SALINA, KS. 67401

QC000000

AASF #2UH-60-ASAM-03 TB 1-1520-237-20-217 INSP &REMOVAL OF SUSPECT PRIMARY SERVOASSY C/W 2815.7 ACFT HRS HRSRS (XS9537)

06-Jan-2000 1

SALINA, KS

QC000000

AASF #2INSPECT TAIL LANDING GEAR STRUT I/A/WUH-60-00-ASAM-04 COMPLETED 03 MAR00TENTION PIN COMPLIED WITH (XD8508)

03-Mar-2000 1

SALINA, KS. 67401

QC000000

AASF #2UH-60-00-ASAM-05 (TB 1-1520-237-20-219) INSPFIRE EXTINGUISHER WIRING FOR CORRECTMARKING AND ROUTING C/W AT 2863.1 ACFTHRS (XD8508)

23-May-2000 1

SALINA, KS

QC000000

AASF #2UH-60-00-ASAM-06 (CHG 1 TO TB 1-1520-237-20-219) INSP FIRE EXTINGUISHER WIRING FORCORRECT MARKING AND ROUTING C/W AT2901.0 ACFT HRS (XD8508)

27-Jun-2000 1

SALINA, KS

QC000000



8.7.DATE

6.REMARKS

4. 5.



AASF #2UH-60-00-01 TB 1-1520-237-20-221 ALL H-60AIRCRAFT INITIAL AND RECURRINGINSPECTION OF MAIN ROTOR SPINDLE LUGSC/W (XS9537)

13-Jul-2000 1

SALINA, KS

QC000000

AASF #2UH-60-00-02 (TB 1-1520-237-20-222) INSP INPUTMODULE RECORDS C/W AT 2912.6 ACFT HRS(XD8508)

03-Aug-2000 1

SALINA, KS. 67401

QC000000

AASF #2UH-60-00-ASAM-07 TB 1-1520-237-20-224, ONETIME INSPECTION OF WIRE HARNESSESCONNECTING THE NO. 1 AND NO. 2 JUNCTIONBOXES THAT HAVE BEEN REFURBISHED C/W(XS9537)

21-Sep-2000 1

SALINA, KS

QC000000

AMCOM OLR/MWOBRANCH

ACE/CPCE PERFORMED AT 2960 ACFT HRSBY TEAM MEMBER K/W AMCOM OLR/MWOBRANCH KILLEEN, TX (JP2527)

16-Oct-2000 1

SALINA, KS

QC000000

AASF #2UH-60-01-01 (TB 1-1520-237-20-225) INITIALAND RECURRING INSP OF MAIN LANDINGGEAR DRAG BEAM ASSY AND DECREASETORQUE ON THE JACKPAD NUT C/W (XD8508)

08-Nov-2000 1

SALINA, KS 67401

QC000000

AASF #2UH-60-01-03 TB 1-1520-237-20-229 INSPECTIONAND REMOVAL OF LATERAL SERVOBELLCRANK ASSEMBLY MANUFACTURED BYTHE PURDY MACHINE COMPANY CAGE CODE15152 C/W (XS9537)

05-Jan-2001 1

SALINA,KS 67401

QC000000

AASF #2UH-60-01-04 TB 1-1520-237-20-228 INSPECTFOR INSTALLATION OF FUEL MONITORINGSYSTEM C/W (XS9537)

05-Jan-2001 2

SALINA, KS

QC000000

AASF #2UH-60-01-02 TB 1-1520-237-20-225, REVISIONTO UH-60-01-01, INITIAL AND RECURRINGINSPECTION OF MAIN LANDING GEAR DRAGBEAM ASSY AND DECREASE TORQUE ON THEJACKPAD NUT C/W AT 3167.4 ACFT HRS.(XS9537)

15-Jan-2001 1

SALINA,KS 67401

QC000000

AASF #2UH-60-01-05 TB 1-1520-237-20-230 ALL H-60AIRCRAFT REVISION TO UH-60-00-01INSPECTION OF MAIN ROTOR SPINDLE C/WAT 3001.0 ACFT HRS. (XS9537)

23-Mar-2001 1

SALINA, KS

QC000000

AASF #2UH-60-01-06 TB 1-1520-237-20-231 ALL H-60SERIES AIRCRAFT, INSPECTION OF ALL SASACTUATORS C/W AT 2994.0 ACFT HRS.(XS9537)

27-Mar-2001 1

SALINA, KS

QC000000

AASF #2PMS-2 COMPLETED AT 2994.0 ACFT HRS NEXTPMS-2 WILL BE DUE AT 3494.0 ACFT HRS.(XS9537)

04-Apr-2001 1

SALINA, KS

QC000000

AASF #2UH-60-01-SOF-12 (TB1-1520-237-20-236) INSPEXPANDABLE PIN IAW MSG PRIOR TO NEXTFLT BUT NLT 27 AUG O1. (XD8508)

24-Apr-2001 1

SALINA, KS 67401

QC000000

AASF #2UH-60-01-07 TB 1-1520-237-20-232 ALL H-60SERIES AIRCRAFT, INPSECTION OF MAINROTOR FLIGHT CONTROL SELF LOCKINGBOLTS C/W AT 3052.1 ACFT HRS (XS9537)

29-May-2001 1

SALINA, KS

QC000000



8.7.DATE

6.REMARKS

4. 5.



AASF #2UH-60-01-08 TB 1-1520-237-20-232 REVISIONTO UH-60-01-07 INSPECTION OF MAIN ROTORFLIGHT CONTROL SELF LOCKING BOLTS C/W3052.1 ACFT HRS (XS9537)

13-Jun-2001 1

SALINA, KS

QC000000

AASF #2UH-60-01-09 TB 1-1520-237-20-233 ONE TIMEINSPECTION OF MAIN ROTOR BLADEEXPANDABLE PINS C/W AT 3052.1 ACFT HRS.(XS9537)

13-Jun-2001 2

SALINA, KS 67401

QC000000

AASF #2UH-60-01-10 TB 1-1520-237-20-234 ONE TIMEINSPECTION OF MAIN ROTOR BLADEEXPANDABLE PINS C/W AT 3068.7 ACFT HRS.(XS9537)

17-Jul-2001 1

SALINA, KS

QC000000

AASF #2UH-60-01-11 TB 1-1520-237-20-235 DECREASETHE INTERVAL BETWEEN REQUIRED INSP OFM/R HUB ASSY FOR CRACKS IN SPECIFIEDAREAS FROM 200 TO 100 HRS ANDIMPLEMENT A BEFORE 1ST FLT OF DAYVISUAL INSP OF THE VISIBLE AREA OF HUBNEAR THE 11:00 BOLT HOLE (XD8508)

24-Aug-2001 1

SALINA, KS. 67401

QC000000

AASF #2UH-60-01-12 TB 1-1520-237-20-236 INSPEXPANDABLE ;INS IAW MSG PRIOR TO NEXTFLIGHT BUT NLT 27AUG01 (XD8508)

24-Aug-2001 2

SALINA, KS

QC000000

AASF#2ACE/CPCE PERFORMED AT 3120 ACFT HRS.BY TEAM MEMBERS W & TT. AMCOMPROJECT OLR.KILLEEN, TX (JP2527)

27-Sep-2001 1

SALINA, KANSAS

QC000000

AASF #2UH-60-02-ASAM-01 TB 1-1520-237-20-239 H-60SERIES, INITIAL AND RECURRINGINSPECTION OF THE TAIL ROTOR FAIRINGASSEMBLY C/W AT 3139.6 ACFT HRS (XS9537)

16-Nov-2001 1

SALINA, KS

QC000000

AASF # 2INSPECT OIL COOLER FAN SHAFT ASSEMBLYFORWARD MOUNT FLANGE IAW UH-60-02-01(TB 1-1520-237-20-240) PRIOR TO NEXTFLIGHT, BUT NLT 30 NOVEMBER 2001,COMPLETED 19 NOV. 01 AT 3143.0 ACFT HRS.(XD8508)

19-Nov-2001 1

SALINA, KS. 67401

QC000000

AASF #2UH-60-02-03 TB 1-1520-237-10-241 ALL H-60SERIES AIRCRAFT ONE TIME INSPECTION OFTHE FLIGHT CONTROL SYSTEM, PITCH TRIMASSEMBLY C/W AT 3147.5 ACFT HRS (XS9537)

13-Dec-2001 1

SALINA, KS

QC000000

AASF # 2UH-60-02-02 (TB1-1520-237-20-237) INSPECTMAIN ROTOR HUB RECORDS AND DATAPLATE FOR REWORK CANDIDATE C/W AT3148 ACFT HRS (XD8508)

15-Dec-2001 1

SALINA, KS. 67401

QC000000

AASF #2UH-60-02-04 (TB1-1520-237-20-242) COMPLIEDWITH AT 3172.8 ACFT HRS (XD8508)

29-Jan-2002 1

SALINA, KS. 67401

QC000000

AASF #2INSP ENGINE CONTROL QUADRANT POWERCONTROL LEVER (PCL) WIRING UH-60-02-ASAM-03 TB 1-1520-237-20-245 C/W AT 3209.5ACFT HRS. (XS9537)

13-Feb-2002 1

SALINA, KS

QC000000

AASF #2INSPECT THE CONTROL ROD JAMNUTS IAWUH-60-02-ASAM-02 TB 1-1520-237-20-246 C/WAT 3180.3 ACFT HRS (XS9537)

13-Feb-2002 2

SALINA, KS

QC000000



8.7.DATE

6.REMARKS

4. 5.



AASF #2INSPECT EXPANDABLE PINS IAW UH-60-02-05TB 1-1520-237-20-243 C/W AT 3197.5 ACFTHRS. (XS9537)

14-Feb-2002 1

SALINA, KS

QC000000

AASF #2UH-60-02-ASAM-04 (TB1-1520-237-20-244)RESTRAINT SYSTEM INSPECTION CW AT3191.9 ACFT HRS (XD8508)

29-Mar-2002 1

SALINA, KS 67401

QC000000

AASF #2UH-60-02-ASAM-05 (TB1-1520-237-20-251)INSPECTION OF M/R SPINDLE ASSY'S CWAT 3197.9 ACFT HRS APR 9 02 (XD8508)

09-Apr-2002 1

SALINA, KS. 67401

QC000000

AASF #2UH-60-02-ASAM-06 TB 1-1520-237-20-252INSPECT SWAGE PINS/COLLARS ON BOOSTSERVO ASSEMBLIES C/W AT 3208.2 ACFTHRS. (XS9537)

19-Apr-2002 1

SALINA, KS

QC000000

AASF #2UH-60-02-07 MAIN MODULE PLANETARYCARRIER ASSEMBLY C/W AT 3209.5 ACFTHRS. (XS9537)

02-May-2002 1

SALINA, KS

QC000000

AASF #2MAIN MODULE PLANETARY CARRIERASSEMBLY UH-60A, EH-60A,UH-60Q UH-60-02-08 TB 1-1520-237-20-255 C/W AT 3209.5 ACFTHRS (XS9537)

07-May-2002 1

SALINA, KS

QC000000

AASF #2MAIN MODULE PLANETARY CARRIERASSEMBLY UH-60A, EH-60A,UH-60Q UH-60-02-09 TB 1-1520-237-20-258 C/W AT 3209.5 ACFTHRS (XS9537)

23-May-2002 1

SALINA, KS

QC000000

AASF #2MAIN MODULE PLANETARY CARRIERASSEMBLY UH-60A, EH-60A,UH-60Q UH-60-02-10 TB 1-1520-237-20- C/W AT 3211.7 ACFT HRS(XS9537)

11-Jun-2002 1

SALINA, KS

QC000000

AASF #2UH-60 SERIES AIRCRAFT INSPECT AN/ARC-220 WIRING FOR CHAFING UH-60-02-ASAM-08TB 1-1520-237-20-256 C/W AT 3254.2 ACFTHRS. (XS9537)

14-Jun-2002 1

SALINA, KS

QC000000

AASF #2H-60 SERIES AIRCRAFT TAIL ROTORQUADRANT HARDWARE INSTALLATION UH-60-02-ASAM-09 TB 1-1520-237-20-257 C/W AT3221.8 ACFT HRS 20020815 (XS9537)

15-Jun-2002 1

SALINA, KS

QC000000

AASF #2UH-60-02-11 TB 1-1520-237- ONE TIMEINSPECTION OF MAIN ROTOR BLADE CUFFASSEMBLY C/W AT 3221.8 ACFT HRS (XS9537)

12-Aug-2002 1

SALINA,KS

QC000000

AASF #2UH-60-02-12 TB 1-1520-237- REVISION TO UH-60-02-11 ONE TIME INSPECTION OF MAINROTOR BLADE CUFF ASSEMBLY C/W AT3221.8 ACFT HRS (XS9537)

13-Aug-2002 1

SALINA, KS

QC000000

DYN CORPACE/CPCE PERFORMED AT 3232 ACFT HRSBY TEAM MEMBERS K&W AMCOM PROJECTOLR. (JP2527)

26-Sep-2002 1

KILLEEM TX 76543

QC000000

AASF #2INSPECT AN/ARC-220 WIRING FOR CHAFINGUH-60-02-ASAM-11 TB 1-1520-237-20-261 C/W A3231.5 ACFT HRS (XD8508)

27-Sep-2002 1

SALINA, KS 67401

QC000000

PROJECT OLRINSTALLATION OF THE 90 DEGREEBACKSHELL I/A/W UH-60-02-ASAM-11COMPLETED (JC1523)

15-Nov-2002 1

KILLEEM TX 76543

QC000000



8.7.DATE

6.REMARKS

4. 5.



AASF # 2UH-60-03-ASAM-01 BELLCRANK SUPPORTASSY RETIREMENT LIFE C/W AT 3391.0 ACFT.HRS. (JD8508)

16-Dec-2002 1

SALINA, KS.

QC000000

AASF # 2UH-60-03-ASAM-02 TAIL ROTOR SERVORETIREMENT LIF C/W AT 3391.0 ACFT. HRS.(JD8508)

16-Dec-2002 2

SALINA, KS.

QC000000

AASF # 2UH-60-03-ASAM-02 TAIL ROTOR SERVORETIREMENT LIFE AT 3291.3 ACFT HRS.(JD8508)

20-Jan-2003 1

SALINA, KS.

QC000000

AASF # 2UH-60-03-02 COMPLIED WITH ON MAIN ROTORBLADE CUFF BOLTS. INSPECT FORCORROSION AND CRACKS. (JD8508)

23-Jan-2003 1

SALINA, KS.

QC000000

AASF # 2UH-60-03-03 PERFORMANCE PLANNINGDURING DESERT OPS N/A (JD8508)

21-Feb-2003 1

SALINA, KS.

QC000000

DYN CORPACE/CPCE PERFORMED AT 3391 ACFT HRSBY TEAM MEMBERS K&I AMCOM PROJECTOLR. (JP2527)

10-Sep-2003 1

KILLEEM TX 76543

QC000000

AASF # 2UH-60-04-01 FWD BELLCRANK SUPPORTINSTALLATION HARDWARE C/W AT 3396.4ACFT HRS. (JD8508)

08-Oct-2003 1

SALINA, KS.

QC000000

AASF #2UH-60-04-ASAM-01 ALL UH-60A/L, GLARESHIELD LIGHTING CIRCUIT BREAKERREPLACEMENT C/W AT 3493.0 ACFT HRS.(XS9537)

29-Jan-2004 1

SALINA,KS

QC000000

ARMY AVIATIONSUPPORT FACILITY #2

UH-60-04-ASAM-02, LOOSE NUTS ON TAILROTOR DIVE SHAFT, N/A BY ACFT HRS ANDS/N (XD8508)

01-Apr-2004 1

SALINA, KS 67401

QC000000

AASF #2PMS-2 COMPLETED AT 3493 ACFT HRS. NEXTPMS-2 WILL BE DUE AT 3993.0 ACFT HRS(XS9537)

07-Apr-2004 1

SALINA,KS

QC000000

AASF #2UH-60-04-ASAM-03 ALL H-60 SERIESAIRCRAFT, FUEL SYSTEM INTEGRITYCHECKS, COMPLETED AT ACFT HRS (XS9537)

08-Apr-2004 1

SALINA, KS

QC000000

AASF # 2UH-60-04-02 DISABLING OF COCKPIT AIRBAGSYSTEM AT 3542.7 ACFT. HRS. (JD8508)

16-Jun-2004 1

SALINA, KS.

QC000000

AASF # 2UH-60-04-03 CRASHWORTHY EXTERNAL FUESYSTEM NA THIS ACFT AT 3549.8 ACFT. HRS.(JD8508)

30-Jun-2004 1

SALINA, KS.

QC000000

DYNCORP OLRACE/CPCE PERFORMED AT 3558 ACFT HRSBY TEAM MEMBERS K&W AMCOM PROJECTOLR.KILLEEN, TX (JP2527)

07-Jul-2004 1

KILLEEN TX 76543

QC000000

ASF # 2UH-60-04-04 MAIN ROTOR HUBSUBASSEMBLY REWORK C/W AT 3575..0ACFT. HRS. (JD8508)

17-Aug-2004 1

SALINA, KS.

QC000000

AASF # 2UH-60-04-ASAM-04 FUEL SYSTEM INTEGRITYCHECK REVISED AT ACFT. HRS. (JD8508)

18-Aug-2004 1

SALINA, KS.

QC000000

AASF # 2UH-60-04-ASAM-05 RESTRAINT SYSTEMINSPECTION C/W AT 3591.1 ACFT. HRS.(JD8508)

28-Sep-2004 1

SALINA, KS.

QC000000



8.7.DATE

6.REMARKS

4. 5.



AASF # 2UH-60-05-ASAM-01 REVISED FUEL SYSTEMINTEGRITY CHECK ACFT. HRS. (JD8508)

07-Jan-2005 1

SALINA, KS.

QC000000

AASF # 2UH-60-05-ASAM-02 BLUE FORCE TRACKERN/A THIS ACFT. AT 3641.0 ACFT. HRS. (JD8508)

03-Mar-2005 1

SALINA, KS.

QC000000

ASF # 2UH-60-05-01 REACTIVATION OF COCKPITAIRBAG NA THIS ACFT AT 3654.7 ACFT. HRS.(JD8508)

17-Mar-2005 1

SALINA, KS.

QC000000

AASF # 2UH-60-05-ASAM-03 AIRCREW RESTRAINTSYSTEM COMPATIBILITY C/W AT 3656.8 ACFT.HRS. (JD8508)

07-Apr-2005 1

SALINA, KS.

QC000000

AASF # 2UH-60-05-ASAM-04 TAIL LANDING GEAR YOKEASSY N/A BY P/N AT 3656.8 ACFT. HRS.(JD8508)

12-Apr-2005 1

SALINA, KS.

QC000000

AASF # 2UH-60-05-ASAM-05 TIE ROD ASSY C/W AT3661.2 ACFT. HRS. (JD8508)

03-May-2005 1

SALINA, KS.

QC000000

AASF # 2UH-60-05-ASAM-06 TROOP SEAT RESTRAINTBUCKLE C/W AT 3661.2 ACFT. HRS. (JD8508)

03-May-2005 2

SALINA, KS.

QC000000

DYNCORP OLRACE/CPCE PERFORMED AT 3665 ACFT HRSBY TEAM MEMBERS K&W AMCOM PROJECTOLR.KILLEEN, TX (JP2527)

19-May-2005 1

KILLEEN TX 76543

QC000000

AASF # 2UH-60-05-ASAM-08 TIE ROD REINSPECTIONC/W AT 3673.1 ACFT. HRS. (JD8508)

07-Jun-2005 1

SALINA, KS.

QC000000

AASF #2UH-60-05-02 ENHANCED SCHEDULEDMAINTENANCE PROGRAM C/W AT 3675.0ACFT. HRS. (BM7522)

21-Jun-2005 1

SALINA KS 67401

QC000000

AASF # 2UH-60-05-ASAM-07 AIR INTRUSION OFHYDRAULIC SYSTEM C/W AT 3677.6 ACFT.HRS. (JD8508)

28-Jun-2005 1

SALINA, KS.

QC000000

AASF # 2UH-60-05-ASAM-09 CRASHWORTHYEXTERNAL FUEL SYSTEM (CEFS)INSTALLATION BOLTS, (JD8508)

03-Aug-2005 1

SALINA, KS. 67401

QC000000

AASF #2C/W REQUIREMENTS OF UH-60-05-ASAM-10N/A BY S/N (JD8508)

21-Aug-2005 1

SALINA, KS. 67401

QC000000

AASF #2C/W REQUIREMENTS OF UH-60-05-ASAM-11AT ACFT HRS (JD8508)

29-Sep-2005 1

SALINA, KS. 67401

QC000000

AASF #2UH-60-06-ASAM-01 TAIL LNDING GEAR SHOCKSTRUT. COMPLIED WITH AT 3791.2ACFT HRS--DATE 12 MAY 2006 JDH

14-Dec-2005 1

SALINA, KANSAS

JM884376

AASF #2ISAQ 121, UH-60A WITH MAIN MODULEASSEMBLIES P/N 70351-08100-075 & 076EQUIPED WITH IMPROVED MAINTRANSMISSION PLANETARY CARRIERASSEMBLY, P/N 70351-08175-046.TEMPORARY AS WELL AS PERMANENTCHANGES TO CONFIGURATIONS.

02-Feb-2006 1

SALINA, KS. 67401

JD508508



8.7.DATE

6.REMARKS

4. 5.



AASF #2AWR 548, UHH-60A AIRCRAFT EQUIPPEDWITH RT-1518C/ARC-164 HAVE QUICK II (HQII)UHF/AM RADIO. SUCCESSFUL COMPLETIONOF EMCTEST AND DAILY INSPECTION, ANDINCLUDES TEMPORARY OR PERMANENTCHANGES IN CONFIGURATION

02-Feb-2006 2

SALINA, KS. 67401

JD508508

CO.B 449TH ASB, 36CAB AVIM

UH-60-06-ASAM-02 MAIN ROTOR RIGIDCONNECTING LINK/ PITCH CONTROLASSEMBLIES--COMPLIED WITH AT 3791.2ACFT HRS--UPPER CADMIUM PLATED STEELNUTS--JDH

13-May-2006 1

FT.HOOD,TX

JH430868

CO.B 449TH ASB, 36CAB

ACFT RIGG CHECKED AND VERIFIED I/A/WTM1-1520-237-6 PARA 11-4-42, 11-4-58. RIGGCHECK DONE WITH BLADES OFF, .5 WASADDED TO READINGS. MIXER ROD RIGG PINSTOPS AT THE ROLL CONTROL ROD IN MIXERWHEN BIAS IS PUT IN. READINGS ARE--LCANGLE -.05, HC ANGLE 16.15, FC ANGLE 33.2,LC ANGLE 7.8 (15.6), RT C ANGLE 7.3 (14.6)--T/R BIAS RED--5.060, BLUE 4.568, YELLOW5.080, BLACK 4.557---JH430868

19-May-2006 1

FT.HOOD, TX 76544

JH430868

CO.B 449TH ASB, 36THCAB

ACE/CPCE PERFORMED AT 3791 ACFT HRSAT FT. HOOD, TX BY ACE TEAM MEMBER C

19-May-2006 2

FT.HOOD,TX 76544

JH430868

CO. B 449TH, 36 CABPMI-1 COMPLETED AT 3791.2 ACFT HRS. NEXTPMI-2 DUE AT 4141.2 ACFT HRS (GN318165)

27-May-2006 1

FT.HOOD,TX 76544

GN318165

36TH CAB 1-108TH AVNCO.D

UH-60-06-ASAM-03 COMPLIED WITH 14-Jun-2006 1

FT. HOOD, TEXAS

JR759141

36TH CAB 1-108TH AVNCO.D

UH-60-06-ASAM-04 COMPLIED WITH 24-Jun-2006 1

FT. HOOD, TEXAS

JR759141

36 CAB 1-108TH AVNCO.D

UH-60-06-SOF-02 COMPLIED WITH (N/A THISACFT).

25-Jun-2006 1

FT. HOOD, TEXAS

JR759141

36TH CAB 1-108TH AVNCO. D

UH-60-06-ASAM-05 COMPLIED WITH AT 3831.4ACFT HRS.

04-Aug-2006 1

FT. HOOD, TEXAS

JR759141

AASF IDARNGACFT RECEIVED FROM KAARNG @ 3854.5ACFT HRS.

31-Aug-2006 1

BOISE, ID

BJ117531

AASF IDARNGUH-60-06-SOF-01, M/R HUB ASSY C/W @ 3854.5ACFT HRS.

31-Aug-2006 2

BOISE, ID

BJ117531

AASF IDARNGUH-60-07-ASAM-01, WHITE ENGINE CABLEHARNESS REROUTING C/W.

10-Jan-2007 1

BOISE, ID

BJ117531

AASF IDARNGUH-60-07-ASAM-02, REVISION TO UH-60-07-ASAM-01 C/W.

10-Jan-2007 2

BOISE, ID

BJ117531

AASF IDARNGUH-60-07-ASAM-04, AUTOROTATION RPMVERIFICATION C/W.

11-Jan-2007 1

BOISE, ID

BJ117531



8.7.DATE

6.REMARKS

4. 5.



AASF IDARNGUH-60-07-ASAM-03, YAW AND COLLECTIVEBOOST SERVOS ROLL PIN C/W.

17-Jan-2007 1

BOISE, ID

BJ117531

AASF IDARNGUH-60-07-ASAM-05, ARC-220/KY-100 START-UPPROCEDURES C/W.

24-Jan-2007 1

BOISE, ID

BJ117531

AASF IDARNGUH-60-07-ASAM-06, INTERNAL RESCUE HOISTCABLE (GUARD) DEFLECTOR C/W, N/A THISACFT.

09-Feb-2007 1

BOISE, ID

BJ117531

AASF IDARNGUH-60-06-ASAM-02, REPLACEMENT OF M/RP/C LINK JAM NUTS COMPLETED AT 4039.8ACFT HRS.

14-Mar-2007 1

BOISE, ID

BJ117531

AASF IDARNGUH-60-07-ASAM-07, INSTALLATION OF STATICBONDING JUMPERS ON CEFS ACFT C/W. N/ATHIS ACFT.

15-May-2007 1

BOISE, ID

BJ117531

AASF IDARNGUH-60-07-AMAM-01, COMMON MISSILEWARNING SYSTEM (CMWS) C/W.

24-May-2007 1

BOISE, ID

BJ117531

AMCOM PROJECT OLRANNUAL ACE EVALUATION COMPLETED AT3968 ACFT HRS AT FT SILL, OK BY TEAMMEMBERS K & W

18-Jun-2007 1

KILLEEN, TX

JP862527

D CO 1/168 CSABUH-60-07-ASAM-08, SUSPECT HMU C/W AT3984.5 ACFT HRS.

16-Jul-2007 1

FT. SILL, OK

BJ117531

D CO 1/168 CSABUH-60-07-ASAM-09, DEFECTIVE DCU, N/A THISACFT.

23-Jul-2007 1

FT. SILL, OK

BJ117531

36TH CAB 1-108TH AVNCO. D

ERROR 04-Aug-2007 1

FT. HOOD, TEXAS

JR759141

D CO 1/168 CSABUH-60-07-ASAM-10, MAIN FUEL MANIFOLDCHAFING C/W AT 4006.8 ACFT HRS.

31-Aug-2007 1

UAAF, KUWAIT

BJ117531

D CO 1/168 CSABAWR 911 DATED 19 SEP 06, APU IBFINSTALLATION P/C/W, 3989.5 ACFT HRS.

01-Sep-2007 1

UAAF, KUWAIT

BJ117531

D CO 1/168 CSABAWR 1145 DATED 31 JAN 06, BFTINSTALLATION P/C/W, 3989.5 ACFT HRS.

01-Sep-2007 2

UAAF, KUWAIT

BJ117531

D CO 1/168 CSABAWR 1223 DATED 29 MAR 05, IR ANTI-COLLISION LIGHT INSTALLED AT 3989.5 ACFTHRS.

01-Sep-2007 3

UAAF, KUWAIT

BJ117531

D CO 1/168 CSABAWR 1270 DATED 31 AUG 06, EIBF "B" KITINSTALLED AT 3989.5 ACFT HRS.

01-Sep-2007 4

UAAF, KUWAIT

BJ117531

D CO 1/168 CSABAWR 1277 DATED 29 JUL 05, EDMINSTALLATION P/C/W, 3989.5 ACFT HRS.

01-Sep-2007 5

UAAF, KUWAIT

BJ117531

D CO 1/168 CSABAWR 1324 DATED 06 JUN 06, CMWSINSTALLATION P/C/W, 3989.5 ACFT HRS.

01-Sep-2007 6

UAAF, KUWAIT

BJ117531

D CO 1/168 CSABISAQ 108 DATED 01 SEP 06, BPS "B" KITINSTALLED AT 3989.5 ACFT HRS.

01-Sep-2007 7

UAAF, KUWAIT

BJ117531

D CO 1/168 CSABISAQ 114 DATED 28 JAN 05, AIR WARRIOR "B"KIT INSTALLED AT 3989.5 ACFT HRS.

01-Sep-2007 8

UAAF, KUWAIT

BJ117531



8.7.DATE

6.REMARKS

4. 5.



D CO 1/168 AVNERROR 15-Sep-2007 1

UAAF, KUWAIT

BJ117531

D CO 1/168 AVNH-60-08-AMAM-01, MAIN LANDING GEARSHOCK STRUTS C/W AT 4083.2 ABFT HRS.

18-Oct-2007 1

UAAF, KUWAIT

BJ117531

D CO 1/168 AVNH-60-08-ASAM-02, POWER AVAILABLECONTROL CABLE C/W AT 4112.1 ACFT HRS.

06-Nov-2007 1

UAAF, KUWAIT

BJ117531

D CO 1/168 AVNH-60-08-ASAM-01, TROOP/GUNNERS SEATUPPER ENERGY ATTENUATING WIRES C/W AT4151.2 ACFT HRS.

26-Nov-2007 1

UAAF, KUWAIT

BJ117531

D CO 1/168 AVNH-60-08-AMAM-02, TAIL ROTOR OUTBOARDRETENTION PLATE SHIMS C/W AT 4151.2ACFT HRS.

27-Nov-2007 1

UAAF, KUWAIT

BJ117531

D CO 1/168 AVNH-60-08-ASAM-05, TAIL ROTOR QUADRANTSPRING CAPSULE ASSEMBLY INITIALCOMPLIANCE AT 4151.2 ACFT HRS.

12-Dec-2007 1

UAAF, KUWAIT

BJ117531

D CO 1/168 AVNH-60-08-ASAM-04, PILOT'S LOWER SEAT RAILCHAFING ELECTRICAL HARNESS C/W AT4151.2 ACFT HRS.

12-Dec-2007 2

UAAF, KUWAIT

BJ117531

D CO 1-168 AVNH-60-08-AMAM-03, HIGH TEMPERATURESTABILITY (HTS0 OIL, C/W 4151.2 ACFT HRS

21-Dec-2007 1

UAAF, KUWAIT

RN021857

L3PMI-2 COMPLETED AT 4151.2 ACFT HRS. PMI-1 DUE AT 4511.2 ACFT HRS.

27-Dec-2007 1

UAAF, KUWAIT

BJ117531

D CO 1/168 AVNH-60-08-ASAM-03, CHANGES TO CURRENTFUEL SYSTEM INTEGRITY CHECKS C/W AT4151.2 ACFT HRS.

02-Jan-2008 1

UAAF, KUWAIT

BJ117531

D CO 1-168 AVH-60-08-SOF-01, MAIN ROTOR EXPANDABLEPIN INSPECTION CHANGE, C/W 4152.8 ACFTHRS

29-Jan-2008 1

UAAF, KUWAIT

RN021857

D CO 1-168 AVNH-60-08-AMAM-05, GOODRICH INTERNALRESCUE HOISTS, C/W 4152.8 ACFT HRS

29-Jan-2008 2

UAAF, KUWAIT

RN021857

D CO 1-168 AVNH-60-08-AMAM-04, COCKPIT DOORJETTISONABLE WINDOWS, C/W 4152.8 ACFTHRS

29-Jan-2008 3

UAAF, KUWAIT

RN021857

D CO 1/168 AVNH-60-08-AMAM-06, COMMON MISSILEWARNING SYSTEM SEQUENCERS C/W AT4160.3 ACFT HRS.

06-Feb-2008 1

UAAF, KUWAIT

BJ117531

D CO 1/168 AVNH-60-08-ASAM-06, MAIN ROTOR PYLONSLIDING FORWARD FAIRING C/W AT 4186.7ACFT HRS.

05-Mar-2008 1

UAAF KUWAIT

BJ117531

D CO 1-168TH GSABH-60-08-AMAM-07, AN/ASN-128B/D, CW 4223.0ACFT HRS

25-Mar-2008 1

UAAF

RN021857

D CO 1/168 AVNH-60-08-ASAM-08, SELF-RETAINING FLIGHTCONTROL BOLTS C/W AT 4237.5 ACFT HRS.

07-Apr-2008 1

UAAF KUWAIT

BJ117531

D CO 1/168 AVNAWR 1303, DAVID CLARK PASSENGER ICSSYSTEM DATED 26 JUN 06 C/W AT 4277.9ACFT HRS.

06-May-2008 1

UAAF, KUWAIT

BJ117531



8.7.DATE

6.REMARKS

4. 5.



TFAVCRADA3T INSPECTION COMPLETED ON 22 MAY2008 AT 4434.6 ACFT BY TFAVCRADPERSONAL

22-May-2008 1

CAMP BUEHRING,KUWAIT

JH658239

CO D 2-211TH GSABUH-60-08-AMAM-08, FLIGHT CONTROLRIGGING UPDATE COMPLETED, DISCREPANTP/N'S FOUND

23-May-2008 1

CAMP BUERHING,KUWAIT

GM423025

D. CO. 2/211 GSABH-60-08-AMAM-08. REPLACED DISREPANTCABIN FIXED CONTROL ROD WITH P/N 70400-02270-048 NSN 3040-01-137-5522 ACFT HRS4388.6

19-Jul-2008 1

KUWAIT

DS419987

D. CO. 2/211 GSABH-60-08-ASAM-10 COMPLETED 21 JULY 08ACFT HRS 4388.6

22-Jul-2008 1

KUWAIT

DS419987

D CO 2/211TH GSABSOLID M/R BLADE PINS INSTALLED @ 4441.5A/C HOURS. OPERATE UNDER ISAQ 127

21-Aug-2008 1


TM444739

D CO 2/211TH GSABH-60-08-ASAM-11 FLIGHT CONTROL INSP. C/W@ 4441.5 ACFT HOURS. NO DESCREPANTPARTS FOUND

27-Aug-2008 1


TM444739

D 2/211 GSABUH-60-08-ASAM-11 COMPLETED, INSPECTEDOK

27-Aug-2008 2

CAMP BUEHRING

DP323684

L-3 COMMUNICATIONS12 STATION VIP INTERCOM II ICS SYSTEMINSTALLED. FLY IAW AWR 1348 (CURRENTVERSION) UNLESS SUPERCEDED, RECINDED,OR SYSTEM REMOVED.

01-Sep-2008 1

CAMP BUEHRING

HA009430

D CO. 2/211 GSABH-60-08-ASAM-12 COMPLETED NODISCREPANT PARTS INSTALLED ON ACFT

17-Sep-2008 1

KUWAIT

DS419987

D CO 2/211TH GSABPMI 1 COMPLETED AT 4468.1 A/C HOURS.NEXT PHASE (PMI 2) DUE AT 4871.1 A/CHOURS

20-Sep-2008 1


TM444739

D CO. 2/211 GSABH-60 -08-ASAM-13 COMPLETED INSP. PASSACFT HRS 4471.6

24-Sep-2008 1

KUWAIT

DS419987

DS/2INSTALLED CMWS 5TH ELECTRO OPTICALMISSLE SENSOR

08-Oct-2008 1

CAMP BEURING,KUWAIT

JK437168

D CO 2/211TH GSABH-60-09-SOF-01 INSP FOR DESCREPANTHYDRO MECHANICAL UNITS. C/W. NODESCREPANT PARTS INSTALLED.

23-Oct-2008 1


TM444739

D/2-211 TH AVNUH-60-09-SOF-03, INSPECT FOR DISCREPANTRC ITEMS COMPLIED WITH, INSPECT OK

14-Nov-2008 1


GM423025

D CO 2/211TH GSABAIRCRAFT AUTHORIZED TO OPERATECONTRARY TO H-60-09-SOF-02 FOR REMOVALOF ALQ-144S IAW MEMORANDUM DTD 17NOVEMBER 2008 FROM LTC LAMAR BLAIRTHRU ARCENT C3, BG WENDEL, THRUDEPUTY COMMANDING GENERAL, MGANDERSON, CAMP ARIFJAN, KUWAIT

19-Nov-2008 1


TM444739



8.7.DATE

6.REMARKS

4. 5.



D CO 2/211 GSABH-60-09-SOF-02, REMOVAL OF ALQ-144 WITHCMWS A KIT INSTALLED. C/W

19-Jan-2009 1

UAAF CAMP BUEHRING,KUWAIT

DP323684

AASF# 1 NJH-60-09-ASAM-07 FIRE EXTINGUISHER WIRING( BREAKAWAY THREAD)

04-May-2009 2

LAKEHURST, NEWJERSEY 08733

JS889951

AASF#1 NJH-60-09-ASAM-08 ENGINE COWLING WEIGHTLIMIT RESTRICTION

04-May-2009 3


JS889951

AASF#1H-60-09-ASAM-05 UPDATE TO LIFE LIMITCHANGE FOR TAIL ROTOR (TR) QUADRANTSPRING CAPSULES COMPLIED WITH 04 MAY2009

04-May-2009 4


JS889951

DOL AVIMH-60-08-ASAM-09 H-60M SPLINDLE LUG INSP,NA THIS ACFT.

10-Jun-2009 1

FT DRUM NY

FS607593

DOL AVIMH-60-09-SOF-04 H-60K/L/M MAINTRANSMISSION MODULE PLANETARYCARRIER ASSEMBLY, NA THIS ACFT.

10-Jun-2009 2

FT DRUM NY

FS607593

DOL AVIMACE/CPCE INSPECTION COMPLETED @4594.9 ACFT HRS. BY ACE TEAM MEMBER SSAND YY

11-Jun-2009 1

FT DRUM NY

BG625396

DOL AVIMH-60-09-ASAM-09 FIRE EXTINGUISHER WIRING(BREAKAWAY THREAD) (REVISION TO ASAMH-60-09-ASAM-07) C/W AT 4594.9 ACFT HRS.

16-Jun-2009 1

FT DRUM NY

FS607593

DOL AVIMH-60-09-ASAM-10 H-60M M/R SPINDLE LUGINSP. N/A THIS ACFT.

16-Jun-2009 2

FT DRUM NY

FS607593

DOL AVIMH-60-09-ASAM-03 H-60L/M UTILITY MODULEPRESSURE/RETURN LINES. N/A THIS ACFT.

16-Jun-2009 3

FT DRUM NY

FS607593

DOL AVIMH-60-09-ASAM-04 ALL H-60 RESCUE HOISTMARK 44 MOD 0 CARTRIDGE ACTIVATIONDEVICE. N/A THIS ACFT.

16-Jun-2009 4

FT DRUM NY

FS607593

DOL AVIMH-60-09-ASAM-06 ALL H-60M ICS CORD RE-ROUTING. N/A THIS ACFT.

16-Jun-2009 5

FT DRUM NY

FS607593

DOL AVIMH-60-09-ASAM-11 CARGO DOOR WINDOWJETTISON LEVER INSPECTION C/W AT 4594.9ACFT HRS.

26-Jun-2009 1

FT DRUM NY

FS607593

DOL AVIMALL 5000 HOUR CONTROL BOLTS P/N'S 70400-08159-101 THRU -108, REPLACED DURINGRESET AT 4594.9 ACFT HRS.

13-Jul-2009 1

FT DRUM NY

FS607593

DOL AVIM5000 HOUR STABILATOR PIVOT ANDACTUATOR BOLS, REPLACED DURING RESETAT 4594.9 ACFT HRS.

13-Jul-2009 2

FT DRUM NY

FS607593

DOL AVIMALL 48 MONTH INSPECTIONS ( FUEL CELLORING, FUEL CELL CORROSION, CABIN TUB,ANDADJUSTABLE FLT CONTROL RODSINSP.)COMPLETED DURING RESET AT 4594.9ACFT HRS.

13-Jul-2009 3

FT DRUM NY

FS607593

DOL AVIM5000 HOUR STABILATOR PIVOT BOLTS,REPLACED DURING RESET AT 4594.9 ACFTHRS.

13-Jul-2009 4

FT DRUM NY

FS607593



8.7.DATE

6.REMARKS

4. 5.



DOL AVIMH-60-09-AMAM-03 H-60M SWASHPLATERETIREMENT LIFE INCREASE, N/A THIS ACFT.

14-Jul-2009 1

FT DRUM NY

FS607593

DOL AVIMTB 1-1500-200-20-31 AIRCRAFT DESERTOPERATIONS CLEANING REQUIREMENTS.C/W DURING RESET AT 4594.9 ACFT HRS

14-Jul-2009 2

FT DRUM NY

FS607593

DOL AVIMTB 1-1520-237-30-1 H-60A/L AIRCRAFT DESERTOPERATIONS SPECIAL INSPECTION ANDCLEANING REQUIREMENT(RESET). C/W AT4594.9 ACFT HRS

14-Jul-2009 3

FT DRUM NY

FS607593

DOL AVIMALL PHASE MAINTENANCE INSPECTIONS FORPMI-1 AND PMI-2 C/W DURING RESET AT4594.9 ACFT HRS. NEXT PHASE DUE AT 4954.9ACFT HRS.

14-Jul-2009 4

FT DRUM NY

FS607593

DOL AVIMACFT FLT CONT RIG COMPLETED PRIMARYSERVO BIAS PLUS NO ADDITIONALADJUSTMENTS. T/R BIAS IS RED= 4.930 -5.260, BLU=4.160 - 4.480, YEL=4.880 - 5.200,BLK=4.130 - 4.460, PISTON TRVL OUT= 3.520 -3.490, IN= 0.0 - 0.050. CABLE TENSION L/155R/155 AT 21C

14-Jul-2009 5

FT DRUM NY

FS607593

DOL AVIMAWR 1467R3 - ACFT OPERATING UNDER AWR1467 DATED 23 JAN 09 FOR INSTALLATION OFTHE DOPPLER GLOBAL POSITIONING SYSTEMNAVIGATION SYSTEM PREPLANED PRODUCTIMPROVEMENT (DGNS-P3I), AN/ASN-128D A-KIT AND B-KIT.

15-Jul-2009 1

FT DRUM NY

FS607593

DOL AVIMAWR 1324R7 - ACFT OPERATING UNDER AWR1324 DATED 23 MAR 07 FOR INSTALLATIONOF THE CMWS ICMD ON UH-60A/LHELICOPTERS. (UPDATED REVISION)

15-Jul-2009 2

FT DRUM NY

FS607593

DOL AVIMAWR 1347R9 - ACFT OPERATING UNDER AWR1347 DATED 17 MAR 09 FOR INSTALLATIONOF THE EDM AND BFT (QUAD BAYINSTALLATION) (UPDATED REVISION)

15-Jul-2009 3

FT DRUM NY

FS607593

DOL AVIMAWR 1348R4 - ACFT OPERATING UNDER AWR1348 DATED 18 MAR 09 FOR INSTALLATIONOF THE 12 STATION WALL MT ICS, OR 12STAION VIP II ICS, AUX COM PANEL, AND 8PTICS INSTALLED. (UPDATED REVISION)

15-Jul-2009 4

FT DRUM NY

FS607593

DOL AVIMAWR 1455 - ACFT OPERATING UNDER AWR1455 DATED 20 NOV 07 FOR INSTALLATION OFTHE BATTELLE CAUTION ADVISORYPANEL(CAP).

15-Jul-2009 5

FT DRUM NY

FS607593

DOL AVIMAWR 1479 - ACFT OPERATING UNDER AWR1479 DATED 4 JAN 08 FOR UH-60AHELICOPTERS WITH MAIN MOD PN 70351-08100-075, -076 EQUIPED WITH IMPROVEDPLANETARY CARRIER ASSEMBLY PN 70351-08175-046.

15-Jul-2009 6

FT DRUM NY

FS607593

DOL AVIMAWR 1494R3 - ACFT OPERATING UNDER AWR1494 DATED 14 APR 09 FOR UH-60A/LHELICOPTERS EQUIPPED WITH THE CMWS5TH SENSOR A AND B KIT. (UPDATEDREVISION)

15-Jul-2009 7

FT DRUM NY

FS607593



8.7.DATE

6.REMARKS

4. 5.



