1. NOMENCLATURE 2. MODEL 3. AIRCRAFT SERIAL ... UTILITY EH-60A 8524475 1. NOMENCLATURE 2. MODEL 3....

PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN

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

8524475EH-60AHELICOPTER, UTILITY

3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE

of 3

DR21-Jun-2004

(NOORGANIZATION/PID)

0.0 LILLY, THOMASM

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

DM01-Sep-1991

DYNCORP OLR(SH6210)

2.001-OCT-1995

LILLY, THOMASM

IMPROVED ENGINE COWLINGRELEASE HANDLE ASSEMBLY

1-1520-237-50-64MWO:

Mnt LevelPriority

DU10-Aug-1987

LEAR SEIGLER,FHU AZ(PCW/JH5095)

6.003-NOV-1987

LILLY, THOMASM

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

55-1520-237-50-46MWO:

Mnt LevelPriority

DR13-Apr-2001

USAAVNC, FT.RUCKER, AL(JH5095)

1.006-FEB-2003

LILLY, THOMASM

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

OM16-Dec-2002

USAAVNC, FT.RUCKER, AL(JH5095)

0.006-Jan-2003

BELFORD, MAEP

ALL ARMY AIRCRAFT, INSPECTION OFTHE BATTERY BOX, CY8515

GEN-03-ASAM-01MWO:

Mnt LevelPriority

DN16-Oct-1989

DYNCORP-E(PCW/JH5095)

23.014-JUN-1990

LILLY, THOMASM

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

55-1520-237-50-49MWO:

Mnt LevelPriority

DM15-Nov-1989


23.014-JUN-1990

LILLY, THOMASM

MODIFICATION OF DOWEL PINRETENTION MAIN GEARBOX

55-1520-237-50-43MWO:

Mnt LevelPriority

FR02-Nov-2009

USAACE 0.018-Dec-2013

WILLIAMS,OLIVIA D

SINGLE INSTALLATION OF ATTITUDEHEADING REFERENCE UNIO (AHRU)

1-1520-237-20-2MWO:

Mnt LevelPriority

DN30-Jun-1994

70TH TRANS BNAPO AE 0902(ST1133)

0.518-Jan-1994

BELFORD, MAEP

INSPECTION OF APU FORMS ANDRECORDS

1-2835-214-20-1MWO:

Mnt LevelPriority

DN01-Oct-1988

TRACOR(PCW/JH5095)

10.018-JUL-1989

LILLY, THOMASM

EH-60A INSTALLATION OF AFCSINLINE FILTER P/N C5144887

55-1520-237-55-6MWO:

Mnt LevelPriority

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

DA FORM 2408-5, AUG 2004 EQUIPMENT MODIFICATION RECORD

PIDMWODATE HRS





of 3

DN31-Oct-1996

DYNCORP-EOLR APO 9250(SH6210)

35.018-NOV-1997

LILLY, THOMASM

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

1-1520-237-50-74MWO:

Mnt LevelPriority

DR15-Jul-1985

PCW(PCW/JH5095)

5.019-OCT-1995

LILLY, THOMASM

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

DN23-Jan-1989

PCW(PCW/JH5095)

5.019-OCT-1995

LILLY, THOMASM

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

55-1520-237-50-44MWO:

Mnt LevelPriority

DN01-May-1994

DYNCORP OLR(SH6210)

128.019-OCT-1995

LILLY, THOMASM

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

1-1520-237-50-66MWO:

Mnt LevelPriority

DN01-Feb-1993

DYNCORP OLR(SH6210)

416.019-OCT-1995

LILLY, THOMASM

INSTALLATION OF THE AN/ARC-201SINCGARS AND TSEC KY-58ENCODER/DECODER UNITS IN THEEH-60A QUICK FIX HELICOPTER

1-1520-237-50-67MWO:

Mnt LevelPriority

DN17-Jun-1989

DYNCORP OLR(SH6210)

6.019-OCT-1995

LILLY, THOMASM

INCOROPORATION OF EXHAUSTEXTENDER DOUBLERS

55-1520-237-50-51MWO:

Mnt LevelPriority

DN17-Jan-1989

PCW(PCW/JH5095)

5.019-OCT-1995

LILLY, THOMASM

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

55-1520-237-50-52MWO:

Mnt LevelPriority

DR25-Jan-2007

USAAWC, FT.RUCKER, AL(RC1002)

8.023-OCT-2007

LILLY, THOMASM

MODIFICATION INSTRUCTIONS FORTHE DUAL INSTALLATION OFATTITUDE HEADING REFERENCEUNITS (AHRU) ON THE UH-60A/L, HH-60A, AND HH-60L HELICOPTER (NSN1520-01-035-0266) (EIC: RSA) (NSN1520-01-298-4532) (EIC: RSM) (NSN1520-01-471-6743) (EIC: NA) (NSN 1520-01-459-9468) (EIC: NA)

1-1520-237-20-94MWO:

Mnt LevelPriority



PIDMWODATE HRS





of 3

DM22-Feb-1991


860.024-SEP-1991

LILLY, THOMASM

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

1-1520-237-50-59MWO:

Mnt LevelPriority

DN24-Mar-1988

LSI/MSC(PCW/JH5095)

3.027-SEP-1988

LILLY, THOMASM

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

55-1520-237-50-47MWO:

Mnt LevelPriority

DN09-Jun-1988

STAB AMPSYSTEMIMPROVEMENTS(PCW/JH5095)

92.028-JUN-1989

LILLY, THOMASM

INCORPORATION OF STABILATORAMPLIFIER IMPROVEMENTS(INCLUDES MODIFICATION OFSTABILIZATION TEST SET) (UH-60AHELICOPTERS)

55-1520-237-50-42MWO:

Mnt LevelPriority

DU31-May-1995


24.028-SEP-1995

LILLY, THOMASM

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

1-1520-237-50-73MWO:

Mnt LevelPriority

DN30-Jun-2004

USAACE, FT.RUCKER, AL(RJ0827)

1.029-OCT-2008

LILLY, THOMASM

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

1-1520-237-50-92MWO:

Mnt LevelPriority

DN15-Nov-1990


4.030-JUL-1991

LILLY, THOMASM

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

1-1520-237-50-61MWO:

Mnt LevelPriority

DN01-Aug-1991

DYNCORP=E(PCW/JH5095)

8.030-JUL-1991

LILLY, THOMASM

STAB GROUNDING STRAP55-1520-237-50-54MWO:

Mnt LevelPriority

DN15-Jan-1991


8.030-JUL-1991

LILLY, THOMASM

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

55-1520-237-50-58MWO:

Mnt LevelPriority

DR01-Jul-2008

CSC, USAACE,FT. RUCKER, AL.(RC1002(CFT128CSC) RC

30.031-Jul-2010

BELFORD, MAEP

INSTALLATION OF ELECTRONIC DATAMANAGEMENT SYSTEM (EDM) FORBLUE FORCE TRACKING (BFT)

RSN LSF01106MWO:

Mnt LevelPriority



NUMBER PIDENTRY

ORGANIZATION LOCATION8.7.

DATE6.

REMARKS4. 5.

EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL

Page 1 of 61

SIKORSKY, ACFTWAIVER (W0037)- AUTHORIZATION FORDELIVERY OF UNQUALIFIED ANTENNACOUPLERS AND LOW PASS FILTERS ANDINSTALLATION OF ARC-186 RADIO SETS(ACFT 570 & SUBSEQUENT). (MW3045)

05-Nov-1984 1

STRATFORD, CT

thomas.m.lilly

SIKORSKY. ACFTWAIVER (W0043)- AUTHORIZATION FORDELIVERY OF WITH ARC-186 RADIO SETSPRIOR TO APPORVAL OFELECTROMAGNECTIC COMPATABLILITY (ECM)TESTING (MW3045)

05-Nov-1984 2

STRATFORD, CT

thomas.m.lilly

SIKORSKY, ACFTNOTE: SOF MESSAGE THAT ARE N/A LISTEDFOR REFERENCE PURPOSES AS DIRECTEDBY NAVPRO LTR. 4855 S/N QAV/ 84-272 DATED05 NOV 84 (MW3045)

05-Nov-1984 3

STRATFORD, CT

thomas.m.lilly

SIKORSKY, ACFTUH-60A-84-01 N/A THIS ACFT. (MW3045) 05-Nov-1984 4

STRATFORD, CT

thomas.m.lilly

SIKORSKY, ACFTUH-60A-84-03 APPLIES TO UH-60A ACFT S/N 77-22714 THRU 82-23671. (MW3045)

05-Nov-1984 5

STRATFORD, CT

thomas.m.lilly

SIKORSKY, ACFTACFT M/R HEAD RIGGED I/A/W/SA DRAWING70400-00003 REV. E. SYSTEM CONTROLSHAVE BEEN BIASED IN ACCORD A. AFTCONTROL SERVO INPUT ROD HAS BEENLENGTHENED 1/2 TURN. B. LATERALCONTROL SERVO INPUT ROD HAS BEENLENGTHENED 3/8 TURN. (STEVE SMITH)SIKORSKY (MW3045)

08-Aug-1986 1

STRATFORD, CT

thomas.m.lilly

SIKORSKY, ACFTNOTE: WHEN ACFT RIGGING IS BIASEDRIGGING HOLES ARE TEMPORARILY LOST ATTHE ABOVE 3 POINTS. (MW3045)

08-Aug-1986 2

STRATFORD, CT

thomas.m.lilly

SIKORSKY, ACFTUH-60A-83-12 TB-55-1520-237-20-46-INSP OFT/R ASSY FOR BENT SERVO VALVE INPUTSTEM C/W. (STEVE SMITH) SIKORSKY(MW3045)

16-Aug-1986 1

STRATFORD, CT

thomas.m.lilly

SIKORSKY, ACFTUH-60A-84-02 TB-55-1520-237-20-48 ONE TIMEINSP OF WIRE HARNESS ROUTING FORFEEDER HARNESS BETWEEN #1 AND #2JUNCTION BOXES C/W. (STEVE SMITH)SIKORSKY (MW3045)

16-Aug-1986 2

STRATFORD, CT

thomas.m.lilly

SIKORSKY, ACFTUH-60A-85-02 SOF MAINT MANDATORY TOCHANGE THE AUTOROTATION ROM LIMITSC/W (STEVE SMITH) SIKORSKY, (MW3045)

16-Aug-1986 3

STRATFORD, CT

thomas.m.lilly

SIKORSKY, ACFTC/W SOF MESSAGE 291515Z DATED JUL 1986(UH-60A-86-12) TB55-1520-237-20-78 UH-60ACFT LOCATION AND CHANGE OUT OFLISTED S/N YAW AND COLLECTIVE BOOSTSERVO'S. (STEVE SMITH) SIKORSKY (MW3045)

16-Aug-1986 4

STRATFORD, CT

thomas.m.lilly

SIKORSKY, ACFTSOF 291415Z DATED JULY 86 (UH-60A-86-13)UH-60 SERIES ACFT, RMVL OF AN310-8 NUTS(STEVE SMITH) SIKORSKY (MW3045)

28-Aug-1986 1

STRATFORD, CT

thomas.m.lilly

SIKORSKY, ACFTC/W SOF MESSAGE 191300Z DATED AUG 1986(UH-60A-86-15) UH-/EH60A SERIES ACFT,REVISION TO RMVL OF AN310-8 NUTS, NSN5310-00-167-1289 (STEVE SMITH) SIKORSKY(MW3045)

28-Aug-1986 2

STRATFORD, CT

thomas.m.lilly

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, OCT 1991

NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 2 of 61

SIKORSKY, ACFTOCM/ACE PERFORMED AT 0009 ACFT HRS ATLAKEHURST NAS BY ACE TEAM MEMBER (K)AVSCOM OCM SEC ST LOUIS MO. (MW3045)

24-Sep-1986 1

STRATFORD, CT

thomas.m.lilly

SIKORSKY, ACFTSOF UH-60A-87-01 ONE TIME VALIDATION OFCOFFECT TORQUE OF T700 ENG FUELDIFFERENTIAL PRESSURE INDICATOR. C/W AT836 ACFT HRS. EH-60 MAINT MANAGER, TFSIMOJAVE AIRPORT, MOJAVE CA. 93501(MW3045)

16-Feb-1987 1

STRATFORD, CT

thomas.m.lilly

SIKORSKY ACFTONE TIME INSP OF INTERMEDIATE G/B TOVERIFY THE PRESENCE OF LUBE HOLE FORINPUT BEARINGS. INSP PERFORMEDACCORDING TO SIKORSKY E.I. NUM E70L-725-35-090- DATE: 08-19-87 G/B S/N A005-01253CENTER HOUSING S/N D315-00106 REV. B(SIKORSKY) (MW3045)

01-Sep-1987 1

STRATFORD, CT

thomas.m.lilly

HAWTHORN AVIATION55-1520-237-50-46 INSTAL. OF STAB. SLEW UPSWITCH ACCORDING TO CORR. LTR. DTD.02JUL1987 COMPLIED WITH @158.4 ACFT HRS(KM0000)

03-Nov-1987 1

FT. HUACHUCA

thomas.m.lilly

TFSI MOJAVE AIRPORTUH-60-88-ASAM-01 ALL H-60 SERIESAIRCRAFT INSPECTION FOR CERTAIN SERIALNUMBER T/R BLADE ASSY'S COMPLIED WITHAT 163.5 ACFT HRS (DM0000)

17-Feb-1988 1

MOJAVE, CALIFORNIA

thomas.m.lilly

TFSI MOJAVE AIRPORTUH-60-88-ASAM-02 ALL UH/EH-60 AIRCRAFTONE TIME INSPECTION OF THE T/R G/BOUTPUT SHAFT COMPLIED WITH @ 163.5ACFT HRS (DH0000)

06-Apr-1988 1

MOJAVE CA

thomas.m.lilly

TFSI MOJAVE AIRPORTUH-60-88-ASAM-03 ALL H-60 ACFT LIFEEXTENTION OF THE H-60 ACFT MAIN MODULESHAFT. C/W @ 163.5 ACFT HRS (AH0000)

23-May-1988 1

MOJAVE AIRPORTMAJOVE CA

thomas.m.lilly

EH60 MAINTSUPERVISOR TFSI

UH-60-88-ASAM-05 ALL H-60 SERIES ACFTINITIATION OF AUXILIARY POWER UNITMAXIMUM ALLOWABLE TIME (MAOT) INTERMS OF APU OPERATION HRS AND APUSTARTS COMPLIED WITH @ 192.1 ACFT HRS(SP0000)

27-Jun-1988 1

MOJAVE AIRPORT, CA

thomas.m.lilly

EH-60 MAINTSUPERVISOR TFSI

UH-60-99-ASAM-06 H-60 SERIES ACFT.OVERHAUL LIFE FOR THE TRANSMISSION OILCOOLER BLOWER COMPLIED WITH @ 211.9ACFT HRS (SP0000)

13-Jul-1988 1

MOJAVE AIRPORT,MOJAVE CA

thomas.m.lilly

EH-60 MAINT.SUPERVISOR TFSI

UH-60-88-ASAM-07 ALL H-60 SERIES ACFTREVISION TO SOF 88-05 CONCERNINGOPERATING TIME/START CALCULATIONS ANDFORMS INFO. COMPLIED WITH @ 213.1 ACFTHRS (SP0000)

25-Jul-1988 1

MOJAVE AIRPORT CA.

thomas.m.lilly

EH60 MAINTSUPERVISOR TFSI

UH-60-88-ASAM-08 H-60 ACFT REVISION TOOVERHAUL LIFE FOR THE TRANSMISSION OILCOOLER BLOWER COMPLIED WITH @ 214.6ACFT HRS (SP0000)

30-Jul-1988 1

MOJAVE AIRPORT, CA

thomas.m.lilly

EH MAINT SUPERVISORTFSI

55-1520-237-20-100 (UH-60-88-09) INSP. OF ARAMANUFACTURED CREW SEATS FOR LOOSECLEVIS SCREWS C/W @ 214.6 ACFT HRS(SP0000)

03-Aug-1988 1

MOJAVE AIRPORT, CA

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 3 of 61

CA-AVRADSOF GEN 88-02 ONETIME INSP FOR CORRECTINTERNAL PER TABLE FIRE EXT (GL0000)

21-Sep-1988 1

(NO LOCATION)

thomas.m.lilly

AVCRAD FAT55-1520-237-55-5 KIT #70219-02121 4-P ROLLABSORBERSINSTALLED BY AVCRAD FAT(SP0000)

08-Oct-1988 1

(NO LOCATION)

thomas.m.lilly

DA AVCARD55-1520-237-20-101 ( UH-60-88-10) INSP. OFTROOP / GUNNER SEAT AND 3 MAN MEDEVACSUPPORT ASSY. (SP0000)

12-Oct-1988 1

FRESCO CA

thomas.m.lilly

ACE TEAM MEMBERAVSCOM

OCM/ACE PERFORMED AT 289.0 ACFT HRS(TH0000)

18-Jul-1989 1

FITHEN, GERMANY

thomas.m.lilly

QUESTECH, INCAWR DATED 21 SEPT 1989, TO COMPLY WITHAWR THE DF ANTENNA HOUSINGINSULATORS WERE REPLACED WITH P/N 1951-1-4116-4. (SP0000)

21-Dec-1989 1

(NO LOCATION)

thomas.m.lilly

H CO 4TH AVN REGTSOF UH-60-90-01 ONE TIME & RECURRINGINSP OF M/R BLADE EXPANDIBLE PINSCOMPLIED WITH @ 418.6 ACFT HRS (HC0000)

23-Apr-1990 1

APO NY 09457

thomas.m.lilly

AVSCOM OCMSECOCM/ACE PERFORMED AT 465.0 ACFT HRS BYACE TEAM MEMBER K AVSCOM OCMSEC STLOUIS MO (RL0000)

31-Jul-1990 1

FINTHEN GERMANY

thomas.m.lilly

H CO 4TH AVN REGTSOF MSG UH-60A-90-02 ONE TIME INSP OF T/RPITCH BEAM RETAINING WASHER AND PITCHBEAM RETAINING NUT AND EMPHASIZEDRECURRING VISUAL INSPECTION C/W @ 471.0ACFT HRS ON 23 AUG 90. (RL0000)

28-Aug-1990 1

APO NY 09457

thomas.m.lilly

H CO 4TH AVN REGTINSP FOR DEFECTIVE ICE RATE INDICATORS(TB 55-1520-237-20-113) ON ALL H-60 ACFT C/W@ 471.0 ACFT HRS ON 27 AUG 90. (RL0000)

31-Oct-1990 1

APO NY 09457

thomas.m.lilly

H CO 4TH AVN REGTUH-60-91-ASAM-04 (TB 1-55-1520-237-20-122)ALL ACFT OPERATION IN SWA (DESERTSTORM) EXCEEDING THE RETIREMENT(FINITE) LIFE ON CERTAIN COMPONENTS NOTAPPLICABLE THIS ACFT AT 479.5 ACFT HRS(KG0000)

28-Feb-1991 1

APO NY 09457

thomas.m.lilly

H CO 4TH REGTUH-60-91-ASAM-05 (TB 55-1520-20-122)INSPECTION FOR FOUR UNSERVICEABLESPINDLES COMPLIED WITH @ 479.5 ACFT HRS(KG0000)

28-Feb-1991 2

APO NY 09457

thomas.m.lilly

H CO 4TH REGTUH-60-91-ASAM-07 ADVANCE NOTIFICATIONOF MANUAL CHANGES CONCERNING MAINTRANSMISSION MODULES C/W @ 502.8 ACFTHRS (DL0000)

05-Apr-1991 1

APO NY 09457

thomas.m.lilly

H CO 4TH REGTUH-60-91-ASAM-01 ONE TIME REPLACEMENTAND 30 HR SPECIAL INSPECTION OF THE TAILROTOR PITCH BEAM RETAINING WASHERCOMPLIED WITH @ 510.3 ACFT HRS (DL0000)

05-Apr-1991 2

APO NY 09457

thomas.m.lilly

H CO 4TH REGTGEN-ASAM-03 ALL EH-60A/EH-1H AND OH-58DACFT, AUTHORIZATION FOR INSTALLATIONAND USING CRYPTOGRAPHIC COMPUTER, KIT-1C COMPLIED WITH @ 510.3 ACFT HRS(RL0000)

16-Apr-1991 1

APO NY 09457

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 4 of 61

I CO 4TH AVN REGTH-60-91-ASAM-08 ONE TIME INSP OF FIREEXTINGUISHER SYSTEM, C/W @ 510.3 ACFTHRS (LK0000)

13-May-1991 1

APO NY 09185

thomas.m.lilly

I CO 4TH AVN REGTUH-60-91-ASAM-09 ONE TIME INSP. & INSP.PROCEDURE CHANGE OF M/R SPINDLEELASTOMETRIC BEARINGS C/W @ 510.3 ACFTHRS (LK0000)

13-May-1991 2

APO NY 91085

thomas.m.lilly

ACE TEAMOCM/ACE PERFORMED AT 541.0 ACFT HRS BYACE TEAM MEMBER FROM AVSCOM OCMSECST LOUIS, MO (NA0000)

30-Jul-1991 1

FINTHEN GERMANY

thomas.m.lilly

H CO 4TH AVN REGTUH-60-91-ASAM-10 (TB 1-1520-237-20-127) ONETIME INSPECTION AND REPLACEMENT OFMAIN LANDING GEAR, BRAKE ASSY PISTONINSULATOR COMPLIED WITH 5 AUG 91 AT543.8 ACFT HRS (KL0000)

05-Aug-1991 1

APO NY 09185

thomas.m.lilly

T TRP 4/11 ACRUH-60-92-ASAM-01, ONE TIME SER. NO.CHECK FOR DEFECTIVE SPINDLES COMPLIEDWITH @ 561.0 ACFT HRS ON 9 JAN 92 (TI0009)

09-Jan-1992 1

APO AE 09146

thomas.m.lilly

ACE TEAMOCW/ACE PERFORMED AT 608.0 ACFT HRS BYTEAM AVS COM OCMSEC. ST LOUIS MO.(CB0000)

13-Jul-1992 1

FULDA GERMANY

thomas.m.lilly

T TRP 4/11 ACRUH-60-92-ASAM-03 ENG CLEANING, ENG. LIFELIMITED COMPONENT TRACKING AND SINGLEENG. FLIGHT PLANNING PROCEDURECOMPLIED WITH 15 JUL 92 @ 608.9 ACFT HRS(TH0000)

15-Jul-1992 1

APO AE 09146

thomas.m.lilly

T TRP 4/11 ACRUH-60-92-ASAM-04 USE OFRECOVERY/RECYCLE EQUIPMENT ON ALL AIRCOND. OR REFRIG. SYSTEMS COMPLIED WITHON 15 JUL 92 @ 608.9 ACFT HRS (TH0000)

15-Jul-1992 2

APO AE 09146

thomas.m.lilly

T TRP 4/11 ACRUH-60-92-ASAM-05 INSP/REPLACEMENT OFM/R BLADE PINS COMPLIED WITH 21 AUG 92@ 617.4 ACFT HRS (TH0000)

02-Sep-1992 1

APO AE 09146

thomas.m.lilly

T TRP 4/11TH ACR( LATE ENTRY) PHASE #1 COMPLETED @ 491.5ACFT HRS. PHASE #2 DUE AT 991.5 ACFT HRS(TH0000)

07-Oct-1992 1

APO AE 09146

thomas.m.lilly

T TRP 4/11TH ACRUH-60-ASAM-06 INSP OF PEDAL ADJUSTERASSY HDWR COMPLIED WITH 25 SEP 92 @634.6 ACFT HRS (TH0000)

08-Oct-1992 1

APO AE 09146

thomas.m.lilly

T TRP 4/11TH ACRUH-60-ASAM-93-01 ONE TIME OPERATIONALOF THE TRANSMISSION AND GEARBOX CHIPDETECTOR COMPLIED WITH @ 647.0 ACFTHRS ON 9 OCT 92 (JI0000)

30-Nov-1992 1

APO AE 09146

thomas.m.lilly

C-CO 7/1 AVN3 DEG. BIAS IAW UH-60-93-ASAM-08COMPLIED WITH @ 687.5 ACFT HRSBLK=4.636, 4.963=.327/ YELLOW=4.029,4.376=.347/ RED=4.099, 4.415=.316/BLUE=4.667, 5.004=.337 (SC3577)

16-Apr-1993 1

APO AE 09250

thomas.m.lilly

C-CO 7/1 AVNUH-60-93-ASAM-12 INFORMATIONAL, ONETIME BRIEFING OF PILOTS/T'S M/R VIBRATIONCOMPLIED WITH @ 688.3 ACFT HRS (FA2050)

16-Apr-1993 2

APO AE 09250

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 5 of 61

C-CO7-1 AVNUH-60-93-ASAM-11 ONE TIME INSP OF H-60HELICOPTER CREW RESTRAINT, BUCKLE/CROTCH ASY COMPLIED WITH @ 688.3 ACFTHRS. (FA2050)

29-Apr-1993 1

APO AE 09250

thomas.m.lilly

C-CO 7-1 AVN REGTUH-60-93-ASAM-13 INFORMATIONAL BRIEF TOALL H-60(UH/EH/WH/) SERIES PILOTS,MAINTENANCE OFFICERS, TECNICALINSPECTORS AND CREWCHIEFS PRIOR TOTHE NEXT MISSION FLIGHT (FA2050)

10-Jun-1993 1

APO AE 09250

thomas.m.lilly

AVSCOM TEAMMEMBER

OCM/ACE PERFORMED AT 715.0 ACFT HRS ATKATTERBACH, GE BY TEAM MEMBERCHURCH AVSCOM OCM SEC ST LOUIS MO.(RC0000)

04-Aug-1993 1

KATTER BACHGERMANY

thomas.m.lilly

C-CO 7-1 AVNUH-60-93-ASAM-16 ONE TIME INSP OF HYD.PUMP MODULE KNURLED BLEED RELIEFKNOB SECURING PIN DUE N/L/T 17 AUG 93COMPLIED WITH @ 716.7 ACFT HRS ON 17AUG 93 (MM0000)

10-Sep-1993 1

APO AE 09250

thomas.m.lilly

C-CO 7-1 AVNLATE ENTRY UH-60-93-ASAM-07INFORMATIONAL T/R G/B SHAFT BOREEXPANDED CORROSION REPAIR LIMITCOMPLIED WITH @ 752.5 ACFT HRS ON 27OCT 93 (MM0000)

27-Oct-1993 1

APO AE 09250

thomas.m.lilly

C-CO 7-1 AVNLATE ENTRY UH-60-93-ASAM-90 ONE TIMEINSP TO DETERMINE COMPLIANCE WITHSYSTEM MWO'S COMPLIED WITH @ 688.3ACFT HRS 28 APR 93 (MM0000)

27-Oct-1993 2

APO AE 09250

thomas.m.lilly

C-CO 7-1 AVN APO AE09250

LATE ENTRY UH-60-92-ASAM-09 ONE TIMEINSP TO DETERMINE COMPLIANCE WITHSYSTEM MWO'S COMPLIED WITH @ 688.3ACFT HRS 28 APR 93 (MM0000)

28-Oct-1993 1

APO AE 09250

thomas.m.lilly

C-CO 7-1 AVNUH-60-94 ASAM-01 ONE TIME INSP OF MASTERWARNING PANELS FOR NVG COMPATIBILITY/REWORK, COMPLIED WITH @ 795.3 ACFTHRS. (MM0000)

22-Feb-1994 1

APO AE 09250

thomas.m.lilly

C-CO 7-1 AVNUH-60-94-ASAM-02 ONE TIME INSP OF ARALYNYARD PULL TYPE RELEASE BUCKLES P/ND4495-28 SER# 642 THRU 1058 IF INSTALLEDREPLACE C/W 780.9 ACFT HRS (MM0000)

22-Feb-1994 2

APO AE 09250

thomas.m.lilly

C-CO 7-1 AVNUH-60-ASAM-03 ONE TIMEREFURBISHEDMENT OF M/R SPINDLE ANDREPLACEMENT OF CERTAIN M/R THRUSTBEARINGS WITHIN 10 HRS/14 DAYS AWAITINGPMS2 (MM0000)

22-Feb-1994 3

APO AE 09250

thomas.m.lilly

C-CO 7-1 AVNUH-60-94-ASAM-05 INSP. OF COCKPITSTANDARDIZATION OF RESTRAINT RELEASESYSTEMS IN H-60 ACFT COMPLIED WITH 28FEB 94 @ 797.5 ACFT HRS. (MM0000)

22-Feb-1994 4

APO AE 09250

thomas.m.lilly

C-CO 7-1 AVNUH-60-94-ASAM-07 CHANGE TO H-60OVERHAUL AND RETIREMENT TABLE C/W 15MAR 94 AT 800.0 ACFT HRS ( TB 1-1520-237-20-154). (MM0000)

22-Feb-1994 5

APO AE 09250

thomas.m.lilly

C-CO 7-1 AVNUH-60-94-ASAM-08 REVISION TO ASAM-07 C/W11 APR 94 @ 822.4 ACFT HRS (MM0000)

11-Apr-1994 1

APO AE 09250

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 6 of 61

C-CO 7-1 AVNUH-60-94-ASAM-09 MAIN PRIMARY SERVO S/NVERIFICATION & INSP COMPLETED AT 822.4ACFT HRS (MM0000)

11-Apr-1994 2

APO AE 09250

thomas.m.lilly

C-CO 7-1 AVNUH-60-94-ASAM-10 REVISION TO 94-ASAM-03ONE TIME REFURBISHMENT OF M/R SPINDLEAND REPLACEMENT OF CERTAIN M/R THRUSTBEARING COMPLIED WITH 20 APR 94 AT 824.6ACFT HRS (MM0000)

21-Apr-1994 1

APO AE 09250

thomas.m.lilly

ACE TEAM MEMBERACE/AACE PERFORMED AT 856.0 A/C HRS ATKATTERBACH, GERMANY BY ACE TEAMMEMBER J AVSCOM AC/OCM (FS0000)

26-May-1994 1

KATTERBACH,GERMANY

thomas.m.lilly

A-CO 603RD ASBUH-60-94-ASAM-12 AUTHORIZATION FOR UH-60L ACFT TO BE UTILIZED FOR EXTERNALLOAD OPS N/A THIS ACFT @ 856.9 ACFT HRS(MM0000)

11-Jul-1994 1

APO AE 09250

thomas.m.lilly

C-CO 7-1 AVNUH-60-94-ASAM-11 INFO-M/R BLADE DE-ICEHEATER MATREST MEAS. TEST METHODUH/EH-60 SERIES ACFT C/W 20 APR 94 AT824.6 ACFT HRS (MM0000)

11-Jul-1994 2

APO AE 09250

thomas.m.lilly

D CO 7-1 AVNUH-60-95-ASAM-01 DELETION OF THE WORDS"HOIST POINT AND" FROM FWD TIEDOWNRINGS COMPLIED WITH AT 874.5 ACFT HRS(FS0000)

30-Nov-1994 1

APO AE 09250

thomas.m.lilly

D CO 7-1 AVNUH-60-95-ASAM-04 INSP OF PIVOT BOLTSREQ'D N/L/T 894.5 HRS OR 16 DEC 94 C/W 8DEC 94 AT 874.5 ACFT HRS (FS0000)

08-Dec-1994 1

APO AE 09250

thomas.m.lilly

D CO 7-1 AVNUH-60-95-ASAM003 INSP OF T/R BLADES BYSER NO. FOR PIVOT BEARING RESHIMMINGREQ'D N/L/T 2 DEC 94 C/W 16 NOV 94 (FS0000)

16-Dec-1994 1

APO AE 09250

thomas.m.lilly

D CO 7-1 AVNUH-60-95-ASAM-02 ACFT REQ. TO OPERATEWITH BOOST PUMPS ON AT ALL TIMES WITHALL FUELS C/W AT 874.5 ACFT HRS (FS0000)

27-Dec-1994 1

APO AE 09250

thomas.m.lilly

D CO 7-1 AVNUH-60-95-SOF-01 2 PART OF 3 PART SOFCOMPLETED ONE TIME RECORD ANDULTRASONIC INSP DUE ON ALL T/R G/BCOMPLIED WITH 20 JAN 95 (FS0000)

20-Jan-1995 1

APO AE 09250

thomas.m.lilly

D CO 7-1 AVNUH-60-95-ASAM-05 CHANGE IN RETIREMENTLIFE FOR SERVO BEAM RAILS (FS0000)

30-Jan-1995 1

APO AE 09250

thomas.m.lilly

D CO 7-1 AVNUH-60-95-SOF-02 ONE TIME INSP OF M/RBLADES FOR RETIREMENT LIFE CHANGE(FS0000)

08-Mar-1995 1

APO 09250

thomas.m.lilly

D CO 7-1 AVNUH-60-95-ASAM-06 ONE TIME INSP/RECURRING MAIN TRANSMISSION SUPPORTBEAMS FOR CRACKS OR WORKINGS.COMPLIED WITH AT 926.1 ACFT HRS (FS0000)

23-Jun-1995 1

APO AE 09250

thomas.m.lilly

D CO 7-1 AVNUH-60-95-ASAM-07 INSP OF TROOP/GUNNERSEAT ATTENUATION WIRE. SHIMMINGROLLERS. C/W @ 929.1 ACFT HRS (FS0000)

18-Jul-1995 1

APO AE 09250

thomas.m.lilly

ACE TEAM MEMBERACE/AACE PERFORMED AT 934.0 ACFT HRS(FS0000)

31-Aug-1995 1

APO AE 09250

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 7 of 61

A-CO 603RD ABSUH-60-96-SOF-01 CHANGE IN TBO TIME FORCERTAIN SERIAL NUMBERED BELLCRANKSUPPORT ASSY C/W AT 944.0 ACFT HRS(FS0000)

07-Nov-1995 1

APO AE 09250

thomas.m.lilly

A-CO 603RD ABSUH-60-96-ASAM-01 INSPECTION OF FLIGHTCONTROL PIVOT BOLTS C/W AT 946.0 ACFTHRS (FS0000)

27-Nov-1995 1

APO AE 09250

thomas.m.lilly

A-CO 603RD ABSUH-60-ASAM-02 INSPECTION OF MAIN ROTORSHAFT NUT BOLTS C/W AT 946.0 ACFT HRS(FS0000)

27-Nov-1995 2

APO AE 09250

thomas.m.lilly

A-CO 603RD ABSUH-60-SOF-02 ONE TIME INSP FORSUSPECTIAL ROTOR INBOARD RETENTIONPLATES C/W AT 946.0 ACFT HRS (FS0000)

27-Nov-1995 3

APO AE 09250

thomas.m.lilly

A-CO 603RD ABSUH-60-96-SOF-03 ALL UH/EH/MH-60 A/L/K ACFTCHANGE IN RETIREMENT LIFE OF M/R BLADECUFF COMPLIED WITH AT 946.0 ACFT HRS(FS0000)

06-Dec-1995 1

APO AE 09250

thomas.m.lilly

A CO 603RD ABSUH-60-96-SOF-04 INSPECT AFT BELLCRANKSUPPORT ASSY COMPLIED WITH AT 948.0ACFT HRS (FS0000)

13-Dec-1995 1

APO AE 09250

thomas.m.lilly

RAYTHEON CORPLATE ENTRY UH-60-95-ASAM-08 GASGENERATOR TURBINE ROTOR BLADE INFOCOMPLIED WITH (FS0000)

08-Jan-1996 1

APO AE 09250

thomas.m.lilly

RAYTHEONAEROSPACE

UH-60-96-ASAM-03 INSP OF M/R SHAFT BOLTSC/W AT 946.0 ACFT HRS (WM0000)

19-Jan-1996 1

APO AE 09250

thomas.m.lilly

RAYTHEONAEROSPACE

UH-60-96-ASAM-04 ALL UH-60 SERIES ACFTWITH FAST ROPE INSERTION/EXTRACTIONSYSTEM (FRIES) BAR INSTALLED UNDER AWRN/A THIS ACFT. (WM0000)

21-Feb-1996 1

APO AE 09250

thomas.m.lilly

RAYTHEONAEROSPACE

PMS II COMPLETED AT 946.0 ACFT HRS, NEXTPMS II DUE AT 1446 ACFT HRS. (WM0000)

13-Mar-1996 1

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-96-ASAM-05 INCREASE IN FATIGUE LIFEOF FWD SUPPORT ASSY COMPLIED WITH AT978.2 ACFT HRS (WM0000)

12-Jul-1996 1

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-96-ASAM-06 INSP OF RECORD FORSUPPORT SPINDLE RETAINING ROD P/N 70102-08102-102/103 C/W 27 AUG 96 AT 979.5 ACFTHRS (WM0000)

27-Aug-1996 1

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-96-ASAM-08 INCREASE IN FATIGUE LIFEOF THE AEREX T/R INBOARD RETENTIONPLATE C/W @ 980.7 ACFT HRS (WM0000)

04-Sep-1996 1

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-96-ASAM-06 INSP OF MAIN ROTORSPINDLE CRACKS . LATE ENTRY. (WM0000)

04-Sep-1996 2

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-96-ASAM-10 REPLACEMENT OFSPINDLE ELASTOMERIC BEARINGS TEFLONSLEEVE DURING PMS II C/W AT 911.5 ACFTHRS (WM0000)

13-Sep-1996 1

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-96-ASAM-11 INCREASE FATIGUE LIFEOF FENN MANUFACTURED M/R BLADE CUFFS,C/W 23 SEP 96 (MW3045)

23-Sep-1996 1

KATTERBACH, GE APOAE 09250

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 8 of 61

D-CO 2-1 AVNUH-60-96-ASAM-11 INCREASE FATIGUE LIFEOF FENN MANUFACTURED M/R BLADE CUFFSP/N 70150-09109-091/043 SN FM 0080 THRU0679 C/W AT 911.5 ACFT HRS (WM0000)

24-Sep-1996 1

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-02 ONE TIME INSP OF T/R D/SCOUPLINGS AND HARDWARE, COMPLIEDWITH AT 995.0 ACFT HRS (MW3045)

25-Oct-1996 1

KATTERBACK GE APOAE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-02 ONE TIME INSP OF T/R D/SCOUPLINGS AND HARDWARE, COMPLIEDWITH AT 995.0 ACFT HRS (WM0000)

25-Oct-1996 2

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-03 MANDATORY, T-700 ENGGG ROTOR ASSY SUBJECT REPL., COMPLIEDWITH AT 995.0 ACFT HRS (MW3045)

30-Oct-1996 1


thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-01 REWORK OF M/R HUBASSY EDGE BREAK AND NDI. COMPLIED WITHAT 1002.0 ACFT HRS (MW3045)

22-Nov-1996 1


thomas.m.lilly

D-CO-2-1 AVNUH-60-97-ASAM-01 REWORK OF M/R HUBASSY EDGE BREAK AND NDI COMPLIED WITHAT 1002.0 ACFT HRS (WM0000)

22-Nov-1996 2

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNSOF MSG UH-60-97-01 REMVL. OF CERTAINREWORKED M/R SWASHPLATE ASSY,COMPLIED WITH AT 1004.2 ACFT HRS(MW3045)

05-Dec-1996 1


thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-01 REMOVAL OF CERTAINREWORKED M/R SWASHPLATE ASSYCOMPLIED WITH AT 1004.2 ACFT HRS(WM0000)

05-Dec-1996 2

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-04 CHANGE IN RETIREMENTLIFE OF MAIN ROTOR BLADE CUFFS C/W @1065.0 ACFT HRSCFT HRS (WM0000)

31-Dec-1996 1

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-05 ONE TIME INSP FORREMOVAL AND REWORK OF CERTAINVISCOUS DAMPER ASSY., COMPLIED WITH AT1006.0 ACFT HRS (MW3045)

06-Jan-1997 1


thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-07 ALL H-60 ACFT, REPL OFSPECIFIC S/N T/R SERVOS N/L/T 10 HRS OR 14DAYS, COMPLIED WITH AT 1005.7 ACFT HRS(MW3045)

21-Jan-1997 1


thomas.m.lilly

D-CO9 2-1 AVNUH-60-97-ASAM-07 ALL H-60 ACFTREPLACEMENT OF SPECIFIC SERIALNUMBERED T/R SERVOS N/L/T 10 HRS/14 DAYC/W @ 1005.7 ACFT HRS (WM0000)

21-Jan-1997 2

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-07 INSP OF CERTAIN LATERALBELLCRANK ASSY REMOVAL, COMPLIEDWITH AT 1006.0 ACFT HRS (MW3045)

23-Jan-1997 1


thomas.m.lilly

D-CO 2-1 AVNUH-60-98-ASAM-08 INSP AND REMOVEAL OFCERTAIN CONNECTING LINK MANUFACTUREDBY PURDY, COMPLIED WITH AT 1006.0 ACFTHRS (MW3045)

24-Jan-1997 1


thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-06 INSP OF CERTAIN LATERALBELLCRANK ASSY REMOVAL C/W @ 1006.0ACFT HRS (WM0000)

24-Jan-1997 2

APO AE 09250

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 9 of 61

D-CO 2-1 AVNUH-60-97-ASAM-08 INSP AND REMOVAL OFCERTAIN CONNECTING LINK MANUFACTUREDBY PURDY C/W @ 1006 ACFT HRS (WM0000)

27-Jan-1997 1

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-98-ASAM-09 ALL H-60 ACFT WITH M/RSHAFT EXT ASSY WITH CERTAIN CAGECODES AND S/N MANUFACTURED BY PURDYCORP. OR FENN CO. HAVE REDUCED TIMELIFE COMPLIED WITH AT 1011.6 ACFT HRS(MW3045)

31-Jan-1997 1


thomas.m.lilly

D-CO 2-1 AVNUH-60-98-ASAM-09 ALL H-60 ACFT WITH M/RSHAFT EXT ASSY WITH CERTAIN CAGECODES AND S/N MANUFACT. BY PURDY CORPOR FENN HAVE REDUCED TIME LIFE C/W1011.6 ACFT HRS (WM0000)

31-Jan-1997 2

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNSOF MSG UH-60-98-01 (OPERATIONAL), UH/EH-60 ACFT RISK MANAGEMENT OF 230 GAL EXTTANK FLT OPERATIONS C/W 1088.3 ACFT HRS(WM0000)

03-Feb-1997 1

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-98-ASAM-10 ESTABLISHMENT OFFATIGUE LIFE FOR MAIN SUPPORT BRIDGEASSY, COMPLIED WITH AT 1020.0 ACFT HRS(MW3045)

19-Feb-1997 1


thomas.m.lilly

D-CO 2-1 AVNUH-60-98-ASAM-10 ESTABLISHEMENT OFFATIGUE LIFE FOR MAIN SUPPORT BRIDGEASSY C/W @ 1020 ACFT HRS (WM0000)

19-Feb-1997 2

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-98-ASAM-11 INCREASE IN FATIGUE LIFEFOR CERTAIN M/R BLADE CUFFS, COMPLIEDWITH AT 1022.0 ACFT HRS (MW3045)

10-Mar-1997 1


thomas.m.lilly

D-CO 2-1 AVNUH-60-97-11 INCREASE IN FATIGUE LIFE FORCERTAIN MAIN ROTOR BLADE CUFFS C/W @1022 ACFT HRS (WM0000)

10-Mar-1997 2

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-12 RESTORATION OF LIFE OFT/R INBOARD RETENTION PLATE C/W @1023.0 ACFT HRS (WM0000)

16-Apr-1997 1

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-ASAM-13, 1X INSP OF M/R SPINDLESPHERICAL BRNG FOR EXIST. OF INNERSLEEVE C/W @ 1032.4 ACFT HRS (WM0000)

19-Jun-1997 1

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-17 ONE TIME INSPECTION OFINTERNAL RESECUE HOSET BRACKET ASSY.C/W @ 1049.4 ACFT HRS (WM0000)

15-Aug-1997 1

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-14 ONE TIME INSPECTION OFBELLCRANK SUPPORT P/N 70400-08158-101COMPLIED WITH AT 1049.4 ACFT HRS (SH6210)

18-Aug-1997 1


thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-15 ONE TIME INSPECTION OFLOWER M/R P/C ROD END P/N 70101-08202-101COMPLIED WITH AT 1049.4 ACFT HRS (SH6210)

18-Aug-1997 2


thomas.m.lilly

D-CO AVNUH-60-97-ASAM-16 ONE TIME INSPECTION OFLATERAL SWASHPLATE LINK P/N 70400-08151-050 COMPLIED WITH AT 1049.4 ACFT HRS(SH6210)

18-Aug-1997 3


thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 10 of 61

D-CO 2-1 AVNUH-60-97-ASAM-17 ONE TIME INSPECTION OFINTERNAL RESCUE HOIST PRACKET ASSY,COMPLIED WITH AT 1049.4 ACFT HRS (SH6210)

18-Aug-1997 4


thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-14 ONE TIME INSPECTION OFBELLCRANK SUPPORT P/N 70400-08158-101COMPLIED WITH @ 1049.4 ACFT HRS(WM0000)

18-Aug-1997 5

APO AE 09250

thomas.m.lilly

D-CO 2-1 ANVUH-60-97-ASAM-15 ONE TIME INSPECTION OFLOWER M/R P/C ROD END FOR P/N 70101-08207-101. C/W @ 1049.4 ACFT HRS (WM0000)

18-Aug-1997 6

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-16 ONE TIME INSPECTION OFLATERAL SWASHPLATE LINK PN 70400-08151-050. C/W @ 1049.4 ACFT HRS (WM0000)

18-Aug-1997 7

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-18 VISUAL INSPECTION OFM/R SWASHPLATE OUTER DIAMETERSURFACE. COMPLIED WITH AT 1067.0 ACFTHRS (SH6210)

12-Sep-1997 1


thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-18 VISUAL INSPECTION OFM/R SWASHPLATE OUTER DIAMETER/SURFACE. COMPLIED WITH @ 1067 ACFT HRS(WM0000)

12-Sep-1997 2

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-19 ONE TIME INSPECTION OFANVIS/HUD POWER SUPPLY, COMPLIED WITHAT 1066.5 ACFT HRS (SH6210)

03-Oct-1997 1


thomas.m.lilly

D-CO 2-1 AVNUH-60-97-ASAM-19 ONE TIME INSP OFANVIS/HUD POWER SUPPLY C/W @ 1066.5ACFT HRS (WM0000)

03-Oct-1997 2

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-98-ASAM-01 REVISION OF M/R SHAFTEXTENSION ASSY SERVICE LIFE. COMPLIEDWITH AT 1068.0 ACFT HRS (SH6210)

