1. nomenclature 2. model 3. aircraft serial ... utility eh-60a 8524475 1. nomenclature 2. model 3....
TRANSCRIPT
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
8524475EH-60AHELICOPTER, UTILITY
3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE
Page 1 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
DYNCORP-E(PCW/JH5095)
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
DATEORAPPLYINGMWO TITLEAND MAN
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
8524475EH-60AHELICOPTER, UTILITY
3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE
Page 2 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
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
DATEORAPPLYINGMWO TITLEAND MAN
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
8524475EH-60AHELICOPTER, UTILITY
3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE
Page 3 of 3
DM22-Feb-1991
DYNCORP-E(PCW/JH5095)
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
DYNCORP-E(PCW/JH5095)
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
DYNCORP-E(PCW/JH5095)
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
DYNCORP-E(PCW/JH5095)
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
DA FORM 2408-5, AUG 2004 EQUIPMENT MODIFICATION RECORD
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
KATTERBACK GE APOAE 09250
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
KATTERBACK GE APOAE 09250
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
KATTERBACK GE APOAE 09250
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
KATTERBACK GE APOAE 09250
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
KATTERBACK GE APOAE 09250
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
KATTERBACK GE APOAE 09250
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
KATTERBACK GE APOAE 09250
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
KATTERBACK GE APOAE 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 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
KATTERBACK GE APOAE 09250
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
KATTERBACK GE APOAE 09250
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
KATTERBACK GE APOAE 09250
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
KATTERBACK GE APOAE 09250
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
KATTERBACK GE APOAE 09250
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
KATTERBACK GE APOAE 09250
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
KATTERBACK GE APOAE 09250
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
KATTERBACK GE APOAE 09250
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
KATTERBACK GE APOAE 09250
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
KATTERBACK GE APOAE 09250
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
KATTERBACK GE APOAE 09250
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
AMCO PROJECT OLREAST
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
AMCO PROJECT OLREAST
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
AMCO PROJECT OLREAST
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 25 of 61
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEH-60-11-ASAM-06 (CYCLIC STICK STOP BOLTS)C/W @ 5971.6 ACFT HRS (AFS 40)
03-Apr-2011 3
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEDELAYED ENTRY: ACFT INDUCTED INTO ULLS-A(E) ON 17 MAR 11 AT 5945.8 ACFT HRS.
06-Apr-2011 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
bryan.w.hollis
USAACEH-60-11-ASAM-06 (CYCLIC STICK STOP BOLTS)C/W @ 6064.85 ACFT HRS.
13-Jun-2011 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
tony.barnes
USAACE720 HR PMI #10 COMPLETED @ 6064.8 ACFTHRS. NEXT PMI #11 DUE @ 6784.8 ACFT HRS.
17-Jun-2011 2
LOWE AHP, FT.RUCKER, AL.
bryan.w.hollis
USAACET/R CABLE TENSION CK COMPLETED @6074.0 ACFT HRS. RH: 145 LH: 150 TEMP -31
22-Jun-2011 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEACFT OPERATING IAW AWR 1639 (R-3) DTD 01JUN 11 (BFT/EDM) @ 6079.0 ACFT HRS.
01-Jul-2011 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEH-60-11-SOF-01 (DISCREPANT SELF LOCKINGDOUBLE HEXAGON NUTS) COMP THIS DATE@ 6096.1 (AFS 37)
09-Jul-2011 2
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEH-60-11-ASAM-14 (ENGINE COWLING REPAIRRESTRICTIONS) C/W THIS DATE @ 6128.5ACFT HRS. (AFS 545)
22-Jul-2011 2
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
janice.m.bruce
USAACEH-60-12-SOF-01 - TAIL ROTOR INTERMEDIATEGEARBOX COMPLETED AT 6307.2 ACFT HRSAS PER FORM 730
08-Oct-2011 1
LOWE AHP, FT.RUCKER, AL.
olivia.d.williams
USAACEH-60-12-SOF-02 (TAIL ROTOR INTERMEDIATEGEARBOX) C/W AT 6307.2 ACFT HRS.
10-Oct-2011 1
LOWE AHP, FT.RUCKER, AL.
debra.r.chancellor
USAACEH-60-12-SOF-03 (TAIL ROTOR INTERMEDIATEGEARBOX) C/W AT 6322.3 ACFT HRS. (AFS472).