DOL AVIMAWR 1539 - ACFT OPERATING UNDER AWR1539 DATED 29 AUG 08 FOR UH-60A/L/MHELICOPTERS EQUIPPED WITH AEROSPACEFILTRATION SYSTEMS (AFS) APU INLETBARRIER FILTERS. (UPDATED REVISION)

15-Jul-2009 8

FT DRUM NY

FS607593

DOL AVIM DS2FCC COMPLETE 19 JUL 09 AT 4600.6 HOURSFOR INSTALLATION OF AN/ASN 128D (128DDGNS P3I) IAW AWR 1467 R3 DATED 23 JAN 09

20-Jul-2009 1

FT. DRUM, NY

AP667239

DOL AVIMMAIN ROTOR AND TAIL ROTOR RIG CHECK,MAIN NO CHANGE, TAIL ROTOR BIAS IS RED4.700 - 5.010 = .310, BLU 4.040 - 4.350 = .310,YEL 4.720 - 5.030 = .310, BLK 4.070 - 4.380 =.310. PISTON TRAVEL 0.050 - 3.49, CABLETENSION IS L145 R145 AT 24'C. COMPLETEDAT 4600.6 ACFT HRS.

21-Jul-2009 1

FT DRUM NY

FS607593

AASF#1TAIL ROTOR BIAS FOR T/R RIG CHECK RED IS5.080-5.00=.08 BLK IS 4.42-4.38=.04 YEL IS 5.11-5.02=.09 BLU IS 4.38-4.35=.03 CABLE TENSIONAVERAGE WAS 151.5@ 25C COMPLETED @4604.9 ACFT HOURS

10-Aug-2009 1


DR620912

AASF#1COMPLIED WITH H-60-09-AMAM-04 A2C2S NOTINSTALLED

24-Aug-2009 1


DR620912

AASF#1COMPLIED WITH H-60-9-AMAM-06 CARGOHOOK CAD LIFE REDUCTION

01-Sep-2009 1


DR620912

AASF#1AWR 1516 DTD 6MAR09 R-1 ACFT OPERATINGWITH THE EBC-406HM ELT SN# 401177

02-Sep-2009 1


DR620912

AASF#1COMPLIED WITH H-60-09-AMAM-07 @ 4611ACFT HOURS

20-Sep-2009 1


DR620912

AASF#1COMPLIED WITH H-60-10-ASAM-01 01-Oct-2009 1


DR620912

AASF#1COMPLIED WITH H-60-10-ASAM-03 12-Nov-2009 1


DR620912

AASF#1COMPLIED WITH H-60-10-AMAM-04 128B/CINSP

13-Nov-2009 1


DR620912

AASF#1COMPLIED WITH H-60-10-AMAM-05 LCFCHANGE 60B

05-Jan-2010 1


DR620912

AASF#1 NJ ARNGCOMPLIED WITH GEN-10-AMAM-02 04-Feb-2010 1


MB869714

AASF#1 NJ ARNGCOMPLIED WITH GEN-10-AMAM-02 2408-17CHANGE NCS MAGNUS TABLET COMPUTER

04-Feb-2010 2


MB869714



8.7.DATE

6.REMARKS

4. 5.



AASF#1 NJARNGCOMPLIED WITH H-60-10-AMAM-11 OILSAMPLE SCHEDULE CHANGES @ 4653.2 ACFTHRS

05-Feb-2010 1


MB869714

AASF#1 LAKEHURSTCOMPLIED WITH H-60-ASAM-10-06 (AUTOIGNITION & TRANSIENT DROOPIMPROVEMENT)

16-Feb-2010 1


MB869714

AASF#1 NJARNGH-60-10-SOF-01 COMPLIED WITH(REDESIGNATION AND REDUCED SERVICELIFE OF MAIN ROTOR BLADES)

21-Apr-2010 1


DM649028

AASF#1 NJNGCOMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-07 (STABILATOR HINGE FITTINGSPHERICAL BEARING MIGRATION)

11-May-2010 1


MB869714

AASF#1 NJARNGCOMPLIED WITH REQUIREMENTS OF H-60-10-AMAM-12(IMPROVED DRAG BEAM, WATERACCUMULATION)

11-May-2010 2


MB869714

CSCACE COMPLETED AT 4688.8 A/C HRS. BY ACETEAM MEMBERS B/G. AFMA RASM-E, AMCOM

13-May-2010 1


JG389608

AASF#1 NJARNGLOWER TAIL CONE SHEAR DECK REPAIREDIAW MEC# F1089854 DATED 18-MAY-10

27-May-2010 1


MB869714

AASF#1 NJARNGCOMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-08 (APU FIREWALL CLEARANCE) PASS

11-Jun-2010 1


MB869714

AASF#1 NJARNGCOMPLIED WITH REQUIREMENTS OF H-60-10-SOF-02 (CHANGE IN SPINDLE NDI TO 360HOURS AND REDUCTION OF LIFE FOR M/RSPINDLES AND SUBCOMPONENTS)

28-Jun-2010 1


DM649028

AASF#1 NJARNGCOMPLIED WITH REQUIREMENTS OF H-60-10-AMAM-16 (CMWS DISPENSE SWITCH GUARDS)

07-Jul-2010 1

07LAKEHURST, NEWJERSEY 08733

MB869714

AASF#1 NJARNGCOMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-11, COMMON COMPONENTRETIREMENT CHANGE TIMES UPDATE,INCLUDING CHANGES 1 & 2

27-Jul-2010 1


DM649028

AASF#1 NJARNGH-60-10-ASAM-11, ALL H-60 AND H-64 SERIESAIRCRAFT, T700 SERIES ENGINES COMMONCOMPONENT RETIREMENT CHANGE TIMESCOMPLIED WITH

02-Aug-2010 1


DM649028

AASF #2COMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-12 (T700 SERIES ENGINES COMMONCOMPONENT RETIREMENT CHANGE TIMES)

10-Aug-2010 1

W.TRENTON, NEWJERSEY 08628

FD986611

AASF # 2COMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-15 (ESSS FUEL SYSTEM VENT ELBOW)

12-Aug-2010 1

W.TRENTON, NEWJERSEY 08628

FD986611

AASF # 2COMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-16 (RESCUE HOIST CABLE CUTHARNESS CONNECTOR)

13-Sep-2010 1

WEST TRENTON, NEWJERSEY 08628

FD986611



8.7.DATE

6.REMARKS

4. 5.



AASF #2, NJARNGCOMPLIED WITH REQUIREMENTS OF UH-60-11-AMAM-03 (OIL COOLER FAN AXIAL BEARING)

01-Nov-2010 1

W. TRENTON, NEWJERSEY 08628

JP589937

AASF#2COMPLIED WITH THE REQUIREMENTS OF H-60-11-ASAM-03

02-Dec-2010 1


JG784911

AASF#1 NJARNGCOMPLIED WITH REQUIREMENTS OF H-60-11-ASAM-04 (TACAN RECEIVER SERVICEBULLETIN 37)

07-Dec-2010 1


MB869714

AASF#1 NJARNGH-60-11-AMAM-04, AMCOM CHANGE 61COMPLIED WITH

07-Dec-2010 2


DM649028

AASF#1 NJARNGOPTION II CABIN HEATER SYSTEM INSTALLEDIN AIRCRAFT

08-Dec-2010 1


DM649028

AASF#1 NJARNGH-60-10-ASAM-04 STABILITY AUGMENTATIONSYSTEM LINKS (SAS) COMPLIED WITH

25-Jan-2011 1


DM649028

AASF#1NJARNGCOMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-06 (MEDEVAC CAROUSELREFURBISHMENT)

10-Feb-2011 1


MB869714

AASF#1 NJARNGH-60-11-ASAM-06: CYCLIC STICK STOP BOLTSCOMPLIED WITH

17-Feb-2011 1


DM649028

AASF#1 NJARNGCOMPLIED WITH REQUIREMENTS OF H-60-11-ASAM-08 (UPPER APX100 / 118 ANTENNASAFETY )

03-Mar-2011 1


MB869714

CSCACE COMPLETED AT 4829.3 A/C HRS. BY ACETEAM MEMBERS B/G. AFMA, RASM-E, AMCOM

11-Apr-2011 1


JG389608

1109TH TASM-GH-60-11-AMAM-09 ENGINE COMPONENTOPERATING HOUR RECORD HAS BEENCOMPLIED WITH IAW AMTRACKS. DURINGLOG BOOK REVIEW, AMAM HAD NOT BEENSIGNED OFF OR RECORDED IAW MESSAGE.AMAM COMPLIED WITH ON 17 MAY 11,SUBMITTED BY JAMES GREEN

02-Jun-2011 1

GROTON, CT 06340

MB844514

CT AVCRADCOMPLIED WITH THE REQUIREMENTS OF H-60-11-AMAM-13 (EXTERNAL RESCUE HOISTMOUNT FITTING)

15-Jun-2011 1

GROTON, CT

RL668948



8.7.DATE

6.REMARKS

4. 5.



AASF#1, NJARNGAIRCRAFT OPERATED WITHIN LIMITATIONSAND RESTRICTIONS LISTED IN AWR'S1516R6(ELT) 29OCT10, 1054R10(BAMBIBUCKET) 09MAR11, 1127R3, 12FEB10,(HELIBASKET W/ LONG LINE), 1347R13 (EDMW/ QUADBAY BFT)27DEC10, 1279R3, 11JUN10,(DOORS/WINDOWS REMOVED), 1310,04NOV05, (HAVEQUICK), 1425R14, 18AUG10,(CMWS ICMD P3I), 1346R17, 15JUL10, (IVHMS),1466R03, 01DEC10, (GARMIN 496), 1467R4,01MAR10, (128 DELTA GPS), 1479R1,04JAN10, (MAIN MOD W/ IMP CARRIER),1539R1, 30AUG10, (APU IBF), 1494R5,30SEP10, (CMWS 5TH SENSOR),AWR 1750ROO25 MAR 11,(ANVIS), 1120R08, 30NOV10 (M240W/PEQ LASER), 967R01, 21 DEC 01, (ARN 123FM IMMUNE VOR).

17-Jun-2011 1


EV601757

1109TH TASMGCOMPLIED WITH THE REQUIREMENTS OF H-60-11-ASAM-13 (ENG AIR INLET ANTI-ICING/MODULATING VALVE)

30-Jun-2011 1

GROTON,CT

WS521003

CT AVCRADCOMPLIED WITH THE REQUIREMENTS OF H-60-11-ASAM-14 (ENGINE COWLING REPAIRRESTRICTIONS)

08-Jul-2011 1

GROTON, CT

RL668948

CT AVCRADCOMPLIED WITH THE REQUIREMENTS OF H-60-11-SOF-01 (DISCREPANT SELF LOCKINGDOUBLE HEXAGON NUTS)

08-Jul-2011 2

GROTON, CT

RL668948

CT AVCRADTAIL ROTOR BIAS FOR T/R RIG CHECK RED IS4.717-5.056=.339 BLK IS 4.075-4.404=.329 YELIS 4.708-5.046=.338 BLU IS 4.081-4.417=.336COMPLETED @ 4887.1 ACFT HOURS

12-Jul-2011 1

GROTON, CT

RL668948

CT AVCRADCOMPLIED WITH THE REQUIREMENTS OF H-60-11-AMAM-15 (INTEGRATED VEHICLE HEALTHMANAGEMENT SYSTEM ACCELEROMETERS)

13-Jul-2011 1

GROTON, CT

RL668948

1109TH AVCRADPMI-1 COMPLETED AT 4887.1 ACFT HRS. NEXTPMI-2 DUE AT 5247.1 ACFT HRS

27-Jul-2011 1

GROTON, CT

RL668948

AASF #1 NJARNGCOMPLIED WITH THE REQUIREMENTS OF H-60-11-AMAM-20 (AN/ASN-128D DOPPLER ANDAMPS SOFTWARE UPGRADE)

21-Sep-2011 1

LAKEHURST NJ

SZ628863

B CO 1/150TH AHBH-60-11-AMAM-19, AMCOM CHANGE 62COMPLIED WITH

05-Oct-2011 1

CAMP ATTERBURY

DM649028

CO B 777 ASBH-60-12-SOF-01, TAIL ROTOR INTERMEDIATEGEARBOX, COMPLIED WITH

08-Oct-2011 1

CAMP ATTERBURY, IN

AL727224

B CO, 777TH ASBCOMPLIED WITH THE REQUIREMENTS OF H-60-12-SOF-02: TAIL ROTOR INTERMEDIATEGEARBOX

11-Oct-2011 1

CAMP ATTERBURY IN

DM649028

B CO 777 ASBH-60-12-SOF-03, TAIL ROTOR INTERMEDIATEGEARBOX, COMPLIED WITH

15-Oct-2011 1

CAMP ATTERBURY, IN

AL727224

AASF2, WVARNGAIRCRAFT TRANSFERED FROM NJ-ARNG TOCO C 1/150TH AVIATION UIC WV75C0 @ 4932.8AIRCRAFT HOURS.

31-Oct-2011 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-12-ASAM-02, DRAG BEAMREPLACEMENT COMPLIED WITH.

06-Dec-2011 1

WHEELING, WV 26003

KS173337



8.7.DATE

6.REMARKS

4. 5.



AASF 2MEC F138982 A TEMPERARY REPAIRAPPROVED FOR CONDUIT ON TAIL ROTORPYLON BY FABRICATINGA 1/2 INCHPOLYURETHANE TUBING CUT TO FIT ANDSECURED WITH ZIP TIES. REPLACE AT NEXTPMI OR 260.6 HRS(5247.3)

11-Jan-2012 1

WHEELING, WV 26003

KS173337

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR UH-60A/L HELICOPTERS TO OPERATE WITH THEDAVID CLARK PASSENGER INTERCOMSYSTEM (ICS) INSTALLED (AWR 1303/R3)DATED 13 JUL 10, THIS IS A TEMPORARYCHANGE TO AIRCRAFT CONFIGURATION.

10-Feb-2012 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOROPERATION OF UH/HH-60A/L/M AIRCRAFTWITH THE EBC-406HM EMERGENCY LOCATORTRANSMITTER (ELT) INSTALLED (AWR1516/R6) DATED 29 OCT 10, THIS IS ATEMPORARY CHANGE TO AIRCRAFTCONFIGURATION.

10-Feb-2012 2

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR THEGARMIN GPSMAP 696, 695, 496, 495, 396, 296OR 295 ON UH ARMY UH/HH-60A/L/MHELICOPTERS (AWR1466/R4) DATED 31 AUG11, THIS IS A TEMPORARY CHANGE TOAIRCRAFT CONFIGURATION.

10-Feb-2012 3

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-12-ASAM-05, ALL H-60M AIRCRAFT,FREQUENCY MODULATION (FM) #2 ANTENNACONNECTOR BRACKET N/A THIS AIRCRAFT

14-Feb-2012 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-12-ASAM-04, ALL H-60M SERIESAIRCRAFT, AN/ARC-231, N/A THIS AIRCRAFT

14-Feb-2012 2

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-12-SOF-04, SAFETY OF FLIGHT (SOF),EMERGENCY, ALL H-60 SERIES AIRCRAFT,BREEZE EASTERN EXTERNAL RESCUE HOISTOPERATIONS COMPLIED WITH, PROVISIONSNOT INSTALLED ON THIS AIRCRAFT.

17-Feb-2012 1

WHEELING, WV 26003

DN337516

AASF2H-60-ASAM-06 ALL H-60 SERIES AIRCRAFT,UPPER BULKHEAD FUEL SYSTEMBREAKAWAY VALVE AND FIREEXTINGUISHING SYSTEM DIRECTIONALVALVE

23-Feb-2012 1

WHEELING, WV 26003

KS173337

AASF2, WVARNGH-60-12-AMAM-07, ALL H-60M SERIESAIRCRAFT, MAIN ROTOR BLADE WATERINTRUSION INSPECTION, NA THIS AIRCRAFT.

09-Mar-2012 1

WHEELING, WV 26003

DN337516

L-3ACE COMPLETED AT 5027.6 A/C HRS. BY ACETEAM MEMBERS B/G. AFMA, RASM-E,AMCOM.

15-Mar-2012 1

WHEELING, WV 26003

JG389608

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR 1750 R1,DATED 27 MAR 12) FOR THE OPERATION OFTHE AVIATOR'S NIGHT VISION IMAGINGSYSTEM (ANVIS) AN/AVS-6 SERIES NIGHTVISION GOGGLES (NVG) IN THE UH-HH-60A/L/M AIRCRAFT.

08-May-2012 1

WHEELING, WV 26003

DN337516



8.7.DATE

6.REMARKS

4. 5.



AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR UH/HH-60A/L HELICOPTERS WITH INTEGRATEDVEHICLE MANAGEMENT SYSTEM (IVHMS)HEALTH USAGE MANAGEMENT SYSTEM(HUMS) SOFTWARE BLOCK 5.0 INSTALLED(AWR 1823)

14-May-2012 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-12-AMAM-09, ALL H-60 SERIESAIRCRAFT, HYDRAULIC LINE CHAFE DUE TOMISSING CLAMPS COMPLIED WITH @ 5079.0AIRCRAFT HOURS.

17-May-2012 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR THEOPERATION OF UH-60A/L/M HELICOPTERSWITH THE M-240H MACHINE GUN INSTALLED(AWR 1120R8), THIS IS A TEMPORARYCHANGE TO AIRCRAFT CONFIGURATION.

25-Jun-2012 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGAVIATION MAINTENANCE ACTION MESSAGE(AMAM), MAINTENANCE MADATORY, ALL H-60A/K/L SERIES AIRCRAFT, RESCINDEDCOMMON COMPONENT REMOVAL DATES, H-60-12-AMAM-12 COMPLIED WITH @ 5098.2ACFT HOURS.

10-Jul-2012 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORHINESS RELEASE (AWR) FOR UH-60A/L HELICOPTERS TO OPERATE WITH THEDAVID CLARK PASSENGER INTECOM SYSTEM(ICS) INSTALLED (AWR1303/R4) DATED 05JULY 12. THIS IS A TEMPORARY CHANGE TOAIRCRAFT CONFIGURATION.

11-Jul-2012 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-12-ASAM-08, ALL H-60 SERIESAIRCRAFT, CARGO HOOK MANUAL RELEASESPRING ASSEMBLY, COMPLIED WITH @5100.0 ACFT HOURS

18-Jul-2012 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-12-AMAM-14, ALL H-60L SERIESAIRCRAFT, AN/ARN-149 LOW FREQUENCY(LF) AUTOMATIC DIRECTION FINDER (ADF)N/A THIS AIRCRAFT

23-Jul-2012 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-12-ASAM-09, RESCUE HOIST CARTRIDGEACTUATED DEVICE (CAD) ELECTRICALCONNECTOR N/A THIS AIRCRAFT.

23-Aug-2012 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR THEELECTRONIC DATA MANAGER (EDM) AND/ORBLUE FORCE TRACKING SYSTEM (BFT) ONUH/EH/HH-60A/L HELICOPTERS (AWR 1800/R1)DATED 20 JULY 12.

24-Aug-2012 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR UH-60A/L AND HH-60A/L HELICOPTERS EQUIPPEDWITH SEI INDUSTRIES BAMBI WATERBUCKETS (AWR 1054/R11) DATED 22 AUG 12,THIS IS A TEMPORARY CHANGE TO AIRCRAFTCONFIGURATION.

24-Aug-2012 2

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR THEUH/HH-60A/L/M WITH A NCS MAGNUS MODELRNM101 LAPTOP ONBOARD AND OPERATING(AWR 1648/R2) DATED 9 MAR 12. THIS IS ATEMPORARY CHANGE TO AIRCRAFTMODIFICATION.

24-Aug-2012 3

WHEELING, WV 26003

DN337516



8.7.DATE

6.REMARKS

4. 5.



AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR THEOPERATION OF THE AVIATORS NIGHT VISIONIMAGING SYSTEM (ANVIS) AN/AVS-6 SERIESNIGHT VISION GOGGLES (NVG) IN THE UH/HH-60A/L/M AIRCRAFT (AWR 1750/R1) DATED27MAR12, THIS IS A TEMPORARY CHANGE TOAIRCRAFT CONFIGURATION.

24-Aug-2012 4

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-12-ASAM-07, AVIATION SAFETY ACTIONMESSAGE (ASAM), MAINTENANCEMANDATORY, ALL H-60 SERIES AIRCRAFT,ELECTRICAL WIRING CHAFE, COMPLIED WITH@ 5132.3 AIRCRAFT HOURS.

29-Aug-2012 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-12-AMAM-15, AVIATION SAFETY ACTIONMESSAGE (AMAM), MAINTENANCEMANDATORY, ALL H-60 SERIES AIRCRAFT,TRIM ACTUATORS COMPLIED WITH @ 5134.9AIRCRAFT HOURS.

29-Aug-2012 2

WHEELING, WV 26003

DN337516

AASF2, WVARNGMEC F152729 AUTHORIZATION TO INSTALLTHE HUD TGT DISCONNECT REFERENCINGMEO A6206 AND TM 1-1500-323-24-1. THESEDISCONNECTS ARE BETWEEN THE HUD TGTAMPLIFIERS (2EA.) AND SPLICE GROUPS SG-138-16/SG138-15 (#1 TGT AMP). AUTHORIZEDBY [email protected] 860-481-9428.

07-Sep-2012 1

WHEELING, WV 26003

DN337516

AASF 2 WVARNGH-60-11-AMAM-17,AVIATION MAINTENANCEACTION MESSAGE(AMAM),MAINTENANCEMANDATORY,ALL H-60 SERIES AIRCRAFT,TAIL ROTOR INBOARD/OUTBOARDRETENTION SHIMS, COMPLIED WITH @ 5141.2

17-Sep-2012 1

WHEELING, WV 26003

KS173337

AASF2 WVARNGT/R BIAS FOR RIG CHECK YELLOW IS 4.732-5.050=.318, BLUE IS 4.161-4.498=.317, RED IS4.741-5.079=.339, BLACK IS [email protected]

18-Sep-2012 1

WHEELING, WV 26003

KS173337

AASF2H-60-13-AMAM-02, AVIATION MAINTENANCEACTION MASSAGE(AMAM),MAINTENANCEMANDATORY,ALL HH/UH-60 A/L SERIESAIRCRAFT, ATTITUDE HEADING REFERENCESYSTEM(AHRS) WIRING HARNESSES,COMPLIED WITH

06-Nov-2012 1

WHEELING, WV 26003

KS173337

AASF2, WVARNGH-60-13-AMAM-03, AVIATION MAINTENANCEACTION MESSAGE (AMAM) MAINTENANCEMADATORY, ALL H-60 SERIES AIRCRAFT,DIGITAL ENGINE CONTROL UNIT (DECU) /ELECTRONIC DIGITAL CONTROL UNIT(EDECU) TURBINE GAS TEMPERATURE (TGT)BIAS, COMPLIED WITH @ 5225.5 AIRCRAFTHOURS.

28-Nov-2012 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-13-AMAM-04, AVIATION MAINTENANCEACTION MESSAGE (AMAM), MAINTENANCEMANDATORY, UNIT LEVEL LOGISTICSSYSTEM-AVIATION (ENHANCED) (ULLS-A(E)AMCOM LOGISTICS CENTER (ALC), LCFCHANGE 63 REQUIREMENTS COMPLIED WITH.

29-Nov-2012 1

WHEELING, WV 26003

DN337516



8.7.DATE

6.REMARKS

4. 5.



AASF2, WVARNGH-60-13-ASAM-01, AVIATION SAFETY ACTIONMESSAGE (ASAM), MAINTENANCEMANDATORY, ALL H-60 SERIES AIRCRAFT,ANIT COLLISON LIGHTS POWER SUPPLYCOMPLIED WITH @ 5225.5 AIRCRAFT HOURS.

30-Nov-2012 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORHTINESS RELEASE (AWR) FOROPERATION OF UH/HH-60A/L/M AIRCRAFTWITH THE EBC-406HM ELT INSTALLED(AWR1516/R7) DATED 11OCT12, THIS IS ATEMPORARY CHANGE TO AIRCRAFTCONFIGURATION.

12-Dec-2012 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR THEOPERATION OF UH-60A/L/M HELICOPTERSWITH THE M-240H MACHINE GUN INSTALLED(AWR1120/R9) DATED 30NOV12, THIS IS ATEMPORARY CHANGE TO AIRCRAFTCONFIGURATION.

12-Dec-2012 2

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR UH-60A/L HELICOPTERS EQUIPPED WITH SEIINDUSTRIES BAMBI WATER BUCKETS(AWR1054/R12) DATED 16NOV12, THIS IS ATEMPROARY CHANGE TO AIRCRAFTCONFIGURATION.

12-Dec-2012 3

WHEELING, WV 26003

DN337516

AASF2, WVARNGMEC F159547 C, REPAIR LEFT AND RIGHTHAND BEADED PANELS AND INSTALL 70070-20470-012 GUNNERS WINDOW PLATING,AUTHORIZED [email protected] 860-481-9428. MEC COMPLETED @ 5246.7 AIRCRAFTHOURS.

14-Jan-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-13-AMAM-05, ALL H-60 SERIESAIRCRAFT, MAIN LANDING GEAR WHEELBRAKE ASSEMBLY COMPLIED WITH @ 5246.7AIRCRAFT HOURS.

28-Jan-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-13-AMAM-06, ALL UH-60A/L/M SERIESAIRCRAFT, CRASHWORTHY EXTERNAL FUELSYSTEM (CEFS) N/A THIS AIRCRAFT.

11-Feb-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGMEC F161249, REPLACE TAPERED PIN (2EA)ON REMOTE CONTROL LEVER UNIT(FORWARD QUADRANT) PN 70400-02620-041USING SAC DWG 70400-02620 REV B ANDIETM WP 1107 AS REFERENCE. AUTHORIZEDBY [email protected] 860-481-9428. MEC COMPLETED @ 5246.7 AIRCRAFTHOURS.

14-Feb-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGMEC F161924 A, RIGHT HAND SIDE BL 34.5BEAM REPAIR IAW SIKORSKY PROCEDUREAJM-BL34-1C, DMWR 1-1520-237-23-1, ANDMEO A5485B; AUTHORIZED [email protected] 860-481-9428. MEC COMPLETED @ 5246.7 AIRCRAFTHOURS.

28-Feb-2013 1

WHEELING, WV 26003

DN337516



8.7.DATE

6.REMARKS

4. 5.



AASF2, WVARNGMEC F161971, REPAIR STATION 363, 3/8"CRACK PROPAGATING ON THE ENGINE DECKWEB IAW SIKORSKY OEM PROCEDURE FTR5479T008, WO 301638, DMWR 1-1520-237-2, TM1-1500-203-23 AND TM 55-1500-345-23;AUTHORIZED [email protected] 860-481-9428. MEC COMPLETED @ 5246.7 AIRCRAFTHOURS.

28-Feb-2013 2

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-12-ASAM-01, TAIL ROTOR OUTPUTBEVEL GEAR NDI, COMPLIED WITH @ 5246.7AIRCRAFT HOURS.

01-Mar-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-13-ASAM-04, ALL H-60 SERIESAIRCRAFT, PLASTIC MEDIA BLAST (PMB) ANDOXIDE FLAKE RESIDUE COMPLIED WITH @5246.7 AIRCRAFT HOURS.

21-Mar-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR ALLUH/HH/-60A/L/M HELICOPTERS EQUIPPEDWITH THE TITANIUM (1000997-001(S7020-12008-043)) OR STAINLESS STEEL RESCUE HOISTCABLE (GUARD) DEFLECTOR (AWR 1566 R-3)DATED 18 MAR 13.

26-Mar-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR UH-60A/L HELICOPTERS EQUIPPED WITH AN/APX-118 COMMON TRANSPONDER (CXP) (AWR1738-R1) DATED 1 FEB 13.

26-Mar-2013 2

WHEELING, WV 26003

DN337516

L-3ACE COMPLETED AT 5246.7 A/C HRS. BY ACETEAM MEMBERS B/G. AFMA, RASM-E,AMCOM.

26-Mar-2013 3

WHEELING, WV 26003

JG389608

AASF2, WVARNGH-60-13-ASAM-05, BREEZE EASTERNVARIABLE SPEED ELECTRIC RESCUE HOISTCOMPLIED WITH, N/A THIS AIRCRAFT.

09-Apr-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-13-ASAM-06, PHASE MAINTENANCEINSPECTION (PMI) CHECKLIST CHANGES,COMPLIED WITH @ 5246.7 AIRCRAFT HOURS.

08-May-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-13-AMAM-05, MAIN LANDING GEARWHEEL BRAKE ASSEMBLY, COMPLIED WITH@ 5246.7 AIRCRAFT HOURS.

08-May-2013 2

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-13-AMAM-07, LOAD DEMAND SPINDLE(LDS) CABLE CLEARANCE, COMPLIED WITH @5246.7 AIRCRAFT HOURS.

08-May-2013 3

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-13-SOF-01, ATTITUDE HEADINGREFERENCE SET (AHRS), COMPLIED WITH @5246.7 AIRCRAFT HOURS.

31-May-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOROPERATION OF THE AVIATOR'S NIGHT VISIONIMAGING SYSTEM (ANVIS) AN/AVS-6 SERIESNIGHT VISION GOGGLES IN UH-60A/L/MAIRCRAFT (AWR 1750-R2) DATED 29MAR13.

20-Jun-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-13-AMAM-11, MAIN TRANSMISSIONFILTER BOWL ATTACHMENT HARDWAREREPLACEMENT COMPLIED WITH @ 5246.7AIRCRAFT HOURS.

01-Jul-2013 1

WHEELING, WV 26003

DN337516



8.7.DATE

6.REMARKS

4. 5.



AASF2, WVARNGPMI-2 COMPLETED @ 5246.7 AIRCRAFTHOURS.

25-Jul-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGMEC F171138, DATED 22 AUG 2013,AUTHORITY TO REPAIR 0.72 INCH MINORDENT LOCATED ON THE BOTTOM LEFT SIDEFORWARD END OF STABILATOR IAW DMWR 1-1560-287, AUTHORIZED [email protected] 860-481-9428.

24-Aug-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-13-AMAM-10, LEGITIMATE CODE FILE(LCF) CHANGE 64 REQUIREMENTS COMPLIEDWITH

24-Aug-2013 2

WHEELING, WV 26003

DN337516

AASF2, WVARNGMAIN ROTOR AND TAIL ROTOR COMPLETEDRIG COMPLETED @ 5246.7 AIRCRAFT HOURS:MEASUREMENTS ARE AS FOLLOWS: LOWCOLL ANGLE 8.9, 9.0, 8.9, 9.0; HIGH COLLECANGLE AVERAGE 15; FWD CYCLIC AVERAGE34; AFT CYCLIC ANGLE 19.2; LEFT CYCLICANGLE 15.0; RIGHT CYCLIC ANGLE 14.2: TAILROTOR CABLE TNESION LEFT 170 RIGHT 170@ 29 DEG C: TAIL ROTOR BIAS BLADE SETRED 3.0 DEG DIM A 4.798 DIM B 5.128 FIN DEG3.0, BLK BLADE SET 3.1 DIM A 4.088 DIM B4.418 FIN DEG 3.1, YEL BLADE SET 3.1 DIM A4.730 DIM B 5.062 FIN DEG 3.1, BLUE BLADESET 3.0 DIM A 4.068 DIM B 4.427 FIN DEG 3.0,T/R SERVO PISTON TRAVEL INITIALEXTENDED 3.52 RETRACTED 0.0, HIGH FULLAFT 3.507 LOW COLL FUL RIGHT YAW 0.014.

26-Aug-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-13-AMAM-01, FLIGHT CONTROL RIGGINGPROCEDURES COMPLIED WITH @ 5246.7AIRCRAFT HOURS

28-Aug-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-13-AMAM-15, CEFS RIGHT HAND FUELCELL COVER PLATE INSPECTION N/A THISAIRCRAFT.

26-Sep-2013 1

WHEELING, WV 26003

KM238565

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR UH-60A/L HELICOPTERS TO OPERATE WITH THEDAVID CLARK PASSENGER INTERCOM (ICS)SYSTEM INSTALLED (AWR 1303) R6 DATED23OCT13.

23-Oct-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOROPERATION OF APPLE IPAD 3RDGENERATION DEVICES ON US ARMY UH/HH-60A/L/M HELICOPTERS (AWR 1914) DATED 28OCT 13.

28-Oct-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR UH-60A/L HELICOPTERS EQUIPPED WITH SEIINDUSTRIES BAMBI WATER BUCKETS (AWR1054) R13 DATED 31OCT13.

31-Oct-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-14-SOF-01, ALL H-60A/L SERIESAIRCRAFT, BREEZE EASTERN EXTERNALRESCUE HOIST INSTALLATION, N/A THISAIRCRAFT.

01-Nov-2013 1

WHEELING, WV 26003

DN337516



8.7.DATE

6.REMARKS

4. 5.



AASF2, WVARNGTAIL ROTOR RIG CHECK COMPLETED @5274.7 AIRCRAFT HOURS; RED 1ST DEG 2.9,BLACK 1ST DEG 2.8, YELLOW 1ST DEG 3.2,BLUE 1ST DEG 2.9: RED 2ND DEG 2.9 BLACK2ND DEG 2.8, YELLOW 2ND DEG 3.1, BLUE2ND DEG 2.9: PISTON 3.52 IN AND .075 GAP.

08-Nov-2013 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-14-ASAM-02, ALL H-60 SERIESAIRCRAFT, HEALTH USAGE MONITORINGSYSTEM (HUMS) ACCELEROMETERSCOMPLIED @ 5281.0 AIRCRAFT HOURS.

22-Nov-2013 1

WHEELING, WV 26003

DN337516

W8RJAAH-60-14-AMAM-03 (DISCREPANT CONNECTINGLINKS) C/W

08-Jan-2014 1

WHEELING, WV

DH354745

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR UH-60A/L HELICOPTERS WITH INTEGRATEDVEHICLE HEALTH MANAGEMENT SYSTEM(IVHMS) (AWR 1346) R21 DATED 24JAN14.

23-Jan-2014 1

WHEELING, WV 26003

DN337516

WUASC0H-60-14-ASAM-03 (ENGINE INLET BARRIERFILTER BRACKET REMOVAL) C/W

24-Jan-2014 1

WILLIAMSTOWN, WV

DH354745

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOROPERATION OF APPLE IPAD 3RDGENERATION DEVICES ON US ARMY UH/HH-60A/L/M HELICOPTERS (AWR 1914) R2 DATED14JAN14.

29-Jan-2014 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGAVIATION MAINTENANCE ACTION MESSAGE(AMAM), ULLS-AE AMCOM LOGISTICSCENTER (ALC) LCF CHANGE 65 COMPLIEDWITH.

07-Feb-2014 1

WHEELING, WV 26003

DN337516

L3ACE COMPLETED AT 5342.4 ACFT HRS. BYACE TEAM MEMBERS B/G, AFMA, RASME,AMCOM.

20-Mar-2014 1

WILLIAMSTOWN, WV

JG389608

W8RJAAH-60-14-AMAM-08 AN/ASE 15 E CIRCUITBREAKER PROTECTION C/W

08-Apr-2014 1

WILLIAMSTOWN, WV

DH354745

AASF #1 WVARNGH-60-14-AMAM-10 (HONTEK COATED MRBLADE REMOVAL) C/W

18-Apr-2014 1

WILLIAMSTOWN, WV

JA215043

AASF#1 WVARNGH-60-14-AMAM-12 (MR SPINDLE NUTRETIREMENT LIFE EXTENSION) C/W

23-Apr-2014 1

WILLIAMSTOWN, WV

JA215043

AASF2, WVARNGH-60-14-AMAM-14, INTEGRATED VEHICLEHEALTH MANAGEMENT SYSTEM (IVHMS)CABLING COMPLIED WITH.

29-Apr-2014 1

WHEELING, WV 26003

DN337516

AASF #1, WVARNGM/R RIG CHECK COMPLETED AT 5364.9 ACFTHRS; LOW COLL ANGLE AVG -.825, HIGHCOLL ANGLE AVG 14.675, COLL RANGE 15.5,FWD CYCLIC ANGLE 33.3 TOTAL, AFT CYCLICANGLE 19.2 TOTAL, LEFT CYCLIC ANGLE 16.2TOTAL, RIGHT CYCLIC ANGLE 14.3 TOTAL,PRIMARY SERVO CONTROL ROD LAT ADJ 1/4"FLAT CC.

05-May-2014 1

WILLIAMSTOWN, WV

JA215043

AASF2, WVARNGH-60-14-SOF-03, DISCREPANT SELF LOCKINGDOUBLE HEXAGON NUTS COMPLIED WITH.

23-Jun-2014 1

WHEELING, WV 26003

DN337516



8.7.DATE

6.REMARKS

4. 5.



AASF2, WVARNGH-60-14-AMAM-16, ATTITUDE HEADINGREFERENCE UNIT 2410 TRACKING COMPLIEDWITH.

14-Jul-2014 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR UH/HH-60A/L/M OPERATIONS WITH COCKPITDOORS/WINDOWS AND OR CABINDOORS/WINDOWS REMOVED (AWR1279) R5DATED 13 JUN 14

16-Jul-2014 1

WHEELING, WV 26003

KM238565

AASF2, WVARNGH-60-14-ASAM-09, ENGINE OUTPUT SHAFTCOMPLIED WITH @ 5424.7 AIRCRAFT HOURS.

30-Jul-2014 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-14-SOF-04, OPERATORS ANDCREWMEMBERS CHECKLIST COMPLIED WITH@ 5473.3 AIRCRAFT HOURS

29-Aug-2014 1

WHEELING, WV 26003

KM238565

AASF2, WVARNGH-60-14-ASAM-10, MAIN TRANSMISSIONCARRIER ASSEMBLY COMPLIED WITH @5474.6 AIRCRAFT HOURS.

04-Sep-2014 1

WHEELING, WV 26003

KM238565

AASF2, WVARNGH-60-14-AMAM-19, UNIT LEVEL LOGISTICSSYSTEM-AVIATION (ENHANCED) ULLS-A(E)LCF CHANGE 66 REQUIREMENTS COMPLIEDWITH @ 5475.6 AIRCRAFT HOURS.

15-Sep-2014 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-15-AMAM-02, IVHMS WIRINGMANAGEMENT COMPLIED WITH @ 5484.6AIRCRAFT HOURS.

23-Oct-2014 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-15-SOF-01, SAFETY OF FLIGHT (SOF),OIL COOLER FAN AXIAL BEARING COMPLIEDWITH @ 5487.2 AIRCRAFT HOURS.

30-Oct-2014 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-15-ASAM-01, LIGHT EMITTING DIODE(LED) CAUTION ADVISORY PANEL (CAP)COMPLIED WITH.

20-Nov-2014 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-15-AMAM-05, AHRS EMERGENCYPROCEDURES COMPLIED WITH @ 5505.4AIRCRAFT HOURS.

18-Dec-2014 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-15-AMAM-06, IDENTIFICATION OFAVIATION SURVIVAL EQUIPMENT COMPLIEDWITH @ 5526.3

06-Mar-2015 1

WHEELING, WV 26003

KM238565

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR UH-60A/L HELICOPTERS WITH IVHMS HUMSSOFTWARE BLOCK 5.0 INSTALLED , AWR 1823DATED 29 MAY 2014/R1.

19-Mar-2015 1

WHEELING, WV 26003

DN337516

L-3ACE COMPLETED AT 5550.6 A/C HRS. BY ACETEAM MEMBERS B/G. AFMA, RASME, AMCOM.

31-Mar-2015 1

WHEELING, WV 26003

JG389608

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOROPERATION OFTHE AVIATOR'S NIGHT VISIONIMAGING SYSTEM (ANVIS) AN/AVS-6 SERIESNIGHT VISION GOGGLES (NVG) IN UH/HH-60A/LIM AIRCRAFT (AWR 1750R3 DATED 31MAR 15).

31-Mar-2015 2

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR UH-60A/L AND HH-60A/L HELICOPTERS EQUIPPEDWITH SEI INDUSTRIES BAMBI WATERBUCKETS (AWR 1054R15) DATED 6APR15.

06-Apr-2015 1

WHEELING, WV 26003

DN337516



8.7.DATE

6.REMARKS

4. 5.



AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOR EH-60A AND UH/HH-60A/L/M HELICOPTERSEQUIPPED WITH OREGON AERO SEATCUSHIONS (AWR 1309R9) DATED 15 APR 15.

15-Apr-2015 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGAIRWORTHINESS RELEASE (AWR) FOROPERATION OF THE GOODRICH 42305-5INTERNAL RESCUE HOIST (IRH) ON UH-60A/LHELICOPTERS (AWR 1308)

21-Apr-2015 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-15-AMAM-10, AV-DEC GASKETINSPECTION COMPLIED WITH.

05-May-2015 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-15-ASAM-03, TROOP SEAT ENERGYATTENUATORS COMPLIED WITH.

15-May-2015 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-15-AMAM-11, MODE-S TRANSPONDERADDRESS REVIEW COMPLIED WITH.

01-Jun-2015 1

WHEELING, WV 26003

KM238565

AASF2, WVARNGAIRCRAFT MODE-S TRANSPONDER ADDRESS(H-60-15-AMAM-11) IS 53405444.

01-Jun-2015 2

WHEELING, WV 26003

KM238565

AASF2, WVARNGH-60-15-AMAM-14, LEGITIMATE CODE FILE(LCF) CHANGE 67 REQUIREMENTS COMPLIEDWITH.

24-Jul-2015 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-15-SOF-02, FRIES RELEASE CABLECOMPLIED WITH, NOT INSTALLED ON THISAIRCRAFT.

28-Sep-2015 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-15-AMAM-18, MEDEVAC CAROUSELCOMPLIED WITH, N/A THIS AIRCRAFT.

29-Sep-2015 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGM/R RIG COMPLETED @ 5601.1 ACFT HRS;LOW COLL ANGLE AVG -0.550, HIGH COLLANGLE AVG 15.10, COLL ANGLE SPREAD AVG15.65, FWD CYCLIC ANGLE TOTAL 34.10, AFTCYCLIC ANGLE TOTAL 19.00, LEFT CYCLICANGLE TOTAL 15.20, RT CYCLIC ANGLETOTAL 14.50. PRIMARY SERVO CONTROL RODBIAS; FWD 1 FLAT C/W, AFT 1 FLAT CCW, LATNO CHANGE. BLADE ANGLEMEASUREMENTS; RED 0.3 SET 3.0 FINAL,BLUE -0.1 SET 3.00 FINAL, YELLOW 0.4 SET3.00 FINAL, BLACK 0.4 SET 3.10 FINAL.DIMENSIONAL CHECK DIFFERENCE; RED0.330, BLUE 0.330, YELLOW 0.310, BLACK0.330. T/R PUSHROD LENGTH 12.58. T/RCABLE TENSION; L/H 150, R/H 150,DIFFERENCE 0, TEMP 21 DEG C. TAIL ROTORPISTON TRAVEL; OUT 3.53 INITIAL 3.51 AFTER,IN 0.00 INITIAL 0.029 AFTER. ACFT RIGGED BYZM250409 AND JF319519.

30-Sep-2015 1

WHEELING, WV 26003

KM238565

AASF2, WVARNGH-60-16-AMAM-01, EIBF FRAMES COMPLIEDWITH @ 5601.1 ACFT HRS.

04-Nov-2015 1

WHEELING, WV 26003

KM238565

AASF2, WVARNGH-60-16-ASAM-01, INBOARD RETENTIONPLATE TORQUE CHECK COMPLIED WITH.

12-Nov-2015 1

WHEELING, WV 26003

DN337516

AASF2, WVARNGH-60-16-AMAM-03, PERSONNEL LOCATOR SETREMOVAL COMPLIED WITH, NOT INSTALLEDON THIS AIRCRAFT.

23-Nov-2015 1

WHEELING, WV 26003

DN337516



8.7.DATE

6.REMARKS

4. 5.



SES, LLCAIRCRAFT INDUCTED INTO THE BESTPROGRAM AT 5619.9 ACFT HRS

14-Jan-2016 1

HUNTSVILLE

ED046014

SES, LLCH-60-16-AMAM-04 NOT COMPLIED WITH 16-Jan-2016 1

HUNTSVILLE

ED046014

SES, LLCH-60-16-ASAM-02 NOT COMPLIED WITH 16-Jan-2016 2

HUNTSVILLE

ED046014


DATE AC HRS SHAFT VERTICAL REASON FOR VIB CHECKLONGITUDINALLATERAL

IPS READINGS4.