07-Oct-1997 1


thomas.m.lilly

D-CO 2-1 AVNUH-60-98-ASAM-01 REVISION OF M/R SHAFTEXTENSION ASSY SERVICE LIFE. C/W @ 1068ACFT HRS (WM0000)

07-Oct-1997 2

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-98-ASAM-02 ONE TIME INSPECTION OFPUSHRODS P/N 70400-08155-050/051COMPLIED WITH AT 1070.2 ACFT HRS (SH6210)

21-Oct-1997 1


thomas.m.lilly

D-CO 2-1 AVNUH-60-98-ASAM-02 ONE TIME INSP OFPUSHRODS PN70400-08155-050&051COMPLIED WITH AT 1070.2 ACFT HRS(WM0000)

21-Oct-1997 2

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVNUH-60-98-ASAM-03 ONE TIME INSPECTIONFOR SWASH PLATE LINK ASSY P/N 70400-08110-054 COMPLIED WITH AT 1071.2 ACFTHRS. (SH6210)

04-Nov-1997 1


thomas.m.lilly

D-CO 2-1 AVNUH-60-98-SOF-01 ACFT RISK MANAGEMENTOF 230 GALLON EXTERNAL TANKS FLIGHTOPERATIONS (SH6210)

03-Feb-1998 1

KATTERBACK, GE APOAE

thomas.m.lilly

D-CO 2-1 AVNTB1-1520-237-20-205 (UH-60-98-ASAM-04) INSPFOR LOOSE HUCK BOLTS ON OVERHAULEDPRIMARY, YAW BOOST, COLLECTIVE BOOST,AND T/R SERVOS. (WM0000)

12-Mar-1998 1

APO AE 09250

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 11 of 61

D-CO 2-1 AVNUH-60-98-ASAM-12 RESTORATION OF LIFE OFT/R INBOARD RETENTION PLATE, COMPLIEDWITH AT 1023.0 ACFT HRS. (MW3045)

16-Apr-1998 1

KATTERBACK, GE APOAE 09250

thomas.m.lilly

D-CO 2-1 AVNTB1-1520-237-20-203 (UH-60-98-ASAM-05) ALLUH-60 AIRCRAFT WITH THE SWASHPLATELINK ASSY. P/N:70400-08110-054/061MANUFACTURED BY TEK (CAGE CODE 65780)C/W AT ACFT. HRS. (SH6210)

15-May-1998 1

DATTERBACH, GE APOAE 09250

thomas.m.lilly

D CO 2-1 AVNTB1-2840-248-20-22 (UH-60-99-ASAM-03) ONETIME INSP OF T700-GE-700/701/701C ENGINES.(MW3045)

20-Nov-1998 1

APO AE 09250

thomas.m.lilly

D CO 2-1 AVN REGTUH-60-99-ASAM-04 INFORMATIONAL TO RELAYTHAT THERE HAS BEEN AN UPGRADE TOCURRENT ODV**S. N/A TO THIS ACFT (AP5959)

02-Dec-1998 1

APO AE 09250

thomas.m.lilly

D CO 2-1 AVN REGTTB1-1520-237-20-209 (UH-60-99-ASAM-05) ONETIME INSP OF M/R SPINDLE BEARING ASSYFOR EXISTENCE OF SLEEVE BEARING.(AP5959)

08-Dec-1998 1

APO AE 09250

thomas.m.lilly

D CO 2-1 AVNTB1-1520-237-20-210 (UH-60-99-ASAM-06)INSPECTION AND REVISED RETIREMENT LIFEOF M/R PITCH HORNS P/N 70102-08111-047(CN9073)

11-Dec-1998 1

APO AE 09250

thomas.m.lilly

D CO 2-1TB1-1520-237-20-211 (UH-60-99-ASAM-08)REVISED RETIREMENT LIFE OF FWDBELLCRANK SUPPORT ASSY, PN 70400-08162-042/043/045 (MU1539)

18-Jun-1999 1

APO AE 09250

thomas.m.lilly

D CO 201 AVNTB1-1520-237-20-212 (UH-60-99-ASAM-07) INSPOF M/R HUB (NDI). (DP8686)

04-Aug-1999 1

APO AE 09250

thomas.m.lilly

D CO 2-1 AVNUH-60-99-ASAM-12 INSPECTION INTERVALCHANGE FOR HAMILTON STANDARD HMU**SP/N 4046T52G01, G04, G06, G09 AND G11 USEDON THE T700-GE-700 ENGINE. (CN2162)

24-Aug-1999 1

KATTERBACH GE APOAE 09250

thomas.m.lilly

D CO 2-1 AVNTB1-1520-237-20-214 (UH-60-99-ASAM-09) ONETIME INSP OF THE M/R BLD EXPANDABLE PIN.(DP8686)

04-Sep-1999 1

APO AE 09250

thomas.m.lilly

D CO 2-1 AVNTB1-1520-237-20-213 (UH-60-99-ASAM-10) INSPAND PREVENTIVE MAINTENANCE ON THE #2CROSSFEED BREAKAWAY VALVE. (DP8686)

04-Sep-1999 2

APO AE 09250

thomas.m.lilly

D CO 2-1 AVNUH-60-99-ASAM-11 UPDATE THE SERVICE LIFEOF SOME ROTQATING COMPONENTS IN THET700-GE-700/701C ENGINES. C/W AT 1366.3ACFT HRS BY SSG WHITE (MW3045)

12-Sep-1999 1

APO AE 09250

thomas.m.lilly

D-CO 2-1 AVN,KATTERBACH, GE APOAE 09250

UH-60-99-ASAM-02 INSP OF EXT. RESCUEHOIST, N/A THIS ACFT (MW3045)

04-Nov-1999 1

KATTERBACH, GE APOAE 09250

thomas.m.lilly

D CO 2-1 AVNTB1-1520-237-20-208 (UH-60-99-ASAM-01)RESTORATION OF FULL SERVICE LIFE ON THESWASHPLATE LINK ASSY. P/N:70400-08110-054/061, MFG'D BY TEK (CAGE CODE 65780)C/W AT ACFT. HRS. (WM0000)

04-Nov-1999 2

APO AE 09250

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 12 of 61

D CO 2-1 AVNTB1-1520-237-20-216 (UH-60-00-ASAM-02)CYCLIC STICK WIRING BUNDLE RELOCATION.(MU1539)

03-Jan-2000 1

APO, AE 09250

thomas.m.lilly

D CO 2-1 AVNTB1-1520-237-20-217 (UH-60-00-ASAM-03) INSPAND REPL OF SUSPECT PRIMARY SERVOASSEMBLIES. (HM2040)

06-Jan-2000 1

APO, AE 09250

thomas.m.lilly

D CO 2-1 AVNTB1-1520-237-20-218 (UH-60-00-ASAM-04) INSPOF T/L/G SHOCK STRUT FOR MISSINGBEARING RETENTION PIN. (MK7715)

07-Mar-2000 1

APO, AE 09250

thomas.m.lilly

A CO 601 DASBTB1-1520-237-20-219 (UH-60-00-ASAM-05) INSPOF FIRE EXTINGUISHER WIRING. (DW4596)

22-May-2000 1

APO, AE 09250

thomas.m.lilly

AMCOM PROJECT OLRTB1-1520-237-20-232 (SOF UH-60-01-08) INSPOF M/R FLIGHT CONTROL SELF-LOCKINGBOLTS. (DW4596)

15-Jun-2000 1

HAAF, GA 31409

thomas.m.lilly

A CO 601 DASBUH-60-00-ASAM-06 INSPECTION OF FIREEXTINGUISHER WIRING (CHANGE TO 00-ASRM-05) C/W 1435.Y (LL3858)

28-Jun-2000 1

PAO, AE 09250

thomas.m.lilly

A CO 601 DASBTB1-1520-237-20-221 (SOF UH-60-00-01) INSPOF M/R SPINDLE LUGS (RP8646)

12-Jul-2000 1

APO, AE 09250

thomas.m.lilly

A CO 601 DASBPMS II COMPLETED AT 1435.6 ACFT HRS NEXTPHASE DUE AT 1935.6 ACFT HRS (LL3858)

12-Jul-2000 2

APO, AE 09250

thomas.m.lilly

AMCOM-E OLR,HUNTSVILLE, AL

ACE/CPCE PERFORMED AT 1442.9 ACFT HRSAT KATTERBAC H, GERMANY BY MEMBERSS4CC (IK3963)

24-Oct-2000 1

KATTERBACH, GE

thomas.m.lilly

D/2-1 AVN REGT APO AE09250

SOF UH-60-01-01 INSPECT MAIN LANDINGGEAR DRAG BE AMS C/W (JT5515)

05-Nov-2000 1

APO, AE 09250

thomas.m.lilly

D/2-1 AVN REGTSOF UH-60-01-02 REVISION OF SOF UH-60-01-01 C/W (JT5515)

28-Dec-2000 1

APO, AE 09250

thomas.m.lilly

D/2-A AVN REGTTB1-1520-237-20-229 (SOF UH-60-01-03)REMOVAL OF LATERAL SERVO BELLCRANKASSY. MANUFACTURED BY PURDY MACHINECOMPANY, CAGE CODE 15152 (JT5515)

05-Jan-2001 1

APO AE 09250

thomas.m.lilly

D/2-1 AVN REGTTB1-1520-237-20-228 (SOF UH-60-01-04), RISKMANAGEMENT OF 230 GALLON EXTERNALTANK FLIGHT OPERATIONS. (JT5515)

05-Jan-2001 2

APO AE 09250

thomas.m.lilly

D/2-1 AVN REGTSOF UH-60-01-05 INSP OF M/R SPINDLEWITHIN 100 HRS BUT, NLT 3 JUL 01 C/W(JT5515)

05-Mar-2001 1

APO AE 09250

thomas.m.lilly

D/2-1 AVN REGTSOF UH-60-01-06 INSP OF SAS ASSY PRIOR TONEXT FLT C/W (JT5515)

26-Mar-2001 1

APO AE 09250

thomas.m.lilly

D/2-1 AVN REGTSOF UH-60-01-07 INSP M/R FLT CONTROLSELF LOCKING BOLTS C/W (JT5515)

29-May-2001 1

APO AE 09250

thomas.m.lilly

D/2-1 AVN REGTSOF UH-60-01-08 INSP M/R FLT CONROL SELFLOCKING BOLTS C/W (JT5515)

01-Jun-2001 1

APO AE 09250

thomas.m.lilly

D/2-1 AVN REGTSOF UH-60-01-09 INSP M/R EXPANDABLE PINSC/W (JT5515)

08-Jun-2001 1

APO AE 09250

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 13 of 61

D 2-1 AVN REGTSOF UH-60-01-10 INSPECT ALL H-60 ACFT FORAPEX MANUFACTURED M/R BLADE PINS(JT5515)

01-Jul-2001 1

APO AE 09250

thomas.m.lilly

D CO 2-1 AVN REGTINSPECT ALL H-60 ACFT FOR APEXEXPANDABLE PINS (JT5515)

19-Jul-2001 1

APO AE 09250

thomas.m.lilly

D CO 2-1 AVN REGTSOF UH-60-01-11 INSPECT M/R HUB IAW UH-60-01-11 (TB1-1520-237-20-235) PRIOR TO NEXTFLT BUT N/L/T 07-SEP-2001 C/W. (MB5388)

24-Aug-2001 1

APO AE 09250

thomas.m.lilly

D CO 2-1 AVN REGTSOF UH-60-01-12 INSPECT M/R EXPANDABLEPINS FOR CHANGE IN TENSION C/W. (MB5388)

24-Sep-2001 1

APO AE 09250

thomas.m.lilly

D CO 2-1 AVN REGTUH-60-02-ASAM-01 INSPECT T/R FAIRING FORINJECTION MOLDED PLASTIC ORFIBERGLASS C/W 16-NOV-01 (MB5388)

15-Nov-2001 1

APO AE 09250

thomas.m.lilly

D/ 2-1 AVNUH-60-02-SOF-01 INSPECTION OF AIL COOLERFLANGE HARDWARE IN ACFT THAT HAVE NOTCOMPLETED PMS-2 C/W (MB5388)

17-Nov-2001 1

APO, AE 09250

thomas.m.lilly

D CO 2-1 AVN REGTSOF UH-60-02-02 INSP M/R HUB FOR SPECIFICPART NUMBERS TO IDENTIFY IF REWORDEDOR REWORKABLE. HUB REPLACEMENT DUEPRIOR TO OR DURING NEXT PMS II BUT N/L/T20040930. C/W. (DP8686)

07-Dec-2001 1

APO, AE 09250

thomas.m.lilly

D CO 2-1 AVN REGTSOF UH-60-02-03 INSPECT PITCH TRIM SERVOFOR PROPER INSTALLATION OF CLEVIS PINC/W AT 1476.5 ACFT HRS ON 20011211 (JT5515)

11-Dec-2001 1

APO, AE 09250

thomas.m.lilly

D CO 2-1 AVN REGTSOF UH-60-02-04 (TB1-1520-237-20-242) ONETIME INSP OF ALL UH-60 ACFT FOR PROPERGROMMET INSTALLATION ON APU SHROUDASSY (APU FUEL LINE) C/W. (TG0232)

26-Jan-2002 1

APO, AE 09250

thomas.m.lilly

D CO 2-1 AVN REGTUH-60-02-SOF-05, INSP M/R EXPANDABLE PINSFOR PROPER SWAGED PINS C/W 20020205 @1477.5 ACFT HRS (TL1252)

06-Feb-2002 1

APO, AE 09250

thomas.m.lilly

D CO 2-1 AVN REGTASAM UH-60-02-03 INSPECT ENGINE PCLQUADRANT BEFORE NEXT PMS-2 NLT 15 FEB05 C/W (JT5515)

13-Feb-2002 1

APO, AE 09250

thomas.m.lilly

USAAVNC,TB1-1520-237-20-245 (UH-60-02-ASAM-03)INSPECTION OF ENGINE CONTROLQUADRANT POWER CONTROL LEVER (PCL)WIRING. (JH5095)

18-Feb-2002 1

FORT RUCKER, AL

thomas.m.lilly

D CO 2-1 AVN REGTASAM UH-60-02-02 INSPECT M/R FLTCONTROL RODS FOR CRACKED JAMNUTSC/W 20020208 @ 1480.8 ACFT HRS (JT5515)

19-Feb-2002 1

APO, AE 09250

thomas.m.lilly

D/ 2-1 AVN REGTASAM-UH-60-02-04 INSP RESTRAINT SYS FORPACIFIC SCIENTIFIC MANUFACTUREDRESTRAINTS BETWEEN JUN-95 TGRY MAR-01(TL1252)

15-Mar-2002 1

APO, AE 09250

thomas.m.lilly

D/ C0 2-1 AVN REGTASAM-UH-60-02-05 REPLACE ALL M/RSPINDLE ASSY. THAT WHEREMANUFACTURED BY CHICAGO RAWHIDES/N**S C325-0001 THRU C325-02407 (TL1252)

26-Mar-2002 1

APO, AE 09250

thomas.m.lilly

D CO 2-1 AVN REGTUH-60-02-ASAM-06 H-60 SERIES, COLLECTIVEAND YAW BOOST SERVO ASSEMBLIESSWAGE PIN COLLARS. TB1-1520-27-20-252C/W AT 1482.8 ACFT HRS. (TL1252)

22-Apr-2002 1

APO, AE 09250

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 14 of 61

D CO 2-1 AVN REGTUH-60-02-SOF-07 MAIN MODULE PLANETARYCARRIER ASSY SUPERCEDED BY UH-60-02-SOF-08 14832.2 ACFT HRS (TL1252)

02-May-2002 1

APO, AE 09250

thomas.m.lilly

D CO 2-1 AVN REGTUH-60-02-SOF-08 MAIN MODULE PLANETARYCARRIER ASSY (TB1-1520-237-20-255) C/W AT1482.2 ACFT HRS. (TL1252)

04-May-2002 1

APO, AE 09250

thomas.m.lilly

D CO 2-1 AVN REGTUH-60-02-SOF-09 UH-60A/Q & EH-60A MAINMODULE PLANETARY CARRIER ASSY. (TB1-1520-237-258) C/W AT 1482.8 ACFT HRS.(TL1252)

22-May-2002 1

APO, AE 09250

thomas.m.lilly

AMCO PROJECT OLREAST

UH-60-02-SOF-10 UH-60A & EH-60A MAINMODULE PLANETARY CARRIER ASSY, (RAF)C/W AT 1483.8 ACFT HRS (PG4153)

07-Jun-2002 1

HAAF, GA 31409

thomas.m.lilly

AMCO PROJECT OLDRUH-60-02-ASAM-08 UH-60 SERIES ACFT,INSPECT AN/ARC-220 WIRING FOR CHAFFING(TB1-1520-237-20-256) N/A THIS ACFT. ARC-220NOT INSTALLED (DW4596)

12-Jun-2002 1

HAAF, GA 31409

thomas.m.lilly


UH-60-02-ASAM-09, H-60 ACFT TAIL ROTORQUADRANT HARDWARE INSTALLATION. (TB1-1520-237-20-257) COMPLIED WITH AT 1483.8ACFT HRS (DW4596)

13-Jun-2002 1

HAAF, GA 31409

thomas.m.lilly


UH-60-02-SOF-11-H-60 SERIES ONE-TIMEINSPECTION OF MAIN ROTOR BLADE CUFFASSY. SPERCEDED BY UH-60-02-SOF-12(PG4153)

09-Aug-2002 1

HAAF, GA 31409

thomas.m.lilly


UH-60-02-SOF-12 H-60 SERIES REVISION TOUH-60-02-SOF-11, ONE-TIME INSPECTION OFMAIN ROTOR BLADE CUFF ASSEMBLYCOMPLIED WITH AT 1483.8 ACFT HRS(DW4596)

27-Aug-2002 1

HAAF, GA 31409

thomas.m.lilly

USAAVNCACFT. ARRIVED AT USAAVNC, FT. RUCKER, AL.ON 05SEP02 WITH 1487.3 ACFT HRS. FROMGERMANY, ACFT WENT TO HAAF, SAVANNAH,GA. FOR EH DE-MOD. NO ACCEPTANCE INSP.WAS COMPLETED BY DYNCORP PERSONNELFROM THIS LOCATION. (MF4187)

05-Sep-2002 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCACFT OPERATING UNDER AWOR REL DTD13MAY02 FOR SPECIFIED EH60 ACFT TOOPERATE WITH ALL MISSION EQUIPMENTREMOVED AND SELECTED EQUIPMENTINSTALLED(SEE AWOR REL). THIS AWOR RELSUPERCEDES AWOR REL'S WITH SAMESUBJECT DTD 15JAN02, 06JUN01 AND 21NOV00. (MF4187)

05-Sep-2002 2

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCTB1-1520-237-20-261 (UH-60-02-ASAM-11)INSPECT AN/ARC-220 WIRING FOR CHAFINGC/W AT 1499.0 ACFT HRS. (JH5095)

24-Sep-2002 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCWHILE AT A HOVER AND PILOT RELEASEDTRIM SWITCH A/C ROLLED RIGHT. DURINGSHUTDOWN WHEN SAS 1 WAS DE-SELECTEDA/C JERKED. REPLACED ROLL TRIM SERVOAT 1499.3 ACFT. HRS. (MF4187)

27-Sep-2002 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCACFT 8524475 PLACED IN SHORT TERMSTORAGE (1-45 DAYS). ACFT HRS 1548.0.(JH5095)

26-Nov-2002 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 15 of 61

USAAVNCUH-60-03-ASAM-01 FWD BELLCRANKSUPPORT ASSY RETIREMENT LIFE C/W AT1548 ACFT HRS. (JH5095)

09-Dec-2002 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCUH-60-03-ASAM-02 TAIL ROTOR SERVO ASSYRETIREMENT LIFE C/W AT 1548 ACFT HRS.(JH5095)

09-Dec-2002 2

FT. RUCKER, AL

thomas.m.lilly

USAAVNCGEN-03-ASAM-01 (SINCGARS) ARC-201BATTERY BOX (JH5095)

17-Dec-2002 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCAWOR REL 13 MAY 02(2) INSTALLATION OFTHE DOPPLER/GPS AN/ASN-128B C/W THISDATE AT 1548 ACFT HRS. (JH5095)

24-Jan-2003 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCAWOR REL 13MAY02(3) INSTALLATION OF THEPROVISIONS FOR THE INSTALLATION OF ACARGO HOOK C/W THIS DATE AT 1548 ACFTHRS. (JH5095)

24-Jan-2003 2

FT. RUCKER, AL

thomas.m.lilly

USAAVNCAWOR REL 13MAY02 (1) INSTALLATION OFTHE PROVISIONS FOR THE INSTALLATION OFTHE ANVIS/HUD AN/AVS-7 C/W THIS DATE AT1548.0 ACFT HRS. (JH5095)

24-Jan-2003 3

FT. RUCKER, AL

thomas.m.lilly

USAAVNCTB1-1520-237-20-242 (SOF UH-60-02-04),INSPECT APU FUEL LINES FOR PROPERGROMMET AT APU SHROUD ASSY. (JH5095)

28-Jan-2003 1

FT. RUCKER, AL

thomas.m.lilly

DYNCORP PROJECTGOLR FT. CAMPBELL, KY

OCM/ACE PERFORMED AT 1658 ACFT HR BYTEAM MEMBER QQ AM COM PROJECT OLR(LS2032 L. SANDERS)

18-Mar-2003 1

FORT CAMPBELL, KY

thomas.m.lilly

USAAVNCACFT OPERATING UNDER AWORTHINESSRELEASE DTD 06JUN03 (EH-60 DE-MOD)WHICH SUPERSEDES AWOR RELEASES DTD11OCT02, 13MAY02, 15JAN02, 06JUN01 AND21NOV00. A COPY OF THE AWOR REL ISLOCATED IN THE BACK OF THIS HISTORICALBOOK. AWR 927 R5. (JH5095)

19-Jun-2003 1

FORT RUCKER, AL

thomas.m.lilly

USAAVNCSOF UH-60-04-01, INSP OF FORWARDBELLCRANK SUPPORT INSTALLATIONHARDWARE. C/W AT 1722.0 ACFT HRS (LW2720R/SPEC)

02-Oct-2003 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCACFT OPERATING UNDER AWOR RELEASE#1153 DTD 31 DEC 03 (JP-8+100) (JB2761R/SPEC)

07-Jan-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG. 70400-0003REV.E. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD. A. AFT CONTROL SERVOINPUT ROD HAS BEEN LENGTHEN 1/2 TURN.B. LATERAL CONTROL SERVO INPUT RODHAS BEEN SHORTEN 1 1/2 TURN. C. FORWARDCONTROL SERVO INPUT ROD HAS BEENSHORTEN 1/2 TURN AT 1722.0 ACFT HRS(LW2720 R/SPEC)

21-Jan-2004 1

FT. RUCKER, AL

thomas.m.lilly

DYNCORP PROJECTOCM/ACE PERFORMED AT 1753 ACFT HRS BYTEAM MEMBER UU AM COM PROJECT OLR(HM9565)

17-Mar-2004 1

OLR FT.C. KY

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 16 of 61

USAAVNCUH-60-04-ASAM-02, INSP OF T/R D/SHAFTFLANGE NUT. C/W AT 1793 ACFT HRS (LW2720R/SPEC)

01-Apr-2004 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNC,UH-60-04-ASAM-01 GLARE SHIELD LIGHTINGCIRCUIT BREAKER REPLACEMENT C/W AT1834.7 ACFT HRS. (IP2860, R/SPEC)

12-Apr-2004 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCSOF UH-60-04-02 DISABLING OF COCKPITAIRBAG SYSTEM C/W AT 1931.8 ACFT. HRS.(JB2761 R/SPEC)

10-Jun-2004 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCTB1-1520-237-20-167 INSP AND REPAIR OFSTATION 635 FRAME ASSY FOR TAIL WHEELSTRUT COMP. @ 1931.8 ACFTHRSINSTALLATION CLEARANCE. (JB2761R/SPEC)

24-Jun-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCTEST ATLTIMETER SYSTEM,ALTITUDEREPORTING EQ. & TRANSPONDERS I/A/WCOR LETTER DTD 29AUG 00 & DPC 5660COMPLETED @ 1931.8 ACFT HRS. THIS DATE(JB2761 R/SPEC)

04-Jul-2004 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCUH-60-04-ASAM-03 FUEL SYSTEM INTEGRITYCHECKS C/W AT ACFT HRS C/W AT 1931.8ACFT. HRS. (JB2761 R/SPEC)

07-Jul-2004 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNC,ACFT MAIN ROTOR HEAD RIGGED I/A/W SADWG. 70400-00003 REV. E. SYSTEMCONTROLS HAVE BEEN BIASED IN ACCORD.(A) AFT CONTROL SERVO INPUT ROD HASBEEN LENGTHENED 1/2 TURN. (B) LATERALCONTROL SERVO INPUT ROD HAS BEENSHORTENED 1/2 TURN. (C) FORWARDCONTROL SERVO INPUT ROD HAS BEENSHORTENED 1/2 TURN. @ 1931.8 ACFT HRS.(JB2761 R/SPEC)

10-Jul-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCPMS2 PHASE INSP # 4 CPMPLETER ON THISDATE @ 1931.8 ACFT HRS NEXT PHASE #5DUE ON 2431.8 ACFT HRS. (JB2761 R/SPEC)

13-Jul-2004 1

FT. RUCKER,AL

thomas.m.lilly

USAAVNC,UH-60-04-ASAM-04, REVISION TO UH-60-04-ASAM-03, FUEL SYSTEM INTEGRITY CHECKSC/W AT 1968.1 ACFT. HRS. (MF4817 R/SPEC.)

13-Aug-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCSOF UH-60-04-04 TECHNICAL, RCS CSGLD-1860 (R1), H-60 MAIN ROTOR HUBSUBASSEMBLY REWORK, UH-60-60-04-04 C/WAT 1968.1 ACFT. HRS. (MF4187 R/SPEC.)

14-Aug-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-MIM-04-008 INSPECTION OF WIRINGAND REPAIR TO POWER WIRING ANDINSULATION SLEEVING OF AIRCRAFTRETRACTABLE LANDING LIGHT C/W AT 1973.7ACFT. HRS. (MF4187 R/SPEC.)

17-Aug-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-04-ASAM-05, RESTRAINT SYSTEMINSPECTION C/W AT 2068.9 ACFT. HRS.(MF4187 R/SPEC.)

24-Sep-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCCHANGED FROM PMS-2 TO PMD ANDINTERVAL INCREASED FROM 500 TO 700 HRS.I/A/W AWR 1220 @ 2157.1 ACFT. HRS. NEXTPHASE #5 DUE @ 2631.8 ACFT. HRS. (MF4187R/SPEC.)

22-Oct-2004 1

FT. RUCKER, AL.

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 17 of 61

USAAVNCFOUND INDICATIONS OF A POSSIBLE BIRDSTRIKE ON PILOTS LOWER WINDSCREEN NODAMAGE FOUND AT 2162.7 ACFT. HRS.CLEANED AND INSP. OK (MF4187 R/SPEC.)

23-Oct-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCACFT OPERATING UNDER AWR 1220. A COPYOF THIS AWR IS LOCATED IN THE HISTORICALRECORDS (MF4187 R/SPEC.)

28-Oct-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCIMPLEMENTATION OF 700 HOUR ESM IAW AWRDTD 28 OCT, R-1 C/W AT 2200.6 ACFT. HRS.(MF4187 R/SPEC.)

05-Nov-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-05-ASAM-01 REVISION OF FUELSYSTEM INTEGRITY CHECKS C/W AT 2298.9ACFT. HRS. (MF4187 R/SPEC.)

10-Jan-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-05-ASAM-02 BLUE FORCE TRACKER(BFT) N/A THIS ACFT. C/W AT 2394.7 ACFT.HRS. (MF4187 R/SPEC.)

02-Mar-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-05-SOF-01 REACTIVATION OF COCKPITAIRBAG SYSTEM (CABS) C/W AT 2415.4 ACFT.HRS. (MF4187 R/SPEC.)

17-Mar-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-05-SOF-02 ENHANCED SCHEDULEDMAINTENANCE (ESM) PROGRAMIMPLEMENTION N/A THIS ACFT. C/W AT 2434.5ACFT. HRS. (MF4187 R/SPEC.)

25-Mar-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAACETM1-1520-237-23, CHG 8 CHIP LIGHT, INPUTMOD. TSN: 2462. NO PARTICLE DESCRIPTIONPROVIDED ON 2408-13-1/2. (MF4187)

06-Apr-2005 1

LOWE AHP

thomas.m.lilly

USAAVNCUH-60-05-ASAM-03 AIRCREW RESTRAINTSYSTEM COMPATIBILITY C/W AT 2464.4 ACFT.HRS. (MF4187 R/SPEC.)

08-Apr-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-05-ASAM-04 INSP OF TAIL LANDINGGEAR YOKE ASSY C/W AT 2470.2 ACFT HRS.(MF4187 R/SPEC.)

09-Apr-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCDAMAGE FOUND TO RIGHT TRAILING EDGEON STABILATOR ON POST FLIGHT AT 2509.9ACFT. HRS. REPAIRED STABILATOR TRAILINGEDGE. (MF4187 R/SPEC.)

19-Apr-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-05-ASAM-06 TROOP SEAT RESTRAINTBUCKLE COMPLETD AT 2530.1 ACFT HRS.(MF4187 R/SPEC.)

29-Apr-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-05-ASAM-07 AIR INTRUSION OFHYDRAULIC SYSTEM COMPLETD AT 2570.4ACFT HRS. (MF4187 R/SPEC.)

10-May-2005 1

FT. RUCKER, AL.

thomas.m.lilly

DYNCORP FT. CKY.AMCOM/OLR

OCM/ACE PERFORMED AT 2615 ACFT. HRS. BYTEAM MEMBER M (JB7079)

01-Jun-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNC,UH-60-05-ASAM-01 REVISION OF FUELSYSTEM INTEGRITY CHECKS C/W @ 2615.0ACFT HRS. (PART 2) (CA3091 R/SPEC.)

07-Jul-2005 1

FT. RUCKER,AL

thomas.m.lilly

USAAVNC,M/R RIG COMPLETED @ 2615.0 ACFT HRS. NOADJUSTMENTS MADE. (CA3091 R/SPEC)

14-Jul-2005 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 18 of 61

USAAVNC,700 HR PHASE #5 COMPLETED @ 2615.0 ACFTHRS. NEXT PHASE #6 DUE @ 3315.0 ACFTHRS. (CA3091 R/SPEC)

22-Jul-2005 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCUH-60-05-ASAM-09 CRASHWORTHYEXTERNAL FUEL SYSTEM (CEFS)INSTALLATION BOLTS C/W AT 2616.0 ACFT.HRS. (MF4187 R/SPEC.)

02-Aug-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNC,ACFT MAIN ROTOR HEAD RIGGED I/A/W SADWG. 70400-00003 REV. E. SYSTEMCONTROLS HAVE BEEN BIASED IN ACCORD.(A) AFT CONTROL SERVO INPUT ROD HASBEEN LENGTHENED 1/2 TURN. (B) LATERALCONTROL SERVO INPUT ROD HAS BEENSHORTENED 1 FULL TURN. (C) FORWARDCONTROL SERVO INPUT ROD HAS BEENSHORTENED 1/2 TURN. @ 2615.0 ACFT HRS.(CA3091 R/SPEC)

03-Aug-2005 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCT/R BIAS MEASUREMENTS COMPLETED I/A/WTM1-1520-237-23, PARA 11-4-6.RED:5.167/4.845, YELLOW:5.195/4.862,BLUE:4.369/4.054, BLACK:4.473/4.137. (MF4187R/SPEC.)

12-Aug-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCALCL LTR DTD 12 OCT05 ONE TIMEINSPECTION OF TAIL LANDING GEARDEFLECTOR (WIRE CUTTER) IAW EMAILINSTRUCTIONS FROM ACLC C/W AT 2672.4ACFT. HRS. (MF4187 R/SPEC.)

16-Oct-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCAIRWORTHINESS RELEASE 1220 DTD 06 OCT05 TO CONDUCT ESM OPERATIONALEVALUATION AT THE USAAVNC, FT. RUCKER,AL. COMPLETED AT 2685.9 ACFT. HRS. PMIINTERVAL INCREASED FROM 700 TO 720 HRSI/A/W 1220 NEXT PHASE #6 DUE AT 3335.0ACFT. HRS. (MF4187 R/SPEC.)

19-Oct-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCACFT. OPERATING UNDER AIRWORTHNESSRELEASE DTD 06 OCT 05 TO CONDUCT ESMOPERATIONAL EVALUATION AT THEUSAAVNC, FT. RUCKER, AL. (AWR 1220)(MF4187 R/SPEC.)

19-Oct-2005 2

FT. RUCKER, AL.

thomas.m.lilly

USAAVNC#2 CROSSFEED BEAKAWAY VALVE REPLACEDI/A/W TB1-1520-237-20-213 THIS DATE AT2685.9 ACFT. HRS. (MF4187 R/SPEC.)

22-Oct-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-05-ASAM-11 WIRING HARNESSCHAFFING C/W AT 2685.9 ACFT. HRS. (MF4187R/SPEC.)

24-Oct-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCM/R RIG CHECK COMPLETED AT 2739.2 ACFT.HRS. NO ADJUSTMENT MADE. (MF4187R/SPEC.)

29-Nov-2005 1

FT. RUCKER, AL.

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 19 of 61

USAAVNCAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG. 70400-00003REV. C. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD. A. LATERAL CONTROLSERVO INPUT ROD P/N 70400-02258-046 HASBEEN SHORTENED 2/3 TURN. B. AFTCONTROL SERVO INPUT ROD P/N 70400-02258-045 HAS HAD NO CHANGE. C. FORWARDCONTROL SERVO INPUT ROD P/N 70400-02258-047 HAS HAD NO CHANGE*****NOTE*******WHEN AIRCRAFT RIGGING IS BIASEDRIGGING PIN HOLES ARE TEMPORARILY LOSTAT THE ABOVE 3 POINTS.C/W AT 2740.7 ACFT.HRS. (MF4187 R/SPEC.)

30-Nov-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-06-ASAM-01 TAIL LANDING GEARSTRUT C/W AT 2814.6 ACFT. HRS. (MF4187R/SPEC.)

06-Jan-2006 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCM/R RIG CHECK COMPLETED AT 2834.8 ACFT.HRS. NO ADJUSTMENTS MADE` (MF4187R/SPEC.)

14-Jan-2006 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCACFT CONTINUES TO OPERATE UNDER AWR1153, JP-8+100 FUEL, R2 DTD 30-JAN-06.(RJ0827, R/SPEC)

31-Jan-2006 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCUH-60-05-ASAM-11 WIRING HARNESSCHAFFING C/W AT 3014.8 ACFT. HRS. (MF4187R/SPEC.)

11-Mar-2006 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCACFT. CONTINUES TO OPERATE UNDER AWR927 REV. 5, DEMOD. AT 3107.5 ACFT. HRS.(MF4187 R/SPEC.)

04-Apr-2006 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCUH-60-06-ASAM-02 MAIN ROTOR (M/R) RIGIDCONNECTING LINK/PITCH CONTROLASSEMBLIES C/W AT 3151.4 ACFT. HRS.(MF4187 R/SPEC.)

14-Apr-2006 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCACFT. OPERATING UNDER AIRWORTHNESSRELEASE DTD 16 MAR 05 FOR INSTALLATIONOF EYEBOLTS ON UH-60A/L HELICOPTERBIFILAR ARMS TO SECURE SAFETYHARNESSES AT 3151.4 ACFT. HRS. (AWR 1251)(MF4187 R/SPEC.)

15-Apr-2006 1

FT. RUCKER, AL.

thomas.m.lilly

AMCOM OLR/DYNCORPOCM/ACE PERFORMED AT 3216 ACFT. HRS. BYTEAM MEMBER J (LH9501)

04-May-2006 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCACLC EMAIL DTD 27 MAR 06 ONE TIMEINSPECTION OF LOWER CONSOLE CIRCUITBREAK PANEL ASSEMBLIES FOR WATERPENETRATION C/W AT 3215.8 ACFT. HRS.(MF4187 R/SPEC.)

04-May-2006 2

FT. RUCKER, AL.

thomas.m.lilly

USAAWCUH-60-06-ASAM-04 COCKPIT AIRBAG SYSTEM(CABS) ELECTRONIC CRASH SENSOR UNIT(ECSU) DRAIN PLUGS COMPLETED AT 3260.3ACFT HRS. (MF4187 R/SPEC.)

22-Jun-2006 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCUH-60-06-SOF-02 DISABLING OF COCKPITAIRBAG SYSTEM (CABS) C/W AT 3260.3 ACFT.HRS. (MF4187 R/SPEC.)

22-Jun-2006 2

FT. RUCKER, AL.

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 20 of 61

USAAWCGEN-MIM-06-001 INSPECTION OF T700 SERIESENGINE OIL FILLER ASSEMBLY (CC0814,R/SPEC)

14-Aug-2006 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R CABLE TENSION CHECK COMPLETED AT3305.2 ACFT HRS. RH=184, LH=184, 30*C.(CC0814, R/SPEC)

12-Sep-2006 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R BIAS MEASUREMENTS COMPLETED I/A/WTM1-1520-237-23, PARA 11-4-6.RED:4.923/4.643, YELLOW:4.937/4.657,BLUE:4.363/4.083, BLACK:4.305/4.083 (CC0814,R/SPEC)

12-Sep-2006 2

FT. RUCKER, AL

thomas.m.lilly

USAAWCM/R RIG CHECK COMPLETED AT 3305.2 ACFT.HRS. NO ADJUSTMENT MADE. (CC0814,R/SPEC)

12-Sep-2006 3

FT. RUCKER, AL

thomas.m.lilly

USAAWC720 PMI #6 COMPLETED AT 3305.2 ACFT HRS.NEXT PMI #7 DUE AT 4025.2ACFT HRS.(CC0814, R/SPEC)

15-Sep-2006 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCUH-60-06-ASAM-02 MAIN ROTOR (M/R) RIGIDCONNECTING LINK/PITCH CONTROLASSEMBLIES C/W AT 3305.2 ACFT. HRS.(CC0814, R/SPEC)

23-Sep-2006 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCONE TIME EVACUATION MISSION COMP FROMS. TRACKING TO PARKING J-8 @ 3398.3 ACFTHRS. APU FIRE LIGHT ILLUMINATESINTERMITTENTLY WITH APU RUNNING ANDNOT RUNNING. REPLACED FIRE DETECTOR.(JT0967 R/SPEC.)

07-Nov-2006 1

FT. RUCKER, AL

thomas.m.lilly

USAAWC, FT. RUCKER,AL

UH-60-07-ASAM-02 REVISION TO UH-60-07-ASAM-01, REROUTING OF WHITEENGINE/AIRFRAME HARNESS ASSEMBLYCOMPLETED AT 3502.8 ACFT HRS. (RJ0827,R/SPEC)

21-Dec-2006 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCUH-60-07-ASAM-04 AUTOROTATIONALCHARTS COMPLETED AT 3512 ACFT HRS.(JB2761 R/SPEC)

30-Dec-2006 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCUH-60-07-ASAM-03 YAW AND COLLECTIVEBOOST SERVOS ROLL PIN COMPLETED AT3512 ACFT HRS. (JB2761 R/SPEC)

03-Jan-2007 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCACFT OPERATING UNDER AWR 1153 (R3)(JP8+100 FUEL), DTD 19DEC06. 3534.9 ACFTHRS. (MF4187 R/SPEC.)

19-Jan-2007 1

FT. RUCKER, AL.

thomas.m.lilly

USAACETM1-1520-237-23 CHIP LIGHT, IGB TSN: 3543.(DOES NOT LOCK IN PLACE) REPLACED CHIPDETECTER CK'D. OK. (MF4187)

24-Jan-2007 1

LOWE AHP

thomas.m.lilly

USAAWCUH-60-07-ASAM-05 ARC-220/KY-100 START-UPPROCEDURES (N/A THIS ACFT., KY-100 NOTINSTALLED) AT 3544.3 ACFT. HRS. (MF4187R/SPEC.)

25-Jan-2007 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCUH-60-07-ASAM-06 INTERNAL RESCUE HOISTCABLE (GUARD) DEFLECTOR C/W AT 3546.3ACFT. HRS. (MF4187 R/SPEC.)

10-Feb-2007 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCUH-60-07-AMAM-01 COMMON MISSILEWARNING SYSTEM (CMWS) N/A THIS ACFT. @3676.5 ACFT. HRS. (MF4187 R/SPEC.)

28-Mar-2007 1

FT. RUCKER, AL.

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 21 of 61

USAAWCUH-60-07-ASAM-07 INSTALLATION OF STATICBONDING JUMPERS, N/A TO THIS ACFT. C/WAT 3777.8 ACFT. HRS. (MF4187 R/SPEC.)

09-May-2007 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCACFT. OPERATING UNDER AWR 1251, REV. 1,DTD. 16MAR07 (INSTL. OF EYEBOLTS ONBIFILAR FOR SAFETY HARNESSES). 3778.5ACFT. HRS. (MF4187 R/SPEC.)

17-May-2007 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCM/R RIG CHECK COMPLETED AT 3826.8 ACFT.HRS. NO ADJUSTMENTS MADE. (MF4187R/SPEC.)

09-Jul-2007 1

FT. RUCKER, AL.

thomas.m.lilly

USAACETM1-1520-237-23 (2) CHIP LIGHT, IGB TSN:3827, NO PARTICLE DESCRIPTION PROVIDEDON 2408-13-1/2. (MF4187)

09-Jul-2007 2

LOWE AHP

thomas.m.lilly

DYNCORP OLROCM/ACE PERFORMED AT 3842 ACFT. HRS. BYTEAM MEMBER R. AMCOM PROJECT OLR.(TS0568)

17-Jul-2007 1

FT. CAMPBELL, KY.

thomas.m.lilly

USAAWCACFT. OPERATING UNDER AWR 1220, REV. 3,DTD. 27JUL07. IMPLEMENTATION OF 720HOUR (ESM) REQUIREMENTS AT 3897.5 ACFT.HRS. (MF4187 R/SPEC.)

31-Jul-2007 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCACFT. OPERATING UNDER ISAQ 128 REV. 3DTD. 02MAR07. (FOGS) (AHRU) AT 4001.2ACFT. HRS. (MF4187)

22-Oct-2007 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCM/R RIG CHECK COMPLETED AT 4001.2 ACFT.HRS. NO ADJUSTMENTS MADE. (RC1002)

30-Oct-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R CABLE TENSION CHECK COMPLETED AT4001.2 ACFT HRS. RH=155, LH=156, 28*C.(RC1002)

01-Nov-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R BIAS MEASUREMENTS COMPLETED I/A/WTM1-1520-237-23, PARA 11-4-6.RED:4.704/5.035, YELLOW:4.691/5.035,BLUE:4.082/4.420, BLACK:4.042/4.380 (RC1002)

01-Nov-2007 2

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-AMAM-01 (MAIN LANDING GEARSHOCK STRUTS) C/W @ 4001.2 ACFT HRS.AFS560. (RC1002)

05-Nov-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCM/R RIG CHECK COMPLETED AT 4001.2 ACFT.HRS. NO ADJUSTMENTS MADE. (RC1002)

05-Nov-2007 2

FT. RUCKER, AL

thomas.m.lilly

USAAWC720 HR PMI #7 C/W @ 4001.2 ACFT HRS. NEXTPMI #8 DUE @ 4721.2 ACFT HRS. (RC1002)

06-Nov-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-ASAM-02 (POWER AVAILABLECONTROL CABLE) C/W @ 4001.2 ACFT HRS.AFS560. (RC1002)

08-Nov-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-ASAM-01 (TROOP/GUNNERS SEATUPPER ENERGY ATTENUATING WIRES) C/W @4001.2 ACFT HRS. AFS560. (RC1002)

09-Nov-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-AMAM-02 (TAIL ROTOR OUTBOARDRETENTION PLATE SHIMS) C/W @ 4001.2 ACFTHRS. AFS525. (RC1002)

03-Dec-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R CABLE TENSION CHECK COMPLETED AT4001.2 ACFT HRS. RH=145, LH=145, 70*C.(RC1002)

06-Dec-2007 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 22 of 61

USAAWCH-60-08-ASAM-03 (CHANGES TO CURRENTFUEL SYSTEM INTEGRITY CHECKS) C/W @4001.2 ACFT HRS. A (RC1002)

08-Dec-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-ASAM-05 TAIL ROTOR QUADRANTSPRING CAPSULE ASSEMBLY C/W AT 4006.8ACFT. HRS. (MF4187 R/SPEC.)

16-Dec-2007 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCH-60-08-ASAM-04 PILOT'S LOWER SEAT RAILCHAFING ELECTRICAL HARNESS C/W AT4010.3 ACFT. HRS. (MF4187 R/SPEC.)

18-Dec-2007 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCT/R CABLE TENSION CHECK COMPLETED AT4010.3 ACFT. HRS. R/H = 146, L/H = 145, 21`C.(MF4187 R/SPEC.)

19-Dec-2007 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCH-60-08-AMAM-04(COCKPIT DOORJETTISONABLE WINDOWS C/W OLD -SYTLEWITH SLIDING WINDOWS, (P+CP). AT 4060.9ACFT HRS (MW0980 R/SPEC.)

19-Jan-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-SOF-01 M/R BLADE EXPANDABLE PININSPECTION CHANGE C/W AT 4086.3 ACFTHRS. (MW0980 R/SPEC.)

28-Jan-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCACFT NO LONGER OPERATING UNDER AWR1153, DTD 19DEC06, JP8+100 FUEL. 4096.7ACFT HRS. (MF4187 R/SPEC.)