14-Oct-2011 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEH-60-11-AMAM-19 (IMMC LCF CHG 62REQUIREMENTS )C/W @ 6339.7 ACFT HRS
22-Oct-2011 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEACFT OPERATING IAW AWR 1505 (R-4) DTD 21OCT 11 (5-MICRON METAL MESH HYD FILTER)
22-Oct-2011 3
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEACFT NO LONGER OPERATING IAW AWR 1529(R-1) DTD 07 OCT 10 (SUPERCEDED)
28-Oct-2011 1
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEACFT OPERATING IAW AWR 1529 (R-2) DTD 07OCT 11 @ 6348.8 ACFT HRS.
28-Oct-2011 2
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEH-60-11-AMAM-17 (TR INBOARD/OUTBOARDRETENTION PLATE SHIMS) COMP @ 6416.9ACFT HRS. (AFS 528)
07-Dec-2011 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEBFT EDM ROUTER 3.1 UPGRADE COMPLETED@ 6416.9 ACFT HRS.
21-Dec-2011 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACESPECIAL INSPECTION OF CABIN CONTROLROD ENDS COMP @ 6521.6 ACFT HRS NOFAULTS FOUND.
26-Feb-2012 1
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEACFT OPERATING IAW AWR 1251 (R-4) DTD 22FEB 12 (BIFILIAR EYEBOLTS) - SUPERSEDESAWR 1251 (R-3)
27-Feb-2012 1
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEACFT OPERATING UNDER AWR 1251, R4 DTD22FEB12, EYEBOLTS ON BIFILAR ARMS,SUPERSEDING 1251 R3.
27-Feb-2012 2
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEACFT OPERATING UNDER AWR 1648, R1 DTD26MAY10, MAGNUS LAPTOP.
28-Feb-2012 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEACFT OPERATING IAW AWR 1648, R2 DTD09MAR12, MAGNUS LAPTOPS, SUPERSEDINGR1.
20-Mar-2012 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEAWR 1750: ACFT OPERATING IAW AWR 1750,R1 DTD 27MAR12, AN/AVS-6 SERIES NVG.
03-Apr-2012 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEAWR 1681: ACFT OPERATING IAW AWR 1681,R3 DTD 04MAY12, EH60 DE-MOD,SUPERSEDING REV 2.
08-May-2012 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
L-3 RASM-EOCM/ ACE PERFORMED AT 6723.8 AIRCRAFTHOURS BY TEAM MEMBERS QQ AND P
17-May-2012 1
LOWE AHP, FT.RUCKER, AL.
jacob.a.weikart
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 41 of 61
USAACEMAIN MOD (A265-01113) FILTER BUTTONPOPPED @ 6742.1 ACFT H RS . REPLACEDFILTERS.
24-May-2012 1
LOWE AHP, FT.RUCKER, AL.
janice.m.bruce
USAACEAWR 1220: ACFT OPERATING IAW AWR 1220,R6 DTD 25MAY12, ENHANCED SCHEDULEDMAINTENANCE. SUPERSEDING REV 5.
25-May-2012 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEAWR 1515: ACFT OPERATING IAW AWR 1515,R2 DTD 07JUN12, TRC MEMS RATEGYROSCOPES, SUPERSEDING REVISION 1.
14-Jun-2012 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEACFT DATE OF MANUFACTURE IS AUG 1986 18-Jun-2012 1
LOWE AHP, FT.RUCKER, AL.
vickie.l.meadows
USAACEMEC F148226, AUTHORIZATION GRANTED TOUSE LOCALLY FABRICATED TOOLS TOREPLACE THE UPPER ACT AIRFRAME FITTINGBEARING.
22-Jun-2012 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEMEC F148491, AUTHORIZATION GRANTED TOREPAIR TRANSITION COWLING VOID. 6761.6ACFT HRS.