7923273HELICOPTER, UTILITYUH-60A3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL

Report Date: 17-Jan-2016 1/4

POST PHASE04-Nov-2015 OIL COOLER 0.2005601.1

100 HR REQ21-Mar-1995 #1 ENG OUT 0.25002494.3

100 HR REQ21-Mar-1995 #2 ENG OUT 0.2002494.3

100 HR REQ21-Mar-1995 #2 ENG OUT 0.30.6502494.3

100 HR REQ21-Mar-1995 AXIAL FAN 0.30.6502494.3

MWO 1-1520-237-50-7331-Aug-1995 #1 ENG OUT 0.47002509.2

MWO 1-1520-237-50-7331-Aug-1995 #2 ENG OUT 0.49002509.2

100 HR13-May-1999 #1 ENG OUT 0.27002698.3

100 HR13-May-1999 #2 ENG OUT 0.5002683.3

100 HR13-May-1999 AXIAL FAN 0.440.1902698.3

100 HR REQ21-May-1999 #1 ENG OUT 0.5002700.5

100 HR REQ21-May-1999 #2 ENG OUT 0.27002700.5

100 HR REQ21-May-1999 AXIAL FAN 0.440.1902700.5

100 HR REQ17-Dec-1999 #1 ENG OUT 0.2002794.4

100 HR REQ17-Dec-1999 #2 ENG OUT 0.08002794.4

100 HR REQ17-Dec-1999 AXIAL FAN 0.50.0602794.4

100 HR REQ29-Jun-2000 #1 ENG OUT 0.23002901

100 HR REQ29-Jun-2000 #2 ENG OUT 0.7002901

100 HR REQ29-Jun-2000 AXIAL FAN 0.480.9902901

PMS-2 AND 100 HR REQ22-Mar-2001 #1 ENG OUT 0.14002994

PMS-2 AND 100 HR REQ22-Mar-2001 #2 ENG OUT 0.32002994

PMS-2 AND 100 HR REQ22-Mar-2001 AXIAL FAN 0.290.9702994

REINSTALLED DRIVE SHAFT08-Feb-2002 #2 ENG OUT 0.14003179.6

PMS-2 COMPLETION01-Apr-2004 #1 ENG OUT 0.36003493

PMS-2 COMPLETION01-Apr-2004 #2 ENG OUT 0.35003493

PMS-2 COMPLETION01-Apr-2004 AXIAL FAN 0.230.7103493

100 HR REQ29-Sep-2004 #1 ENGINE 0.23003591.1

EDITION OF JAN 64 IS OBSOLETE For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

DA FORM 2408-15-2 E, OCT 91 AIRCRAFT VIBRATION RECORD


IPS READINGS4.



100 HR REQ29-Sep-2004 #2 ENGINE 0.15003591.1

100 HR REQ29-Sep-2004 AXIAL FAN 0.230.5603591.1

PMI-1 COMPLETION AND 120 HR REQ27-May-2006 #1 ENGINE 0.23003791.2

PMI-1 COMPLETION AND 120 HR REQ27-May-2006 #2 ENGINE 0.02003791.2

PMI-1 COMPLETION AND 120 HR REQ27-May-2006 AXIAL FAN 0.190.3903791.2

120 HOUR22-Mar-2007 #1 ENG 0.29003917.1

120 HOUR22-Mar-2007 #2 ENG 0.18003917.1

120 HOUR22-Mar-2007 OIL COOLER 0.59003917.1

120 HOUR22-Mar-2007 T/R 0.06003917.1

120 HR26-Sep-2007 #1 ENG 0.23004039.8

120 HR26-Sep-2007 #2 ENG 0.26004039.8

120 HR26-Sep-2007 OIL COOLER 0.52004039.8

POST PHASE19-Jan-2008 #1 ENG 0.26004151.2

POST PHASE19-Jan-2008 #2 ENG 0.49004151.2

POST PHASE19-Jan-2008 T/R 0.09004151.2

POST PHASE19-Jan-2008 OIL COOLER 0.74004151.2

UNSCHEDULED MAINTENANCE12-Mar-2008 T/R 0.08004197.3

120 HOUR02-May-2008 #1 ENG 0.29004267.5

120 HOUR02-May-2008 #2 ENG 0.27004267.5

120 HOUR02-May-2008 OIL COOLER 0.5004267.5

120 HOUR02-May-2008 T/R 0.14004267.5

120 HR28-Jul-2008 #1 0.08004388.6

120 HR, ENG REPLACEMENT28-Jul-2008 #2 0.42004388.6

120 HR28-Jul-2008 T/R 0.11004388.6

120 HR28-Jul-2008 OIL COOLER 0.55004388.6

POST PHASE23-Sep-2008 #1 ENG 0.27004471.6

POST PHASE23-Sep-2008 #2 ENG 0.23004471.6




IPS READINGS4.



POST PHASE23-Sep-2008 OIL COOLER 0.59004471.6

POST PHASE24-Sep-2008 T/R 0.07004471.6

RESET16-Jul-2009 #1 DCS 0.36004594.9

RESET16-Jul-2009 #2 DCS 0.29004594.9

RESET16-Jul-2009 OIL COOLER 00.2504594.9

RESET16-Jul-2009 TAIL ROTOR 0.13004594.9

T/R RIG CHECK19-Jul-2009 TAIL ROTOR 0.07004597.6

T/R RIG CK21-Jul-2009 TAIL ROTOR 0.15004600.6

ENG REINSTALLATION21-Jul-2009 #1 DCS 0.09004600.6

9/11 RET IB RETENT PLATE T/R RIG CHECK12-Aug-2009 T/R 0.07004604.9

9-11 I/B RETENTION PLATE20-Oct-2009 T/R 0.14004615.2

120 HOURS29-Jun-2010 #1 HSS 0.18004713.7

120 HOURS29-Jun-2010 #2 HSS 0.22004713.7

120 HRS29-Jun-2010 OIL COOLER 00.2104713.7

120 HOURS29-Jun-2010 TAIL ROTOR 0.03004713.7

120 HR.26-Apr-2011 OIL COOLER 0.110.3604835.4

120 HR.26-Apr-2011 #1 HSS 0.25004835.4

120 HR.26-Apr-2011 #2 HSS 0.29004835.4

120 HR.26-Apr-2011 T/R 0.06004835.4

120 HR INSP03-Mar-2012 OIL COOLER 00.4705007.1

120 HR INSP03-Mar-2012 #1 ENG HSS 0.21005007.1

120 HR INSP03-Mar-2012 #2 ENG HSS 0.21005007.1

120 HR INSP03-Mar-2012 TAIL ROTOR 0.2005007.1

120 HR INSP21-Aug-2012 #1 ENG HSS 0.22005125.8

120 HR INSP21-Aug-2012 #2 ENG HSS 0.26005125.8

120 HR INSP21-Aug-2012 OIL COOLER 00.1605125.8

120 HR INSP21-Aug-2012 TAILROTOR 0.12005125.8




IPS READINGS4.



REINSTALLED28-Sep-2013 TAIL ROTOR 0.08005256.1

REINSTALLED28-Oct-2013 TAIL ROTOR 0.09005265.7

REINSTALLED FROM INBRD RETENTION CHKS08-Nov-2013 TAIL ROTOR 0.06005275.2

120 HR09-Apr-2014 TAIL ROTOR 0.13005364.9

120 HR09-Apr-2014 OIL COOLER 0.210.605364.9

120 HR09-Apr-2014 #1 HSS 0.15005364.9

120 HR09-Apr-2014 #2 HSS 0.1005364.9

POST PHASE04-Nov-2015 #1 ENG HSS 0005601.1

POST PHASE04-Nov-2015 #2 HSS 0.01005601.1

POST PHASE04-Nov-2015 TAIL ROTOR 0.02005601.1

6. Remarks

JM689994

POST PHASE TEST FLIGHTIVHMS .02 IPS

04-Nov-2015

AASF2WV75C0



h

CONDITION ITEMS

kjifdcba g.

RMVL HR

RMVL HRSWUC HRS)COMPO/H

NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE

SINCEPREVSER NO.ANDNOMENCLATURE DUE

REPLACE

INST HRSTIMEINST HRSNO.COMPONENTPNCOMP REP.O/H ORNOMEN6.

3. PART NUMBER ORMODEL

2. NSN 4. SERIAL NUMBER 5. WUC1. NOMENCLATURE

Report Date: 1/1217-Jan-2016

79232731520010350266 00HELICOPTER, UTILITY

156001095713502C12D

00UNK327370219-05001-042TAIL CONE FITTING CCCC COND COND

162001231183103A01

05510BEM316770250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001231183103A01 R/H

04470IA0041070250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001421089003B01

05247BMC89170250-13101-044SHOCK ABSORBER (TAIL) CCCC COND COND

165001285302405A01Z

16404595A106-00055R70106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z

4444595R106-0328170106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z


165001285302405A01Z


531501537465205A02H YELLOW

04887B9411269270103-08108-041SOLID BLADE PIN CCCC COND COND

531501537465205A02H BLACK


531501537465205A02H BLUE


531501537465205A02H BLUE


531501537465205A02H BLACK


531501537465205A02H RED


531501537465205A02H YELLOW


531501537465205A02H RED


161501199764605A03A

0459515152192470104-08000-050SWASHPLATE ASSY CCCC COND COND

161501078571806A11

30984595A258-0373870351-08080-043ACCESSORY MODULE CCCC COND COND

161501383899206A11

5304595A258-0701070351-08080-045ACCESSORY MODULE CCCC COND COND

For use of this form, see DA PAM 738-751; the proponet agency is DCSLOGEDITION MAY 67 IS OBSOLETE

DA FORM 2408-16-E, OCT 91 AIRCRAFT COMPONENT HISTORICAL RECORD

h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






161501503311506A

24134595A2650033470351-08100-076MAIN TRANSMISSIONMODULE

CCCC COND COND

161501230621806E

38504595A2640177170351-08001-046INPUT MODULE CCCC COND COND

161501353382506E

17504595A264-0628970351-08001-049INPUT MODULE CCCC COND COND

168001074515206F

45054595A0050011570357-06300-042INTERMEDIATE GEARBOX CCCC COND COND

161501376508906G01

1204595A0060301470358-06600-046TAIL ROTOR GEARBOXASSY

CCCC COND COND

161501524780506H04 2

04595C845-0481270361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501524780506H04 1

04595C845-0494270361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501081277506H06

45954595A2710009970361-03001-045SHAFT ASSY, T/R DRV SEC1

CCCC COND COND

161501158951706H08

21014595WG6366P0000770361-03009-047SHAFT ASSY, T/R DRV SEC2

CCCC COND COND

161501082650006H09

45954595A2720024870361-05001-045SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501082650006H09


CCCC COND COND

161501082650006H09


CCCC COND COND

161501083295306H11


CCCC COND COND

161501277910606H12


CCCC COND COND

432001207722807A01

1712560171912ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01 # 1

12934889K3275ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01

11665269K1045ABR70652-02300-050PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

481001102247307B05A

11464595198270306-02107-104VALVE, SOLENIOD CCCC COND COND

481001102247307B05A

11464595P-31670306-02107-104VALVE, SOLENIOD CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






165001222431607B12

176648879353275A3197170-5ACCUMULATOR CCCC COND COND

168001342049608B20

1146459522370450-01043-124PANEL INDICATOR (PDU) CCCC COND COND

168001342049608B20

11464595355270450-01043-124PANEL INDICATOR (PDU) CCCC COND COND

168001566036608F01

049260135630279-0302IVHMU (CBM MONITORSYSTEM)

CCCC COND COND

611501114969609A01

530459525-A233128B302-8-DMGENERATOR CCCC COND COND

611501114969609A01

1146459580E28B302-8-DMGENERATOR CCCC COND COND

161501260074911C21

05601439170670400-02300-046MIXER ASSEMBLY CCCC COND COND

156001411515111D17

00UNK273-0170209-22103-065SERVO BEAM FITTING CCCC COND COND

156001411515611D17


156001411515011D17


156001411514811D17


168001261204411D25

19105083B2920552470400-06641-117STABILATOR ACTUATOR CCCC COND COND

168001261204411D25

76050981772DL2155M20STABILATOR ACTUATOR CCCC COND COND

599601316274311D26 1

108850982241A70902-02001-048STABILATOR AMPLIFIER CCCC COND COND

599601316274311D26 2

8315081R9300017170902-02001-048STABILATOR AMPLIFIER CCCC COND COND

299501496368615A04

0560148614504587ENGINE SEQUENCINGUNIT

CCCC COND COND

599601415867319D01A

99245953301A822-0787-001AMPLIFIER, RADIOFREQUENCY

CCCC COND COND

582101413423419D02

03328517AA8220786001CONTROL, HF RADIO SET CCCC COND COND

NSN PENDING19E04B

052813440P320A002-03SIGNAL DATACONVERTER

CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






589501245909019E05A

1335601160EESM-C-967292RECEIVER-TRANSMITTERRADAR

CCCC COND COND

581001376138019H

942480529410N616736-1TSEC/KY-100 PROCESSOR CCCC COND COND

661001490516852A

430550812095210825050-1-001AUTOMAT FLT CONTCOMPUTER

CCCC COND COND

SIGNIFICANT HISTORICAL EVENTS7.




kjigfdcbaRMVL HR RMVL HRS

NOMEN HRS)COMPO/HO/HLOCATIONNSNWUC

he (ACFTLIFESINCEPRESER NO.ANDAND

INST HRSP/N DUEREPLACE

INST HRSTIMENO.COMPONENTNOMENCLATURE

NOMEN REP.O/H OCOMP6.

4. SERIAL NUMBER3. PART NUMBER OR MODEL2. NSN 5. WUC1. NOMENCLATUR

Report Date:

TIME CHANGE COMPONENTS5/1217-Jan-2016

00

156001081924402C15J20000

UNK3273 0070209-06051-043TAIL PYLON FITTING RCRC20000

161501450483405A01A10465

C30800297 0536570103-08112-047HUB, M/R ROTOR ASSY RCRC5100

161501442692605A01I BLACK11680

A00105362 1567524770102-08200-069MAIN ROTOR SPINDLEASSY

RCRC8000

161501442692605A01I BLUE11881


RCRC8000

161501442692605A01I RED13247


RCRC8000

161501442692605A01I YELLOW12564

D00100441 683524770102-08200-069MAIN ROTOR SPINDLEASSY

RCRC8000

161501074515105A01L14639

B28600498 3956459570351-08186-043MAIN ROTOR SHAFTEXTENDER

RCRC14000

161501127738805A01T13000

U-10 4724472470107-08400-046BIFILAR, M/R ROTORASSY

RCRC13000

161501106190305A02 RED10341

A00704213 4860560170150-09100-043MAIN ROTOR BLADEASSY

RCRC9600

161501106190305A02 BLACK12379


RCRC9600

161501106190305A02 YELLOW12934


RCRC9600

161501106190305A02 BLUE13475


RCRC9600

161501113818805B02 BL/BLK11725

A00903149 3876560170101-31000-043TAIL ROTOR BLADEASSY

RCRC10000

161501113818805B02 R/Y12772

A00905678 2829560170101-31000-043TAIL ROTOR BLADEASSY

RCRC10000

161501083681206G01B17601

K25700321 0560170102-11101-042O/B RETENTION PLATE(T/R)

RCRC12000

414001329342806H237115

1342 890548552E15-1FAN AXIAL 002520

156001129125607A2416133

B11205407 1754488770410-02500-049SAS ACTUATOR RCRC13000

156001129125607A24 ROLL14989

B11205422 2606459570410-02500-049SAS ACTUATOR RCRC13000

156001129125607A2414256

D112-13142 3814507070410-02500-049SAS ACTUATOR RCRC13000

For use of this form, see DA PAM 738-751; The proponet agency isDCSLOG

EDITION MAY 67 IS OBSOLETE

AIRCRAFT COMPONENT HISTORICALRECORD

DA FORM 2408-16-E, OCT 91









Report Date:


00

161501141753211C236311

233-03412 444459570400-06100-042TAIL ROTOR PITCHCHANGE SHAFT

002160

165001305695411C2515699

B300-00067 389645952227000-17TAIL ROTOR SERVOASSY

RCRC15000

165001143122611D01 A27394

B303-05171 16014595274000-1031MAIN ROTOR PRIMARYSERVO

RCRC24400

165001143122611D01 F26183

B303-06435B 2812459570410-02820-054MAIN ROTOR PRIMARYSERVO

RCRC24400

165001143122611D0127668

B30310028 1327459570410-02820-054MAIN ROTOR PRIMARYSERVO

RCRC24400

156001158968511D0413000

A345-00953 4724472470400-08102-045AFT BELLCRANK RCRC13000

156001164416111D0519494

A39101787 0249470400-08112-045AFT TIE ROD SUPTFITTING

RCRC17000

168001164416011D065693

MM00239 0349370400-08111-042AFT TIE ROD ASSY RCRC2200

156001286887011D076900

390-01255 2095459570400-08117-049AFT BELLCRANK SPTASSY

RCRC4400

304001189971111D0812497

C38000081 3098459570400-08151-050LATERAL SWASHPLATELINK

RCRC11000

168001221286311D0922994

F337-01039 1601459570400-08166-041LATERAL SERVOBELLCRANK

RCRC20000

168001158965311D1116601

R34600674 0560170400-08104-048AFT WALKING BEAM RCRC11000

156001083295411D1314565

D34400052 4030459570400-08115-043LEFT TIE ROD RCRC14000

156001296948611D148747

288-01312 0524770400-08114-051RIGHT TIE ROD ASSY RCRC3500

168001158965211D1519151

6693600642 444459570400-08101-046FORWARD BELLCRANK RCRC15000

156001221261911D1618151

B36703344 444459570400-08162-042FORWARD BELLCRANKSUPPORT

RCRC14000













Report Date:


00

SIGNIFICANT HISTORICAL EVENTS7.





ji kgfdcbaRMVL HRSRMVL HRSCOMPO/HNOMENWUC

HRS)O/HLOCATIONNSN

AND he SINCELIFE (ACFT

PREVSER NO. OAND

NOMENCLATURE PN TIMEINST HRS DUEREPLACE

INST HRSNO.COMPONENTNOMEN REP.O/H ORCOMP6.

1520010350266HELICOPTER,UTILITY

UH-60A 7923273 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 8 of 12

17-Jan-2016

COND COND

156001095713502C12D

00TAIL CONE FITTING UNK327370219-05001-042 CCCC

20000 20000

156001081924402C15J

00TAIL PYLON FITTING UNK327370209-06051-043 RCRC

COND COND

162001231183103A01

05510FWD FIXED GEARSHOCK

BEM316770250-12051-045 CCCC

COND COND

1620012311831 R/H03A01


IA0041070250-12051-045 CCCC

COND COND

162001421089003B01

05247SHOCK ABSORBER(TAIL)

BMC89170250-13101-044 CCCC

5100 10465

161501450483405A01A

05365HUB, M/R ROTOR ASSY C3080029770103-08112-047 RCRC

8000 11680

1615014426926 BLACK05A01I

15675247MAIN ROTOR SPINDLEASSY

A0010536270102-08200-069 RCRC

8000 11881

1615014426926 BLUE05A01I


A0010796870102-08200-069 RCRC

8000 13247

1615014426926 RED05A01I


A0011178970102-08200-069 RCRC

8000 12564

1615014426926 YELLOW05A01I


D0010044170102-08200-069 RCRC

14000 14639

161501074515105A01L

39564595MAIN ROTOR SHAFTEXTENDER

B2860049870351-08186-043 RCRC

13000 13000

161501127738805A01T

47244724BIFILAR, M/R ROTORASSY

U-1070107-08400-046 RCRC

COND COND

165001285302405A01Z

16404595DAMPER ASSY, M/R A106-00055R70106-08100-046 CCCC

COND COND

165001285302405A01Z

4444595DAMPER ASSY, M/R R106-0328170106-08100-046 CCCC

COND COND

165001285302405A01Z


COND COND

165001285302405A01Z


9600 10341

1615011061903 RED05A02

48605601MAIN ROTOR BLADEASSY

A0070421370150-09100-043 RCRC

9600 12379

1615011061903 BLACK05A02


A0070906670150-09100-043 RCRC

9600 12934

1615011061903 YELLOW05A02


A0071311370150-09100-043 RCRC

9600 13475

1615011061903 BLUE05A02


A0071312170150-09100-043 RCRC

COND COND

5315015374652 YELLOW05A02H

04887SOLID BLADE PIN B9411269270103-08108-041 CCCC

EDITION MAY 67 IS OBSOLETE For use of this form, see DA PAM 738-751; the proponet agency is DCSLOG

AIRCRAFT COMPONENT HISTORICAL RECORDDA FORM 2408-16 E, OCT 91


HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 9 of 12

17-Jan-2016

COND COND

5315015374652 BLACK05A02H


COND COND

5315015374652 BLUE05A02H


COND COND

5315015374652 BLUE05A02H


COND COND

5315015374652 BLACK05A02H


COND COND

5315015374652 RED05A02H


COND COND

5315015374652 YELLOW05A02H


COND COND

5315015374652 RED05A02H


COND COND

161501199764605A03A

04595SWASHPLATE ASSY 15152192470104-08000-050 CCCC

10000 11725

1615011138188 BL/BLK05B02

38765601TAIL ROTOR BLADEASSY

A0090314970101-31000-043 RCRC

10000 12772

1615011138188 R/Y05B02

28295601TAIL ROTOR BLADEASSY

A0090567870101-31000-043 RCRC

COND COND

161501078571806A11

30984595ACCESSORY MODULE A258-0373870351-08080-043 CCCC

COND COND

161501383899206A11

5304595ACCESSORY MODULE A258-0701070351-08080-045 CCCC

COND COND

161501503311506A

24134595MAIN TRANSMISSIONMODULE

A2650033470351-08100-076 CCCC

COND COND

161501230621806E

38504595INPUT MODULE A2640177170351-08001-046 CCCC

COND COND

161501353382506E

17504595INPUT MODULE A264-0628970351-08001-049 CCCC

COND COND

168001074515206F

45054595INTERMEDIATEGEARBOX

A0050011570357-06300-042 CCCC

COND COND

161501376508906G01

1204595TAIL ROTOR GEARBOXASSY

A0060301470358-06600-046 CCCC

12000 17601

161501083681206G01B

05601O/B RETENTION PLATE(T/R)

K2570032170102-11101-042 RCRC

COND COND

1615015247805 206H04

04595DRIVESHAFT ASSYENGINE

C845-0481270361-08014-041 CCCC

COND COND

1615015247805 106H04

04595DRIVESHAFT ASSYENGINE

C845-0494270361-08014-041 CCCC

COND COND

161501081277506H06

45954595SHAFT ASSY, T/R DRVSEC 1

A2710009970361-03001-045 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 10 of 12

17-Jan-2016

COND COND

161501158951706H08


WG6366P0000770361-03009-047 CCCC

COND COND

161501082650006H09

45954595SHAFT ASSY, T/R SEC3,4,5

A2720024870361-05001-045 CCCC

COND COND

161501082650006H09


A2720025270361-05001-045 CCCC

COND COND

161501082650006H09


A2720025670361-05001-045 CCCC

COND COND

161501083295306H11


A2730009770361-05002-045 CCCC

COND COND

161501277910606H12


A2740010970361-06002-044 CCCC

2520 7115

414001329342806H23

8905485FAN AXIAL 134252E15-1 00

COND COND

432001207722807A01

17125601PUMP MODULE ASSY,HYDRAUL

71912ABR53023-06 CCCC

COND COND

4320012077228 # 107A01


K3275ABR53023-06 CCCC

COND COND

432001207722807A01


K1045ABR70652-02300-050 CCCC

13000 16133

156001129125607A24

17544887SAS ACTUATOR B1120540770410-02500-049 RCRC

13000 14989

1560011291256 ROLL07A24

26064595SAS ACTUATOR B1120542270410-02500-049 RCRC

13000 14256

156001129125607A24

38145070SAS ACTUATOR D112-1314270410-02500-049 RCRC

COND COND

481001102247307B05A

11464595VALVE, SOLENIOD 198270306-02107-104 CCCC

COND COND

481001102247307B05A

11464595VALVE, SOLENIOD P-31670306-02107-104 CCCC

COND COND

165001222431607B12

17664887ACCUMULATOR 9353275A3197170-5 CCCC

COND COND

168001342049608B20

11464595PANEL INDICATOR (PDU) 22370450-01043-124 CCCC

COND COND

168001342049608B20

11464595PANEL INDICATOR (PDU) 355270450-01043-124 CCCC

COND COND

168001566036608F01

04926IVHMU (CBM MONITORSYSTEM)

0135630279-0302 CCCC

COND COND

611501114969609A01

5304595GENERATOR 25-A233128B302-8-DM CCCC

COND COND

611501114969609A01

11464595GENERATOR 80E28B302-8-DM CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 11 of 12

17-Jan-2016

COND COND

161501260074911C21

05601MIXER ASSEMBLY 439170670400-02300-046 CCCC

2160 6311

161501141753211C23

4444595TAIL ROTOR PITCHCHANGE SHAFT

233-0341270400-06100-042 00

15000 15699

165001305695411C25

38964595TAIL ROTOR SERVOASSY

B300-000672227000-17 RCRC

24400 27394

1650011431226 A11D01

16014595MAIN ROTOR PRIMARYSERVO

B303-05171274000-1031 RCRC

24400 26183

1650011431226 F11D01


B303-06435B70410-02820-054 RCRC

24400 27668

165001143122611D01


B3031002870410-02820-054 RCRC

13000 13000

156001158968511D04

47244724AFT BELLCRANK A345-0095370400-08102-045 RCRC

17000 19494

156001164416111D05

02494AFT TIE ROD SUPTFITTING

A3910178770400-08112-045 RCRC

2200 5693

168001164416011D06

03493AFT TIE ROD ASSY MM0023970400-08111-042 RCRC

4400 6900

156001286887011D07

20954595AFT BELLCRANK SPTASSY

390-0125570400-08117-049 RCRC

11000 12497

304001189971111D08

30984595LATERAL SWASHPLATELINK

C3800008170400-08151-050 RCRC

20000 22994

168001221286311D09

16014595LATERAL SERVOBELLCRANK

F337-0103970400-08166-041 RCRC

11000 16601

168001158965311D11

05601AFT WALKING BEAM R3460067470400-08104-048 RCRC

14000 14565

156001083295411D13

40304595LEFT TIE ROD D3440005270400-08115-043 RCRC

3500 8747

156001296948611D14

05247RIGHT TIE ROD ASSY 288-0131270400-08114-051 RCRC

15000 19151

168001158965211D15

4444595FORWARD BELLCRANK 669360064270400-08101-046 RCRC

14000 18151

156001221261911D16

4444595FORWARD BELLCRANKSUPPORT

B3670334470400-08162-042 RCRC

COND COND

156001411515111D17

00SERVO BEAM FITTING UNK273-0170209-22103-065 CCCC

COND COND

156001411515611D17


COND COND

156001411515011D17


COND COND

156001411514811D17





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 12 of 12

17-Jan-2016

COND COND

168001261204411D25

19105083STABILATOR ACTUATOR B2920552470400-06641-117 CCCC

COND COND

168001261204411D25

7605098STABILATOR ACTUATOR 1772DL2155M20 CCCC

COND COND

5996013162743 111D26

10885098STABILATOR AMPLIFIER 2241A70902-02001-048 CCCC

COND COND

5996013162743 211D26

8315081STABILATOR AMPLIFIER R9300017170902-02001-048 CCCC

COND COND

299501496368615A04

05601ENGINE SEQUENCINGUNIT

48614504587 CCCC

COND COND

599601415867319D01A

9924595AMPLIFIER, RADIOFREQUENCY

3301A822-0787-001 CCCC

COND COND

582101413423419D02

03328CONTROL, HF RADIOSET

517AA8220786001 CCCC

COND COND

NSN PENDING19E04B

05281SIGNAL DATACONVERTER

3440P320A002-03 CCCC

COND COND

589501245909019E05A

1335601RECEIVER-TRANSMITTER RADAR

160EESM-C-967292 CCCC

COND COND

581001376138019H

9424805TSEC/KY-100PROCESSOR

29410N616736-1 CCCC

COND COND

661001490516852A

43055081AUTOMAT FLT CONTCOMPUTER

2095210825050-1-001 CCCC

7. SIGNIFICANT HISTORICAL DATA




HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 BEM3167 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

17-Jan-2016

9000 14510

165001125090703A01A

00PISTON, MAIN L/GEARSTR

BEM316770250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 BEM3167 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

17-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 IA00410 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

17-Jan-2016

9000 13470

1650011250907 R/H03A01A

00MAIN SHOCK STRUTPISTON

IA0599270250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 IA00410 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

17-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615014426926MAIN ROTORSPINDLE ASSY

70102-08200-069 A00105362 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

17-Jan-2016

COND COND

3110011589607 BLACK05A01I02C

5561567THRUST BEARING B32542344SB7002-048 CCCC

COND COND

1615011614373 BLACK05A01I02

5401567SPHERICAL BEARINGASSY

B32431522SB7001-048 CCCC

13000 17040

5310011269444 BLACK05A01I04

6511011M/R SPINDLE NUT C4791194770102-08105-102 RCRC

8000 11680

5306014606020 BLACK05A01I06

10111011TIE ROD (M/R SPINDLE) C5040183938023-10372-101 RCRC

20000 23504

1615012149140 BLACK05A01I07

11871011HORN ASSEMBLY A2411570470102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

17-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

17-Jan-2016

COND COND

3110011589607 BLUE05A01I02C


COND COND

1615011614373 BLUE05A01I02


B32425083SB7001-048 CCCC

13000 16881

5310011269444 BLUE05A01I04

00M/R SPINDLE NUT F4790102970102-08105-102 RCRC

8000 11881

5306014606020 BLUE05A01I06

00TIE ROD (M/R SPINDLE) D5040008038023-10372-101 RCRC

20000 23881

1615012149140 BLUE05A01I07






HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

17-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

17-Jan-2016

COND COND

3110011589607 RED05A01I02C


COND COND

1615011614373 RED05A01I02


C32408452SB7001-048 CCCC

13000 18247

5310011269444 RED05A01I04


COND COND

1615014331966 RED05A01I06

00TIE ROD (M/R SPINDLE) C5041304170102-08102-103 CCCC

1700 6947

1615010842285 RED05A01I07

00CONTROL HORN ASSY H2410160970102-08111-043 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

17-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-069 D00100441 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

17-Jan-2016

COND COND

3110011589607 YELLOW05A01I02C

683683THRUST BEARING C32503887SB7002-048 CCCC

COND COND

1615011614373 YELLOW05A01I02


LK4697SB7001-048 CCCC

13000 17564

5310011269444 YELLOW05A01I04


8000 12564

5306014606020 YELLOW05A01I06

00TIE ROD (M/R SPINDLE) C5040399538023-10372-101 RCRC

20000 24564

1615012149140 YELLOW05A01I07






HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-069 D00100441 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

17-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70150-09100-043 A00704213 05A024. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

17-Jan-2016

COND COND

156001447977405A02E

04860M/R BLADE TIP CAP B8490787470150-09207-041 CCCC

5000 6090

161501099234105A02I

35593908M/R BLADE CUFF A2370657070150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

17-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

17-Jan-2016

COND COND

156001447977405A02E

26402822M/R BLADE TIP CAP A8491131270150-09207-041 CCCC

5000 6860

161501099234105A02I

33152396M/R BLADE CUFF A2370958770150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

17-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

17-Jan-2016

COND COND

156001447977405A02E

3572267M/R BLADE TIP CAP B8490793770150-09207-041 CCCC

5000 8334

161501099234105A02I

00M/R BLADE CUFF F2370004970150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

17-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

17-Jan-2016

COND COND

156001447977405A02E

11781726M/R BLADE TIP CAP A8491423570150-09207-041 CCCC

5000 7699

161501099234105A02I

28931717M/R BLADE CUFF 3315093570150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

17-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615011997646SWASHPLATE ASSY 70104-08000-050 151521924 05A03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

17-Jan-2016

COND COND

161501087160205A03A01

129129STATIONARYSWASHPLATE

015152-187470104-08010-044 CCCC

11000 15595

161501357508905A03A02

00ROTATINGSWASHPLATE ASSEMBL

15152192470104-08001-045 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615011997646SWASHPLATE ASSY 70104-08000-050 151521924 05A03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

17-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

17-Jan-2016

17000 21595

161501078571106A08

02413SWASHPLATE GUIDE AER0118470351-08227-041 RCRC

3000 7595

161501110149106A13

02413HOUSING ASSY MGB A2110143070351-08110-045 RCRC

7600 12195

304001415838806A18

02413MAIN ROTOR SHAFT E2530461770351-08131-048 RCRC

12000 16595

161501497725706A19

02413PLANETARY CARRIERASSY

F2400013770351-08175-046 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

17-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615013765089TAIL ROTORGEARBOX ASSY

70358-06600-046 A00603014 06G014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

17-Jan-2016

12000 15627

161501074515306G01C

968120I/B RETENTION PLATET/R

C2590072170358-06612-042 RCRC

5000 9595

304001292161706G01D

0120GEARSHAFT, BEVEL F3200092170358-06620-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615013765089TAIL ROTORGEARBOX ASSY

70358-06600-046 A00603014 06G014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

17-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



4140013293428FAN AXIAL 52E15-1 1342 06H234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

17-Jan-2016

2520 7115

311001127300506H23A

890890BALL BRNG ANN (OILCOOLER FWD)

1342AFTZ33C32 RCRC

2520 7115

311001127300506H23A

890890BALL BRNG ANN (OILCOOLER FWD)

1342FWDZ33C32 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



4140013293428FAN AXIAL 52E15-1 1342 06H234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

17-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70400-06100-042 233-03412 11C234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

17-Jan-2016

2160 6311

311001113828811C23A

00BRNG T/R PITCH CHGSHAFT

10827SB1162-102 RCRC

COND COND

534001094578911C23C

573573CLEVIS, ROD END 233034122607201070400-06702-041 CCCC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70400-06100-042 233-03412 11C234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

17-Jan-2016




PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN

8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.

AFT BELLCRANK SPT ASSY 7923273390-012551. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


12-Dec-1995 OT

QC00000016-Jan-1996

0.5AASF #1,TOPEKA, KS.(GP9820)

ALL UH-60 SERIES AIRCRAFT,REMOVAL OF SPECIFIC SERIALNUMBERED AFT BELLCRANKSUPPORT ASSEMBLIES, P/N 70400-08117-049

UH-60-96-04MWO:

Priority Mnt Level

For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1-E, OCT 91

PIDMWODATE HRS



AFT BELLCRANK 7923273A345-009531. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


10-Jul-2010 OT

DM64902827-Jul-2010

1AASF#1 NJARNGALL H-60 SERIES AIRCRAFT:COMMON COMPONENTRETIREMENT CHANGE TIMESUPDATE

H-60-10-ASAM-11MWO:

Priority Mnt Level




7923273116305-302AUXILIARY POWER UNIT826043

234

802

1519

4556

197

197

3

3

5=

TOTAL COMPONENT COUNTS

COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-

READING AT INSTALLATION OF

MODULE/RECORDER3

READING AT REMOVAL OF

7. HISTORY RECORDER S/N

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE

OPERATING HOURSTEMP/TEMP INDEXLCF - 2LCF - 1

HISTORICAL COUNTS ON COMPONENT/MODULE

7. HISTORY RECORDER S/N6.

5. NHA - Serial Number4. P/N3. NOMENCLATURE2. Serial Number1. MODEL

**Note - APU Information LCF1 = NUMBER OF OVERHAULS LCF2 = STARTS SINCEOVERHAUL TTI = STARTS SINCE NEW OPH = ONLY FOR APU's WITH HOUR METERINSTALLED - ENTER TIME ON METER

For use of this form, see DA PAM 738-751; the proponet agency is DCSLOG

HISTORY RECORDER, COMPONENT, MODULE RECORDDA FORM 2408-16-1-E, OCT91

OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-

12.HISTORY COUNTS AT LAST DEPOTREPL

11.

O/H OR

10.

SERIAL NUMBER9.PART NUMBERNOMENCLATURE

8.

ReportDate:

Major Nomenclature Major Part NumberMajor Wuc Major Serial Number

17-Jan-2016 2/2

15B 116305-302 AUXILIARY POWER UNIT 826043

763435903

0000V42-C56134502902WHEEL,COMPRESSOR

7322

6000

763435903

0000V82-HC6434503991WHEEL, TURBINE

7322

6000


8/27/200812:00:00 AM

1 REPAIRED I/A/W DMWR 55-2835-209. APU TSN=802, SSN=4556, TSO=39,SSO=197, POH=3. METER READING: EVENTS=1519, HOURS=234. INSPECTORSTAMP #277.

QC000000 HAMILTONSUNDSTRAND

SAN DIEGO,CA

REVERSE OF DA FORM 2408-16-1 E, OCT 91

365

360

5497.5

7923273 197 0

e. ACFT HRS INSTALLEDc. TIME SINCE NEW OR OVERHAULc. SERIAL NUMBER

UH-60A 826043 Days

b. MAKE OR TYPE d. ACFT HRS LAST OIL CHANGEb. SERIAL NUMBER

HELICOPTER, UTILITY AUXILIARY POWER UNIT Hrs

a. NOMENCLATURE AND TYPEa. NOMENCLATUREFREQUENCY

COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b

SAMPLE DATE PIDSAMPLELAST OILEND ITEM

RESULTSDATE RESULTS RECEIVED7. 8.6. REASON FORHOURS5.4.

COMPONENTCHANGE

JW82396104-Jun-2009NORMALINITIAL0.0802459502-Jun-2009

MB86971409-Jun-2010NORMALROUTINE94.0802468902-Jun-2010

KS17333711-Jan-2012NORMALROUTINE390.0802498509-Dec-2011

DN33751602-Jul-2012NORMALROUTINE385.080238529-Jun-2012

KM23856522-Aug-2013ABNORMALROUTINE185.080298716-Aug-2013

KM23856509-Sep-2013NORMALSPECIAL192.080299404-Sep-2013

DN33751602-Sep-2014NORMALROUTINE4672.64715473.316-Aug-2014

DN33751610-Dec-2014NORMALROUTINE4695.54795497.509-Dec-2014

DN33751606-Nov-2015NORMALROUTINE103.64955601.104-Nov-2015

ANALYSIS FINDING: SAMPLING TECHNIQUE. LAB RECOMMENDATIONS: RESAMPLE AT THE END OF THE NEXT FLIGHT DAY/CYCLE.04SEP13

9. REMARKS:

For use of this form, see DA PAMs 738-751; the proponent agency is DCSLOGDA FORM 2408-20, DEC 91, MAY BE USED

OIL ANALYSIS LOGDA FORM 2408-20, OCT 1997

PIDMWODATE HRS



BIFILAR, M/R ROTOR ASSY 7923273U-101. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


14-Jul-2010 OT

DM64902827-Jul-2010


H-60-10-ASAM-11MWO:

Priority Mnt Level



PIDMWODATE HRS



CLEVIS, ROD END 792327323303412260720101. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


14-Jul-2010 OT

DM64902827-Jul-2010


H-60-10-ASAM-11MWO:

Priority Mnt Level



PIDMWODATE HRS



7923273UH-60AHELICOPTER, UTILITY

3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE


DR03-Dec-2005

PROJECT OLRDYNCORPFTCKY (CB9208)

3702-Feb-2006

CIV CONTROL ,QUALITY

INSTALLATION OF ELECTRONIC DATAMANAGEMENT (EDM) SYSTEM FORBLUE FORCE TRACKING

1-1520-237-50-EDMMWO:

Mnt LevelPriority

OU15-Jun-1990

W3EMB5 (NOPID)

102-Jul-1990


ONE TIME INSPECTION OF MAINROTOR PITCH CONTROL HORNS

55-1520-237-20-117MWO:

Mnt LevelPriority

DM18-Jun-1993

CCAD (NO PID) 296903-Mar-1995


INCORPORATION OF UH-60AREFURBISHMENT/STANDARDIZATIONPROGRAM

1-1520-237-55-07MWO:

Mnt LevelPriority

DM12-Aug-1983

PROJECT OLRFTC KY (NOPID)

4803-Mar-1995


UPPER CARGO TRACK ASSEMBLY55-1520-237-50-12MWO:

Mnt LevelPriority

DN25-May-1983


203-Mar-1995


MODIFICATION OF MAIN ROTORSERVO INPUT PUSHROD ASSEMBLY(UH-60A HELICOPTERS)

55-1520-237-50-13MWO:

Mnt LevelPriority

DN18-Jun-1993



SERVO BEAM RAILING REPLACEMENT1-1520-237-50-11MWO:

Mnt LevelPriority

DN07-Mar-1995



INCORPORATION OF IMPROVEDAIRSPEED SYSTEM (UH-60AHELICOPTERS)

1-1520-237-50-22MWO:

Mnt LevelPriority

DN01-May-1994



INCORPORATION OF IMPROVED FIREEXTINGUISHER CIRCUIT ANDHELLFIRE CONNECTOR (UH-60 A/LAND EH-60A)

1-1520-237-50-66MWO:

Mnt LevelPriority

DN01-Feb-1993



INSTALLATION OF DUAL AN/ARC-186/ARC-201 (V) FM RADIO SYSTEMSAND HARDWIRING OF TSEC KY-58 (UH-60A HELICOPTERS) NATIONALSTOCK NUMBER (NSN) 1520-01-035-0266

1-1520-237-50-69MWO:

Mnt LevelPriority


DA FORM 2408-5 E, OCT 91 EQUIPMENT MODIFICATION RECORD

PIDMWODATE HRS






DN29-Jul-1994



INSTALLATION OF ELECTRICALLYHEATED GLASS CENTER WINDSHIELD(UH-60A HELICOPTER)

1-1520-237-50-70MWO:

Mnt LevelPriority

DN30-Apr-1987

PROJECT OLRFT CAMPBELL(NO PID)

6704-Mar-1988


INCORPORATION OF WIRE STRIKEPROTECTION SYSTEM (WSPS) (UH-60A HELICOPTER)

55-1520-237-50-24MWO:

Mnt LevelPriority

DN30-Jun-2004

DOL-AVIM, FT.DRUM, NY

9006-Jul-2009

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE DOPPLERGPS NAVIGATION SET (DGNS)

1-1520-237-50-92MWO:

Mnt LevelPriority

DN28-Oct-1996

CCAD (NO PID) 607-Jan-1999


MODIFICATION OF CHIP DETECTORWIRING FOR UH-60A HELICOPTERS

1-1520-237-50-26MWO:

Mnt LevelPriority

DN23-Apr-2004

OLR/LSI 1007-Mar-2007

CIV ALIPERTI,JOHN J

INSTALLATION OF BALLISTICPROTECTION SYSTEM

1-1520-237-50-BPSMWO:

Mnt LevelPriority

DR11-Aug-2000

DYNCORP OLRKILLEEN TX(JC8143)

308-Aug-2001


INSTALLATION OF THEPILOT/COPILOT SEATS MA-16(IMPROVED) INERTIA REEL IN ALL UH-60 HELICOPTERS

1-1520-237-50-79MWO:

Mnt LevelPriority

FR03-Oct-2007

CTAVCRAD ATNJARNG

2408-Dec-2010

D, MINSTALLATION OF OPTION II CABINHEATER SYSTEM

SSI NO. 50-36 REV.AMWO:

Mnt LevelPriority

FR08-Oct-2008

DS/2 7608-Oct-2008

CIV KNIGHT,JEFFREY A

INSTALLATION OF CMWS 5THELECTRO OPTICAL MISSLE SENSOR

1-1520-237-99-50MWO:

Mnt LevelPriority

DN31-Oct-1996

PROJ OLR,DYNA CORP(MT4634)

3509-Apr-1997


INSTALLATION OF REDUCEDDIAMETER BALLISTIC TOLERANTFUEL LINES (UH-60A/L AND EH-60AHELICOPTERS)

1-1520-237-50-74MWO:

Mnt LevelPriority

DN05-Oct-1994

PROJ OLR,DYNA CORP(MT4634)

18409-Apr-1997


INSTALLATION OF HEADS UP DISPLAY(HUD) AN/AVS-7 FOR UH-60AHELICOPTERS AND UH-60LHELICOPTERS

1-1520-237-50-62MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN01-Nov-2007

PROJECT OLR,DYNCORP,FTCKY (CB 9208)

90010-Jan-2006


MODIFICATION OF CMWS/IRMD AAR-57

1-1520-237-50-93MWO:

Mnt LevelPriority

DT18-Jun-2003

PROJECT OLRDYNCORPFTCKY (CB 9208)

8010-Jan-2006


INLET BARRIER FILTER SYSTEM FORTHE HAMELTON STANDARD T-62T-40-1

AFS-BH-APU-IBF-IPMWO:

Mnt LevelPriority

DN17-Jan-1989

LSSI/OLR (NOPID)

211-Jul-1989


MODIFICATION OF BEARINGRETAINER SPRING CLIP, TAIL ROTORSERVO (UH/EH-60A HELICOPTERS)

55-1520-237-50-52MWO:

Mnt LevelPriority

DN23-Jan-1989

LSSI/OLR (NOPID)

1611-Jul-1989


MODIFICATION OF MAIN ROTOR HEADANTI-FLAP BRACKETS (UH-60A ANDEH-60A HELICOPTERS)