31-Jan-2008 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCH-60-08-AMAM-05 GOODRICH INTERNALRESCUE HOISTS ACFT HRS 4105.2 (MW0980R/SPEC)

04-Feb-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWC#2 CROSSFEED BREAKAWAY VALVEREPLACED I/A/W TB1-1520-237-20-213 08 FEB08 ACFT HRS 4124.0 (MW0980 R/SPEC)

08-Feb-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-AMAM-06 COMMON MISSILE WARNINGSYSTEM (CMWS) SEQUENCERS ACFT HRS4124.0 (MW0980)

08-Feb-2008 2

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-ASAM-06 M/R PYLON SLIDINGFORWARD FAIRING C/W AT 4215.8 ACFT HRS(RJ0827, R/SPEC)

15-Mar-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-AMAM-07 AN/ASN-128B/D DOPPLERGPS NAVIGATION SET (DGNS) (4269.6 ACFTHRS) (RJ0827, R/SPEC)

29-Mar-2008 1

FT. RUCKER, AL

thomas.m.lilly

DYCORP, INTL - AMCOMRASM-E

ACE/OCM INSP C/W @ 4359 ACFT HRS, BYTEAM MEMBER R (TS0568)

12-May-2008 1

FT CAMPBELL, KY

thomas.m.lilly

USAAWCT/R BIAS MEASUREMENTS COMPLETED @4359.3 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:5.154/4.814, YELLOW:5.211/4.871,BLUE:4.576/4.236, BLACK: 4.551/4.211.(RJ0827, R/SPEC)

12-May-2008 2

FT. RUCKER, AL

thomas.m.lilly

USAAWCMAIN ROTOR RIG CK PERFORMEND @ 4359.3ACFT HRS: NO ADJ WERE MADE. (RJ0827,R/SPEC)

13-May-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R BIAS MEASUREMENTS COMPLETED @4359.3 ACFT HRS I/A/W TM1-1520-237-23 PARA11-4-6 RED: 5.117/4.786, BLUE:4.365/4.030,YELLOW: 5.097/4.749, BLACK: 4.330/3.991(RJ0827, R/SPEC)

20-May-2008 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 23 of 61

USAAWCT/R CABLE TENSION CK DUE AT 4378.9 +1.0ACFT HRS (TEMP 20 C L/H -137 R/H - 137)(TP1634, R/SPEC)

03-Jun-2008 1

FT. RUCKER

thomas.m.lilly

USAAWCACFT OPERATING UNDER AWR 1220 REV. 3.DTD 22 MAY 2008 IMPLEMENTATION OF 720HOUR (ESM) REQUIREMENTS @ 4386.6 ACFTHRS (TP1634 R/SPEC)

04-Jun-2008 1

FT. RUCKER,AL

thomas.m.lilly

USAACEAIRCRAFT MAINTAINED AS PRESCRIBED INAIRWORTHINESS 1220, DATED 22 MAY 2008.REVISION 4. ( ENHANCED SCHEDULEDMAINTENANCE.) COMPLIED WITH @ 4386.6AIRCRAFT HOURS. (SA1319, R/SPEC)

04-Jun-2008 2

FT. RUCKER, AL

thomas.m.lilly

USAAWCCOMPLIED WITH REQ. OF H-60-08-AMAM-08(FLIGHT CONTROL RIGGING UPDATED) AT4395.0 ACFT HRS (TP1634 R/SPEC)

07-Jun-2008 1

FT. RUCKER,AL

thomas.m.lilly

USAACECOMPLIED WITH THE REQ. OF H-60-08-ASAM-10 PAR. 7.1-7.2(ELECTRICAL WIRE CHAFEISSUES ) AT 4489.2 ACFT HRS (TP1634 R/SPEC)

15-Jul-2008 1

FT. RUCKER,AL

thomas.m.lilly

USAACET/R BIAS MEASUREMENTS COMPLETED @4566.3 ACFT HRS I/A/W TM1-1520-237-23 PARA11-4-6 YELLOW: 5.022/4.701; RED: 5.069/4.739;BLUE: 4.491/4.191; BLACK: 4.399/4.061.(JB2761 R/SPEC)

04-Sep-2008 1

FT. RUCKER, AL.

thomas.m.lilly

USAACET/E TENSION CHECK COMPLETED AT 4577.3ACFT HRS LH166;RH 167 @32 C (TP1634R/SPEC)

13-Sep-2008 1

FT. RUCKER,AL

thomas.m.lilly

USAACEH-60-08-ASAM-13 FIRE EXTINGUISHING TUBEUNION RING COMPLIED WITH AT 4604.9 ACFTHRS (TP1634 R/SPEC)

24-Sep-2008 1

FT. RUCKER,AL

thomas.m.lilly

USAACEAIRCRAFT OPERATING WITHIN LIMITATIONSAND RESTRICTIONS SPECIFIED IN THEENCLOSED AIRWORTHINESS 1251, DATED 01SEP 08. REVISION 2 ( EYEBOLTS). COMPLIEDWITH @ 4605.4 AIRCRAFT HOURS. (SA1319,R/SPEC)

24-Sep-2008 2

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-09-SOF-01 HYDRO-MECHANICAL UNIT(HMU) H-60-09-SOF-01 COMPLETED AT 4682.8-ACFT HRS. (TP1634 R/ SPEC)

23-Oct-2008 1

FT. RUCKER,AL

thomas.m.lilly

USAACEH-60-09-SOF-02 AN/ALQ-144 INFRAREDCOUNTERMEASURE SYSTEM (IRCMS)COMPLETED @ -4708.6 ACFT HRS. NA TO THISACFT. (DW 0950 R/SPEC)

08-Nov-2008 1

FT RUCKER,AL

thomas.m.lilly

USAACEH-60-09-SOF-02 AN/ALQ-144 INFRAREDCOUNTERMEASURE SYSTEM (IRCMS)COMPLETED @ ---4708.0---------ACFT HRS. NATO THIS ACFT. (T.POLLARD,1634 ( AFS 517))

08-Nov-2008 2

FT. RUCKER,AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 24 of 61

USAACEMEC REQUEST AUTORIZED TO EXTEND THERETIREMENT LIFE OF THE MAINTRANSMISSION HOUSING (S/N: A265-00160)TO MATCH THE SHAFT (S/N: D253-00262) TBOTIME. MEC#: F83696. EXTENSION APPROVEDPER TN63866. POC IS CARL PIERCE AME 256-313-3113 DSN 897-3113 . TASK NUMBER :63866.JAY P. MERKEL CHIF, UTILITY DIV. AVIATIONENGINERING DIRECTORATE. AUTORIZED BYTAMMY GRIFFIN, FT. RUCKER, AL 334-255-9142. (JT0967 R/SPEC)

17-Nov-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-09-SOF-03 H-60-09-SOF-03 POSSIBLERETIREMENT LIFE OVERFLIGHT COMPLETEDAT 4708.0 ACFT. (T/POLLARD 1634 (AFS584))

17-Nov-2008 2

FT. RUCKER,AL

thomas.m.lilly

USAACET/R BIAS MEASUREMENTS COMPLETED AT4712.3 ACFT HRS I/A/W TM 1-1520-237-23 PARA11-4-6. RED: 4.812/5.145/.333, BLUE:4.140/4.477/.337, BLACK: 4.097/4.434/.337,YELLOW: 4.817/5.149/.332 (BH0315 R/SPEC)

04-Dec-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLIED WITH REQUIREMENTS OFPARAGRAPH 7.3-7.10 OF H-60-08-ASAM-10 AT4712.3 ACFT HRS (BH0315 R/SPEC)

09-Dec-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-08-ASAM-14 (ENGINE HARNESSES)COMPLIED WITH AT 4712.3 ACFT HRS (BH0315R/SPEC)

09-Dec-2008 2

FT. RUCKER, AL

thomas.m.lilly

USAACEPHASE INSPECTION # 8 COMPLETED AT4712.3 ACFT HRS. NEXT PHASE (#9) DUE AT5432.3 (BH0315 R/SPEC)

09-Dec-2008 3

FT. RUCKER, AL

thomas.m.lilly

USAACEM/R RIG CHECK COMPLETED AT 4712.3 ACFTHRS. NO ADJUSTMENTS TO FWD & AFTPRIMARY SERVO CONTROL ROD BIAS, LATPRIMARY CONTROL ROD BIAS .25 TURNCOUNTER CLOCKWISE (BH0315 R/SPEC)

08-Jan-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACET/R CABLE TENSION C/W AT 4712.3 ACFT HRS(TEMP 22 C L/H -155 R/H - 155) (RC1002)

08-Jan-2009 2

FT. RUCKER, AL

thomas.m.lilly

USAACEREPLACED T/R SPRING CAPSULE (P/N 70400-0660-045/048) AT 4712.3 ACFT HRS (TP1634(595))

08-Jan-2009 3

FT. RUCKER,AL

thomas.m.lilly

USAACET/R BIAS MEASUREMENTS COMPLETED @4722.9 ACFT HRS I/A/W TM1-1520-237-23 PARA11-4-6 RED: 4.824/305=5.129BLUE:4.130/302=4.432 YELLOW:4.863/303=5.166 BLACK:4.111/304=4.415(TP1634)

09-Feb-2009 1

FT. RUCKER,AL

thomas.m.lilly

USAACET/R CABLE TENSION CHECK C/W AT 4722.9ACFT HRS ; L/H 143; R/H 143 @ 22 C. (TP1634R/SPEC)

15-Feb-2009 1

FT. RUCKER,AL

thomas.m.lilly

USAACEET/R CABLE TENSION CHECK COMPLETED AT4732.6 ACFT HRS; L/H 145-21C, R/H 145 - 21 C ;IN CONJUCTION WITH T/R RIGGING (TP1634)

21-Feb-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACET/R BIAS MEASUREMENTS COMPLETED @4732.6 ACFT HRS I/A/W TM1-1520-237-23 PARA11-4-6 RED: 5251/4905=.346BLUE:4472/4130=.342 YELLOW:5094/4750=.334,BLACK: 4481/4140=.341 (TP1634)

21-Feb-2009 2

FT. RUCKER,AL

thomas.m.lilly


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USAACET/R BIAS MEASUREMENTS COMPLETED @4733.6 ACFT HRS I/A/W TM1-1520-237-23 PARA11-4-6 RED: 4.336/4.627=0.291BLUE:3.720/4.020=0.300YELLOW:4.338/4.678=0.289 BLACK: 3.720/4.020=0.300(TP1634)

23-Feb-2009 1

FT. RUCKER,AL

thomas.m.lilly

USAACET/R BIAS MEASUREMENTS COMPLETED @4742.5 ACFT HRS I/A/W TM1-1520-237-23 PARA11-4-6 RED: 4.786/308 = 5.094 BLUE:4.094/306=4.400 YELLOW: 4.736/305=5.041BLACK: 4.078/.305=4.383 (TP1634)

26-Feb-2009 1

FT. RUCKER,AL

thomas.m.lilly

USAACEH-60-09-ASAM-04 RESCUE HOIST MARK 44MOD 0 CARTRIDGE ACTIVATION DEVICE (CAD)N/A THIS ACFT AT 4744.7 ACFT HRS. (MB1137)

01-Mar-2009 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEH-60-09-ASAM-05 UPDATE TO LIFE LIMITCHANGE OF TAIL ROTOR (TR) QUADRANTSPRING CAPSULES NLT THAN 03 APR.09COMPLETED @ 4750.4 (TP1634)

04-Mar-2009 1

FT. RUCKER. AL

thomas.m.lilly

DYNCORPINTERNATIONAL

OCM/ACE PERFORMED @ 4796 ACFT HRS. BYTEAM MEMBER J AMCOM RASM - E (LH9501)

17-Mar-2009 1

FT. CAMPBELL, KY

thomas.m.lilly

USAACEMAIN MOD MOUNT BUSHING HAVE SURFACEDTO (.020). TM REQUIRES THE BUSHING TO AT.000 TO .005 (FLUSH WITH BEAM). REQUEST ISGRANTED TO FOLLOW SIKORSKY FSEGRECOMMENDATION TO RESET BUSHINGS ASPER MEC F90238 AUTHORIZED BY TAMMYGRIFFIN DTD 31 MAR 09. MEC CAN BELOCATED IN THE BACK OF THE HISTORICALRECORDS. (DW 0950, R/SPEC)

26-Mar-2009 1

FT RUCKER,AL

thomas.m.lilly

USAACEH-60-09-ASAM-07 H-60-09-ASAM-07, FIREEXTINGUISHER WIRING (BREAKAWAYTHREAD) COMPLETED AT 4796.4 ACFT HRS.(JC6208 REC/SPEC)

08-Apr-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACE9-APR-09 T/R CABLE TENSION CKCOMPLETED AT 4796.4 ACFT HRS. R-155; L-155; @24*C. (JC6208 REC/SPEC)

09-Apr-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACET/R BIAS MEASUREMENTS COMPLETED @4796.4 ACFT HRS I/A/W TM1-1520-237-23 PARA11-4-6 RED: 4.762/5.065/.303 BLUE:4.049/4.351/.302 YELLOW: 4.745/5.049/.304BLACK: 4.046/4.349/.303 (JC6208 REC/SPEC)

10-Apr-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEACFT MAIN ROTOR HEAD RIGGED SYSTEMCONTROLS HAVE BEEN BIASED IN ACCORD.A) AFT CONTROL SERVO INPUT ROD HASBEEN LENGTHENED 1/2 TURN. B) LATERALCONTROL SERVO INPUT ROD HAS NOADJUSTMENT CHANGE. C) FORWARDCONTROL SERVO INPUT ROD HAS BEENSHORTENED 1/2 TURN. NOTE: WHEN ACFTRIGGING IS BIASED, RIGGING PIN HOLES ARETEMPORARILY LOST AT THE ABOVE 3 POINTS.COMPLETED @4796.4 ACFT HRS. (JC6208REC/SPEC)

12-Apr-2009 1

FT. RUCKER, AL

thomas.m.lilly


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Page 26 of 61

USAACEH-60-09-ASAM-09 FIRE EXTINGUISHER WIRING(BREAKAWAY THREAD) COMPLETED AT4869.2 ACFT HRS. (JC6208 R/SPEC.)

13-May-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACET/R BIAS MEASUREMENTS COMPLETED @4873.7 ACFT HRS I/A/W TM1-1520-237-23 PARA11-4-6 RED: 5.072/4.738/.334 BLUE:4.394/4.069/.330 YELLOW: 5.052/4.720/.332BLACK: 4.371/4.039/.332 (JC6208 R/SPEC)

22-May-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACET/R CABLE TENSION CK COMPLETED AT4873.7 ACFT HRS. R-145; L-145; @24*C.(JC6208 R/SPEC)

22-May-2009 2

FT. RUCKER, AL

thomas.m.lilly

USAACEACFT MAIN ROTOR HEAD RIGGED SYSTEMCONTROLS HAVE BEEN BIASED IN ACCORD.A) AFT CONTROL SERVO INPUT ROD HASBEEN LENGTHENED 1/2 TURN. B) LATERALCONTROL SERVO INPUT ROD HAS NOADJUSTMENT CHANGE. C) FORWARDCONTROL SERVO INPUT ROD HAS BEENSHORTENED 1/2 TURN. NOTE: WHEN ACFTRIGGING IS BIASED, RIGGING PIN HOLES ARETEMPORARILY LOST AT THE ABOVE 3 POINTS.COMPLETED @4873.7 ACFT HRS. (JC6208R/SPEC)

22-May-2009 3

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-09-ASAM-08 ENGINE COWLING WEIGHTRESTRICTION COMPLETED AT 4874.7 ACFTHRS. (JC6208 R/SPEC.)

23-May-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLIED WITH H-60-09-ASAM-11 (CARGODOOR WINDOW EMERGENCY JETTISONHANDLE ASSEMBLY) @ 4957.1 ACFT HRS.*FAILED* (JC6208)

26-Jun-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLIED WITH REQUIREMENTS OF TB 1-1520237-23-9 AND TB 1-1520-237-10 (SC2006,R/SPEC)

26-Jun-2009 2

FT. RUCKER, AL

thomas.m.lilly

USAACETHIS ACFT NO LONGER OPERATING UNDERLIMITATIONS AND RESTRICTIONS UNDER AWR1515, DATED 10 JUN 08. REFER TO ISAQDATED 02 MAR 07 FOR FOGS ISAQ 128 @4978.4 ACFT HRS. (JC6208)

08-Jul-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEACFT MAIN ROTOR HEAD RIGGED SYSTEMCONTROLS HAVE BEEN BIASED IN ACCORD.A) AFT CONTROL SERVO INPUT ROD HASBEEN LENGTHENED 1/2 TURN. B) LATERALCONTROL SERVO INPUT ROD HAS NOADJUSTMENT CHANGE. C) FORWARDCONTROL SERVO INPUT ROD HAS BEENSHORTENED 1/2 TURN. NOTE: WHEN ACFTRIGGING IS BIASED, RIGGING PIN HOLES ARETEMPORARILY LOST AT THE ABOVE 3 POINTS.COMPLETED @4998.2 ACFT HRS. (JC6208)

20-Jul-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACET/R BIAS CHECK COMPLETED AT 4998.2 ACFTHRS. RED: 5.012/4.683/.329 BLACK:4.405/4.076/.329 YELLOW: 5.168/4.840/.328BLUE: 4.359/4.030/.329 (JC6208)

21-Jul-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACECABLE TENSION CHECK COMPLETED @4998.2 ACFT HRS. L/H-147 R/H- 147 @ 22*C(JC6208)

21-Jul-2009 2

FT. RUCKER, AL

thomas.m.lilly


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Page 27 of 61

USAACEACFT GROUNDED FOR H-60-09-ASAM-07 & H-60-09-ASAM-09 NOT COMPLIED WITH. ***ASAM**S COMPLIED WITH @ 5051.3 ACFTHRS.*** (JC6208)

14-Aug-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACET/R RIG CHECK COMPLETED @ 5071.0 ACFTHRS. BLUE: 4.334/4.020/.314 RED:5.100/4.762/.338 BLACK: 5.048/4.762/.332YELLOW: 4.349/4.028/.321 (JC6208)

22-Aug-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-09-AMAM-04 H-60-09-AMAM-04 CO-PILOTSEAT INTERFERENCE WITH ARMY AIRBORNCOMMAND CONTROL SYSYEM (A2C2S)COMPLETED AT 5076.0 ACFT HRS. (JC6208)

26-Aug-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLIED WITH REQUIREMENTS OF H-60-09-AMAM-06 AT5078.0 ACFT HRS. CARGO HOOKCARTRIDGE ACTUATED DEVICE (CAD) LIFEREDUCTION. AFS793 (JB2761 R/SPEC)

28-Aug-2009 1

FT. RUCKER, AL.

thomas.m.lilly

USAACECOMPLY WITH REQUIREMENTS OF GEN-09-AMAM-03, ULLS-A (E), NLT 08 SEP 09**COMPLIED WITH @ 5087.7 ACFT HRS. N/ADUE TO UNITNOT CURRENTLY UTILIZING ULLS-A (E). AFS 778** (JC6208 R/SPEC)

04-Sep-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEMAIN MOD BUTTON POPPED ON POST FLIGHT@ 5093.0 ACFT HRS. REPLACED FILTERS (-105INSTALLED) NO CHIPS FOUND. RESETBUTTON PER WP 0116. (JC6208 R/SPEC)

04-Sep-2009 2

FT. RUCKER, AL

thomas.m.lilly

USAACEALL H-60 AIRCRAFT "COMPLY WITHREQUIREMENTS OF H-60-09-AMAM-07 NLT 23SEP 09". ** COMPLIED WITH @ 5118.1 ACFTHRS. FAILED. AFS784 (JC6208 R/SPEC)

16-Sep-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEMAIN MOD TRANSMISSION FILTER BYPASSINDICATOR BUTTON POPPED @ 5175.5 ACFTHRS. (JC6208 R/SPEC)

29-Sep-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEREPLACED MAIN MOD TRANSMISSION FILTERAND RESET BUTTONS @ 5175.5 ACFT HRS.(JC6208 R/SPEC)

30-Sep-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-10-ASAM-01 HAMILTON-SUNSTRANDHYDRO-MECHANICAL UNITS COMPLETED AT5195.7 ACFT HRS. (AFS 778) (JC6208 R/SPEC)

07-Oct-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLY WITH REQUIREMENTS OF H-60-10-AMAM-02, AIRCRAFT REDESIGNEDPLANETARY GEAR CARRIER RETIREMENTLIFE, NLT 19 OCT 09. COMPLIED WITH @5207.3 AIRCRAFT HOURS (SA1319, R/SPECINSP: AFS 778)

10-Oct-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEPERMISSION TO DEVIATE FROM MANUAL ANDBE ABLE TO REPLACE HARDWARE ON THETAIL ROTOR SYSTEM OF THE UH-60AASSIGNED TO FT. RUCKER WITH LIKEHARDWARE WITHOUT THE REQUIREMENT OFA TAIL ROTOR BALANCE I/A/W MEC F97372. ACOPY OF THIS MEC IS LOCATED IN THEHISTORICAL RECORDS. COMPLIED WITH @5239.5 AIRCRAFT HOURS (SA1319, R/SPEC)

15-Oct-2009 1

FT. RUCKER, AL

thomas.m.lilly


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REMARKS4. 5.


Page 28 of 61

USAACECABLE TENSION CHECK COMPLETED FORREPLACEMENT OF T/R PYLON PULLEY @5239.5 ACFT HRS. L/H-158 R/H- 160 (SA1319,R/SPEC)

22-Oct-2009 1

FT.RUCKER, AL

thomas.m.lilly

USAACET/R BIAS: BLACK: 4.0010-4.3185/.3175 RED:4.7345-5.0615/ .325 BLUE: 4.0025- 4.3375/.355YELLOW: 4.7440-5.0815/ .3375 TRAVEL: .032-3478 (SA1319, R/SPEC)

23-Oct-2009 1

FT.RUCKER, AL

thomas.m.lilly

USAACECABLE TENSION CHECK COMPLETED FORREPLACEMENT OF CABLE PULLEY @ 5239.5AIRCRAFT HRS. R 19 DEGREES L 21 DEGREES. R/H 154/ 152/155/154 L/H 152/ 154/ 152 / 155.(SA1319, R/SPEC)

23-Oct-2009 2

FT. RUCKER, AL

thomas.m.lilly

USAACECABLE TENSION CHECK DUE 9 TO 11 FLTHOURS COMPLETED 5249.6 AIRCRAFTHOURS. CHECKED AT 21°C OR 70°F L/H 165R/H 120 (SA1319, R/SPEC)

28-Oct-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACECABLE TENSION CHECK (FAILED) @ 5249.6AIRCRAFT HOURS. CHECKED AT 18°C L/H- 154R/H- 155 STABILIZED WHEN COMPARED TOTHE PREVIOUS READINGS R/H: 155 L/H: 154AT 19°C. (SA1319, R/SPEC)

28-Oct-2009 2

FT. RUCKER, AL

thomas.m.lilly

USAACEOPERATE IAW ISAQ 128 DTD 02 MAR 07 ( ISAQ128) ( FOGS) SUPERSEDED BY AWR 1529DATED 07 OCT 09. COMPLIED WITH @ 5258.7AIRCRAFT HOURS. (SA1319, R/SPEC)

31-Oct-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEAIRCRAFT OPERATING IN ACCORDANCE WITHLIMITATIONS AND RESTRICTIONS IN AWR1529, DATED 07 OCT 09 ( AHRU/AHRS).COMPLIED WITH @ 5258.7 AIRCRAFT HOURS.(SA1319, R/SPEC)

31-Oct-2009 2

FT. RUCKER, AL

thomas.m.lilly

USAACEAIRCRAFT OPERATING IN ACCORDANCE WITHAWR 1479 DATED 4 JAN 08. COMPLIED WITH@ 5287.2 AIRCRAFT HOURS. (SA1319, R/SPEC)

10-Nov-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLY WITH REQUIREMENTS OF H-60-10-ASAM-03 NLT 17 NOV 09. ( FIRE BOTTLEDISCHARGE LINES AND NOZZLES). COMPLIEDWITH @ 5291.7 AIRCRAFT HOURS. (SA1319,R/SPEC INSP: AFS 732)

13-Nov-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLY WITH REQUIREMENTS OF H-60-10-AMAM-04, ASN-128B/C DOPPLER GLOBALPOSITIONING. COMPLIED WITH @ 5291.7AIRCRAFT HOURS. (SA1319, R/SPEC INSP:AFS 757)

15-Nov-2009 1

FT.RUCKER, AL

thomas.m.lilly

USAACEAIRCRAFT OPERATING WITH LIMITATIONSAND RESTRICTIONS SPECIFIED IN THEENCLOSED AWR # 927 DATED 06 JUN 03.COMPLIED WITH @ 5293.3 AIRCRAFT HOURS(SA1319, R/SPEC)

16-Nov-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLY WITH REQUIREMENTS OF H-60-10-ASAM-04, STABILITY AUGMENTATION SYSTEM(SAS) LINKS, NLT 21 NOV 09. COMPLIED WITH@ 5305.7 AIRCRAFT HOURS (SA1319, R/SPECINSP: AFS 576)

19-Nov-2009 1

FT. RUCKER, AL

thomas.m.lilly


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REMARKS4. 5.


Page 29 of 61

USAACEM/R BLADE SPAR PRESSURE CHECK.READINGS AS THE FOLLOWING: RED 9.0BLACK 9.0 YELLOW 9.25 BLUE 9.0 TEMP: 11°C. COMPLIED WITH @ 5308.9 AIRCRAFTHOURS. (SA1319, R/SPEC)

24-Nov-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEACFT NO LONGER OPERATING INACCORDANCE WITH AWR 1479 DATED 4 JAN08. COMPLIED WITH @ 5335.2 AIRCRAFTHOURS. (SA1319, R/SPEC INSP: AFS 642)

01-Jan-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEM/R RIG CHECK COMPLETED AT 5343.3 ACFTHRS. NO ADJUSTMENTS TO FWD , AFT, LAT,OR THE PRIMARY SERVO CONTROL RODBIAS. (SA1319, R/SPEC)

07-Jan-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEGEN-10-AMAM-02 DISTRIBUTION OF NEWACFT ELECTRONIC LOGBOOK, N/A THISLOCATION, C/W AT 5369.3 (SC2006, R/SPECINSP: AFS 592)

25-Jan-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-10-AMAM-11 OIL SAMPLING CHANGESCOMPLETED AT __5377.8___________ACFT.HRS. (SC2006, R/SPEC INSP: AFS 594)

02-Feb-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEOPERATING WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1505 REV.3DTD 21 OCT 09 @ 5377.8 ACFT HRS. (VM4663)

02-Feb-2010 2

FT RUCKER, AL

thomas.m.lilly

USAACEAIRCRAFT DATE OF MANUFACTOR FROMACFT DATA PLATE IS AUG 1986 (SC2006,R/SPEC)

08-Feb-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-10-ASAM-06 AUTO-IGNITION ANDTRANSIENT DROOP IMPROVEMENT TDIMODIFICATION COMPLETED AT 5378 ACFTHRS. (DK1063 (AFS 528))

10-Feb-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEGEN-H-60-10-AMAM-05, (ULLS-A (E) CHANGE60B LEGITIMATE CODE FILE CHANGES, N/ATHIS LOCATION, CW AT 5377.8 (SC2006,R/SPEC INSP: AFS 598)

13-Feb-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEPMI PHASE # 9 COMPLETED @ 5377.8 ACFTHR. NEXT PHASE #10 DUE AT 6097.8 ACFTHRS. (JB2761 R/SPEC)

22-Feb-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEACFT MAIN ROTOR HEAD RIGGED SYSTEMCONTROLS HAVE BEEN BIASED IN ACCORD.A) AFT CONTROL SERVO INPUT ROD HAD NOCHANGE. B) LATERAL CONTROL SERVOINPUT ROD HAS ADJUSTMENT OF 2 FLATS IN.C) FORWARD CONTROL SERVO INPUT RODHAS HAD NO CHANGE. . COMPLETED @5377.8 ACFT HRS. (JB2761 R/SPEC)

22-Feb-2010 2

FT. RUCKER, AL.

thomas.m.lilly

USAACET/R BIAS MEASUREMENTS COMPLETED @5377.8 ACFT HRS I/A/W TM1-1520-237-23 PARA11-4-6 RED: 5.051/4.721/.330 BLUE:4.462/4.136/.326 YELLOW: 5.097/4.767/.330BLACK: 4.488/4.162/.326 (JB2761 R/SPEC)

22-Feb-2010 3

FT. RUCKER, AL.

thomas.m.lilly

USAACET/R CABLE TENSION C/W @ 5377.8 ACFT HRSW/ L/H-149; R/H-147.5 @ 21°/C. (JB2761R/SPEC)

22-Feb-2010 4

FT. RUCKER, AL.

thomas.m.lilly


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Page 30 of 61

USAACEOPERATING I/A/W AWR 1251 DTD 26 FEB 10REV-3 COMPLIED W @ 5388.5 ACFT HRS(SC2006, R/SPEC)

01-Mar-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEACFT OPERATING IAW AWR 1681 DTD 10 MAY10 (EH-60 DEMOD)

18-Mar-2010 1

LOWE AHP, FT.RUCKER, AL.

kathleen.m.jungell

USAACEOPERATING WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1455 REV 1DTD 23 OCT 09 @ 5489.3 ACFT HRS. (VM4663)

19-Apr-2010 1

FT RUCKER, AL

thomas.m.lilly

USAACET/R RIG CHECK COMPLETED @ 5489.3 ACFTHRS. BLUE: 4.513/4.183/.330 RED:5.201/4.874/.372 BLACK: 4.481/4.152/.329YELLOW: 5.168/4.835/.333 PRI SERVO RODBIAS: 3.450/.015 (SC2006, R/SPEC)

22-Apr-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEYAW LINKED PASSED I/A/W H-60-10-ASAM-04(SC2006, R/SPEC)

22-Apr-2010 2

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-08-AMAM-12 MAIN TRANSMISSION OILGAGE TUBE ASSY CW @ 5506.7 ACFT HRS.(SC2006, R /SPEC)

28-Apr-2010 1

LOWE AHP

thomas.m.lilly

USAACEACFT BEING OPERATED IAW MEO A6055 - M/RDROOP STOP BUSHING DE-BOND.REPLACEMENT DUE NEXT PMI @ 6097.8 ACFTHRS. (KJ0605)

01-May-2010 1

LOWE AHP

thomas.m.lilly

USAACECURRENTLY OPERATING UNDER AWR 1681DTD 10 MAY 10. NO LONGER OPERATINGUNDER AWR 927 DTD 06 JUN 03. IT HAS BEENSUPERCEDED BY AWR 1681. (SC2006,R./SPEC)

18-May-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-10-ASAM-07 STABILATOR HINGEFITTINGS C/W AT 5554.9 ACFT HRS. (SC2006,R/SPEC (AFS 77))

20-May-2010 1

FT. RUCKER, AL

thomas.m.lilly

CSC FT CAMPBEL KYOCM/ACE PERFORMED AT 5559. ACFT HRS BYTEAM MEMBER DD AMCOM/RASM-E (JB9001)

27-May-2010 1

FT CAMPBELL KY

thomas.m.lilly

USAACE,T/R BIAS MEASUREMENTS: RED- 5.080-4.750-.330 BLUE-4.447-4.105-.341 BLACK-4.410-4.064-.345 YELLOW--4.938-4.579-.359 @ 5559.1 ACFTHRS. (VM4663)

27-May-2010 2

FT RUCKER, AL

thomas.m.lilly

USAACEACFT OPERATING UNDER AWR 1220 R5 DTD28 MAY 10 (EH60 ENHANCED SCHEDULEMAINTENANCE (ESM) PROGRAM) @ 5560.4ACFT HRS (SC2006, R/SPEC (AFS 594))

01-Jun-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLETED IAW H-60-10-ASAM-08 @ 5562.9ACFT HRS (AUXILIARY POWER UNIT [APU]AND APU FIREWALL). (SC2006, R/SPEC (AFS745))

05-Jun-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLETED IAW H-60-09-ASAM-11 @ 5566.9(CARGO DOOR WINDOW JETTISON HANDLEWEBBING STRAP) (SC2006, R/SPEC)

07-Jun-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACET/R SYS RIG CHECK: RED: 4.347/4.648 BLUE:4.447/4.105 BLACK: 3.678/3.973 YELLOW:4.251/4.546 @ 5578.4 ACFT HRS. (SC2006,R/SPEC)

12-Jun-2010 1

FT. RUCKER, AL

thomas.m.lilly


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Page 31 of 61

USAACEH-60-10-SOF-02 SPINDLE LUG NDI ANDRETIREMENT LIFE CHANGES C/W AT 5603.5ACFT HRS. (SC2006, R/SPEC (AFS 594))

22-Jun-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-10-AMAM-16 COMMON MISSILE WARNINGSYSTEM GUARDED DISPENSE SWITCH C/W AT5618.6 ACFT HRS BUT N/A TO THIS ACFT.(SC2006, R/SPEC (AFS 594))

25-Jun-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACE#2 ENGINE CHIP DETECTOR LIGHT CAME ONDURING GROUND TAXI BACK TO PAD.INSTALLED SCAVANGE SCREENS TODETERMINE THE SOURCE OF METAL.MAINTENANCE COMPLETE. (SC2006, R/SPEC(AFS 34))

15-Jul-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEMEC F104952B, WAIVER FROM REQUIREMENTOF TTS 78148 TO INSPECT SEC IVDRIVESHAFT, EXTENDED FOR 90 DAYS FROM19JUL10. THIS ENTRY SERVES FOR NOTICEOF EXPIRATION ALSO AND WILL NOTREQUIRE A SEPARATE ENTRY FOR SUCH.

19-Jul-2010 1


dean.a.keirn

USAACEH-60-10-ASAM-11 COMMON COMPONENTRETIREMENT CHANGE TIMES UPDATE C/W AT5685.6 ACFT HRS. (DW0950)

02-Aug-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEH-60-10-ASAM-12 T700 SERIES ENGINESCOMMON COMPONENT RETIIREMENTCHANGE TIMES C/W AT 5689.7 ACFT HRS.(DW0950) (A FS594)

10-Aug-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEAWR 1681 DATED 10 MAY 10 COMPLETED AT5695.2 ACFT HRS. (SC2006, R/SPEC)

11-Aug-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEH-60-10-ASAM-15 IMPROVE EXTERNALSTORES SUPPORT SYSTEM (ESSS) FUEL;SYSTEM VENT ELBOW C/W AT 5702.8 ACFTHRS. (SC2006, R/SPEC) (A FS 87)

12-Aug-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEOPERATING WITHIN LIMITATIONS ANDRESTRICTIONS AS SPECIFIED IN AWR 1639 R-2(BFT/EDM) DTD 28 MAY 10 @ 5708.8 ACFT HRS.(SC2006, R /SPEC (A FS 594))

17-Aug-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEH-60-08-ASAM-11 COMPLIED WITHREQUIREMENTS OF H-60-08-ASAM-11 FLIGHTCONTROL INSPECTION AT __4566.3 ___ ACFTHRS. (SC2006, R /SPEC)

23-Aug-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACET/R BIAS MEASUREMENTS: RED--4.705 -5.041= .336 BLUE--4.088 - 4.426 =.338 BLACK--4.088 - 4.424 =.336 YELLOW--4.702 - 5.021 = .319@ 5730.1 ACFT HRS. (SC2006, R /SPEC)

04-Sep-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEH-60-10-ASAM-16 RESCUE HOIST CABLE CUTHARNESS CONNECTOR C/W AT 5731.2 ACFTHRS. W/ NO HOIST INSTALLED. (SC2006 ( AFS77))

09-Sep-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEH-60-08-ASAM-12 PARKER AEROSPACE AIRTURBINE STARTER (ATS) COMPLETED @4599.5 ACFT HRS. (SC2006, R /SPEC)

19-Sep-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEOPERATING IAW AWR 1529 (R-1) DTD 07 OCT10 (FOGS) @ 5819.9 ACFT HRS. (KJ0605)

07-Oct-2010 1

LOWE AHP

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 32 of 61

USAACEOPERATING IAW AWR 1514 (R-1) DTD 03 AUG10 @ 5833.9 ACFT HRS. (KJ0605)

18-Oct-2010 1

LOWE AHP

thomas.m.lilly

USAACEH-60-11-AMAM-04 H-60-11-AMAM-04 ULLS-A(E)(IMMC) (LCF CHANGE 61) C/W AT 5833.9 ACFTHRS. (SC2006 ( AFS 594))

26-Oct-2010 1

LOWE AHP

thomas.m.lilly

USAACEH-60-11-AMAM-03 H-60-11-AMAM-03 OILCOOLER FAN AXIAL BEARING C/W AT 5833.9ACFT HRS. (SC2006 (AFS 594))

26-Oct-2010 2

LOWE AHP

thomas.m.lilly

USAACEOPERATING IAW AWR 1515 DTD 14 JUN 10(MEMS TRC) YAW S/N: B000348 @ 5834.3 ACFTHRS. (KJ0605)

01-Nov-2010 1

LOWE AHP

thomas.m.lilly

USAACEMEC - F118390 ENG COWLING HAS VOIDSGREATER THAN 2 INCH IN DIAMETEREXCEEDING LIMITS IN TM 1-1520-237-23-6.ALSO COWLING HAS CRACK IN THECOMPOSITE WHERE IT ATTACHES TO THE AFTHINGE. AUTHORIZATION GRANTED TO REPAIRVOIDS BY CORE REPL & SKIN OVERLAY REFDMWR 1-1520-237-23-2 WP 027500 THRU 028000, TM 1-1520-237-23-6 WP 0387 OO AND TM 1-1500-204-23-10. (SC2006)

23-Nov-2010 1

LOWE AHP

thomas.m.lilly

USAACE#1 ENG COWLING DOOR REPLACED (SC2006) 24-Nov-2010 1

LOWE AHP

thomas.m.lilly

USAACEH-60-11-ASAM-03 HAMILTON STANDARDHYDRO-MECHANICAL UNITS (HMU) AT 5839.9ACFT HRS. (SC2006 ( AFS 545))

29-Nov-2010 1

LOWE AHP

thomas.m.lilly

USAACEH-60-11-ASAM-04 AN/ARN-153 TCN-500 TACANRECEIVER BEARING ERROR C/W AT 5839.9ACFT HRS. (SC2006 (AFS 545))

02-Dec-2010 1

LOWE AHP

thomas.m.lilly

USAACEACFT PLACED IN SHORT TERM STORAGE AT5839.9 ACFT HRS. (SC2006 (AFS 150))

06-Dec-2010 1

LOWE AHP

thomas.m.lilly

USAACEMEC - F118390 (A) THIS ADDENDUM REMOVESTHE REQUIREMENT TO INSTALL METALPLATES TO CRACK REPAIR. REPAIR THECRACK PER TM 1-1520-237-23-6, WP 0387 00TYPE II REPAIRABLE DAMAGE (PG 0387 00-7)IS MORE THAT AN ADEQUATE REPAIR ANDDRILLING HOLES TO INSTALL THE PLATE MAYWEAKEN THE COWLING. ALL OTHERSTANDARDS STILL APPLY. (SC2006)

13-Dec-2010 1

LOWE AHP

thomas.m.lilly

USAACEACFT TRANSFERRED TO HUNTSVILLE,AL FORPAINT ON THIS DATE @ ACFT HRS 5854.9.(DW0950, REC/SPEC)

21-Jan-2011 1

LOWE AHP

thomas.m.lilly

USAACEACFT PAINT STRIPPED BY TYPE VII PBM(HO666422)

31-Jan-2011 1

LOWE AHP

thomas.m.lilly

USAACEAIRCRAFT PRIMED WITH ONE COAT (MIL-PRF-2377J) PAINTED WITH ONE COAT (MIL-DTL-64159 TYPE II) (HO666422)

01-Feb-2011 1

LOWE AHP

thomas.m.lilly

USAACEH-60-11-AMAM-06 MEDICAL CAROUSELREFURBISHMENT C/W AT 5857.2 ACFT HRS.(HO666422)

08-Feb-2011 1

LOWE AHP

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 33 of 61

USAACEACFT RECEIVED FROM HUNTSVILLE, AL @5859.4 ACFT HRS. (KJ0605)

08-Feb-2011 2

LOWE AHP

thomas.m.lilly

USAACEH-60-11-ASAM-08 LOS / IFF ANTENNA ANDIVHMS ACCELEROMETER CONNECTORSSAFETY WIRE C/W AT 5862.9 ACFT HRS. (AFS767) (KJ0605 R/ SPEC)

11-Feb-2011 1

LOWE AHP

thomas.m.lilly

USAACE, FT. RUCKER,AL

H-60-11-ASAM-09 -INTERNAL AUXILIARY FUELTRANSFER SYSTEMS - C/W @ 5964.0 ACFTHRS. (AFS 76) (IAFTS - NOT INSTALLED)

29-Mar-2011 1

LOWE AHP

kathleen.m.jungell

USAACET/R RIG CHECK COMPLETED @ 5971.6 ACFTHRS. RED: 4.802/5.104/.302 , YELLOW:5.067/4.767/.300, BLACK: 4.453/4.152.301,BLUE: 4.453/4.154/.299

03-Apr-2011 1


kathleen.m.jungell

USAACET/R CABLE TENSION CHECK COMPLETED @5971.6 ACFT HRS. L/H: 160 LBS, R/H: 160 LBS@ 75 DEGREES.

03-Apr-2011 2


kathleen.m.jungell

USAACEH-60-11-ASAM-06 (CYCLIC STICK STOP BOLTS)C/W @ 5971.6 ACFT HRS (AFS 40)

03-Apr-2011 3


kathleen.m.jungell

USAACET/R BIAS CK COMPLETED @ 5972.1 ACFT HRS.BLUE 4.530-4.195=.335, RED 5.155-4.823=.332,YELLOW 5.150-4.812=.338, BLACK 4.509-4.175=.324

04-Apr-2011 1


kathleen.m.jungell

USAACEDELAYED ENTRY: ACFT INDUCTED INTO ULLS-A(E) ON 17 MAR 11 AT 5945.8 ACFT HRS.

06-Apr-2011 1


dean.a.keirn

USAACET/R BIAS CK COMPLETED @ 5972.5 ACFT HRS.BLACK: 4.48 / 4.15 / .33 YELLOW : 5.05 / 4.72 /.33 BLUE: 4.48 / 4.15 / .33 RED: 5.05 / 4.72 /.33

06-Apr-2011 2


kathleen.m.jungell

USAACET/R BIAS CK COMPLETED @ 5972.5 ACFTHRS.BLACK: 4.48 / 4.15 / .33 YELLOW : 5.05 /4.72 / .33 BLUE: 4.48 /4.15 / .33 RED: 5.05 / 4.72 /.33

06-Apr-2011 3


kathleen.m.jungell

USAACET/R CABLE TENSION CK COMPLETED @5980.9 ACFT HRS. FAILED & READJUSTED SETTENSION L/H: 156 R/H: 160 @ 78*F

11-Apr-2011 1


kathleen.m.jungell

USAACET/R RIG (BIAS) CK COMPLETED @ 5980.9 ACFTHRS. RED BEFORE 4.764 AFTER 5.072 =.308 BLUE BEFORE 4.077 AFTER 4.387 = .310YELLOW BEFORE 4.626 AFTER 4.936 =.310BLACK BEFORE 4.088 AFTER 4.396 = .308

12-Apr-2011 1


kathleen.m.jungell

USAACET/R CABLE TENSION CK COMPLETED @5989.5 ACFT HRS. R/H 158 L/H 156 @ 23.5 DEGC

14-Apr-2011 1


kathleen.m.jungell

USAACEH-60-AMAM-11 (AWR RELEASE STATUSUPDATE) C/W THIS DATE @ 6008.8 ACFT HRS.AFFECTED AWR'S NO LONGER APPLIED TOA/C. (AFS 594)

27-Apr-2011 1


kathleen.m.jungell


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 34 of 61

USAACETAIL ROTOR BIAS READINGS COMPLETED @6027.8 ACFT HRS. RED: 4.764/5.072 = .308;BLUE: 4.077/4.387 = .310; YELLOW: 4.626/4.936=.310; BLACK: 4.088/4.396 = .308.

09-May-2011 1


jeanora.g.thompson

USAACEH-60-11-AMAM-09 (DA FORM 2408-19-3 ENGINERECORD) C/W THIS DATE @ 6058.0 (AFS 545)

18-May-2011 1


kathleen.m.jungell

USAACEMEC F127642 - AUTHORIZATION GRANTED TOREPAIR (BY DAMON N HAY) BEARING ON THEUPPER PYLON STAB FITTING WORNEXCESSIVELY AND NEEDS REPLACEMENT.TM 1-1520-237-23-6 (WP 0432) CALLS OUTSIKORSKY TOOL IT 70700-20129-041 THATWOULD BE USE TO REMOVE THE SPHERICALBEARING AND THE TOW HAT BUSHING WHILETHE FITTING IS INSTALLED ON THE ACFT.SIKORSKY TOOOL KIT DOES NOT THAV THEPROPER TOOKING TO REMOVE AND ISNTALLTHE HAT BUSHINGS AS MENTIONED IN THE INTHE TM WP. THIS MEC IS TO REQUESTAUTHORIZATION TO USE THE TOOLS CALLEDFOR IN AFS DRAWING # 6277 IN CONJUCTIONWITH THE CUTTER AND STAKING TOOLSFROM SIKORSKY. ALL NOTES & WRNINGSSTILL APPLIES AS PER WP. THIS TASKREQURRES TWO SKILLED MACHINISTS.REFERENCE PREVIOUS APPROVALS UNDERMECS F124430, F124623, F125583, F125696,F126277, F126950 & F127190.

02-Jun-2011 1


kathleen.m.jungell

USAACET/R BIAS READINGS TO BE ENTERED INTOACFT HISTORICAL RECORDS COMPLETED AT6064.8 ACFT HRS. RED: 4.788/5.090/.302;YELLOW: 4.742/5.045/.303; BLUE:4.161/4.465/.304; BLACK: 4.199/4.500/.301

11-Jun-2011 1


bryan.w.hollis

USAACET/R CABLE TENSION CHECK READINGS TO BEENTERED INTO ACFT HISTORICAL RECORDSCOMPLETED AT 6064.8 ACFT HRS. L/H - 182,R/H - 182 @ 32.2° C.

11-Jun-2011 2


bryan.w.hollis

USAACEM/R RIG CHECK COMPLETED AT 6064.8 ACFTHRS. PRIMARY SERVO CONTROL ROD BIASADJUSTMENTS NOTED: FWD - 1/2 TURNSHORTEN; AFT - 1/2 TURN LENGTHEN; LAT -NEUTRAL.

11-Jun-2011 3


bryan.w.hollis

USAACEH-60-11-ASAM-06 (CYCLIC STICK STOP BOLTS)C/W @ 6064.85 ACFT HRS.