26-Jun-2012 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
rhonda.e.jackson
USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-09 AT 6761.3 ACFT HRS. (AFS 14)
09-Jul-2012 3
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
rhonda.e.jackson
USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-12-AMAM-09 HYDRAULIC LINE CHAFE @6761.5
09-Jul-2012 5
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
rhonda.e.jackson
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 42 of 61
USAACEH-60-12-AMAM-12 (RESCINDED COMMONCOMPONENT REMOVAL DATE) COMP @ 6765.6ACFT HRS. (AFS594)
17-Jul-2012 2
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEH-60-12-ASAM-08 (CARGO HOOK MANUALRELEASE SPRING ASSY) COMP @ 6766.3ACFT HRS (AFS 457)
19-Jul-2012 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEAWR 1220: ACFT OPERATING IAW AWR 1220,R7 DTD 31JUL12, ESM, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.
01-Aug-2012 2
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACET/R CABLE TENSION COMP @ 6780.5 LH: 133RH: 13133 @ 226.9 ° C (PASSED)
01-Aug-2012 3
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEAWR 1251: ACFT OPERATING IAW AWR 1251,R5 DTD 31AUG12, EYEBOLTS, SUPERSEDINGANY PRIOR REVISIONS OF THIS AWR.
31-Aug-2012 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
FT. RUCKER, ALH-60-12-AMAM-15 (TRIM ACTUATORS) COMP @6877.4 ACFT HRS. (AFS 594)
17-Sep-2012 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-12-ASAM-07, ELECTRICAL WIRE CHAFE, ONTHIS DATE.
03-Oct-2012 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEH-60-12-ASAM-07 (ELECTRICAL WIRE CHAFE)COMP @ 6929.0 ACFT HRS. (AFS 121 )
04-Oct-2012 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEH-60-13-AMAM-02 (AHRS) WIRING COMP/PASS@ 7001.6 ACFT HRS. (AFS 594)
07-Nov-2012 1
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEH-60-13-ASAM-01 (ANTI-COLLISION LIGHTSPOWER SUPPLY) INSP COMP (PASS) @ 7027.3ACFT HRS. (AFS 42)
28-Nov-2012 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEINSP A470 - REPLACE NUMBER TWOCROSSFEED VALVE COMP @ 7067 ACFT HRS.
12-Dec-2012 2
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEH-60-13-AMAM-04 (ULLS-AE LCF CHANGE 63REQUIREMENTS) COMP @ 7075.2 ACFT RHS.(AFS 594)
10-Jan-2013 2
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEH-60-13-AMAM-05 (MLG BRAKES) COMP @7103.8 ACFT HRS. (AFS 576)
20-Jan-2013 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEM/R RIG COMP @ 7124.2 ACFT HRS. PRIMARYSERVO CONTROL ROD BIAS: NOADJUSTMENTS MADE.
03-Feb-2013 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEH-60-13-AMAM-06 (CEFS) NA @ 7129.1 ACFTHRS. CEFS NOT INSTALLED (AFS 472)
13-Feb-2013 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEH-60-13-ASAM-03 (M/R SPINDLE ANTI-FLAPASSEMBLIES) C/W @ 7169.9 ACFT HRS. (AFS410)
02-Mar-2013 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEH-60-13-AMAM-07 (LOAD DEMAND SPINDLECABLE CLEARANCE) C/W @ 7213.3 (AFS 594)
01-Apr-2013 1
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEH-60-13-ASAM-05 (ELECTRIC RESCUE HOIST)CW @ 7213.3 ACFT HRS. (AFS 121)
08-Apr-2013 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 46 of 61
USAACEH-60-13-ASAM-06 (PMI CHECKLIST CHANGES)C/W @ 7249.6 ACFT HRS. (AFS 76)
10-May-2013 1
LOWE AHP, FT.RUCKER, AL.
tony.barnes
USAACEH-60-13-SOF-01 WAS C/W AT 7279.9 ACFT HRS 31-May-2013 1
LOWE AHP, FT.RUCKER, AL.
rhonda.e.jackson
L-3 RASM-EOCM/ACE PERFORMED AT 7320.1 AIRCRAFTHOURS BY TEAM MEMBERS P AND QQ
21-Jun-2013 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
rhonda.e.jackson
USAACEH-60-13-AMAM-01 (FLIGHT CONTROL RIGGINGPROCEDURES) C/W AT 7320.1 ACFT HRS.
27-Jun-2013 4
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
rhonda.e.jackson
USAACEGEN-13-AMAM-04 AN/APN-209 RADARALTIMETER SET COMPONENT TRACKINGCOMPLETED AT 7330.3 ACFT HRS.