55-1520-237-50-44MWO:

Mnt LevelPriority

DR21-Jun-2004

PROJECT OLRDYNCORPFTCKY

7513-Feb-2006

SSG JOHNSON,BRIAN D

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE AN/APX-118 TRANSPONDER MODE STRANSPONDER (CXP) ON UH-60A/LAIRCRAFT (NSN 1520-01-035-0266)(NSN 1520-01-298-4532)

1-1520-237-50-84MWO:

Mnt LevelPriority

DR28-Feb-2005


9413-Feb-2006

SSG JOHNSON,BRIAN D

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE AIRWARRIOR MICROCLIMATE COOLINGSYSTEM AND MASK BLOWER WIRINGASSEMBLY ON THE UH-60A/LAIRCRAFT (NSN 1520-01-035-0266)(NSN 1520-01-298-4532)

1-1520-237-50-85MWO:

Mnt LevelPriority

DM08-Feb-2005


36113-Feb-2006

SSG JOHNSON,BRIAN D

ENGINE INLET BARRIER FILTER1-1520-237-50-90MWO:

Mnt LevelPriority

DN06-Nov-2003


3513-Feb-2006

SSG JOHNSON,BRIAN D

INSTALLATION OF AUXILIARY POWERUNIT (APU) INLET BARRIER FILTER(IBF) SYSTEM FOR T-62T-40-1

1-1520-237-50-APU-IBFMWO:

Mnt LevelPriority

DM08-Feb-2005


20013-Feb-2006

SSG JOHNSON,BRIAN D

INSTALLATION OF BLUE FORCETRACKER REVISION 2

1-1520-237-50-BFT2MWO:

Mnt LevelPriority



PIDMWODATE HRS






DR21-Apr-2006


90013-Feb-2006

SSG JOHNSON,BRIAN D

INSTALLATION OF COMMON MISSILEWARNING SYSTEM (CMWS) ANDIMPROVED COUNTERMEASURESDISPENSER SYSTEM (ICDS)

1-1520-237-50-CMWSMWO:

Mnt LevelPriority

DN15-Jan-1991

LSSI/OLR (NOPID)

613-Nov-1991


INCORPORATION OF ENGINE DRIVESHAFT BALANCING PROCEDURE (UH-60A/EH-60A HELICOPTERS)

55-1520-237-50-58MWO:

Mnt LevelPriority

DR30-Apr-1991

LSSI/OLR (NOPID)

11613-Nov-1991


MODIFICATION OF THE HOVERINFERRED SUPPRESSION SYSTEM(UH-60A HELICOPTERS) NATIONALSTOCK NUMBER (NSN) 1520-01-035-0266

1-1520-237-50-63MWO:

Mnt LevelPriority

DN15-Nov-1990

LSSI/OLR (NOPID)

613-Nov-1991


INSTALLATION OF IMPROVEDTIEDOWN RING EYEBOLT (UH-60A/LAND EH-60A)

1-1520-237-50-61MWO:

Mnt LevelPriority

FN15-Sep-1993

DYNCORP-OLRKILLEEN, TX

614-Aug-2001

SGT HARKEY,JAMES D

MODIFICATION OF RADIO SETCONTROL C-10604(V)6/ARC-186(NSN5821-01-076-2245) (EIC: N/A)FORANVIS LIGHTING PROGRAM

11-5821-318-30-2MWO:

Mnt LevelPriority

DR04-Jun-2001

DYNCORP OLRKILLEEN TX(JC8143)

30015-Aug-2001


INSTALLATION OF HFCOMMUNICATION SYSTEM AN/ARC-220(V) AND TSEC/KY-100 IN UH60/LHELICOPTER NSN 1520-01-035-0266UH-60A NSN 1520-01-298-4532 UH-60L

1-1520-237-50-76MWO:

Mnt LevelPriority

DN15-Jan-1989

LSSI (NO PID) 1015-Jan-1989


INCORPORATION OFELECTROMAGENTIC INTERFERENCE(EMI) PROTECTION FOR LEFT ANDRIGHT RELAY PANELS (UH-60A/EH-60A HELICOPTERS)

1-5945-237-50-1MWO:

Mnt LevelPriority

DM22-Feb-1991

LSSI/OLR (NOPID)

60615-Jun-1993


INCORPORATE ELECTRO-MAGNETICENVIRONMENT (EME) PROTECTIONPROVISIONS ON DELIVERED UH-60A/LAND EH-60A HELICOPTERS

1-1520-237-50-59MWO:

Mnt LevelPriority



PIDMWODATE HRS






DR13-Apr-2001

PROJECT OLRKILLEEN, TX(JC1523)

8015-Nov-2002


INSTALLATION OF SEALED LEAD-ACIDBATTERY (SLAB) SYSTEM ANDRELOCATION OF UTILITY LIGHTPOWER (UH-60A/L HELICOPTERS) UH-60A NSN 1520-01-035-0266 UH-60LNSN 1520-01-298-4532

1-1520-237-50-77MWO:

Mnt LevelPriority

DN24-Oct-1984

SIKORSKY (NOPID)

117-May-1984


MIXER RET55-1520-237-50-27MWO:

Mnt LevelPriority

DN08-Nov-1984

SIKORSKY (NOPID)

417-May-1984


KICK PLATES55-1520-237-50-10MWO:

Mnt LevelPriority

DN08-Nov-1984

SIRKORSKY(NO PID)

1.517-May-1984


STAB. GROUND55-1520-237-50-29MWO:

Mnt LevelPriority

DN08-Nov-1984

SIKORSKY (NOPID)

117-May-1984


CHAFF DISP.55-1520-237-50-30MWO:

Mnt LevelPriority

DN24-Oct-1984

SIKORSKY (NOPID)

1.517-May-1984


MAIN ROTOR DAMPER CABLES55-1520-237-50-17MWO:

Mnt LevelPriority

DM01-Jan-1984

SIKORSKY (NOPID)

117-May-1984


FORWARD STOPS55-1520-237-50-8MWO:

Mnt LevelPriority

DN08-Nov-1984

SIKORSKY (NOPID)

317-May-1984


RES. HOIST PROVISIONS55-1520-237-50-9MWO:

Mnt LevelPriority

DN24-Mar-1988

DYNCORP FTHOOD TX (NOPID)

117-Nov-1988


INSTALLATION OF SELF-SEALINGADAPTERS

55-2840-248-50-28MWO:

Mnt LevelPriority

DM18-Apr-1988


117-Nov-1988


INSTALLATION OF IMPROVEDCARTRIDGE ACTUATED DEVICE

55-4030-237-50-01MWO:

Mnt LevelPriority



PIDMWODATE HRS






DU13-Jun-1985


419-Aug-1985


MODIFICATION OF IMPROVED MAINROTOR-TAIL ROTOR PITCH CONTROLROD BOLTS (UH-60A HELICOPTERS)

55-1520-237-50-31MWO:

Mnt LevelPriority

DR06-Oct-2008

LEAR SIEGLERSERVICES INC

91219-Oct-2010

CIV SHAAK,CHARLES

INSTALLATION OF INTEGRATEDVEHICLE HEALTH MANAGEMENTSYSTEM (IVHMS) HEALTH USAGEMANAGEMENT SYSTEM (HUMS) FORUH-60 A/L HELICOPTERS

1-1520-237-50-100 (IVHMS1)MWO:

Mnt LevelPriority

DR07-Nov-2008

LEAR SIEGLERSERVICES INC

25019-Oct-2010

CIV SHAAK,CHARLES

AN/AAR-57 IMPROVEDCOUNTERMEASURE DISPENSERSYSTEM (ICMD) COMMON MISSILEWARNING SYSTEM (MWS) (P31)

1-1520-237-50-97 (D1)MWO:

Mnt LevelPriority

DN31-Aug-1992

120-Apr-2006

IMPROVED CARGO HOOK KEEPERINSTALLATION FOR UH-60AHELICOPTERS

1-1520-237-50-15MWO:

Mnt LevelPriority

DU30-Nov-1983


120-Dec-1983


CARGO HOOK EXTERNAL SPRINGRETROFIT KIT

55-1520-237-50-28MWO:

Mnt LevelPriority

DU30-Mar-1987

LSSI/HAAF (NOPID)

4021-Apr-1987


MODIFICATION OF MAIN ROTORBLADE DE-ICE DISRUPTOR HARNESSAND TAIL ROTOR SLIP RINGHARNESS (UH-60A HELICOPTERS)

55-1520-237-50-36MWO:

Mnt LevelPriority

OT07-Jul-1989

W3EMB5 (NOPID)

421-Aug-1989


TBO/REPLACE LIFE REVISIONSCHEDULE

55-1520-237-20-104MWO:

Mnt LevelPriority

DN15-May-1984


20021-May-1985


INCORPORATION OF WATERINTEGRITY IMPROVEMENTS (UH-60AHELICOPTERS)

55-1520-237-50-18MWO:

Mnt LevelPriority

FR28-Jun-2008

1109TH TASMG 5022-MAY-2014

SGT NELSON,DAVID E

INSTALLATION OF AUTO RELIGHT &TRANSIENT DROOP IMPROVEMENTFOR T700-GE-701D ENGINES ON UH-60A/HH-60A AIRCRAFT

01-1520-237-30-3MWO:

Mnt LevelPriority



PIDMWODATE HRS






DM11-Oct-1983


123-Feb-1984


IMPROVED CARGO HOOK KEEPERINSTALLATION FOR UH-60AHELICOPTERS

55-1520-237-50-15MWO:

Mnt LevelPriority

DR15-Jul-1985


1223-Jun-1986


MODIFICATION OF DIRECTIONALCONTROL CABLE SYSTEM (UH-60A &EH-60A HELICOPTERS) NATIONALSTOCK NUMBER (NSN) 1520-01-035-0266 & 1520-01-082-0686

55-1520-237-50-34MWO:

Mnt LevelPriority

DM15-Jun-1991

LSSI/OLR (NOPID)

023-Mar-1993


INCOROPORATION OF EXHAUSTEXTENDER DOUBLERS

1-1520-237-50-51MWO:

Mnt LevelPriority

DN01-Jun-1988

LSSI/OLR (NOPID)

023-Mar-1993


CRASHWORTHY ARMORED CREWSEATS/IMPROVED SEATINGRESTRAINT SYSTEM

55-1680-237-50-01MWO:

Mnt LevelPriority

DM01-Sep-1991

LOCKHEED (NOPID)

323-Mar-1993


IMPROVED ENGINE COWLINGRELEASE HANDLE ASSEMBLY

1-1520-237-50-64MWO:

Mnt LevelPriority

OR24-Jul-2000

AASF #2 SALINA,KS. 67401(XD8508)

1324-May-2000


ALL H-60 SERIES AIRCRAFT, TAILNUMBERS 77-22715 THROUGH 90-26367, INSPECTION OF FIREEXTINGUISHER WIRING

1-1520-237-20-219MWO:

Mnt LevelPriority

DN26-Mar-1984


20025-Jan-1985


MODIFICATION TO INSTALL ROTORBLADE DE-ICE KIT (UH-60AHELICOPTERS)

55-1520-237-50-5MWO:

Mnt LevelPriority

DN01-Oct-1982


2825-Jan-1985


INCORPORATION OF A ENGINEPRIME/BOOST SYSTEM (UH-60AHELICOPTERS)

55-1520-237-50-7MWO:

Mnt LevelPriority

DN26-Mar-1984


625-Jan-1985


INCORPORATION OF IMPROVEDDROOP STOP CAM ASSEMBLIES (UH-60A HELICOPTERS)

55-1520-237-50-16MWO:

Mnt LevelPriority



PIDMWODATE HRS






DM01-Apr-1985


15225-Jan-1985


INCORPORATION OF FUEL BOOSTPUMP SYSTEM

55-1520-237-50-25MWO:

Mnt LevelPriority

DN26-Mar-1984


1225-Jan-1985


BLADE DE-ICE CHECKOUT APU (UH-60A HELICOPTERS)

55-1520-237-50-4MWO:

Mnt LevelPriority

DN15-Dec-1984


225-Jan-1985


MODIFICATION OF MAIN ROTORSLIDING COVER (UH-60AHELICOPTERS)

55-1520-237-50-32MWO:

Mnt LevelPriority

DN26-Mar-1984


425-Jan-1985


IMPROVED ANTI-ICING MODULATINGVALVE SENSE LINE INSTALLATION(UH-60A HELICOPTERS)

55-1520-237-50-3MWO:

Mnt LevelPriority

DN24-Mar-1988


226-Mar-1988


MODIFICATION OF WIRE STRIKEPROTECTION SYSTEM (WSPS) (UH/EH-60A HELICOPTER)

55-1520-237-50-47MWO:

Mnt LevelPriority

DU10-Aug-1987


627-Jan-1988


INCORPORATION OF STABILATORSLEW-UP SWITCH (UH-60AHELICOPTER)

55-1520-237-50-46MWO:

Mnt LevelPriority

DN01-Sep-1986


105427-Jan-1988


INCORPORATION OF ANVISCOMPATIBLE LIGHTING SYSTEM

55-1520-237-50-20MWO:

Mnt LevelPriority

OM24-Sep-2002

AASF #2 SALINA,KS. (XD8508)

127-Sep-2002


UH-60 SERIES AIRCRAFT, REVISIONTO UH-60-02-ASAM-08 (TB 1-1520-237-20-256) INSPECT AN/ARC-220 WIRINGFOR CHAFING

UH-60-02-ASAM-11MWO:

Mnt LevelPriority

DR08-Nov-1996

DYNCOP OLR FTHOOD TX(JC1523)

17829-Aug-2000


INSTALLATION OF AN/ASN-128BDOPPLER/GPS NAVIGATION SYSTEMIN UH-60A/L HELICOPTER

1-1520-237-50-75MWO:

Mnt LevelPriority

DN30-Apr-1997

DYNCOP OLR FTHOOD TX(JC1523)

5229-Aug-2000


INSTALLATION OF THE AVIATOR'SNIGHT VISION IMAGING SYSTEM(ANVIS) LIGHTING UPDATE EH/UH-60A/L

1-1520-237-50-56MWO:

Mnt LevelPriority



PIDMWODATE HRS






OM02-Jun-1986

LSSI/HAAF (NOPID)

030-Apr-1986


REPLACEMENT OF STABILATORACTUATORS, P/N 70400-06641-115

55-1520-237-20-77MWO:

Mnt LevelPriority

OE30-Apr-1986

B CO 158TH AVNBN (NO PID)

1530-Apr-1986


RELOCATION OF THE AUTOMATICFLIGHT CONTROL SYSTEM (AFCS)PANEL

55-1520-237-20-1MWO:

Mnt LevelPriority

DN16-Oct-1989

LSSI/OLR (NOPID)

1930-Nov-1990


MODIFICATION OF FLIGHT CONTROLMIXER ASSEMBLY (UH-60A/EH-60AHELICOPTERS)

55-1520-237-50-49MWO:

Mnt LevelPriority

DN01-Oct-1990

LSSI/OLR (NOPID)

630-Nov-1990


INCORPORATION OF ENGINEQUADRANT SECONDARY STOP TONO. 1 AND NO. 2 ENGINE POWERCONTROL LEVERS (UH-60AHELICOPTERS)

55-1520-237-50-39MWO:

Mnt LevelPriority

DM15-Nov-1989

LSSI/OLR (NOPID)

1730-Nov-1990


MODIFICATION OF DOWEL PINRETENTION MAIN GEARBOX

1-1520-237-50-43MWO:

Mnt LevelPriority

DN01-Mar-1989

LSSI/OLR (NOPID)

330-Nov-1990


INCORPORATION OF IMPROVEDTIEDOWN FITTINGS

1-1520-237-50-53MWO:

Mnt LevelPriority

DN01-Oct-1991

LSSI/OLR (NOPID)

230-Nov-1990


INCORPORATION OF STABILATORACTUATOR GROUNDING STRAP FORUH-60A/EH-60A HELICOPTERS

1-1520-237-50-54MWO:

Mnt LevelPriority

DU31-May-1995

PROJ. OLR,LMLM (NO PID)

2431-Aug-1995


MODIFICATION OF THE ENGINE TRIMBALANCE HARDWARE (EH/UH-60AAND UH-60L HELICOPTERS)

1-1520-237-50-73MWO:

Mnt LevelPriority




7923273HELICOPTER, UTILITY UH-60A

7. FREQUENCY 4.

5. ITEMS TO BE INSPECTED

2. MODEL 3. SERIAL NUMBER 1. NOMENCLATURE

8. NEXTNO DUE 6. REFERENCE 9. COMPLETED AT

INSP

A001 11 Dec 20157H-60-09-ASAM-11CARGO DOOR WINDOWJETTISON LEVER

04 Dec 2015D

A020 5625.210TM 1-1520-237-PMDPERFORM M/R SPINDLE LUGS,M/R CUFF, TIP CAPSINSPECTION

5615.2H

A022 17 Dec 201514TM 1-1520-237-23-914 DAY FLYABLE STORAGEENGINE RUN UP

03 Dec 2015D

A092 05 Jan 201630TM 11-6140-203-23&P30 DAY SLAB BATTERYINSPECTION (D8565/11-1)

06 Dec 2015D

A100 14 Dec 201530DA PAM 738-751#1 ENGINE HISTORY RECORDERREADING DUE

14 Nov 2015D

A101 14 Dec 201530DA PAM 738-751#2 ENGINE HISTORY RECORDERREADING DUE

14 Nov 2015D

A103 26 Dec 201530TM 1-1500-344-23AIRCRAFT WASH DUE 26 Nov 2015D

A110 5641.140TM 1-1520-237-PMSPMS 40 HOUR INSPECTION 5601.1H

A115 26 Dec 201530TM 1-1520-237-23-12LUBE REQUIRMENTS 26 Nov 2015D

A115 5648.540TM 1-1520-237-23-12LUBE REQUIRMENTS 5608.5H

A116 5961.1360H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

5601.1H

A116 04 Nov 201612H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

04 Nov 2015M

A117 5961.1360H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 5601.1H

A117 04 Nov 201612H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 04 Nov 2015M

A140 5724.6120AWR 1346R16, IVHMSIN ACF

DOWNLOAD AND REVIEW IVHMSDATA

5604.6H

A160 25 Jan 201690TM 1-1520-237-23-1290 DAY CORROSIONINSPECTION

27 Oct 2015D

A177 02 Feb 201690AR 95-190 DAY REVIEW/UPDATE OF 365-4 ENTRIES

04 Nov 2015D

A210 5721.1120TM 1-1520-237-23-12120 HOUR INSPECTIONREQUIREMENTS

5601.1H

A211 5961.1360H-60-10-AMAM-11APU OIL SAMPLE 5601.1H

A211 04 Nov 201612H-60-10-AMAM-11APU OIL SAMPLE 04 Nov 2015M

A213 5724.6120TM 1-2840-248-23ENGINE COMPRESSORCLEANING

5604.6H

A214 5721.1120TM 1-1520-237-23-12CLEAN TAIL WHEEL ADAPTER 5601.1H

A220 26 Oct 201612AR 95-1/TM 55-1680-317-23

AIRCRAFT SURVIVAL KITINSPECTION

26 Oct 2015M

For use of this form, see DA PAM 738-751; the proponent agency is DCSLOGDA FORM 2408-18, NOV 91, MAY BE USED

DA FORM 2408-18 E, OCT 97 EQUIPMENT INSPECTION LIST

A = APU OPERATING HOURS P = APU STARTS F = HOT SECTION FACTORSFREQUENCY LEGEND: H = ACFT HRS D = DAYS M = MONTHS Y = YEARS R = ROUNDS C = CYCLES S = ENG1 STARTS Z = ENG2 STARTS



7. FREQUENCY 4.




INSP

A230 05 Mar 2016120MWO 1-1520-237-50-77INSPECT BATTERYCOMPARTMENT FORCORROSION (SLAB)

06 Nov 2015D

A295 5961.1360TM 1-1520-237-23-12STABILATOR ACTUATOR ASSYLUBE

5601.1H

A296 5961.1360TM 1-1520-237-23-12STABILATOR INSPECTION 5601.1H

A298 5923360TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 5563H

A298 07 Apr 201612TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 07 Apr 2015M

A299 5961.1360TM 1-1520-237-23-12SWASHPLATE LUBE 5601.1H

A299 27 Oct 201612TM 1-1520-237-23-12SWASHPLATE LUBE 27 Oct 2015M

A320 5961.1360TM 1-2840-248-23ENGINE INSPECTION &CLEANING

5601.1H

A400 6321.1720TM 1-1520-237-PMIPMI-1 5601.1H

A401 5966.7720TM 1-1520-237-PMIPMI-2 5246.7H

A408 5967.1720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-2, AREA 5 AND 6)

5247.1H

A410 6321.1720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-1, AREA 1 THRU 4)

5601.1H

A415 6321.1720H-60-10-AMAM-11MAIN GEARBOX OIL SAMPLE-PART # 073, 074, 076

5601.1H

A440 5967.1720TM 1-1520-237-23-12CLEAN TAIL WHEEL LOCKPIN 5247.1H

A470 5791.61500TM 1-1520-237-23-12REPLACE NUMBER TWOCROSSFEED VALVE

4291.6H

A471 6754.92160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (FWD)

4594.9H

A472 6848.82160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)

4688.8H

A473 6754.92160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (AFT)

4594.9H

A476 9594.95000TM 1-1520-237-23-12REPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS

4594.9H

A477 9594.95000TM 1-1520-237-23-12REPLACEMENT OF STABILATORACTUATOR BOLTS

4594.9H

A480 9594.95000TM 1-1520-237-23-12REPLACE PIVOT BOLT 70400-08159-101,102,103,104

4594.9H

A485 9594.95000TM 1-1520-237-23-12REPLACE BELLCRANK BOLT70400-08159-105,106,107,108

4594.9H

A496 22 Apr 20166TM 1-1500-204-23-1CF3BR FIRE EXTINGUISHERWEIGHT TEST & INSPECTION

22 Oct 2015M

A501 27 Apr 20166TM 1-1520-237-23-12MAIN ROTOR BLADE PRESSURECHECK

27 Oct 2015M






7. FREQUENCY 4.




INSP

A502 06 May 20166TM 1-1520-237-23-12INSPECT AND TEST GROUNDRECEPTACLE IAW TM 1-1500-204-23

06 Nov 2015M

A530 06 Nov 201612DA PAM 738-751AIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)

06 Nov 2015M

A532 09 Nov 201612TM 1-1500-204-23-4COMPASS SWING / RMI 09 Nov 2015M

A533 04 Nov 201612TM 1-1520-237-23-12PITOT STATIC SYSTEMINSPECTION

04 Nov 2015M

A534 26 Oct 201724TM 1-1500-204-23-1FIRST AID KIT INSPECTION 26 Oct 2015M

A538 29 Oct 201612TM 1-1520-237-23-12FAT/OAT GAUGEINSPECTION/TEST

29 Oct 2015M

A541 05 Nov 201612TM 1-1520-237-23, C4REPLACE DIGITAL CLOCKBATTERY

05 Nov 2015M

A550 05 Nov 201612AWR1346R16IVHUMS BATTERYREPLACEMENT

05 Nov 2015M

A553 04 Nov 201612AR 95-1AIRCRAFT WEIGHINGINVENTORY (365-1)

04 Nov 2015M

A580 13 Nov 201624TM 11-6140-203-23&PRETURN SLAB TO AVIM FORCAPACITY CHECK (VEREY 24MONTH)

13 Nov 2014M

A621 04 Nov 201724AR 95-1AIRCRAFT WEIGHING CLASS 2 04 Nov 2015M

A625 01 Dec 201560TM 11-6140-203-23&PREPLACEMENT OF SLABBATTERY (SLAB)

01 Dec 2010M

A630 01 Feb 2023114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 Aug 2013M

A633 01 May 2020114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 Nov 2010M

A638 01 May 2020114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #2,CARTRIDGE, DODIC MH92

01 Nov 2010M

A640 01 Feb 2023114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #2,CARTRIDGE, DODIC MH92

01 Aug 2013M

A648 31 Jul 2023180TM 1-1520-237-23REPLACE T/R SPRING CAPSULEASSY

31 Jul 2008M

A660 01 Dec 201672TB 9-1300-385REPLACE THRUSTEREMERGENCY RELEASE CARGOHOOK, MJ20

01 Dec 2010M

A665 15 Jul 201748H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215

15 Jul 2013M

A670 15 Jul 201748TM 1-1520-237-23-1CABIN TUB INSPECTION 15 Jul 2013M

A673 15 Jul 201748TM 1-1520-237-23-12FUEL CELL CORROSIONINSPECTION

15 Jul 2013M

A675 15 Jul 201748TM 1-1520-237-23-12FLIGHT CONTROL ROD INSP 15 Jul 2013M

A695 5966.7720H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

5246.7H






7. FREQUENCY 4.




INSP

A695 25 Jul 201748H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

25 Jul 2013M

A755 90009000H-60-10-ASAM-11PC LINK TO SWASHPLATEBOLTS REPLACEMENT

0H

E015 04 May 20166MWO 1-1520-237-50-92ASN 128D DOPPLER GPSBATTERY REPLACEMENT

04 Nov 2015M

E040 03 Feb 201690TM 11-5841-294-12APR-39 RADAR/LASERWARNING OPNL CHECK, 5841-01-236-8951

05 Nov 2015D

E108 31 Dec 201530TM 11-5810-262-23KY-58 PMCS/OPNL CHECK(STANDBY)

01 Dec 2015D

E135 04 May 20166TM 11-5821-333-12AN/ARC-201(V) SINCGARSRADIO HUB BATT REPL

04 Nov 2015M

E155 02 May 2016180TM 11-5810-262-23KY-58 BATTERY REPLACEMENT 04 Nov 2015D

E300 31 Dec 201530AWR 1516R3 FOR ELTEMERGENCY LOCATORTRANSMITTER SELF TEST (EBC-406HM)

01 Dec 2015D

E300 5730.8120AWR 1516R3 FOR ELTEMERGENCY LOCATORTRANSMITTER SELF TEST (EBC-406HM)

5610.8H

E320 29 Oct 2016360AWR 1516 FOR ELTEMERGENCY LOCATORTRANSMITTER G-SWITCH (EBC-406HM)

04 Nov 2015D

E325 01 May 201760AWR 1516R2 FOR ELTREPLACEMENT OF ELTBATTERY PN GS-46

01 May 2012M

E330 19 Oct 20166AWR1346R16UNDER WATER ACOUSTICBEACON BATTERYREPLACEMENT

19 Oct 2010Y

E652 05 Nov 201612PD2006-034MTSUBJECT 008-00 PG7

BATTERY REPLACEMENT FORIVHMS HISTORY RECORDER

05 Nov 2015M





ECD00366

79232736035T00G01ENGINE ASSY, TURBINEGEE306518

2245

4485

7066

30710

3677

8949

1163

2289

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE





T700-GE-700




OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


17-Jan-2016 2/12

04A 6035T00G01 ENGINE ASSY, TURBINE GEE306518

25472263558021308

38321678996841568GEC0065316035T02G01COLD SECTIONMODULE

COND

COND

34192933976491885

2410000GGMH19226039T58G02COMBUSTION LINER

COND

COND

32622827172871756

338324877121401113MRSG59616055T20G05MTCHDROTOR/STATOR ASSY

COND

COND

25472933976491885

2277000AMDA36155043T24G14STAGE 1 NOZZLEASSY

COND

COND

44823060989372283

24261198250801885GEL8074776064T98G01POWER TURBINEMODULE

COND

COND

02933976491885

0000GED0065186035T01G01ACCESSORY MODULE

COND

COND

02933976491885

0000SUSJ27696034T62P13PARTICLESEPARATOR BLOWER

COND

COND

44852933976491885

3081000UDAJ56655074T79G07FUEL CONTROL

COND

COND

20392933976491885

0000APM882RT4076T64G01POU ASSY-O/S DRAINVALVE

COND

COND

44852933976491885

5033000ECD008584046T29G13ELECTRICALCONTROL UNIT

COND

COND

35082933976491885

126856952377759ECD003664046T26G03HISTORY RECORDER

COND

COND


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


17-Jan-2016 3/12


02933976491885

0000UDC018014046T25G01COOLER, OIL

COND

COND

23302933976491885

0000M54795066T38G04ANTI-ICE VALVE

COND

COND


5/28/201512:00:00 AM

1 28MAY2015-ENGINE INSPECTED, SERVICED, AND TESTED ON FEDS SER#003 TSN: 4485. SW88461, MO-TASMG,SPRINGFIELD, MO

ZM250409 TASMG MO



ECD00366

GEE3065186035T02G01COLD SECTION MODULEGEC006531

1268

4793

5695

23493

2377

11531

759

2145

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


17-Jan-2016 5/12

04A01 6035T02G01 COLD SECTION MODULE GEC006531

38301667896761566

41551278563923196AGRA34215056T66G02POWER TAKEOFFDRIVE

COND

COND

38301667896761566

38301667896761566GLB204796035T77G14COMPRESSORROTOR ASSEMBLY

COND

COND

38301667896761566

38301667896761566GATBC6946035T88P04GAS GENERATORTURBINE SHAFT

7475

11000

38301667896761566

0000BJWD92585036T95P01INNER BALANCEPISTON SE

COND

COND

38301667896761566

0000BER7464M6035T79P02COMPRESSORDISCHARGE SEAL

COND

COND

38301667896761566

0000FIAALTG46035T83P01COMPRESSOR REARSHAFT

5305

5000

38301667896761566

38301667896761566GATAS2885044T07P01NO 3 LABYRINTHSEAL

COND

COND

38301667896761566

38301667896761566BIWAM9225035T57P02VORTEX SPOILER

COND

COND

38301667896761566

116449371387458GATCKV135043T04P02TIE ROD,COMPRESSOR

9141

10000

38301667896761566

2900130072042201GATHW0104045T08P01RING, SPACERCOMPRESSOR

7405

10000

38301667896761566

0000GLHTFJRN6055T59P01COMPRESSORIMPELLER

5305

5000


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


17-Jan-2016 6/12


576524719128132540

0000GGTE03533065T21G01OUTPUT SHAFT ASSY

COND

COND

38301667896761556

0000GLHTFLWC6032T26G09STAGE 1 BLISK

5305

5000

38301667896761556

0000GLHTFD616032T27P08STAGE 2 BLISK

7305

7000

38301667896761556

0000GLHTFJN96038T08P04STAGE 3 & 4 BLISK

7305

7000

38301667896761556

0000GLHTFHL56038T09P04STAGE 5 BLISK

7305

7000

38301667896761556

0000BARB29696043T45P01NO 3 BALL BEARING

COND

COND

38301667896761556

279154619122387676106064T15P01NO 4 ROLLERBEARING

COND

COND




ECD00366

GEC0065313065T21G01OUTPUT SHAFT ASSYGGTE0353

2240

0

6921

0

3659

0

1154

0

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


17-Jan-2016 8/12

04A01G 3065T21G01 OUTPUT SHAFT ASSY GGTE0353

0000

0000FCADB5316064T34P02NO 1 BALL BEARING

COND

COND

0000

0000FCADC7105121T46P02NO 2 ROLLERBEARING

COND

COND




ECD00366

GEE3065186055T20G05MTCHD ROTOR/STATORASSY

MRSG5961

1268

3629

5695

25945

2377

12502

759

1242

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


17-Jan-2016 10/12

04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRSG5961

338324877121401113

0000GATHGA8R6064T85P01STAGE 1 TURBINEDISK

6022

5000

338324877121401113

338324877121401113GGAC45796039T57G24G/G STATOR ASSY

COND

COND

338324877121401113

0000GATHG3MN6064T86P01STAGE 2 TURBINEDISK

6022

5000

338324877121401113

45320981098315GFFR85NJ6064T81P01STAGE 1 FWDCOOLING PLATE

5569

5000

338324877121401113

0000PAMEV2606064T82P01STAGE 1 REARCOOLING PLATE

6022

5000

338324877121401113

0000PAMEN9396064T83P01STG 2 FWD COOLINGPLATE

6022

5000

338324877121401113

0000GFF5CGFH6064T84P02STAGE 2 REARCOOLING PLATE

6022

5000

338324877121401113

338324877121401113GGAG59616039T54G13G/G ROTORASSEMBLY

COND

COND




ECD00366

GEE3065186064T98G01POWER TURBINE MODULEGEL807477

2242

2426

6965

11982

3665

5080

1157

1885

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


17-Jan-2016 12/12

04A03 6064T98G01 POWER TURBINE MODULE GEL807477

24241189850751883

24241189810751883GGAP44985043T75G07POWER TURBINEROTOR

COND

COND

1857571428571428

1857571428571428GAT6439P6038T32P01STAGE 3 TURBINEDISK

4816

5000

1857571428571428

1857571428571428GAT8673P6038T34P05STAGE 4 TURBINEDISK

4816

5000

24241189850751883

3054952952941553GATM71785125T92G01REPOWER TURBINESHAFT

4186

5000

24241189850751883

45231925084763114MABK41185034T27P01NO 5 ROLLERBEARING

COND

COND

24241189850751883

3728403236271345BARA98815034T04P01NO 6 BALL BEARING

COND

COND


6/16/200712:00:00 AM

1 16JUNE07 CCAD POWER TURBINE REPAIRED 10JUN07 IAW DMWR 1-2840-248-& CHANGES AND RECAPPED AED P3430B DTD 03DEC01./S/ R.HERRERA. AIRCRAFT DATA TECHNICIAN.

ZM250409 CCAD CORPUS CHRISTI TX



CAO00522

79232736035T00G01ENGINE ASSY, TURBINEGEE307361

3074

2544

12823

12762

6409

6237

1676

1597

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE





T700-GE-700




OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


17-Jan-2016 2/12


25421273152331594

37612283686032153GEC0076346035T02G01COLD SECTIONMODULE

COND

COND

22951146748781473

2416000GGMP86076039T58G02COMBUSTION LINER

COND

COND

22951146748781473

1879626848441469MRS070226055T20G03MTCHDROTOR/STATOR ASSY

COND

COND

22951146748781473

1600000AMDA07925043T24G14STAGE 1 NOZZLEASSY

COND

COND

35421273152331594

25401267252281590GEL0373616064T98G01POWER TURBINEMODULE

COND

COND

22951146748781473

2689000GED0062026035T01G01ACCESSORY MODULE

COND

COND

22951146748781473

3000000SUSJ37616034T62P13PARTICLESEPARATOR BLOWER

COND

COND

22951146748781473

2117000UDA860775074T79G07FUEL CONTROL

COND

COND

22951146748781473

994000APM529RU4076T64G01POU ASSY-O/S DRAINVALVE

COND

COND

22951146748781473

366000EMDE06374046T29G13ELECTRICALCONTROL UNIT

COND

COND

22951146748781473

28251152860501552CAO005224046T26G03HISTORY RECORDER

COND

COND


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


17-Jan-2016 3/12


22951146748781473

3148000UDC017634046T25G01COOLER, OIL

COND

COND

23421146748781473

0000COMH69554046T28G14ANTI-ICE VALVE

COND

COND


4/1/200912:00:00 AM

1 WO#900085 ENGINE MINOR REPAIRED FOR OIL LEAKS. REPLACED PTMODULE, G AXIS SEAL AND COLD SECTION MODULE. COMPLIED WITHUH60-08 ASAM 14. ENGINE TESTED ON ENGINE TEST STAND S/M 003 ANDACCEPTED AS SERVICABLE ENGINE. TSN 2544 INSP JW49152

JW749152 MOAVCRAD MOAVCRAD

7/20/201512:00:00 AM

1 25FEB08 ENGINE AND SUBCOMPONENT HOURS CORRECTED AS PER 2410HOTLINE AND WEBSITE (RALPH) TS689275 AASF2 IAARNG

DN337516 DET 2 CO. D 1/15OTHAVN

WHEELING, WV

7/20/201512:00:00 AM

2 30 AUG05 CCAD-ENGINE REPAIRED 27AUG05 IAW DMWR 1-2840-248&CHANGES AND RECAP AED-P3430B DTD 03DEC01, /S/ C. PLATZ,RECORDS CLERK.

DN337516 DET 2 CO. D 1/150THAVN

WHEELING, WV



CAO00522

GEE3073616035T02G01COLD SECTION MODULEGEC007634

3072

3761

12792

22836

6405

8603

1673

2153

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


17-Jan-2016 5/12


37602275085972151

509816786111282294SAP694495044T27G02POWER TAKEOFFDRIVE

COND

COND

37602275085972151

424118126106662376GLB003766035T77G10COMPRESSORROTOR ASSEMBLY

COND

COND

37602275085972151

2977669463892110GATFA2856035T88P04GAS GENERATORTURBINE SHAFT

11094

11000

37602275085972151

0000WESP75745036T95P01INNER BALANCEPISTON SE

COND

COND

37602275085972151

0000BIW03A446035T79P04COMPRESSORDISCHARGE SEAL

COND

COND

37602275085972151

3257931082602115GATM65696035T83P01COMPRESSOR REARSHAFT

4814

5000

37602275085972151

0000VAEAU4035044T07P01NO 3 LABYRINTHSEAL

COND

COND

37602275085972151

29321303550851756BIWCH7565035T57P02VORTEX SPOILER

COND

COND

37602275085972151

21161662149551338GATPR1505043T04P02TIE ROD,COMPRESSOR

10955

10000

37602275085972151

416815602168173514GATF96654045T08P01RING, SPACERCOMPRESSOR

8903

10000

37602275085972151

0000GLHTL0W86055T59P01COMPRESSORIMPELLER

8071

5000


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


17-Jan-2016 6/12


37602275085972151

3822900677152136GGA002996039T56G04OUTPUT SHAFT ASSY

COND

COND

37602275085972151

0000GLHTLE266032T26G09STAGE 1 BLISK

8071

5000

37602275085972151

0000GLHTLE5N6032T27P08STAGE 2 BLISK

10071

7000

37602275085972151

0000GLHTLC776038T08P04STAGE 3 & 4 BLISK

10071

7000

37602275085972151

0000GLHTKAH16038T09P04STAGE 5 BLISK

10071

7000

37602275085972151

0000TMKAEAAD6064T35P01NO 3 BALL BEARING

COND

COND

37602275085972151

12328514897FCAK08206064T15P01NO 4 ROLLERBEARING

COND

COND


7/20/201512:00:00 AM

1 20FEB09 CCAD C/S MOD REPAIRED IAW DMWR 1-3840-248 & CHANGESAND RECAPPED DTD 03DEC01. FUEL INJECTORS CLEANED AND FLOWEDPER DMWR AT C/S TSN 3760 ON 19FEB09 /S/ R.HERRERA, AIRCRAFT DATATECHNCICIAN.

DN337516 DET 2 CO.D 1/150THAVN

WHEELING, WV



CAO00522

GEC0076346039T56G04OUTPUT SHAFT ASSYGGA00299

3072

3823

12792

9092

6405

7721

1673

2138

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


17-Jan-2016 8/12

04A01G 6039T56G04 OUTPUT SHAFT ASSY GGA00299

3822900677152136

29791350354101253BARA50265034T07P03NO 1 BALL BEARING

COND

COND

3822900677152136

0000TMKAEDF55035T69P01NO 2 ROLLERBEARING

COND

COND


7/20/201512:00:00 AM

1 20FEB09 CCAD OUTPUT SHAFT REPAIRED 19FEB09 IAW DMWR 1-2840-248& CHANGES AND RECAPPED DTD 03DEC01 /S/ R. HERRERA, AIRCRAFTDATA TECHNICIAN.

DN337516 DET 2 CO. D 1/150THAVN

WHEELING, WV



CAO00522

GEE3073616055T20G03MTCHD ROTOR/STATORASSY

MRS07022

2825

1879

11528

6268

6050

4844

1552

1469

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


17-Jan-2016 10/12

04A02B 6055T20G03 MTCHD ROTOR/STATOR ASSY MRS07022

1879626848441469

17071579729851075GAT9408W6064T85P01STAGE 1 TURBINEDISK

6118

5000

1879626848441469

1879626848441469GGA00137A6039T57G13G/G STATOR ASSY

COND

COND

1879626848441469

46324081036325GATH8E586064T86P01STAGE 2 TURBINEDISK

7362

5000

1879626848441469

0000GFF5CL986064T81P01STAGE 1 FWDCOOLING PLATE

7825

5000

1879626848441469

0000GFF5CM9M6064T82P01STAGE 1 REARCOOLING PLATE

7825

5000

1879626848441469

0000GFF5CD436064T83P01STG 2 FWD COOLINGPLATE

7825

5000

1879626848441469

0000GFF5CLD16064T84P02STAGE 2 REARCOOLING PLATE

7825

5000

1879626848441469

1879626848441469GGA070226039T54G13G/G ROTORASSEMBLY

COND

COND




CAO00522

GEE3073616064T98G01POWER TURBINE MODULEGEL037361

4072

2540

12792

12672

6405

5228

1673

1590

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


17-Jan-2016 12/12

04A03 6064T98G01 POWER TURBINE MODULE GEL037361

22951146748781473

22951146748781473GGA113255043T75G07POWER TURBINEROTOR

COND

COND

22951146748781473

22951146748781473GATLL1876038T32P01STAGE 3 TURBINEDISK

6532

5000

22951146748781473

22951146748781473GATLF6346038T34P05STAGE 4 TURBINEDISK

6532

5000

22951146748781473

658153722672228GATH934T5125T92G01POWER TURBINESHAFT

8169

5000

22951146748781473

732406812297MABR56285034T27P01NO 5 ROLLERBEARING

COND

COND

22951146748781473

100341331457639BARB27735034T04P01NO 6 BALL BEARING

COND

COND



ZM250409

PIDMWODATE HRS



ENGINE ASSY, TURBINE 7923273GEE3065181. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


30-Jun-1994 OR

ZM25040922-Jul-2015

1CO D 1/150 AVNONE TIME INSPECTION ANDCONVERSION OF FORMS ANDRECORDS FOR T700-GE-700, -701AND -701C SERIES GAS TURBINEENGINES

1-2840-248-20-2MWO:

Priority Mnt Level

29-Nov-2006 OM

ZM25040922-Jul-2015

1CO D 1/150 AVNALL H-60 SERIES AIRCRAFT,REROUTING OF WHITEENGINE/AIRFRAME HARNESSASSEMBLY


Priority Mnt Level

19-Dec-2006 OM

ZM25040922-Jul-2015

1CO D 1/150 AVNREROUTING OF WHITEENGINE/AIRFRAME HARNESS ASSY

UH060-07-ASAM-02MWO:

Priority Mnt Level

16-Jul-2007 OM

ZM25040922-Jul-2015

1CO D 1/150 AVNALL H-60 SERIES AIRCRAFT,HAMILTON-SUNDSTRAND HYDRO-MECHANICAL UNITS PN 4046T52G01AND 4046T52G04 REMOVE FROMSERVICE


Priority Mnt Level

13-Aug-2007 OM

ZM25040922-Jul-2015

1D CO 1/150 AVNALL H-60 SERIES AIRCRAFT, MAINFUEL MANIFOLD CHAFING


Priority Mnt Level

20-Dec-2007 OM

ZM25040922-Jul-2015

1CO D 1/150 AVNINSPECTION TO DETERMINE IFENGINE HAS BEEN SERVICED WITHMIL-PRF-23699 HTS OIL

UH-60-08-AMAM-03MWO:

Priority Mnt Level

28-Feb-2008 OT

ZM25040922-Jul-2015

1DET 2 CO D1/150TH AVN

T700 SERIES ENGINE EXTERNALWASH PROCEDURES (H-60-08-ASAM-07) ADD NEW PROCEDURES TOTHE PMI SEQUENCE 6.37 AND 6.43(DRAIN ENGINEOIL TANK ANDREFILL)

(ASAM) H-60-08-ASAM-07MWO:

Priority Mnt Level

22-Sep-2008 OM

ZM25040922-Jul-2015

1CO D 1/150 AVNALL H-60 AND H-64 SERIESAIRCRAFT, SUSPECT ENGINEHARNESSES

H-60-08-ASAM-14MWO:

Priority Mnt Level

12-Jan-2009 FM

ZM25040922-Jul-2015

1CO D 1/150 AVNALL H-60A/K/L AND AH-64 SERIESAIRCRAFT, T701C GAS GENERATORROTOR ASSEMBLIES, FOR SN'SINSTALLED.


Priority Mnt Level



PIDMWODATE HRS





01-Oct-2009 FM

ZM25040922-Jul-2015

1CO D 1/150 AVNREMOVE SUSPSECT HAMILTONSUNDSTRAND HMUS FROMSERVICE

H-60-10-ASAM-01MWO:

Priority Mnt Level

24-Jun-2011 OR

ZM25040922-Jul-2015

1CO D 1/150 AVNINSP ANTI-ICEING START/BLEEDVALVEACTUATING SHAFT

H-60-11-ASAM-11MWO:

Priority Mnt Level

05-Sep-2012 FU

ZM25040922-Jul-2015

1CO D 1/150 AVNENGINE ANTI-ICE / START BLEEDVALVE (AISBV) PART NUMBER.