13-Jun-2011 1


kathleen.m.jungell

USAACEACFT NO LONGER OPERATING IAW MEOA6055 - M/R DROOP STOP BUSHING DE-BOND.REPLACED DURING 720 HR INS COMPLETED@ 6064.8 ACFT HRS.

13-Jun-2011 2


kathleen.m.jungell

USAACEH-60-11-AMAM-13 - EXTERNAL RESCUE HOISTMOUNT FITTING - NA TO THIS ACFT @ 6064.8ACFT HRS (AFS 594)

15-Jun-2011 1


kathleen.m.jungell


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 35 of 61

USAACET/R CABLE TENSION CK COMPLETED AT6064.8 ACFT HRS L/H-182, R/H 182 @ 32.2DEGREES 'C'

17-Jun-2011 1


tony.barnes

USAACE720 HR PMI #10 COMPLETED @ 6064.8 ACFTHRS. NEXT PMI #11 DUE @ 6784.8 ACFT HRS.

17-Jun-2011 2


bryan.w.hollis

USAACET/R CABLE TENSION CK COMPLETED @6074.0 ACFT HRS. RH: 145 LH: 150 TEMP -31

22-Jun-2011 1


kathleen.m.jungell

USAACEMAIN MOD SN: A26501113, TSN: 4972 -IMPENDING BYPASS BUTTON POPPED(8524475 @ 6079.0 ACFT HRS.) - REPLACEDM/MOD FILTER IAW TM 1-1520-237-23-7

30-Jun-2011 1


kathleen.m.jungell

USAACEACFT OPERATING IAW AWR 1639 (R-3) DTD 01JUN 11 (BFT/EDM) @ 6079.0 ACFT HRS.

01-Jul-2011 1


kathleen.m.jungell

USAACEH-60-11-ASAM-13 (ENG AIR INLET ANTI-ICING/MODULATING VALVE) COMP WITH BORESCOPE - BOTH VALVES PASSED. (AFS 594)

09-Jul-2011 1


kathleen.m.jungell

USAACEH-60-11-SOF-01 (DISCREPANT SELF LOCKINGDOUBLE HEXAGON NUTS) COMP THIS DATE@ 6096.1 (AFS 37)

09-Jul-2011 2


kathleen.m.jungell

USAACEH-60-11-AMAM-15 (IVHMS ACCELEROMETERS)INSP COMP THIS DATE @ 6097.3 ACFT NOTIVHMS EQUIPPED. (AFS 594 )

12-Jul-2011 1


kathleen.m.jungell

CSCOCM/ACE PERFORMED AT 6103.6 ACFT HRSBY TEAM MEMBER R. AFMA RASM-E.

18-Jul-2011 1

FT.CAMPBELL, KY.42223

dean.a.keirn

USAACEACFT OPERATING IAW MEO A6055 (REV. B)DUE TO BLUE /R LEAD DROOP STOP BUSHINGDE-BOND. REPLACEMENT OF BLUE M/R LEADDROOP STOP BUSHING REQUIRED AT THENEXT PMI DUE AT 6184.2 ACFT HRS.

22-Jul-2011 1


kathleen.m.jungell

USAACEH-60-11-ASAM-14 (ENGINE COWLING REPAIRRESTRICTIONS) C/W THIS DATE @ 6128.5ACFT HRS. (AFS 545)

22-Jul-2011 2


kathleen.m.jungell

USAACEDELAYED ENTRY: MEC F52915 (APPROVEDBY TAMMY S GRIFFIN 18 AUG 06) TO WELDHOLE IN THE STAGE 3 DUCT OF THE HIRRSUNIT. REPAIR: WELD MATERIAL AMS5510WITH WELDING ROD AMS5680 IAW DMWR 1-1520-237 (TAKS 03-16-03), AED A2221 AND TME1-1500-204-23

01-Aug-2011 1


kathleen.m.jungell

USAACEDELAYED ENTRY: MEC F58652 DTD 08 FEB 07(AUTHORIZED BY TAMMY S GRIFFIN 13 FEB07) - TO REPLACE R/H BEADED PANEL.REPAIR SHALL BE ACCOMPLISHED PERGUIDELINES IN SRA A -518-05 (WHICHINCLUDE PROCESS CONTROL 5726)

01-Aug-2011 2


kathleen.m.jungell


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 36 of 61

USAACEDELAYED ENTRY: MEC F61638 (AUTHORIZEDBY TAMMY S GRIFFIN 02 MAY 07) TO REPLACEB NUT ON LDS CABLE CRACKED, - REPLACENUT WITH NEW ONE USING SIKORSKY FIELDTEC REPORT 0087T009 DTD 3/19/07. AND THATENGINEERING STANDARD BE MADE TOCONTINUE REPLACEMENT OF FUTURE LDSCABLE NUTS P/N M61529-7 ON OTHERAIRCRAFT ON THE FORT RUCKER FLEET.

01-Aug-2011 3


kathleen.m.jungell

USAACEDELAYED ENTRY: MEC F79725 - REPAIRAUTHORIZED BY CHARLES A OVERMAN (06AUG 08) WP 0494 TABLE 1 GIVES LIMITS ONTHE INNER DUCT SUPPORT LINK BUT NOT ONTHE SUPPORT CLEVIS. THE INSPECTIONCRITERIA IT GIVES FOR THE SUPPORT LINKCAN AN ONLY BE EVALUATED WITH THELINKS REMOVED. THE #2 HIRSS WASREMOVED FOR A UPPER CARGO DOORTRACK REPLACEMENT. INSPECTING THEHIRSS IT WAS FOUND TO HAVE AXIAL PLAYBUT NOT RADIAL PLAY. REQUEST LIMITATIONON THE AXIAL PLAY ALLOWED. THE TM DOESNOT GIVE AN INSPECTION PROCEDURE ORLIMITS TO AXIAL AND RADIAL PLAY OF THELINK AND CLEVIS ASSEMBLY. - COMPLY WITHTHE DISPOSITION AND CRITERIA OF MECF79684( WHICH STATES TO MONITOR ANDREPLACE @ NEXT PMI)

01-Aug-2011 4


kathleen.m.jungell

USAACEDELAYED ENTRY: MEC F81373 DTD 09 SEP 08- CRACK ON THE TR DEICE CABLE HOUSINGTHAT COMES OFF OF THE DEICE ROTOR.WORK PACKAGE 1194 IN TM 1-1520-237-23STATES THAT THE ENTIRE OLD STYLESLIPRING MUST BE CHANGED IF ONE CABLEIS BAD BY THE CRITERIA IN THE WORKPACKAGE. IN THE PAST WE HAVE CUT THEBAD CABLE AND THE OPPOSITE CABLE TOEQUALIZE THE BALANCE, THIS REPAIR WASAPPROVED FOR OTHER ACFT UNDER MECF73966. REQUEST PERMISSION TO CUT THEBAD CABLE AND THE CABLE THAT IS 180DEGREES OUT TO EQUALIZE THE BALANCE.THE ACFT IS 151 HRS FROM PHASE AT WHICHTIME THE BAD SLIPRING WILL BE REPLACEWITH THE NEW STYLE. REQUEST TO CUTBAD CABLE AND THE OPPOSITE CABLE TOEQUALIZE BALANCE IS APPROVED BY TAMMYS GRIFFIN (10 SEP 08) DISABLING THE ANTI-ICE SYSTEM RENDERS THE ACFT "PARTIALLYMISSION CAPABLE" (PMC) FROM ICINGCONDITIONS. THE ACFT SHALL BE CARRIEDAS PMC WITH AN ENTRY ON THE DA FORM2408-13 UNTIL SUCH TIME THAT THE DE-ICESYSTEM IS FULLY REPAIRED/CORREC. THISIS A TEMPORARY AUTHORIZATION ANDSLIPRING SHALL BE FULLYREPAIRED/CORRECED. REQUEST TO CUTBAD CABLE AND THE OPPOSITE CABLE TOEQUALIZE BALANCE IS APPROVED BY TAMMYS GRIFFIN (10 SEP 08)

02-Aug-2011 1


kathleen.m.jungell


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 37 of 61

USAACEDELAYED ENTRY: MEC F90238 A - ADDENDUMA AUTHORIZED BY TAMMY S GRIFFIN 03 APR09 - PERMISSION GRANTED TO RE-INSTALLEDORIGINAL BUSHINGS AS LONG AS THEY MEETCRITERIA OF MANUFACTURER'SDRAWINGAND SIKORSKY INSTALLATION DRAWING.MEC CAN BE LOCATED IN THE BACK OF THEHISTORICAL BOOK.

02-Aug-2011 2


kathleen.m.jungell

USAACEDELAYED ENTRY: MEC F87406 DTD 29 JAN 09(AUTHORIZED BY TAMMY S GRIFFIN 13 FEB09) MAIN MAIN MOD A265-00160 AUTHORIZEDTO BE OVERSERVICE BY THREE QUARTSBEYOND THE FULL SERVICE LEVEL. THIS ISPROVIDED THAT THE REFERENCEDPUBLISHED FLUCTUATIONTROUBLESHOOTING PROCDURE WASFOLLOWED. THIS IS A ONE TIME DISPOSITIONFOR THIS ACFT SERIAL NUMBER ONLY.******THIS MAIN MOD TRANSMISSION IS NOLONGER INSTALLED********THIS ENTRY IS FORHISTORICAL PURPOSES ONLY.

04-Aug-2011 1


kathleen.m.jungell

USAACEACFT OPERATING IAW MEO A6055 (REV. B)DUE TO BLUE /R LEAD DROOP STOP BUSHINGDE-BOND. REPLACEMENT OF BLUE M/R LEADDROOP STOP BUSHING REQUIRED AT THENEXT PMI DUE AT 6184.2 ACFT HRS. HRSWERE ENTERED IN ERROR. CORRECT ACFTHRS ARE 6424.8

08-Aug-2011 1


kathleen.m.jungell

USAACEDELAYED ENTRY: MEC F117558 DTD 04 NOV 10REQUEST TO REPAIR L/H BEADED PANEL -REQUEST TO KEEP IN SERVICE DENIED - A/CNEED TO BE REPAIRED. INSTALL MWO KITAND FOLLOW/SHORE TO PREVIOUSLYESTABLISHED PARAMETERS FOR SHORINGAND FOLLOW INSTALLATION PROCEEDURESFOR THE MWO BEADED PANEL KIT.(AUTHORIZED BY DAMON N HAY 05 NOV 10

12-Aug-2011 1


kathleen.m.jungell

USAACEDELAYED ENTRY: MEC F100437 DTD 03 NOV09 - REQUEST TO RE-BOND STAINLESSSTEEL SHIM AROUND LOCK PIN BUSHINGHOLE. MEC CANCELED. PART WASREPLACED RATHER THAN BEING REPAIRED.(AUTHORIZED BY TAMMY S GRIFFIN 05 NOV09)

12-Aug-2011 2


kathleen.m.jungell

USAACEMAIN MOD SN: A26501113, TSN: 56096 @ 6203ACFT HRS. MAIN MOD TRANSMISSIONIMPENDING BYPASS BUTTON EXTENED.REPLACE FIRST STAGE FILTER ELEMENT IAWTM 1-1520-237-23-7 WP 626

15-Aug-2011 1


kathleen.m.jungell

USAACEDELAYED ENTRY: MEC F83696 DTD 30 OCT 08 -(MAIN MOD SN: A265-00160) HOUSING TBOEXT - REMOVED FROM HISTORICAL BOOK -THIS MAIN MOD TRANSMISSION WASREMOVED 24 MAR 09.

16-Aug-2011 1


kathleen.m.jungell


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 38 of 61

USAACEDELAYED ENTRY: MEC F65518 DTD 08 AUG 07- DROOP BUSHIN ON SPINDLE A204-11042HAVE BECOME UNSEATED. REQUEST TODEVIATE FROM WP 0566 00 AND REPLACEBUSHING WITHOUT REMOVING M/R SPINDLEAND M/R BLADE. SIMILAR REPAIRS HAVEBEEN COMPLETED UNDER MEC 62486, 62652,64685 AND 65413. PROCEDURE MAY BEPERFORMED WITHOUT REMOVING THESPINDLE OR BLADE. (AUTHORIZED BY TAMMYS GRIFFIN 10 AUG 07) THE BLADE ANDSPINDLE ARE NO LONGER INSTALLED ONTHIS ACFT.

16-Aug-2011 2


kathleen.m.jungell

USAACEH-60-11-AMAM-20 C/W THIS DATE @ 6278.6ACFTR HRS. (AN/ASN-128D SOFTWAREUPGRADE) SOFTWARE NOT INSTALLED

23-Sep-2011 1


janice.m.bruce

USAACEH-60-12-SOF-01 - TAIL ROTOR INTERMEDIATEGEARBOX COMPLETED AT 6307.2 ACFT HRSAS PER FORM 730

08-Oct-2011 1


olivia.d.williams

USAACEH-60-12-SOF-02 (TAIL ROTOR INTERMEDIATEGEARBOX) C/W AT 6307.2 ACFT HRS.

10-Oct-2011 1


debra.r.chancellor

USAACEH-60-12-SOF-03 (TAIL ROTOR INTERMEDIATEGEARBOX) C/W AT 6322.3 ACFT HRS. (AFS472).

14-Oct-2011 1


bryan.w.hollis

USAACEMAIN MOD SN: A265-01113, TSN: 5218 MAINMOD FILTER BUTTON POPPED @ 6325 ACFTHRS. COMPLETED SERVICEABILITY ISNP IAWWP 0626, 655, 656

18-Oct-2011 1


kathleen.m.jungell

USAACEH-60-11-AMAM-19 (IMMC LCF CHG 62REQUIREMENTS )C/W @ 6339.7 ACFT HRS

22-Oct-2011 1


janice.m.bruce

USAACEACFT NO LONGER OPERATING IAW AWR 1505(R-3) DTD 21 OCT 09 -SUPERCEDED BY AWR1505 R-4 DTD 21 OCT 11

22-Oct-2011 2


kathleen.m.jungell

USAACEACFT OPERATING IAW AWR 1505 (R-4) DTD 21OCT 11 (5-MICRON METAL MESH HYD FILTER)

22-Oct-2011 3


kathleen.m.jungell

USAACEACFT NO LONGER OPERATING IAW AWR 1529(R-1) DTD 07 OCT 10 (SUPERCEDED)

28-Oct-2011 1


kathleen.m.jungell

USAACEACFT OPERATING IAW AWR 1529 (R-2) DTD 07OCT 11 @ 6348.8 ACFT HRS.

28-Oct-2011 2


kathleen.m.jungell

USAACEH-60-AMAM-03 (TRANSPONDER & COMMONMISSILE WARNING SYSTEM) C/W CMWS MWONOT INSTL (AFS 732) @ 6357.8 ACFT HRS.

31-Oct-2011 1


kathleen.m.jungell

USAACEOPERATE IAW AWR 1455 (R-2) DTD 31 OCT 11(CAP) -SUPERCEDES AWR 1455 (R-1) DTD 23OCT 09

04-Nov-2011 1


kathleen.m.jungell


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 39 of 61

USAACEACFT OPERATING IAW AWR 1455 (R-3) DTD 10NOV 11 - SUPERCEDES AWR 1455 (R-2) DTD 31OCT 11 @ 6398.9 ACFT HRS.

21-Nov-2011 1


kathleen.m.jungell

USAACEACFT OPERATING IAW AWR 1153 (R-6) (JP-8-100) DTD 18 NOV 11 @6411.3 ACFT HRS.

05-Dec-2011 1


kathleen.m.jungell

USAACET/R BIAS COMPLETED @ 6410.5 ACFT HRS. :BLUE: 4.107-3.778=.329, RED: 4.615-4.281=.334,BLACK: 4.067-3.734=.333, YELLOW: 4.668-4.334=.334

05-Dec-2011 2


kathleen.m.jungell

USAACEH-60-12-ASAM-02 (DRAG BEAMREPLACEMENT) COMP @ 6413.9 ACFT HRSL/H: PASS R/H: FAIL (AFS 594)

06-Dec-2011 1


kathleen.m.jungell

USAACEH-60-11-AMAM-17 (TR INBOARD/OUTBOARDRETENTION PLATE SHIMS) COMP @ 6416.9ACFT HRS. (AFS 528)

07-Dec-2011 1


kathleen.m.jungell

USAACET/R BIAS COMPLETED @ 6416.9 ACFT HRS.RED: 5.228-4.881=.347 BLACK: 4.450-4.112=.338 YELLOW: 5.078-4.742=.336BLUE: 4.493-4.158=.335 MR#115383

10-Dec-2011 1


kathleen.m.jungell

USAACEBFT EDM ROUTER 3.1 UPGRADE COMPLETED@ 6416.9 ACFT HRS.

21-Dec-2011 1


kathleen.m.jungell

USAACEACFT NO LONGER OPERATING IAW MEOA6055 DUE TO BLUE M/R LEAD DROOP STOPBUSHING DE-BOND. BUSHING REPLACED @6426.3 ACFT HRS.

06-Jan-2012 1


kathleen.m.jungell

USAACEDELAYED ENTRY: ACFT OPERATING UNDERAWR 1738 DTD 01FEB11, AN/APX-118 CXP.AWR DOES **NOT** REQUIRE ANY 2408-13-1ENTRIES. THIS AWR SUPERSEDES ISAQ 116.

19-Jan-2012 1


dean.a.keirn

USAACEACFT NO LONGER OPERATING IAW AWR 1639(R-3) DTD 01 JUN 11 -SUPERCEDED BY AWR1800 DTD 30 NOV 11

19-Jan-2012 2


kathleen.m.jungell

USAACEACFT OPERATING IAW AWR 1800 DTD 30 NOV11 (EDM & BFT) @ 6458.5 ACFT HRS. -SUPERCEDES AWRS 1284, 1347, 1414 & 1639

19-Jan-2012 3


kathleen.m.jungell

USAACEACFT OPERATING IAW MEO A6055 DUE TORED M/R LEAD DROOP STOP BUSHING DE-BONDED. REPLACEMENT OF M/R DROOPSTOP BUSHING REQUIRED AT THE NEXT PMIDUE AT 6784.8 ACFT HRS.

02-Feb-2012 1


kathleen.m.jungell

USAACE10 FEB 12 - MAIN MOD ASSY SN: A265-01113,TSN: 5397 - MAIN MOD IMPENDING BYPASSINDICATOR POPPED. (8524475 @ 6504.1 ACFTHRS) AFTER RECORDS CK, FOUND BUTTONHAS NOT POPPED 3 TIMES IN LAST 200 HRSIAW TM 1-1520-237-23-7 WP 626, REPLACED1ST STAGE FILTER ELEMENT

10-Feb-2012 1


kathleen.m.jungell


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 40 of 61

USAACEH-60-12-SOF-04 - C/W @ 6506.9 ACFT HRS.N/A THIS ACFT EQUIP NOT INSTALLED . (AFS)

17-Feb-2012 1


kathleen.m.jungell

USAACESPECIAL INSPECTION OF CABIN CONTROLROD ENDS COMP @ 6521.6 ACFT HRS NOFAULTS FOUND.

26-Feb-2012 1


kathleen.m.jungell

USAACEACFT OPERATING IAW AWR 1251 (R-4) DTD 22FEB 12 (BIFILIAR EYEBOLTS) - SUPERSEDESAWR 1251 (R-3)

27-Feb-2012 1


kathleen.m.jungell

USAACEACFT OPERATING UNDER AWR 1251, R4 DTD22FEB12, EYEBOLTS ON BIFILAR ARMS,SUPERSEDING 1251 R3.

27-Feb-2012 2


dean.a.keirn

USAACEACFT OPERATING UNDER AWR 1648, R1 DTD26MAY10, MAGNUS LAPTOP.

28-Feb-2012 1


dean.a.keirn

USAACEH-60-12-ASAM-06 (UPPER BULKAWAY FUELSYSTEM BREAKAWAY VALVE ANDFIREEXTINGUISHING SYSTEM DIRECTIONALVALVE) INSP COMP-PASSED @ 6541.2 ACFTHRS. (AFS 77)

07-Mar-2012 1


kathleen.m.jungell

USAACEACFT OPERATING IAW AWR 1648, R2 DTD09MAR12, MAGNUS LAPTOPS, SUPERSEDINGR1.

20-Mar-2012 1


dean.a.keirn

USAACEAWR 1750: ACFT OPERATING IAW AWR 1750,R1 DTD 27MAR12, AN/AVS-6 SERIES NVG.

03-Apr-2012 1


dean.a.keirn

USAACEH-60-12-SOF-05 CAHNGE TO DEPOT REPAIREDLEGACY MAIN ROTOR BLADES COMPLIANCEDATE - COMP @ 6640.0 ACFT HRS. - NO -43XBLADES INSTALLED (AFS 594)

10-Apr-2012 1


kathleen.m.jungell

USAACE14 APR 12 - MAIN MOD ASSY SN: A265-01113,TSN: 5564 (8524475 @ 6661 ACFT HRS) - OILFILTER IMPENDING BYPASS BUTTON POPPED- INSP COMP IAW TM 1-1520-237-23 WP 626 -REPLACED FILTER AND RESET BUTTON

14-Apr-2012 1


kathleen.m.jungell

USAACEAWR 1681: ACFT OPERATING IAW AWR 1681,R2 DTD 14FEB12, EH60 DE-MOD,SUPERSEDING ALL PREVIOUS REVISIONS OF1681.

03-May-2012 1


dean.a.keirn

USAACEACFT OPERATING IAW MEO A6241 REV A . # 1ENG LATCH BRACKET REPAIRED IAW MEOA6241 TO BE REPLACED NLT THAN 90 DAYSFROM DATE OF INSTALLATION. DUE CHANGENLT 03 AUG 12

05-May-2012 1


kathleen.m.jungell

USAACEAWR 1681: ACFT OPERATING IAW AWR 1681,R3 DTD 04MAY12, EH60 DE-MOD,SUPERSEDING REV 2.

08-May-2012 1


dean.a.keirn

L-3 RASM-EOCM/ ACE PERFORMED AT 6723.8 AIRCRAFTHOURS BY TEAM MEMBERS QQ AND P

17-May-2012 1


jacob.a.weikart


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 41 of 61

USAACEMAIN MOD (A265-01113) FILTER BUTTONPOPPED @ 6742.1 ACFT H RS . REPLACEDFILTERS.

24-May-2012 1


janice.m.bruce

USAACEAWR 1220: ACFT OPERATING IAW AWR 1220,R6 DTD 25MAY12, ENHANCED SCHEDULEDMAINTENANCE. SUPERSEDING REV 5.

25-May-2012 1


dean.a.keirn

USAACEAWR 1515: ACFT OPERATING IAW AWR 1515,R2 DTD 07JUN12, TRC MEMS RATEGYROSCOPES, SUPERSEDING REVISION 1.

14-Jun-2012 1


dean.a.keirn

USAACEACFT DATE OF MANUFACTURE IS AUG 1986 18-Jun-2012 1


vickie.l.meadows

USAACEMEC F148226, AUTHORIZATION GRANTED TOUSE LOCALLY FABRICATED TOOLS TOREPLACE THE UPPER ACT AIRFRAME FITTINGBEARING.

22-Jun-2012 1


dean.a.keirn

USAACEMEC F148491, AUTHORIZATION GRANTED TOREPAIR TRANSITION COWLING VOID. 6761.6ACFT HRS.

26-Jun-2012 1


dean.a.keirn

USAACEACFT NO LONGER OPERATING UNDER MEOA6055(BUSHINGS DE-BONDED)- THEBUSHINGS (BLUE & RED) WERE REPLACE ATPHASE IAW IETM AT 6761.6 ACFT HRS.

28-Jun-2012 1


rhonda.e.jackson

USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-09 (HYDRAULIC LINE CHAFE DUE TOMISSING CLAMPS) @ 6761.6 ACFT HRS.

08-Jul-2012 1


vickie.l.meadows

USAACEMAIN ROTOR RIG CHECK COMPLETED AT6768.6 ACFT HRS THE FOLLOWING ADJ WEREMADE: FWD: NONE AFT: NONE LAT: SHORTEN2.5 FLATS

09-Jul-2012 1


rhonda.e.jackson

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-12-ASAM-01(TAIL ROTOR OUTPUT BEVELGEAR NONDESTRUCVTIVE INSPECTION) AT6761.6 ACFT HRS. (AFS 106) (T/R GB SN: A006-01066 - GS/B SN: G320-00132)

09-Jul-2012 2


rhonda.e.jackson

USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-09 AT 6761.3 ACFT HRS. (AFS 14)

09-Jul-2012 3


rhonda.e.jackson

USAACET/R BIAS CHECK COMPLETED IAW WP 1052RED 5.1405-4.773=0.332 BLUE 4.500-4.168=0.332 BLACK 5.086-4.757=.329 YELLOW4.478-4.148=0.330

09-Jul-2012 4


rhonda.e.jackson

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-12-AMAM-09 HYDRAULIC LINE CHAFE @6761.5

09-Jul-2012 5


vickie.l.meadows

USAACE720 HR PMI # 11 COMPLETED AT 6761.6 ACFTHRS. NEXT PMI#12 IS DUE AT 7481.6 ACFTHRS.

17-Jul-2012 1


rhonda.e.jackson


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 42 of 61

USAACEH-60-12-AMAM-12 (RESCINDED COMMONCOMPONENT REMOVAL DATE) COMP @ 6765.6ACFT HRS. (AFS594)

17-Jul-2012 2


kathleen.m.jungell

USAACEH-60-12-ASAM-08 (CARGO HOOK MANUALRELEASE SPRING ASSY) COMP @ 6766.3ACFT HRS (AFS 457)

19-Jul-2012 1


kathleen.m.jungell

USAACET/R CABLE TENSION CK COM @ 6771.4 ACFTHRS. (FAILED) L/H: 134 RH: 133 MR : 87703@ 27.8 ° C MR # 107157

24-Jul-2012 1


kathleen.m.jungell

USAACEAWR 1303: ACFT OPERATING IAW AWR 1303,R4 DTD 05JUL12, DAVID CLARK VIP ICS.EQUIPMENT MAY BE INSTALLED/REMOVEDPER MISSION REQUIREMENTS.

30-Jul-2012 1


dean.a.keirn

USAACEMEC F150472, AUTHORIZATION GRANTED TOEXTEND THE REPLACEMENT DATE OF THELEFT ENG COWL LATCH (AS PREV REPAIRED05MAY12 IAW MEO A6241 REV A) 90 DAYSFROM DATE OF THIS MEC. NOW DUE 28OCT12.

30-Jul-2012 2


dean.a.keirn

USAACEAWR 1514: ACFT OPERATING IAW AWR 1514,R2 DTD 27JUL12, DGNS-P3I AN/ASN-128D AAND B KIT, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.

01-Aug-2012 1


dean.a.keirn

USAACEAWR 1220: ACFT OPERATING IAW AWR 1220,R7 DTD 31JUL12, ESM, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

01-Aug-2012 2


dean.a.keirn

USAACET/R CABLE TENSION COMP @ 6780.5 LH: 133RH: 13133 @ 226.9 ° C (PASSED)

01-Aug-2012 3


kathleen.m.jungell

USAACEAWR 1800: ACFT OPERATING IAW AWR 1800,R1 DTD 20JUL12, EDM AND/OR BFT,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.

02-Aug-2012 1


dean.a.keirn

USAACE08 AUG 12 - MAIN MOD SN: A265-01113, TSN:5684 @ 6791 ACFT HRS. M/M FILTER BUTTONPOP. PERFORMED COMPLETE SVCABILITY CKIAW TM 1-1520-237-23 WP 0626 & 0627

08-Aug-2012 1


kathleen.m.jungell

USAACENO LONGER OPERATING IAW MEC F150472 &MEO A6241 - L/H ENGINE COWLING LATCHSUPPORT REPLACED THIS DATE @ 6830.4ACFT HRS IAW 1-1520-237-23 WP 0324

20-Aug-2012 1


kathleen.m.jungell

USAACEH-60-12-ASAM-09 (BREEZE EASTERNEXTERNAL RESCUE HOIST CARTRIDGEACTUATED DEVICE (CAD) ELECTRICALCONNECTOR) NA THIS ACFT @ 6838.4 ACFTHRS. ( AFS 594 )

22-Aug-2012 1


kathleen.m.jungell

USAACE23 AUG 13 - ENG ASSY SN: GE-E-306009 WITHENG CUMULATIVE CTS: 3117 / 11132 / 18415 /5851 (HR SN: CAO01295 RDGS: 524 / 2143 / 458/ 6561) ACFT 8524475 @ 6841.6 ACFT HRS.CHIP LITE APPEARED - COMPTROUBLESHOOTING PROCEDURE 46 WP 0055TM1-2840-248-23 (NO CHIPS FOUND)

23-Aug-2012 1


kathleen.m.jungell


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 43 of 61

USAACEAWR 1153: ACFT OPERATING IAW AWR 1153,R7 DTD 24AUG12, JP-8+100, SUPERSEDINGALL PRIOR REVISIONS OF THIS AWR.

29-Aug-2012 1


dean.a.keirn

USAACEAWR 1251: ACFT OPERATING IAW AWR 1251,R5 DTD 31AUG12, EYEBOLTS, SUPERSEDINGANY PRIOR REVISIONS OF THIS AWR.

31-Aug-2012 1


dean.a.keirn

USAACEAIRCRAFT BEING OPERATED IAW MEO A6055REV C DUE TO RED MAIN ROTOR DROOPSTOP BUSHING DE-BONDED. REPLACEMENTOF M/R DROOP STOP BUSHING REQUIRE ATTHE NEXT PMI 360 HR DUE AT 7121.6 ACFTHRS.

05-Sep-2012 1


kathleen.m.jungell

FT. RUCKER, ALH-60-12-AMAM-15 (TRIM ACTUATORS) COMP @6877.4 ACFT HRS. (AFS 594)

17-Sep-2012 1


USAACE

USAACEAWR 1455: ACFT OPERATING IAW AWR 1455,R4 DTD 18SEP12, BATTELLE CAP,SUPERSEDING ANY PRIOR REVISIONS OFTHIS AWR. THIS AWR ALSO REPLACES ISAQ123 (2MAR06).

21-Sep-2012 1


dean.a.keirn

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-12-ASAM-07, ELECTRICAL WIRE CHAFE, ONTHIS DATE.

03-Oct-2012 1


dean.a.keirn

USAACE03 OCT 12 - MAIN MOD SN: A265-01113 TSN:5821 (8524475 @ 6928.0 ACFT HRS) MAIN MODFILTER BUTTON POPPED - COMPLETED M/MSERVICABILITY INSP IAW WP 0626 NO CHIPSOR PARTICALS FOUND OK REPLACED M/MFILTERS.

03-Oct-2012 2


kathleen.m.jungell

USAACEH-60-12-ASAM-07 (ELECTRICAL WIRE CHAFE)COMP @ 6929.0 ACFT HRS. (AFS 121 )

04-Oct-2012 1


kathleen.m.jungell

USAACEMEC F154149, AUTHORIZATION GRANTED FORA DEVIATION OF THE PEDAL ADJUST ACCESSCOVER INSTALLATION PN 70209-01013-101/102. BOLT PN AN3-3A MAY BE USED INLIEU OF SCREW MS27039-1-07.

15-Oct-2012 1


dean.a.keirn

USAACEAWR 1220: ACFT OPERATING IAW AWR 1220,R8 DTD 01NOV12, ENHANCED SCHEDULEDMAINTENANCE, SUPERSEDING ANY PRIORREVISIONS OF THIS AWR.

01-Nov-2012 1


dean.a.keirn

USAACEH-60-13-AMAM-02 (AHRS) WIRING COMP/PASS@ 7001.6 ACFT HRS. (AFS 594)

07-Nov-2012 1


kathleen.m.jungell

USAACEH-60-13-ASAM-01 (ANTI-COLLISION LIGHTSPOWER SUPPLY) INSP COMP (PASS) @ 7027.3ACFT HRS. (AFS 42)

28-Nov-2012 1


kathleen.m.jungell

USAACEH-60-13-AMAM-03 (DIGITAL ENGINE COTNROLUNIT/ELECTRONIC DIGITAL ENGINE CONTROLUNIT TURBINE GAS TEMPERATURE BIAS) C/W@ 7027.3 ACFT HRS. (AFS 42)

28-Nov-2012 2


kathleen.m.jungell


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 44 of 61

USAACE12 DEC 12 - ENG ASSY SN: GE-E-306112 WITHENG CUMULATIVE CTS: 3193/15056/9112/7095HR (ECDH0618) RDGS: 497/2192/639/1295 -(8524475 @ 7067 ACFT HRS) DURING THE 25GALLON FUEL CHECK THE #1 ENGINE FUELPRESSURE CAUTION LIGHT ILLUNINATEDAND THE ENGINE FLAMED OUT DURINGSTART WITH THE FUEL SELECTOR HANDLE INTHE CROSSFEED POSITON AND THE PCL ATIDLE. THE ENGINE HAD BEEN PRIMED IAW TM1-1520-237-MTF. THIS HAPPENED 2 TIMES.REPLACED #2 MAIN FUEL BREAKAWAY VALVEON #2 RACETRACK IAW TM 1-1520-237-23 WP0075 & WP 0992.

12-Dec-2012 1


kathleen.m.jungell

USAACEINSP A470 - REPLACE NUMBER TWOCROSSFEED VALVE COMP @ 7067 ACFT HRS.

12-Dec-2012 2


kathleen.m.jungell

USAACE#2 MAIN FUEL BREAKAWAY VALVE REPLACED(ON RACETRACK) REPLACED IAW TM-1-1520-237-23 WP 0992

19-Dec-2012 1


kathleen.m.jungell

USAACE10 JAN 13 - MAIN MOD ASSY SN: A265-01113,TSN: 5968 - MAIN TRANSMISSION BYPASSBUTTON EXTENDED (8524475 @ 7075 ACFTHRS) MAIN TRANSMISSION, INPUT MODULES,AND MAIN MODULE FILTER BUTTONSERVICED IAW TM 1-1520-237-23 WP 0626,0655, & 0657. MR# 120831

10-Jan-2013 1


kathleen.m.jungell

USAACEH-60-13-AMAM-04 (ULLS-AE LCF CHANGE 63REQUIREMENTS) COMP @ 7075.2 ACFT RHS.(AFS 594)

10-Jan-2013 2


kathleen.m.jungell

USAACEH-60-13-AMAM-05 (MLG BRAKES) COMP @7103.8 ACFT HRS. (AFS 576)

20-Jan-2013 1


kathleen.m.jungell

USAACEAIRCRAFT BEING OPERATED IAW MEO A6055REV C DUE TO RED MAIN ROTOR DROOPSTOP BUSHING DE-BONDED. REPLACEMENTOF M/R DROOP STOP BUSHING REQUIRE ATTHE NEXT PMI 360 HR DUE AT 7126.7 ACFTHRS

25-Jan-2013 1


kathleen.m.jungell

USAACEACFT NO LONGER OPERATING IAW MEOA6055 REV C (MAIN ROTOR DROOP STOPBUSING DE-BONED) M/R DROOP STOPBUSING REPLACED @ 7124.2 ACFT HRS.

01-Feb-2013 1


kathleen.m.jungell

USAACEM/R RIG COMP @ 7124.2 ACFT HRS. PRIMARYSERVO CONTROL ROD BIAS: NOADJUSTMENTS MADE.

03-Feb-2013 1


kathleen.m.jungell

USAACEAWR 1738: ACFT OPERATING IAW AWR 1738,R1 DTD 01FEB13, AN/APX-118 COMMONTRANSPONDER, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR AND ISAQ 116 WITHALL REVISIONS.

04-Feb-2013 1


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 45 of 61

USAACETAIL ROTOR BIAS COMPLETED AT 7124.2ACFT HRS

COLOR / DIM A /DIM B / DIFFERENCE /BLDE SET DEG / BLD

FINAL DEGRED 4.869 5.209.340 Not Given 3.0BLACK 4.0674.411 .344

Not Given 3.0YELLOW 4.8325.166 .334

Not Given 3.0BLUE 4.0834.434 .351

Not Given 3.0(MR # 100893 & MR #120212)

04-Feb-2013 2


kathleen.m.jungell

USAACEH-60-13-AMAM-06 (CEFS) NA @ 7129.1 ACFTHRS. CEFS NOT INSTALLED (AFS 472)

13-Feb-2013 1


kathleen.m.jungell

USAACEAWR 1251: ACFT OPERATING IAW AWR 1251,R6 DTD 28FEB13, EYEBOLTS ON BIFILARARMS, SUPERSEDING ALL PRIOR VERSIONSOF THIS AWR.

01-Mar-2013 1


dean.a.keirn

USAACEH-60-13-ASAM-03 (M/R SPINDLE ANTI-FLAPASSEMBLIES) C/W @ 7169.9 ACFT HRS. (AFS410)

02-Mar-2013 1


kathleen.m.jungell

USAACEH-60-13-ASAM-04 (PLASTIC MEDIA BLAST &OXIDE FLAKE RESIDE) C/W @ 7208.2 ACFTHRS. (AFS 594)

27-Mar-2013 1


kathleen.m.jungell

USAACEAWR 1750: ACFT OPERATING IAW AWR 1750,R2 DTD 29MAR13, AN/AVS-6 NVG,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR AND THE AMSRD-AMR-AE-T AWR FOROPERATION OF THE ANVIS AN/AVS-6 SERIESNVG IN ARMY AIRCRAFT DTD 26JUN06.

29-Mar-2013 1


dean.a.keirn

USAACEH-60-13-AMAM-07 (LOAD DEMAND SPINDLECABLE CLEARANCE) C/W @ 7213.3 (AFS 594)

01-Apr-2013 1


kathleen.m.jungell

USAACEH-60-13-ASAM-05 (ELECTRIC RESCUE HOIST)CW @ 7213.3 ACFT HRS. (AFS 121)

08-Apr-2013 1


kathleen.m.jungell

USAACEMAIN MOD SN: A265-01113, TSN: 6112 - FILTERBYPASS BUTTON POPPED @ 7219.3 ACFTHRS. COMPLETED MAIN TRANSMISSIONSERVICABILITY INSPECTION IAW TM 1-1520-237-23 WPS 0626,0655,0656

09-Apr-2013 1


kathleen.m.jungell

USAACEAWR 1800: ACFT OPERATING IAW AWR 1800,R2 DTD 22MAR13, EDM AND/OR BFT,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR AND AWR'S 1284, 1347, 1414 AND 1639.

11-Apr-2013 1


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 46 of 61

USAACEH-60-13-ASAM-06 (PMI CHECKLIST CHANGES)C/W @ 7249.6 ACFT HRS. (AFS 76)

10-May-2013 1


tony.barnes

USAACEH-60-13-SOF-01 WAS C/W AT 7279.9 ACFT HRS 31-May-2013 1


rhonda.e.jackson

L-3 RASM-EOCM/ACE PERFORMED AT 7320.1 AIRCRAFTHOURS BY TEAM MEMBERS P AND QQ

21-Jun-2013 1


jacob.a.weikart

USAACEM/R RIG COMPLETED AT 7320.1 ACFT HRS,THE FOLLOWING ADJ WERE MADE: FWD:SHORTEN 1/2 LENGTH AFT: LENGTHEN 1/2TURN LAT: NEUTRAL

27-Jun-2013 1


rhonda.e.jackson

USAACETAIL ROTOR BIAS COMPLETED AT 7320.1ACFT HRS COLOR \ DIM A \ DIM B \ DIFF \BLADE SET DEG \ BLADE FINAL DEGRED4.782 5.114 .332 0.23BLACK 4.096 4.408 .312 0.13YELLOW 4.80 4.122 .322 0.33BLUE 4.117 4.422 .305 0.23

27-Jun-2013 2


rhonda.e.jackson

USAACET/R CABLE TENSION CK COMPLETED AT7320.1 ACT HRS- L/H: 154 R/H 154 AT 28.5'C

27-Jun-2013 3


rhonda.e.jackson

USAACEH-60-13-AMAM-01 (FLIGHT CONTROL RIGGINGPROCEDURES) C/W AT 7320.1 ACFT HRS.

27-Jun-2013 4


rhonda.e.jackson

USAACEMAIN ROTOR RIG COMPLETED AT 7320.1 ACFTHRS, THE FOLLOWING ADJ WERE MADE-FWD: SHORTEN 1/2 TURN AFT: LEGTHEN 1/2TURN LAT: NEUTRAL

27-Jun-2013 5


rhonda.e.jackson

USAACEH-60-13-AMAM-11 CW AT 7320.1 ACFT HRS. 12POINT BOLTS NOT INSTALED, FAIL AFS 594

08-Jul-2013 1


rhonda.e.jackson

USAACEMEC F169141, Authorization granted to repairCRACKED 34.5 CHANNEL IAW AJM-BL34-1Cfor RBL 34.5 and standard sheet metal practicesper TM 1-1520-237-23-6 and TM 1-1500-204-23series. 7320.1 ACFT HRS.

10-Jul-2013 1


dean.a.keirn

USAACET/R CABLE TENSION CK COMPLETED AT7330.3 ACFT HRS L/H: 140 R/H: 140 AT 27'C

31-Jul-2013 1


rhonda.e.jackson

USAACEGEN-13-AMAM-04 AN/APN-209 RADARALTIMETER SET COMPONENT TRACKINGCOMPLETED AT 7330.3 ACFT HRS.

31-Jul-2013 2


rhonda.e.jackson

USAACEAWR 1251: ACFT OPERATING IAW AWR 1251,R7 DTD 28AUG13, EYEBOLTS, SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR.

29-Aug-2013 1


dean.a.keirn

USAACECOMPLED WITH REQUIREMENTS OF H-60-13-AMAM-10 (LCF CHANGE 64) @ 7415 ACFT.HRS.

07-Sep-2013 1


stephanie.n.ziglar


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 47 of 61

USAACETAIL ROTOR BIAS COMPLETED AT 7320.1ACFT HRS COLOR \ DIM A \ DIM B \ DIFF \BLADE SET DEG \ BLADE FINAL DEGRED4.79 5.09 .300 0.03BLACK 4.09 4.39 .300 0.03YELLOW 4.78 5.10 .320 0.23BLUE 4.11 4.43 .320 0.23

03-Oct-2013 1


stephanie.n.ziglar

USAACEAWR 1505: ACFT OPERATING IAW AWR 1505,R5 DTD 18OCT13, 5-M HYD FILTER,SUPERSEDING ANY PRIOR VERSION OF THISAWR.

22-Oct-2013 1


dean.a.keirn

USAACEAWR 1529: ACFT OPERATING IAW AWR 1529,R3 DTD 30OCT13, DUAL AHRS, SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR.

31-Oct-2013 1


dean.a.keirn

USAACEMEC F174620, AUTHORIZATION GRANTED TOREPAIR VOID IN RH ESSS PLATFORM PANEL.7480.6 ACFT HRS.

01-Nov-2013 1


dean.a.keirn

USAACEMEC F174619, AUTHORIZATION GRANTED TOREPAIR VOID IN LH ESSS PLATFORM PANEL.7480.6 ACFT HRS.

01-Nov-2013 2


dean.a.keirn

USAACEMEC F174613, AUTHORIZATION GRANTED TOREPAIR VOID IN RH OIL COOLER ACCESSDOOR. 7480.6 ACFT HRS.

01-Nov-2013 3


dean.a.keirn

USAACEMEC F174611, AUTHORIZATION GRANTED TOREPAIR VOID IN LH OIL COOLER ACCESSDOOR. 7480.6 ACFT HRS.

01-Nov-2013 4


dean.a.keirn

USAACEMEC F174608, AUTHORIZATION GRANTED TOREPAIR AN APPROX 0.250" CRACK IN LH TAILSTRUT ACCESS UPPER FORWARD CORNER.7480.6 ACFT HRS.

01-Nov-2013 5


dean.a.keirn

USAACEH-60-14-SOF-01 ,INSPECTION FOR BREEZEEASTERN EXTERNAL RESCUE HOISTINSTALLATION, COMPLETED AT 7480.6 ACFTHRS. NOT INSTALLED ON THIS AIRFRAME ATTHIS TIME.

04-Nov-2013 1


christina.l.negron

USAACEMEC F174917, AUTHORIZATION GRANTED TOREPAIR VOID IN FWD SLIDING PYLON. 7480.6ACFT HRS.

07-Nov-2013 1


dean.a.keirn

USAACEMEC F174985, Authorization granted to uselocally fabricated tool to replacebearing/bushing in upper actutator fitting.

07-Nov-2013 2


dean.a.keirn

USAACEMEC F174951A, AUTHORIZATION GRANTED TOTEST #1 AND #2 MAIN FUEL CHECK VALVESBY INCREASING THE PRESSURE IN STEP 28,WP 1013, EM0013, UP TO BUT NOT EXCEEDING60 PSI. 7480.6 ACFT HRS.

12-Nov-2013 1


dean.a.keirn

USAACEENTRY DATED 25 NOV 2013, ENTRY #2INCORRECTLY STATES THAT PHASE #13 ISDUE AT 8280.6 ACFT HRS. PHASE #13 IS DUEAT 8200.6 ACFT HRS.

13-Nov-2013 1


christina.l.negron


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 48 of 61

USAACEH-60-12-ASAM-02- DRAG BEAMREPLACEMENT C/W AT 7480.6 ACFT HRS.REPLACE R/H DRAG BEAM WITH NEW 043STYLE.

14-Nov-2013 1


christina.l.negron

USAACETAIL ROTOR CABLE TENSION CHECKCOMPLETED AT 7480.6 ACFT HRS. ADJUSTED,TEMP: 23.6 C MR#107156 160 L/H 160 R/H MR#126114

22-Nov-2013 1


christina.l.negron

USAACEMAIN ROTOR RIG COMPLETED AT 7481.6 ACFTHRS. FWD: NO ADJUSTMENT, AFT:: NOADJUSTMENT LAT: NO ADJUSTMENT.

22-Nov-2013 2


christina.l.negron

USAACETAIL ROTOR BIAS CHECK COMPLETED AT7480.6 ACFT HRS. COLOR DIM A DIMB DIFFERENCE SET DEGFINAL DEGRED 4.759 5.0860.327 0.53.0BLACK 4.039 4.364 0.3250.3 3.0YELLOW 4.745.065 0.325 0.53.0BLUE 4.038 4.364 0.3260.3 3.0

22-Nov-2013 3


christina.l.negron

USAACEAWR 1251: ACFT OPERATING IAW AWR 1251,R8 DTD 26NOV13, EYEBOLTS ON BIFILARARMS, SUPERSEDING ALL PRIOR VERSIONSOF THIS AWR.