31-Jul-2013 2
LOWE AHP, FT.RUCKER, AL.
rhonda.e.jackson
USAACEAWR 1251: ACFT OPERATING IAW AWR 1251,R7 DTD 28AUG13, EYEBOLTS, SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR.
29-Aug-2013 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACECOMPLED WITH REQUIREMENTS OF H-60-13-AMAM-10 (LCF CHANGE 64) @ 7415 ACFT.HRS.
07-Sep-2013 1
LOWE AHP, FT.RUCKER, AL.
stephanie.n.ziglar
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEMEC F174620, AUTHORIZATION GRANTED TOREPAIR VOID IN RH ESSS PLATFORM PANEL.7480.6 ACFT HRS.
01-Nov-2013 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEMEC F174619, AUTHORIZATION GRANTED TOREPAIR VOID IN LH ESSS PLATFORM PANEL.7480.6 ACFT HRS.
01-Nov-2013 2
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEMEC F174613, AUTHORIZATION GRANTED TOREPAIR VOID IN RH OIL COOLER ACCESSDOOR. 7480.6 ACFT HRS.
01-Nov-2013 3
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEMEC F174611, AUTHORIZATION GRANTED TOREPAIR VOID IN LH OIL COOLER ACCESSDOOR. 7480.6 ACFT HRS.
01-Nov-2013 4
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
USAACEMEC F174917, AUTHORIZATION GRANTED TOREPAIR VOID IN FWD SLIDING PYLON. 7480.6ACFT HRS.
07-Nov-2013 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEMEC F174985, Authorization granted to uselocally fabricated tool to replacebearing/bushing in upper actutator fitting.
07-Nov-2013 2
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
USAACEMAIN ROTOR RIG COMPLETED AT 7481.6 ACFTHRS. FWD: NO ADJUSTMENT, AFT:: NOADJUSTMENT LAT: NO ADJUSTMENT.
22-Nov-2013 2
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEAWR 1444: ACFT OPERATING IAW AWR 1444,R6 DTD 11JUL13, SINGLE AHRS.
18-Dec-2013 2
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEH-60-14-AMAM-05 LEGITIMATE CODE FILECHANGE 65 REQUIREMENTS COMPLETED AT7680.4 ACFT HRS.
05-Apr-2014 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACEH-60-14-AMAM-12 MAIN ROTOR SPINDLE NUTRETIREMENT LIFE COMPLIED WITH
29-Apr-2014 1
LOWE AHP, FT.RUCKER, AL.
mark.a.trehern
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEH-60-14-AMAM-14 (IVHMS CABLING)REQUIREMENTS COMPLETED AT 7759.6 ACFTHRS (MWO NOT APPLIED)
28-May-2014 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
olivia.d.williams
USAACEACFT OPERATING IAW AWR 1505, R6 DTD03JUN14, 5M HYD FILTER, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.
04-Jun-2014 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEACFT OPERATING IAW AWR 1251, R9 DTD06JUN14, EYEBOLTS, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.
06-Jun-2014 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
DCR RASM-COCM/ACE PERFORMED AT 7869.3 AIRCRAFTHOURS BY TEAM MEMBERS P AND QQ
25-Jul-2014 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEACFT OPERATING IAW AWR 1514, R3 DTD31JUL14, DGNS, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.
31-Jul-2014 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACEH-60-14-SOF-04 (OPERATORS ANDCREWMEMBERS CHECKLIST) C/W 27 AUG 14AT 7913.2 ACFRT. HRS.
27-Aug-2014 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
USAACEACFT OPERATING IAW AWR 1220, R9 DTD31OCT14, ESM, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.
03-Nov-2014 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEACFT OPERATING IAW AWR 1455, R5 DTD28OCT14, BATTELLE CAP, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.
03-Nov-2014 2
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACECOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-19 LCF CHANGE 66 @ 7962.4
08-Nov-2014 1
LOWE AHP, FT.RUCKER, AL.
vickie.l.meadows
USAACEH-60-15-ASAM-01 LED CAUTION ADVISORYPANEL REQUIREMENTS COMPLETED AT 7973ACFT HRS.
21-Nov-2014 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
USAACEACFT OPERATING IAW AWR 1251, R10 DTD26NOV14, EYEBOLTS, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.