H-60-12-ASAM-10MWO:

Priority Mnt Level



PIDMWODATE HRS





31-Jul-1989 OM

DN33751620-Jul-2015

1DET 2 CO. D1/150TH AVN

MODIFICATION OF GG ROTORASSEMBLY T700/701 REWORK T700ENGINES

55-2840-248-50-32MWO:

Priority Mnt Level

15-Aug-1990 OM

DN33751620-Jul-2015


INSTALLATION OF SELF SEALADAPTER ASSEMBLY

55-2840-248-50-28MWO:

Priority Mnt Level

25-Jan-1991 DN

DN33751620-Jul-2015


MODIFICATION OF POWER TAKEOFFDRIVE ASSEMBLY P/N 5044T27G01

55-2840-248-50-27MWO:

Priority Mnt Level

31-Mar-1993 DR

DN33751620-Jul-2015


INSTALLATION OF PTO DRIVEASSEMBLY P/NS 5044T27G02 OR5056T66G02 (T700-GE-700 AND 701ENGINES)

1-2840-248-50-29MWO:

Priority Mnt Level

30-Jun-1994 OR

DN33751620-Jul-2015


ONE TIME INSPECTION ANDCONVERSION OF FORMS ANDRECORDS FOR T700-GE-700, -701AND -701C SERIES GAS TURBINEENGINES

1-2840-248-20-2MWO:

Priority Mnt Level

05-Nov-1998 OM

DN33751620-Jul-2015


ALL UH-60A AND EH-60A SERIESHELICOPTERS, ONE TIMEINSPECTION OF ALL T700-GE-700ENGINE RECORDS


Priority Mnt Level

02-Aug-1999 FM

DN33751620-Jul-2015


ALL AH-64 AND UH-60 SERIESAIRCRAFT - ONE TIME INSPECTIONOF T700-GE-700/701/701C ENGINES

1-2840-248-20-23MWO:

Priority Mnt Level

20-Dec-2007 OM

DN33751620-Jul-2015


INSPECTION TO DETERMINE IFENGINE HAS BEEN SERVICED WITHMIL-PRF-23699 HTS OIL

H-60-08-AMAM-03MWO:

Priority Mnt Level

22-Sep-2008 OM

DN33751620-Jul-2015


ALL H-60 AND H-64 SERIESAIRCRAFT, SUSPECT ENGINEHARNESSES

H-60-08-ASAM-14MWO:

Priority Mnt Level



T/T I HIST RCDR SNSERIAL NO. OP HRSLCF-2LCF-1POSHOURSAIRCRAFT AIRCRAFT ENGINE SERIAL NO. 13.12.11. 14.10.9.8.7.6.

(256)123-3456HUNTSVILLEK08DD23. UIC 5. TELEPHONE NUMBER4. LOCATION

16046 SESI

2. Organization

CSGLD-1052

REQUIREMENT CONTROL SYMBOL(Julian)1. PERIOD ENDING DATE


1GEE306518 ECD00366226870773682116756207923273

2GEE307361 CAO005223096128386412167856207923273


ENGINE COMPONENT OPERATING HOURS RECORDDA FORM 2408-19-3 E, DEC 1991

Eddie.Denney

Highlight

Eddie.Denney

Highlight

PIDMWODATE HRS



FORWARD BELLCRANK SUPPORT 7923273B367033441. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


14-Jul-2010 OT

DM64902827-Jul-2010


H-60-10-ASAM-11MWO:

Priority Mnt Level



PIDMWODATE HRS



FUEL CONTROL 7923273UDAJ56651. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


19-Aug-2013 FM

DN33751629-Aug-2013

1AASF2,WVARNG

WOODWARD HYDR-MECHANICALUNIT (HMU) P3 TUBE

H-60-13-ASAM-10MWO:

Priority Mnt Level



PIDMWODATE HRS



HUB, M/R ROTOR ASSY 7923273C308002971. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


30-Dec-2013 FM

DN33751620-May-2014

10AASF2,WVARNG

MAIN ROTOR HUB ASSEMBLYH-60-14-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



INPUT MODULE 7923273A264017711. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


02-Aug-2000 OT

QC00000003-Aug-2000

1AASF #2 SALINA,KS. 67401(XD8508)

ALL H-60 SERIES AIRCRAFT,REMOVAL OF INPUT MODULE GEARBOX ASSEMBLIESWITHPOTENTIALLY CRACKED BEVELGEARS

UH-60-00-02MWO:

Priority Mnt Level



360

360

5601.1

7923273 5529.9 4595


UH-60A A00500115 Days


HELICOPTER, UTILITY INTERMEDIATE GEARBOX Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

JM88437602-May-2006NORMALROUTINE3791.03701379101-May-2006

AH31189124-Jul-2006NORMALROUTINE3831.03741383120-Jul-2006

BJ11753104-Dec-2006NORMALROUTINE3870.03780387029-Nov-2006

BJ11753105-Feb-2007NORMALROUTINE112.03813390331-Jan-2007

BJ11753105-Apr-2007NORMALROUTINE130.03831392103-Apr-2007

TL96948521-Jun-2007NORMALROUTINE173.03874396416-Jun-2007

TL96948528-Sep-2007NORMALROUTINE249.03950404025-Sep-2007

TL96948519-Oct-2007NORMALROUTINE288.03989407916-Oct-2007

TL96948512-Nov-2007NORMALROUTINE330.04031412109-Nov-2007

BJ11753104-Jan-2008NORMALROUTINE360.04061415101-Jan-2008

TL96948510-Mar-2008NORMALROUTINE399.04100419006-Mar-2008

TL96948503-Apr-2008NORMALROUTINE439.04140423031-Mar-2008

TL96948502-May-2008ABNORMALROUTINE477.04178426801-May-2008

RM17316607-May-2008NORMALSPECIAL487.04188427807-May-2008

DS41998721-May-2008NORMALROUTINE520.04221431120-May-2008

GM42302518-Jun-2008ABNORMALROUTINE556.04257434715-Jun-2008

GM42302524-Jun-2008NORMALSPECIAL562.04263435321-Jun-2008

DS41998722-Jul-2008NORMALROUTINE598.04299438919-Jul-2008

GM42302520-Aug-2008NORMALROUTINE643.04344443419-Aug-2008

DP32368426-Sep-2008NORMALROUTINE681.04382447224-Sep-2008

DP32368404-Oct-2008NORMALROUTINE684.04385447503-Oct-2008

DS41998702-Nov-2008NORMALROUTINE716.04417450731-Oct-2008

DS41998709-Dec-2008NORMALROUTINE757.04458454806-Dec-2008

DS41998731-Dec-2008NORMALROUTINE784.04485457528-Dec-2008

FS60759315-May-2009NORMALPRE RESET804.04505459512-May-2009

MM112233POST RESET0.045954594.915-Jul-2009

MM112233POST RESET7.04512460221-Jul-2009

DR62091209-Dec-2009NORMAL40 HOUR38.04543463303-Dec-2009

MB86971409-Jun-2010NORMALSPECIAL94.04599468902-Jun-2010

MB86971413-Jan-2011NORMALROUTINE191.04696478605-Jan-2011

DM64902805-Aug-2011ABNORMALBASELINE294.04799488901-Aug-2011

DM64902826-Aug-2011ABNORMALLAB REQUES298.04803489319-Aug-2011

DN33751617-Sep-2011NORMALSPECIAL1.04819490912-Sep-2011

KS17333711-Jan-2012NORMALROUTINE77.04895498509-Dec-2011

DN33751604-Jan-2013NORMALROUTINE334.05152524203-Jan-2013

DN33751619-Nov-2013NORMALROUTINE370.05188527814-Nov-2013

DN33751610-Dec-2014NORMALROUTINE589.05407.55497.509-Dec-2014

DN33751606-Nov-2015ABNORMALROUTINE103.65511.15601.104-Nov-2015

LAB REQUES9.75520.85610.830-Nov-2015



360

360

5601.1

7923273 5529.9 4595


UH-60A A00500115 Days


HELICOPTER, UTILITY INTERMEDIATE GEARBOX Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


DRAIN FLUSH AND REFILL, RESAMPLE PRIOR TO FLIGHT3JAN13 - ROUTINE OIL SAMPLE, ACFT HOURS 5242.314NOV13- ROUTINE OIL SAMPLE ACFT HRS 5277.906 NOV 15 - ABNORMAL SAMPLE WATER EXCEEDS PPM LIMIT - LAB RECOMMENDATION - DRAIN AND FLUSH THEN RESAMPLE AFTER NEXT FLIGHT24 NOV 15 -SPECIAL SAMPLE PER AOAP LAB REQUEST

9. REMARKS:



PIDMWODATE HRS



INTERMEDIATE GEARBOX 7923273A005001151. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


08-Oct-2011 OE

AL72722408-Oct-2011

0.3B CO 777 ASBONE TIME INSPECTION OFINTERMEDIATE GEAR BOXES WITHINSTALLATION TIMES OF UNDER 100HOURS

H-60-12-SOF-01MWO:

Priority Mnt Level

10-Oct-2011 OE

AL72722411-Oct-2011

0.2B CO 777 ASBONE TIME INSPECTION OF NEWINTERMEDIATE GEAR BOXESINSTALLED REDUCE FROM 100HOURS TO 50 HOURS FOR LACK OFLUBRICATION (CLEARSINTERMEDIATE GEARBOXESREPAIRED BY CCAD

H-60-12-SOF-02MWO:

Priority Mnt Level

14-Oct-2011 OE

AL72722415-Oct-2011

0.2B CO 777 ASBAUTHORIZE THE USE OF GEARBOX70357-06300-042&044 THAT HAVEBEEN INSPECTED THROUGHWHOLESALE SUPPY ON ANY H-60A/L/K/M

H-60-12-SOF-03MWO:

Priority Mnt Level



PIDMWODATE HRS



LATERAL SERVO BELLCRANK 7923273F337-010391. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Jan-2001 OT

QC00000005-Jan-2001

1AASF #2 SALINA,KS (XS9537)

H-60 SERIES AIRCRAFT, REMOVALOF LATERAL SERVO BELLCRANKASSEMBLY MANUFACTURED BY THEPURDY MACHINE COMPANY, CAGECODE 15152

UH-60-01-03MWO:

Priority Mnt Level

14-Jul-2010 OT

DM64902827-Jul-2010


H-60-10-ASAM-11MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR BLADE ASSY 7923273A007042131. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


28-Feb-1998 DM

JA00113914-Sep-2010

1CCAD/WOMUAAINCREASE IN FATIGUE LIFE FORTHE MAIN ROTOR BLADE CUFFS,P/N 7-150-09109-041, 70150-09109-043

H-60-97-ASAM-11MWO:

Priority Mnt Level

12-Aug-2002 OT

JA113914-Sep-2010

1CCAD/W0MUAAALL H-60 SERIES AIRCRAFT,REVISION TO UH-60-02-11, ONE-TIMEINSPECTION OF MAIN ROTORBLADE CUFF ASSEMBLY

UH-60-02-12MWO:

Priority Mnt Level

07-Jan-2003 OT

JA113914-Sep-2010

1CCAD/W0MUAAALL H-60 SERIES AIRCRAFT,INSPECTION OF MAIN ROTORBLADE CUFF ASSEMBLY

UH-60-03-02MWO:

Priority Mnt Level

15-Sep-2005 DO

JA113914-Sep-2010

13CCAD/W0MUAARECAP REQUIREMENTS FOR THEUH-60 MAIN ROTOR BLADE P/N:70150-09100-043 NSN: 1615-01-106-1903

DMWR 1-1615-281 C1MWO:

Priority Mnt Level

14-Apr-2010 DU

JA113914-Sep-2010

3CCAD/W0MUAADEPOT REPAIRED LEGACY MAINROTOR BLADES

H-60-10-S0F-01MWO:

Priority Mnt Level

09-Mar-2015 DI

NG030609-Mar-2015

12.51109TH TASMGPMI INSPECTION COMPLETED,HEATER MAT RESISTANCE CHECKCOMPLETED AND FOUNDSERVICEABLE, SPAR PRESSURECHECK COMPLETED AND FOUNDSERVICEABLE, REPLACED NICKELSTRIP IAW MEC F194836 AND SRAAX 220713R1, REPLACED 4 EA. CUFFLINERS, REPLACED 4 EA. OUTERCUFF BUSHINGS, PAINTED ANDSTENCILED, WEIGHT AND BALANCECOMPLETED USING AVIONBALANCER

F194836MWO:

Priority Mnt Level



PIDMWODATE HRS





28-Feb-1998 OM

MF203419-Apr-2012

1CCAD/W0MUAAINCREASE IN FATIGUE LIFE FORTHE MAIN ROTOR BLADE CUFFS,P/N 70150-09109-041 AND 70150-09109-43

UH-60-97-ASAM-11 TB 1-1MWO:

Priority Mnt Level

12-Aug-2002 OT

MF203419-Apr-2012

1CCAD/W0MUAAALL H-60 SERIES AIRCRAFT,REVISION TO UH-60-02-11, ONE-TIMEINSPECTION OF MAIN ROTORBLADE CUFF ASSEMBLY

UH-60-02-12MWO:

Priority Mnt Level

07-Jan-2003 OT

MF203419-Apr-2012

1CCAD/W0MUAAALL H-60 SERIES AIRCRAFT,INSPECTION OF MAIN ROTORBLADE CUFF ASSEMBLY

UH-60-03-02MWO:

Priority Mnt Level

15-Sep-2005 DO

MF203419-Apr-2012

13CCAD0W0MUAARECAP REQUIREMENTS FOR THEUH-60 MAIN ROTOR BLADE P/N:70150-09100-043 NSN: 1615-01-106-1903

DMWR 1-1615-281 C1MWO:

Priority Mnt Level

14-Apr-2010 OM

MF203419-Apr-2012

3CCAD/W0MUAADEPOT REPAIRED LEGACY MAINROTOR BLADES

H-60-10-SOF-01 14-APR-10 MWO:

Priority Mnt Level

07-May-2015 DI

NG030607-May-2015

121109TH TASMGPMI 2 COMPLETED, HEATER MATRESISTANCE CHECK COMPLETEDAND FOUND SERVICEABLE, SPARPRESSURE CHECK COMPLETEDAND FOUND SERVICEABLE,REPLACED NICKEL STRIP IAW SRAAX220713R1 AND MEC F197137,CRACK AT STA. 300 ZONE 4REPAIRED IAW W/P 585, TOP ANDBOTTOM ROOT END FAIRING CRACKREPAIRED IAW W/P 585, TOPLEADING CUFF BUSHING REPLACEDIAW W/P 612. PAINTED ANDSTENCILED BLADE, WEIGHT ANDBALANCE COMPLETED USINGAVION BALANCER.

F197137MWO:

Priority Mnt Level



PIDMWODATE HRS





15-Sep-2005 DO

RS100501-Nov-2013

13CCAD/W0MUAARECAP REQUIREMENTS FOR THEUH-60 MAIN ROTOR BLADE P/N:70150-09100-043 NSN: 1615-01-106-1903

DMWR 1-1615-281 C1MWO:

Priority Mnt Level

09-Apr-2012 OT

RS100501-Nov-2013

1CCAD/W0MUAACHANGE TO DEPOT REPAIREDLEGACY MAIN ROTOR BLADESCOMPLIANCE DATE

H-60-12-SOF-05MWO:

Priority Mnt Level

05-Mar-2015 DI

NG030605-Mar-2015

12.51109TH TASMGPMI 2 INSPECTION COMPLETED.HEATER MAT RESISTANCE CHECKCOMPLETED AND FOUNDSERVICEABLE, SPAR PRESSURECHECK COMPLETED AND FOUNDSERVICEABLE, REPLACED NICKELSTRIP IAW SRA AX220713R1, 2 PLYLAYUP TO REPAIR SMALL ROOTEND FAIRING CRACK, PAINTED ANDSTENCILED, WEIGHT AND BALANCECOMPLETED USING AVIONBALANCER

AX220713R1MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 7923273A001053621. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


13-Feb-2013 FM

KS17333702-Mar-2013

0.2AASF2ONE TIME INSPECTION OF MAINROTOR SPINDLE ANTI-FLAPASSEMBLIES

H-60-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS





26-Feb-2013 FM

KS17333701-Mar-2013

0.2AASF2PERFORM ONE-TIME INSPECTIONFOR SUSPECT MAIN ROTORSPINDLE ANTI-FLAP BRACKETASSEMBLIES

H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS





13-Feb-2013 FM

KS17333702-Mar-2013


H-60-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 7923273D001004411. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


13-Feb-2013 FM

KS17333702-Mar-2013


H-60-ASAM-03MWO:

Priority Mnt Level



0

720

5247

7923273 3437.9 4595


UH-60A A26500334 Days


HELICOPTER, UTILITY MAIN TRANSMISSION MODULE Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

MM112233BASELINE0.024134594.915-Jul-2009

MM112233BASELINE7.02420460221-Jul-2009


MB86971409-Dec-2010NORMALROUTINE180.025934775.221-Dec-2010

DN33751612-Mar-2012NORMALBASELINE417.02830501207-Mar-2012


DN33751606-Nov-2015NORMALROUTINE354.13419.15601.104-Nov-2015

07 MAR 12 - BASELINE SAMPLE11-JAN-13 ROUTINE SAMPLE

9. REMARKS:



PIDMWODATE HRS



MAIN TRANSMISSION MODULE 7923273A265003341. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


16-Jun-2003 OU

LT822315-Sep-2007

10CCAD, C.C.TEXAS 78419-5260

MAIN MODULE PLANETARYCARRIER ASSEMBLY RETIREMENETLIFE, ALL UH-60A, EH-60A AND UH-60Q SERIES AIRCRAFT

1-1520-237-20-265MWO:

Priority Mnt Level

26-Mar-2014 FM

DN33751620-May-2014

1AASF2,WVARNG

MAIN TRANSMISSION FILTER BOWLAND CHIP DETECTOR ATTACHMENTHARDWARE REPLACEMENT.

H-60-14-AMAM-09MWO:

Priority Mnt Level



9369.1149895619.9B112054221560011291256SAS ACTUATOR70410-02500-04907A24

Report Date: MAJOR COMPONENT LISTINGSorted By: Work Unit Code

1/319-Jan-2016

DUE

AIRCRAFT HRS TO

REPLACESERIAL NONSNPART NOMENCLATUREPART NO

UH-60AMODEL:

WUC

7923273

CURR

AIRCRAFT SERIAL NO:

Major Component Listing for 16 Items

14380.1200005619.9UNK32731560010819244TAIL PYLON FITTING70209-06051-04302C15J

4845.1104655619.9C308002971615014504834HUB, M/R ROTOR ASSY70103-08112-04705A01A

6060.1116805619.9A001053621615014426926MAIN ROTOR SPINDLE ASSY70102-08200-06905A01I



6944.1125645619.9D001004411615014426926MAIN ROTOR SPINDLE ASSY70102-08200-06905A01I

9019.1146395619.9B286004981615010745151MAIN ROTOR SHAFT EXTENDER70351-08186-04305A01L

7380.1130005619.9U-101615011277388BIFILAR, M/R ROTOR ASSY70107-08400-04605A01T

4721.1103415619.9A007042131615011061903MAIN ROTOR BLADE ASSY70150-09100-04305A02




6105.1117255619.9A009031491615011138188TAIL ROTOR BLADE ASSY70101-31000-04305B02

7152.1127725619.9A009056781615011138188TAIL ROTOR BLADE ASSY70101-31000-04305B02

11981.1176015619.9K257003211615010836812O/B RETENTION PLATE (T/R)70102-11101-04206G01B

1495.171155619.913424140013293428FAN AXIAL52E15-106H23

10513.1161335619.9B112054071560011291256SAS ACTUATOR70410-02500-04907A24


2/319-Jan-2016

9369.1149895619.9B112054221560011291256SAS ACTUATOR70410-02500-04907A24

8636.1142565619.9D112-131421560011291256SAS ACTUATOR70410-02500-04907A24

691.163115619.9233-034121615011417532TAIL ROTOR PITCH CHANGE SHAFT70400-06100-04211C23

10079.1156995619.9B300-000671650013056954TAIL ROTOR SERVO ASSY2227000-1711C25

21774.1273945619.9B303-051711650011431226MAIN ROTOR PRIMARY SERVO274000-103111D01

20563.1261835619.9B303-06435B1650011431226MAIN ROTOR PRIMARY SERVO70410-02820-05411D01

22048.1276685619.9B303100281650011431226MAIN ROTOR PRIMARY SERVO70410-02820-05411D01

7380.1130005619.9A345-009531560011589685AFT BELLCRANK70400-08102-04511D04

13874.1194945619.9A391017871560011644161AFT TIE ROD SUPT FITTING70400-08112-04511D05

73.156935619.9MM002391680011644160AFT TIE ROD ASSY70400-08111-04211D06

1280.169005619.9390-012551560012868870AFT BELLCRANK SPT ASSY70400-08117-04911D07

6877.1124975619.9C380000813040011899711LATERAL SWASHPLATE LINK70400-08151-05011D08

17374.1229945619.9F337-010391680012212863LATERAL SERVO BELLCRANK70400-08166-04111D09

10981.1166015619.9R346006741680011589653AFT WALKING BEAM70400-08104-04811D11

8945.1145655619.9D344000521560010832954LEFT TIE ROD70400-08115-04311D13

3127.187475619.9288-013121560012969486RIGHT TIE ROD ASSY70400-08114-05111D14

13531.1191515619.966936006421680011589652FORWARD BELLCRANK70400-08101-04611D15

12531.1181515619.9B367033441560012212619FORWARD BELLCRANK SUPPORT70400-08162-04211D16

NSN SERIAL NOPART NO PART NOMENCLATURE

AIRCRAFT

DUE REPLACE

HRS TO

CURR

Major Component Listing for 76F01

AIRCRAFT SERIAL NO:MODEL: UH-60A 7923273

WUC


3/319-Jan-2016


AIRCRAFT

DUE REPLACE

HRS TO

CURR

Major Component Listing for 16-1 Items


WUC

-34323432 08260432835013692818AUXILIARY POWER UNIT116305-30215B


AIRCRAFT

DUE REPLACE

HRS TO

CURR

Major Component Listing for 714 Engines


WUC

PIDMWODATE HRS



MTCHD ROTOR/STATOR ASSY 7923273MRS070221. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


31-Jul-1989 DM

DN33751620-Jul-2015


MODIFICATION OF GG ROTORASSEMBLY T700/701

MWO 55-2840-248-50-32MWO:

Priority Mnt Level

30-Aug-1994 OM

DN33751620-Jul-2015


ONE TIME INSP/CONVERION OFFORMS & RECORDS FORT700/701/701C ENGINES

TB 1-2840-248-20-2MWO:

Priority Mnt Level

25-Oct-1996 OM

DN33751620-Jul-2015


ALL UH-60A, EH-60A AIRCRAFT WITHT700-GE-700 ENGINES SUBJECT:REPLACEMENT OF UNDAMPED GASGENERATOR ROTOR/STATORASSEMBLIES


Priority Mnt Level



PIDMWODATE HRS



PLANETARY CARRIER ASSY 7923273F240001371. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Oct-2009 ON

DR62091205-Oct-2009

1AASF#1LAKEHUSRT NJ08733

PLANETARY GEAR RETIREMENTLIFE

H-60-10-AMAM-02MWO:

Priority Mnt Level



PIDMWODATE HRS



PUMP MODULE ASSY, HYDRAUL 792327371912ABR1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


29-Jul-2005 DR

SS090710-Dec-2012

5.4CCADRECAPPED DMWR 1-4320-271MWO:

Priority Mnt Level



PIDMWODATE HRS



SAS ACTUATOR 7923273B112054221. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


23-Mar-2001 FT

QC00000027-Mar-2001

0.5AASF #2 SALINA,KS (XS9537)

ALL H-60 SERIES AIRCRAFT,INSPECTION OF ALL SASACTUATORS

UH-60-01-06MWO:

Priority Mnt Level



SECTION I COCKPITSES BEST

4. EQUIPMENT CHECKLIST

7923273 UH-60A

3. AREA NAME 2. MODEL 1. SERIAL NUMBER


1RECEIVER RADIO - R-1496A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER

QTY REQ:NOMENCLATURITEM NO

1DISPLACEMENT GYRO - CN-1314/A (9000C)

Unt

UUUUUUnt

Unt

Un

Unt

Un2

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GYRO, DIRECTIONAL - CN-998/ASN-43

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SIGNAL DATA CONVERTER - CV-3338A/ASN-128B

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING FOR KIT-1A/1C/TSEC - MT-3949A/U

Unt

UUUUUUnt

Unt

Un

Unt

Un0

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER - R-2139/ARN-123(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING - MT-4834/ARN-123(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMMAND INSTR SYS PROCESSOR - 70600-01038-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING RACK - 70600-01038-102

Unt

UUUUUUnt

Unt

Un

Unt

Un1

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT FOR TSEC/KY-58 - 5290279-502

Unt

UUUUUUnt

Unt

Un

Unt

Un1

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#2 VHF-FM ANTENNA - AS-4171/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un1

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SAS AMPLIFIER - 70901-02908-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO ASSEMBLY - 70600-01047-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2RATE GYRO - TRU-2A/A

Unt

UUUUUUnt

Unt

Un

Unt

Un2

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1AMPILIFIER IMPEDANCE - AM-4859A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


For use of this form, see DA PAM 738-751; the proponent agency is DCSLOGEDITION OF JAN 64 IS OBSOLETE

AIRCRAFT INVENTORY RECORDDA FORM 2408-17 E, NOV 91



7923273 UH-60A



1VHF/AM ANTENNA FILTER - 70600-01012-102

Unt

UUUUUUnt

Unt

Un

Unt

Un1

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2VHF/FM ANTENNA FILTER - 70600-01011-103

Unt

UUUUUUnt

Unt

Un

Unt

Un2

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER RADAR - RT-1193/ASN-128

Unt

UUUUUUnt

Unt

Un

Unt

Un1

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2ANTENNA - AS-3831/APN-209(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un2

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GLIDE SLOPE ANTENNA - 70600-01043-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#2 VHF-FM, VHF-AM SENSE ANTENNA - 70600-01019-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2FIRST AID KIT - 6545-00-919-6650

Unt

UUUUUUnt

Unt

Un

Unt

Un2

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRE EXTINGUISHER - FR23-4-11848

Unt

UUUUUUnt

Unt

Un

Unt

Un1

25

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BAROMETERIC ALTIMETER - AAU-31/A-1

Unt

UUUUUUnt

Unt

Un

Unt

Un1

26

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BAROMETERIC ALTIMETER - AAU-32/A

Unt

UUUUUUnt

Unt

Un

Unt

Un1

27

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2CREW SEAT - D3801-2

Unt

UUUUUUnt

Unt

Un

Unt

Un2

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF-AM RADIO SET - RT-1518/ARC-164(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

31

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2INTERPHONE CONTROL - C6533/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un2

32

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER/TRANSMITTER - RT-1115D/APN-209

Unt

UUUUUUnt

Unt

Un

Unt

Un1

33

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1INDICATOR ALTIMETER - ID-1917C/APN-209

Unt

UUUUUUnt

Unt

Un

Unt

Un1

34

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






7923273 UH-60A



1CONTROL RADIO SET - C-7392/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

35

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2CONTROL - C-10604(V)6/ARN-184

Unt

UUUUUUnt

Unt

Un

Unt

Un1

36

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPARATOR SIGNAL DATA - CM482/ARC-186(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

38

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2MOUNTREVERSIBLE ARC-186/ARC-201 - 4290268-501

Unt

UUUUUUnt

Unt

Un

Unt

Un2

40

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPUTER DISPLAY UNIT - CP-1252C/ASN-128B

Unt

UUUUUUnt

Unt

Un

Unt

Un1

42

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CIVIL NAVIGATION CONTROL - C-10048/ARN-123(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

43

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS SET CONTROLLER - C-8021E/ASN-75

Unt

UUUUUUnt

Unt

Un

Unt

Un1

44

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RADIO RETRANSMISSION PANEL -70550-01008-042

Unt

UUUUUUnt

Unt

Un

Unt

Un1

45

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MAGNETIC COMPASS - MS17983-4

Unt

UUUUUUnt

Unt

Un

Unt

Un1

46

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2OUTSIDE AIR TEMP INDICATOR - MS28028-1

Unt

UUUUUUnt

Unt

Un

Unt

Un2

47

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOR WING PANEL - 70500-01152-093

Unt

UUUUUUnt

Unt

Un

Unt

Un1

48

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOR WING PANEL - 70500-01152-094

Unt

UUUUUUnt

Unt

Un

Unt

Un1

49

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MISC. SWITCH PANEL - 70450-01090-044

Unt

UUUUUUnt

Unt

Un

Unt

Un1

50

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1STABILATOR/FLT CONT PANEL - 70902-01070-048

Unt

UUUUUUnt

Unt

Un

Unt

Un1

51

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2AHRU MOUNTING PLATE FOGS

Unt

UUUUUUnt

Unt

Un

Unt

Un0

60

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






7923273 UH-60A



1MOUNTING BASE APX-118

Unt

UUUUUUnt

Unt

Un

Unt

Un1

61

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1765200-20 FOGS CONTROL UNIT (AHRU)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

62

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2ATTITUDE & HEADING REFERENCE UNIT, CN-1716/A (FOGS)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

63

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO ASSEMBLY 70600-01213-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

64

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER




5/5Report Date: 16-Jan-2016AREA NAMEMODELSERIAL NUMBER

SECTION I COCKPITSES BEST7923273 UH-60A

NAME OR PIDNUMBER DATE

db c

DATE NUMBER RANKRANK NAME OR PID

CHECK CHECK

ba ad

5. VERIFICATION

c

ED0460141 CIV 16-Jan-2016

b. LOCATION/REMARKSCHECK NO.

6. LOCATION OR REMARKS

a. ITEM NUMBER

Nomenclature

DISPLACEMENT GYRO - CN-1314/A (9000C)

1 Aircraft arrived to the BEST Program in this configuration.2

MOUNTING FOR KIT-1A/1C/TSEC - MT-3949A/U


CONTROL - C-10604(V)6/ARN-184


COMPARATOR SIGNAL DATA -CM482/ARC-186(V)


AHRU MOUNTING PLATEFOGS


765200-20 FOGS CONTROLUNIT (AHRU)


ATTITUDE & HEADINGREFERENCE UNIT, CN-1716/A(FOGS)


RATE GYRO ASSEMBLY 70600-01213-041


REVERSE OF DA FORM 2408-17 E, NOV 91

SECTION II CABINSES BEST


7923273 UH-60A



1CARGO HOOK, FE-7590-145 70800-02503-111

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MARKER BEACON ANTENNA - 70600-02011-103

Unt

UUUUUUnt

Unt

Un

Unt

Un1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-105

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRST AID KIT - 6545-00919-6650

Unt

UUUUUUnt

Unt

Un

Unt

Un1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2FIRE EXTINGUISHER - FR23-4-11848

Unt

UUUUUUnt

Unt

Un

Unt

Un1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CRASH AXE - 56D6221

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HAND SET - H-250/U

Unt

UUUUUUnt

Unt

Un

Unt

Un1

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SLAB BATTERY -D8565/11-1

Unt

UUUUUUnt

Unt

Un

Unt

Un1

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3INTERPHONE CONTROL - C6533/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un2

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ADAPTER FUEL DRAIN - 70307-03018-102

Unt

UUUUUUnt

Unt

Un

Unt

Un1

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


4LOCK ASSY BLADE TIEDOWN - 70700-20369-041

Unt

UUUUUUnt

Unt

Un

Unt

Un4

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2PLUG ASSY INTAKE - HIRSS SUPP - 70700-20515-041/042

Unt

UUUUUUnt

Unt

Un

Unt

Un2

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2PLUG ASSY EXHAUST - HIRSS - 70700-20515-043

Unt

UUUUUUnt

Unt

Un

Unt

Un0

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PLUG ASSY APU EXHAUST - 70700-20509-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

15

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






7923273 UH-60A



1COVER ASSY OIL COOLER - 70700-20511-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BLADE FOLD SET - 70700-20412-011

Unt

UUUUUUnt

Unt

Un

Unt

Un0

17

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER PITOT TUBE - 70700-20460-041

Unt

UUUUUUnt

Unt

Un

Unt

Un2

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


7TROOP SEATS - 70500-02151-045

Unt

UUUUUUnt

Unt

Un

Unt

Un7

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3TROOP SEATS - 70500-02151-047

Unt

UUUUUUnt

Unt

Un

Unt

Un4

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


10RESTRAINT SYSTEM - 70500-02153-103

Unt

UUUUUUnt

Unt

Un

Unt

Un11

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GUNNER SEAT - 70500-02152-047

Unt

UUUUUUnt

Unt

Un

Unt

Un1

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GUNNER SEAT - 70500-02152-048

Unt

UUUUUUnt

Unt

Un

Unt

Un1

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2RESTRAINT SYSTEM - 70500-02156-102

Unt

UUUUUUnt

Unt

Un

Unt

Un2

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ICS WALK-AROUND CORD - 70602-02016-041

Unt

UUUUUUnt

Unt

Un

Unt

Un2

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PORTABLE INSP. FLOOD LIGHT - 15-0366-1

Unt

UUUUUUnt

Unt

Un

Unt

Un1

29

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HYD. PUMP HANDLE - 15400-50126

Unt

UUUUUUnt

Unt

Un

Unt

Un1

30

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRING KEY - 70550-03101-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

31

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2EQUIPMENT LOGBOOK - MIL-D-43064

Unt

UUUUUUnt

Unt

Un

Unt

Un1

32

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1WEIGHT AND BALANCE HANDBOOK - TM 55-1500-342-23

Unt

UUUUUUnt

Unt

Un

Unt

Un1

34

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






7923273 UH-60A



1ELECTRONIC SEQUENCE UNIT - 163290-100-E

Unt

UUUUUUnt

Unt

Un

Unt

Un1

52

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION II CABINSES BEST7923273 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

ED0460141 CIV 16-Jan-2016



a. ITEM NUMBER

Nomenclature

FIRE EXTINGUISHER - FR23-4-11848


INTERPHONE CONTROL -C6533/ARC


PLUG ASSY EXHAUST - HIRSS- 70700-20515-043


COVER ASSY OIL COOLER -70700-20511-041


BLADE FOLD SET - 70700-20412-011


TROOP SEATS - 70500-02151-047


RESTRAINT SYSTEM - 70500-02153-103


GUNNER SEAT - 70500-02152-048


ICS WALK-AROUND CORD -70602-02016-041


EQUIPMENT LOGBOOK - MIL-D-43064



SECTION III TRANSITION SECTIONSES BEST


7923273 UH-60A



1ANTENNA LOOP - AS-2108A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un0

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2IFF ANTENNA - 70600-02010-103

Unt

UUUUUUnt

Unt

Un

Unt

Un2

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF/AM ANTENNA - 70600-03002-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PUMP FUEL SAMPLER - 82829/4P156-3

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPENSATOR MAGNETIC FLUX - CN-405/ASN

Unt

UUUUUUnt

Unt

Un

Unt

Un1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS TRANSMITTER - T-611/ASN-43

Unt

UUUUUUnt

Unt

Un

Unt

Un1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GPS ANTENNA - 22433-40

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF AMPLIFIER - AM-7531/URC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA. GPS (BFT) S67-1575-863

Unt

UUUUUUnt

Unt

Un

Unt

Un1

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA, L-BAND (BFT) S65-8282-301

Unt

UUUUUUnt

Unt

Un

Unt

Un1

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT, IFM AMPLIFIER-MT-6592/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un1

42

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3933/ARN-149(V)1, ANTENNA, LOOP

Unt

UUUUUUnt

Unt

Un

Unt

Un1

49

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1TROOP COMMANDER ANTENNA (CMWS ONLY)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

50

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IVHMU (CBM MONITOR SYSTEM)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

55

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION III TRANSITION SECTIONSES BEST7923273 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

ED0460141 CIV 16-Jan-2016



a. ITEM NUMBER

Nomenclature

ANTENNA LOOP - AS-2108A/ARN-89


HF AMPLIFIER - AM-7531/URC1 Aircraft arrived to the BEST Program in this configuration.8

IVHMU (CBM MONITORSYSTEM)



SECTION IV TAIL CONESES BEST


7923273 UH-60A



2VOR/LOC ANTENNA - 70600-05002-101

Unt

UUUUUUnt

Unt

Un

Unt

Un2

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IFM AMPLIFIER - AM-7189A/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF ANTENNA - 4700516-30

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION IV TAIL CONESES BEST7923273 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

ED0460141 CIV 16-Jan-2016



a. ITEM NUMBER

Nomenclature

IFM AMPLIFIER - AM-7189A/ARC



SECTION V TAIL ROTOR PYLONSES BEST


7923273 UH-60A



1CU-2457/ARC(405-11-1), VHF-FM #1 COUPLER ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM10-267, VHF-FM #2 (LEADING EDGE) ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM10-3230, VHF-FM TROOP COMMANDER ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un0

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION V TAIL ROTOR PYLONSES BEST7923273 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

ED0460141 CIV 16-Jan-2016



a. ITEM NUMBER

Nomenclature

FM10-3230, VHF-FM TROOPCOMMANDER ANTENNA



PIDMWODATE HRS



STATIONARY SWASHPLATE 7923273015152-18741. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


14-Jul-2010 OT

DM64902827-Jul-2010


H-60-10-ASAM-11MWO:

Priority Mnt Level



ReportDate:

SUBCOMPONENT LISTING Sorted By: Work Unit Code 1/419-Jan-2016

PART NOMENCLATURE SER NO

AIRCRAFTCURR DUEWUC

MAJORCOMPONENTSERIAL NUMBER

SUBCOMPONENT PART NUMBER

HRS TOREPLACE

7923273MODEL: UH-60A

Sub Component Listing for 16 Items

AIRCRAFT SERIAL NO:

03A01A PISTON, MAIN L/GEAR STR70250-12067-102BEM3167 BEM3167 14510 8890.15619.9

03A01A MAIN SHOCK STRUTPISTON

70250-12067-102IA00410 IA05992 13470 7850.15619.9

05A01I04 M/R SPINDLE NUT70102-08105-102A00105362 C47911947 17040 11420.15619.9

05A01I04 M/R SPINDLE NUT70102-08105-102A00107968 F47901029 16881 11261.15619.9

05A01I04 M/R SPINDLE NUT70102-08105-102A00111789 F47909576 18247 12627.15619.9

05A01I04 M/R SPINDLE NUT70102-08105-102D00100441 F47900279 17564 11944.15619.9

05A01I06 TIE ROD (M/R SPINDLE)38023-10372-101A00105362 C50401839 11680 6060.15619.9

05A01I06 TIE ROD (M/R SPINDLE)38023-10372-101A00107968 D50400080 11881 6261.15619.9

05A01I06 TIE ROD (M/R SPINDLE)70102-08102-103A00111789 C50413041 8047 2427.15619.9

05A01I06 TIE ROD (M/R SPINDLE)38023-10372-101D00100441 C50403995 12564 6944.15619.9

05A01I07 HORN ASSEMBLY70102-08111-047A00105362 A24115704 23504 17884.15619.9

05A01I07 HORN ASSEMBLY70102-08111-047A00107968 A24119030 23881 18261.15619.9

05A01I07 CONTROL HORN ASSY70102-08111-043A00111789 H24101609 6947 1327.15619.9

05A01I07 HORN ASSEMBLY70102-08111-047D00100441 A24117069 24564 18944.15619.9

05A02I M/R BLADE CUFF70150-09109-041A00704213 A23706570 6090 470.15619.9

05A02I M/R BLADE CUFF70150-09109-041A00709066 A23709587 6860 1240.15619.9

05A02I M/R BLADE CUFF70150-09109-041A00713113 F23700049 8334 2714.15619.9

ReportDate:


05A02I M/R BLADE CUFF70150-09109-041A00713121 33150935 7699 2079.15619.9

05A03A02 ROTATING SWASHPLATEASSEMBLY

70104-08001-045151521924 151521924 15595 9975.15619.9

06A08 SWASHPLATE GUIDE70351-08227-041A26500334 AER01184 21595 15975.15619.9

06A13 HOUSING ASSY MGB70351-08110-045A26500334 A21101430 7595 1975.15619.9

06A18 MAIN ROTOR SHAFT70351-08131-048A26500334 E25304617 12195 6575.15619.9

06A19 PLANETARY CARRIER ASSY70351-08175-046A26500334 F24000137 16595 10975.15619.9

06G01C I/B RETENTION PLATE T/R70358-06612-042A00603014 C25900721 15627 10007.15619.9

06G01D GEARSHAFT, BEVEL70358-06620-102A00603014 F32000921 9595 3975.15619.9

06H23A BALL BRNG ANN (OILCOOLER FWD)

Z33C321342 1342AFT 7115 1495.15619.9

06H23A BALL BRNG ANN (OILCOOLER FWD)

Z33C321342 1342FWD 7115 1495.15619.9

11C23A BRNG T/R PITCH CHGSHAFT

SB1162-102233-03412 10827 6311 691.15619.9

WUC PART NOMENCLATURE

HRS TOREPLACE

SUBCOMPONENTPART NUMBER


AIRCRAFTCURR DUE

AIRCRAFT SERIAL NO:UH-60AMODEL:

SER NO

Sub Component Listing for 76F01

7923273


HRS TOREPLACE

SUBCOMPONENTPART NUMBER PART NOMENCLATUREWUC SER NO


AIRCRAFTCURR DUE

Sub Component Listing for 16-1 Items

AIRCRAFT SERIAL NO:

6035T88P04GEC00653104A01C01 GAS GENERATOR TURBINESHAFT

52072268GATBC694 7475

6035T88P04GEC00763404A01C01 GAS GENERATOR TURBINESHAFT

79983096GATFA285 11094

ReportDate:


6035T83P01GEC00653104A01C04 COMPRESSOR REAR SHAFT 30372268FIAALTG4 5305

6035T83P01GEC00763404A01C04 COMPRESSOR REAR SHAFT 17183096GATM6569 4814

5043T04P02GEC00653104A01C07 TIE ROD, COMPRESSOR 68732268GATCKV13 9141

5043T04P02GEC00763404A01C07 TIE ROD, COMPRESSOR 78593096GATPR150 10955

4045T08P01GEC00653104A01C08 RING, SPACERCOMPRESSOR

51372268GATHW010 7405

4045T08P01GEC00763404A01C08 RING, SPACERCOMPRESSOR

58073096GATF9665 8903

6055T59P01GEC00653104A01D COMPRESSOR IMPELLER 30372268GLHTFJRN 5305

6055T59P01GEC00763404A01D COMPRESSOR IMPELLER 49753096GLHTL0W8 8071

6032T26G09GEC00653104A01H STAGE 1 BLISK 30372268GLHTFLWC 5305

6032T26G09GEC00763404A01H STAGE 1 BLISK 49753096GLHTLE26 8071

6032T27P08GEC00653104A01J STAGE 2 BLISK 50372268GLHTFD61 7305

6032T27P08GEC00763404A01J STAGE 2 BLISK 69753096GLHTLE5N 10071

6038T08P04GEC00653104A01K STAGE 3 & 4 BLISK 50372268GLHTFJN9 7305

6038T08P04GEC00763404A01K STAGE 3 & 4 BLISK 69753096GLHTLC77 10071

6038T09P04GEC00653104A01L STAGE 5 BLISK 50372268GLHTFHL5 7305

6038T09P04GEC00763404A01L STAGE 5 BLISK 69753096GLHTKAH1 10071

6064T85P01MRS0702204A02B01 STAGE 1 TURBINE DISK 30223096GAT9408W 6118

6064T85P01MRSG596104A02B01 STAGE 1 TURBINE DISK 37542268GATHGA8R 6022

6064T86P01MRS0702204A02B04 STAGE 2 TURBINE DISK 42663096GATH8E58 7362

6064T86P01MRSG596104A02B04 STAGE 2 TURBINE DISK 37542268GATHG3MN 6022

ReportDate:


6064T81P01MRS0702204A02B05 STAGE 1 FWD COOLINGPLATE

47293096GFF5CL98 7825

6064T81P01MRSG596104A02B05 STAGE 1 FWD COOLINGPLATE

33012268GFFR85NJ 5569

6064T82P01MRS0702204A02B06 STAGE 1 REAR COOLINGPLATE

47293096GFF5CM9M 7825

6064T82P01MRSG596104A02B06 STAGE 1 REAR COOLINGPLATE

37542268PAMEV260 6022

6064T83P01MRS0702204A02B08 STG 2 FWD COOLING PLATE 47293096GFF5CD43 7825

6064T83P01MRSG596104A02B08 STG 2 FWD COOLING PLATE 37542268PAMEN939 6022

6064T84P02MRS0702204A02B09 STAGE 2 REAR COOLINGPLATE

47293096GFF5CLD1 7825

6064T84P02MRSG596104A02B09 STAGE 2 REAR COOLINGPLATE

37542268GFF5CGFH 6022

6038T32P01GEL03736104A03E01 STAGE 3 TURBINE DISK 34363096GATLL187 6532

6038T32P01GEL80747704A03E01 STAGE 3 TURBINE DISK 25482268GAT6439P 4816

6038T34P05GEL03736104A03E02 STAGE 4 TURBINE DISK 34363096GATLF634 6532

6038T34P05GEL80747704A03E02 STAGE 4 TURBINE DISK 25482268GAT8673P 4816

5125T92G01GEL03736104A03F POWER TURBINE SHAFT 50733096GATH934T 8169

5125T92G01REGEL80747704A03F POWER TURBINE SHAFT 19182268GATM7178 4186

450290282604315B02B WHEEL, COMPRESSOR 39003432V42-C5613 7332

450399182604315B03 WHEEL, TURBINE 39003432V82-HC643 7332


HRS TOREPLACE

SUBCOMPONENTPART NUMBER PART NOMENCLATUREWUC SER NO


AIRCRAFTCURR DUE

Sub Component Listing for 714 Engines

AIRCRAFT SERIAL NO:

17-Jan-2016

T700-GE-700ENGINE ASSY, TURBINE

ALT ETFACT TTV°CTIMENUMBERNG %PRESSFATENGINESERIAL 866 +/- 49. TORQUE10.8.7.6.AIRCRAFT REMARKS11. TGTDATE 12.5.4.