25-Nov-2013 1


dean.a.keirn

USAACE720 HOUR PHASE #12 WAS COMPLETED AT7480.6 ACFT HRS, THE NEXT 720 HOUR PHASE(#13) IS DUE AT 8280.6 ACFT HRS.

25-Nov-2013 2


christina.l.negron

USAACEMEC F175919 - DURING PMI INSPECTIONFOUND RIGHT COCKPIT DOOR POSTCHANNED CRACKED AT DOOR CHECK AREA,APPROXIMATELY 1/8 INCH VISIBLE,AUTHORIZATION GRANTED TO REPAIR R/HCOCKPIT DOOR POST AS OUTLINE IN MECF175919

02-Dec-2013 1


olivia.d.williams

USAACEH-60-14-ASAM-02 (HEALTH USAGEMONITORING SYSTEM (HUMS)ACCELEROMETERS) C/W 10 DEC 13 AT 7481.1ACFT. HRS. N/A THIS ACFT.

11-Dec-2013 1


anthony.s.speigner

USAACEH-60-13-AMAM-15 (CRASHWORTHY EXTERNALFUEL SYSTEM (CEFS) RIGHT HAND FUELCELL COVER PLATE) C/W 10 DEC 13 AT 7481.1ACFT. HRS., PASS, CEFS NOT INSTALLED.

11-Dec-2013 2


anthony.s.speigner

USAACEAWR 1529: ACFT IS NO LONGER OPERATINGIAW AWR 1529, ALL REVISIONS. ACFTRECONFIGURED FROM DUAL AHRS TOSINGLE AHRS. SEE AWR 1444.

18-Dec-2013 1


dean.a.keirn

USAACEAWR 1444: ACFT OPERATING IAW AWR 1444,R6 DTD 11JUL13, SINGLE AHRS.

18-Dec-2013 2


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 49 of 61

USAACEH-60-14-AMAM-03 (DISCREPANT CONNECTINGLINKS) C/W 02 JAN 14 AT 7495.5 ACFT HRS,PASS.

03-Jan-2014 1


anthony.s.speigner

USAACET/R CABLE TENSION CHECK COMPLETED 09JAN 14 AT 7498.3 ACFT. HRS., IAW 1-1520-237-23 WP 1747 OUTSIDE OF WINDOW , FAILED ,MR#108407, TEMP: 7 DEG C L/H: 115, R/H: 130ADJUSTED TO L/H: 104, R/H 104.

10-Jan-2014 1


anthony.s.speigner

USAACEH-60-14-ASAM-03 (ENGINE INLET BARRIERFILTER(EIBF) BRACKET REMOVAL) C/W 07JAN 2014 AT 7498.6 ACFT. HRS.

10-Jan-2014 2


anthony.s.speigner

USAACET/R CABLE TENSION CHECK C/W 15 JAN 14 AT7508.1 ACFT. HRS., PASSED I/A/W 1-1520-237-23 WP 1747 M/R TENSIONMETER 109407THERMOMETER 118174 L/H 92 R/H 91 AT 3 DEGC.

15-Jan-2014 1


anthony.s.speigner

USAACEH-60-14-AMAM-08 (AN/ASC-15E CIRCUITBREAKER PROTECTION) C/W 13 MAR 14 AT7637.3 ACFT. HRS.

14-Mar-2014 1


anthony.s.speigner

USAACEAWR 1648: ACFT OPERATING IAW AWR 1648,R3 DTD 28MAR14, MAGNUS LAPTOP,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.

27-Mar-2014 1


dean.a.keirn

USAACEH-60-14-AMAM-05 LEGITIMATE CODE FILECHANGE 65 REQUIREMENTS COMPLETED AT7680.4 ACFT HRS.

05-Apr-2014 1


vickie.l.meadows

USAACEH-60-14-AMAM-10 HONTEK COATED MAINROTOR BLADE REMOVAL COMPLETED AT7693.7 ACFT. HRS. "N/A TO THIS AIRCRAFT.

14-Apr-2014 1


anthony.s.speigner

USAACEH-60-14-AMAM-10 HONTEK COATED MAINROTOR BLADE REMOVAL COMPLETED AT8022.5 ACFT. HRS. "N/A TO THIS AIRCRAFT.

15-Apr-2014 1


anthony.s.speigner

USAACEAWR 1444: ACFT OPERATING IAW AWR 1444,R7 DTD 14APR14, SINGLE AHRS,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.

16-Apr-2014 1


dean.a.keirn

USAACEH-60-14-AMAM-12 (MAIN ROTOR SPINDLE NUTRETIREMENT LIFE EXTENTION) C/W 23 APR 14AT 7714.5 ACFT. HRS.

25-Apr-2014 1


anthony.s.speigner

USAACEH-60-14-ASAM-06 (FLIGHT CONTROL MIXERASSY) C/W 23 APR 14 AT 7714.5 ACFT. HRS.

25-Apr-2014 2


anthony.s.speigner

USAACEH-60-14-AMAM-12 MAIN ROTOR SPINDLE NUTRETIREMENT LIFE COMPLIED WITH

29-Apr-2014 1


mark.a.trehern


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 50 of 61

USAACEACFT OPERATING IAW AWR 1681, R4 DTD30APR14, EH DE-MOD, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR AND AWR'S927 AND 890.

06-May-2014 1


dean.a.keirn

USAACEH-60-14-AMAM-14 (IVHMS CABLING)REQUIREMENTS COMPLETED AT 7759.6 ACFTHRS (MWO NOT APPLIED)

28-May-2014 1


olivia.d.williams

USAACEPOST FLIGHT XMSN (A25-01113) OIL FILTERBUTTON POP, CHECKED AND INSP, FOUNDNO EVIDENCE OF METAL REPLACED MMFILTERS IAW TM 1-1520-237-23 WP 065 06560655 AT 6653 XMSN HRS (ACFT 8524475, ACFTHRS 7759.5)

28-May-2014 2


olivia.d.williams

USAACEACFT OPERATING IAW AWR 1505, R6 DTD03JUN14, 5M HYD FILTER, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

04-Jun-2014 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1251, R9 DTD06JUN14, EYEBOLTS, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

06-Jun-2014 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1515, R3 DTD02JUN14, TRC RATE GYROS, SUPERSEDINGISAQ 126 AND ALL PRIOR VERSIONS OF THISAWR.

10-Jun-2014 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1841, R1 DTD23JUL12, HONEYWELL ATS TESTING.STARTER SN 03 INSTALLED IN THE #2POSITION THIS DATE AT 7833.9 ACFT HRS.

18-Jun-2014 1


dean.a.keirn

USAACEH-60-14-SOF-03, DISCREPANT SELF-LOCKINGNUTS, C/W AT 7842.1 ACFT HRS. PASSED. AFSINSP. 135

25-Jun-2014 1


brian.k.dow

USAACET/R RIG CHECK BLADE ANGLES BLUE 2.8BLACK 2.8 RED 2.8 YELLOW 2.8 @ 7844.8

29-Jun-2014 1


vickie.l.meadows

USAACEH-60-14-AMAM-16, ATTITUDE HEADINGREFERENCE UNIT 2410 TRACKINGCOMPLETED ON 19 JUL 14 AT 7863.6 ACFT.HRS.

16-Jul-2014 1


anthony.s.speigner

DCR RASM-COCM/ACE PERFORMED AT 7869.3 AIRCRAFTHOURS BY TEAM MEMBERS P AND QQ

25-Jul-2014 1


jacob.a.weikart

USAACEACFT OPERATING IAW AWR 1800, R3 DTD16JUL14, EDM AND/OR BFT, SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR ANDAWR'S 1284, 1347, 1414, 1639.

25-Jul-2014 2


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1841, R3 DTD16JUL14, HONEYWELL STARTER PN 3505300-10, SUPERSEDING ALL PRIOR VERSIONS OFTHIS AWR.

25-Jul-2014 3


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1514, R3 DTD31JUL14, DGNS, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.

31-Jul-2014 1


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 51 of 61

USAACEH-60-14-ASAM-09 (ENGINE OUTPUT SHAFT)C/W 31 JUL 14 AT 7869.3 ACFT. HRS.

01-Aug-2014 1


anthony.s.speigner

USAACEMEC F187172, RIGHT CABIN CONDUIT FORTHE TAIL ROTOR CABLE CRACKED.AUTHORIZATION GRANTED TO USE CABLECONDUIT PN 70400-00510-101 (WILL HAVE TOBE TRIMMED TO FIT) IN LIEU OF PN 70400-00510-102. 7869.3 ACFT HRS.

05-Aug-2014 1


dean.a.keirn

USAACET/R CABLE TEMSION CHECK COMPLETED 08AUG 2014 AT 7869.3 ACFT. HRS., ADJUSTEDIAW WP 1747 & WP 1156 TM 1-1520-BLACKHAWK L/H 135, R/H 135 AT 28 DEG C.MR# THERM. 126351/TENS. 122358.

11-Aug-2014 1


anthony.s.speigner

USAACET/R CABLE TENSION CHECK COMPLETED 12AUG 14 AT 7878.0 ACFT. HRS., FAILEDADJUSTED I/A/W TM 1-1520-BLACKHAWK WP1747 & WP 1156 L/H 145, R/H 145 AT 28 DEG C,MR# TENS. 122358 / MR# THERM. 126351.

12-Aug-2014 1


anthony.s.speigner

USAACET/R CABLE TENSION CHECK COMPLETED 16AUG 14 AT 7888.0 ACFT. HRS., FAILED CHECKI/A/W EM0013 WP 1747 00 NUMBER NOTWITHIN 5 DEG. ADJUSTED CABLES TO L/H134, R/R 134 AT 24 DEG C.

18-Aug-2014 1


anthony.s.speigner

USAACET/R CABLE TENSION CHECK COMPLETEDPASSED IAW EM0013 WP 1747 00 AND 1156 00READINGS WERE L/H 133 R/H 133 AT 28.7 DEGF.

22-Aug-2014 1


anthony.s.speigner

USAACEH-60-14-SOF-04 (OPERATORS ANDCREWMEMBERS CHECKLIST) C/W 27 AUG 14AT 7913.2 ACFRT. HRS.

27-Aug-2014 1


anthony.s.speigner

USAACEH-60-14-ASAM-10 (MAIN TRANSMISSIONPLANATARY CARRIER ASSEMBLY) C/W 04SEPT 14 AT 7922.0 ACFT. HRS.

04-Sep-2014 1


anthony.s.speigner

USAACEMEC F189704, LEFT UPPER CARGO DOORTRACK LOWER FLANGE CRACKED.Authorization granted to repair as follows: 1.Stop drill crack. 2. Fabricate doubler out of.025" stainless steel per print in process control5722. 3. Install wet using 9309.3NA and pickingup existing fasteners. 7950.5 ACFT HRS.

18-Sep-2014 1


dean.a.keirn

USAACEMEC F189733, RIGHT UPPER CARGO DOORTRACK CRACKED. Authorization granted torepair as follows:1. Stop drill crack. 2. Fabricatedoubler out of .025" stainless steel per print inprocess control 5722.3. Install wet using9309.3NA and picking up existing fasteners.7950.5 ACFT HRS.

18-Sep-2014 2


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 52 of 61

USAACEACFT OPERATING IAW AWR 1153, R8 DTD10OCT14, JP-8+100 FUEL, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

27-Oct-2014 1


dean.a.keirn

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-15-SOF-01 (OIL COOLER FAN AXIAL BEARING) @ 7962.4 ACFT HRS

28-Oct-2014 1


theresa.d.pollard

USAACEACFT OPERATING IAW AWR 1220, R9 DTD31OCT14, ESM, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.

03-Nov-2014 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1455, R5 DTD28OCT14, BATTELLE CAP, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

03-Nov-2014 2


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1153, R9 DTD05NOV14, JP-8+100 OR F-24+100 FUEL,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.

07-Nov-2014 1


dean.a.keirn

USAACECOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-19 LCF CHANGE 66 @ 7962.4

08-Nov-2014 1


vickie.l.meadows

USAACEH-60-15-ASAM-01 LED CAUTION ADVISORYPANEL REQUIREMENTS COMPLETED AT 7973ACFT HRS.

21-Nov-2014 1


olivia.d.williams

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-15-ASAM-01(LED CAUTION ADVISORY PANEL) AT 7972.7 ACFT HRS

21-Nov-2014 2


theresa.d.pollard

USAACEACFT OPERATING IAW AWR 1251, R10 DTD26NOV14, EYEBOLTS, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

25-Nov-2014 1


theresa.d.pollard

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-15-AMAM-05 ( AHRS EMERGENCYPROCEDURES) @ 8010.1 ACFT HRS

12-Dec-2014 1


theresa.d.pollard

USAACEH-60-15-AMAM-05 AHR EMERGENCEYPROCEDURES REQUIREMENTS COMPLETEDAT 8353.6

12-Dec-2014 2


olivia.d.williams

USAACEDELAYED ENTRY: ACFT OPERATING UNDERMEO A6116 INSTALLATION OF FUEL FLAG FORE/UH-60 FLEET @ FT RUCKER, AL ACFTCURRENT HRS 8054.3

26-Jan-2015 1


theresa.d.pollard

USAACEACFT OPERATING IAW AWR 1738, R2 DTD23JAN15, AN/APX-118 CXP, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR AND ISAQ 116.

04-Feb-2015 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1220, R10 DTD26JAN15, ESM, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.

11-Feb-2015 1


dean.a.keirn

USAACECOMPILED WITH THE REQUIRMENTS OF ( H-60-15-AMAM-06) IDENTIFICATION OF AVIATIONSERVIVABILITY EQUIPMENT AT 8082.8 ACFTHRS (CMWS MWO NOT INSTALLED, NOTAPPLIABLE ( AFS 765)

13-Feb-2015 1


theresa.d.pollard


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 53 of 61

USAACEACFT IS NO LONGER OPERATING IAW AWR1514, ALL VERSIONS. ACFT IS OPERATING IAWAWR 1753, R5 DTD 30JAN15, DGNS AN/ASN-128B/D, SUPERSEDING ALL PRIOR VERSIONSOF THIS AWR AND AWR'S 1467, 1292 AND 1514.

19-Feb-2015 1


dean.a.keirn

USAACEH-60-15-AMAM-06 IDENTIFICATION OFAVIATION SURVIVAILITY EQUIPMENT C/W 13FEB 2015.

27-Feb-2015 1


anthony.s.speigner

USAACEACFT OPERATING IAW AWR 1965, R0 DTD08OCT14, APPLE IPAD DEVICES.

04-Mar-2015 1


dean.a.keirn

USAACETEST STARTER SN 03 REMOVED THIS DATE AT8112 ACFT HRS WITH 1199 TTSN. ACFTCONTINUES TO OPERATE IAW AWR 1841 (SEEPRIOR ENTRY FOR DETAILS), TEST STARTERSN 02 INSTALLED THIS DATE WITH 961 TTSN.

18-Mar-2015 1


dean.a.keirn

USAACE24-MAR-15- TRANSMISSION S/N A26501113IMPENDING BYPASS BUTTON POPPED;REPLACED FILTER BUTTON AND 1ST ANDSECOND STAGE FILTERS. IAW EM 0013 WP0626 00 W/TSN 7017

24-Mar-2015 1


theresa.d.pollard

USAACEACFT OPERATING IAW AWR 1750, R3 DTD31MAR15, AN/AVS-6 NVG, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR AND THEAMSRD-AMR-AE-T AWR DTD 26JUN06.

09-Apr-2015 1


dean.a.keirn

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-15-ASAM-03 TROOP/GUNNER SEAT ENGERYATTENUATORS, NOT INSTALLED (AFS 765) @8151.1 ACFT HRS

13-Apr-2015 1


theresa.d.pollard

USAACECOMPLIED WITH REQUIREMENTS OF H-60-15-ASAM-03 TROOP/GUNNER SEAT ENERGYATTENUATORS. NOT APPLICABLE BY MDS @8151.1 AFS 765

13-Apr-2015 2


vickie.l.meadows

USAACEGEN-12-AMAM-07 ACFT FIRST AID KITMODERNIZATION @ 8170.7 ACFT HRS

27-Apr-2015 1


theresa.d.pollard

USAACECOMPLIED WITH H-60-15-AMAM-11( MODE-STRANSPONDER ADDRESS REVIEW) @ 8197.3ACFT HRS

09-May-2015 1


theresa.d.pollard

COMPLIED WITH THE REQUIREMENTS OF H-60-15-AMAM-10 ( AV-DEC GASKET INSPECTION)@8191.0 ACFT HRS

12-May-2015 1


COMPLIED WITH THE REQUIREMENTS OF H-60-15-AMAM-10 ( AV-DEC GASKET INSPECTION)@8191.0 ACFT HRS

12-May-2015 2


USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-15-AMAM-10 ( AV-DEC GASKET INSPECTION)@8191.0 ACFT HRS

12-May-2015 3


theresa.d.pollard


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 54 of 61

USAACEACFT OPERATING IAW AWR 1505, R7 DTD13MAY15, 5M HYD FILTERS, SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR.

13-May-2015 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1251, R11 DTD27MAY15, EYEBOLTS ON BIFILAR,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.

28-May-2015 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1681, R5 DTD22JUN15, EH DE-MOD, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR AND AWR'S927 AND 890.

23-Jun-2015 1


dean.a.keirn

DCR RASM-COCM/ACE PERFORMED AT 8199.8 ACFT. HRS.BY TEAM MEMBER UU AMCOM RASM-C.

01-Jul-2015 1

FT. CAMPBELL, KY42223

MO09565

USAACEMEC F300442, 8199.8 ACFT HRS,AUTHORIZATION GRANTED TO REPAIR 2DEBONDS OF APPROX 4 X 8 AND 4 X 4 INCHESIN THE RH APU DOOR PANEL.

22-Jul-2015 1


dean.a.keirn

USAACEH-60-15-AMAM-14 LEGITIMATE CODE FILE(LCF) CHANGE 67 REQUIREMENTS C/W AT8199.8

25-Jul-2015 1


olivia.d.williams

USAACEACFT OPERATING IAW AWR 1738, R3 DTD17JUL15, AN/APX-118 CXP, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

28-Jul-2015 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1841, R4 DTD29JAN15, STARTER PN 3505300-10,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.

31-Jul-2015 1


dean.a.keirn

USAACEMAIN ROTOR RIGGING CHECK COMPLETEDAT 8199.8 ACFT HRS.CONTROL POSITION:LOWCOLL ANGLE90 DEG R 180 DEG FWD 270DEG L 0 DEG AFT TOTAL DEG AVGDEG COLL. RANGE 9.3 -2.6-10.7 1.2 -2.8 -0.7HIGH COLL ANGLE:90 DEG R 180 DEGFWD 270 DEG L 0 DEG AFT TOTALDEG AVG DEG COLL. RANGE 19.910.7 10.8 19.1 60.515.125 15.825FWD CYCLIC ANGLE:90DEG R 180 DEG FWD 270 DEG L 0 DEGAFT TOTAL DEG AVG DEG COLL.RANGE -2.1 31.033.1AFT CYCLE ANGLE:90 DEG R 180 DEGFWD 270 DEG L 0 DEG AFT TOTALDEG AVG DEG COLL. RANGE 24.75.7 19.0LEFT CYCLEANGLE:90 DEG R 180 DEG FWD 270 DEGL 0 DEG AFT TOTAL DEG AVG DEGCOLL. RANGE -8.27.0 15.2RIGHT CYCLIC ANGLE:90DEG R 180 DEG FWD 270 DEG L 0 DEGAFT TOTAL DEG AVG DEG COLL.RANGE 7.5-8.0 15.5

10-Aug-2015 1


christina.l.negron


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 55 of 61

USAACEMAIN ROTOR RIGGING CHECK COMPLETEDAT 8199.8 ACFT HRS. PRIMARY SERVOCONTROL ROD BIAS: FWD: 1 1/2 OUT, AFT: 11/2 IN, LAT: 1 FLAT OUT.

10-Aug-2015 2


christina.l.negron

USAACETAIL ROTOR CABLE TENSION CHECKCOMPLETED AT 8199.8 ACFT HRS, IAW H-60-15-AMAM-03, LEFT CABLE162 LBS RIGHT 164LBS @ 27.3 DEGREES CELCIUSTHERMOMETER MR# 118177 TENSIONMETERMR# 126115 (CHECKED AT 5/32)

11-Aug-2015 1


christina.l.negron

USAACETAIL ROTOR BIAS CHECK COMPLETED AT8199.8 ACFT HRS. COLOR DIM ADIM B DIFFERENCE 1ST DEG2ND DEG FINAL DEGREERED4.79 5.09 0.30 0.03.0 3.0BLACK 4.064.37 0.31 0.0 3.03.0YELLOW 4.79 5.090.30 0.0 3.03.0 BLUE 4.06 4.380.32 0 .0 3.03.0

11-Aug-2015 2


christina.l.negron

USAACE720 HOUR PHASE # 13, WAS COMPLETED AT8199.8 ACFT HRS. THE NEXT 720 HOURPHASE (#14) IS DUE AT 8919.8 ACFT HRS.

13-Aug-2015 1


christina.l.negron

USAACEMAIN ROTOR RIGGING CHECK COMPLETEDAT 8199.8 ACFT HRS.CONTROL POSITION:LOWCOLL ANGLE90 DEG R 180 DEG FWD 270DEG L 0 DEG AFT TOTAL DEG AVGDEG COLL. RANGE 9.4 -1.4-11.6 0.1 -3.5 -0.875HIGH COLL ANGLE:90 DEG R 180 DEGFWD 270 DEG L 0 DEG AFT TOTALDEG AVG DEG COLL. RANGE 19.811.5 9.2 18.0 58.514.625 15.5FWD CYCLIC ANGLE:90 DEGR 180 DEG FWD 270 DEG L 0 DEG AFTTOTAL DEG AVG DEG COLL. RANGE -2.7 30.433.1AFT CYCLE ANGLE:90 DEG R 180 DEGFWD 270 DEG L 0 DEG AFT TOTALDEG AVG DEG COLL. RANGE 24.24.8 19.4LEFT CYCLEANGLE:90 DEG R 180 DEG FWD 270 DEGL 0 DEG AFT TOTAL DEG AVG DEGCOLL. RANGE -9.16.1 15.2RIGHT CYCLIC ANGLE:90DEG R 180 DEG FWD 270 DEG L 0 DEGAFT TOTAL DEG AVG DEG COLL.RANGE 6.3-8.0 14.3

14-Aug-2015 1


christina.l.negron

USAACEMAIN ROTOR RIGGING CHECK COMPLETEDAT 8199.8 ACFT HRS. PRIMARY SERVOCONTROL ROD BIAS: FWD: 2 1/2 FLATS OUT,AFT: 2 1/2 FLATS IN, LAT: 2 FLATS OUT.

14-Aug-2015 2


christina.l.negron


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 56 of 61

USAACEMEC F301955, 8199.8 ACFT HRS,AUTHORIZATION GRANTED TO REPAIR THECP CYCLIC STICK YOKE HOUSING PER DMWR1-1680-323 DTD 30 DEC 2011, PARAGRAPH 3-12 BY REMOVING MINIMAL MATERIAL NOT TOEXCEED EXISTING DEPTH.

18-Aug-2015 1


dean.a.keirn

USAACEMEC F302302, 8199.8 ACFT HRS.AUTHORIZATION GRANTED FOR CCAD TOREPLACE THE LH FLOOR SUPPORT TEEANGLE IAW DMWR 1-1520-237.

25-Aug-2015 1


dean.a.keirn

USAACETHIS ACFT NO LONGER OPERATING IAW AWR1251 (BILFILAR EYEBOLTS) AT 8203.1 ACFTHRS.

04-Sep-2015 1


christina.l.negron

USAACECOMPLIED WITH THE REQUIEMENTS OF H-60-15-AMAM-18, MEDEVAC CAROUSEL @ 8243.5ACFT HRS

29-Sep-2015 1


theresa.d.pollard

USAACEACFT OPERATING IAW AWR 1965 R1(OPERATION OF APPLE IPAD DEVICES ON USARMY UH/HH-60A/L/M HELICOPTERS) DTD 16SEP 15

14-Oct-2015 1


theresa.d.pollard

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-16-AMAM-01 (EIBF FRAMES) @ 8310.0 ACFTHRS

28-Oct-2015 1


theresa.d.pollard

USAACEACFT NO LONGER OPERATING IAW AWR 1841,ALL REVISIONS, TEST STARTER SN 02REMOVED THIS DATE AT 8321 ACFT HRS WITH1169 TTSN.

02-Nov-2015 1


dean.a.keirn

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-16-ASAM-01 (INBOARD RETENTION PLATETORQUE CHECKS) @ 8335.3 ACFT HRS

11-Nov-2015 1


theresa.d.pollard

USAACEACFT OPERATING IAW AWR 1738, R4 DATED28DEC15 (AN/APX-118 CXP). SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR AND ISAQ116.

05-Jan-2016 1


chelsey.p.phillips

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-16-ASAM-02, DEFECTIVE FUEL HOSES

08-Jan-2016 1


theresa.d.pollard

USAACEACFT OPERATING IAW AWR 1800, R4 DTD05JAN16, SINGLE EDM AND/OR BFT,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR AND AWR'S 1284, 1347, 1414 AND 1639.

08-Jan-2016 2


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 57 of 61

USAACEMR RIG CHECK COMPLTED 28 HJAN. 16 . LOWCOLL ANGLE: 90* RIGHT 4.7/180*FWD -1.5/270*LEFT -10.5/ 0 *AFT 3.3 TOTAL -4 AVG* -1TOLERANCE: -1.3 TO 0.0 (BLADES ON) +1.0 TO0.0 ( BLADES OFF) HIGH COLL ANGLE- 908RIGHT 20.1 180* FWD 11.4/270*LEFT 9.5 0 AFT18.5/ TOATAL 59.5 TOLERANCE 15.5 MINIMUMRANGE ( SEE NOT E) FWD CYCLIC HIGH COLL/90* RIGHT -2.2 / 270* LEFT 30.8/ TOTAL 33-TOLERANCE - DIFFEERENCE BETWEEN 270 *& 90 * POSITIONS +33.0 MIN.. AFT CYCLEANGLE / 90 R- 25/ 270* LEFT 4.8, TOTAL 20.2DIFFERNCE BETWEEN 90* & 270 POSITIONSNOT LESS THAN +19 LEFT ANGLE / 180* FWD -8.3 0 AFT 6.7 T9OTAL 15 SUM OF 180* & 0POSITION TO BE 15 TO 17 " RIGHT ANGLE ..180FWD 6.7 0 AFT -8.7 TOTAL 15.4 - SUM OF160" & 0 POSITION TO BE 14 TO 16"

28-Jan-2016 1


theresa.d.pollard

USAACEACFT NO LONGER OPERATING UNDER AWR1251, ALL VERSIONS. AWR WAS ALLOWED TOTERMINATE ON 31JAN16 AND EYEBOLTS AREBEING REMOVED.

02-Feb-2016 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1913, R2 DTD12FEB16, ACN LOGBOOK, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

17-Feb-2016 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1681, R6 DTD13APR16, EH60A DEMOD, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR AND AWR'S927 AND 890.

13-Apr-2016 1


dean.a.keirn

LOCKHEED MARTINRASM-C

OCM/ACE PERFORMED AT 8560.2 AIRCRAFTHOURS BY TEAM MEMBERS P AND R

19-Apr-2016 1


jacob.a.weikart

USAACEMEC F311566, 8560.2 ACFT HRS.AUTHORIZATION GRANTED FOR CCAD DFT ATFORT RUCKER , AL TO REPLACE 34.5CHANNEL IAW AJMBL34-1C

20-Apr-2016 1


theresa.d.pollard

USAACEACFT OPERATING WITIN LIMITAIONS ANDRESTRICTIONS SPECIFIED IN AWR 1800 R5,DTD 27 APR 16. SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.

13-May-2016 1


theresa.d.pollard

USAACEACFT OPERATING IAW AWR 1444, R8 DTD25MAY16, SINGLE AHRS, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

01-Jun-2016 1


dean.a.keirn

USAACEACFT NO LONGER OPERATING IAW AWR 1505,ALL VERSIONS. SAMPLING VALVE NOTINSTALLED AND 5M FILTERS PN 7596335-101,NSN 4330-01-601-1254 ARE NOW STANDARDH60 IETM EQUIPMENT.

02-Jun-2016 1


dean.a.keirn

USAACECOMPLIED WITH THE REQUIREMENTS OF GEN-16-AMAM-04, TRNSPONDER BATTERYREPLACEMENT, NOT INSTALLED ON THISAIRCRAFT @ 8612.5 ACFT HRS

04-Jun-2016 1


theresa.d.pollard


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 58 of 61

USACEENTRY ENTERED IN ERROR DTD 04 JUN 2016,GEN-16-AMAM-04, TRANSPONDER BATTERYREPLACEMENT

04-Jun-2016 2


theresa.d.pollard

USAACE04 JUN 2016 -COMPLIED WITH THEREQUIREMENTS OF GEN-16-AMAM-04,TRANSPONDER BATTERY REPLACEMENT,NOT INSTALLED ON THIS ACFT AT 8560.2ACFT HRS

07-Jun-2016 1


theresa.d.pollard

USAACEACFT OPERATING IAW AWR 1515, R4 DTD17MAY16, TRC MEMS GYROSCOPES,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR AND ISAQ 126.

08-Jun-2016 1


dean.a.keirn

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-15-ASAM-07 ( MAIN ROTOR BLADEDEBONDING AND TIP RIB CRACKING @ 8560.2ACFT HRS

15-Jun-2016 1


theresa.d.pollard

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-16-SOF-01, UPPER CABIN FRAME CRACKING@ 8560.2 ACFT HRS

21-Jun-2016 1


theresa.d.pollard

USAACECOMPLIED WITH THE REQUIREMENTS H-60-16-AMAM-09 COMPONENTS DUPLICATION @8561.6 ACFT HRS

23-Jun-2016 1


theresa.d.pollard

USAACEMEC F315604, 8625.1 ACFT HRS, XMSN SNA265-01482 WITH TSN 3400 (TSO 425). DURINGHOVER MAIN TRANSMISSION OIL PRESSUREFLUCTUATES FROM 25 TO 50 PSI. PRESSUREIS 50 PSI ON LEVEL GROUND FLAT PITCH.FLUCTUATION VERIFIED WITH A DIRECTREADING GAGE TO ELIMINATE POSSIBLEINDICATION FAULTS. REQUESTAUTHORIZATION TO COMPLETEPROCEDURES IN BLACKHAWK NEWSLETTER, ISSUE 44 MAY/JUNE 2000. THEAVIATION ENGINEERING DIRECTORATE (AED)HAS REVIEWED THE SUBJECT REQUESTFROM AN AIRWORTHINESS ANDENGINEERING PERSPECTIVE AND APPROVESTHE REQUEST. ENSURE THE OIL DIPSTICK ISRE-MARKED TO IDENTIFY THE CORRECT OILLEVEL WITH THE ADDITIONAL QUARTS.ANNOTATE THE MODIFIED DIPSTICK AND THEAMOUNT OF ADDITIONAL QUARTS OF OILREQUIRED ON THE APPROPRIATE AIRCRAFTHISTORICAL RECORD. 03AUG16: 3 QUARTSADDED.

01-Aug-2016 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1153, R10 DTD25JUL16, JP-8 +100 OR F-24 +100 FUEL,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.

09-Aug-2016 1


dean.a.keirn

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-SOF-02, RESCUE HOIST OPERATIONALRESTRICTIONS HOIST NOT INSTALLED

15-Aug-2016 1


theresa.d.pollard


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 59 of 61

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-16-ASAM-06, IMPROVED TAIL ROTORQUADRANT SUPPORT. ( FAILED) @ 8663.2ACFT HRS

23-Aug-2016 1


theresa.d.pollard

USAACECOMPLY WITH REQUIREMENTS OF H-60-16-AMAM-10, ULLS-A(E)

01-Sep-2016 1


theresa.d.pollard

USAACEACFT OPERATING IAW AWR 1800, R6 DTD12AUG16, EDM AND/OR BFT, SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR ANDAWR'S 1284, 1347, 1414 AND 1639.

23-Sep-2016 1


dean.a.keirn

USAACEMEC F315604A, 8625.1 ACFT HRS, XMSN SNA265-01482, TSN 3400, AUTHORIZATIONGRANTED TO PERFORM THE TROUBLESHOOTING PROCEDURES IAW MAIN XMSN -NEWSLETTER ARTICLE (ATTACHED). ONCETROUBLE SHOOTING PROCEDURES HAVEBEEN COMPLETED, REPORT FINDINGS TOTHE UNDERSIGNED.

30-Sep-2016 1


dean.a.keirn

USAACEMEC F315604B, 8625.1 ACFT HRS, XMSN SNA265-01482, TSN 3400, AUTHORIZATIONGRANTED TO ADD ADDITIONAL QUART OFOIL, FOR A TOTAL OF 3 QUARTS. CONTINUEWITH TROUBLESHOOTING PROCEDURESTEPS AFTER ADDITION OF OIL.

06-Oct-2016 1


dean.a.keirn

USAACEMEC F315604C, 8625.1 ACFT HRS, XMSN SNA265-01482, TSN 3400, CORRECTION:FLUCTUATION STOPPED WITH THE ADDITIONOF 2 QUARTS OF OIL OVER THE FULL MARKAFTER THE ADDENDUM ATROUBLESHOOTING EFFORT. 1.AUTHORIZATION GRANTED TO ADD THE TWOQUARTS OF ADDITIONAL OIL. 2. OPERATETHE AIRCRAFT FOR A MINIMUM OF FIVEADDITIONAL FLIGHTS TO INSURE THE OILPRESSURE DOES NOT FLUCTUATE AND THEOIL SERVICE LEVEL REMAINS CONSTANT. 3.REMARK THE MAIN TRANSMISSION DIPSTICK.CHECK THE SERVICE LEVEL AFTEREACH OFTHE FIVE FLIGHTS TO IDENTIFY THE "NEW"NORMAL OIL SERVICING LEVEL. 4. ADD AWRITE UP TO THE AIRCRAFT LOG BOOKSTATING THAT THE OIL DIPSTICK HAS BEENMODIFIED TO IDENTIFY THE CORRECT OILLEVEL FOR THAT MAIN TRANSMISSION. BESURE TO ANNOTATE THE MAINTRANSMISSION PART AND SERIAL NUMBER INTHE LOG BOOK ENTRY.

07-Oct-2016 1


dean.a.keirn

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-17-ASAM-01, UULS-AE CADS

07-Oct-2016 2


theresa.d.pollard

USAACEACFT OPERATING IAW AWR 1965, R2 DTD07OCT16, PORTABLE ELECTRONIC DEVICES,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR AND AWR 1914.

11-Oct-2016 1


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 60 of 61

USAACEACFT OPERATING IAW AWR 1455, R6 DTD14OCT16, BATTELLE CAP, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR AND ISAQ 123.

26-Oct-2016 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1753, R6 DTD14OCT16, DGNS AN/ASN-128B/D,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR AND AWR'S 1292, 1467, AND 1514.

26-Oct-2016 2


joanna.n.lucier

USAACEACFT OPERATING IAW AWR 1965, R3 DTD19OCT16, PORTABLE ELECTRONIC DEVICES,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR AND AWR 1914.

27-Oct-2016 1


dean.a.keirn

USAACEACFT NOW OPERATING IAW AWR 1693, R3DTD 28JAN16, RESA.

28-Oct-2016 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1220, R11 DTD31OCT16, ESM, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.

01-Nov-2016 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 2064, R0 DTD09DEC16, COBRA MICROPHONE.

12-Dec-2016 1


dean.a.keirn

USAACECOMPLIED WITH THE REQUIREMENT OF H-60-17-SOF-01, RESCUE HOIST EMERGENCYPROCEDURES @ 8801.4 ACFT HRS

20-Dec-2016 1


theresa.d.pollard

USAACEOMPLIED WITH THE REQUIREMENTS H-60-17-AMAM-01, ULLS-A (E) LCF CHANGE 68

20-Dec-2016 2


theresa.d.pollard

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-17-ASAM-04, AIRFRAME STRUCTURALPARTS

10-Jan-2017 1


theresa.d.pollard

USAACECOMPLIED WITH H-60-17-ASAM-05 MAINROTOR BLADE QUALITY ESCAPEMENT AT8838.8 AC HOURS.(KATY DAVIS)

23-Feb-2017 1


theresa.d.pollard

USAACEACFT OPERATING IAW AWR 1738, R5 DTD24FEB2017, AN/APX-118/118A CXP.

08-Mar-2017 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1965, R4 DTD15MAR17, TABLETS ON US ARMY UH/HH-60HELICOPTERS, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.

22-Mar-2017 1


dean.a.keirn

USAACECOMPLIED WITH H-60-17-AMAM-07, EXTERNALMOUNTED RESCUE HOIST (EMRH) ARMADAPTOR CORROSION CONTROL,COMPLETED AT ACFT HOURS 8866.6

24-Mar-2017 1


theresa.d.pollard

USAACEACFT OPERATING IAW AWR 1800, R7 DTD23MAR17, SINGLE EDM AND/OR BFT,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR AND AWR'S 1284, 1347, 1414 AND 1639.

03-Apr-2017 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1750, R4 DTD29MAR17, AN/AVS-6 NVG, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

04-Apr-2017 1


thomas.e.mitchell


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 61 of 61

USAACEACFT OPERATING IAW AWR 1681, R7 DTD17APR17, EH DE-MOD, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR AND AWR'S927 AND 890.

24-Apr-2017 1


dean.a.keirn

USAACEACFT BEING TRANSFERRED TO BESTPROGRAM, HUNTSVILLE, AL. AT 8875.6 ACFTHRS.

25-Apr-2017 1


katy.t.davis

SESIACFT TRANSFERED TO BEST PROGRAM ONTHIS DATE @ 8875.6 ACFT HRS FROM USAACEFT. RUCKER, AL. DATA PLATE INSTALLED

28-Apr-2017 1

HUNTSVILLE

michael.t.wood

SESIH-60-16-AMAM-07 NOT COMPLIED WITH 01-May-2017 1

HUNTSVILLE

michael.t.wood

SESIH-60-17-ASAM-07 NOT COMPLIED WITH 01-May-2017 2

HUNTSVILLE

michael.t.wood

SESIH-60-17-SOF-04 NOT COMPLIED WITH 16-Jun-2017 1

HUNTSVILLE

james.m.aldrich


DATE AC HRS SHAFT VERTICAL REASON FOR VIBRATION CHECKLONGITUDINALLATERALIPS READINGS4.

8524475HELICOPTER, UTILITYEH-60A

3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL

Page 1 of 10

a b c d e f g

100 HOUT CHECK26-Jul-1991 OIL COOLER 0.130.210.001,348.4

PMSII COMPLETION03-May-1996 L/H ENG 0.000.000.29946.0

PMS II COMPLETION03-May-1996 R/H ENG 0.000.000.09946.0

REMOVAL & REINSTALLATION30-Oct-1996 OIL COOLER 0.080.000.16995.0

100 HR INSPECTION12-Aug-1997 L/H ENG 0.000.000.451,046.9

100 HR INSPECTION12-Aug-1997 R/H ENG 0.000.000.291,046.9

100 HR INSPECTION21-Aug-1997 L/H ENG 0.000.000.731,144.7

100 HR INSPECTION21-Aug-1997 OIL COOLER 0.150.000.241,144.7

100 HR INSPECTION21-Aug-1997 R/H ENG 0.000.000.291,144.7

100 HR INSPECTION07-Jan-1999 L/H ENG 0.000.000.271,247.0

100 HR INSPECTION07-Jan-1999 R/H ENG 0.140.000.241,247.0

100 HOUR CHECK26-Jul-1999 L/H ENG 0.000.000.281,348.4

100 HOUR CHECK26-Jul-1999 R/H ENG 0.000.000.171,348.4

ENGINE INSTALLED11-Oct-2002 R/H ENG. 0.040.000.001,503.6

100 HR INSP TQ=3708-Nov-2002 L/H ENG 0.120.000.001,547.4

100 HR INSP08-Nov-2002 OIL COOLER 0.250.020.001,547.4

100 HR INSP TQ=3608-Nov-2002 R/H ENG. 0.210.000.001,547.4

100 HR INSP TQ=3611-Mar-2003 #1 ENG 0.120.000.001,640.3

100 HR INSP TQ=3311-Mar-2003 #2 ENG 0.270.000.001,640.3

100 HR INSP11-Mar-2003 OIL COOLER 0.200.440.001,640.3

VIB CK. DUE FOR SEC 1 T/R D/S05-Feb-2004 OIL COOLER 0.220.330.001,722.0

D/S VIBE CHECK DUE 38%05-Feb-2004 R/H ENG 0.090.000.001,722.0

D/S VIBE CHECK DUE 38%12-Feb-2004 L/H ENG 0.140.000.001,722.0

100 HR INSP TQ=3711-Mar-2004 L/H ENG 0.160.000.001,745.6

100 HR INSP11-Mar-2004 OIL COOLER 0.290.480.001,745.6

100 HR INSP TQ= 3611-Mar-2004 R/H ENG 0.160.000.001,745.6


DA FORM 2408-15-2, OCT 1991 AIRCRAFT VIBRATION RECORD




Page 2 of 10

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100 HR INSP TQ=3716-Apr-2004 L/H ENG 0.320.000.001,846.4