25-Nov-2014 1
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-15-AMAM-05 ( AHRS EMERGENCYPROCEDURES) @ 8010.1 ACFT HRS
12-Dec-2014 1
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
USAACEH-60-15-AMAM-05 AHR EMERGENCEYPROCEDURES REQUIREMENTS COMPLETEDAT 8353.6
12-Dec-2014 2
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEACFT OPERATING IAW AWR 1220, R10 DTD26JAN15, ESM, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.
11-Feb-2015 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEH-60-15-AMAM-06 IDENTIFICATION OFAVIATION SURVIVAILITY EQUIPMENT C/W 13FEB 2015.
27-Feb-2015 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACEACFT OPERATING IAW AWR 1965, R0 DTD08OCT14, APPLE IPAD DEVICES.
04-Mar-2015 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
vickie.l.meadows
USAACEGEN-12-AMAM-07 ACFT FIRST AID KITMODERNIZATION @ 8170.7 ACFT HRS
27-Apr-2015 1
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
USAACECOMPLIED WITH H-60-15-AMAM-11( MODE-STRANSPONDER ADDRESS REVIEW) @ 8197.3ACFT HRS
09-May-2015 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
COMPLIED WITH THE REQUIREMENTS OF H-60-15-AMAM-10 ( AV-DEC GASKET INSPECTION)@8191.0 ACFT HRS
12-May-2015 2
LOWE AHP, FT.RUCKER, AL.
USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-15-AMAM-10 ( AV-DEC GASKET INSPECTION)@8191.0 ACFT HRS
12-May-2015 3
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 54 of 61
USAACEACFT OPERATING IAW AWR 1505, R7 DTD13MAY15, 5M HYD FILTERS, SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR.
13-May-2015 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEACFT OPERATING IAW AWR 1251, R11 DTD27MAY15, EYEBOLTS ON BIFILAR,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.
28-May-2015 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEH-60-15-AMAM-14 LEGITIMATE CODE FILE(LCF) CHANGE 67 REQUIREMENTS C/W AT8199.8
25-Jul-2015 1
LOWE AHP, FT.RUCKER, AL.
olivia.d.williams
USAACEACFT OPERATING IAW AWR 1738, R3 DTD17JUL15, AN/APX-118 CXP, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.
28-Jul-2015 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEACFT OPERATING IAW AWR 1841, R4 DTD29JAN15, STARTER PN 3505300-10,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.
31-Jul-2015 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACETHIS ACFT NO LONGER OPERATING IAW AWR1251 (BILFILAR EYEBOLTS) AT 8203.1 ACFTHRS.
04-Sep-2015 1
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
USAACECOMPLIED WITH THE REQUIEMENTS OF H-60-15-AMAM-18, MEDEVAC CAROUSEL @ 8243.5ACFT HRS
29-Sep-2015 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-16-AMAM-01 (EIBF FRAMES) @ 8310.0 ACFTHRS
28-Oct-2015 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
chelsey.p.phillips
USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-16-ASAM-02, DEFECTIVE FUEL HOSES
08-Jan-2016 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEACFT OPERATING IAW AWR 1913, R2 DTD12FEB16, ACN LOGBOOK, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.
17-Feb-2016 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
LOCKHEED MARTINRASM-C
OCM/ACE PERFORMED AT 8560.2 AIRCRAFTHOURS BY TEAM MEMBERS P AND R
19-Apr-2016 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
USAACEACFT OPERATING IAW AWR 1444, R8 DTD25MAY16, SINGLE AHRS, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.
01-Jun-2016 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 58 of 61
USACEENTRY ENTERED IN ERROR DTD 04 JUN 2016,GEN-16-AMAM-04, TRANSPONDER BATTERYREPLACEMENT
04-Jun-2016 2
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
USAACECOMPLIED WITH THE REQUIREMENTS H-60-16-AMAM-09 COMPONENTS DUPLICATION @8561.6 ACFT HRS
23-Jun-2016 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-SOF-02, RESCUE HOIST OPERATIONALRESTRICTIONS HOIST NOT INSTALLED
15-Aug-2016 1
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
USAACECOMPLY WITH REQUIREMENTS OF H-60-16-AMAM-10, ULLS-A(E)
01-Sep-2016 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-17-ASAM-01, UULS-AE CADS
07-Oct-2016 2
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEACFT NOW OPERATING IAW AWR 1693, R3DTD 28JAN16, RESA.