GEE306518

3. ENGINE SERIAL NUMBER2. ENGINE MODEL1. NOMENCLATUREReport Date: Page 1 of 1

16-Nov-2015 7923273 POST PHASE 120KIASHRSS AND BAFFLESINSTALLED

6500 105 102 199.7-42250 845


T700 SERIES TURBINE ENGINE ANALYSIS CHECK RECORDDA FORM 2408-19-2 E, DEC 91

17-Jan-2016

T700-GE-700ENGINE ASSY, TURBINE

ALT ETFACT TTV°CTIMENUMBERNG %PRESSFATENGINESERIAL 866 +/- 49. TORQUE10.8.7.6.AIRCRAFT REMARKS11. TGTDATE 12.5.4.

GEE307361

3. ENGINE SERIAL NUMBER2. ENGINE MODEL1. NOMENCLATUREReport Date: Page 1 of 1

20-Jul-2015 7923273 POST RESET ENGINE TEAC8000 90 89 197.3122831 846

16-Nov-2015 7923273 POST PHASE 120KIASHRSS AND BAFFLESINSTALLED

6500 100 102 0.9898.1-43078 845


T700 SERIES TURBINE ENGINE ANALYSIS CHECK RECORDDA FORM 2408-19-2 E, DEC 91

PIDMWODATE HRS



TAIL ROTOR BLADE ASSY 7923273A009031491. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


14-Nov-2001 OM

RS100521-Mar-2014

1CCAD/W0MUAAINTIAL AND RECURRINGINSPECTION OF THE TAIL ROTORFAIRING ASSEMBLEY

UH-60-02-ASAM-01 TB 1MWO:

Priority Mnt Level

15-Sep-2005 DR

RS100521-Mar-2014

15.1CCAD/W0MUAARECAP REQUIREMENTS FOR THEUH-60 TAIL ROTOR BLADE P/N:70101-31000-043 NSN:1615011138188

1-1615-287 C1 TB1-1520-MWO:

Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR BLADE ASSY 7923273A009056781. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


14-Nov-2001 OM

MF00203408-Dec-2014

0.1CCAD/W0MUAAINITIAL AND RECURRINGINSPECTION OF THE TAIL ROTORFAIRING ASSEMBLY

UH-60-02-ASAM-01 TB 1-1MWO:

Priority Mnt Level

15-Sep-2005 DR

MF00203408-Dec-2014

15.1CCAD/W0MUAARECAPPED1-1615 287 C1MWO:

Priority Mnt Level



360

360

5497.5

7923273 1144.9 4595


UH-60A A00603014 Days


HELICOPTER, UTILITY TAIL ROTOR GEARBOX ASSY Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

MM112233BASELINE0.01204594.915-Jul-2009

MM112233BASELINE7.0127460221-Jul-2009

MM112233BASELINE0.0127460222-Jul-2009

MB86971409-Dec-2009NORMAL40 HOUR0.01584633.203-Dec-2009


MB86971413-Jan-2011NORMALROUTINE184.0311478605-Jan-2011

KS17333717-Jan-2012ABNORMALROUTINE383.0510498509-Dec-2011

KS17333725-Jan-2012NORMALLAB REQ387.0514498919-Jan-2012


DN33751619-Nov-2013NORMALROUTINE676.0803527814-Nov-2013

DN33751610-Dec-2014NORMALROUTINE895.91022.55497.509-Dec-2014

DN33751606-Nov-2015NORMALROUTINE103.61126.15601.104-Nov-2015

NEEDS DRAIN AND FLUSH AND RESAMPLE AFTER NEXT FLIGHT3JAN12 - ROUTINE OIL SAMPLE, ACFT HOURS 5242.314NOV13-ROUTINE OIL SAMPLE, ACFT HRS 5277.9

9. REMARKS:



PIDMWODATE HRS



TAIL ROTOR GEARBOX ASSY 7923273A006030141. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


28-Aug-2003 DU

AB242227-Nov-2007

0.5CCAD,C.C.TEXAS78419-5260

RECAPITALIZATION OF THE UH-60TAIL ROTOR GEARBOX ASSY, PN:70358-06600-046

AED T3150, REV B. DMWR MWO:

Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR PITCH CHANGE SHAFT 7923273233-034121. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


27-Jan-2014 TT

DH35474527-Jan-2014

1W8RJAAH-60-14-SOF-02 T/R PITCH CHANGESHAFT ASSY

H-60-14-SOF-02MWO:

Priority Mnt Level



2015/12/16 AWBS 10.0 Page 1 of 13

CHART A - BASIC WEIGHT CHECKLIST RECORDCOMPARTMENT: A - ELECTRONICS COMPARTMENT STA 162 - 204

MDS: UH-60ASERIAL NO: 79-23273CONSTANT: 1,000

1. (151104) AASF2 Wheeling WV2. (140820) AASF2 Wheeling WV3. (130820) Wheeling, WV

4. (120829) Wheeling, WV5. (110913) LAKEHURST, NJ6. (110802) Groton CT7. (110308) LAKEHURST, NJ

Item Number Item Description Weight

(lb)

Long. Arm (in)

Long. Mom.

(lb-in)In

A/CMan. Inv. Date

151104

140820

130820

120829

110913

110802

110308

A -000.00 MASTER CHART A RELEASED 2 JUL 09 0.1 2015/11/04 O O O O O O O

A -001.00 NOSE DOOR 0.1 2015/11/04 O O O O O O O

A -002.00 RADAR RECEIVER R-2218/APR-39(V) 2.0 164.00 0.33 X 2015/11/04 I I I I I I I

A -003.00 LOWER SHELF WL - 215 0.1 2015/11/04 O O O O O O O

A -004.00COMMAND INSTRUMENT (CIS) PROCESSOR CP-2036/A 5.7 175.00 1.00 X 2015/11/04 I I I I I I I

A -005.00 COMPUTER KIT-1C/TSEC 8.3 176.00 1.46 2015/11/04 O O O O O O O

A -006.00IFF TRANSPONDER RT-1836/APX-118(V) 1008939G-5 11.0 176.00 1.94 X 2015/11/04 I I I I I I I

A -007.00 SIGNAL DATA CONVERTER CV-3338A/ASN-128B 13.5 177.00 2.39 2015/11/04 O O O O O O O

A -008.00SIGNAL DATA CONVERTER (ALT) CV-3338B/ASN-128D P30A002-02 11.0 177.00 1.95 X 2015/11/04 I I I I I I I

A -009.00 AHRU, LHS (FOGS GYRO) 765100-0020 6.0 178.00 1.07 2015/11/04 O O O O O O O

A -010.00 AHRU, RHS (FOGS GYRO) 765100-0020 6.0 178.00 1.07 2015/11/04 O O O O O O O

A -011.00SIGNAL DATA CONVERTER, (HUD) CV-4229/AVS-7 13.7 178.00 2.44 X 2015/11/04 I I I I I I I

A -012.00DISPLACEMENT GYRO CONTROL, LHS CN-1314/A (9000C) 5.7 179.00 1.02 X 2015/11/04 I I I I I I I

A -013.00DISPLACEMENT GYRO CONTROL, RHS CN-1314/A (9000C) 5.7 179.00 1.02 X 2015/11/04 I I I I I I I

A -014.00TRANSMITTER, RATE GYROSCOPE, LHS TRU-2A/A NSN 6615-01-059-7909 1.7 181.00 0.31 X 2015/11/04 I I I I I I I

A -015.00TRANSMITTER, RATE GYROSCOPE, RHS TRU-2A/A NSN-6615-01-059-7909 1.7 181.00 0.31 X 2015/11/04 I I I I I I I

A -016.00 PROCESSOR, DIGITAL CP-1597A/APR-39(V) 5.9 193.00 1.14 X 2015/11/04 I I I I I I I

A -017.00 SAS AMPLIFIER 70901-02908 2.7 198.00 0.53 X 2015/11/04 I I I I I I I

A -018.00 RECEIVER, VOR R-2139/ARN-123(V) 9.2 204.00 1.88 X 2015/11/04 I I I I I I I

A -019.00 CANTED BULKHEAD STA 185 0.1 2015/11/04 O O O O O O O

A -020.00 DIRECTION GYRO CN-998(B)/ASN-43 5.5 182.00 1.00 X 2015/11/04 I I I I I I I

A -021.00 RECEIVER, ADF R-1496/APN-89 6.9 184.00 1.27 X 2015/11/04 I I I I I I I

A -022.00 RECEIVER R-2382/ARN-149(V)1 6.0 184.00 1.10 2015/11/04 O O O O O O O

A -023.00 UPPER SHELF WL - 226 0.1 2015/11/04 O O O O O O O

A -024.00 SECURITY SET, LHS TSEC/KY-58 4.9 190.00 0.93 X 2015/11/04 I I I I I I I

A -025.00 SECURITY SET, CENTER TSEC/KY-58 4.9 190.00 0.93 X 2015/11/04 I I I I I I I

A -026.00 SECURITY SET, RHS TSEC/KY-58 4.9 190.00 0.93 X 2015/11/04 I I I I I I I

A -027.00SIGNAL DATA CONVERTER, FWD (INST) 70450-01916 9.2 199.00 1.83 X 2015/11/04 I I I I I I I

A -028.00SIGNAL DATA CONVERTER, AFT (INST) 70450-01916 9.2 204.00 1.88 X 2015/11/04 I I I I I I I

A -029.00 RECEIVER R-2594/ARN-147(V) 8.0 204.00 1.63 2015/11/04 O O O O O O O

A -030.00 AFT CANTED BULKHEAD, RHS 0.1 2015/11/04 O O O O O O O

2015/12/16 AWBS 10.0 Page 2 of 13

CHART A - BASIC WEIGHT CHECKLIST RECORDCOMPARTMENT: B - COCKPIT COMPARTMENT STA 204 - 247





(lb)

Long. Arm (in)

Long. Mom.

(lb-in)In

A/CMan. Inv. Date

151104

140820

130820

120829

110913

110802

110308

B -001.00 INSTRUMENT PANEL, LHS 0.1 2015/11/04 O O O O O O O

B -002.00AIR BAG W/GAS GENERATOR, GLARESHIELD 70070-95117 2.7 205.00 0.55 2015/11/04 O O O O O O O

B -003.00 AIRSPEED INDICATOR 70450-01042 1.0 206.00 0.21 X 2015/11/04 I I I I I I I

B -004.00VERTICAL SITUATION INDICATOR 70450-01040 / NSN-6610-01-155-8315 5.7 206.00 1.17 X 2015/11/04 I I I I I I I

B -005.00HORIZONTAL SITUATION INDICATOR 70450-01040 6.5 206.00 1.34 X 2015/11/04 I I I I I I I

B -006.00 RADAR ALTIMETER APN-209, RT-1115J 3.7 206.00 0.76 X 2015/11/04 I I I I I I I

B -007.00 ALTIMETER AAU-31/A 2.2 206.00 0.45 X 2015/11/04 I I I I I I I

B -008.00 VERTICAL SPEED INDICATOR 70450-01088 1.6 206.00 0.33 X 2015/11/04 I I I I I I I

B -009.00 CO-PILOT DISPLAY UNIT 70450-01916 4.3 206.00 0.89 X 2015/11/04 I I I I I I I

B -009.01 CLOCK ABU-11A/ 1.0 206.00 0.21 X 2015/11/04 I I I I I I I

B -010.00 INSTRUMENT PANEL, CENTER 0.1 2015/11/04 O O O O O O O

B -011.00 CAUTION / ADVISORY PANEL 70550-01107 5.4 206.00 1.11 X 2015/11/04 I I I I I I I

B -012.00 CENTRAL DISPLAY UNIT 70450-01916 9.0 206.00 1.85 X 2015/11/04 I I I I I I I

B -013.00AUXILIARY FUEL MANAGEMENT PANEL 70550-01411 2.6 206.00 0.54 2015/11/04 O O O O O O O

B -014.00 COCKPIT DISPLAY UNIT (IVHMS) 10150-0201 4.1 206.00 0.84 X 2015/11/04 I I I I I I I

B -015.00 RADAR SIGNAL INDICATOR IP-1150/APR-39(V) 2.0 206.00 0.41 X 2015/11/04 I I I I I I I

B -016.00 BLADE DEICE, TEST 70902-01099 1.0 206.00 0.21 X 2015/11/04 I I I I I I I

B -017.00FAULT MONITOR PANEL, BLADE DE-ICE 70902-01110 2.0 206.00 0.41 X 2015/11/04 I I I I I I I

B -018.00 ICE RATE METER, BLADE DE-ICE 70550-01124 3.0 206.00 0.62 X 2015/11/04 I I I I I I I

B -019.00 INSTRUMENT PANEL, RHS 0.1 2015/11/04 O O O O O O O

B -020.00AIR BAG W/GAS GENERATOR, GLARESHIELD 70070-95117 2.7 205.00 0.55 2015/11/04 O O O O O O O

B -021.00 RADAR ALTIMETER ID-1917C/APN-209(V) 2.0 206.00 0.41 X 2015/11/04 I I I I I I I

B -022.00 ENCODING BAROMETRIC ALTIMETER AAU-32A 2.2 206.00 0.45 X 2015/11/04 I I I I I I I

B -023.00 VERTICAL SPEED INDICATOR 70450-01088 1.6 206.00 0.33 X 2015/11/04 I I I I I I I

B -024.00VERTICAL SITUATION INDICATOR 70450-01040 / NSN-6610-01-155-8315 5.7 206.00 1.17 X 2015/11/04 I I I I I I I

B -025.00HORIZONTAL SITUATION INDICATOR 70450-01040 6.5 206.00 1.34 X 2015/11/04 I I I I I I I

B -026.00 AIRSPEED INDICATOR 70450-01042 1.0 206.00 0.21 X 2015/11/04 I I I I I I I

B -027.00 PILOT’S DISPLAY UNIT 70450-01916 4.3 206.00 0.89 X 2015/11/04 I I I I I I I

B -027.01 CLOCK ABU-11A/ 1.0 206.00 0.21 X 2015/11/04 I I I I I I I

B -028.00 LOWER CONTROL CONSOLE, LHS 0.1 2015/11/04 O O O O O O O

B -029.00 STORES JETTISON PANEL 7-517400101 2.0 212.00 0.42 2015/11/04 O O O O O O O

B -030.00 ADF RECEIVER C-7392/ARN-89 3.3 215.00 0.71 X 2015/11/04 I I I I I I I

B -031.00 ADF CONTROL PANEL C-12491/ARN-149(V)1 2.0 215.00 0.43 2015/11/04 O O O O O O O

B -032.00CIVIL NAVIGATION CONTROL C-12550/ARN-147(V) 2.0 218.00 0.44 2015/11/04 O O O O O O O

B -033.00 CIVIL NAV CONTROL, VOR ARN-123 2.0 218.00 0.44 X 2015/11/04 I I I I I I I

B -034.00 ICS BOX C-6533/ARC 1.8 221.00 0.40 X 2015/11/04 I I I I I I I

2015/12/16 AWBS 10.0 Page 3 of 13






(lb)

Long. Arm (in)

Long. Mom.

(lb-in)In

A/CMan. Inv. Date

151104

140820

130820

120829

110913

110802

110308

B -035.00CONTROL PANEL, VHF/AM C-10604A(V)6/ARC-186A(V) 2.0 224.00 0.45 2015/11/04 O O O O O O O

B -036.00COMMUNICATIONS SECURITY CONTROL PANEL KY-58/Z-AHP 2.0 227.00 0.45 X 2015/11/04 I I I I I I I

B -036.01CONTROL PANEL, VHF/FMC-11466A/ARC-201A(V) 1.7 229.00 0.39 X 2015/11/04 I I I I I I I

B -037.00 CONTROL HEAD, CMWS C-12645-ALE A100766... 2.6 231.00 0.60 2015/11/04 O O O O O O O

B -038.00 LOWER CONTROL CONSOLE, CENTER 0.1 2015/11/04 O O O O O O O

B -039.00DOPPLER/GPS CONTROL PANEL CP-1252C/ASN-128B 6.0 216.00 1.30 X 2015/11/04 I I I I I I I

B -040.00STABILATOR/FLIGHT CONTROL PANEL 70902-01070 5.0 222.00 1.11 X 2015/11/04 I I I I I I I

B -041.00CONTROL PANEL, VHF/AM C-10604A(V)6/ARC-186 2.0 224.00 0.45 X 2015/11/04 I I I I I I I

B -042.00RECEIVER/TRANSMITTER CONTROL RT-1296A/APX-100(V) 8.0 227.00 1.82 2015/11/04 O O O O O O O

B -043.00REMOTE CONTROL UNIT (CONTROL HEAD) AN/APX-118 1008940P-4 3.0 227.00 0.68 X 2015/11/04 I I I I I I I

B -044.00 FUEL BOOST PUMP CONTROL 70902-01115 1.2 231.00 0.28 X 2015/11/04 I I I I I I I

B -045.00 LOWER CONTROL CONSOLE, RHS 0.1 2015/11/04 O O O O O O O

B -046.00 COMPASS CONTROL PANEL C-8021A/ASN-75 2.2 212.00 0.47 X 2015/11/04 I I I I I I I

B -047.00 CONTROL UNIT (AHRU) 765200-20 FOGS 2.0 212.00 0.42 2015/11/04 O O O O O O O


B -049.00 UHF/AM RADIO RT-1518C/ARC-164 9.0 218.00 1.96 X 2015/11/04 I I I I I I I

B -050.00 ICS BOX C-6533/ARC 1.8 221.00 0.40 X 2015/11/04 I I I I I I I

B -051.00CONTROL PANEL, VHF/FM C-11466A/ARC-201A(V) 2.0 224.00 0.45 X 2015/11/04 I I I I I I I

B -052.00 CONTROL INDICATOR 2566/AAR-47(V) 1.5 225.00 0.34 2015/11/04 O O O O O O O


B -054.00CONTROL DISPLAY UNIT AN/ARC-220 C-12436/URC 3.2 231.00 0.74 X 2015/11/04 I I I I I I I

B -054.01CONTROL, HEADS UP DISPLAY AN/AVS-7 2.0 242.00 0.48 X 2015/11/04 I I I I I I I

B -055.00 PILOTS SEAT WELL 0.1 2015/11/04 O O O O O O O

B -055.01VHF/FM RADIO RT-1477/ARC-201C(V)NSN 5821-01-306-4653 6.7 223.00 1.49 X 2015/11/04 I I I I I I I

B -056.00VHF/FM RADIO RT-1477/ARC-201C(V) NSN-5821-01-306-4653 6.7 229.00 1.53 X 2015/11/04 I I I I I I I

B -057.00 VHF AM/FM RADIO RT-1300A/ARC-186(V) 6.4 234.00 1.50 X 2015/11/04 I I I I I I I

B -058.00 DIMMER CONTROL, SEARCH LIGHT 70553-618... 2.8 236.00 0.66 X 2015/11/04 I I I I I I I

B -059.00 UNGROUPED ITEMS 0.1 2015/11/04 O O O O O O O

B -060.00REMOTE DATA CONCENTRATOR (IVHMS) 30201-0501 (QUAD BAY) 4.3 205.00 0.88 X 2015/11/04 I I I I I I I

B -061.00 BPS, COCKPIT FLOOR-02 12.0 208.10 2.50 2015/11/04 O O O O O O O



2015/12/16 AWBS 10.0 Page 4 of 13






(lb)

Long. Arm (in)

Long. Mom.

(lb-in)In

A/CMan. Inv. Date

151104

140820

130820

120829

110913

110802

110308


B -065.00 BPS, COCKPIT VER-06 9.0 231.20 2.08 2015/11/04 O O O O O O O

B -066.00 BPS, COCKPIT VER-05 9.0 231.20 2.08 2015/11/04 O O O O O O O

B -067.00 PILOT SEAT & RESTRAINT D3801-01/70500-01... 113.0 235.00 26.56 X 2015/11/04 I I I I I I I

B -068.00CO-PILOT SEAT & RESTRAINT D3801-01/70500-01151 113.0 235.00 26.56 X 2015/11/04 I I I I I I I

B -069.00ELECTRONIC CRASH SENSOR UNIT (AIR BAG SYSTEM) 70070-95117 3.2 236.00 0.76 2015/11/04 O O O O O O O

B -070.00DC-DC POWER CONVERTER (EDM) 143-1075-003 (QUAD BAY) 2.0 237.00 0.47 X 2015/11/04 I I I I I I I

B -071.00BFT PALLET ASSY & W3 HARNESS 040409-002 (QUAD BAY) 26.0 237.00 6.16 X 2015/11/04 I I I I I I I

B -072.00 ARMORED WING, LHS 70500-01152 16.0 238.00 3.81 X 2015/11/04 I I I I I I I

B -073.00 ARMORED WING, RHS 70500-01152 16.0 238.00 3.81 X 2015/11/04 I I I I I I I

B -074.00LATERAL AIR BAG W/GAS GENERATOR, LHS 70070-95117 3.5 238.00 0.83 2015/11/04 O O O O O O O

B -075.00LATERAL AIR BAG W/GAS GENERATOR, RHS 70070-95117 3.5 238.00 0.83 2015/11/04 O O O O O O O

B -076.00 CONTROL, RESCUE HOIST KIT 70550-01119 2.0 240.00 0.48 X 2015/11/04 I I I I I I O

B -077.00 MCU, PILOTS/CO-PILOTS HOSES 5.0 240.00 1.20 2015/11/04 O O O O O O O

B -078.00FIRE EXTINGUISHER, SEAT, LHS NSN-6830-00-555-8837 6.1 243.00 1.48 X 2015/11/04 I I I I I I I

B -079.00 SAS/FPS COMPUTER (AFCS) 70901-02903 15.3 243.00 3.72 X 2015/11/04 I I I I I I I

B -080.00 MAIN TERMINAL, KY-100, ARC-220 4700479-10 6.0 244.50 1.47 X 2015/11/04 I I I I I I I

B -081.00 DATA TRANSFER UNIT (IVHMS) 30192-0201 1.8 245.00 0.44 X 2015/11/04 I I I I I I I

B -082.00 MILTOPE (LAPTOP) WIRE HARNESS 40427 3.8 247.00 0.94 2015/11/04 O O O O O O I

2015/12/16 AWBS 10.0 Page 5 of 13

CHART A - BASIC WEIGHT CHECKLIST RECORDCOMPARTMENT: C - FORWARD CARGO COMPARTMENT STA 247 - 288





(lb)

Long. Arm (in)

Long. Mom.

(lb-in)In

A/CMan. Inv. Date

151104

140820

130820

120829

110913

110802

110308

C -001.00FIRST AID KIT, CO-PILOT SEAT, LHS NSN-6545-00-919-6650 1.3 247.00 0.32 X 2015/11/04 I I I I I I I

C -002.00FIRST AID KIT, CO-PILOT SEAT, LHS NSN-6545-00-919-6650 1.3 247.00 0.32 X 2015/11/04 I I I I I I I

C -003.00FIRST AID KIT, PILOT SEAT, RHS NSN-6545-00-919-6650 1.3 247.00 0.32 X 2015/11/04 I I I I I I I

C -004.00WALK AROUND ICS CORD, 50* (STOWED), RHS 70602-02016 2.1 247.00 0.52 X 2015/11/04 I I I I I I O

C -005.00MAINTENANCE FLOODLIGHT (STOWED) 15-0366-1 1.9 247.00 0.47 X 2015/11/04 I I I I I I I

C -005.01ELT EBC-406 HM TRANSMITTER AND MOUNT BRACKET 2.5 247.00 0.62 X 2015/11/04 I I I I I I I

C -006.00 ICS BOX (CO-PILOT SEAT), LHS C-6533/ARC 1.8 248.00 0.45 X 2015/11/04 I I I I I I I

C -007.00 ICS BOX (PILOT SEAT), RHS C-6533/ARC 1.8 248.00 0.45 X 2015/11/04 I I I I I I I

C -008.00 CRASH AXE NSN-4210-00-243-0863 2.8 249.00 0.70 X 2015/11/04 I I I I I I I

C -009.00MCU, W/POWER WIRES & MASK BLOWER HARNESSES, CO-PILOTS 14.0 250.00 3.50 2015/11/04 O O O O O O O

C -010.00MCU, W/POWER WIRES & MASK BLOWER HARNESSES, PILOTS 14.0 250.00 3.50 2015/11/04 O O O O O O O

C -011.00MCU, W/POWER WIRES & MASK BLOWER HARNESSES, CREWMEMBERS, LHS 14.0 250.00 3.50 2015/11/04 O O O O O O O

C -012.00MCU, W/POWER WIRES & MASK BLOWER HARNESSES, CREWMEMBERS, RHS 14.0 250.00 3.50 2015/11/04 O O O O O O O

C -013.00 BATTERY, ACFT (SLAB) D8565/11-1 35.0 252.00 8.82 X 2015/11/04 I I I I I I I

C -014.00 BATTERY, ACFT (ALTERNATE) BB 716/A 16.7 252.00 4.21 2015/11/04 O O O O O O O

C -015.00 BATTERY COVER 70209-02532 2.5 253.00 0.63 X 2015/11/04 I I I I I I I

C -016.00SOUNDPROOFING, SIDEWALL PANEL, LHS 70500-02053 4.0 257.00 1.03 X 2015/11/04 I I I I I I I

C -017.00SOUNDPROOFING, SIDEWALL PANEL, RHS 70500-02053 4.0 257.00 1.03 X 2015/11/04 I I I I I I I

C -018.00 MCU MOUNT ASSY LSF 00447-001 37.0 260.00 9.62 2015/11/04 O O O O O O O

C -019.00FIRE EXTINGUISHER, CABIN, RHS NSN-4210-00-555-8837 6.1 263.00 1.60 X 2015/11/04 I I I I I I I

C -020.00SUPPORT, UPPER TROOP SEATS (MEDEVAC) 70500-03104 23.0 265.00 6.10 2015/11/04 O O O O O O O

C -021.00SUPPORT, LOWER TROOP SEATS (MEDEVAC) 70500-03102 61.0 267.00 16.29 2015/11/04 O O O O O O O

C -022.00TROOP SEAT & BELTS, LH (MEDEVAC) 70500-02151 16.0 269.00 4.30 2015/11/04 O O O O O O O

C -023.00TROOP SEAT & BELTS, CENTER (MEDEVAC) 70500-02151 16.0 269.00 4.30 2015/11/04 O O O O O O O

C -024.00TROOP SEAT & BELTS, RH (MEDEVAC) 70500-02151 16.0 269.00 4.30 2015/11/04 O O O O O O O

C -025.00 CREWMEMBERS HOSES, MCU 5.0 270.00 1.35 2015/11/04 O O O O O O O

C -026.00 SOUNDPROOFING, CEILING, LHS 70500-02062 4.0 271.00 1.08 X 2015/11/04 I I I I I I I

C -027.00 SOUNDPROOFING, CEILING, RHS 70500-02062 3.0 271.00 0.81 X 2015/11/04 I I I I I I I

C -028.00SOUNDPROOFING, CEILING, CENTER 70500-02061 3.0 271.00 0.81 X 2015/11/04 I I I I I I I

2015/12/16 AWBS 10.0 Page 6 of 13

CHART A - BASIC WEIGHT CHECKLIST RECORDCOMPARTMENT: C - FORWARD CARGO COMPARTMENT STA 247 - 288





(lb)

Long. Arm (in)

Long. Mom.

(lb-in)In

A/CMan. Inv. Date

151104

140820

130820

120829

110913

110802

110308

C -029.00CONVERTER MEDEVAC KIT NSN-6130-00-421-5314 96.0 276.00 26.50 2015/11/04 O O O O O O O

C -030.00 MACHINE GUN MOUNT ARM, LHS M240 10.1 280.00 2.83 2015/11/04 O O O O O O O

C -031.00 MACHINE GUN MOUNT ARM, RHS M240 10.1 280.00 2.83 2015/11/04 O O O O O O O

C -032.00 TROOP SEAT SUPPORT 70500-02160 8.3 280.00 2.32 X 2015/11/04 I I I I I I I

C -033.00 CREW CHIEF / GUNNER SEAT, LHS 70500-02152 24.5 282.00 6.91 X 2015/11/04 I I I I I I I

C -034.00 CREW CHIEF SEAT, RHS 70500-02152 24.5 282.00 6.91 X 2015/11/04 I I I I I I I

C -035.00 TROOP COMMANDER’S SEAT 70500-02151 16.3 282.00 4.60 2015/11/04 O O O O O O O

C -036.00 BALLASTIC PROTECTION SYSTEM 0.1 2015/11/04 O O O O O O O

C -037.00 BPS BRACKET A17 0.5 251.50 0.13 2015/11/04 O O O O O O O



C -040.00 BPS, PAX FLOOR-01B 3.0 254.80 0.76 2015/11/04 O O O O O O O

C -041.00 BPS, PAX FLOOR-01C 4.0 255.40 1.02 2015/11/04 O O O O O O O

C -042.00 BPS, PAX FLOOR-01A 37.0 261.00 9.66 2015/11/04 O O O O O O O



C -045.00 BPS, PAX VER-02 36.0 287.70 10.36 2015/11/04 O O O O O O O

2015/12/16 AWBS 10.0 Page 7 of 13

CHART A - BASIC WEIGHT CHECKLIST RECORDCOMPARTMENT: D - CENTER CARGO COMPARTMENT STA 288 - 343





(lb)

Long. Arm (in)

Long. Mom.

(lb-in)In

A/CMan. Inv. Date

151104

140820

130820

120829

110913

110802

110308

D -001.00SUPPORT, SOUNDPROOFING70500-02059-064 2.0 295.00 0.59 X 2015/11/04 I I I I I I I

D -001.01SOUNDPROOFING, CEILING, CENTER 70500-02063 9.0 310.00 2.79 X 2015/11/04 I I I I I I I

D -002.00 ICS BOX C-6533/ARC 1.8 322.00 0.58 X 2015/11/04 I I I O O O O

D -003.00 TROOP SEAT, FWD, LH 70500-02151 16.3 322.00 5.25 X 2015/11/04 I I I I I I I

D -004.00 TROOP SEAT, FWD, CENTER 70500-02151 16.3 322.00 5.25 X 2015/11/04 I I I I I I I

D -005.00 TROOP SEAT, FWD, RH 70500-02151 16.3 322.00 5.25 X 2015/11/04 I I I I I I I

D -006.00 WIRING RESCUE HOIST KIT 70070-30005 10.0 324.00 3.24 X 2015/11/04 I I I I I I O

D -007.00 SUPPORT SOUNDPROOFING 70500-02059-058 2.0 326.00 0.65 X 2015/11/04 I I I I I I I

D -008.00 TROOP SEAT SUPPORT 70500-02160 8.3 331.00 2.75 X 2015/11/04 I I I I I I I

D -009.00 TROOP SEAT, REAR, LH 70500-02151 16.3 338.00 5.51 X 2015/11/04 I I I I I I I

D -010.00 TROOP SEAT, REAR, CENTER LH 70500-02151 16.3 338.00 5.51 X 2015/11/04 I I I I I I I

D -011.00 TROOP SEAT, REAR, CENTER RH 70500-02151 16.3 338.00 5.51 X 2015/11/04 I I I I I I I

D -012.00TROOP SEAT, REAR, RH (ALT SEATING) 70500-02151 16.3 338.00 5.51 X 2015/11/04 I I I I I I I

D -013.00TUBE & RESTRAINT (MEDEVAC 6-MAN), LHS 70802-12433 8.0 338.00 2.70 2015/11/04 O O O O O O O

D -014.00TUBE & RESTRAINT (MEDEVAC 6-MAN), RHS 70802-12433 8.0 338.00 2.70 2015/11/04 O O O O O O O

D -015.00 C2 CONSOLE & RACK 040321 78.0 340.00 26.52 2015/11/04 O O O O O O O

D -016.00 DRIP PAN CEILING, CENTER 70500-02070 14.0 342.00 4.79 X 2015/11/04 I I I I I I I

D -017.00 BALLASTIC PROTECTION SYSTEM 0.1 2015/11/04 O O O O O O O

D -018.00 BPS, PAX VER-05 36.0 288.00 10.37 2015/11/04 O O O O O O O

D -019.00 BPS, PAX FLOOR-03 88.0 293.90 25.86 2015/11/04 O O O O O O O


D -021.00 BPS B-KIT BRACKETS & FASTENERS 15.0 309.50 4.64 2015/11/04 O O O O O O O



2015/12/16 AWBS 10.0 Page 8 of 13

CHART A - BASIC WEIGHT CHECKLIST RECORDCOMPARTMENT: E - AFT CARGO COMPARTMENT STA 343 - 398





(lb)

Long. Arm (in)

Long. Mom.

(lb-in)In

A/CMan. Inv. Date

151104

140820

130820

120829

110913

110802

110308

E -001.00 SOUNDPROOFING, CEILING, LHS 70500-02072 5.0 344.00 1.72 X 2015/11/04 I I I I I I I

E -002.00 SOUNDPROOFING, CEILING, RHS 70500-02072 5.0 344.00 1.72 X 2015/11/04 I I I I I I I

E -003.00SUPPORT, UPPER PEDESTAL (MEDEVAC) 70802-12600 11.0 344.00 3.78 2015/11/04 O O O O O O O

E -004.00 PEDESTAL (MEDEVAC 6 MAN) 70802-12300 313.0 344.00 107.67 2015/11/04 O O O O O O O

E -005.00 PEDESTAL (MEDEVAC 4 MAN) 70802-12300 270.0 344.00 92.88 2015/11/04 O O O O O O O

E -006.00LITTER SUPPORT (MEDEVAC LH UPPER) 70802-12420 81.0 344.00 27.86 2015/11/04 O O O O O O O

E -007.00LITTER SUPPORT (MEDEVAC LH LOWER) 70802-12420 81.0 344.00 27.86 2015/11/04 O O O O O O O

E -008.00LITTER SUPPORT (MEDEVAC RH UPPER) 70802-12420 81.0 344.00 27.86 2015/11/04 O O O O O O O

E -009.00LITTER SUPPORT (MEDEVAC RH LOWER) 70802-12420 81.0 344.00 27.86 2015/11/04 O O O O O O O

E -009.01SUPPORT, SOUNDPROOFING70500-02059-060 2.0 360.00 0.72 X 2015/11/04 I I I I I I I

E -010.00 TRAPPED FUEL, AUXILIARY LINES 9.0 360.00 3.24 2015/11/04 O O O O O O O

E -011.00 RESCUE HOIST, INTERNAL (W/OIL) 42305R1 181.0 368.00 66.61 2015/11/04 O O O O O O O

E -012.00ADAPTER PLATE, RESCUE HOIST KIT 70801-02000 19.0 368.00 6.99 2015/11/04 O O O O O O O

E -013.00ELECTRONIC CONTROL UNIT C-12510/AAR-57(V) A100631-100 16.0 371.20 5.94 2015/11/04 O O O O O O O

E -014.00 SOUNDPROOFING, CEILING 70500-52064 8.0 379.00 3.03 X 2015/11/04 I I I I I I I

E -015.00 E.S.U. HONEYWELL APU 2118806-2 or 2118806-1 6.0 384.00 2.30 2015/11/04 O O O O O O O

E -016.00 E.S.U. SUNDSTRAND APU 163290-100 4.0 384.00 1.54 X 2015/11/04 I I I I I I I

E -017.00 AN/PRC-117F #1 (LINE OF SIGHT) 10513-0500-0... 18.0 385.00 6.93 2015/11/04 O O O O O O O

E -018.00 AN/PRC-117F #2 (SATCOM) 10513-0500-011 18.0 385.00 6.93 2015/11/04 O O O O O O O

E -019.00HEADSET & HEADSET HARNESSES (4 EA) 18284-01 & 04-0333-1 9.0 385.00 3.47 2015/11/04 O O O O O O O

E -020.00 AIRCRAFT INTERFACE UNIT (AIU) 780-2000-001 3.0 386.00 1.16 2015/11/04 O O O O O O O

E -021.00SIDEWALL SOUNDPROOFING PANEL, LHS 70500-02068 2.0 388.00 0.78 X 2015/11/04 I I I O O O O

E -022.00SIDEWALL SOUNDPROOFING PANEL, RHS 70500-02068 2.0 388.00 0.78 X 2015/11/04 I I I O O O O

E -023.00 TROOP SEAT, FWD, LH 70500-02151 16.3 392.00 6.39 X 2015/11/04 I I I I I I I

E -024.00 TROOP SEAT, FWD, CENTER, LH 70500-02151 16.3 392.00 6.39 X 2015/11/04 I I I I I I I

E -025.00 TROOP SEAT, FWD, CENTER, RH 70500-02151 16.3 392.00 6.39 X 2015/11/04 I I I I I I I

E -026.00 TROOP SEAT, FWD, RH 70500-02151 16.3 392.00 6.39 X 2015/11/04 I I I I I I I

E -027.00 PUMP HANDLE, APU STOWED 466536A 1.0 397.00 0.40 X 2015/11/04 I I I I I I I

E -028.00AFT BULKHEAD SOUNDPROOFING, BLANKETS 70500-03050 3.0 398.00 1.19 X 2015/11/04 I I I O O O O

E -029.00AFT BULKHEAD SOUNDPROOFING, DOOR, LHS 70500-53050 3.0 398.00 1.19 X 2015/11/04 I I I I I I I

E -030.00AFT BULKHEAD SOUNDPROOFING, DOOR, RHS 70500-53050 3.0 398.00 1.19 X 2015/11/04 I I I I I I I

E -031.00 BALLASTIC PROTECTION SYSTEM 0.1 2015/11/04 O O O O O O O

E -032.00 BPS, PAX FLOOR-10 7.0 357.30 2.50 2015/11/04 O O O O O O O

2015/12/16 AWBS 10.0 Page 9 of 13

CHART A - BASIC WEIGHT CHECKLIST RECORDCOMPARTMENT: E - AFT CARGO COMPARTMENT STA 343 - 398





(lb)

Long. Arm (in)

Long. Mom.

(lb-in)In

A/CMan. Inv. Date

151104

140820

130820

120829

110913

110802

110308



E -035.00 BPS BRACKET A15L 1.0 390.30 0.39 2015/11/04 O O O O O O O

E -036.00 BPS BRACKET A15R 1.0 390.30 0.39 2015/11/04 O O O O O O O

E -037.00 BPS BRACKET A23 0.5 397.30 0.20 2015/11/04 O O O O O O O

2015/12/16 AWBS 10.0 Page 10 of 13

CHART A - BASIC WEIGHT CHECKLIST RECORDCOMPARTMENT: F - AFT SECTION STA 398 - AFT





(lb)

Long. Arm (in)

Long. Mom.

(lb-in)In

A/CMan. Inv. Date

151104

140820

130820

120829

110913

110802

110308

F -001.00ACCUMULATOR, HYDRAULIC W/FLUID 70651-03201 31.0 402.00 12.46 X 2015/11/04 I I I I I I I

F -002.00ACCUMULATOR, HYD WINTERIZATION KIT W/FLUID 70651-03201 31.0 411.00 12.74 2015/11/04 O O O O O O O

F -003.00 TRAPPED FUEL 12.0 414.00 4.97 X 2015/11/04 I I I I I I I

F -004.00 CARGO NET, LHS FDC-1555-149 1.9 421.00 0.80 X 2015/11/04 I I I I I I I

F -005.00 CARGO NET, RHS FDC-1555-149 1.9 421.00 0.80 X 2015/11/04 I I I I I I I

F -006.00 UNUSABLE FUEL W/BOOST PUMPS INSTALLED 17.0 421.00 7.16 X 2015/11/04 I I I I I I I

F -006.01HF RECEIVER/TRANSMITTERRT-1749/URC 11.6 475.00 5.51 X 2015/11/04 I I I I I I I

F -007.00AMPLIFIER, IFM AM-7189A/ARC AN/ARC-186/ARC-201(V) 10.0 473.00 4.73 X 2015/11/04 I I I I I I I

F -008.00 POWER AMPLIFIER TC-100D 15.0 474.00 7.11 2015/11/04 O O O O O O O

F -009.00INTEGRATED VEHICLE HEALTH MANAGEMENT UNIT (IVHMU) 30279-0302 20.0 474.00 9.48 X 2015/11/04 I I I I I I I

F -010.00HF AMPLIFIER COUPLER AM, 7531/URC 4700479-10 18.6 475.00 8.84 X 2015/11/04 I I I I I I I

F -011.00 SEQUENCER, #1 SA-2669/ALE-479V) A100685 3.5 496.40 1.74 2015/11/04 O O O O O O O

F -012.00 SEQUENCER, #2 SA-2669/ALE-47(V) A100685 3.5 496.40 1.74 2015/11/04 O O O O O O O

F -013.00OIL, INTERMEDIATE GEARBOX (0.38 GAL) MIL-L-7808 / MIL-L-23699 / DOD-L-85734 3.0 664.00 1.99 X 2015/11/04 I I I I I I I

F -014.00 RADAR RECEIVER R-2218/APR-39(V) 2.0 687.00 1.37 X 2015/11/04 I I I I I I I

F -015.00OIL, TAIL ROTOR GEARBOX MIL-L-23699 / MIL-L-7808 / DOD-L-85734 2.0 732.00 1.46 X 2015/11/04 I I I I I I I

2015/12/16 AWBS 10.0 Page 11 of 13

CHART A - BASIC WEIGHT CHECKLIST RECORDCOMPARTMENT: G - UPPER DECK STA 241 - 485





(lb)

Long. Arm (in)

Long. Mom.

(lb-in)In

A/CMan. Inv. Date

151104

140820

130820

120829

110913

110802

110308

G -001.00 WORK PLATFORM 70219-04902 6.0 281.00 1.69 X 2015/11/04 I I I I I I I

G -002.00 GENERATOR, LHS 70550-02031 29.0 302.00 8.76 X 2015/11/04 I I I I I I I

G -003.00 GENERATOR, RHS 70550-02031 29.0 302.00 8.76 X 2015/11/04 I I I I I I I

G -004.00 OIL, MAIN GEARBOX DOD-L-85734 OR MIL-L-23699 77.0 347.00 26.72 X 2015/11/04 I I I I I I I

G -005.00 OIL, MAIN GEARBOX MIL-L-7808 71.0 347.00 24.64 2015/11/04 O O O O O O O

G -006.00 ENGINE ASSEMBLY, LHS W/FULL ENGINE OIL T-700-GE-701D 465.0 375.00 174.38 2015/11/04 O O O O O O O

G -007.00 ENGINE ASSEMBLY, RHS W/FULL ENGINE OIL T-700-GE-701D 465.0 375.00 174.38 2015/11/04 O O O O O O O

G -008.00 ENGINE ASSEMBLY, LHS W/FULL ENGINE OIL T-700-GE-700 465.0 375.00 174.38 X 2015/11/04 I I I I I I I

G -009.00 ENGINE ASSEMBLY, RHS W/FULL ENGINE OIL T-700-GE-700 465.0 375.00 174.38 X 2015/11/04 I I I I I I I

G -010.00 GENERATOR, AUXILIARY, APU 70550-02032 26.0 418.00 10.87 X 2015/11/04 I I I I I I I

G -011.00 APU, HONEYWELL W/OIL 3800480-2 91.0 431.00 39.22 2015/11/04 O O O O O O O

G -012.00 APU, SUNDSTRAND W/OIL NSN-2835-01-369-2... 89.0 431.00 38.36 X 2015/11/04 I I I I I I I

G -013.00 APU INLET BARRIER FILTER ASSY (AFS) 104002-101 6.0 435.00 2.61 2015/11/04 O O O O O O O

G -014.00 FIRE EXTINGUISHER BOTTLE W/CARTRIDGE, LHS 70310-03101 5.9 453.00 2.67 X 2015/11/04 I I I I I I I

G -015.00 FIRE EXTINGUISHER BOTTLE W/CARTRIDGE, RHS 70310-03101 5.9 453.00 2.67 X 2015/11/04 I I I I I I I

2015/12/16 AWBS 10.0 Page 12 of 13

CHART A - BASIC WEIGHT CHECKLIST RECORDCOMPARTMENT: H - EXTERNAL EQUIPMENT STA 0 - 770





(lb)

Long. Arm (in)

Long. Mom.