100 HR INSP16-Apr-2004 OIL COOLER 0.240.170.001,846.4

100 HR INSP TQ=3516-Apr-2004 R/H ENG 0.230.000.001,846.4

PHASE 4 INSP TQ=3520-Jul-2004 L/H #1 ENG 0.130.000.001,931.8

PHASE # 4 INSP20-Jul-2004 OIL COOLER 0.100.310.001,931.8

PHASE #4 INSP TQ=3320-Jul-2004 R/H #2 ENG 0.360.000.001,931.8

100 HR. INSP. TQ=3610-Sep-2004 L/H ENG 0.180.000.002,029.5

100 HR. INSP.10-Sep-2004 OIL COOLER 0.260.040.002,029.5

100 HR. INSP. NO TQ. LISTED10-Sep-2004 R/H ENG 0.170.000.002,029.5

100 HR. INSP. TQ=3714-Oct-2004 L/H ENG 0.240.000.002,136.0

100 HR. INSP.14-Oct-2004 OIL COOLER 0.140.310.002,136.0

100 HR. INSP. TQ=3514-Oct-2004 R/H ENG 0.150.000.002,136.0

120 HR. INSP. TQ=3601-Dec-2004 L/H ENG 0.240.000.002,255.0

120 HR. INSP.01-Dec-2004 OIL COOLER 0.080.330.002,255.0

120 HR. INSP. TQ=3501-Dec-2004 R/H ENG 0.080.000.002,255.0

REM. & REINST.17-Dec-2004 OIL COOLER 0.010.100.002,279.1

120 HR. INSP. TQ=3714-Feb-2005 L/H ENG 0.300.000.002,374.7

120 HR. INSP.14-Feb-2005 OIL COOLER 0.050.130.002,374.7

120 HR. INSP. TQ=3514-Feb-2005 R/H ENG 0.180.000.002,374.7

120 HR. INSP. TQ=3715-Apr-2005 L/H ENG 0.240.000.002,495.9

120 HR. INSP.15-Apr-2005 OIL COOLER 0.050.210.002,495.9

120 HR. INSP. TQ=3515-Apr-2005 R/H ENG 0.120.000.002,495.9

#1 ENG. CHANGE TQ=3609-May-2005 L/H ENG 0.260.000.002,567.0

700 HR PHASE #5 TQ=35%28-Jul-2005 L/H ENGINE 0.070.000.002,619.3

700 HR PHASE #528-Jul-2005 OIL COOLER 0.170.620.002,619.3

700 HR PHASE #5 TQ=35%28-Jul-2005 R/H ENGINE 0.100.000.002,619.3






Page 3 of 10

a b c d e f g

120 HR. INSP. TQ=3523-Nov-2005 L/H ENG 0.180.000.002,738.7

120 HR. INSP.23-Nov-2005 OIL COOLER 0.110.220.002,738.7

120 HR. INSP. TQ=3523-Nov-2005 R/H ENG 0.410.000.002,738.7

120 HR. INSP. TQ. NOT PROVIDED20-Jan-2006 L/H ENG 0.310.000.002,855.9

120 HR. INSP.20-Jan-2006 OIL COOLER 0.210.130.002,855.9

120 HR. INSP. TQ. NOT PROVIDED20-Jan-2006 R/H ENG 0.320.000.002,855.9

120 INSP TQ=3619-Feb-2006 L/H #1 ENG 0.450.000.002,972.3

120 INSP19-Feb-2006 OIL COOLER 0.460.210.002,972.3

120 INSP TQ=3619-Feb-2006 R/H #2 ENG 0.250.000.002,972.3

120 HR. INSP. TQ=3629-Mar-2006 L/H ENG. 0.440.000.003,091.6

120 HR. INSP.29-Mar-2006 OIL COOLER 0.220.260.003,091.6

120 HR. INSP. TQ=3529-Mar-2006 R/H ENG. 0.390.000.003,091.6

120 HR. INSP. TQ. NOT PROVIDED08-May-2006 L/H ENG. 0.020.000.003,215.8

120 HR. INSP.08-May-2006 OIL COOLER 0.230.260.003,215.8

120 HR. INSP. TQ. NOT PROVIDED08-May-2006 R/H ENG. 0.030.000.003,215.8

720 HR. PMI #6 TQ. NOT PROVIDED20-Sep-2006 L/H ENG 0.230.000.003,305.2

720 HR PMI #6 VERT. NOT PROVIDED20-Sep-2006 OIL COOLER 0.000.430.003,305.2

720 HR. PMI #6 TQ. NOT PROVIDED20-Sep-2006 R/H ENG 0.150.000.003,305.2

120 HR. INSP. TQ. NOT PROVIDED28-Nov-2006 #1 ENG 0.460.000.003,429.6

120 HR. INSP. TQ. NOT PROVIDED28-Nov-2006 #2 ENG 0.360.000.003,429.6

120 HR. INSP. TQ. NOT PROVIDED28-Nov-2006 OIL COOLER 0.000.170.003,429.6

120 HR. INSP. TQ. NOT PROVIDED25-Jan-2007 L/H ENG. 0.440.000.003,542.8

120 HR. INSP. TQ. NOT PROVIDED25-Jan-2007 OIL COOLER 0.000.320.003,542.8

120 HR. INSP. TQ. NOT PROVIDED25-Jan-2007 R/H ENG. 0.390.000.003,542.8

REM. & REINST. TQ.=3714-Feb-2007 R/H ENG. 0.240.000.003,546.7

120 HR. INSP. TQ. NOT PROVIDED28-Mar-2007 L/H ENG. 0.260.000.003,670.3






Page 4 of 10

a b c d e f g

120 HR. INSP. VERT. NOT PROVIDED28-Mar-2007 OIL COOLER 0.000.180.003,670.3

120 HR. INSP. TQ. NOT PROVIDED28-Mar-2007 R/H ENG. 0.040.000.003,670.3

REM. & REINSTL. TQ. NOT PROVIDED14-May-2007 L/H ENG. 0.090.000.003,777.8

REM. & REINSTL. TQ. NOT PROVIDED16-May-2007 R/H ENG. 0.240.000.003,777.8

120 HR. INSP. TQ=3424-May-2007 L/H ENG. 0.460.000.003,793.8

120 HR. INSP. VERT. NOT PROVIDED24-May-2007 OIL COOLER 0.000.320.003,793.8

120 HR. INSP. TQ=3424-May-2007 R/H ENG. 0.490.000.003,793.8

120 HR. INSP. TQ. NOT PROVIDED20-Aug-2007 L/H ENG. 0.440.000.003,913.5

120 HR. INSP. VERT. NOT PROVIDED20-Aug-2007 OIL COOLER 0.000.280.003,913.5

120 HR. INSP. TQ. NOT PROVIDED20-Aug-2007 R/H ENG. 0.230.000.003,913.5

720 PMI #7 TQ. NOT PROVIDED07-Nov-2007 #1 ENG. 0.260.000.004,001.2

720 PMI #7 TQ. NOT PROVIDED07-Nov-2007 #2 ENG. 0.220.000.004,001.2

720 PMI #7 VERT. NOT PROVIDED07-Nov-2007 OIL COOLER 0.000.350.004,001.2

BALANCE CHECK VERT. NOT PROVIDED07-Dec-2007 OIL COOLER 0.000.660.004,001.2

DRIVESHAFT BALANCE CHECK DUE 36 = TQ14-Feb-2008 #1 ENG 0.400.000.004,124.0

DRIVESHAFT BALANCE CHECK DUE 37 = TQ14-Feb-2008 #2 ENG 0.400.000.004,124.0

BALANCE CHECK TQ NOT PROVIDED14-Feb-2008 OIL COOLER 0.000.860.004,124.0

120 HR MTP TQ=37%23-Mar-2008 L/H ENG 0.410.000.004,247.6

120 HR MTP SECOND NUMBER NOT GVN23-Mar-2008 OIL COOLER 0.000.740.004,247.6

120 HR MTP TQ=37%23-Mar-2008 R/H ENG 0.410.000.004,247.6

120 HR MTP NO TQ PROVIDED09-May-2008 L/H ENG 0.390.000.004,359.3

120 HR MTP09-May-2008 OIL COOLER 0.000.730.004,359.3

120 HR MTP NO TQ PROVIDED09-May-2008 R/H ENG 0.370.000.004,359.3

VIBE CK COMPLETED22-May-2008 R/H ENG 0.370.000.004,359.3

120 HOUR MTP TQ= 34%09-Jul-2008 L/H #1 ENG 0.380.000.004,489.2

120 HR MTP09-Jul-2008 OIL COOLER 0.000.790.004,489.2






Page 5 of 10

a b c d e f g

120 HOUR MTP TQ= 33%09-Jul-2008 R/H #2 ENG 0.370.000.004,489.2

120 HOUR INSP22-Sep-2008 #1 ENG 0.360.000.004,602.7

120 HOUR INSP22-Sep-2008 #2 ENG 0.320.000.004,602.7

120 HR INSP22-Sep-2008 OIL COOLER 0.000.970.004,602.7

720 HR PHASE #8 - NO TQ NOTED10-Jan-2009 #1 ENG 0.310.000.004,712.3

720 HR PHASE #8 - NO TQ NOTED10-Jan-2009 #2 ENG 0.350.000.004,712.3

720 HR PHASE #810-Jan-2009 OIL COOLER 0.000.030.004,712.3

720 HR PAHSE #810-Jan-2009 TAIL ROTOR 0.000.000.084,712.3

RESHIMMING OF SEC I D/S- NO TQ NOTED.14-Jan-2009 OIL COOLER 0.000.620.004,712.8

T/R RIG24-Feb-2009 T/R BAL 0.080.000.004,733.6

T/R REINST. OF T/R BLADES26-Feb-2009 T/R BAL 0.080.000.004,742.5

REMOVAL AND REINSTALLATION14-Apr-2009 ENGINE #1 0.280.000.004,796.4

REMOVAL AND REINSTALLATION14-Apr-2009 ENGINE #2 0.280.000.004,796.4

REMOVAL AND REINSTALLATION OF OIL COOLER14-Apr-2009 OIL COOLER 0.000.060.004,796.4

ECU REPLACEMENT TQ = 6017-Apr-2009 ENGINE #1 0.280.000.004,797.2

ECU REPLACEMENT TQ = 6017-Apr-2009 ENGINE #2 0.280.000.004,797.2

ECU REPLACEMENT TQ = 6017-Apr-2009 OIL COOLER 0.000.060.004,797.2

ECU REPLACEMENT TQ = 6017-Apr-2009 TR 0.140.000.004,797.2

120 HR MTP MOC DUE03-May-2009 #1 ENGINE 0.380.000.004,836.3

120 HR MTP MOC DUE03-May-2009 #2 ENGINE 0.370.000.004,836.3

120 HR MTP MOC DUE03-May-2009 OIL COOLER 0.000.390.004,836.3

120 HOUR MTP MOC DUE TQ: 34%27-Jun-2009 #1 ENGINE 0.130.000.004,957.1

120 HOUR MTP MOC DUE- TQ: 33%27-Jun-2009 #2 ENGINE 0.420.000.004,957.1

120 HOUR MTP MOC DUE.27-Jun-2009 OIL COOLER 0.000.610.004,957.1

120 HR MTP MOC DUE NO TORQ GIVEN24-Aug-2009 #1 ENGINE 0.310.000.005,071.0

120 HR MTP MOC DUE NO TORQ. GIVEN24-Aug-2009 #2 ENGINE 0.140.000.005,071.0






Page 6 of 10

a b c d e f g

120 HR. MTP MOC DUE (F/A)24-Aug-2009 OIL COOLER 0.000.620.005,071.0

VIBE CK DUE FOR OIL COOLER RMVL21-Sep-2009 OIL COOLER 0.000.340.005,134.0

120 HR MTP MOC08-Oct-2009 ENG #1 0.310.000.005,195.7

120 HR MTP MOC08-Oct-2009 ENG #2 0.110.000.005,195.7

120 HR MTP MOC08-Oct-2009 OIL COOLER 0.000.050.005,195.7

120 HR. INSP24-Feb-2010 #1 L/H ENG 0.170.000.005,377.8

120 HR INSP24-Feb-2010 #2 R/H ENG 0.250.000.005,377.8

120 HR INSP24-Feb-2010 OIL COOLER 0.000.300.005,377.8

720 HR PHASE #9 TQ = 130 LBS25-Feb-2010 # 1 ENG 0.170.000.005,379.8

720 HR PHASE #9 TQ = 130 LBS25-Feb-2010 # 2 ENG 0.250.000.005,379.8

720 HR PHASE #925-Feb-2010 OIL COOLER 0.000.300.005,379.8

120 HR MTP MOC TQ 3523-Apr-2010 # 1 ENGINE 0.370.000.005,498.3

120 HR MTP MOC TQ 3623-Apr-2010 # 2 ENGINE 0.130.000.005,498.3

120 HR MTP MOC23-Apr-2010 OIL COOLER 0.000.520.005,498.3

120 HR MTP MOC TQ - 34 IN LB27-Jun-2010 # 1 ENGINE 0.430.000.005,619.6

120 HR MTP MOC TQ - 35 IN LB27-Jun-2010 # 2 ENGINE 0.310.000.005,619.6

120 HR MTP MOC TQ - N/A27-Jun-2010 OIL COOLER 0.000.800.005,619.6

REPLACED ECU ON # 2 ENG02-Jul-2010 # 2 ENGINE 0.340.000.005,634.6

REPLACED # 2 ENGINE18-Jul-2010 # 2 ENGINE 0.290.000.005,670.6

120 HR MTP MOC DUE03-Sep-2010 #1 ENGINE 0.290.000.005,731.1

120 HR MTP MOC DUE03-Sep-2010 #2 ENGINE 0.140.000.005,731.1

120 HR MTP MOC DUE03-Sep-2010 OIL COOLER 0.000.870.005,731.1

120 HR INSP18-Dec-2010 R/H ENG #2 0.130.000.005,448.3

120 HR INSP18-Dec-2010 OIL COOLER 0.000.500.005,848.3

120 HR INSP18-Dec-2010 L/H ENG #1 0.250.000.005,848.3

SHAFT BALANCE DUE TQ=3621-Mar-2011 R/R #2 ENG 0.140.000.005,953.6






Page 7 of 10

a b c d e f g

T/R BALANCE CK04-Apr-2011 T/R 0.000.020.005,971.6

T/R BALANCE05-Apr-2011 T/R 0.000.070.005,972.1

T/R BALANCE06-Apr-2011 T/R 0.000.190.005,972.5

T/R BALANCE TQ TO 90-100" LBS12-Apr-2011 T/R 0.000.050.005,980.9

# 2 ENG RE-INSTALLED30-Apr-2011 #2 ENG 0.080.000.006,008.8

#1 ENG RE-INSTALLED30-Apr-2011 # 1 ENG 0.300.000.006,008.8

120 HR MTP MOC15-Jun-2011 #1 ENG 0.070.000.006,065.0

120 HR MTP MOC15-Jun-2011 #2 ENG 0.270.000.006,065.0

120 HR MTP MOC15-Jun-2011 OIL COOLER 0.000.510.006,065.0

120 HR MTP MOC15-Jun-2011 TAIL ROTOR 0.000.010.006,065.0

120 HR MTP MOC09-Aug-2011 ENG #1 0.240.000.006,188.2

120 HR MTP MOC09-Aug-2011 ENG # 2 0.410.000.006,188.2

120 HR MTP MOC09-Aug-2011 OIL COOLER 0.000.470.006,188.2

120 HR MTP MOC TQ 100"#S09-Aug-2011 T/R 0.000.090.006,188.2

REPL OF RED TR BOOT23-Aug-2011 T/R 0.000.080.006,231.2

FOR WT IN THREE QUADERANT12-Sep-2011 T/R 0.000.100.006,258.0

120 HR MTP MOC07-Oct-2011 ENG # 1 0.180.000.006,307.2

120 HR MTP MOC07-Oct-2011 ENG # 2 0.430.000.006,307.2

120 HR MTP MOC07-Oct-2011 OIL COOLER 0.000.480.006,307.2

120 HR MTP MOC07-Oct-2011 T/R 0.000.130.006,307.2

T/R BLADES OUT OF TRACK05-Dec-2011 T/R 0.000.070.006,410.5

120 HR MTP MOC21-Dec-2011 T/R 0.000.140.006,416.9

120 HR MTP MOC21-Dec-2011 ENG # 1 0.140.000.006,416.9

120 HR MTP MOC21-Dec-2011 ENG # 2 0.490.000.006,416.9

120 HR MTP MOC21-Dec-2011 OIL COOLER 0.000.460.006,416.9

120 HR MTP MOC08-Mar-2012 ENG # 1 0.190.000.006,541.2






Page 8 of 10

a b c d e f g

120 HR MTP MOC08-Mar-2012 ENG # 2 0.490.000.006,541.2

120 HR MTP MOC08-Mar-2012 OIL COOLER 0.000.030.006,541.2

120 HR MTP MOC08-Mar-2012 T/R 0.000.060.006,541.2

REPL T/R PADDLE DEICE CABLE ELEC CONNECT09-Mar-2012 T/R 0.000.160.006,544.9

120 HR MTP MOC15-Apr-2012 ENG # 1 0.190.000.006,661.2

120 HR MTP MOC15-Apr-2012 ENG # 2 0.480.000.006,661.2

120 HR MTP MOC15-Apr-2012 OIL COOLER 0.000.420.006,661.2

120 HR MTP MOC15-Apr-2012 T/R 0.000.090.006,661.2

TQ=35 POST PHASE16-Jul-2012 ENG #1 0.420.000.006,765.5

TQ=35 POST PHASE16-Jul-2012 ENG #2 0.320.000.006,765.5

POST PHASE16-Jul-2012 OIL COOLER 0.000.310.006,765.6

POST PHASE16-Jul-2012 T/R 0.000.020.006,765.6

#1 ENG REPLACEMENT16-Sep-2012 #1 ENG 0.190.000.006,877.4

120 HR MOC21-Sep-2012 T/R 0.000.100.006,885.0

120 HR MOC21-Sep-2012 OIL COOLER 0.000.370.006,885.0

120 HR MOC21-Sep-2012 #1 ENG 0.140.000.006,885.0

120 HR MOC21-Sep-2012 #2 ENG 0.390.000.006,885.0

REPL # 2 ENG07-Oct-2012 ENG # 2 0.300.000.006,929.7

ENG REPL20-Oct-2012 ENG # 2 0.160.000.006,952.0

120 MTP MOC10-Nov-2012 ENG # 1 0.070.000.007,007.0

120 MTP MOC10-Nov-2012 ENG # 2 0.100.000.007,007.0

120 MTP MOC10-Nov-2012 OIL COOLER 0.000.510.007,007.0

120 MTP MOC10-Nov-2012 T/R 0.000.060.007,007.0

REM & REINSTL09-Feb-2013 T/R 0.000.040.007,124.2

120 HR MTP MOC23-Feb-2013 ENG # 1 0.060.000.007,145.9

120 HR MTP MOC23-Feb-2013 ENG # 2 0.100.000.007,145.9






Page 9 of 10

a b c d e f g

120 HR MTP MOC23-Feb-2013 OIL COOLER 0.000.350.007,145.9

120 HR MTP MOC23-Feb-2013 T/R 0.000.110.007,145.9

120 HR INSP09-May-2013 #1 ENG 0.040.000.007,249.6

120 HR INSP09-May-2013 #2 ENG 0.090.000.007,249.6

120 HR INSP09-May-2013 OIL COOLER 0.000.380.007,249.6

120 HR INSP09-May-2013 T/R 0.000.070.007,249.6

DUE FOR REPLACING ZIP TIE11-May-2013 T/R 0.000.090.007,251.1

120 HR INSP17-Aug-2013 # 1 ENG 0.050.000.007,367.9

120 HOUR INSP17-Aug-2013 # 2 ENG 0.220.000.007,367.9

120 HOUR INSP17-Aug-2013 T/R 0.000.100.007,367.9

120 HOUR INSP17-Aug-2013 OIL COOLER 0.000.370.007,367.9

POST 720 HR PHASE #1210-Dec-2013 #1 ENG 0.370.000.007,481.6

POST 720 HR PHASE # 12.10-Dec-2013 #2 ENG 0.310.000.007,481.6

POST 720 HR PHASE #12.10-Dec-2013 OIL COOLER 0.440.000.007,481.6

POST 720 HR PHASE #1210-Dec-2013 T/R D/S 0.000.140.007,481.6

120 HR. INSP.08-May-2014 #1 ENG 0.190.000.007,724.1

120 HR. INSP.08-May-2014 #2 ENG 0.380.000.007,724.1

120 HR. INSP.08-May-2014 OIL COOLER 0.000.600.007,724.1

120 HR. INSP.08-May-2014 T/R 0.000.050.007,724.1

120 HR. INSP.02-Jul-2014 #1 ENG 0.220.000.007,845.2

120 HR. INSP.02-Jul-2014 #2 ENG 0.210.000.007,845.2

120 HR. INSP.02-Jul-2014 OIL COOLER 0.000.750.007,845.2

120 HR. INSP.02-Jul-2014 T/R 0.000.110.007,845.2

120 VIB CK09-Nov-2014 #1 ENG 0.200.000.007,962.4

120 VIB CK09-Nov-2014 #2 ENG 0.210.000.007,962.4

120 VIB CKS09-Nov-2014 T/R BAL 0.000.050.007,962.4






Page 10 of 10

a b c d e f g

120 HR VIBE CHECK09-Nov-2014 OIL COOLER 0.000.510.007,962.4

POST 720 HOUR PHASE26-Aug-2015 #1 ENG 0.080.000.008,201.6

POST 720 HOUR PHASE26-Aug-2015 #2 ENG 0.200.000.008,201.6

POST 720 HOUR PHASE26-Aug-2015 OIL COOLER 0.100.000.008,201.6

POST 720 HOUR PHASE26-Aug-2015 T/R D/S 0.000.060.008,201.6

120 HR MTF VIB CHECK19-Feb-2016 #1 ENG 0.380.000.008,446.8

120 HR MTF VIB CHECK19-Feb-2016 #2 ENG 0.400.000.008,446.8

120 HR MTF VIB CHECK19-Feb-2016 OIL COOLER 0.000.130.008,446.8

120 HR MTF VIB CHECK19-Feb-2016 T/R 0.000.080.008,446.8

120 VIB CHECK04-Jan-2017 1 ENG 0.270.000.008,801.4

04-Jan-2017 OIL COOLER 0.000.330.008,801.4

04-Jan-2017 T/R BLADE 0.000.000.008,808.1

120 VIB CHECK08-Jan-2017 2 ENG 0.450.000.008,801.4

5. REMARKS



(ACFT HRS)

ji kgfdcba

RMVL HRSRMVL HRSCOMPO/HNOMENWUC O/HLOCATIONNSN

AND he SINCELIFE

PREVSER NO.ANDNOMENCLATURE P/N TIMEINST HRS MENT DUEREPLACINST HRSNO.COMPONENT

NOMEN REPLACE -O/H ORCOMP6.

1520010820686HELICOPTER, UTILITY EH-60A 8524475 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Condition Change Components Page 1 of 4

COND COND

156001113021502C12D

00TAIL CONE FITTING B497-0036470219-05001-044 CCCC

COND COND

162001231183103A01

07481FWD FIXED GEAR SHOCK BEM214670250-12051-045 CCCC

COND COND

162001231183103A01

3528590FWD FIXED GEAR SHOCK BEM300170250-12051-045 CCCC

COND COND

162001421089003B01

18938200SHOCK ABSORBER (TAIL) K0020052570250-13101-044 CCCC

COND COND

165001285302405A01Z

14206009DAMPER ASSY, M/R A106-0094070106-08100-046 CCCC

COND COND

165001285302405A01Z

7435840DAMPER ASSY, M/R A1060063570106-08100-046 CCCC

COND COND

165001285302405A01Z

12147375DAMPER ASSY, M/R A1061127470106-08100-046 CCCC

COND COND

165001285302405A01Z

3478124DAMPER ASSY, M/R WG300580009070106-08100-046 CCCC

COND COND

161501199764605A03A

00SWASHPLATE ASSY A107-0108170104-08000-050 CCCC

COND COND

161501503311506A

68348876MAIN TRANSMISSION MODUL A2650132870351-08100-076 CCCC

COND COND

161501078571806A11

82878876ACCESSORY MODULE A258-0312470351-08080-043 CCCC

COND COND

161501383899206A11

72778876ACCESSORY MODULE A2580454070351-08080-045 CCCC

COND COND

161501074121906E

40158876INPUT MODULE A26400100D70351-08001-043 CCCC

COND COND

161501527817506E

7208876INPUT MODULE A2640879270351-08001-050 CCCC

COND COND

168001074515206F

00INTERMEDIATE GEARBOX A005-0125370357-06300-042 CCCC

COND COND

161501376508906G01

38235972TAIL ROTOR GEARBOX ASSY A0060106670358-06600-046 CCCC

COND COND

161501524780506H04

06762DRIVESHAFT ASSY ENGINE C845-0625870361-08014-041 CCCC

COND COND

161501524780506H04

1696417DRIVESHAFT ASSY ENGINE C8450758370361-08014-041 CCCC

COND COND

1615010812775 106H06

00SHAFT ASSY, T/R DRV SEC 1 A271-0102870361-03001-045 CCCC

COND COND

161501158951706H08

08200SHAFT ASSY, T/R DRV SEC 2 WG30059-0026770361-03009-047 CCCC

COND COND

1615011589522 506H09

00SHAFT ASSY, T/R SEC 3,4,5 A272-0328970361-05001-051 CCCC

APD LC v2.00EDITION MAY 1967 IS OBSOLETE For use of this form, see DA PAM 738-751; the proponet agency is DCSLOG

AIRCRAFT COMPONENT HISTORICAL RECORDDA FORM 2408-16, OCT 1991

(ACFT HRS)

ji kgfdcba


AND he SINCELIFE





COND COND

1615011589522 306H09

00SHAFT ASSY, T/R SEC 3,4,5 A2720319970361-05001-051 CCCC

COND COND

1615011589522 406H09

00SHAFT ASSY, T/R SEC 3,4,5 A2720329070361-05001-051 CCCC

COND COND

1615010832953 606H11

04001SHAFT ASSY, T/R DRV SEC 6 D55370361-05002-045 CCCC

COND COND

1615011585788 706H12

00SHAFT ASSY, T/R DRV SEC 7 A2740105570361-06002-047 CCCC

COND COND

432001207722807A01

03995PUMP MODULE ASSY, HYDR K5638ABR53023-06 CCCC

COND COND

432001207722807A01

42088876PUMP MODULE ASSY, HYDR W0H9AA11ABR53023-06 CCCC

COND COND

432001207722807A01

19168876PUMP MODULE ASSY, HYDR 241574ABR70652-02300-050 CCCC

COND COND

481001102247307B05A

06986VALVE, SOLENIOD 210363213850-3-1 CCCC

COND COND

481001102247307B05A

08772VALVE, SOLENIOD 213593213850-3-1 CCCC

COND COND

165001222431607B11

06762ACCUMULATOR 5790A70651-03201-105 CCCC

COND COND

1680012255633 PILOT08B20

01722PANEL INDICATOR (PDU) 514770450-01043-121 CCCC

COND COND

168001342049608B20

07135PANEL INDICATOR (PDU) 90470450-01043-124 CCCC

COND COND

611501114969609A01

14878876GENERATOR 5428B302-8-DM CCCC

COND COND

611501114969609A01

53748876GENERATOR 800800428B302-8-DM CCCC

COND COND

161501260074911C21

07706MIXER ASSEMBLY 43228370400-02300-046 CCCC

COND COND

168001261204411D25

17827481STABILATOR ACTUATOR B292-U075470400-06641-117 CCCC

COND COND

168001571757811D25

08772STABILATOR ACTUATOR 2055DL2155M31MOD1 CCCC

COND COND

299501496368615A04

03216ENGINE SEQUENCING UNIT 13814504587 CCCC

COND COND

599601188333219D01F

05840AMPLIFIER, RADIO FREQUEN 782622-6545-003 CCCC

COND COND

589501518878319E04B

1765840SDC - DOPPLER NAVIGATION 1806P320A002-03 CCCC

COND COND

584101245909119E05A

6658772RECEIVER-TRANSMITTER, R 2684JJA3060585 CCCC



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE





COND COND

584101245909319E05C

268394INDICATOR,HEIGHT 413FFA3060591 CCCC



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE




Time Change Components Page 1 of 3

20000 20000

156001081924402C15J

00TAIL PYLON FITTING B496-0003670209-06051-043 RCRC

5100 9871

161501450483405A01A

23537124HUB, M/R ROTOR ASSY 151520079770103-08112-047 RCRC

14000 21124

161501074515105A01L

07124MAIN ROTOR SHAFT EXTEND 2012135770351-08186-043 RCRC

13000 13000

161501127738805A01T

56715671BIFILAR, M/R ROTOR ASSY C3270002470107-08400-046 RCRC

12000 11567

161501083681206G01B

1356923O/B RETENTION PLATE (T/R) C257-0008970102-11101-042 RCRC

2520 10720

414001329342806H23

9768200FAN AXIAL 41252E15-1 01

13000 16982

156001129125607A24

42208202SAS ACTUATOR B1120226570410-02500-049 RCRC

13000 16813

156001129125607A24

03813SAS ACTUATOR C112-0401370410-02500-049 RCRC

13000 19764

156001129125607A24

10927856SAS ACTUATOR C1125198070410-02500-049 RCRC

2160 9988

161501141753211C23

22858876T/R PITCH CHANGE SHAFT 2330294270400-06100-042 10482

11000 19159

165001625043611C25

7178876SERVO ASSY, TAIL ROTOR C3000691270410-06520-048 RCRC

24400 30207

165001143122611D01

30698876SERVO, PRIMARY MAIN ROT B303-11137274000-1031 RCRC

24400 30453

165001143122611D01

28238876SERVO, PRIMARY MAIN ROT B303-1433270410-02820-054 RCRC

24400 30453

165001143122611D01

28238876SERVO, PRIMARY MAIN ROT B303-1442370410-02820-054 RCRC

13000 19172

156001158968511D04

27048876AFT BELLCRANK 345-0275870400-08102-045 RCRC

17000 17000

156001164416111D05

00AFT TIE ROD SUPT FITTING A391-0108870400-08112-045 RCRC

2200 10975

168001164416011D06

08775AFT TIE ROD ASSY MM0171970400-08111-042 RCRC

4400 11785

156001286887011D07

14918876AFT BELLCRANK SPT ASSY 390-0278770400-08117-049 RCRC

11000 19876

304001287243811D08

08876LATERAL SWASHPLATE LINK 15152-0507170400-08151-061 RCRC

11000 13985

168001221286311D09

58918876LATERAL SERVO BELLCRAN F3370084270400-08166-041 RCRC

11000 17191

168001158965311D11

26858876AFT WALKING BEAM E346-0082870400-08104-048 RCRC



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE




Time Change Components Page 2 of 3

4600 12756

156001289269711D13

7208876LEFT TIE ROD ASSY 3440270370400-08115-046 RCRC

3500 11069

156001296948611D14

13078876RIGHT TIE ROD ASSY 288-0144970400-08114-051 RCRC

15000 22867

168001158965211D15

10098876FORWARD BELLCRANK 199070400-08101-046 RCRC

5600 13467

156001221261911D16

10098876FWD BELLCRANK SPT ASSY B367-0641070400-08162-042 RCRC



COMPO/H OR REPLACE -

NOMENCOMPONENT NO. INST HRS

REPLAC MENT DUEINST HRS TIMEP/NNOMENCLATURE

AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND

NSN LOCATION O/HWUC NOMEN O/H COMPRMVL HRS RMVL HRS

a b c d f g ki j

Page 3 of 3Time Change Components

7. SIGNIFICANT HISTORICAL DATA

27-Jul-2004 1 27 JUL 04- 2401-16 INITIATED I/A/W UH-60-MIMI-04-006/007, CHANGE TO TRACKINGM/L/G STRUT, AFS009, JH5095, USAAVNC, FT. RUCKER, AL.

18-Nov-2010 2 LEFT TIE ROD S/N: E344-00492 MUST BE REMOVED FROM SERVICE IF REMOVEDPRIOR TO 140000 ACFT HRS OR 14 JUL 12. SC2006, R/SPEC, USAACE, FT.RUCKER, AL.

18-Nov-2010 3 NO DATE WUC: 06H18E PN: SB1138-101 PSN: B626-23239 BALL BRNG ANNVISCOUS, STA 410.5 INSTALLLED AT PHASE. (NO PID) (NO LOCATION)

27-Jul-2004 5 27 JUL 04- 2401-16 INITIATED I/A/W UH-60-MIM-04-006/007, CHANGE TO TRACKINGM/L/G STRUT, AFS009, JH5095, USAAVNC, FT. RUCKER, AL.

18-Nov-2010 6 WUC: 06H18E PN: SB1138-101 PSN: B626-23239 BALL BRNG ANN VISCOUS,STA 410.5 INSTALLLED AT PHASE.

APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991




AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 4 of 4Condition Change Components


27-Jul-2004 4 27 JUL 04- 2408-16 INITIATED I/A/W UH-60-MIM-04-006/007, CHANGE TO TRACKINGM/L/G STRUT, AFS009, JH5095, USAAVNC, FT. RUCKER, AL.

27-Jul-2004 7 WUC: 11C25 PN: 70410-06520-046 PSN: B300-01144 TAIL ROTOR SERVOASSY - REPLACED TAIL ROTOR SERVO AT PHASE. 27 JUL 04- 2408-16 INITIATEDI/A/W UH-60-MIM-04-006/007, CHANGE TO TRACKING M/L/G STRUT, AFS009,JH5095, USAAVNC, FT. RUCKER, AL.


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1620012311831FWD FIXED GEAR SHOCK 70250-12051-045 BEM2146 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

9000 16481

165001125090703A01A

00PISTON, MAIN L/GEAR STR BEM214670250-12067-102 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


05-Nov-2013 1 INSTALLED FWD FIXED GEAR SHOCK S/N: BEM2146, ON ACFT 8524475, AT 7481 ACFT HRS, WITH TSN: 0.

christina.l.negron USAACE FT RUCKER,AL.


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1620012311831FWD FIXED GEAR SHOCK 70250-12051-045 BEM3001 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

9000 17238

165001125090703A01A

00PISTON, MAIN L/GEAR STR BEM345170250-12067-102 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


15-May-2015 1 INSTALLED FWD FIXED GEAR SHOCK, BEM3001, ON ACFT 8724673 WITH TSN 0, ACFT HRS. 7268.

jimmy.s.caylor USAACE FT.RUCKER,AL.

19-Jul-2016 1 REMOVED FWD FIXED GEAR SHOCK, BEM3001, FROM ACFT 8724673,DUE TO CONTROLLED EXCHANGE,TSN 352, ACFT HRS. 7620.


19-Jul-2016 2 INSTALLED FWD FIXED GEAR SHOCK, BEM3001, ON ACFT 8524475 WITH TSN 352, ACFT HRS. 8590.



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011997646SWASHPLATE ASSY 70104-08000-050 A107-01081 05A03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

COND COND

161501087160205A03A01

60286028STATIONARY SWASHPLATE A222-0087270104-08010-044 CCCC

11000 11000

161501357508905A03A02

359359ROTATING SWASHPLATE A326-0090270104-08001-045 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE

PREVSER NO.ANDNOMENCLATURE P/N TIMEINST HRS

MENT DUEREPLACINST HRSNO.COMPONENT

NOMENREPLACE -

O/H ORCOMP6.

1615015033115MAIN TRANSMISSIONMODULE

70351-08100-076 A26501328 06A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 3

17000 22202

161501078571106A08

10614221SWASHPLATE GUIDE AER0023070351-08227-041 RCRC

3000 9263

161501110149106A13

04221HOUSING ASSY MGB F2110011370351-08110-045 RCRC

7600 13863

304001415838806A18

04221MAIN ROTOR SHAFT E2530450370351-08131-048 RCRC

12000 18263

161501497725706A19

04221PLANETARY CARRIER ASSY F2400027070351-08175-046 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 3


11-Sep-2009 1 11 SEP 09--OVERHAULED/RECAPPED IAW DMWR 1-1615-371 TSN: 4221, TSO: 0, MP3634, CCAD, CORPUSCHRISTI, TEXAS.

loletia.v.williams CCAD CORPUS CHRISTI, TEXAS.

08-Feb-2011 1 08-FEB-11 -MAIN TRANSMISSION FILTER BUTTON POPPED W/TSN 4560 AT 6013.9 ACFTHRS/LPERFORMED SERCEABILITY CHECK AND REPLACED BYPASS INDICATOR. TPOLLARD, 1634,USAACE, FT. RUCKER, AL

loletia.v.williams USAACE FT. RUCKER, AL

28-Jun-2011 1 MAIN MOD FILTER BUTTON POPPED(ACTION TAKEN: COMP SERVICEABILITY INSP RESET BUTTON,NOCONTAMINATION FOUND TM 1-1520-237-23-7 WP 626) ON (8724671 @ 6181 AIRCRAFT HOURS) MAIN MODWITH TSN: 4728 HOURS. (LW2720 R/SPEC)


14-Sep-2011 1 MAIN MOD FILTER BUTTON POPPED (ACTION TAKEN: COMPLETED SERVICEABILITY IAW IETM TM 1-1520-237-23-7 WP 062600. NO CONTAMINATION OR CHIPS FOUND. ) ON (8724672 @ 6325.3 AIRCRAFT) MAINMODULE SN: A26501328 TSN: 4872. (LW2720 R/SPEC)

loletia.v.williams USAACE FT. RUCKER,AL

03-Nov-2011 1 MAIN TRANSMISSION IMPENDING BYPASS INDICATOR WAS FOUND POPPED (ACTION TAKEN:REPLACED FILTER RESET INDICATOR BUTTON IAW WP065700) C/W @ 6380.3 AIRCRAFT HOURS. MAINTRANSMISSION 4927 MAIN MODULE HOURS. (LW2720 R/SPEC)


23-Nov-2011 1 MAIN MOD IMPLENDING BYPASS BUTTON POPPED ON THE MAIN MODUEL (ACTION TAKEN: RESETBUTTON AND REPLACED STAGE 1 AND 2 FILTERS IAW WP626) C/W @ 6417.7 AIRCRAFT HOURS. MAINMOD TSN: 4965 MAIN MOD HOURS.


29-Nov-2011 1 TRANSMISSION OIL FITER BUTTON FOUND EXTENDED DURING PREFLIGHT (ACTION TAKEN: MAINTRANSMISSION SERVICEABILITY INSPECTION COMPLETED IAW TM 1-1520-237-23-7 WP0626. RESETFILTER BUTTON, REPLACED FIRST STAGE FILTER) NO CHIPS/PARTICLES FOUND DURINGSCREEN/FILTER INSPECTIONS. MAIN MODULE TSN: 4967 MAIN MODULE HOURS ON (8724671 @ 6419.9AIRCRAFT HOURS) (LW2720 R/SPEC)


17-Feb-2012 1 MAIN MOD WITH TSN: 5099 FITLER BUTTON POPPED @ 6552 ACFT HRS. SERVICEABILITY INSPECTIONCOMPLETED NO CHIPS/PARTICLES FOUND ACTION TAKEN REPLACED FIRST STAGE FILTER ELEMENT.

donna.k.moss USAACE FT. RUCKER, AL

31-Mar-2012 1 MAIN MOD IMPENDING BYPASS BUTTON POPPED. FILTER REPLACED ON ACFT 8724671 @ 6631.3 ACFTHRS.

donna.k.moss USAACE FT. RUCKER, AL LOWE AHP

18-Apr-2012 1 XMSN OIL FILTER IMPENDING BYPASS BUTTON POPPED @ 6668.0 ACFT HRS. REPLACED FILTER ANDRESET BUTTON IAW TM 1-1520-237-23 WP 0626 00

mary.b.hodge USAACE FT. RUCKER, AL

27-Apr-2012 1 MAIN MOD IMPENDING BYPASS BUTTON POPPED REPLACED FILTER AND RESET BUTTON.

vickie.l.meadows USAACE FT RUCKER, AL





AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 3 of 3

23-Aug-2012 1 MAIN MODULE INPENDING BYPASS FOUND POPPED ON POSTFLIGHT. ACCEPTABLE FUZZ FOUND. COMPIAW WP0626. 6886.8 ACFT HRS.

jessica.n.kennedy USAACE FT. RUCKER, AL

21-Mar-2013 1 MAIN TRANSMISSION IMPENDING FILTER BUTTON EXTENDED, SERVICABILITY CHECK COMP IAW 1-1520-237-23-6 WP 626. COMPLETED AT 7075.9 ACFT HRS.


04-Jun-2013 1 MAIN MOD S/N A26501328 FILTER BUTTON POPPED AT 7222.6 ACFT HRS W/TSN 5770. PERFORMEDSERVICABILITY INSP IAW WP 0626 TM 1-1520-237-23 OK NO FAULTS NOTED RESET BUTTON

theresa.d.pollard USAACE FT. RUCKER, AL

07-Sep-2013 1 MAIN MOD FILTER BUTTON POPPED. REPLACED STAGE 1 AND 2 FILTER IAW TM 1-1520-237-23. NO CHIPSNOTED. ACFT HRS. 7432.8 ACFT HRS.


22-Nov-2013 1 COMPLIED WITH THE REQUIREMENTS OF H-60-13-AMAM-11 (MAIN TRANSMISSION FILTER BOWL) AT7536.5 ACFT HRS (REPLACED FILTER HOUSING BOLT WITH P/N 70351-48700-102).

felicia.tolver USAACE LOWE FT. RUCKER

14-Oct-2015 1 MAIN MOD (S/N A26501328) FILTER BUTTON POPPED (ACTION TAKEN : COMPLETED SERVICABILITYINSPECTION THROUGH STEP 2 NO CHIPS FOUND IAW EM 0013 WP626) @ TSN 6358.1 ACFT 8724671 ACFTHOURS 7811.1

stephanie.d.hall USAACE FT RUCKER AL

30-Mar-2016 1 MAIN MOD (S/N A26501328) FILTER BUTTON POPPED (ACTION TAKEN : SERVICEABILITY CHECKCOMPLETE IAW EM 0013 WP626) @ TSN 6499.7 ACFT 8724671 ACFT HOURS 7952.7


28-Jun-2016 1 MAIN MOD (S/N A26501328) FILTER BUTTON POPPED (ACTION TAKEN : SERVICEABILITY CHECKPERFORMED IAW TM 1-1520-237 23&P WP 626) @ TSN 6645.6 ACFT 8724671 ACFT HOURS 8098.6


24-Jan-2017 1 MAIN MOD SN A26501328 FILTER BUTTON POPPED @ 6827 TSN 8280 ACFT HRS SERVICEABILITY CHECKCOMP AND RESET FILTER BOWL BUTTON IAW EM 0013 WP 626 NO CHIPS NOTED


04-Apr-2017 1 REMOVED MAIN TRANSMISSION SN: A26501328, FROM ACFT 8724671, AT 8287 ACFT HRS, WITH TSN:6834. REMOVED FOR CONTROLLED EXCHANGE TO ACFT 8524475.

christina.l.negron USAACE FT. RUCKER,AL.

04-Apr-2017 2 INSTALLED MAIN TRANSMISSION SN: A26501328, ON ACFT 8524475, AT 8876 ACFT HRS, WITH TSN: 6834.

christina.l.negron USAACE FT. RUCKER,AL.


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615013765089TAIL ROTOR GEARBOX ASSY 70358-06600-046 A00601066 06G014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

12000 10553

161501074515306G01C

74193823I/B RETENTION PLATE T/R A2590057970358-06612-042 RCRC

5000 10972

304001292161706G01D

03823GEARSHAFT, BEVEL G3200013270358-06620-102 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


02-Apr-2011 1 T/R GEAR BOX INSTALLED ON ACFT 8524475 AT 5972 ACFT HRS WITH TTSN 3823.

olivia.d.williams USAACE FT RUCKER,AL


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



4140013293428FAN AXIAL 52E15-1 412 06H234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

2520 10720

311001127300506H23A

0976BEARING, AXIAL FAN 10995210SFFC3 RCRC

2520 10720

311001127300506H23A

0976BEARING, AXIAL FAN 11000210SFFC3 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


07-Apr-2015 1 RECAPPED IAW DMWR 1-4140-228. TSN: 976, O/H#1.

ET2508 CCAD CORPUS CHRISTI, TX

21-Jul-2015 1 INSTALLED FAN AXIAL, SN: 412, ON ACFT 8524475, AT 8200 ACFT HRS, WITH TSN: 976, 1 PRIOR O/H, ANDTSO: 0.



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011417532T/R PITCH CHANGE SHAFT 70400-06100-042 23302942 11C234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

2160 9988

311001113828811C23A

01237BRNG T/R PITCH CHG SHFT C84010620SB1162-102 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2



of 14

ECD00973

85244756035T00G01T700-GE-700 ENGINE ASSYGE-E-307369

4230

4761

20617

27075

11217

13744

2214

3174

5=

TOTAL COMPONENT COUNTS

COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-

READING AT INSTALLATION OF

MODULE/RECORDER3

READING AT REMOVAL OF

7. HISTORY RECORDER S/N

5=TOTAL COMPONENT COUNTS

COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-READING AT INSTALLATION OF

MODULE/RECORDER3READING AT REMOVAL OF

dcbaLINEOPERATING HOURSTEMP/TEMP INDEXLCF - 2LCF - 1

HISTORICAL COUNTS ON COMPONENT/MODULE

7. HISTORY RECORDER S/N6.

5. S/N4. P/N3. NOMENCLATURE2. ENG S/N1. MODEL

T700-GE-700

For use of this form, see DA PAM 738-751; the proponet agency is DCS,G-4

HISTORY RECORDER, COMPONENT, MODULE RECORDDA FORM 2408-16-1, OCT 1991

OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-

12.HISTORY COUNTS AT LAST DEPOT REPL

11.

O/H OR

10.

SERIAL NUMBER9.PART NUMBERNOMENCLATURE

8.

Major Nomenclature Major Part NumberMajor Wuc Major Serial Number

Page 2 of 14

04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-307369

hr)

332325459108772598

332325459108772598GE-C-0373696035T02G01COLD SECTIONMODULE

COND

COND

3323

3GGM9594E6064T55G01COMBUSTION LINER

COND

COND

332325459108772598

2910696733121145MRSG60376055T20G05MTCHDROTOR/STATOR ASSY

COND

COND

3323

4321AMDA43765043T24G14STAGE 1 NOZZLE

COND

COND

332325459108772598

4698817889032797GE-L-0061136064T98G01POWER TURBINEMODULE

COND

COND

3323

4402GE-D-0076426035T01G01ACCESSORY MODULE

COND

COND

3341

0K62666034T62P18PARTICLESEPARATOR BLOWER

COND

COND

4046

6526UDAJ12195074T79G07FUEL CONTROL

COND

COND

3323

2591APM467RU4076T64G01POU ASSY-O/S DRAINVALVE

COND

COND

3348

2745EMDE01854046T29G13ELECTRICALCONTROL UNIT

COND

COND

332325459108772598

27891900283351636ECD009734046T26G03HISTORY RECORDER

COND

COND

REVERSE OF DA FORM 2408-16-1, OCT 1991

OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 3 of 14


hr)

3323

3664UDC022444046T25G01COOLER, OIL

COND

COND

3964

498COMH110684046T28G14ANTI-ICE VALVE

COND

COND


3/26/201012:00:00 AM

1 CCAD ENGINE REPAIRED 25MAR10 IAW DMWR 1-2840-248 & CHANGESAND RECAPPED DTD 03DEC01. /S/ M. BENAVIDES, AIRCRAFT DATA

dean.a.keirn USAACE FT. RUCKER, AL.

9/21/201012:00:00 AM

1 REPLACED PARTICLE SEPARATOR. HISTORY RECORDER READINGS LCF1:01658, LCF2: 08375, TT INDEX: 19421, OP HRS: 2807, TTSN: 3341 HRS. GA4652R/SPEC. USAACE (AMSS) FT. RUCKER, AL


7/19/201112:00:00 AM

1 ENGINE RECEIVED FROM SUPPLY. 2408-16-1 AND 2410 SHOWED HRREADINGS OF 1636/8335/19002/2789 AND ENG CUMULATIVE COUNTS OF2598/10877/25459/3323. ACTUAL HR READINGS WERE: 1663/8385/19484/2814AND ACTUAL ENG CUMULATIVE COUNTS: 2625/10927/25941/3348.PAPERWORK ADJUSTED LOCALLY AND MCDS UPDATED BY RANDY


7/19/201112:00:00 AM

2 ENGINE RECEIVED FROM SUPPLY. 2408-16-1 AND 2410 SHOWED HRREADINGS OF 1636/8335/19002/2789 AND ENG CUMULATIVE COUNTS OF2598/10877/25459/3323. ACTUAL HR READINGS WERE: 1663/8385/19484/2814AND ACTUAL ENG CUMULATIVE COUNTS: 2625/10927/25941/3348.PAPERWORK ADJUSTED LOCALLY AND MCDS UPDATED BY RANDY


8/14/201212:00:00 AM

1 REMOVED ANTI ICE VALVE S/N G5518 WITH TSN-2043 FOR NON-CONFORMING ACTUATOR SHAFT FOR ANTI-ICE START BLEED VALVEFROM ENGINE S/N GE-E-307369 WITH CUMMULATIVE COUNTS:2864/12142/26583/3964. H.R.(ECD00973) READINGS: 1902/9600/20126/3430 ON


8/14/201212:00:00 AM

2 REMOVED ANTI ICE VALVE S/N G5518 WITH TSN-2043 FOR NON-CONFORMING ACTUATOR SHAFT FOR ANTI-ICE START BLEED VALVEINSTALLED ANTI ICE VALVE S/N AA068 WITH TSN-0 ENGINE S/N GE-E-307369 WITH CUMMULATIVE COUNTS: 2864/12142/26583/3964. H.R.(ECD00973) READINGS: 1902/9600/20126/3430 ON A/C S/N 8624565 @ 6666.6



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 4 of 14


hr)

8/14/201212:00:00 AM

3 REMOVED ANTI ICE VALVE S/N G5518 WITH TSN-2043 FOR NON-CONFORMING ACTUATOR SHAFT FOR ANTI-ICE START BLEED VALVEINSTALLED ANTI ICE VALVE S/N COMH11068 WITH TSN-0 ENGINE S/N GE-E-307369 WITH CUMMULATIVE COUNTS: 2864/12142/26583/3964. H.R.(ECD00973) READINGS: 1902/9600/20126/3430 ON A/C S/N 8624565 @ 6666.6


9/8/201212:00:00 AM

1 FUEL CONTROL S/N: UDAJ1097 REMOVED WITH TTSN: 10431 FROM ENGINES/N: GE-E-307369 WITH TTSN: 4023 PER H-60-12-ASAM-11. ENG CUMCOUNTS: LCF1=2897, LCF2=12383, TTI=26586, HOURS=4023. H/R(ECD00973)READINGS: LCF1=1935, LCF2=9841, TTI=20129, HOURS=3489.

mae.p.belford USAACE FT. RUCKER, AL.