28-Oct-2016 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEACFT OPERATING IAW AWR 1220, R11 DTD31OCT16, ESM, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.
01-Nov-2016 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEACFT OPERATING IAW AWR 2064, R0 DTD09DEC16, COBRA MICROPHONE.
12-Dec-2016 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACECOMPLIED WITH THE REQUIREMENT OF H-60-17-SOF-01, RESCUE HOIST EMERGENCYPROCEDURES @ 8801.4 ACFT HRS
20-Dec-2016 1
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
USAACEOMPLIED WITH THE REQUIREMENTS H-60-17-AMAM-01, ULLS-A (E) LCF CHANGE 68
20-Dec-2016 2
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-17-ASAM-04, AIRFRAME STRUCTURALPARTS
10-Jan-2017 1
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
USAACECOMPLIED WITH H-60-17-ASAM-05 MAINROTOR BLADE QUALITY ESCAPEMENT AT8838.8 AC HOURS.(KATY DAVIS)
23-Feb-2017 1
LOWE AHP, FT.RUCKER, AL.
theresa.d.pollard
USAACEACFT OPERATING IAW AWR 1738, R5 DTD24FEB2017, AN/APX-118/118A CXP.
08-Mar-2017 1
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEACFT OPERATING IAW AWR 1750, R4 DTD29MAR17, AN/AVS-6 NVG, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.
04-Apr-2017 1
LOWE AHP, FT.RUCKER, AL.
thomas.e.mitchell
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
ORGANIZATION LOCATION8.7.
DATE6.
REMARKS4. 5.
EH-60A 8524475HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
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
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEACFT BEING TRANSFERRED TO BESTPROGRAM, HUNTSVILLE, AL. AT 8875.6 ACFTHRS.
25-Apr-2017 1
LOWE AHP, FT.RUCKER, AL.
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
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
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
DA FORM 2408-15-2, OCT 1991 AIRCRAFT VIBRATION RECORD
DATE AC HRS SHAFT VERTICAL REASON FOR VIBRATION CHECKLONGITUDINALLATERALIPS READINGS4.
8524475HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
Page 2 of 10
a b c d e f g
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
DA FORM 2408-15-2, OCT 1991 AIRCRAFT VIBRATION RECORD
DATE AC HRS SHAFT VERTICAL REASON FOR VIBRATION CHECKLONGITUDINALLATERALIPS READINGS4.
8524475HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
DA FORM 2408-15-2, OCT 1991 AIRCRAFT VIBRATION RECORD
DATE AC HRS SHAFT VERTICAL REASON FOR VIBRATION CHECKLONGITUDINALLATERALIPS READINGS4.
8524475HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
DA FORM 2408-15-2, OCT 1991 AIRCRAFT VIBRATION RECORD
DATE AC HRS SHAFT VERTICAL REASON FOR VIBRATION CHECKLONGITUDINALLATERALIPS READINGS4.
8524475HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
DA FORM 2408-15-2, OCT 1991 AIRCRAFT VIBRATION RECORD
DATE AC HRS SHAFT VERTICAL REASON FOR VIBRATION CHECKLONGITUDINALLATERALIPS READINGS4.
8524475HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
DA FORM 2408-15-2, OCT 1991 AIRCRAFT VIBRATION RECORD
DATE AC HRS SHAFT VERTICAL REASON FOR VIBRATION CHECKLONGITUDINALLATERALIPS READINGS4.
8524475HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
DA FORM 2408-15-2, OCT 1991 AIRCRAFT VIBRATION RECORD
DATE AC HRS SHAFT VERTICAL REASON FOR VIBRATION CHECKLONGITUDINALLATERALIPS READINGS4.
8524475HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
DA FORM 2408-15-2, OCT 1991 AIRCRAFT VIBRATION RECORD
DATE AC HRS SHAFT VERTICAL REASON FOR VIBRATION CHECKLONGITUDINALLATERALIPS READINGS4.
8524475HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
DA FORM 2408-15-2, OCT 1991 AIRCRAFT VIBRATION RECORD
DATE AC HRS SHAFT VERTICAL REASON FOR VIBRATION CHECKLONGITUDINALLATERALIPS READINGS4.