(lb-in)In

A/CMan. Inv. Date

151104

140820

130820

120829

110913

110802

110308

H -000.10 EOMS, FWD LHS SU-202/AAR-579V) A100756 2.8 166.40 0.47 2015/11/04 O O O O O O O

H -000.20 EOMS, FWD RHS SU-202/AAR-57(V) A100756 2.8 166.40 0.47 2015/11/04 O O O O O O O

H -001.00 DOOR, COCKPIT LHS 70217-01002-049 32.0 226.00 7.23 X 2015/11/04 I I I I I I I

H -002.00 DOOR, COCKPIT RHS 70217-01002-050 32.0 226.00 7.23 X 2015/11/04 I I I I I I I

H -003.00 WIRE CUTTER ASSEMBLY, LHS MLG 342-8300... 11.0 282.00 3.10 X 2015/11/04 I I I I I I I

H -004.00 WIRE CUTTER ASSEMBLY, RHS MLG 342-8300... 11.0 282.00 3.10 X 2015/11/04 I I I I I I I

H -005.00 IBF FILTERS, LHS (4 EA @ 8.45 LBS PER FILTER) 33.8 295.00 9.97 2015/11/04 O O O O O O O

H -006.00 IBF FILTERS, RHS (4 EA @ 8.45 LBS PER FILTER) 33.8 295.00 9.97 2015/11/04 O O O O O O O

H -007.00 IBF NACELLE ASSY, LHS 21.8 297.80 6.49 2015/11/04 O O O O O O O

H -008.00 IBF NACELLE ASSY, RHS 21.8 297.80 6.49 2015/11/04 O O O O O O O

H -009.00FAIRING, UPPER REMOVABLE ESSS, LHS 70215-42401 3.0 301.00 0.90 2015/11/04 O O O O O O O

H -010.00FAIRING, UPPER REMOVABLE ESSS, RHS 70215-42401 3.0 301.00 0.90 2015/11/04 O O O O O O O

H -011.00 IBF TRANSITION DUCT & FRAME, LHS 11.3 328.80 3.72 2015/11/04 O O O O O O O

H -012.00 IBF TRANSITION DUCT & FRAME, RHS 11.3 328.80 3.72 2015/11/04 O O O O O O O

H -013.00 AIR INLET ASSEMBLY, ENGINE, LHS 70302-101... 38.3 338.00 12.95 X 2015/11/04 I I I I I I I

H -014.00AIR INLET ASSEMBLY, ENGINE, (W/ ICE DETECTOR), RHS 70302-10100 40.3 338.00 13.62 X 2015/11/04 I I I I I I I

H -015.00 MAIN ROTOR BLADES (4 EA) 70150-09100 844.0 341.00 287.80 X 2015/11/04 I I I I I I I

H -016.00DISTRIBUTOR BOX, BLADE DE-ICE W/SLIP RING 70550-02127 & 70550-02128 24.0 341.00 8.18 X 2015/11/04 I I I I I I I

H -017.00 CARGO DOOR ASSEMBLY, LHS 70217-02701 43.0 344.00 14.79 X 2015/11/04 I I I I I I I

H -018.00 CARGO DOOR ASSEMBLY, RHS 70217-02701 43.0 344.00 14.79 X 2015/11/04 I I I I I I I

H -019.00 CARGO HOOK 70800-02503 22.0 353.00 7.77 X 2015/11/04 I I I I I I I

H -020.00TRANSMITTER, IR JAMMER AN/ALQ-144A(V) NSN-5865-01-323-4999 25.6 400.00 10.24 2015/11/04 O O O O O O O

H -021.00 HIRSS ASSEMBLY W/O BAFFLE, LHS 70308-03... 111.0 420.00 46.62 X 2015/11/04 I I I I I I I

H -022.00HIRSS ASSEMBLY W/O BAFFLE, RHS 70308-03610 110.0 420.00 46.20 X 2015/11/04 I I I I I I I

H -023.00 HIRSS BAFFLE, LHS 70308-03801 15.3 420.00 6.43 X 2015/11/04 I I I I I I I

H -024.00 HIRSS BAFFLE, RHS 70308-03801 15.3 420.00 6.43 X 2015/11/04 I I I I I I I

H -025.00 SATCOM ANTENNA 19-430-10P 7.0 432.00 3.02 2015/11/04 O O O O O O O

H -026.00 TROOP COMMANDERS ANTENNA 9-33-26 2.0 460.00 0.92 X 2015/11/04 I I I I I I I

H -027.00 L-BAND ANTENNA W/MOUNT (BFT) 301 3.2 475.00 1.52 X 2015/11/04 I I I I I I O

H -028.00ICMD #1 (CHAFF) DISPENSER, LHS D-61/ALQ-212(V) NSN-1095-01-457-9426 4.9 505.00 2.47 2015/11/04 O O O O O O O

H -029.00ICMD #1 (CHAFF) PAYLOAD MODULE, LHS D-61/ALQ-212(V) 3.6 505.00 1.82 2015/11/04 O O O O O O O

H -030.00ICMD #2 (FLARE) DISPENSER W/CABLE, RHS D-61/ALQ-212(V) 4.9 515.00 2.52 2015/11/04 O O O O O O O

H -031.00ICMD #2 (FLARE) PAYLOAD MODULE, RHS D-61/ALQ-212(V) 3.6 515.00 1.85 2015/11/04 O O O O O O O

H -032.00 HF ANTENNA 4700516-10 7.0 528.00 3.70 X 2015/11/04 I I I I I I I

H -033.00ICMD #3 (FLARE) DISPENSER W/CABLE, LHS D-61/ALQ-212(V) 4.9 535.00 2.62 2015/11/04 O O O O O O O

2015/12/16 AWBS 10.0 Page 13 of 13

CHART A - BASIC WEIGHT CHECKLIST RECORDCOMPARTMENT: H - EXTERNAL EQUIPMENT STA 0 - 770





(lb)

Long. Arm (in)

Long. Mom.

(lb-in)In

A/CMan. Inv. Date

151104

140820

130820

120829

110913

110802

110308

H -034.00ICMD #3 (FLARE) PAYLOAD MODULE, LHS D-61/ALQ-212(V) 3.6 535.00 1.93 2015/11/04 O O O O O O O

H -035.00 TAIL ROTOR BLADES (2 EA) 70101-31000-043 79.4 732.00 58.12 X 2015/11/04 I I I I I I I

H -036.00 EOMS, AFT RHS SU-202/AAR-57(V) 2.8 732.20 2.05 2015/11/04 O O O O O O O

H -037.00 EOMS, AFT LHS SU-202/AAR-57(V) 2.8 734.60 2.06 2015/11/04 O O O O O O O

H -038.00 HORIZONTAL STORES SUPPORT STRUCTURE 0.1 2015/11/04 O O O O O O O

H -039.00HORIZONTAL STORES SUPPORT ASSEMBLY W/FAIRINGS, LHS 70200-42400 202.0 305.00 61.61 2015/11/04 O O O O O O O

H -040.00HORIZONTAL STORES SUPPORT ASSEMBLY W/FAIRINGS, RHS 70200-42400 202.0 305.00 61.61 2015/11/04 O O O O O O O

H -041.00 HORIZONTAL STORES STRUTS AND FAIRINGS 0.1 2015/11/04 O O O O O O O

H -042.00SUPPORT STRUTS AND FAIRINGS ASSEMBLY, LHS 70219-42430 28.0 302.00 8.46 2015/11/04 O O O O O O O

H -043.00SUPPORT STRUTS AND FAIRINGS ASSEMBLY, RHS 70219-42430 28.0 302.00 8.46 2015/11/04 O O O O O O O

H -044.00 VERTICAL STORES PYLON BL 80 0.1 2015/11/04 O O O O O O O

H -045.00RACK ATTACHMENT FITTING (BL 80), LHS 70219-42412 25.0 316.00 7.90 2015/11/04 O O O O O O O

H -046.00RACK ATTACHMENT FITTING (BL 80), RHS 70219-42412 25.0 316.00 7.90 2015/11/04 O O O O O O O

H -047.00PYLON FAIRING ASSEMBLY (BL 80), LHS 70215-42407 8.0 316.00 2.53 2015/11/04 O O O O O O O

H -048.00PYLON FAIRING ASSEMBLY (BL 80), RHS 70215-42407 8.0 316.00 2.53 2015/11/04 O O O O O O O

H -049.0014" BOMB RACK & HARDWARE ASSEMBLY (BL 80, LHS (230 GAL) 70200-42400 18.0 316.00 5.69 2015/11/04 O O O O O O O

H -050.0014" BOMB RACK & HARDWARE ASSEMBLY (BL 80), RHS (230 GAL) 70200-42400 18.0 316.00 5.69 2015/11/04 O O O O O O O

H -051.0030" BOMB RACK & HARDWARE ASSEMBLY (BL 80), LHS (450 GAL) 70200-42400 65.0 316.00 20.54 2015/11/04 O O O O O O O

H -052.0030" BOMB RACK & HARDWARE ASSEMBLY (BL 80, RHS (450 GAL) 70200-42400 65.0 316.00 20.54 2015/11/04 O O O O O O O

H -053.00 VERTICAL STORES PYLON, BL 112 0.1 2015/11/04 O O O O O O O

H -054.00RACK ATTACHMENT FITTING (BL 112), LHS 70219-42412 25.0 316.00 7.90 2015/11/04 O O O O O O O

H -055.00RACK ATTACHMENT FITTING (BL 112), RHS 70219-42412 25.0 316.00 7.90 2015/11/04 O O O O O O O

H -056.00PYLON FAIRING ASSEMBLY (BL 112), LHS 70215-42407 10.0 316.00 3.16 2015/11/04 O O O O O O O

H -057.00PYLON FAIRING ASSEMBLY (BL 112), RHS 70215-42407 10.0 316.00 3.16 2015/11/04 O O O O O O O

H -058.0014" BOMB RACK & HARDWARE ASSEMBLY (BL 112), LHS (230 GAL) 70200-42400 18.0 316.00 5.69 2015/11/04 O O O O O O O

H -059.0014" BOMB RACK & HARDWARE ASSEMBLY (BL 112), RHS (230 GAL) 70200-42400 18.0 316.00 5.69 2015/11/04 O O O O O O O

2015/12/16 AWBS 10.0 Page 1 of 11S = Chart C Review W = WeighingA = Addition R = RemovalH = Header I = Inventory

CHART C - BASIC WEIGHT AND BALANCE RECORDMDS: UH-60A SERIAL NO: 79-23273 CONSTANT: 1,000

Date Act. Item No. Description Weight (lb)

Long. Arm (in)

Long. Mom.

(lb-in)

Basic Weight

(lb)

Basic Long. Arm (in)

Basic Long. Mom.

(lb-in)

1995/03/14 A B -026.00 APN-209 RCVR/XMSN INDICATOR 4.0 208.00 0.83 10,889.0 359.52 3,914.87

1995/03/14 R B -044.00 COMM. SECURITY CONTROL KY-58 RHS 1.0 225.00 0.23 10,888.0 359.54 3,914.64

1995/03/14 A B -067.00 MOUNT,REVERSIBLE,ARC-186/201 3.0 223.00 0.67 10,891.0 359.50 3,915.31

1995/03/14 A B -068.00 MOUNT,REVERSIBLE,ARC-186/201 3.0 229.00 0.69 10,894.0 359.46 3,916.00

1995/03/14 A B -069.00 MOUNT,MT-6051 ARC-186 1.0 234.00 0.23 10,895.0 359.45 3,916.23

1995/03/14 A B -070.00 CONTROL C-10604 ARC-186 3.0 227.00 0.68 10,898.0 359.42 3,916.91

1995/03/14 A B -071.00 CONTROL C-10604 ARC-186 3.0 229.00 0.69 10,901.0 359.38 3,917.60

1995/03/14 A B -072.00 RADIO SET RT-1300/ARC-186 7.0 229.00 1.60 10,908.0 359.30 3,919.20

1995/03/14 A B -073.00 RADIO SET RT-1300/ARC-186 7.0 234.00 1.64 10,915.0 359.22 3,920.84

1995/03/14 A B -074.00 REMOTE FILL KY-58 1.0 214.00 0.21 10,916.0 359.20 3,921.05

1995/03/14 A C -024.00 MOUNT SUPPORT M60D 20.0 270.00 5.40 10,936.0 359.04 3,926.45

1995/03/14 A C -025.00 MWO 1-1520-237-50-59 EME PROTECT 29.0 254.30 7.37 10,965.0 358.76 3,933.83

1995/03/14 A C -026.00 MWO 55-1520-237-50-70 HEATED W/S 12.0 254.50 3.05 10,977.0 358.65 3,936.88

1995/03/14 A D -027.00 MWO 1-1520-237-55-7 REFURB KIT 52.0 301.10 15.66 11,029.0 358.38 3,952.54

1995/03/14 A D -029.00 MWO 55-1520-237-50-66 IMP F/EXT C 3.0 337.20 1.01 11,032.0 358.37 3,953.55

1995/03/14 A D -030.00 MWO 1-1520-237-50-69 SINCGARS WIR 16.0 306.00 4.90 11,048.0 358.30 3,958.45

1995/03/14 A F -032.00 MWO 1-1520-237-50-63 HIRSS FIX PV 5.0 413.00 2.07 11,053.0 358.32 3,960.51

1995/03/14 A F -033.00 MOUNTING #1FM,MT-6592/ARC-201 2.0 476.00 0.95 11,055.0 358.34 3,961.46

1995/03/14 A F -036.00 SHELF AND BYPASS, #1FM 2.0 476.00 0.95 11,057.0 358.36 3,962.42

1995/03/14 A H -055.00 WIRE STRIKE MOD KIT,237-50-24 4.0 247.40 0.99 11,061.0 358.32 3,963.41

1995/03/14 A H -056.00 WIRE STRIKE MOD KIT,237-50-47 31.0 279.60 8.67 11,092.0 358.10 3,972.07

1995/03/14 A H -057.00 MWO ANTI FLAP 1.0 341.00 0.34 11,093.0 358.10 3,972.41

1995/03/14 A H -058.00 STAB ACT GROUNDING STRAP MWO 1.0 708.00 0.71 11,094.0 358.13 3,973.12

1995/03/14 A H -059.00 MOUNT, ANTENNA 1.0 752.00 0.75 11,095.0 358.17 3,973.87

1995/03/14 A H -060.00ANTENNA, VHF/FM, AS-4153/ARC WITH COUPLER, CU-2457/ARC 1.0 752.00 0.75 11,096.0 358.20 3,974.63

1995/03/14 A D -028.00 MWO 55-1520-237-50-43 DOWEL PIN 0.0 339.60 0.00 11,096.0 358.20 3,974.63

1995/03/14 R A -030.00 MOUNTING, LHS S1660-60036-1 1.0 190.00 0.19 11,095.0 358.22 3,974.44

1995/03/14 R A -034.00 MOUNTING, CENTER, S1660-60036-1 1.0 190.00 0.19 11,094.0 358.23 3,974.25

1995/03/14 R A -037.00 ADAPTER, RHS FOR KY-58 Z-AHQ 4.0 190.00 0.76 11,090.0 358.30 3,973.49

1995/03/14 R A -038.00 MOUNTING, RHS, S1660-60036-1 1.0 190.00 0.19 11,089.0 358.31 3,973.30

1995/03/14 R C -023.00 TROOP SEAT & BELTS 16.0 282.00 4.51 11,073.0 358.42 3,968.78

1995/03/14 R D -021.00 TROOP SEAT & BELTS 16.0 338.00 5.41 11,057.0 358.45 3,963.38

1995/03/14 R B -046.00 RCVR-XMTTR CONTROL 7.0 227.00 1.59 11,050.0 358.53 3,961.79

1995/03/14 R B -049.00 VHF/FM RADIO ARC-114 7.0 228.00 1.60 11,043.0 358.62 3,960.19

1995/03/14 R B -051.00 VHF/AM RADIO ARC-115 7.0 232.00 1.62 11,036.0 358.70 3,958.57

1995/03/14 A G -050.00 RADIATOR WET 23.0 399.00 9.18 11,059.0 358.78 3,967.74

1995/03/14 A H -039.00 ANTENNA, UHF/AM 3.0 454.00 1.36 11,062.0 358.80 3,969.11

1995/03/14 A H -040.00 FAIRING ASSY-CENTER MRP 5.0 492.00 2.46 11,067.0 358.87 3,971.57

1995/03/14 A H -041.00 FAIRING ASSY-CENTER IR KIT 11.0 500.00 5.50 11,078.0 359.01 3,977.07

1995/03/14 ICALCULATED WEIGHT & MOMENT AS PER950314 INVENTORY (C.C.A.D. ) 11,078.0 359.01 3,977.07

1995/03/14 W BASIC A/C, WEIGHED AT: C.C.A.D 11,134.0 359.54 4,003.07 11,134.0 359.54 4,003.07

1995/03/14 I ANNUAL REVIEW & INVENTORY COMP 11,134.0 359.54 4,003.07

1995/12/26 A C -027.00 SURVIVAL KIT 28.0 282.00 7.90 11,162.0 359.34 4,010.97

1995/12/26 A C -028.00 SURVIVAL KIT 28.0 282.00 7.90 11,190.0 359.15 4,018.86




Long. Arm (in)

Long. Mom.

(lb-in)

Basic Weight

(lb)


Basic Long. Mom.

(lb-in)

1995/12/26 A C -029.00 SURVIVAL KIT 28.0 282.00 7.90 11,218.0 358.95 4,026.76

1995/12/26 A F -037.00 AIRCRAFT TIEDOWN KIT 45.0 420.80 18.94 11,263.0 359.20 4,045.69

1996/05/09 A A -002.00 COMPUTER KIT 1C 11.0 176.00 1.94 11,274.0 359.02 4,047.63

1996/05/09 A A -032.00 SECURITY SET, CENTER KY-58 9.0 190.00 1.71 11,283.0 358.89 4,049.34

1996/05/09 A B -043.00 COMM. SECURITY CONTROL KY-58 CNT 2.0 224.00 0.45 11,285.0 358.86 4,049.79

1996/09/10 R B -026.00 APN-209 RCVR/XMSN INDICATOR 4.0 208.00 0.83 11,281.0 358.92 4,048.96

1996/03/14 ICALCULATED WEIGHT & MOMENT AS PERANNUAL INVENTORY (AASF #1 KS) 11,281.0 358.92 4,048.96

1997/03/18 A B -026.00 APN-209 RCVR/XMSN INDICATOR 4.0 208.00 0.83 11,285.0 358.86 4,049.79

1997/03/18 A B -052.00 VHF/AM/FM RADIO ARC-186 7.0 232.00 1.62 11,292.0 358.79 4,051.41

1997/03/18 A B -061.00 CONTROL EXTENDED RANGE KIT 10.0 240.00 2.40 11,302.0 358.68 4,053.81

1997/03/18 A B -062.00 CONTROL RESCUE HOIST KIT RHS 2.0 240.00 0.48 11,304.0 358.66 4,054.29

1997/03/14 ICALCULATED WEIGHT & MOMENT AS PERANNUAL INVENTORY (AASF#1, KS) 11,304.0 358.66 4,054.29

1997/03/14 W BASIC A/C, WEIGHED AT: AASF#1, KS 11,099.0 359.05 3,985.07 11,099.0 359.05 3,985.07

1997/04/09 H MWO 1-1520-237-50-62 APPLIED

1997/04/09 A AA -040.00 THERMOCOUPLE AMPLIFIER EA-2 1.0 183.60 0.18 11,100.0 359.03 3,985.26

1997/04/09 A AN/AVS-7 HUDS INSTALLATION 18.0 203.90 3.67 11,118.0 358.78 3,988.93

1997/04/09 A MWO 1-1520-237-50-74 APPLIED 3.0 391.10 1.17 11,121.0 358.79 3,990.10

1997/10/28 R F -037.00 AIRCRAFT TIEDOWN KIT 45.0 420.80 18.94 11,076.0 358.54 3,971.17

1997/10/28 A F -037.00 ACFT TIEDOWN/SPILL KIT 90.0 420.80 37.87 11,166.0 359.04 4,009.04

1998/03/25 ICALCULATED WEIGHT & MOMENT AS PER12 MONTH INVENTORY (AASF#2, KS) 11,166.0 359.04 4,009.04

1999/03/10 W BASIC A/C, WEIGHED AT: SALINA, KS 11,293.0 358.38 4,047.13 11,293.0 358.38 4,047.13

1999/03/10 I DD 365-1 INVENTORY COMPLETED 11,293.0 358.38 4,047.13

1999/03/10 ICalculated weight and moment as per 12 Month Inventory completed at (AASF#2, KS) 11,293.0 358.38 4,047.13

2000/03/04 ICalculated weight and moment as per 12 Month Inventory completed at (AASF#2, KS) 11,293.0 358.38 4,047.13

2000/08/30 R A -001.00LOWER SHELF CIS PROCESSOR 70600-01038-103 5.0 175.00 0.88 11,288.0 358.46 4,046.26

2000/08/30 R A -004.00SIGNAL DATA CONVERTER CV-3338/ASN-128 12.0 177.00 2.12 11,276.0 358.65 4,044.13

2000/08/30 R B -037.00 DOPPLER CONTROL PANEL 7.0 216.00 1.51 11,269.0 358.74 4,042.62

2000/08/30 R ICS/STORAGE BOX 1.0 247.00 0.25 11,268.0 358.75 4,042.37

2000/08/30 HMWO 1-1520-237-50-75 INSTALLATION OF THE AN/ASN-128B DOPPLER/GPS NAVIGATION SYST...

2000/08/30 A A -001.01 DIGITAL CIP PROCESSOR CP20236A 5.0 175.00 0.88 11,273.0 358.67 4,043.25

2000/08/30 A A -004.01 SIGNAL DATA CONVERTER CV-3338/ASN-128 12.0 177.00 2.12 11,285.0 358.47 4,045.37

2000/08/30 A GPS REMOTE FILL PROCESSOR 0.5 214.00 0.11 11,285.5 358.47 4,045.48

2000/08/30 A ZERIOIZE SWITCH ASSEMBLY 0.5 238.00 0.12 11,286.0 358.46 4,045.60

2000/08/30 A B -037.01DOPPLER/GPS CONTROL PANEL CP1252C/ASN 128B 7.0 216.00 1.51 11,293.0 358.37 4,047.11

2000/08/30 A ASN-128B SYSTEM WIRING 9.0 220.00 1.98 11,302.0 358.26 4,049.09

2000/08/30 A ENCLOSURE DATA LOAD/ICS 1.5 247.00 0.37 11,303.5 358.25 4,049.46

2000/08/30 A DATA LOADER RECEPTACLE 1.0 250.00 0.25 11,304.5 358.24 4,049.71

2000/08/30 A GPS ANTENNA PROVISION 1.0 460.00 0.46 11,305.5 358.25 4,050.17

2000/08/30 A GPS ANTENNA 0.7 460.00 0.32 11,306.2 358.25 4,050.49




Long. Arm (in)

Long. Mom.

(lb-in)

Basic Weight

(lb)


Basic Long. Mom.

(lb-in)

2000/08/30 A MWO 1-1520-237-50-56 6.4 187.50 1.20 11,312.6 358.16 4,051.69

2002/01/29 A B -050.00 CONTROL, CHAFF DISPENSER 1.0 231.00 0.23 11,313.6 358.15 4,051.92

2002/01/29 ICalculated Weight and Moment per Inventory Completed at AASF#2, KS 11,313.6 358.15 4,051.92

2001/03/29 W BASIC A/C, WEIGHED AT : SALINA, KS 11,378.0 358.17 4,075.29 11,378.0 358.17 4,075.29

2001/08/14 H MWO 1-1520-237-50-76 HF AN/ARC-220

2001/08/14 A B -079.00 MAIN TERMINAL (KY-100) 6.0 247.50 1.49 11,384.0 358.11 4,076.78

2001/08/14 A B -080.00 CONTROL DISPLAY UNIT C-12436/VRC 5.0 244.00 1.22 11,389.0 358.06 4,078.00

2001/08/14 A B -081.00 CONSOLE EXTENSION 6.0 247.00 1.48 11,395.0 358.01 4,079.48

2001/08/14 A F -038.00 BATTERY BOX CY 85151/ARC 2.0 475.00 0.95 11,397.0 358.03 4,080.43

2001/08/14 A F -039.00 HF RECEIVER TRANSMITTER RT-1749/VRC 13.0 475.00 6.18 11,410.0 358.16 4,086.60

2001/08/14 A F -040.00 MOUNT HF R/T 2.0 475.00 0.95 11,412.0 358.18 4,087.55

2001/08/14 A F -041.00 HF AMPLIFIER COUPLER AM-7531/VRC 19.0 475.00 9.03 11,431.0 358.37 4,096.58

2001/08/14 A F -042.00 MOUNT HF AMPLIFIER COUPLER 3.0 475.00 1.43 11,434.0 358.41 4,098.00

2001/08/14 A F -043.00 SHELF TRANSITION 6.0 475.00 2.85 11,440.0 358.47 4,100.85

2001/08/14 A HF AN/ARC-220 WIRING AND STRUCTURE 33.2 403.60 13.40 11,473.2 358.60 4,114.25

2001/08/14 R SHELF ASSY IFM 4.0 473.00 1.89 11,469.2 358.56 4,112.36

2001/08/14 A H -062.00 HF ANTENNA 7.0 528.00 3.70 11,476.2 358.66 4,116.06

2001/10/10 A F -034.00 AMPLIFIER, #1FM, AN-7189A/ARC 10.0 476.00 4.76 11,486.2 358.76 4,120.82

2002/03/26 ICalculated Weight and Moment per Inventory Completed at SALINA, KS 11,486.2 358.76 4,120.82

2002/11/15 HMWO 1-1520-237-50-77 INSTALLATION OF THE SEALED LEAD ACID BATTERY AND RELOCATION OF THE UTILITY LIGHT POWER

2003/02/15 R B -065.00 BATTERY CHARGER/ANALYZER 4.0 243.00 0.97 11,482.2 358.80 4,119.84

2003/02/15 R C -009.00 BATTERY 17.0 252.00 4.28 11,465.2 358.96 4,115.56

2003/02/15 R C -010.00 BATTERY COVER 2.0 252.00 0.50 11,463.2 358.98 4,115.06

2003/02/15 A C -009.00 BATTERY D8565/11-1 35.0 252.00 8.82 11,498.2 358.65 4,123.88

2003/02/15 A C -010.00 BATTERY COVER 70209-02532-044 2.0 252.00 0.50 11,500.2 358.64 4,124.38

2003/02/15 A C -010.01 BATTERY JUNCTION BOX ASSY 70550-02212-041 2.0 252.00 0.50 11,502.2 358.62 4,124.88



2005/01/21 R A -025.00 ANTENNA AS-2891/APR-39 RHS 1.0 165.00 0.17 11,501.2 358.63 4,124.72

2005/01/21 R A -032.00 SECURITY SET, CENTER KY-58 9.0 190.00 1.71 11,492.2 358.77 4,123.01


2005/01/21 A A -036.00 SECURITY SET, RHS KY-58 5.0 190.00 0.95 11,502.2 358.62 4,124.91

2005/03/10 A B -044.00 COMM. SECURITY CONTROL KY-58 RHS 2.0 225.00 0.45 11,504.2 358.60 4,125.36

2005/03/10 A A -025.00 ANTENNA AS-2891/APR-39 RHS 1.0 165.00 0.17 11,505.2 358.58 4,125.52



2005/07/29 A B -076.00 VHF-FM RADIO, RT-1477/ARC-201 7.0 229.00 1.60 11,692.0 360.16 4,210.96

2005/07/29 A B -078.00 CONTROL PANEL, C-11466A/ARC-201 3.0 227.00 0.68 11,695.0 360.12 4,211.64

2006/01/04 R A -002.00 COMPUTER KIT 1C 11.0 176.00 1.94 11,684.0 360.30 4,209.71

2006/01/04 R A -032.00 SECURITY SET, CENTER KY-58 5.0 190.00 0.95 11,679.0 360.37 4,208.76




Long. Arm (in)

Long. Mom.

(lb-in)

Basic Weight

(lb)


Basic Long. Mom.

(lb-in)

2006/01/04 R A -036.00 SECURITY SET, RHS KY-58 5.0 190.00 0.95 11,674.0 360.44 4,207.81

2006/01/04 R B -021.00 IRCM PANEL AN/ALQ-144 1.0 207.00 0.21 11,673.0 360.46 4,207.60

2006/01/04 R B -043.00 COMM. SECURITY CONTROL KY-58 CNT 2.0 224.00 0.45 11,671.0 360.48 4,207.15

2006/01/04 R B -044.00 COMM. SECURITY CONTROL KY-58 RHS 2.0 225.00 0.45 11,669.0 360.50 4,206.70

2006/01/04 R B -050.00 CONTROL, CHAFF DISPENSER 1.0 231.00 0.23 11,668.0 360.51 4,206.47

2006/01/04 R B -079.00 MAIN TERMINAL (KY-100) 6.0 247.50 1.49 11,662.0 360.57 4,204.99

2006/01/04 R C -029.00 AMSS Kit 65.0 282.00 18.33 11,597.0 361.01 4,186.66

2006/01/04 R D -012.00 TROOP SEAT & BELTS LHS 16.0 322.00 5.15 11,581.0 361.07 4,181.50

2006/01/04 R D -013.00 TROOP SEATS & BELTS CENTER 16.0 322.00 5.15 11,565.0 361.12 4,176.35

2006/01/04 R D -014.00 TROOP SEAT & BELTS RHS 16.0 322.00 5.15 11,549.0 361.17 4,171.20

2006/01/04 R D -018.00 TROOP SEAT & BELTS LHS 16.0 338.00 5.41 11,533.0 361.21 4,165.79

2006/01/04 R D -019.00 TROOP SEAT & BELTS CENTER 16.0 338.00 5.41 11,517.0 361.24 4,160.38

2006/01/04 R D -020.00 TROOP SEAT & BELTS RHS 16.0 338.00 5.41 11,501.0 361.27 4,154.98

2006/01/04 R H -030.00 TRANSMITTER, IR JAMMER ALQ-144 28.0 400.00 11.20 11,473.0 361.18 4,143.78

2006/01/04 R E -016.00 TROOP SEATS & BELTS LHS 16.0 392.00 6.27 11,457.0 361.13 4,137.50

2006/01/04 R E -017.00 TROOP SEATS & BELTS LHS 16.0 392.00 6.27 11,441.0 361.09 4,131.23

2006/01/04 R E -018.00 TROOP SEATS & BELTS RHS 16.0 392.00 6.27 11,425.0 361.05 4,124.96

2006/01/04 R E -019.00 TROOP SEATS & BELTS RHS 16.0 392.00 6.27 11,409.0 361.00 4,118.69

2006/02/14 H MWO 1-1520-237-50-CMWS

2006/02/14 R H -047.00 ANTENNA-TROOP COMMANDER 2.0 739.00 1.48 11,407.0 360.94 4,117.21

2006/02/14 A H -065.00 TROOP COMMANDERS ANTENNA A100740-101 2.0 460.00 0.92 11,409.0 360.95 4,118.13

2006/02/14 A EOMS SENSORS STRUCTURE, FWD A100632-101 3.0 174.00 0.52 11,412.0 360.91 4,118.65

2006/02/14 A CMWS RELAY BOX A100695 3.0 225.00 0.68 11,415.0 360.87 4,119.33

2006/02/14 ACMWS AUXILLIARY CIRCUIT BREAKER PANEL A100680 2.0 232.00 0.46 11,417.0 360.85 4,119.79

2006/02/14 ACMWS SAFETY SWITCH ASSEMBLY SA-2671/ALE(V) A100693 1.0 292.00 0.29 11,418.0 360.84 4,120.08

2006/02/14 A CMWS WIRE HARNESS INSTALLATION A100601-1... 43.0 360.00 15.48 11,461.0 360.84 4,135.56

2006/02/14 ACMWS ELECTRONIC CONTROL UNIT STUCTURE A100631 3.0 371.00 1.11 11,464.0 360.84 4,136.68

2006/02/14 A CMWS TERMINAL JUNCTION BOX A100696 3.0 385.00 1.16 11,467.0 360.85 4,137.83

2006/02/14 A TROOP COMMANDERS ANTENNA MOUNT A100743 1.0 460.00 0.46 11,468.0 360.86 4,138.29

2006/02/14 AICMD #1 (CHAFF) DISPENSER STRUCTURE, LHS A100674 1.0 505.00 0.51 11,469.0 360.87 4,138.80

2006/02/14 AICMD#2 (FLARE) DISPENSER STRUCTURE, RHS A100665 7.0 515.00 3.61 11,476.0 360.96 4,142.40

2006/02/14 AICMD #3 (FLARE) DISPENSER STRUCTURE, LHS A100651 7.0 535.00 3.75 11,483.0 361.07 4,146.15

2006/02/14 H MWO 1-1520-237-50-BFT2

2006/02/14 A BFT STRUCTURAL INSTALLATION 5.0 237.00 1.19 11,488.0 361.01 4,147.33

2006/02/14 A BFT WIRE HARNESS INSTALLATION 19.9 325.00 6.47 11,507.9 360.95 4,153.80

2006/02/14 A BFT LNA INSTALLATION 2.6 470.00 1.22 11,510.5 360.98 4,155.02

2006/02/14 A GPS ANTENNA MOUNT INSTALLATION 1.0 472.00 0.47 11,511.5 360.99 4,155.49

2006/02/14 A EIS (L-BAND) ANTENNA MOUNT INSTALLATION 1.6 475.00 0.76 11,513.1 361.00 4,156.25

2006/02/14 A H -074.00 GPS ANTENNA (BFT) 0.2 472.00 0.09 11,513.3 361.00 4,156.35

2006/02/14 A H -075.00 EIS (L-BAND) ANTENNA (BFT) 1.4 475.00 0.67 11,514.7 361.02 4,157.01

2006/02/14 R H -074.00 GPS ANTENNA (BFT) 0.2 472.00 0.09 11,514.5 361.02 4,156.92




Long. Arm (in)

Long. Mom.

(lb-in)

Basic Weight

(lb)


Basic Long. Mom.

(lb-in)

2006/02/14 A H -074.00 GPS ANTENNA (BFT) S67-1575-86 0.2 472.00 0.09 11,514.7 361.02 4,157.01

2006/02/14 R H -075.00 EIS (L-BAND) ANTENNA (BFT) 1.4 475.00 0.67 11,513.3 361.00 4,156.35

2006/02/14 A H -075.00 EIS (L-BAND) ANTENNA (BFT) S65-8282-301 1.4 475.00 0.67 11,514.7 361.02 4,157.01

2006/02/14 H MWO 1-1520-237-50-85

2006/02/14 APROVISIONS FOR MICROCLIMATE COOLING SYSTEM 7.5 250.00 1.88 11,522.2 360.95 4,158.89

2006/02/14 A C -034.00 CREWMEMBER HOSES 5.0 270.00 1.35 11,527.2 360.91 4,160.24

2006/02/14 A C -035.00 MCU MOUNT ASSEMBLY 19.0 260.00 4.94 11,546.2 360.74 4,165.18

2006/02/14 A B -085.00 PILOT AND COPILOT HOSES 5.0 240.00 1.20 11,551.2 360.69 4,166.38

2006/02/14 H MWO 1-1520-237-50-84

2006/02/14 A ELECTRICAL CABLES 4.5 211.00 0.95 11,555.7 360.63 4,167.33

2006/02/14 A A -041.00 IFF TRANSPONDER P/N 1008939G-5 10.8 176.00 1.90 11,566.5 360.46 4,169.23

2006/02/14 A A -042.00 TRANSPONDER MOUNT 1.5 176.00 0.26 11,568.0 360.43 4,169.49

2006/02/14 A B -086.00 RCU P/N 1008940P-4 3.0 227.00 0.68 11,571.0 360.40 4,170.17

2006/02/14 HAPU INLET BARRIER FILTER SYSTEM INSTALLATION

2006/02/14 A AIBF INLET BARRIER FILTER SYSTEM 6.0 433.00 2.60 11,577.0 360.44 4,172.77

2006/02/14 H MWO 1-1520-237-50-90

2006/02/14 A EIBF A-KIT COMPONENTS 16.0 178.00 2.85 11,593.0 360.18 4,175.62

2006/02/14 H MWO 1-1520-237-50-EDM

2006/02/14 A WIRING INSTALLATION 4.0 237.00 0.95 11,597.0 360.14 4,176.57

2006/02/14 A B -087.00DC-DC POWER CONVERTER (P/N: 143-1075-003) (EDM) 2.0 237.00 0.47 11,599.0 360.12 4,177.04

2006/02/16 R A -003.00 MOUNTING MT-3949A/U 2.0 176.00 0.35 11,597.0 360.15 4,176.69

2006/02/16 R Chaff/Flare Despencer Assembly 16.0 505.00 8.08 11,581.0 359.95 4,168.61

2006/02/16 R IFF Transponder AN/APX-100 6.0 227.00 1.36 11,575.0 360.02 4,167.25

2006/02/16 R Electrical Cables AN/APX-100 4.5 211.00 0.95 11,570.5 360.08 4,166.30

2006/03/08 A D -021.00 TROOP SEAT & BELTS (ALT) 16.0 338.00 5.41 11,586.5 360.05 4,171.70

2006/03/08 A D -020.00 TROOP SEAT & BELTS RHS 16.0 338.00 5.41 11,602.5 360.02 4,177.11

2006/03/08 A D -019.00 TROOP SEAT & BELTS CENTER 16.0 338.00 5.41 11,618.5 359.99 4,182.52

2006/03/08 A D -018.00 TROOP SEAT & BELTS LHS 16.0 338.00 5.41 11,634.5 359.96 4,187.93

2006/03/08 A D -012.00 TROOP SEAT & BELTS LHS 16.0 322.00 5.15 11,650.5 359.91 4,193.08

2006/03/08 A D -013.00 TROOP SEATS & BELTS CENTER 16.0 322.00 5.15 11,666.5 359.85 4,198.23

2006/03/08 A D -014.00 TROOP SEAT & BELTS RHS 16.0 322.00 5.15 11,682.5 359.80 4,203.38

2006/03/08 R C -014.01 FIRE EXT CO2 P/N A 52471-1-S 10.0 263.00 2.63 11,672.5 359.88 4,200.75

2006/03/08 A C -014.00 FIRE EXTINGUISHER 8.0 263.00 2.10 11,680.5 359.82 4,202.86

2006/03/08 R B -063.01 FIRE EXT CO2 P/N A 52471-1-S 10.0 243.00 2.43 11,670.5 359.92 4,200.43

2006/03/08 A B -063.00 FIRE EXTINGUISHER 8.0 243.00 1.94 11,678.5 359.84 4,202.37


2006/03/08 A A -036.00 SECURITY SET, RHS KY-58 5.0 190.00 0.95 11,688.5 359.69 4,204.27

2006/03/08 A B -021.00 IRCM PANEL AN/ALQ-144 1.0 207.00 0.21 11,689.5 359.68 4,204.48

2006/03/08 A B -043.00 COMM. SECURITY CONTROL KY-58 CNT 2.0 224.00 0.45 11,691.5 359.66 4,204.93

2006/03/08 A B -044.00 COMM. SECURITY CONTROL KY-58 RHS 2.0 225.00 0.45 11,693.5 359.63 4,205.38

2006/03/08 R B -070.00 CONTROL C-10604 ARC-186 3.0 227.00 0.68 11,690.5 359.67 4,204.70

2006/03/08 R B -072.00 RADIO SET RT-1300/ARC-186 7.0 229.00 1.60 11,683.5 359.75 4,203.09

2006/03/08 A B -079.00 MAIN TERMINAL (KY-100) 6.0 247.50 1.49 11,689.5 359.69 4,204.58




Long. Arm (in)

Long. Mom.

(lb-in)

Basic Weight

(lb)


Basic Long. Mom.

(lb-in)

2006/03/08 R C -013.00 TROOP SEATS AND BELTS 16.0 262.00 4.19 11,673.5 359.82 4,200.39

2006/03/08 A C -013.00 TROOP SEATS AND BELTS 16.0 262.00 4.19 11,689.5 359.69 4,204.58

2006/03/08 A C -029.00 AMSS Kit 65.0 282.00 18.33 11,754.5 359.26 4,222.91

2006/03/08 A E -016.00 TROOP SEATS & BELTS LHS 16.0 392.00 6.27 11,770.5 359.30 4,229.18

2006/03/08 A E -017.00 TROOP SEATS & BELTS LHS 16.0 392.00 6.27 11,786.5 359.35 4,235.45

2006/03/08 A E -018.00 TROOP SEATS & BELTS RHS 16.0 392.00 6.27 11,802.5 359.39 4,241.72

2006/03/08 A E -019.00 TROOP SEATS & BELTS RHS 16.0 392.00 6.27 11,818.5 359.44 4,248.00

2006/03/08 R F -037.00 ACFT TIEDOWN 81.5 420.80 34.30 11,737.0 359.01 4,213.70

2006/03/08 A H -030.00 TRANSMITTER, IR JAMMER ALQ-144 28.0 400.00 11.20 11,765.0 359.11 4,224.90

2006/03/08 A H -033.00 CENTER BODY, TAIL PIPE LHS 2.0 402.00 0.80 11,767.0 359.11 4,225.71

2006/03/08 A H -034.00 CENTER BODY, TAIL PIPE RHS 2.0 402.00 0.80 11,769.0 359.12 4,226.51

2006/03/08 A H -035.00 EXHAUST MODULE, LHS 29.0 419.00 12.15 11,798.0 359.27 4,238.66

2006/03/08 A H -036.00 EXHAUST MODULE, RHS 29.0 419.00 12.15 11,827.0 359.42 4,250.81

2006/03/08 A H -037.00 SUPPRESSOR, LHS IR KIT 158.0 435.00 68.73 11,985.0 360.41 4,319.54

2006/03/08 R H -033.00 CENTER BODY, TAIL PIPE LHS 2.0 402.00 0.80 11,983.0 360.41 4,318.74

2006/03/08 R H -034.00 CENTER BODY, TAIL PIPE RHS 2.0 402.00 0.80 11,981.0 360.40 4,317.93

2006/03/08 R H -035.00 EXHAUST MODULE, LHS 29.0 419.00 12.15 11,952.0 360.26 4,305.78

2006/03/08 R H -036.00 EXHAUST MODULE, RHS 29.0 419.00 12.15 11,923.0 360.11 4,293.63

2006/03/08 R H -037.00 SUPPRESSOR, LHS IR KIT 158.0 435.00 68.73 11,765.0 359.11 4,224.90



2006/07/06 R C -024.00 MOUNT SUPPORT M60D 20.0 270.00 5.40 11,650.0 358.40 4,175.34

2006/07/06 A C -024.01 L/SIDE M-240H GUN MOUNT 27.0 270.00 7.29 11,677.0 358.19 4,182.63

2006/07/06 A C -024.02 R/SIDE M-240H GUN MOUNT 27.0 270.00 7.29 11,704.0 357.99 4,189.92

2007/02/22 R A -002.00 COMPUTER KIT-1C/TSEC 8.0 174.00 1.39 11,696.0 358.12 4,188.52

2007/02/22 R B -047.01 KING FM985 TRANCEIVER 2.0 226.00 0.45 11,694.0 358.14 4,188.07

2007/02/22 R C -011.01 BPS PAX FLOOR-01B 3.0 254.80 0.76 11,691.0 358.17 4,187.31

2007/02/22 R C -011.02 BPS PAX FLOOR-01C 4.0 255.40 1.02 11,687.0 358.20 4,186.29

2007/02/22 R B -040.00 CONTROL PANEL RT-1296/APX-100 8.0 227.00 1.82 11,679.0 358.29 4,184.47

2007/02/22 A B -040.00REMOTE CONTROL UNIT, AN/APX-118 P/N 1008940P-4 3.0 227.00 0.68 11,682.0 358.26 4,185.15

2007/02/22 A A -002.00 IFF TRANSPONDER P/N 1008939G-5 11.0 176.00 1.94 11,693.0 358.08 4,187.09

2007/02/22 A A -002.01AN/APX-118 TRANSPONDER MOUNT NSN 5975-01-063-4022 2.0 176.00 0.35 11,695.0 358.05 4,187.44

2007/04/11 A B -034.00FM CONTROL PANEL, C-11466A/ARC-201 NSN-5821-01-231-5660 2.0 229.00 0.46 11,697.0 358.03 4,187.90

2007/04/11 R B -050.00 VHF CONTROL AN/ARN-186(V) C-10604 2.0 231.00 0.46 11,695.0 358.05 4,187.44

2007/04/11 A B -069.00VHF/FM RADIO RT-1477/ARC-201C(V) NSN-5821-01-306-4653 7.0 223.00 1.56 11,702.0 357.97 4,189.00

2007/04/11 A C -011.01 BPS PAX FLOOR-01B 3.0 254.80 0.76 11,705.0 357.95 4,189.76

2007/04/11 A C -011.02 BPS PAX FLOOR-01C 4.0 255.40 1.02 11,709.0 357.91 4,190.78

2007/04/11 A H -014.00TRANSMITTER, IR JAMMER AN/ALQ-144A(V) NSN-5865-01-323-4999 26.0 400.00 10.40 11,735.0 358.00 4,201.18

2007/04/11 ICalculated Weight and Moment per Inventory Completed at AASF, BOISE, ID 11,735.0 358.00 4,201.18

2007/09/13 A B -067.01 BPS COCKPIT FLOOR-02 12.0 208.10 2.50 11,747.0 357.85 4,203.68




Long. Arm (in)

Long. Mom.