9/20/201212:00:00 AM

1 FUEL CONTROL S/N: UDAJ1097 REINSTALLED WITH TTSN: 10431, TSO: 7814,OH: 1 ON ENGINE S/N: GE-E-307369 WITH TTSN: 4023 PER H-60-12-ASAM-11.ENG CUM COUNTS: LCF1=2897, LCF2=12383, TTI=26586, HOURS=4023. H/R(ECD00973) READINGS: LCF1=1935, LCF2=9841, TTI=20129, HOURS=3489.


9/20/201212:00:00 AM

2 REMOVED FUEL CONTROL SN: UDAJ1097 WITH TSN: 10431, TSO: 7814, OH: 1FROM ENG SN: GE-E-307369 WITH OP HRS 4046 DUE OVERHAUL PER H-60-12-ASAM-11.


9/20/201212:00:00 AM

3 INSTALLED FUEL CONTROL SN: UDAJ1219 WITH TSN: 6526, TSO: 0, OH: 1ON ENGINE SN: GE-E-307369 WITH OP HRS 4046. COMPONENT C/W H-60-12-ASAM-11.


9/24/201212:00:00 AM

1 ENGINE ASSY SN:GE-E-307369 W/ TSN:4046 REMOVED FROM ACFT 8624565@ 6747.3 ACFT HRS; REMOVAL DUE TO LEAKING OIL. ENGINECUMULATIVE COUNTS=LCF1:2907 LCF2:12428 TTI:26586 OP-HRS:4046//HISTORY REC. SN:ECD00973 READINGS=LCF1:01945 LCF2:09886 TTI:20129

rosonda.y.sterling USAACE FT. RUCKER, AL.

9/24/201212:00:00 AM

2 24 SEP 12 - REPLACED SWIRL FRAME OIL RINGS I/A/W TM 1-2840-248-23(ES014206)

tony.barnes USAACE FT. RUCKER, AL.

9/24/201212:00:00 AM

3 ENGINE ASSY SN: GE-E-307369 W/TSN: 4046 INSTALLED ON ACFT 8624565 @6747 ACFT HRS. CUM CTS: LCF1=2907 LCF2=12428 TTI=26586 OP HRS=4046HISTORY RECORDER: ECD00973 READINGS: LCF1=1945 LCF2=9886TTI=20129 OP HRS=3512


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 5 of 14


hr)

jessica.l.wendel USAACE FT. RUCKER, AL

6/17/201512:00:00 AM

1 REMOVED ENG SN: GE-E-307369 W/TTSN: 4743 FROM ACFT 8624565 @ 7417.1ACFT HRS DUE TO LEAKING. (ENG CUM CTS: 3160/13637/27051/4743)( HIST.REC SN: ECD00973 CTS: 2198/11095/20594/4209).

MH02153 USAACE FT. RUCKER, AL

7/28/201512:00:00 AM

1 ENGINE S/N: GE-E-307369 INSTALLED ON ACFT 8524480 AT 8542.2 ACFT HRS.ENG CUM COUNTS: LCF1=3160, LCF2=13637, TTI=27051, HOURS=4743. H/R(ECD00973) READINGS: LCF1=2198, LCF2=11095, TTI=20594, HOURS=4209.

mae.p.belford USAACE FT. RUCKER, AL.

9/3/201512:00:00 AM

1 REMOVED ENGS/N GE-E--307369 FROM ACFT 8524480 AT (8561.4 ACFT HRS)4761 ENG HRS DUE TO DRAIN LEAKING WITH ENG CUM CTS; LCF1 3174,LCF2;13744, TTI; 27075 4761 OP HRS: HR ( ECD00973) LCF1; 2212, LCF2;11202,TTI;20618 OP HRS 4227


9/15/201512:00:00 AM

1 REPLACED SWIRL FRAME IAW WITH 1-2840-2482P2 WP 343

stephanie.d.hall USAACE FT RUCKER, AL

11/1/201512:00:00 AM

1 INSTALLED ENG AT 4761 ENG HRS W/ TSN 4761: ENG CTS: LCF1; 3174, LCF2:13744, TTI: 27075, OP HRS 4761, HR (ECD00973) LCF1: 2214, LCF2; 11217,TTI;20617, OP HRS 4230



of 14

ECD00973

GE-E-3073696035T02G01COLD SECTION MODULEGE-C-037369

2789

3323

19002

25459

8335

10877

1636

2598

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 7 of 14

04A01 6035T02G01 COLD SECTION MODULE GE-C-037369

hr)

332325459108772598

334525128105372336SAP298385044T27G02POWER TAKEOFFDRIVE

COND

COND

332325459108772598

332325459108772598GLH220126035T77G19COMPRESSORROTOR ASSY

COND

COND

332325459108772598

0000GATHNAEP6035T88P07GAS GEN TURBINESHAFT

13789

11000

332325459108772598

0000WESP75525036T95P01INNER BALANCEPISTON SE

COND

COND

332325459108772598

0000BIW039W06035T79P04COMPRESSORDISCHARGE SE

COND

COND

332325459108772598

0000FIAAV5GG6035T83P01COMPRESSOR REARSHAFT

7789

5000

332325459108772598

0000VAEBS7005044T07P01NO 3 LABYRINTH

COND

COND

332325459108772598

21221267840101276OBTE08735035T57P02VORTEX SPOILER

COND

COND

332325459108772598

438812734103303009GATDV9425043T04P02TIE ROD,COMPRESSOR

8401

10000

332325459108772598

2273196128041024GAT7323M4045T08P01RING, SPACERCOMPRESSOR

10516

10000

332325459108772598

0000GLHTLFRM6055T59P01COMPRESSORIMPELLER

7789

5000


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 8 of 14

04A01 6035T02G01 COLD SECTION MODULE GE-C-037369

hr)

332325459108772598

35621982962912328GGA069756039T56G04OUTPUT SHAFT ASSY

COND

COND

332325459108772598

0000GLHTLMFL6032T26G09STAGE 1 BLISK

7789

5000

332325459108772598

0000GLHTM0C76032T27P08STAGE 2 BLISK

9789

7000

332325459108772598

0000GLHTM6MR6038T08P04STAGE 3 & 4 BLISK

9789

7000

332325459108772598

0000GLHTM2W66038T09P04STAGE 5 BLISK

9789

7000

332325459108772598

0000FCAN74116064T35P02NO 3 BALL BEARING

COND

COND

332325459108772598

124230261104TMKAET7R6064T15P01NO 4 ROLLER

COND

COND


3/26/201012:00:00 AM

1 CCAD C/S MOD REPAIRED 25MAR10 IAW DMWR 1-2840-248 & CHANGESAND RECAPPED DTD 03DEC01. FUEL INJECTORS CLEANED AND FLOWEDPER DMWR AT C/S TSN 3323 ON 25MAR10. /S/ M. BENAVIDES, AIRCRAFTDATA TECHNICIAN



of 14

ECD00973

GE-C-0373696039T56G04OUTPUT SHAFT ASSYGGA06975

2789

3562

19002

19829

8335

6291

1636

2328

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 10 of 14

04A01G 6039T56G04 OUTPUT SHAFT ASSY GGA06975

hr)

35621982962912328

16539206FCAF10436064T34P02NO 1 BALL BEARING

COND

COND

35621982962912328

574232933175254770MABC86645035T69P01NO 2 ROLLER

COND

COND


3/26/201012:00:00 AM

1 CCAD OUTPUT SHAFT INSTALLED ON 25MAR10, SERVICEABLE. /S/ M.BENAVIDES, AIRCRAFT DATA TECHNICIAN.



of 14

ECD00973

GE-E-3073696055T20G05MTCHD ROTOR/STATORMRSG6037

2789

2910

19002

6967

8335

3312

1636

1145

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 12 of 14

04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRSG6037

hr)

2910696733121145

164092123879986GATCNK516064T85P01STAGE 1 TURBINE

6149

5000

2910696733121145

2910696733121145GGAC46556039T57G24STATOR GASGENERATOR

COND

COND

2910696733121145

19338116566GATHG7N36064T86P02STAGE 2 TURBINE

7596

5000

2910696733121145

24341620982711782GFFP22736064T81P01STG 1 FWD COOLINGPLATE

5355

5000

2910696733121145

759132083257272PAMEP2296064T82P01STG 1 AFT COOLINGPLATE

7030

5000

2910696733121145

1163101623823427BIWCL8056039T52P03STG 2 FWD COOLINGPLATE

5626

4000

2910696733121145

79659992608528GFF5C9M16064T84P02STG 2 AFT COOLINGPLATE

6993

5000

2910696733121145

2910696733121145GGAG60376039T54G13ROTOR GASGENERATOR

COND

COND


3/26/201012:00:00 AM

1 CCAD MATCHED GG ROTOR/STATOR REPAIRED 25MAR10 IAW DMWR 1-2840-248 & CHANGES AND RECAPPED DTD 03DEC01. /S/ M. BENAVIDES,AIRCRAFT DATA TECHNICIAN



of 14

ECD00973

GE-E-3073696064T98G01POWER TURBINE MODULEGE-L-006113

2789

4698

19002

8178

8335

8903

1636

2797

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 14 of 14

04A03 6064T98G01 POWER TURBINE MODULE GE-L-006113

hr)

4696808988982795

4696808988982795GGA079775043T75G07POWER TURBINEROTOR

COND

COND

4696808988982795

164916251335501GAT6695G6038T32P01STAGE 3 TURBINE

6138

5000

4696808988982795

271744918GATHJ4C86038T34P06STAGE 4 TURBINE

7760

5000

4696808988982795

83613161173286GATHHD565125T92G01POWER TURBINESHAFT

6951

5000

4696808988982795

43944091374273735MABK01375034T27P01NO 5 ROLLER

COND

COND

4696808988982795

113711781485458BARA88965034T04P01NO 6 BALL BEARING

COND

COND


3/15/201012:00:00 AM

1 CCAD POWER TURBINE REPAIRED 13MAR10 IAW DMWR 1-2840-248 &CHANGES AND RECAPPED DTD 03DEC01. /S/ J. DALLY, AIRCRAFT DATATECHNICIAN



of 15

ECD03101

85244756035T00G01T700-GE-700 ENGINE ASSYGE-E-307927

8941

8941

17410

17410

19343

19343

3721

3721

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 2 of 15


hr)

747717028153183092

40592420073971913GEC0078966035T02G01COLD SECTIONMODULE

COND

COND

5129

5443GGMP85776039T58G02COMBUSTION LINER

COND

COND

894117410193423720

30251804474831984MRS089996055T20G05MTCHDROTOR/STATOR ASSY

COND

COND

0

0AMDA70125043T24G14STAGE 1 NOZZLE

COND

COND

756217118157863135

49329472105142654GE-L-0075756064T98G01POWER TURBINEMODULE

COND

COND

2989

0GE-D-9073766035T01G01ACCESSORY MODULE

COND

COND

5849

0K43156034T62P18PARTICLESEPARATOR BLOWER

COND

COND

7343

1185136911024046T52G39FUEL CONTROL

COND

COND

5413

0136TU4076T64G01POU ASSY-O/S DRAINVALVE

COND

COND

9197

1296EMDE01484046T29G13ELECTRICALCONTROL UNIT

COND

COND

0000

0000ECD031014046T26G03HISTORY RECORDER

COND

COND


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 3 of 15


hr)

4047

3602UDC069334046T25G06COOLER, OIL

COND

COND

2989

0COMH58614046T28G14ANTI-ICE VALVE

COND

COND


10/11/200712:00:00 AM

1 11OCT07- ENGINE REPAIRED AND RETURNED TO SERVICE. P/T MODREPLACED, SEE PREVIOUS ENTRY DTD 03OCT07. ENGINE H.R. ECD03101 =ENG CUMULATIVE COUNTS OF: LCF1-2056, LCF2-7589, TTI-16096, HRS-5099.DK1063, R/SPEC; USAAWC, FT. RUCKER, AL.

loletia.v.williams USAAWC FT. RUCKER, AL.

12/14/200712:00:00 AM

1 14DEC07- ENGINE REPAIRED AND RETURNED TO SERVICE. REPLACED C/SMOD AND COMB LINER, SEE PREVIOUS 2 ENTRIES DTD 12DEC07. ENGINECUMULATIVE COUNTS = H.R. ECD03101 READINGS OF: LCF1-2072, LCF2-7629, TTI-16116, HRS-5129. DK1063, R/SPEC; USAAWC, FT. RUCKER, AL.

loletia.v.williams USAAWC FT. RUCKER, AL.

6/15/200912:00:00 AM

1 15 JUN 09 - ENG ASSY SN: GE-E-307927 W/TSN:5849 @ 11905 ACFT HRS. ENGCHIP CAUTION LIGHT ILLUMINATED IN FLIGHT & WAS STEADY DURINGSHUTDOWN. CHIP DETECTOR & FILTER WERE REPLACED. (KJ0605 R/SPEC)USAACE, FT. RUCKER, AL.

loletia.v.williams USAACE FT. RUCKER, AL.

2/9/201012:00:00 AM

1 09 FEB 10 - #1 ENG SN: GEE307927 WITH TSN: 6226 (@ 12270.9 ACFT HRS)CHIP LIGHT - CHIP DETECTION INSP C/W FOUND 2 SMALL CHIPS (PC4683)(KJ0605 R/SPEC) USAACE, FT. RUCKER, AL


2/10/201012:00:00 AM

1 10 FEB 10 - REMOVED FUEL CONTROL S/N UDAJ1493 W/TTSN: 3399 FROMENG GEE-307927 (ACFT 8624515 @ 12272 ACFT HRS) (INTERNAL FAILURE)H/R READINGS MATCH ENG CUMM COUNTS- LCF1: 2477 LCF2: 9558 TTI:16346 OP HRS: 6226. HMU S/N UDAJ2153 W/TTSN: 2956 INSTALLED. RJ0827,USAACE, FT. RUCKER, AL.

thomas.m.lilly USAACE FT. RUCKER, AL

3/12/201012:00:00 AM

1 12 MAR 10 - REMOVED FUEL CONTROL S/N UDAJ2153 W/TTSN: 2964 FROMENG GEE-307927 (ACFT 8624515 @ 12274 ACFT HRS) (INTERNAL FAILURE)H/R (S/N: ECD03101) READINGS MATCH ENG CUMM COUNTS- LCF1: 2487LCF2: 9584 TTI: 16347 OP HRS: 6234. HMU S/N UDAJ6607 W/TTSN: 3363INSTALLED. (KJ0605 R/SPEC) USAACE, FT. RUCKER, AL.


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 4 of 15


hr)


5/16/201012:00:00 AM

1 16 MAY 10 - REMOVED ENG ASSY SN: GE-E-307927 WITH TSN: 6372 FROMACFT 8624515 @ 12411 ACFT HRS. DUE TO SMOKING @ EXHAUST UNDERLOAD. ENGINE CUMULATIVE COUNTS=H.R. (S/N ECD03101) READINGS AT:LCF1=2535, LCF2=9765, TTI=16417, OP HRS=6372 (KJ0605 R/SPEC) USAACE,FT. RUCKER, AL.


5/19/201012:00:00 AM

1 19 MAY 10 - ENGINE IS SMOKING @ EXHAUST UNDER LOAD C-SUMP O-RINGS LEAKING. REPLACE C-SUMP O-RINGS I/A/W TM1-2840-248-23 ANDRETURN TO SERVICEABLE AS PER ES 4206. D. WILLIAMS 0950, USAACE, FT

loletia.v.williams USAACE FT RUCKER,AL

5/8/201212:00:00 AM

1 REMOVED FUEL CONTROL S/N 15464206 FROM ENG AT 7343 ENG HRSW/TSN 1748 (7242.8 ACFT 8724659) DUE TO INTERNAL FAILURE WITH ENGOP HRS 7343: INSTALLED S/N 13691102 W/TSN 1185. AT OP HRS 7343

theresa.d.pollard USAACE FT. RUCKER,AL

7/7/201212:00:00 AM

1 07 JUL 2012 - REMOVED ENG SN: (GE-E-307927) FROM ACFTSN: (8724659)@ 7374.3 AIRCRAFT HOURS, WITH COUNTS OF LCF1: 3092, LCF2: 15318,TTI: 17028, OP HOURS: 7477 FOR FAILURE CODE 301, (STAGE 1COMPRESSOR DAMAGE). HISTORY RECORDER SN: (ECD03101) WITHREADINGS OF LCF1: 3092, LCF2: 15318, TTI: 17028, OP HOURS: 7477.

thomas.e.mitchell USAACE FT. RUCKER, AL.

7/10/201212:00:00 AM

1 COLD SECTION S/N GE-C-037254 REMOVED FROM UNINSTALLED EINGINEWITH LCF1 2120 LCF2 12010 TTI 9235 TTI 4063. REMOVAL DUE TO FOREIGNOBJECT DAMAGE. ENG CUM CTS = LCF1 3092 LCF2 15318 TTI 17028 OP HRS7477. H/R S/N ECD03101 = LCF1 3092 LCF2 15318 TTI 17028 OP HRS.INSTALLED GEC007896 WITH LCF1 1913 LCF2 7397 TTI 24200 OP HRS 4059


8/25/201212:00:00 AM

1 REMOVED ENGINE ASSY S/N: GE-E-307927 W/TSN:7562 FROM ACFT 8724666@ 6226.5 ACFT HRS. (TBO) ENGINE CUMM CNTS: 3135, 15786, 17118, 7562.ENGINE H/R (S/N: ECD03101) READINGS: SAME AS CUMM CNTS.


8/30/201212:00:00 AM

1 REMOVED PT MOD (GE-L-006086) WITH CTS: 2641/13826/7456/4985 FROMUNINSTALLED ENG (GE-E-307927) WITH CTS: 3135/15786/17118/7562 FORTBO. HIS REC (ECD03101) READINGS SAME AS ENG CTS. INSTALLED PTMOD (GE-L-007575) WITH CTS: 2654/10514/9472/4932.

brandi.n.keener USAACE FT RUCKER, AL


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 5 of 15


hr)

9/15/201212:00:00 AM

1 INSTALLED ENGINE S/N: GE-E-307927 W/TSN: 7562 ON ACFT 8524475 @6876.4 ACFT HRS. ENGINE CUMM CNTS: 3135, 15786, 17118, 7562. ENGINEH/R (S/N:ECD03101) READINGS: SAME AS CUMM CNTS>


7/13/201512:00:00 AM

1 REMOVED ENG SN: GE-E-307927, FROM ACFT 8524475, AT 8199.8 ACFT HRS.H.R. SN: ECD03101, H.R. READINGS: LCF1: 3721, LCF2: 19343, TTI: 17410,HRS: 8941. ENG CUMULATIVE COUNTS MATCH THE H.R. READINGS.REMOVAL IS DUE TO MATCHED ROTOR STATOR, STG 1 REAR COOLING PLTIS DUE REPLACEMENT.


7/16/201512:00:00 AM

1 MATCHED ROTOR/STATOR MRS08375 REMOVED FROM UNINSTALLED ENGGE-E-307927 FOR "TIME CHANGE" WITH CUMULATIVE COUNTS:2929/14179/14810/5272. MATCHED ROTOR/STATOR MRS08999 INSTALLEDWITH CUMULATIVE COUNTS: 1984/7483/18044/3025. H.R. ECD03101READINGS = ENG CUMULATIVE COUNTS OF: 3720/19342/17410/8941.


7/28/201512:00:00 AM

1 INSTALLED ENG SN: GE-E-307927, ON ACFT 8524475, AT 8199.8 ACFT HRS.H.R. SN: ECD03101, H.R. READINGS: LCF1: 3721, LCF2: 19343, TTI: 17410,HRS: 8941. ENG CUMULATIVE COUNTS MATCH THE H.R. READINGS.

rick.r.skinner USAACE FT. RUCKER, AL.


of 15

ECD03101

GE-E-3079276035T02G01COLD SECTION MODULEGEC007896

7477

4059

17028

24200

15318

7397

3092

1913

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 7 of 15

04A01 6035T02G01 COLD SECTION MODULE GEC007896

hr)

40562413573811909

39724415279102707SAP356305056T66G02POWER TAKEOFFDRIVE

COND

COND

40562413573811909

40562413573811909GLB005966035T77G10COMPRESSORROTOR ASSY

COND

COND

40562413573811909

35351111263812046GATBW5826035T88P04GAS GEN TURBINESHAFT

14939

11000

40562413573811909

0000WESR05595036T95P01INNER BALANCEPISTON SE

COND

COND

40562413573811909

75473311266395MMTF65376035T79P04COMPRESSORDISCHARGE SE

COND

COND

40562413573811909

154496492198724FIAAK7HG6035T83P01COMPRESSOR REARSHAFT

10930

5000

40562413573811909

1923821136691142GATTB4095044T07P01NO 3 LABYRINTH

COND

COND

40562413573811909

23591745956691468TRU101855035T57P02VORTEX SPOILER

COND

COND

40562413573811909

148191492642783GATHC0RC5043T04P02TIE ROD,COMPRESSOR

15993

10000

40562413573811909

1470972831961004GAT4209H4045T08P01RING, SPACERCOMPRESSOR

16004

10000

40562413573811909

0000GLHTNNLT6055T59P01COMPRESSORIMPELLER

12474

5000


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 8 of 15

04A01 6035T02G01 COLD SECTION MODULE GEC007896

hr)

40562413573811909

50562365797082686GGA060346039T56G04OUTPUT SHAFT ASSY

COND

COND

40562413573811909

0000GLHTNK5D6032T26G09STAGE 1 BLISK

12474

5000

40562413573811909

0000GLHTNWDJ6032T27P08STAGE 2 BLISK

14474

7000

40562413573811909

0000GLHTNTPC6038T08P04STAGE 3 & 4 BLISK

14474

7000

40562413573811909

0000GLHTNW4K6038T09P04STAGE 5 BLISK

14474

7000

40562413573811909

75473311266395395934066064T35P02NO 3 BALL BEARING

COND

COND

40562413573811909

0000FCAY22796064T15P03NO 4 ROLLER

COND

COND


4/26/201212:00:00 AM

1 COLD SECTION GEC 007896, T700-700 WAS REPAIRED IAW DMWR 1-2840-248-12 CHANGE 12. COLD SECTION MODULE TIMES = LCF1 1909, LCF2 7381 TTI24135 EOH 4056 COLD SECTION MODULE TIMES AFTER TEST = LCF1 1913,LCF2 7397, TTI 24200 EOH 4059 RECORDS ARE ON FILE AT THIS FACILITYUNDER WORK ORDER 412929, SHERYL HARPER, T700 ENGINE ANALYST

QC000000 GEES STROTHER

7/10/201212:00:00 AM

1 COLD SECTION INSTALLED ON UNINSTALLED ENGINE (GE-E-307927) WITHLCF1 1913 LCF2 7397 TTI 24200 OP HRS 4059. ENG CUM CTS = LCF1 3092LCF2 15318 TTI 17028 OP HRS 7477. HR S/N ECD01301 READINGS = LCF1 3092LCF2 15318 TTI 17028 OP HRS 7477.



of 15

ECD03101

GEC0078966039T56G04OUTPUT SHAFT ASSYGGA06034

7477

5059

17028

23722

15318

9724

3092

2690

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 10 of 15

04A01G 6039T56G04 OUTPUT SHAFT ASSY GGA06034

hr)

50562365797082686

0000FCAY49806064T34P02NO 1 BALL BEARING

COND

COND

50562365797082686

0000FCAV52945035T69P02NO 2 ROLLER

COND

COND


4/26/201212:00:00 AM

1 COLD SECTION GEC 007896, T700-700 WAS REPAIRED IAW DMWR 1-2840-248-12 CHANGE 12. COLD SECTION MODULE TIMES = LCF1 1909, LCF2 7381 TTI24135 EOH 4056 COLD SECTION MODULE TIMES AFTER TEST = LCF1 1913,LCF2 7397, TTI 24200 EOH 4059 RECORDS ARE ON FILE AT THIS FACILITYUNDER WORK ORDER 412929, SHERYL HARPER, T700 ENGINE ANALYST

QC000000 GEES/STROTHER UNKNOWN


of 15

ECD03101

GE-E-3079276055T20G05MTCHD ROTOR/STATORMRS08999

8941

3025

17410

18044

19342

7483

3720

1984

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 12 of 15

04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRS08999

hr)

30251804474831984

3683135458165GATHH79L6064T85P02STAGE 1 TURBINE

13573

5000

30251804474831984

35931315578192082GGA065106039T57G24STATOR GASGENERATOR

COND

COND

30251804474831984

1046181473653581GATHAPK36064T86P01STAGE 2 TURBINE

12895

5000

30251804474831984

26011364790671233GFFR82TK6064T81P01STG 1 FWD COOLINGPLATE

11340

5000

30251804474831984

1955871553491272BIWBW4176039T50P04STG 1 AFT COOLINGPLATE

10986

4000

30251804474831984

108850863535660PAMEU7646064T83P01STG 2 FWD COOLINGPLATE

12853

5000

30251804474831984

16055092414561GFF5D2A86064T84P02STG 2 AFT COOLINGPLATE

12336

5000

30251804474831984

30251804474831984GGA089996039T54G13ROTOR GASGENERATOR

COND

COND


7/6/201212:00:00 AM

1 TB1-2840-248-20-2 DTD 30JU94 C/W AT CCAD AND LIFE LIMITS C/W IAW TM1-2840-248-23, TABLE 1-10 1JUN99 "STAGE ONE AND TWO GG BLADE SETSCONTAIN NEW OR USED BLADES THAT HAVE ALWAYS BEEN RUN WITHDAMPERS," CCAD-C/W: UH-60-95-ASAM-08 AND 97-ASAM-03, S/ F. ORTIZRECORDS CLERK, CCAD, CC, TX.


7/16/201512:00:00 AM

1 INSTALLED MATCHED ROTOR/STATOR MRS08999 WITH CUMULATIVECOUNTS: 1984/7483/18044/3025 ON ENG GE-E-307927. H.R. ECD03101READINGS = ENG CUMULATIVE COUNTS OF: 3720/19342/17410/8941.



of 15

ECD03101

GE-E-3079276064T98G01POWER TURBINE MODULEGE-L-007575

7562

4932

17118

9472

15786

10514

3135

2654

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 14 of 15


hr)

49309392105062652

49309392105062652GGA073185043T75G07POWER TURBINEROTOR

COND

COND

49309392105062652

25062036360GATHP8C06038T32P02STAGE 3 TURBINE

12310

5000

49309392105062652

6411880798318GATHAACM6038T34P05STAGE 4 TURBINE

11919

5000

49309392105062652

0000GATHWE695125T92G01POWER TURBINESHAFT

12560

5000

49309392105062652

0000FCAV76605034T27P02NO 5 ROLLER

COND

COND

49309392105062652

3436734056711506MDA573PV6064T37P01NO 6 BALL BEARING

COND

COND


4/24/200712:00:00 AM

1 WUC: 04A03 P/N: 6064T98G01 S/N: GE-L-007575POWER TURBINE MODULE24 APR 07 CCAD POWER TURBINE REPAIRED 21APR 07 IAW DMWR 1-2840-248 7 CHANGES AND RECAPPED AED P3430BDTD 03 DEC 01. S/R. HERRERA. AIRCRAFT DATA TECHNICIAN.

thomas.m.lilly CCAD UNKNOWN

3/19/200912:00:00 AM

1 WUC: 04A03 P/N: 6064T98G01 S/N: GE-L-007575POWER TURBINE MODULE19 MAR 09 - INSTALLED PT MOD ON ENG S/N GE-E-306077 ENG CUM CTS: LCF 1 1991, LCF 2 9533, TTI 8758, OP HRS 6585. HRS/N ECD00707 CUM READINGS: LCF 1 1374, LCF 2 16710, TTI 10445, 4765 OPHRS. PT MOD CUM CTS: LCF 1 1965, LCF 2 7002, TTI 8971, OP HRS 3266.TB1027 R/SPEC USAACE FT. RUCKER, AL.

thomas.m.lilly USAACE FT. RUCKER, AL.

2/16/201212:00:00 AM

1 REMOVED PT MOD (GE-L-007575) WITH CTS: 2652/10506/9392/4930 FROMUNINSTALLED ENG (GE-E-306077) WITH CTS: 2678/13037/9179/8249 FOR TBO.HIS REC (ECD00707) READINGS: 2061/20214/10866/6429. *****DELAYEDENTRY MADE BY BK6292 ON 31AUG12*****

olivia.d.williams USAACE FT RUCKER, AL

5/21/2012 1 21 MAY 12 - POWER TURBINE RECAPPED ON 17MAY12 IAW DMWR 1-2840-


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 15 of 15


hr)

12:00:00 AM 248 & CHANGES. MT5543, CCAD CORPUS CHRISTI, TX

MT5543 CCAD CORPUS C, TX

8/30/201212:00:00 AM

1 INSTALLED PT MOD (GE-L-007575) WITH CTS: 2654/10514/9472/4932 ONUNINSTALLED ENG (GE-E-307927) WITH CTS: 3135/15786/17118/7562. HISREC (ECD03101) READING = ENG CTS.

brandi.n.keener USAACE FT RUCKER, AL


STARTS/HOURS

LIFE

STARTS/RMVL

HOURS

COMP

STARTS/INST

HOURS

SINCEO/H

STARTS/RMVL

HOURS

NHA

HOURSSTARTS/

O/H

7k.REPLACE

DUE

7j.O/H OR

REPLACE7i.

7h.COMP

7g.STARTS/HOURS

7f.

7e.NHAINST

7d.NO.

PREV

7c.COMPONENT

SERIAL NUMBER

7b.PART NUMBER

AND NSNAND WUCNOMENCLATURE

7a.

7. REPLACEMENT DUE STARTS/HOURS FOR THE APU AND SUB-COMPONENTS

6d. APU HISTORICAL STARTS/HOURS

1. MODEL

3. SERIAL NUMBER

2. NOMENCLATURE

4. PART NUMBER 5. NHA S/N

6. LINE NUMBER 6a. STARTS LAST O/H 6b. STARTS 6c. OPERATING HOURS

METER READING AT APU INSTALL

3

2-

TOTAL METER COUNTS SINCE INSTALL LINE 3 MINUS LINE 2

PREVIOUS STARTS/HOURS

4=

1+

TOTAL STARTS/HOURS LINE 4 PLUS LINE 1

METER READING AT APU REMOVAL

5=

9

29

7063

29

1308

2

856006

APU

116305-302 8524475

3 9116305-302 856006AUXILIARY POWER UNIT 7063

15B 2835013692818

60206000

starts

RC RC4502902 SIF4724WHEEL, COMPRESSOR 7054 0

15B02B 2835014596002

60206000

starts

RC RC4503991 S046WHEEL, TURBINE 7054 0

15B03 2835013638089

60206000

starts


29-Sep-2014 1 7 MAY 09:APU OVERHAULED IAW DMWR55-2835-209. NEW METER INSTALLED @ 6000 EVENTS / 1154HRS. TBO TIME FOR THIS APU IS 6000 METER EVENTS @ 12000 TOTAL APU STARTS. ENTERED BYKF7892 ESRA, FTCKY. DSN635-6201 4108 THIS DATE, RECEIVED APU S/N: 856006 FOR OVERHAUL.READINGS AT RECEIPT: METER HOUR: 0153; START METER: 1054; TSN: 1307; SSN: 7054. INITIATED NEWFORM. 4272 THIS DATE, OVERHAULED APU S/N: 856006. REPAIR/OVERHAUL PROCESSED INACCORDANCE WITH DMWR 1-2835-209 AS SUPPLEMENTED BY NAVAIRDEPOT MCAS CHPT LES CP23-0-LL-173, REV C AND IS SERVICEABLE FOR INSTALLATION AND CONTINUED SERVICE. WORK PERFORMEDIS AS FOLLOWS: INSTALLED: NEW C/W; NEW T/W; FUEL CONTROL S/N: 111384. NEW METER INSTALLEDAT TSN: 1307 SSN: 7054. METER READINGS AT INSTALL: HOURS: 0001 STARTS: 0020 START METERADVANCED 20 STARTS DURING OPS CHECK. READINGS AT COMPLETION: METER HOURS: 0002; METERSTARTS: 0029; TSN: 1308; SSN: 7063. GP8475 DSN 451-7874 FRC EAST CHERRY POINT Data ReportREPAIR/OVERHAUL PROCESSED I/A/W DMWR 1-2835-209 AS SUPPLEMENTED BY NAVAIRDEPOT MCASCHPT LES CP23-0-LL-173, REV C AND IS SERVICEABLE FOR INSTALLATION AND CONTINUED SERVICE.WORK PERFORMED IAAS FOLLOWS: INSTALLED: NEW C/W; NEW T/W; FUEL CONTROL S/N 111384. NEWMETER INSTALLED AT TSN: 1307 SSN: 7054. METER READINGS AT INSTALL: HOURS: 0001, STARTS:0020, START METER ADVANCES 20 STARTS DURING OP CHECK. READING AT COMPLETION: METERHOURS: 0002; METER STARTS: 0029; TSN: 1308, SSN: 7063.

GP8475 DSN 451-7874 FRC EAST CHERRY PT.

23-Oct-2014 1 INSTALLED ON ACFT. 8524475 AT 7962 ACFT. HRS., WITH METER READINGS AS FOLLOWS: 3 PREVO/HAULS, TSSO: 9, TSSN: 7063, TTSN: 1308.

anthony.s.speigner USAACE FT. RUCKER, AL.

For use of this form, see DA PAM 738-751; the proponent agency is DCS G-4

APD LC v1.00AUXILIARY POWER UNIT AND COMPONENT RECORDDA FORM 2408-16-2, MAR 2014

of 3

8524475HELICOPTER, UTILITY EH-60A

7. FREQUENCY 4. 5. ITEM TO BE INSPECTED

2. MODEL 3. SERIAL NUMBER 1. NOMENCLATURE

8.DUE

NEXT 6. REFERENCE 9. COMPLETED ATINSP NO.

A022 13 Apr 201714TM 1-1520-237-23&P14 DAY FLYABLE STORAGEENGINE RUN UP

30 Mar 2017D

A092 11 Apr 201730TM 11-6140-203-23 P30 DAY SLAB BATTERYINSPECTION (D8565/11-1)

12 Mar 2017D

A103 05 Apr 201730TM 1-1500-344-23AIRCRAFT WASH DUE 06 Mar 2017D

A110 8906.640TM 1-1520-237-PMSPMS 40 HOUR INSPECTION (ESMONLY)

8866.6H

A115 21 Apr 201730TM 1-1520-237-23&PLUBE REQUIRMENTS (ESMONLY)

22 Mar 2017D

A115 8889.940TM 1-1520-237-23&PLUBE REQUIRMENTS (ESMONLY)

8849.9H

A116 8920.2360H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE (ESM ONLY)

8560.2H

A116 24 Jun 201712H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE (ESM ONLY)

24 Jun 2016M

A117 8920.2360H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE(ESM ONLY)

8560.2H

A117 24 Jun 201712H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE(ESM ONLY)

24 Jun 2016M

A160 02 Jun 201790TM 1-1520-237-23&PESM 90 DAY CORROSIONINSPECTION

04 Mar 2017D

A210 8923120TM 1-1520-237-23&P120 HOUR INSPECTIONREQUIREMENTS (ESM ONLY)

8803H

A211 8920.2360H-60-10-AMAM-11APU OIL SAMPLE (ESM ONLY) 8560.2H

A211 24 Jun 201712H-60-10-AMAM-11APU OIL SAMPLE (ESM ONLY) 24 Jun 2016M

A213 8923120TB 1-1520-237-20-266ENGINE COMPRESSORCLEANING (ESM ONLY)

8803H

A295 8920.2360TM 1-1520-237-23&PSTABILATOR ACTUATOR ASSYLUBE (ESM ONLY)

8560.2H

A298 8919.8360TM 1-1520-237-23&PLUBE TAIL WHEEL BEARING 8559.8H

A298 13 Jun 201712TM 1-1520-237-23&PLUBE TAIL WHEEL BEARING 13 Jun 2016M

A299 8920.2360TM 1-1520-237-23&PSWASHPLATE LUBE (ESM ONLY) 8560.2H

A299 14 Jun 201712TM 1-1520-237-23&PSWASHPLATE LUBE (ESM ONLY) 14 Jun 2016M

A440 8919.8720TM 1-1520-237-23&PCLEAN TAIL WHEEL LOCKPIN 8199.8H

A470 10062.91500TM 1-1520-237-23&PREPLACE NUMBER TWOCROSSFEED VALVE

8562.9H

A471 10359.82160TM 1-1520-237-23&PREPLACE T/R SHAFT SUPPORTBEARINGS (FWD)

8199.8H

A472 10359.82160TM 1-1520-237-23&PREPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)

8199.8H

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, OCT 1997 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

of 3




8.DUE


A473 10359.82160TM 1-1520-237-23&PREPLACE T/R SHAFT SUPPORTBEARINGS (AFT)

8199.8H

A476 9998.25000TM 1-1520-237-23&PREPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS

4998.2H

A477 9998.25000TM 1-1520-237-23&PREPLACEMENT OF STABILATORACTUATOR BOLTS

4998.2H

A480 9998.25000TM 1-1520-237-23&PREPLACE PIVOT BOLT 70400-08159-101,102,103,104

4998.2H

A485 9998.25000TM 1-1520-237-23&PREPLACE BELLCRANK BOLT70400-08159-105,106,107,108

4998.2H

A496 03 Jul 2017180TM 1-1520-237-23&PCF3BR FIRE EXTINGUISHERWEIGHT TEST INSPECTION

04 Jan 2017D

A501 02 Aug 2017180TM 1-1520-237-23&PMAIN ROTOR BLADE PRESSURECHECK

03 Feb 2017D

A502 21 Apr 2017180TM 1-1520-237-23&PINSPECT AND TEST GROUNDRECEPTACLE IAW TM 1-1500-204-23

23 Oct 2016D

A530 02 Mar 201812DA PAM 738-751AIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)

02 Mar 2017M

A532 25 Jun 201712TM 1-1500-204-23-4COMPASS SWING / RMI SWING 25 Jun 2016M

A533 01 Aug 201712TM 1-1520-237-23&PPITOT STATIC SYSTEMINSPECTION

01 Aug 2016M

A534 31 May 201712TM 1-1500-204-23-1FIRST AID KIT INSPECTION 31 May 2016M

A538 13 Aug 201712TM 1-1520-237-23&PFAT/OAT GAUGEINSPECTION/TEST

13 Aug 2016M

A553 01 Feb 201812AR 95-1ANNUAL WEIGHT AND BALANCEINVENTORY (365-1)

01 Feb 2017M

A580 27 Dec 201824TM 11-6140-203-23 PRETURN SLAB TO AVIM FORCAPACITY CHECK (EVERY 24MONTH)

27 Dec 2016M

A621 01 Feb 201924AR 95-1AIRCRAFT WEIGHING CLASS 1 01 Feb 2017M

A625 27 Dec 202160TM 11-6140-203-23 PREPLACEMENT OF SLABBATTERY (SLAB)

27 Dec 2016M

A630 01 May 2022114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 Nov 2012M

A633 01 May 2022114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #1,CARTRIDGE DODIC MH92

01 Nov 2012M

A638 01 May 2022114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #2,CARTRIDGE DODIC MH92

01 Nov 2012M

A640 01 Mar 2022114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE CARTRIDGE,31512AS105, 30903824-1

01 Sep 2012M

A648 16 Jan 2024180TM 1-1520-237-23&PREPLACE T/R SPRING CAPSULEASSY

16 Jan 2009M

A660 01 Aug 202172TB 9-1300-385REPLACE THRUSTEREMERGENCY RELEASE CARGOHOOK, MJ20

01 Aug 2015M




of 3




8.DUE


A665 12 Aug 201948H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215

12 Aug 2015M

A670 10 Dec 202048TM 1-1520-237-23&PCABIN TUB INSPECTION 10 Dec 2016M

A675 21 Jul 201748TM 1-1520-237-23&PFLIGHT CONTROL ROD INSP 21 Jul 2013M

A695 8919.8720H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

8199.8H

A695 13 Aug 201948H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

13 Aug 2015M

A755 90009000H-60-10-ASAM-11PC LINK TO SWASHPLATEBOLTS REPLACEMENT

0H




T700-GE-700T700-GE-700 ENGINE ASSY

ALT ETFACT TTV°CTIMENUMBERNG %PRESSFATENGINESERIAL 866 +/- 49. TORQUE10.8.7.6.AIRCRAFT REMARKS11. TGTDATE 12.5.4.

GE-E-307369

3. ENGINE SERIAL NUMBER2. ENGINE MODEL1. NOMENCLATURE

Page 1 of 1

03-Nov-2015 8524475 ENG REPL.6000 96 94 197.8184230 845

29-Jul-2015 8524480 ENGINE REPLACED6000 92 94 0.9797.2194743 842

26-Aug-2015 8524480 ENGINE REINSTALLED4500 101 100 197.5164750.8 840

03-Aug-2011 8624565 ENG REPL.6000 98 94 197.9203350 848

21-Aug-2011 8624565 RESET BASELINE5000 100 94 198243398 850

04-Feb-2012 8624565 RESET BASELINE FOR HITCHECKS FAILING. NEWBASELINE FAT +14, PA -40,TGT 669.

6000 97 98 0.98296.6103728 846

12-Aug-2012 8624565 POST PHASE4000 103 101 197.5183964 846

25-Sep-2012 8624565 BASELINEREINSTALLATION +19 +0681,680,681

4000 100 101 0.9897.3194046 848

25-Jun-2014 8624565 ENGINE REINSTALLATION4000 101 100 197.5204579 845

16-May-2015 8624565 720 HR INSP / PROC 63COMPLETED

4000 101 102 0.9997.8174705 847


T700 SERIES TURBINE ENGINE ANALYSIS CHECK RECORDDA FORM 2408-19-2, DEC 1991

ULLSADMIN

Highlight

T700-GE-700T700-GE-700 ENGINE ASSY

ALT ETFACT TTV°CTIMENUMBERNG %PRESSFATENGINESERIAL 866 +/- 49. TORQUE10.8.7.6.AIRCRAFT REMARKS11. TGTDATE 12.5.4.

GE-E-307927

3. ENGINE SERIAL NUMBER2. ENGINE MODEL1. NOMENCLATURE

Page 1 of 1

16-Sep-2012 8524475 INITIAL INSTALLATION, HITBASE INFO, FAT=30, PA=80,TGT=692

5200 105 99 189.2177562 849

10-Dec-2013 8524475 POST 720 HOUR PHASE7000 100 96 197.3118186 851

26-Aug-2015 8524475 PMI 2 GG RTR REPL, 8201.6ACFT HRS

5000 104 97 1.0798.5208944 851

12-Feb-2016 8524475 ECU REPL5500 106 102 19879199 847

25-Jun-2016 8524475 ENGREMOVED/REINSTALLED

4000 106 97 199.3259320 848

11-Apr-2001 8724659 (NO REMARK)2000 102 105 0.9998.3251990 849

04-Jun-2001 8724659 PROC 634000 99 100 0.9997.9202076 849

27-Nov-2001 8724659 500 HR/ENG REINST4000 102 100 197.8172190 848

10-Feb-2003 8724659 500 HR INSP4000 108 106 197.262688 846

14-Oct-2003 8724659 ENGINE REPLACED6000 95 97 0.9797.4152992 845

12-Mar-2004 8724659 ENGINE REINST./GIMBALSEAL REPLACE

4000 106 106 197.6123210 846

15-Jul-2004 8724659 500 HR. INSP./ENG. REINST4000 96 97 0.9998243337 847

28-Oct-2005 8724659 PHASE #6, NO BUBBLES4000 104 102 196.1184047 845

13-Dec-2005 8724659 COMPLETE W/ALT PWR4000 107 108.5 9.796.364144 844

10-Aug-2006 8724659 ENG INSTALLATION4000 97 99 0.9896.6234457 845

30-May-2007 8724659 P.E.5000 101 101 199.5144849 847

17-Nov-2007 8724659 ENGINE CHANGE PMI #94000 105 105 196.2125102 845

08-Jan-2008 8724659 ENG REPLACE4000 108 104 198.5145129 847

11-Dec-2009 8724659 ENG REINSTALL6000 102 99 197.176118 844

13-Mar-2010 8724659 1.0 ETF (720 HR INSP)4000 110 107 197.396234 846

08-Sep-2010 8724659 720 HOUR PHASE4000 103 99 199.3226518 842

04-Dec-2011 8724659 PHASE GEN TEST FLT4000 108 105 198.2127227 845

28-Mar-2012 8724659 ATF = 1.0 GMTF6000 102 98 197.8107241 845

20-Jul-2012 8724666 BASELINE REPLACED ENG688,690,687 AT+29,AT+50ALT

5000 105 97 198.3207477 848


T700 SERIES TURBINE ENGINE ANALYSIS CHECK RECORDDA FORM 2408-19-2, DEC 1991

ULLSADMIN

Highlight

T/T I HIST RCDR S/NSERIAL 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

17105 SESI

2. ORGANIZATION

CSGLD-1052

REQUIREMENT CONTROL SYMBOL(Julian)1. PERIOD ENDING DATE

Page 1 of 1

1GE-E-207851 ECD0211550452334110349272095098424018

2GE-E-306748 CAO019015555336212134326795098424018

1GE-E-306009 ECD03062438852415836183688008424021

1GE-E-306375 CAO0081060642540017183371286828424024

2GE-E-306513 CAO0075436912173213281242886828424024

1GE-E-307927 ECD0310196151749120579399888458524475

1GE-E-307927 ECD0310196201749120585400088508524475

1GE-E-307927 ECD0310196241749120597400188548524475

1GE-E-307927 ECD0310196321749220610400588618524475

1GE-E-307927 ECD0310196381749220615400688678524475

1GE-E-307927 ECD0310196481749220650401088758524475

1GE-E-307927 ECD0310196481749220650401088758524475

2GE-E-307369 ECD0097347692080112407244888458524475

2GE-E-307369 ECD0097347732080112415245088508524475

2GE-E-307369 ECD0097347772080112426245188548524475

2GE-E-307369 ECD0097347852080112440245588618524475

2GE-E-307369 ECD0097347912080112445245688678524475

2GE-E-307369 ECD0097348002081412483246088758524475

2GE-E-307369 ECD0097348002081412483246088758524475

1GE-E-307779C LMDH459515175712216060549207923300

1GE-E-307779C LMDH459515175712216060549207923300

2GE-E-991580 LMDH495412984461284159649207923300

2GE-E-991580 LMDH495412984461284159649207923300

1GEE-761436C LMDH7060205979345745101262957923304

1GEE-761436C LMDH7060205979345745101262957923304

2GEE767626 LMDH567032824328110062957923304

1GEE767410 LMDH1905103065099119845558223724

2GEE307957C LMDH43576063361182338845558223724

1GEE306276 ECD012633077147802762100841078223726

2GEE307093 CAO012033837100707617234641078223726


ENGINE COMPONENT OPERATING HOURS RECORDDA FORM 2408-19-3, DEC 1991

ULLSADMIN

Highlight

30

0

7572.1

8524475 6833.6 8876

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

EH-60A A26501328 Days

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

HELICOPTER, UTILITY MAIN TRANSMISSION MODULE Hrs

a. NOMENCLATURE AND TYPEa. NOMENCLATUREFREQUENCY

COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 1 of 1

a b

SUBMITTED

c a b

SAMPLE DATE PIDSAMPLELAST OILEND ITEM

RESULTSDATE RESULTS RECEIVED7. 8.6. REASON FORHOURS5.4.