8524475HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
DA FORM 2408-15-2, OCT 1991 AIRCRAFT VIBRATION RECORD
(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
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 2 of 4
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
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
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 3 of 4
COND COND
584101245909319E05C
268394INDICATOR,HEIGHT 413FFA3060591 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
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
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
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
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
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
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
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
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 4 of 4Condition Change Components
7. SIGNIFICANT HISTORICAL DATA
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.
APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991
(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.
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
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
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 2 of 2
7. SIGNIFICANT HISTORICAL DATA
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.
APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991
(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.
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
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
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 2 of 2
7. SIGNIFICANT HISTORICAL DATA
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.
jimmy.s.caylor USAACE FT.RUCKER,AL.
19-Jul-2016 2 INSTALLED FWD FIXED GEAR SHOCK, BEM3001, ON ACFT 8524475 WITH TSN 352, ACFT HRS. 8590.
jimmy.s.caylor USAACE FT.RUCKER,AL.
APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991
(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.
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
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
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 2 of 2
7. SIGNIFICANT HISTORICAL DATA
APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991
(ACFT HRS)
ji kgfdcba
RMVL HRSRMVL HRSCOMPO/HNOMENWUC O/HLOCATIONNSN
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
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
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 2 of 3
7. SIGNIFICANT HISTORICAL DATA
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)
loletia.v.williams USAACE FT. RUCKER, AL
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)
loletia.v.williams USAACE FT. RUCKER, AL
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.
loletia.v.williams USAACE FT. RUCKER, AL
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)
loletia.v.williams USAACE FT. RUCKER, AL
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
APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991
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 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.
jessica.n.kennedy USAACE FT. RUCKER, AL
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.
jessica.n.kennedy USAACE FT. RUCKER, AL
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
stephanie.d.hall USAACE FT RUCKER AL
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
stephanie.d.hall USAACE FT RUCKER AL
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
stephanie.d.hall USAACE FT RUCKER AL
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.
APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991
(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.
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
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
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 2 of 2
7. SIGNIFICANT HISTORICAL DATA
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
APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991
(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.
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
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
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 2 of 2
7. SIGNIFICANT HISTORICAL DATA
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.
christina.l.negron USAACE FT RUCKER,AL.
APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991
(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.
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
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
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 2 of 2
7. SIGNIFICANT HISTORICAL DATA
APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991
Page 1 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-
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 3 of 14
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-307369
hr)
3323
3664UDC022444046T25G01COOLER, OIL
COND
COND
3964
498COMH110684046T28G14ANTI-ICE VALVE
COND
COND
14. SIGNIFICANT HISTORICAL DATA
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
dean.a.keirn USAACE 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
dean.a.keirn USAACE FT. RUCKER, AL.
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
dean.a.keirn USAACE FT. RUCKER, AL.
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
vickie.l.meadows USAACE FT RUCKER, AL
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
vickie.l.meadows USAACE FT RUCKER, AL
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-
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 4 of 14
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-307369
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
vickie.l.meadows USAACE FT RUCKER, AL
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.
donna.k.moss USAACE FT. RUCKER, AL
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.
donna.k.moss USAACE FT. RUCKER, AL
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.
donna.k.moss USAACE FT. RUCKER, AL
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
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-
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 5 of 14
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-307369
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
theresa.d.pollard USAACE FT. RUCKER, AL
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
theresa.d.pollard USAACE FT. RUCKER, AL
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 6 of 14
ECD00973
GE-E-3073696035T02G01COLD SECTION MODULEGE-C-037369
2789
3323
19002
25459
8335
10877
1636
2598
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 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
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-
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 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
14. SIGNIFICANT HISTORICAL DATA
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
dean.a.keirn USAACE FT. RUCKER, AL.
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 9 of 14
ECD00973
GE-C-0373696039T56G04OUTPUT SHAFT ASSYGGA06975
2789
3562
19002
19829
8335
6291
1636
2328
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 10 of 14
04A01G 6039T56G04 OUTPUT SHAFT ASSY GGA06975
hr)
35621982962912328
16539206FCAF10436064T34P02NO 1 BALL BEARING
COND
COND
35621982962912328
574232933175254770MABC86645035T69P01NO 2 ROLLER
COND
COND
14. SIGNIFICANT HISTORICAL DATA
3/26/201012:00:00 AM
1 CCAD OUTPUT SHAFT INSTALLED ON 25MAR10, SERVICEABLE. /S/ M.BENAVIDES, AIRCRAFT DATA TECHNICIAN.
dean.a.keirn USAACE FT. RUCKER, AL.