(lb-in)

Basic Weight

(lb)


Basic Long. Mom.

(lb-in)




2007/09/13 A B -067.05 BPS COCKPIT DOOR-05 9.0 231.20 2.08 11,808.0 357.13 4,216.96

2007/09/13 A B -067.06 BPS COCKPIT DOOR-06 9.0 231.20 2.08 11,817.0 357.03 4,219.04

2007/09/13 A C -008.01AIR WARRIOR MCU POWER WIRES & MASK BLOWER HARNESSES 54.0 250.00 13.50 11,871.0 356.54 4,232.54

2007/09/13 A C -013.01 BPS PAX FLOOR-01A 42.0 260.90 10.96 11,913.0 356.21 4,243.50

2007/09/13 A C -014.01 AIR WARRIOR CREWMEMBERS HOSES 5.0 270.00 1.35 11,918.0 356.17 4,244.85

2007/09/13 A C -024.01 BPS CREWCHIEF VERTICAL R/S 36.0 287.70 10.36 11,954.0 355.97 4,255.21

2007/09/13 A C -024.02 BPS CREWCHIEF VERTICAL L/S 36.0 287.70 10.36 11,990.0 355.76 4,265.56

2007/09/13 A C -026.00 BPS PAX FLOOR-03 91.0 293.90 26.74 12,081.0 355.29 4,292.31

2007/09/13 A C -027.00 BPS PAX FLOOR-04 91.0 293.90 26.74 12,172.0 354.84 4,319.05

2007/09/13 A A -019.00 SECURITY SET, LHS TSEC/KY-58 5.0 190.00 0.95 12,177.0 354.77 4,320.00

2007/09/13 A D -012.01 BPS PAX FLOOR-06 77.0 339.90 26.17 12,254.0 354.67 4,346.18

2007/09/13 A D -012.02 BPS PAX FLOOR-07 77.0 339.90 26.17 12,331.0 354.58 4,372.35

2007/09/13 A D -014.00 BPS PAX FLOOR-10 7.0 357.30 2.50 12,338.0 354.58 4,374.85

2007/09/13 A D -015.00 BPS PAX FLOOR-08 60.0 370.50 22.23 12,398.0 354.66 4,397.08

2007/09/13 A D -016.00 BPS PAX FLOOR-09 69.0 387.90 26.77 12,467.0 354.84 4,423.84

2007/09/13 A H -004.02 EIBF B-KIT 70073-30007-011 155.8 298.30 46.48 12,622.8 354.15 4,470.32

2007/09/13 A H -021.00 ELECTRONIC MODULE, LHS XM-130, 9311431 5.0 505.00 2.53 12,627.8 354.21 4,472.84

2007/09/13 A H -022.00 DISPENSER MODULE, LHS XM-130, 9311434 6.0 505.00 3.03 12,633.8 354.28 4,475.87

2007/09/13 A H -023.00 PAYLOAD MODULE, LHS XM-130, 9311451 4.0 505.00 2.02 12,637.8 354.33 4,477.89

2007/09/13 A B -033.00 RCU, KY-58 CONTROL C-11466A 2.0 227.00 0.45 12,639.8 354.31 4,478.35

2007/12/11 R C -008.01AIR WARRIOR MCU POWER WIRES & MASK BLOWER HARNESSES 54.0 250.00 13.50 12,585.8 354.75 4,464.85

2007/12/11 R C -013.02AIR WARRIOR UNIT MOUNT ASSEMBLY LSF00447-001 37.0 260.00 9.62 12,548.8 355.03 4,455.23

2007/12/11 R C -014.01 AIR WARRIOR CREWMEMBERS HOSES 5.0 270.00 1.35 12,543.8 355.07 4,453.88

2008/02/15 A C -013.03 M4 RIFLE MOUNT ASSEMBLY LSF01738 8.0 261.00 2.09 12,551.8 355.01 4,455.97

2008/02/24 R B -067.10 AIR WARIOR PILOTS/COPILOTS HOSES 5.0 240.00 1.20 12,546.8 355.05 4,454.77

2008/02/24 A D -012.00TROOP SEAT, CENTER (ALTERNATE SEATING) 70500-02151 16.0 338.00 5.41 12,562.8 355.03 4,460.17

2008/02/24 R A -014.00 RECEIVER, VOR R-2594/ARN-147 8.0 204.00 1.63 12,554.8 355.13 4,458.54

2008/02/24 A A -013.00 RECEIVER, VOR R-2139/ARN-123(V) 9.0 204.00 1.84 12,563.8 355.02 4,460.38

2008/02/24 ICalculated Weight and Moment per Inventory Completed at UAAF, Camp Buehring, Kuwait 12,563.8 355.02 4,460.38

2008/02/24 W BASIC A/C, WEIGHED AT : UAAF, KUWAIT 12,381.0 356.78 4,417.26 12,381.0 356.78 4,417.26

2008/04/08 A C -008.01AIR WARRIOR MCU POWER WIRES & MASK BLOWER HARNESSES 54.0 250.00 13.50 12,435.0 356.31 4,430.76

2008/04/08 A C -013.02AIR WARRIOR UNIT MOUNT ASSEMBLY LSF00447-001 37.0 260.00 9.62 12,472.0 356.03 4,440.38

2008/04/08 A C -014.01 AIR WARRIOR CREWMEMBERS HOSES 5.0 270.00 1.35 12,477.0 355.99 4,441.73

2008/04/08 A B -067.10 AIR WARIOR PILOTS/COPILOTS HOSES 5.0 240.00 1.20 12,482.0 355.95 4,442.93

2008/05/08 A D -006.01 DAVID CLARK ICS MASTER STATION 1.5 322.00 0.48 12,483.5 355.94 4,443.42

2008/05/08 R D -006.01 DAVID CLARK ICS MASTER STATION 1.5 322.00 0.48 12,482.0 355.95 4,442.93

2008/05/08 A D -006.01 DAVID CLARK ICS MASTER STATION 1.5 331.00 0.50 12,483.5 355.94 4,443.43




Long. Arm (in)

Long. Mom.

(lb-in)

Basic Weight

(lb)


Basic Long. Mom.

(lb-in)

2008/05/08 A D -006.02DAVID CLARK ICS DUAL HEADSET INTERCOM SYSTEM (2 EA) 1.5 331.00 0.50 12,485.0 355.94 4,443.93

2008/05/08 A E -016.01DAVID CLARK ICS DUAL HEADSET INTERCOM SYSTEM 1.5 395.00 0.59 12,486.5 355.95 4,444.52

2008/10/07 H MWO 1-1520-237-50-99

2008/10/07 AFIXED PROVISIONS - STRUCTUR AND WIRING (LWR TRANSITION) P/N 70070-95142-011 3.1 441.80 1.37 12,489.6 355.97 4,445.89

2008/10/11 A H -047.05SENSOR, EMOS,(LWR TRANSITION) P/N: SU-202/AAR-57(V) 3.0 478.60 1.44 12,492.6 356.00 4,447.33

2008/12/21 R B -067.10 AIR WARIOR PILOTS/COPILOTS HOSES 5.0 240.00 1.20 12,487.6 356.04 4,446.13

2008/12/21 R C -008.01AIR WARRIOR MCU POWER WIRES & MASK BLOWER HARNESSES 54.0 250.00 13.50 12,433.6 356.50 4,432.63

2008/12/21 R C -013.02AIR WARRIOR UNIT MOUNT ASSEMBLY LSF00447-001 37.0 260.00 9.62 12,396.6 356.79 4,423.01

2008/12/21 R C -014.01 AIR WARRIOR CREWMEMBERS HOSES 5.0 270.00 1.35 12,391.6 356.83 4,421.66

2008/12/21 R H -004.02 EIBF B-KIT 70073-30007-011 155.8 298.30 46.48 12,235.8 357.57 4,375.18

2009/01/14 R A -005.02 CMWS FWD LEFT EOMS SENSOR 3.0 174.00 0.52 12,232.8 357.62 4,374.66

2009/01/14 R A -005.03 CMWS FWD RIGHT EOMS SENSOR 3.0 174.00 0.52 12,229.8 357.66 4,374.14

2009/01/14 R B -059.01 BFT PALLET ASSY W/ WIRE HARNESS (040537-001) 26.0 237.00 6.16 12,203.8 357.92 4,367.97

2009/01/14 R B -067.01 BPS COCKPIT FLOOR-02 12.0 208.10 2.50 12,191.8 358.07 4,365.48




2009/01/14 R B -067.05 BPS COCKPIT DOOR-05 9.0 231.20 2.08 12,130.8 358.77 4,352.20

2009/01/14 R B -067.06 BPS COCKPIT DOOR-06 9.0 231.20 2.08 12,121.8 358.87 4,350.12

2009/01/14 R B -074.00 CMWS DCDU 3.0 240.00 0.72 12,118.8 358.90 4,349.40

2009/01/14 R C -011.01 BPS PAX FLOOR-01B 3.0 254.80 0.76 12,115.8 358.92 4,348.63

2009/01/14 R C -011.02 BPS PAX FLOOR-01C 4.0 255.40 1.02 12,111.8 358.96 4,347.61

2009/01/14 R C -013.01 BPS PAX FLOOR-01A 42.0 260.90 10.96 12,069.8 359.30 4,336.65

2009/01/14 R C -024.01 BPS CREWCHIEF VERTICAL R/S 36.0 287.70 10.36 12,033.8 359.51 4,326.30

2009/01/14 R C -024.02 BPS CREWCHIEF VERTICAL L/S 36.0 287.70 10.36 11,997.8 359.73 4,315.94

2009/01/14 R C -026.00 BPS PAX FLOOR-03 91.0 293.90 26.74 11,906.8 360.23 4,289.19

2009/01/14 R C -027.00 BPS PAX FLOOR-04 91.0 293.90 26.74 11,815.8 360.74 4,262.45

2009/01/14 R D -006.01 DAVID CLARK ICS MASTER STATION 1.5 331.00 0.50 11,814.3 360.75 4,261.95

2009/01/14 R D -006.02DAVID CLARK ICS DUAL HEADSET INTERCOM SYSTEM (2 EA) 1.5 331.00 0.50 11,812.8 360.75 4,261.46

2009/01/14 R D -012.01 BPS PAX FLOOR-06 77.0 339.90 26.17 11,735.8 360.89 4,235.28

2009/01/14 R D -012.02 BPS PAX FLOOR-07 77.0 339.90 26.17 11,658.8 361.02 4,209.11

2009/01/14 R D -014.00 BPS PAX FLOOR-10 7.0 357.30 2.50 11,651.8 361.03 4,206.61

2009/01/14 R D -015.00 BPS PAX FLOOR-08 60.0 370.50 22.23 11,591.8 360.98 4,184.38

2009/01/14 R D -016.00 BPS PAX FLOOR-09 69.0 387.90 26.77 11,522.8 360.82 4,157.61

2009/01/14 R E -009.02 CMWS ECU 19.0 371.00 7.05 11,503.8 360.80 4,150.57

2009/01/14 R E -016.01DAVID CLARK ICS DUAL HEADSET INTERCOM SYSTEM 1.5 395.00 0.59 11,502.3 360.80 4,149.97

2009/01/14 R F -013.00 CMWS AFT LEFT EOMS SENSOR 3.0 740.00 2.22 11,499.3 360.70 4,147.75

2009/01/14 R F -014.00 CMWS AFT RIGHT EOMS SENSOR 3.0 740.00 2.22 11,496.3 360.60 4,145.53

2009/01/14 R F -009.01 CMWS SEQUENCER, #1 4.0 515.00 2.06 11,492.3 360.54 4,143.47




Long. Arm (in)

Long. Mom.

(lb-in)

Basic Weight

(lb)


Basic Long. Mom.

(lb-in)

2009/01/14 R F -009.02 CMWS SEQUENCER, #2 4.0 515.00 2.06 11,488.3 360.49 4,141.41

2009/01/14 R H -014.00TRANSMITTER, IR JAMMER AN/ALQ-144A(V) NSN-5865-01-323-4999 26.0 400.00 10.40 11,462.3 360.40 4,131.01

2009/01/14 R H -021.00 ELECTRONIC MODULE, LHS XM-130, 9311431 5.0 505.00 2.53 11,457.3 360.34 4,128.49

2009/01/14 R H -022.00 DISPENSER MODULE, LHS XM-130, 9311434 6.0 505.00 3.03 11,451.3 360.26 4,125.46

2009/01/14 R H -023.00 PAYLOAD MODULE, LHS XM-130, 9311451 4.0 505.00 2.02 11,447.3 360.21 4,123.44

2009/01/14 R H -047.05SENSOR, EMOS,(LWR TRANSITION) P/N: SU-202/AAR-57(V) 3.0 478.60 1.44 11,444.3 360.18 4,122.00

2009/01/14 R H -048.00 CMWS ICMD, #1 CHAFF 4.0 505.00 2.02 11,440.3 360.13 4,119.98

2009/01/14 R H -050.00 CMWS LH CHAFF DISPENSER MODULE 4.0 505.00 2.02 11,436.3 360.08 4,117.96

2009/01/14 R H -052.00 CMWS RH FLARE DISPENSER MODULE 4.0 515.00 2.06 11,432.3 360.02 4,115.90

2009/01/14 R H -053.00 CMWS ICMD, #2 RH FLARE 4.0 515.00 2.06 11,428.3 359.97 4,113.84

2009/01/14 R H -055.00 CMWS LH FLARE DISPENSER MODULE 4.0 535.00 2.14 11,424.3 359.91 4,111.70

2009/01/14 R H -056.00 CMWS ICMD, #3 LH FLARE 4.0 535.00 2.14 11,420.3 359.85 4,109.56

2009/01/14 A B -059.01 BFT PALLET ASSY W/ WIRE HARNESS (040537-001) 26.0 237.00 6.16 11,446.3 359.57 4,115.72

2009/01/20 R C -013.03 M4 RIFLE MOUNT ASSEMBLY LSF01738 8.0 261.00 2.09 11,438.3 359.64 4,113.64

2009/07/07 H MWO 1-1520-237-50-92 DGNS applied

2009/07/07 R A -003.00 SIGNAL DATA CONVERTER CV-3338A/ASN-128B 13.0 174.00 2.26 11,425.3 359.85 4,111.37

2009/07/07 A A -008.00SIGNAL DATA CONVERTER (ALTERNATE) P320A002-02, CV-3338B/ASN-128D 11.0 177.00 1.95 11,436.3 359.67 4,113.32

2009/07/07 AASN-128D WIRING HARNESS KIT INSTALL P/N 1005442-10 7.0 186.00 1.30 11,443.3 359.57 4,114.62

2009/07/07 AASN-128D ANNUNCIATOR P/N LED-40-18-KG-31936, -31937, -31938 1.0 206.00 0.21 11,444.3 359.55 4,114.83

2009/07/07 H END MWO 1-1520-237-50-92 ENTRIES

2009/07/16 R A -011.00 PROCESSOR, DIGITAL CP-1597A/APR-39(V) 6.0 184.00 1.10 11,438.3 359.64 4,113.73

2009/07/16 R A -019.00 SECURITY SET, LHS TSEC/KY-58 5.0 190.00 0.95 11,433.3 359.72 4,112.78

2009/07/16 R A -020.00 SECURITY SET, CENTER TSEC/KY-58 5.0 190.00 0.95 11,428.3 359.79 4,111.83

2009/07/16 R A -021.00 SECURITY SET, RHS TSEC/KY-58 5.0 190.00 0.95 11,423.3 359.87 4,110.88

2009/07/16 R B -053.00SECURE COMMUNICATION CONTROL PANEL KY-100 6.0 253.00 1.52 11,417.3 359.92 4,109.36

2009/07/16 R B -067.07 BFT MILLTOPE (LAPTOP) WIRE HARNESS (040427) 4.0 247.00 0.99 11,413.3 359.96 4,108.37

2009/07/16 R C -004.00WALK AROUND ICS CORD, 50* (STOWED), RHS 70602-02016-041 2.0 247.00 0.49 11,411.3 359.98 4,107.88

2009/07/16 R C -020.00 MACHINE GUN MOUNT ARM, LHS M60D 10.0 280.00 2.80 11,401.3 360.05 4,105.08

2009/07/16 R C -021.00 MACHINE GUN MOUNT ARM, RHS M60D 10.0 280.00 2.80 11,391.3 360.12 4,102.28

2009/07/16 R C -025.00 CMWS SAFETY SWITCH ASSEMBLY 1.0 292.00 0.29 11,390.3 360.13 4,101.98

2009/07/16 R D -003.00 ICS BOX, CEILING C-6533/ARC 2.0 322.00 0.64 11,388.3 360.14 4,101.34

2009/07/16 R D -006.00 TROOP SEAT, FORWARD, LH 70500-02151 16.0 322.00 5.15 11,372.3 360.19 4,096.19

2009/07/16 R F -005.00 CARGO NET, RHS FDC-1555-149 2.0 421.00 0.84 11,370.3 360.18 4,095.35

2009/07/16 ICalculated Weight and Moment per Inventory Completed at Ft. Drum, NY 11,370.3 360.18 4,095.35

2009/07/17 Hposted master chart A dated 19 May 2008. previous inventory has been retained for historical purposes

2009/07/17 ICalculated Weight and Moment per Inventory Completed at FT. DRUM, NY 11,370.3 360.18 4,095.35

2009/07/17 W BASIC A/C, WEIGHED AT : FT. DRUM, NY 11,549.0 360.00 4,157.65 11,549.0 360.00 4,157.65

2010/04/22 A C -004.01 ELT EBC-406HM 2.5 247.00 0.62 11,551.5 359.98 4,158.26




Long. Arm (in)

Long. Mom.

(lb-in)

Basic Weight

(lb)


Basic Long. Mom.

(lb-in)

2010/07/12 A A -019.00 SECURITY SET, RHS TSEC/KY-58 4.9 190.00 0.93 11,556.4 359.90 4,159.20

2010/07/12 A A -020.00 SECURITY SET, CENTER TSEC/KY-58 4.9 190.00 0.93 11,561.3 359.83 4,160.13

2010/07/12 A A -021.00 SECURITY SET, LHS TSEC/KY-58 4.9 190.00 0.93 11,566.2 359.76 4,161.06

2010/07/12 A F -006.00 CARGO NET, RHS FDC-1555-149 1.9 421.00 0.80 11,568.1 359.77 4,161.86

2010/07/12 ICalculated Weight and Moment per Inventory Completed at AASF # 2 W.TRENTON, NJ 11,568.1 359.77 4,161.86

2010/10/12 H***Beginning of MWO 1-1520-237-50-100INTEGRATED VEHICLE HEALTH MANAGEMENTSYSTEM (IVHMS)

2010/10/12 A ELECTRICAL INSTALLATION (IVHMS) 47.0 369.00 17.34 11,615.1 359.81 4,179.20

2010/10/12 A SENSOR / STRUCTURAL INATALLATIONS (IVHMS) 16.0 429.00 6.86 11,631.1 359.90 4,186.06

2010/10/12 A B -016.00 Cockpit Display Unit (CDU) PN: 10150-0201 (IVHMS) 4.1 206.00 0.84 11,635.2 359.85 4,186.91

2010/10/12 A B -058.00 Data Transfer Unit (DTU) PN: 30192-0201 (IVHMS) 1.8 245.00 0.44 11,637.0 359.83 4,187.35

2010/10/12 A B -065.00Remote Data Concentrator (RDC) PN: 30201-0501 (IVHMS) 4.3 205.00 0.88 11,641.3 359.77 4,188.23

2010/10/12 A F -008.00Integrated Vehicle Health Management Unit PN: 30279-0302 (IVHMS) 20.0 474.00 9.48 11,661.3 359.97 4,197.71

2010/10/12 H ***End of MWO 1-1520-237-50-100

2010/10/12 RSAFE/ARM SWITCH ASSYA100710-101 0.6 233.00 0.14 11,660.7 359.98 4,197.57

2010/10/12 RECU STRUCTUREA100631 6.7 371.00 2.49 11,654.0 359.97 4,195.09

2010/10/12 RSEQUENCER MOUNTA100685 3.2 515.00 1.65 11,650.8 359.93 4,193.44

2010/10/12 R CMWS WIRING AND ASSOC HARDWARE 0.8 179.00 0.14 11,650.0 359.94 4,193.29

2010/10/12 A CMWS P3I WIRING AND ASSOC HARDWARE 10.4 209.60 2.18 11,660.4 359.81 4,195.47

2010/10/12 ANVIS SAFE/ARM SWITCH ASSYA102853-101 1.4 233.00 0.33 11,661.8 359.79 4,195.80

2010/10/12 ACREW DISPENSE SWITCH INSTALLATIONA102841 1.2 295.00 0.35 11,663.0 359.78 4,196.15

2010/10/12 AELECTRONIC CONTROL UNIT STRUCTUREA103001 6.9 371.00 2.56 11,669.9 359.79 4,198.71

2010/10/12 ASEQUENCER MOUNT,LHA100769-101 0.8 496.40 0.40 11,670.7 359.80 4,199.11

2010/10/12 ASEQUENCER MOUNT,RHA100769-102 0.8 496.40 0.40 11,671.5 359.81 4,199.51

2010/10/12 A B -088.00CHAFF CONTROLLERA1022859-101(CMWS) 0.8 226.50 0.18 11,672.3 359.80 4,199.69

2010/12/14 H Installation of Option II cabin heater system

2010/12/14 AINSTALLATION KIT, OPTION II CABIN HEATER SYSTEM, P/N 70070-95123-011 15.7 419.20 6.58 11,688.0 359.88 4,206.27

2010/12/14 H end of installation

2011/03/08 R C -004.00WALK AROUND ICS CORD, 50* (STOWED), RHS 70602-02016 2.1 247.00 0.52 11,685.9 359.90 4,205.75

2011/03/08 IAnnual review and inventory completed at: LAKEHURST, NJ 11,685.9 359.90 4,205.75

2011/07/19 H Installation of rescue hoist cable guard and A Kit

2011/07/19 A Mod Kit (Cable guard and A Kit) P/N: 70700-20551-011 8.0 343.19 2.75 11,693.9 359.89 4,208.50

2011/07/19 H End of installation

2011/08/02 A C -004.00WALK AROUND ICS CORD, 50* (STOWED), RHS 70602-02016 2.1 247.00 0.52 11,696.0 359.87 4,209.02

2015/12/16 AWBS 10.0 Page 11 of 11S = Chart C Review W = Weighing Certified copy as of 2015/12/16A = Addition R = Removal Weight & Balance TechnicianH = Header I = Inventory



Long. Arm (in)

Long. Mom.

(lb-in)

Basic Weight

(lb)


Basic Long. Mom.

(lb-in)

2011/08/02 IAnnual review and inventory completed Groton CT 11,696.0 359.87 4,209.02

2011/08/02 W BASIC A/C, WEIGHED AT : Groton, CT 11,559.7 360.23 4,164.11 11,559.7 360.23 4,164.11

2011/09/13 IAnnual review and inventory completed at LAKEHURST, NJ 11,559.7 360.23 4,164.11

2011/09/13 W BASIC A/C, WEIGHED AT : Lakehurst, NJ 11,738.5 359.43 4,219.12 11,738.5 359.43 4,219.12

2012/08/29 IAnnual review and inventory completed at Wheeling, WV 11,738.5 359.43 4,219.12

2013/08/20 A D -002.00 ICS BOX C-6533/ARC 1.8 322.00 0.58 11,740.3 359.42 4,219.75

2013/08/20 A E -021.00SIDEWALL SOUNDPROOFING PANEL, LHS 70500-02068 2.0 388.00 0.78 11,742.3 359.43 4,220.52

2013/08/20 A E -022.00SIDEWALL SOUNDPROOFING PANEL, RHS 70500-02068 2.0 388.00 0.78 11,744.3 359.43 4,221.30

2013/08/20 A E -028.00AFT BULKHEAD SOUNDPROOFING, BLANKETS 70500-03050 3.0 398.00 1.19 11,747.3 359.44 4,222.49

2013/08/20 I Annual review and inventory completed Wheeling, WV 11,747.3 359.44 4,222.49

2013/08/20 W BASIC A/C, WEIGHED AT : AASF2, Wheeling WV 11,606.0 359.27 4,169.63 11,606.0 359.27 4,169.63

2014/06/17 H*** Start Modification "7923273 MWO 1-1520-237-30-3 Eng Auto-Re" 11,606.0 359.27 4,169.63

2014/06/17 AMod Kit - Auto Relight, Relays, CBPanel &Harness Mods 70070-55562-011 5.9 310.20 1.83 11,611.9 359.24 4,171.46

2014/06/17 AMod Kit - Auto Relight &Top Deck Mods 70070-55562-012 4.0 333.90 1.34 11,615.9 359.23 4,172.80

2014/06/17 H*** End Modification "7923273 MWO 1-1520-237-30-3 Eng Auto-Re" 11,615.9 359.23 4,172.80

2014/08/20 IAnnual review and inventory completed AASF2 Wheeling WV 11,615.9 359.23 4,172.80

2015/11/04 ICalculated weight and moment per inventory completed at AASF2 Wheeling WV 11,615.9 359.23 4,172.80

2015/11/04 W BASIC A/C, WEIGHED AT: Wheeling, WV 11,649.0 359.17 4,184.02 11,649.0 359.17 4,184.02

2015/12/16 17:03:10 AWBS 10.0 Page 1

UH-60A 79-23273

F O R M B - H I S T O R YFORM B - AIRCRAFT WEIGHING RECORD 3 - P O I N T

DATE WEIGHED 2006/03/09 MODEL/DESIGN UH-60A SERIAL NUMBER 79-23273PLACE WEIGHED SALINA, KS TECHNICIAN JOHN L. DEGAND DUTY PHONE 822-3463

REACTION SCALE READING CORRECTIONS NET WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOMLEFT MAIN 4,672.0 4,672.0 247.00 1,153,984.00RIGHT MAIN 4,617.0 4,617.0 247.00 1,140,399.00NOSE or TAIL 4,793.0 4,793.0 605.30 2,901,202.90TOTALS 14,082.0 14,082.0 368.95 5,195,585.90

LONGITUDINAL MEASUREMENTSB = Distance from the jig point to the center line of the main reactionsI = Distance from the reference datum line to the jig point

E = 247.00 Distance from the reference datum line to the center line of the main reactionsD = Distance between the main and the nose or tail reactionsF = 605.30 Distance from the reference datum line to the center line of the nose or tail reaction

LATERAL MEASUREMENTSLM = Distance from the lateral reference datum line to the Left Main reactionRM = Distance from the lateral reference datum line to the Right Main reactionNT = Distance from the lateral reference datum line to the Nose or Tail reaction

ADJUSTMENTS NET WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOMLevel Weigh - No CorrectionTotal (As Weighed Above) 14,082.0 368.95 5,195,585.90Total of Column I - 2,412.0 420.75 1,014,849.00Total of Column II +BASIC AIRCRAFT 11,670.0 358.25 4,180,736.90SIMPLIFIED LONG. MOMENT 4,180.74 LAT. MOMENT CONSTANT 1000SCALE TYPE: C55800-3-50 REVERE ELECTRONIC REACTIONS USEDSERIAL NUMBER(S): 5782U FWD JACK POINT: 247.0 AFT JACK POINT: 605.3CALIBRATION ACCURACY:DATE CALIBRATED: 2005/11/17CALIBRATION DUE DATE:ALTITUDE (ft): 0.00LATITUDE:

CORRECTIONSREACTION CALIBRATION SCALE TEMP EQUIPMENT OTHER TOTALLEFT MAINRIGHT MAINNOSE or TAILRemarksACFT WEIGHED I/A/W AR 95-1 & TM 55-1500-342-23.ACFT WEIGHED INSIDE A CLOSED HANGAR IN A LEVEL FLIGHT ATTITUDE.ACFT WEIGHED FULL OF FUEL. 6.7 lbs

COLUMN IItems Weighed But Not Part of Basic Weight WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOM360 GALS JP-8 2,412.0 420.75 1,014,849.00TOTAL of Items Weighed But Not Part of Basic Weight 2,412.0 420.75 1,014,849.00

COLUMN IIBasic Weight Items Not in Aircraft When Weighed WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOMTOTAL Basic Weight Items Not in Aircraft When Weighed

2015/12/16 17:03:10 AWBS 10.0 Page 2

UH-60A 79-23273


DATE WEIGHED 2008/02/24 MODEL/DESIGN UH-60A SERIAL NUMBER 79-23273PLACE WEIGHED UAAF, KUWAIT TECHNICIAN BRIAN D. JOHNSON DUTY PHONE DSN 318-828-1347





ADJUSTMENTS NET WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOMLevel Weigh - No CorrectionTotal (As Weighed Above) 14,793.0 367.21 5,432,113.90Total of Column I - 2,412.0 420.75 1,014,849.00Total of Column II +BASIC AIRCRAFT 12,381.0 356.78 4,417,264.90SIMPLIFIED LONG. MOMENT 4,417.26 LAT. MOMENT CONSTANT 1000SCALE TYPE: GENERAL ELECTRODYNAMIC REACTIONS USEDSERIAL NUMBER(S): I3408 FWD JACKPOINTS AT 247.0

AFT JACKPOINTS AT 605.3CALIBRATION ACCURACY: +/- .03%DATE CALIBRATED: 2007/09/30CALIBRATION DUE DATE:ALTITUDE (ft): 0.00LATITUDE:

CORRECTIONSREACTION CALIBRATION SCALE TEMP EQUIPMENT OTHER TOTALLEFT MAINRIGHT MAINNOSE or TAILRemarksACFT WEIGHED I/A/W AR 95-1 & TM 55-1500-342-23.ACFT WEIGHED INSIDE A CLOSED HANGAR IN A LEVEL FLIGHT ATTITUDE.ACFT WEIGHED FULL OF FUEL. 6.7 lbs/gal.

COLUMN IItems Weighed But Not Part of Basic Weight WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOM360 GALS JP-8 2,412.0 420.75 1,014,849.00TOTAL of Items Weighed But Not Part of Basic Weight 2,412.0 420.75 1,014,849.00


2015/12/16 17:03:10 AWBS 10.0 Page 3

UH-60A 79-23273

F O R M B - H I S T O R YFORM B - AIRCRAFT WEIGHING RECORD 3 - P O I N T ( T A I L )

DATE WEIGHED 2009/07/17 MODEL/DESIGN UH-60A SERIAL NUMBER 79-23273PLACE WEIGHED FT. DRUM, NY TECHNICIAN FLOYD T. SMITH DUTY PHONE DSN 772-7535

REACTION SCALE READING CORRECTIONS NET WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOMLEFT MAIN 4,610.0 4,610.0 247.00 1,138,670.00RIGHT MAIN 4,538.0 4,538.0 247.00 1,120,886.00TAIL 4,811.0 4,811.0 605.30 2,912,098.30TOTALS 13,959.0 13,959.0 370.49 5,171,654.30


E = 247.00 Distance from the reference datum line to the center line of the main reactionsD = Distance between the main and the tail reactionF = 605.30 Distance from the reference datum line to the center line of the tail reaction

LATERAL MEASUREMENTSLM = Distance from the lateral reference datum line to the Left Main reactionRM = Distance from the lateral reference datum line to the Right Main reactionNT = Distance from the lateral reference datum line to the Tail reaction

ADJUSTMENTS NET WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOMLevel Weigh - No CorrectionTotal (As Weighed Above) 13,959.0 370.49 5,171,654.30Total of Column I - 2,410.0 420.75 1,014,007.50Total of Column II +BASIC AIRCRAFT 11,549.0 360.00 4,157,646.80SIMPLIFIED LONG. MOMENT 4,157.65 LAT. MOMENT CONSTANT 1000SCALE TYPE: General Electrodynamic REACTIONS USEDSERIAL NUMBER(S): S0088 FWD JACKPOINTS AT 247.0

AFT JACKPOINTS AT 605.3CALIBRATION ACCURACY:DATE CALIBRATED: 2009/01/09CALIBRATION DUE DATE:ALTITUDE (ft): 0.00LATITUDE:

CORRECTIONSREACTION CALIBRATION SCALE TEMP EQUIPMENT OTHER TOTALLEFT MAINRIGHT MAINTAILRemarksSCALE SET S/N S0088 consisting of Ind. s/n I3418, and cells, s/n C3321RED, C3322BLU, C3323YEL. (C3324GRN not used) ACFT washed, dry, fuel system full using open-port method, weighed in level condition, aircraft weighed at 0 degrees nose up attitude, inside enclosed hangar, using jack/load cells. Above statement per TM 55-1500-342-23 ch11.

COLUMN IItems Weighed But Not Part of Basic Weight WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOM359.7 GALS JP-8 @ 6.7 LPG 2,410.0 420.75 1,014,007.50TOTAL of Items Weighed But Not Part of Basic Weight 2,410.0 420.75 1,014,007.50


2015/12/16 17:03:10 AWBS 10.0 Page 4

UH-60A 79-23273


DATE WEIGHED 2011/08/02 MODEL/DESIGN UH-60A SERIAL NUMBER 79-23273PLACE WEIGHED Groton, CT TECHNICIAN Ronald N. Ladd DUTY PHONE 860-405-2485





ADJUSTMENTS NET WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOMLevel Weigh - No CorrectionTotal (As Weighed Above) 13,955.0 370.86 5,175,324.20Total of Column I - 2,410.0 420.75 1,014,007.50Total of Column II + 14.7 190.00 2,793.00BASIC AIRCRAFT 11,559.7 360.23 4,164,109.70SIMPLIFIED LONG. MOMENT 4,164.11 LAT. MOMENT CONSTANT 1000SCALE TYPE: GENERAL ELECTRODYNAMIC REACTIONS USEDSERIAL NUMBER(S): 50110 FWD JACKPOINTS AT 247.0

AFT JACKPOINTS AT 605.3CALIBRATION ACCURACY:DATE CALIBRATED: 2011/02/14CALIBRATION DUE DATE:ALTITUDE (ft): 0.00LATITUDE:

CORRECTIONSREACTION CALIBRATION SCALE TEMP EQUIPMENT OTHER TOTALLEFT MAINRIGHT MAINTAILRemarksACFT washed, dry, fuel system full weighed in level condition, aircraft weighed at 0 degrees nose up attitude, inside enclosed hangar, using jack/load cellsAbove statement per TM 55-1500-342-23 ch 11.

COLUMN IItems Weighed But Not Part of Basic Weight WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOM359.7 GALS JP-8 @ 6.7 Lb/Gal 2,410.0 420.75 1,014,007.50TOTAL of Items Weighed But Not Part of Basic Weight 2,410.0 420.75 1,014,007.50

COLUMN IIBasic Weight Items Not in Aircraft When Weighed WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOMSecurity Set, RHS TSEC/KY-58 4.9 190.00 931.00Security Set, Center TSEC/KY-58 4.9 190.00 931.00Security Set, LHS TSEC\KY-58 4.9 190.00 931.00TOTAL Basic Weight Items Not in Aircraft When Weighed 14.7 190.00 2,793.00

2015/12/16 17:03:10 AWBS 10.0 Page 5

UH-60A 79-23273


DATE WEIGHED 2011/09/13 MODEL/DESIGN UH-60A SERIAL NUMBER 79-23273PLACE WEIGHED Lakehurst, NJ TECHNICIAN Sheila I. Zelaskowski DUTY PHONE 732 323 2043





ADJUSTMENTS NET WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOMLevel Weigh - No CorrectionTotal (As Weighed Above) 14,143.5 369.85 5,231,020.35Total of Column I - 2,405.0 420.75 1,011,903.75Total of Column II +BASIC AIRCRAFT 11,738.5 359.43 4,219,116.60SIMPLIFIED LONG. MOMENT 4,219.12 LAT. MOMENT CONSTANT 1000SCALE TYPE: REVERE REACTIONS USEDSERIAL NUMBER(S): DT0022, 981423RR, 669735 JACK POINTSCALIBRATION ACCURACY:DATE CALIBRATED: 2011/08/15CALIBRATION DUE DATE:ALTITUDE (ft): 0.00LATITUDE:

CORRECTIONSREACTION CALIBRATION SCALE TEMP EQUIPMENT OTHER TOTALLEFT MAINRIGHT MAINTAILRemarksACFT washed, dry, fuel system full using open-port method. Fuel density 6.68 lbs per gal, weighed in level condition, aircraft weighed at 0 degrees nose up attitude, inside enclosed hangar, using jack/load cells. Scale settings: Altitude: 103 feet and Latitude 40 degrees North.

COLUMN IItems Weighed But Not Part of Basic Weight WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOM360 GALS JP-8 @ 6.68 Lb/Gal 2,405.0 420.75 1,011,903.75TOTAL of Items Weighed But Not Part of Basic Weight 2,405.0 420.75 1,011,903.75

COLUMN IIBasic Weight Items Not in Aircraft When Weighed WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOM

TOTAL Basic Weight Items Not in Aircraft When Weighed

2015/12/16 17:03:10 AWBS 10.0 Page 6

UH-60A 79-23273


DATE WEIGHED 2013/08/20 MODEL/DESIGN UH-60A SERIAL NUMBER 79-23273PLACE WEIGHED AASF2, Wheeling WV TECHNICIAN David E. Nelson DUTY PHONE 304-201-3513





ADJUSTMENTS NET WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOMLevel Weigh - No CorrectionTotal (As Weighed Above) 14,036.0 369.91 5,192,054.46Total of Column I - 2,430.0 420.75 1,022,422.50Total of Column II +BASIC AIRCRAFT 11,606.0 359.27 4,169,631.96SIMPLIFIED LONG. MOMENT 4,169.63 LAT. MOMENT CONSTANT 1000SCALE TYPE: INTERCOMP ROLL-ON REACTIONS USEDSERIAL NUMBER(S): 81107PX0418 Main and tail wheels on platform scales 297.61 - 645.86CALIBRATION ACCURACY: +/- DATE CALIBRATED: 2013/02/11CALIBRATION DUE DATE:ALTITUDE (ft): 1,200.00LATITUDE: 40�° 3’ 50" N

CORRECTIONSREACTION CALIBRATION SCALE TEMP EQUIPMENT OTHER TOTALLEFT MAINRIGHT MAINNOSE or TAILRemarksAIRCRAFT WAS WEIGHED IN THE FOLLOWING CONDITION:- CLEAN AND DRY- ENCLOSED HANGAR WITH BLOWERS OFF- FUEL: FUEL SYSTEM FULL USING OPEN PORT METHOD- FUEL DENSITY = 6.8 LB/GALLON- SCALES: PLATFORMS- ATTITUDE: LONGITUDINALLY AND LATERALLY LEVEL-ACTUAL FUEL DENSITY MEASURED 6.75 (lb/gal)

COLUMN IItems Weighed But Not Part of Basic Weight WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOM360 Gallons Fuel JP-8 @ 6.75 lbs/gal 2,430.0 420.75 1,022,422.50TOTAL of Items Weighed But Not Part of Basic Weight 2,430.0 420.75 1,022,422.50


2015/12/16 17:03:10 AWBS 10.0 Page 7

UH-60A 79-23273


DATE WEIGHED 2015/11/04 MODEL/DESIGN UH-60A SERIAL NUMBER 79-23273PLACE WEIGHED Wheeling, WV TECHNICIAN David E. Nelson DUTY PHONE 304-201-3513

REACTION SCALE READING CORRECTIONS NET WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOMLEFT MAIN 4,053.0 4,053.0 247.00 1,001,091.00RIGHT MAIN 3,949.0 3,949.0 247.00 975,403.00NOSE or TAIL 3,647.0 3,647.0 605.30 2,207,529.10TOTALS 11,649.0 11,649.0 359.17 4,184,023.10




ADJUSTMENTS NET WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOMLevel Weigh - No CorrectionTotal (As Weighed Above) 11,649.0 359.17 4,184,023.10Total of Column I -Total of Column II +BASIC AIRCRAFT 11,649.0 359.17 4,184,023.10SIMPLIFIED LONG. MOMENT 4,184.02 LAT. MOMENT CONSTANT 1000SCALE TYPE: GENERAL ELECTRODYNAMICS CORP REACTIONS USEDSERIAL NUMBER(S): I3433 , C3384, C3385, C3382 Jack points 247.0 and 605.3CALIBRATION ACCURACY: +/-DATE CALIBRATED: 2015/07/24CALIBRATION DUE DATE: 2016/03/20ALTITUDE (ft): 1,200.00LATITUDE:

CORRECTIONSREACTION CALIBRATION SCALE TEMP EQUIPMENT OTHER TOTALLEFT MAINRIGHT MAINNOSE or TAILRemarksAIRCRAFT WAS WEIGHED IN THE FOLLOWING CONDITION:- CLEAN AND DRY- ENCLOSED HANGAR WITH BLOWERS OFF- FUEL: TRAPPED FUEL- SCALES: JACKS/LOAD-CELLS- ATTITUDE: LONGITUDINALLY AND LATERALLY LEVEL

COLUMN IItems Weighed But Not Part of Basic Weight WEIGHT LONG. ARM LONG. MOM LAT. ARM LAT. MOMTOTAL of Items Weighed But Not Part of Basic Weight


2015/12/16 17:03:10 AWBS 10.0 Page 1

RECORD OF WEIGHT AND BALANCE PERSONNEL

MDS: UH-60A SERIAL NO: 79-23273

Last Name First Name M Grade, Rate, or Rank Where Qualified When

Qualified Station Date Assigned

Date Relieved

STATON CLAY SFC SALINA, KS 1996/10/01 SALINA, KS 1996/10/01 2001/10/30

STATON CLAYTON L 1SG SALINA, KS 1997/01/01 SALINA, KS 1997/01/01 2003/09/02

DEGAND JOHN L MSG SALINA, KS 2003/09/02 SALINA, KS 2003/09/02 2003/10/31

STATON CLAYTON L 1SG SALINA, KS 1997/01/01 SALINA, KS 2003/10/31 2004/12/07

DEGAND JOHN L MSG SALINA, KS 2004/09/22 SALINA,KS 2004/10/29 2006/02/07

BRIC CHRISTOPHER J CIV FTCKY 2005/08/16 FTCKY 2006/02/07 2006/02/16

DEGAND JOHN L 1SG SALINA, KS 2003/09/02 SALINA, KS 2006/03/08 2006/03/31

JOHNSON KENNETH W SSG TOPEKA, KS 2000/06/15 FT. HOOD, TX. 2006/04/01 2006/08/20

JOHNSON BRIAN D GS-9 AASF IDAHO 2001/07/21 BOISE, ID 2006/09/12 2008/05/15

Mohacsi Gregory S MSG Ft Eustis, Va 1990/07/06 Camp Buering 2008/05/16 2009/05/13

Smith Floyd T CIV Ft Eustis, VA 1984/09/28 Ft. Drum, NY 2009/05/13 2009/12/01

Bono George W WS-10 Ft. Eustis, Va 1999/04/25 Lakehurst, NJ 2010/03/01 2011/07/14

Ladd Ronald N CIV Groton, CT 1994/05/13 Groton, CT 2011/07/18 2012/08/21

Nelson David E GS-9 AASF2, WVARNG 2007/11/02 Wheeling, WV 2012/08/21 2015/12/15

UNIT UNIQUE INVENTORY ITEMSSES BEST


7923273 UH-60A



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UNIT UNIQUE INVENTORY ITEMSSES BEST7923273 UH-60A


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Nomenclature

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