COMPONENTCHANGE

TP163410-Nov-2010NORMALROUTINE223.04444589709-Nov-2010

loletia.v.williams03-Aug-2011NORMALROUTINE530.04751620403-Aug-2011

kathleen.m.jungell05-Mar-2012NORMALROUTINE885.05106655904-Mar-2012

jessica.n.kennedy19-Oct-2012NORMALROUTINE1246.05467692017-Oct-2012

jessica.n.kennedy25-Mar-2013NORMALROUTINE1402.05623707621-Mar-2013

theresa.d.pollard06-Jun-2013NORMALROUTINE1554.05775722805-Jun-2013

TP163412-Jul-2013ABNORMALROUTINE1604.05825727812-Jul-2013

TP163416-Jul-2013NORMALROUTINE0.05828728115-Jul-2013

jessica.n.kennedy09-Sep-2013NORMALOTHER152.059807440.807-Sep-2013

WB11426227-Feb-2014NOT_TESTEDPRE-RESET286.06114756720-Feb-2014

WB11426227-Feb-2014NORMALPRE-RESET286.06114756727-Feb-2014

WB11426219-Nov-2014ABNORMALPOST PHASE0.06113.87566.818-Nov-2014

WB11426229-Jan-2015NORMALLAB REQUES5.36119.17572.129-Jan-2015

stephanie.d.hall08-Mar-2016NORMALROUTINE356.96476792904-Mar-2016

DRAIN & FLUSH RESAMPLE AT END OF FLIGHT DAYR

9. REMARKS:

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

OIL ANALYSIS LOGDA FORM 2408-20, OCT 1997

0

360

8560.2

8524475 8875.6 0


EH-60A A005-01253 Days


HELICOPTER, UTILITY INTERMEDIATE GEARBOX Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 1 of 1

a b

SUBMITTED

c a b



COMPONENTCHANGE

SC01200608-Sep-2010NORMALROUTINE1730.05731573107-Sep-2010

kathleen.m.jungell23-May-2011NORMALROUTINE2064.06065606520-May-2011

kathleen.m.jungell17-Jun-2011NORMALROUTINE2064.06065606515-Jun-2011

kathleen.m.jungell06-Jan-2012NORMALROUTINE2425.06426642605-Jan-2012

kathleen.m.jungell17-Jul-2012ABNORMALROUTINE38.06762676213-Jul-2012

kathleen.m.jungell19-Jul-2012NORMALLAB REQUES42.06766676618-Jul-2012

kathleen.m.jungell23-Jul-2012NORMALOTHER0.06766676619-Jul-2012

kathleen.m.jungell11-Feb-2013ABNORMALROUTINE360.07126712610-Feb-2013

kathleen.m.jungell19-Feb-2013NORMALLAB REQUES0.07140714016-Feb-2013

stephanie.n.ziglar17-Oct-2013NORMALROUTINE340.07480748016-Oct-2013

anthony.s.speigner16-Dec-2013NORMALBASELINE0.07481748111-Dec-2013

frances.j.grace03-Jul-2014NORMALROUTINE364.07845784502-Jul-2014

chelsey.p.phillips10-Sep-2015ABNORMALBASELINE0.08199.88199.824-Aug-2015

theresa.d.pollard15-Sep-2015NORMALROUTINE13.78213.58213.512-Sep-2015

theresa.d.pollard27-Jun-2016ABNORMALROUTINE346.78560.28560.224-Jun-2016

theresa.d.pollard30-Jun-2016NORMALLAB REQUES3.48563.68563.630-Jun-2016

10 SEPT 15- CODE J: DRAIN & FLUSH SYSTEM. SUBMIT RESAMPLE AFTER 1ST FLIGHT CYCLE DUE TO WATER. CP762924AUG15- BASELINE, ROUTINE- POST 720 HOUR PHASE. CN419210-FEB 13- RESAMPLE AFTER NEXT FLIGHT CYCLE, USAACE FT RUCKER, AL

27-JUN-16- SAMPLE REQUEST #S373: WATER EXCEEDS PPM LIMIT. DRAIN AND FLUSH COMPONENT THEN RESAMPLE AT THE END OF THE NEXTDAY/CYCLE. (MJ026211).

27-JUN-16- DRAIN AND FLUSH COMPONENT THEN RESAMPLE AT THE END OF THE NEXT FLIGHT CYCLE/DAY. (MJ026211)

BASELINE-RESET ROUTINE POST PHASE13JUL 12 POST PHASE OILS

9. REMARKS:



0

360

8199.8

8524475 1399 0


EH-60A 856006 Days


HELICOPTER, UTILITY AUXILIARY POWER UNIT Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 1 of 1

a b

SUBMITTED

c a b



COMPONENTCHANGE

jimmy.s.caylor10-Nov-2014NORMALBASELINE0.01308796209-Nov-2014

theresa.d.pollard10-Sep-2015NORMALBASELINE0.0758199.824-Aug-2015

TP163427-Jun-2016NORMALROUTINE360.422368560.224-Jun-2016

24 AUG 15- BASELINE, ROUTINE, POST 720 HOUR PHASE. CN4192

9. REMARKS:



0

360

8560.2

8524475 6726.6 5972


EH-60A A00601066 Days


HELICOPTER, UTILITY TAIL ROTOR GEARBOX ASSY Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 1 of 1

a b

SUBMITTED

c a b



COMPONENTCHANGE

kathleen.m.jungell05-Apr-2011NORMALINITIAL0.03823597204-Apr-2011

kathleen.m.jungell22-Mar-2011NORMALROUTINE93.03916606520-May-2011

kathleen.m.jungell17-Jun-2011NORMALROUTINE0.03916606515-Jun-2011

kathleen.m.jungell06-Jan-2012NORMALROUTINE361.04277642605-Jan-2012

kathleen.m.jungell17-Jul-2012ABNORMALROUTINE0.04613676213-Jul-2012

kathleen.m.jungell19-Jul-2012NORMALLAB REQUES0.04617676618-Jul-2012

kathleen.m.jungell11-Feb-2013ABNORMALROUTINE360.04977712610-Feb-2013

kathleen.m.jungell19-Feb-2013NORMALLAB REQUES0.04991714016-Feb-2013

janice.m.bruce17-Oct-2013ABNORMALROUTINE340.05331748016-Oct-2013

anthony.s.speigner16-Dec-2013ABNORMALLAB REQUES0.05332748111-Dec-2013

anthony.s.speigner18-Dec-2013NORMALLAB REQUES11.05343749217-Dec-2013

anthony.s.speigner03-Jul-2014ABNORMALROUTINE364.05696784502-Jul-2014

frances.j.grace11-Jul-2014NORMALLAB REQUES368.05700784910-Jul-2014

TP163410-Sep-2015NORMALBASELINE0.06050.88199.824-Aug-2015

theresa.d.pollard27-Jun-2016ABNORMALROUTINE360.46411.28560.224-Jun-2016

TP 0163430-Jun-2016NORMALLAB REQUES3.46414.68563.630-Jun-2016

24 AUG 15- BASELINE, ROUTINE POST PHASE. CN4192LAB REQUEST CODE J

111-DEC-13- RESAMPLE AFTER NEXT FLIGHT CYCLE, USAACE FT RUCKER, AL13 OCT . 13- RESAMPLE AFTER NEXT FLIGHT CYCLE, USAACE FT RUCKER, AL

27 JUN- 16- ABNORMAL RESULTS WATER EXCEEDS PPM LIMIT; DRAIN ANS FLUSH COMPONENT THEN RESAMPLE AT THE END OF THE NEXT FLIGHTDAY/CYCLE(TP1634)

27-JUN-16-SAMPLE REQUEST #S374 WATERXCEEDS PPM LIMIT. DRAIN AND FLUSHNCOMPONENT THEN RESAMPLENAT THENEND OF THE NEXT DAY/CYCLE.(MJ026211).03JUL14, ABNORMAL RESULTS CU. CODE J DRAIN AND FLUSH RESAMPLE AFTER FIRST/NEXT FLIGHT CYCLE.11 FEB 13 - ABNORMAL RESULTS - REASON: AL, CU WEAR METAL CONTENT (CODE J - DRAIN & SVC) RESAMPLE AFT 30 MIN GRD RUN13 JUL 12 POST PHASE OILS

9. REMARKS:



REMARKS

INSTALLED IN UNSERVICEABLE CONDITION, LEAKING AT WEEP HOLE. ACFT 8524475, IS BEING TURNED IN TO THE BLACKHAWK EXCHANGE

PROGRAM.

APD LF v1.00DA FORM 2410, JAN 97, IS OBSOLETEDA FORM 2410, MCDS

COMPONENT REMOVAL / REPAIR / INSTALL / GAIN / LOSS RECORD

For use of this form, see DA PAM 738-751; the proponent agency is DCS, G-4

SECTION I - MAINTENANCE ACTION

SECTION II - IDENTIFICATION

INSTALL REMOVE REPAIR GAIN/LOSS

5. MII 6. CAGE CODE 7. LANDINGS 8. NO. OF PREV

O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE

4. SERIAL NUMBER3. PART NUMBER2. NSN1. NOMENCLATURE

21. VERSION

d. OP HOURSc. TTIb. LCF 2a. LCF 1

17. COMPONENT CUMULATIVE COUNT / HOURS16. CONFIG CODE13. METER HRS

18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H

SECTION III - NEXT HIGHER ASSEMBLY (NHA) INSTALL / REMOVE INFORMATION

X

24. NHA PART NUMBER23. NHA NSN22. NHA NOMENCLATURE

25. NHA SERIAL NUMBER 26. NHA HOURS 27. START METER 28. METER HRS

31. WHEN DISCOVERED30. MALFUNCTION CODE29. HISTORY RECORDER SN

32. HISTORY RECORDER READING 33. NHA CUMULATIVE COUNT / HOURS

SECTION IV - GAIN / LOSS / REPAIR / ADMIN INFORMATION

d. OP HRSc. TTIb. LCF 2a. LCF 1d. OP HRSc. TTIb. LCF 2a. LCF 1

44. DATE

47. LOST / SHIPPED TO 48. LOCATION

45. PID AND TELEPHONE NUMBER 46. AKO USER NAME

43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL

38. ACTUAL FAILURE CODE 39. MAINTENANCE LEVEL

MWO

RECAP

40. MANHOURS 41. SRA 42. UIC

37. NEW NSN36. NEW PART NUMBER35. GAIN OR

LOSS CODE

34. INSPECTION ACTION CODES

X

W0U91T 03-Apr-2017

03-Apr-2017 christ 334-503-3807

1 N W0U91TF

0 0 0 0 0 0 0 8876

8876 0 0

HELICOPTER, UTILITY 1520010820686 EH-60A

8524475

0 0 0 0 0

11D01 0 0

78286 0 0 2823 0 799

B3031433270410-02820-0541650011431226SERVO, PRIMARY MAIN ROTOR

2823

UNCLASSIFIED For Official use Only (FOUO)


REMARKS

INSTALLED IN UNSERVICEABLE CONDITION. LEAKING AT WEEP HOLE. ACFT 8524475 IS BEING TURNED IN TO THE BLACKHAWK EXCHANGE

PROGRAM.








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

W0U91T 03-Apr-2017

03-Apr-2017 christ 334-503-3807

1 N W0U91TF

0 0 0 0 0 0 0 8876

8876 0 0


8524475

0 0 0 0 0

11D01 0 0

78286 0 0 2823 0 799

B3031442370410-02820-0541650011431226SERVO, PRIMARY MAIN ROTOR

2823



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

26-Sep-1986

5 K78286D

1151 0 0 0 0

0


8524475

002 ~ ~

0 0 0

06H06

78286 0 0 0 0 799

A2710102870361-03001-0451615010812775SHAFT ASSY, T/R DRV SEC 1

0



REJECTED

RECORD

REMARKS

THIS M/R PRIMARY SERVO IS IN UNSERVICEABLE CONDITION, ACTUAL FAILURE CODE IS 381. LEAKING FROM HOUSING SEAM. ACFT 8524475 IS

BEING TURNED IN.








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

W0U91T 07-Apr-2017

07-Apr-2017 christ 334-503-3807

1 N W0U91TF

0 0 0 0 0 0 0 8876

8876 0 0


8524475

0 0 0 0 0

11D01 0 0

82106 0 0 3069 0 799

B30311137274000-10311650011431226SERVO, PRIMARY MAIN ROTOR

3069



PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN -


ACCESSORY MODULE 8524475A258-031241. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 14 of 24

21-Mar-2013 FM

jessica.n.kennedy23-Mar-2013

3.0USAACE, FT.RUCKER, AL

COMPLY WITH THE REQUIREMENTSOF H-60-13-ASAM-04(PMB) PLASTICMEDIA BLAST AND OXIDE FLAKERESIDUE

H-60-13-ASAM-04MWO:

Priority Mnt Level


EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991

PIDMWODATE HRS



ANTI-ICE VALVE 8524475COMH58611. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 19 of 24

22-Jun-2011 OM

tony.barnes23-Jun-2011

0.2USAACE, FT.RUCKER, AL.

ANTI-ICE / START BLEED VALVEACTUATOR SHAFTS

H-60-11-ASAM-11MWO:

Priority Mnt Level

05-Sep-2012 OM

kathleen.m.jungell 18-Sep-2012

0.3USAACE, FT.RUCKER, AL(AFS 77)

ALL UH-60A SERIES AIRCRAFTENGINE ANTI-ICE (AISBV)

H-60-12-ASAM-10MWO:

Priority Mnt Level



PIDMWODATE HRS



ANTI-ICE VALVE 8524475COMH110681. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 18 of 24

05-Sep-2012 OM

donna.k.moss14-Sep-2012


ALL UH-60A SERIES AIRCRAFTENGINE ANTI-ICE (AISBV)

H-60-12-ASAM-10MWO:

Priority Mnt Level



Inspection #

8875.68524475EH-60A

Till DueShelf LifeSerial NumberMFG DateLot #NarrativePart NumberDODIC

PROJECTEDDAYS: CURRENT HRS: Ser No.MDS:

Sorted By: Days to InspectionAUTOMATED CADS & PADS PROJECTIONSReport Date: Page 1 of 128-Apr-2017

5,000

MA630 222701-Oct-2010MSB10A001-007#1 MAIN FIRE BOTTLE1512AS105MH92 1768

MA633 22212401-Jan-2010MSB10A001-007#1 RESERVE FIRE BOTTLE1512AS105MH92 1768

MA638 22229901-Jan-2010MSB10A001-007#2 RESERVEFIRE BOTTLE1512AS105MH92 1768

MA640 22266701-Nov-2010MSB10L002-002#2 MAIN FIRE BOTTLE1512AS105MH92 1768

MA660 21662701-Jun-2006BRZ06F001-002CARGO THRUSTER1512AS120MJ20 -667

PIDMWODATE HRS



ENGINE ASSY, TURBINE 8524475GE-E-3073691. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 21 of 24

13-Jul-1989 DM

MB254126-Mar-2010

1.0WOMUAAMODIFICATION OF GAS GENERATORROTOR ASEMB. T700-700/701REWORK & REPLACE 33.0MANHOURS

MWO 55-2840-248-50-32MWO:

Priority Mnt Level

31-Jul-1989 OM

MB254126-Mar-2010

1.0WOMUAAMODIFICATION OF GG ROTORASSEMBLY T700/701 REWORK T700ENGINES

55-2840-248-50-32MWO:

Priority Mnt Level

30-Mar-1990 OM

MB254126-Mar-2010

1.0WOMUAAINSTALLATION OF POWER TAKEOFF ASSEMBLY

55-2840-248-50-29MWO:

Priority Mnt Level

25-Jan-1991 DN

MB254126-Mar-2010

1.0WOMUAAMODIFICATION OF POWER TAKEOFFDRIVE ASSEMBLY P/N 5044T27G01

55-2840-248-50-27MWO:

Priority Mnt Level

23-Sep-1993 DN

MB254126-Mar-2010

1.0WOMUAAINSTALATION OF SELF-SEALINGADAPTER ASSY

MWO 55-2840-50-28MWO:

Priority Mnt Level

30-Jun-1994 OR

MB254126-Mar-2010

1.0WOMUAAONE TIME INSPECTION ANDCONVERSION OF FORMS ANDRECORDS FOR T700-GE-700, -701AND -701C SERIES GAS TURBINEENGINES

1-2840-248-20-2MWO:

Priority Mnt Level

30-Jun-1994 OM

MB254126-Mar-2010

1.0WOMUAAONE TIME INSPECT/ CONERSION OFFORMS & RECORDS FORT700/701/701C ENGINES

TB 55-2840-20-02MWO:

Priority Mnt Level

10-Nov-1998 DM

0.0ONE TIME INSPECTION OF ALL T700-GE-700 ENGINE RECORDS

UH60-99-ASAM-03MWO:

Priority Mnt Level

15-Dec-1998 DM

MB254126-Mar-2010

1.0WOMUAANEW LIFE LIMITS ON G.G. ROTORAND COMPONENTS.

TB1-2840-248-20-22/UH-60MWO:

Priority Mnt Level

27-Aug-2007 DR

MB254126-Mar-2010

1.0WOMUAANEW LIFE LIMITS ON G.G ROTORAND COMPONENTS

TB 1-2840-20-22MWO:

Priority Mnt Level

jeanora.g.thompson 26-Mar-2010

1.0WOMUAAALL H-60 AND H-64 SERIESAIRCRAFT, SUSPECT ENGINEHARNESSES

H-64-08-ASAM-05MWO:



PIDMWODATE HRS




Page 22 of 24

22-Sep-2008 OM

Priority Mnt Level

22-Sep-2008 OM

MB254126-Mar-2010

1.0WOMUAAALL H-60 SERIES AIRCRAFT,SUSPECT ENGINE ELECTRICALHARNESSES.

UH-60-08-ASAM-14MWO:

Priority Mnt Level

30-Jul-2014 FM

vickie.l.meadows31-Jul-2014

2.0USAACE, FTRUCKER, AL

HYDRO-MECHANICAL UNIT QUICKDISCOUNT PINS

H-60-14-ASAM-08MWO:

Priority Mnt Level



PIDMWODATE HRS




Page 23 of 24

31-May-1994 OM

thomas.m.lilly16-Dec-1999

0.5ESRA FTCKY(T.GRODE)

LIFE LIMITS FOR T-700-GE-701 ANDT701 ENGINE COMPONENTS

1-2840-248-20-18MWO:

Priority Mnt Level

30-Jun-1994 OR



ONE TIME INSPECTION ANDCONVERSION OF FORMS ANDRECORDS FOR T700-GE-700, -701AND -701C SERIES GAS TURBINEENGINES

1-2840-248-20-2MWO:

Priority Mnt Level

02-Aug-1999 FM



ALL AH-64 AND UH-60 SERIESAIRCRAFT - ONE TIME INSPECTIONOF T700-GE-700/701/701C ENGINES


Priority Mnt Level

20-Dec-2007 OM

thomas.m.lilly05-Jan-2008

5.0USAAWC(RJ0827)

ALL H-60 AND ALL AH-64 SERIESAIRCRAFT, MIL-PRF-23699 HIGHTEMPERATURE STABILITY (HTS) OIL

H-60-08-AMAM-03MWO:

Priority Mnt Level

22-Sep-2008 OM

thomas.m.lilly27-Oct-2008

0.4USAACE(MB1137)

ALL H-60 AND H-64 SERIESAIRCRAFT, SUSPECT ENGINEHARNESSES

H-60-08-ASAM-14MWO:

Priority Mnt Level

12-Jan-2009 FM

thomas.m.lilly14-Jan-2009

0.1USAACE, FT.RUCKER, AL(KJ0605)

ALL H-60A/K/L AND AH-64 SERIESAIRCRAFT, T701C GAS GENERATOR(GG) ROTOR ASSEMBLIES

H-60-09-ASAM-01MWO:

Priority Mnt Level

01-Oct-2009 OM

thomas.m.lilly14-Oct-2009

0.3USAACE, FT.RUCKER, AL(KJ0605)

ALL H-60A AIRCRAFT, HAMILTON-SUNSTRAND HYDRO-MECHANICALUNITS

H-60-10-ASAM-01MWO:

Priority Mnt Level

30-Jul-2014 FM

anthony.s.speigner 31-Jul-2014

1.0USAACEHYDRO-MECHANICAL UNIT QUICKDISCOUNT PINS

H-60-14-ASAM-08MWO:

Priority Mnt Level



PIDMWODATE HRS



FAN AXIAL 85244754121. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 3 of 24

31-Dec-2004 DM

ET250807-Apr-2015

22.0CCAD, CORPUSCHRISTI, TX

AXIAL FAN: P/N 70361-03005-103,NSN 4140-01-138-6950; P/N 70361-03002-104, NSN 4140-01-158-9515,P/N 70361-03005-105, NSN 4140-01-089-0465, P/N 70361-03005-106, NSN4140-01-266-4519; P/N 70361-03005-107, NSN 4140-01-329-3428; P/N70361-03700-101, NSN 4140-01-266-4518

1-4140-228MWO:

Priority Mnt Level



PIDMWODATE HRS



FUEL CONTROL 8524475136911021. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 24

05-Sep-2012 OM

kathleen.m.jungell 12-Sep-2012

0.5USAACE, FT.RUCKER, AL(AFS 594)

ALL H-60A SERIES AIRCRAFT,HYDRO-MECHANICAL UNIT (HMU)

H-60-12-ASAM-11MWO:

Priority Mnt Level

19-Aug-2013 FN

tony.barnes21-Aug-2013

0.5USAACE FT.RUCKER, AL.

WOODWARD HYDRO-MECHANICALUNIT (HMU) P3 TUBE

H-60-13-ASAM10MWO:

Priority Mnt Level



PIDMWODATE HRS



FUEL CONTROL 8524475UDAJ12191. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 24 of 24

05-Sep-2012 OM

donna.k.moss10-Sep-2012


ALL UH-60A SERIES AIRCRAFT,HYDRO-MECHANICAL UNIT (HMU)

H-60-12-ASAM-11MWO:

Priority Mnt Level

19-Aug-2013 FM

tony.barnes23-Aug-2013

0.5USAACE FT.RUCKER, AL.

WOODWARD HYDRO-MECHANICALUNIT (HMU) P3 TUBE.

H-60-13-ASAM-10MWO:

Priority Mnt Level



PIDMWODATE HRS



HUB, M/R ROTOR ASSY 852447515152007971. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 2 of 24

30-Dec-2013 FN

anthony.s.speigner 04-Jan-2014

0.0USAACEINSPECTION OF MAIN ROTOR HUBASSEMBLY

H-60-14-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



INTERMEDIATE GEARBOX 8524475A005-012531. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 4 of 24

21-Mar-2013 FM

kathleen.m.jungell 27-Mar-2013


PLASTIC MEDIA BLAST (PMB) ANDOXIDE FLAKE RESIDUE

H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN TRANSMISSION 8524475A265013281. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 15 of 24

08-Jun-2002 OT

thomas.m.lilly25-Aug-2010

0.5USAACE, FT.RUCKER, AL(LW2720)

MAIN MODULE PLANETARYCARRIER ASSEMBLY (RAF), ALL UH-60A, EH-60A AND UH-60Q SERIESAIRCRAFT

UH-60-02-10MWO:

Priority Mnt Level

31-Oct-2002 DM

thomas.m.lilly11-Sep-2009

1.0CCAD (MP3634)MAIN GEARBOX MAIN MODULEASSEMBLY; P/N 70351-08100-053(NSN 1615-01-076-1260), P/N 70351-08100-054 (NSN 1615-01-105-1450),P/N 70351-08100-055 (NSN 1615-01-129-7330), P/N 70351-08100-056 (NSN1615-01-105-8713), P/N 70351-08100-057 (NSN 1615-01-134-7274), P/N70351-08100-058 (NSN 1615-01-128-1749), P/N 70351-08100-059 (NSN1615-01-145-3928), P/N 70351-08100-060 (NSN 1615-01-168-2983), P/N70351-08100-061 (NSN 1615-01-284-6419), P/N 70351-08100-062 (NSNPENDING), P/N 70351-08100-063(NSN PENDING), P/N 70351-08100-064 (NSN PENDING), P/N 70351-08100-065 (NSN PENDING), P/N 70351-08100-066 (NSN PENDING), P/N 70351-08100-067 (NSN PENDING), P/N70351-08100-068 (NSN PENDING),P/N 70351-08100-069 (NSN 1615-01-316-2658), P/N 70351-08100-070 (NSN1615-01-316-2659), P/N 70351-08100-071 (NSN 1615-01-375-5846), P/N70351-08100-072 (NSN 1615-01-375-5847), P/N 70351-08100-073, P/N70351-08100-074

1-1615-371MWO:

Priority Mnt Level

15-Feb-2003 OT



MAIN MODULE PLANETARYCARRIER ASSEMBLY RETIREMENTLIFE, ALL UH-60A, EH-60A AND UH-60Q SERIES AIRCRAFT

UH-60-03-03MWO:

Priority Mnt Level

22-May-2003 OT



REVISION TO UH-60-03-03 (TB 1-1520-237-20-264) MAIN MODULEPLANETARY CARRIER ASSEMBLYRETIREMENT LIFE, ALL UH-60A, EH-60A AND UH-60Q SERIES AIRCRAFT

UH-60-03-04MWO:

Priority Mnt Level

05-Oct-2009 OM



REDESIGNED PLANETARY GEARCARRIER RETIREMENT LIFE.(TB1027)

H-60-10-AMAM-02MWO:

Priority Mnt Level

21-Mar-2013 FM

jessica.n.kennedy23-Mar-2013



H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



SAS ACTUATOR 8524475C112-040131. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 17 of 24

23-Mar-2001 FT

mae.p.belford19-Jun-2007

1.0USAAWC, FT.RUCKER, AL.(MF4187)

ALL H-60 SERIES AIRCRAFT,INSPECTION OF ALL SASACTUATORS

UH-60-01-06MWO:

Priority Mnt Level



SECTION I COCKPITEH-60A_BASELINE

4. EQUIPMENT CHECKLIST

8524475 EH-60A

3. AREA NAME 2. MODEL 1. SERIAL NUMBER

Page 1 of 7

1RECEIVER RADIO - R-1496A/ARN-89

U UUUUUUUU UU1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER

QTY REQNOMENCLATURE:ITEM NO

2DISPLACEMENT GYRO - CN-1314/A (9000C)

U UUUUUUUU UU1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GYRO, DIRECTIONAL - CN-998/ASN-43

U UUUUUUUU UU0

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SIGNAL DATA CONVERTER - CV-3338A/ASN-128B

U UUUUUUUU UU1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING FOR KIT-1A/1C/TSEC - MT-3949A/U

U UUUUUUUU UU1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER - R-2139/ARN-123(V)

U UUUUUUUU UU1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING - MT-4834/ARN-123(V)

U UUUUUUUU UU1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMMAND INSTR SYS PROCESSOR - 70600-01038-101

U UUUUUUUU UU1

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING RACK - 70600-01038-102

U UUUUUUUU UU1

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SAS AMPLIFIER - 70901-02908-104

U UUUUUUUU UU1

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO ASSEMBLY - 70600-01047-041

U UUUUUUUU UU1

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO - TRU-2A/A

U UUUUUUUU UU1

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3MOUNT FOR TSEC/KY58 - S1660-60036-001

U UUUUUUUU UU3

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3BATTERY FOR KY 58 - BA-1372/U

U UUUUUUUU UU0

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3INTERFACE ADAPTER (KY-58) - Z-AHQ/TSEC

U UUUUUUUU UU0

15

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, NOV 1991



8524475 EH-60A


Page 2 of 7

3REMOTE CONTROL UNIT (KY-58) - Z-AHP/YSEC

U UUUUUUUU UU0

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1AMPLIFIER IMPEDANCE - AM-4859A/ARN-89

U UUUUUUUU UU1

17

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#2 VHF-FM ANTENNA COUPLER - 70600-01010-104

U UUUUUUUU UU0

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1VHF/AM ANTENNA FILTER - 70600-01012-102

U UUUUUUUU UU1

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2VHF/AM ANTENNA FILTER - 70600-01011-103

U UUUUUUUU UU2

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2ANTENNA - AS-3831/APN-209(V)

U UUUUUUUU UU2

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GLIDE SLOPE ANTENNA - 70600-01043-101

U UUUUUUUU UU1

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#2 VHF-FM, VHF-AM SENSE ANTENNA - 70600-01019-104

U UUUUUUUU UU1

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2FIRST AID KIT - 6545-00-919-6650

U UUUUUUUU UU0

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRE EXTINGUISHER - FR23-4-11848

U UUUUUUUU UU0

25

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2BAROMETERIC ALTIMETER - AAU-32/A

U UUUUUUUU UU2

26

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2CREW SEAT - D3801-2

U UUUUUUUU UU3

27

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2AIRCRAFT CLOCK - ABU-11A

U UUUUUUUU UU2

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER/TRANSMITTER - RT-1477/ARC-201

U UUUUUUUU UU0

29

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2INTERPHONE CONTROL - C6533/ARC

U UUUUUUUU UU2

30

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8524475 EH-60A


Page 3 of 7

1RECEIVER/TRANSMITTER - RT-1115D/APN-209

U UUUUUUUU UU1

31

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1INDICATOR ALTIMETER - ID-1917C/APN-209

U UUUUUUUU UU1

32

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL RADIO SET - C-7392/ARN-89

U UUUUUUUU UU1

33

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL - C-10604(V)6/ARN-186

U UUUUUUUU UU0

34

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL - C-11466A/ARC-201

U UUUUUUUU UU0

35

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPARATOR SIGNAL DATA - CM482/ARC186(V)

U UUUUUUUU UU1

36

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3MOUNT - MT-6051/ARC-186

U UUUUUUUU UU3

37

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER/TRANSMITTER - RT-1296A/APX-100

U UUUUUUUU UU1

38

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CIVIL NAVIGATION CONTROL - C-10048/ARN-123(V)

U UUUUUUUU UU1

39

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS SET CONTROLLER - C-8021E/ASN-75

U UUUUUUUU UU1

40

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RADIO RETRANSMISSION PANEL -70550-01008-042

U UUUUUUUU UU1

41

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MAGNETIC COMPASS - MS17983-4

U UUUUUUUU UU1

42

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2OUTSIDE AIR TEMP INDICATOR - MS28028-1

U UUUUUUUU UU2

43

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOUR WING PANEL - 70500-01152-093

U UUUUUUUU UU0

44

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOUR WING PANEL - 70500-01152-094

U UUUUUUUU UU0

45

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8524475 EH-60A


Page 4 of 7

1STABILATOR/FLT CONT PNL - 70902-01070-048

U UUUUUUUU UU1

46

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL-INDICATOR ASN-132 C-11097/ASN-132

U UUUUUUUU UU0

47

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SIGNAL DATA CONVERTER ASN-132CV-3739/ASN-132

U UUUUUUUU UU0

48

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT FOR ASN-132 MT-4915/A

U UUUUUUUU UU0

49

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1DATA PROCESS SET AN/UYK-64(V)2

U UUUUUUUU UU0

50

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1TACAN RECEIVER/TRANSMITTER RT-1159/A

U UUUUUUUU UU0

51

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ELECTRONIC SEQUENCE UNIT, 163290-100-E

U UUUUUUUU UU1

52

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RADAR DETECTION SET SIGNAL AN/APR39

U UUUUUUUU UU0

53

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IR JAMMER COUNTERMEASURES SET AN/ALQ-144(V)

U UUUUUUUU UU0

54

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1DISPENSER GENERAL PURPOSE AIRCRAFT M130

U UUUUUUUU UU0

55

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3SECURE SPEECH UNIT TSEC/KY-58

U UUUUUUUU UU0

56

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3CONTROL INDICATOR (KY-58) C-8157/ARC

U UUUUUUUU UU0

57

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1KY-100 AIRTERM 0N616736-1

U UUUUUUUU UU0

58

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL DISPLAY UNIT C-12346/URC

U UUUUUUUU UU0

59

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER




of 7SERIAL NUMBER MODEL AREA NAME

8524475 EH-60A_BASELIN SECTION I COCKPITEH-60A

NAME OR PIDNUMBER DATE

db c

DATE NUMBER RANKRANK NAME OR PID

CHECK CHECK

ba ad

5. VERIFICATION

c

michael.t.woo1 CIV 01-May-2017

b. LOCATION/REMARKSCHECK NO.

6. LOCATION OR REMARKS

a. ITEM NUMBER

Nomenclature

DISPLACEMENT GYRO - CN-1314/A (9000C)

1 ACFT ARRIVED IN THIS CONFIGURATION2

GYRO, DIRECTIONAL - CN-998/ASN-43


BATTERY FOR KY 58 - BA-1372/U


INTERFACE ADAPTER (KY-58)- Z-AHQ/TSEC


REMOTE CONTROL UNIT (KY-58) - Z-AHP/YSEC


#2 VHF-FM ANTENNACOUPLER - 70600-01010-104


FIRST AID KIT - 6545-00-919-6650


FIRE EXTINGUISHER - FR23-4-11848


CREW SEAT - D3801-21 ACFT ARRIVED IN THIS CONFIGURATION27

RECEIVER/TRANSMITTER - RT-1477/ARC-201


REVERSE OF DA FORM 2408-17, NOV 1991




db c


CHECK CHECK

ba ad

5. VERIFICATION

c


CONTROL - C-10604(V)6/ARN-186


CONTROL - C-11466A/ARC-2011 ACFT ARRIVED IN THIS CONFIGURATION35

ARMOUR WING PANEL - 70500-01152-093


ARMOUR WING PANEL - 70500-01152-094


CONTROL-INDICATOR ASN-132 C-11097/ASN-132


SIGNAL DATA CONVERTERASN-132CV-3739/ASN-132


MOUNT FOR ASN-132 MT-4915/A


DATA PROCESS SET AN/UYK-64(V)2


TACANRECEIVER/TRANSMITTER RT-1159/A


RADAR DETECTION SETSIGNAL AN/APR39


IR JAMMERCOUNTERMEASURES SETAN/ALQ-144(V)






db c


CHECK CHECK

ba ad

5. VERIFICATION

c


DISPENSER GENERALPURPOSE AIRCRAFT M130


SECURE SPEECH UNITTSEC/KY-58


CONTROL INDICATOR (KY-58)C-8157/ARC


KY-100 AIRTERM 0N616736-11 ACFT ARRIVED IN THIS CONFIGURATION58

CONTROL DISPLAY UNIT C-12346/URC



SECTION II CABINEH-60A_BASELINE


8524475 EH-60A


Page 1 of 5

1INERTIAL NAVIGATION SET - AN/ASN-141

U UUUUUUUU UU0

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BEARING, DISTANCE, HEADING INDICATOR - ID2301/U

U UUUUUUUU UU0

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MARKER BEACON ANTENNA - 70600-02011-103

U UUUUUUUU UU1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-104

U UUUUUUUU UU1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-105

U UUUUUUUU UU1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRST AID KIT - 6545-00919-6650

U UUUUUUUU UU0

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRE EXTINGUISHER - FR23-4-11848

U UUUUUUUU UU0

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CRASH AXE - 56D6221

U UUUUUUUU UU1

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HAND SET - H-250/U

U UUUUUUUU UU1

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SLAB BATTERY - D8565/11-1

U UUUUUUUU UU1

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1INTERPHONE CONTROL - C6533/ARC

U UUUUUUUU UU3

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ADAPTER FUEL DRAIN - 70307-03018-102

U UUUUUUUU UU0

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


4LOCK ASSY BLADE TIEDOWN - 70700-20369-041

U UUUUUUUU UU0

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2PLUG ASSY INTAKE - HIRSS SUPP - 70700-20515-041/042

U UUUUUUUU UU0

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2PLUG ASSY EXHAUST - HIRSS - 70700-20515-043

U UUUUUUUU UU0

15

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER




SECTION II CABINEH-60A_BASELINE


8524475 EH-60A


Page 2 of 5

1PLUG ASSY APU EXHAUST - 70700-20509-041

U UUUUUUUU UU0

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER ASSY OIL COOLER - 70700-20511-041

U UUUUUUUU UU0

17

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BLADE FOLD SET - 70700-20412-011

U UUUUUUUU UU0

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER PITOT TUBE - 70700-20460-041

U UUUUUUUU UU0

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1TROOP SEATS - 70500-02151-045

U UUUUUUUU UU0

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER ENGINE INLET - 83DSCC-D006

U UUUUUUUU UU0

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FITTING ASSEMBLY - L/H - 70751-02023-043

U UUUUUUUU UU0

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FITTING ASSEMBLY - R/H - 70751-02023-044

U UUUUUUUU UU0

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ICS WALK-AROUND CORD - 70602-02023-044

U UUUUUUUU UU0

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PORTABLE INSP. FLOOD LIGHT - 15-0366-1

U UUUUUUUU UU0

25

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HYD. PUMP HANDLE - 15400-50126

U UUUUUUUU UU1

26

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2EQUIPMENT LOGBOOK - MIL-D-43064

U UUUUUUUU UU1

27

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPUTER LOGBOOK

U UUUUUUUU UU1

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1WEIGHT AND BALANCE HANDBOOK - TM 55-1500-342-23

U UUUUUUUU UU1

29

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


4TIEDOWN ASSEMBLY, TOW - 70700-20433-045

U UUUUUUUU UU0

30

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8524475 EH-60A_BASELIN SECTION II CABINEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c




a. ITEM NUMBER

Nomenclature

INERTIAL NAVIGATION SET -AN/ASN-141


BEARING, DISTANCE,HEADING INDICATOR -ID2301/U


FIRST AID KIT - 6545-00919-6650


FIRE EXTINGUISHER - FR23-4-11848


INTERPHONE CONTROL -C6533/ARC


ADAPTER FUEL DRAIN - 70307-03018-102


LOCK ASSY BLADE TIEDOWN- 70700-20369-041


PLUG ASSY INTAKE - HIRSSSUPP - 70700-20515-041/042


PLUG ASSY EXHAUST - HIRSS- 70700-20515-043


PLUG ASSY APU EXHAUST -70700-20509-041






db c


CHECK CHECK

ba ad

5. VERIFICATION

c


COVER ASSY OIL COOLER -70700-20511-041


BLADE FOLD SET - 70700-20412-011


COVER PITOT TUBE - 70700-20460-041


TROOP SEATS - 70500-02151-045


COVER ENGINE INLET -83DSCC-D006


FITTING ASSEMBLY - L/H -70751-02023-043


FITTING ASSEMBLY - R/H -70751-02023-044


ICS WALK-AROUND CORD -70602-02023-044


PORTABLE INSP. FLOODLIGHT - 15-0366-1


EQUIPMENT LOGBOOK - MIL-D-43064


TIEDOWN ASSEMBLY, TOW -70700-20433-045






db c


CHECK CHECK

ba ad

5. VERIFICATION

c



SECTION III TRANSITION SECTIONEH-60A_BASELINE


8524475 EH-60A


Page 1 of 2

1ANTENNA, LOOP - AS-2108A/ARN-89

U UUUUUUUU UU1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2IFF ANTENNA - 70600-02010-103

U UUUUUUUU UU2

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF/AM ANTENNA 70600-03002-104

U UUUUUUUU UU1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PUMP FUEL SAMPLER - 82829/4P156-3

U UUUUUUUU UU0

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPENSATOR MAGNETIC FLUX - CN-405/ASN

U UUUUUUUU UU1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS TRANSMITTER - T-611/ASN

U UUUUUUUU UU1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GPS ANTENNA 22433-40

U UUUUUUUU UU1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF AMPLIFIER COUPLER AM-7531/URC

U UUUUUUUU UU0

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER/TRANSMITTER RT-1749/URC

U UUUUUUUU UU0

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8524475 EH-60A_BASELIN SECTION III TRANSITION SECTIONEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c




a. ITEM NUMBER

Nomenclature

PUMP FUEL SAMPLER -82829/4P156-3


HF AMPLIFIER COUPLER AM-7531/URC


RECEIVER/TRANSMITTER RT-1749/URC



SECTION IV TAIL CONEEH-60A_BASELINE


8524475 EH-60A


Page 1 of 2

2VOR/LOC ANTENNA - 70600-05002-101

U UUUUUUUU UU2

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF ANTENNA 4700516-30

U UUUUUUUU UU0

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8524475 EH-60A_BASELIN SECTION IV TAIL CONEEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c




a. ITEM NUMBER

Nomenclature

HF ANTENNA 4700516-301 ACFT ARRIVED IN THIS CONFIGURATION2


SECTION V TAIL ROTOR PYLONEH-60A_BASELINE


8524475 EH-60A


Page 1 of 2

1TROOP COMMANDER ANTENNA - 70600-06001-104

U UUUUUUUU UU1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#1 VHF-FM ANTENNA - 70600-06002-105

U UUUUUUUU UU1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8524475 EH-60A_BASELIN SECTION V TAIL ROTOR PYLONEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c




a. ITEM NUMBER

Nomenclature


PIDMWODATE HRS



SERVO ASSY, TAIL ROTOR 8524475C300069121. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

16-May-2016 FM

michael.t.wood04-May-2017

0.1SESITAIL ROTOR SERVO SAFETY CABLENOT COMPLIED WITH

H-60-16-AMAM-07MWO:

Priority Mnt Level



PIDMWODATE HRS



STABILATOR ACTUATOR 8524475B292-U07541. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 16 of 24

05-Sep-2013 DT

dean.a.keirn05-Sep-2013

4.0USAACE, AMSS,FT. RUCKER, AL.

MEC F171703, Authorization forjackscrew, and nut tube assembly to bereturned to service if assembly passesthe STATED inspection criteria (REF.DMWR 1-1680-332, dated 31 October2002, Sheet 1, Page 3-12). TSN: 1782.

MEC F171703MWO:

Priority Mnt Level



PIDMWODATE HRS



SWASHPLATE ASSY 8524475A107-010811. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 12 of 24

02-Dec-1996 OT

thomas.m.lilly05-Apr-1996

0.5D-CO 2-1 AVNAPO AE 09250(SH6210)

REMOVAL OF CERTAIN REWORKEDMAIN ROTOR SWASHPLATEASSEMBLIES, ALL UH-60A, UH-60L,EM-60A, AND MH-60K HELICOPTERS

UH-60-97-01MWO:

Priority Mnt Level

08-Sep-1997 OM


1.0USAAVNC, FT.RUCKER, AL(MF4187)

ALL UH-60A, UH-60L, EH-60A,REMOVAL OF SPECIFIC SUSPECTREWORKED MAIN ROTORSWASHPLATE ASSEMBLIES


Priority Mnt Level

30-Oct-1997 OM

thomas.m.lilly15-May-1998

0.1D-CO 2-1 AVNAPO AE 09250(MW3045)

ALL H-60 AIRCRAFT WITH THESWASHPLATE LINK ASSEMBLY, P/N70400-08110-054, MANUFACTUREDBY TEK (CAGE CODE 65780)


Priority Mnt Level

12-Jun-2006 OM

thomas.m.lilly12-Jun-2006

2.0USAAWC, FT.RUCKER, AL(MF4187)

ALL H-60 SERIES AIRCRAFT,SWASHPLATE DUPLEX BEARING


Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR GEARBOX ASSY 8524475A006010661. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 5 of 24

21-Mar-2013 FM

kathleen.m.jungell 27-Mar-2013



H-60-13-ASAM-04MWO:

Priority Mnt Level



REMARKS

THIS T/R PITCH CHANGE SHAFT IS IN UNSERVICEABLE CONDITION, HAS 2 EA BUSHINGS DAMAGED BEYOND LIMITS. ACFT 8524475 IS BEING TURNED

IN.








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H








44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

W0U91T 07-Apr-2017

07-Apr-2017 CHRIST 334-503-3807

2 N W0U91TF

0 0 0 0 0 0 0 8876

8876 0 0


8524475

0 0 0 0 0

11C23 0 0

65780 2 0 2285 1048 710

2330294270400-06100-0421615011417532T/R PITCH CHANGE SHAFT

2285



UNIT UNIQUE INVENTORY ITEMSEH-60A_BASELINE


8524475 EH-60A


Page 1 of 2

1IFM APMLIFIER AM-7189A/ARC

U UUUUUUUU UU1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2ATTITUDE AND HEADING REFERENCE UNIT (CN1716/A)

U UUUUUUUU UU1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT IFM AMP PN: MT-6592/ARC

U UUUUUUUU UU1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BFT ANTENNA GPS PN: S671575-863

U UUUUUUUU UU1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BFT ANTENNA L-BAND PN: S65-8282-301

U UUUUUUUU UU1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


0IGNITION KEYS

U UUUUUUUU UU2

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BFT PALLET ASSY PN: 080094-1

U UUUUUUUU UU 0

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8524475 EH-60A_BASELIN UNIT UNIQUE INVENTORY ITEMSEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c




a. ITEM NUMBER

Nomenclature

IFM APMLIFIER AM-7189A/ARC1 ACFT ARRIVED IN THIS CONFIGURATION1

ATTITUDE AND HEADINGREFERENCE UNIT (CN1716/A)


IGNITION KEYS1 ACFT ARRIVED IN THIS CONFIGURATION6

BFT PALLET ASSY PN: 080094-1



1. NOMENCLATURE 2. MODEL 3. AIRCRAFT SERIAL ... UTILITY EH-60A 8524475 1. NOMENCLATURE 2. MODEL 3....

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Transcript of 1. NOMENCLATURE 2. MODEL 3. AIRCRAFT SERIAL ... UTILITY EH-60A 8524475 1. NOMENCLATURE 2. MODEL 3....