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 11 of 14
ECD00973
GE-E-3073696055T20G05MTCHD ROTOR/STATORMRSG6037
2789
2910
19002
6967
8335
3312
1636
1145
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 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
14. SIGNIFICANT HISTORICAL DATA
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
dean.a.keirn USAACE FT. RUCKER, AL.
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 13 of 14
ECD00973
GE-E-3073696064T98G01POWER TURBINE MODULEGE-L-006113
2789
4698
19002
8178
8335
8903
1636
2797
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 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
14. SIGNIFICANT HISTORICAL DATA
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
dean.a.keirn USAACE FT. RUCKER, AL.
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 1 of 15
ECD03101
85244756035T00G01T700-GE-700 ENGINE ASSYGE-E-307927
8941
8941
17410
17410
19343
19343
3721
3721
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 15
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-307927
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
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-
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 3 of 15
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-307927
hr)
4047
3602UDC069334046T25G06COOLER, OIL
COND
COND
2989
0COMH58614046T28G14ANTI-ICE VALVE
COND
COND
14. SIGNIFICANT HISTORICAL DATA
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
loletia.v.williams 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.
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-
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 4 of 15
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-307927
hr)
thomas.m.lilly USAACE FT. RUCKER, AL
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.
thomas.m.lilly 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
olivia.d.williams USAACE FT RUCKER,AL
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.
jessica.n.kennedy USAACE FT. RUCKER, AL
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
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-
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 5 of 15
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-307927
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>
jessica.n.kennedy USAACE FT. RUCKER, AL
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.
christina.l.negron USAACE FT RUCKER,AL.
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.
dean.a.keirn USAACE FT. RUCKER, AL.
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.
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 6 of 15
ECD03101
GE-E-3079276035T02G01COLD SECTION MODULEGEC007896
7477
4059
17028
24200
15318
7397
3092
1913
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 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
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-
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 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
14. SIGNIFICANT HISTORICAL DATA
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.
olivia.d.williams USAACE FT RUCKER,AL
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 9 of 15
ECD03101
GEC0078966039T56G04OUTPUT SHAFT ASSYGGA06034
7477
5059
17028
23722
15318
9724
3092
2690
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 10 of 15
04A01G 6039T56G04 OUTPUT SHAFT ASSY GGA06034
hr)
50562365797082686
0000FCAY49806064T34P02NO 1 BALL BEARING
COND
COND
50562365797082686
0000FCAV52945035T69P02NO 2 ROLLER
COND
COND
14. SIGNIFICANT HISTORICAL DATA
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
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 11 of 15
ECD03101
GE-E-3079276055T20G05MTCHD ROTOR/STATORMRS08999
8941
3025
17410
18044
19342
7483
3720
1984
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 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
14. SIGNIFICANT HISTORICAL DATA
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.
dean.a.keirn USAACE FT. RUCKER, AL.
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.
dean.a.keirn USAACE FT. RUCKER, AL.
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 13 of 15
ECD03101
GE-E-3079276064T98G01POWER TURBINE MODULEGE-L-007575
7562
4932
17118
9472
15786
10514
3135
2654
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 14 of 15
04A03 6064T98G01 POWER TURBINE MODULE GE-L-007575
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
14. SIGNIFICANT HISTORICAL DATA
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-
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-
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 15 of 15
04A03 6064T98G01 POWER TURBINE MODULE GE-L-007575
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
REVERSE OF DA FORM 2408-16-1, OCT 1991
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
8. SIGNIFICANT HISTORICAL DATA
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
Page 1 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
Page 2 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.
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
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
Page 3 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.
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
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
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
T700 SERIES TURBINE ENGINE ANALYSIS CHECK RECORDDA FORM 2408-19-2, DEC 1991
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
T700 SERIES TURBINE ENGINE ANALYSIS CHECK RECORDDA FORM 2408-19-2, DEC 1991
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
ENGINE COMPONENT OPERATING HOURS RECORDDA FORM 2408-19-3, DEC 1991
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
e. ACFT HRS INSTALLEDc. TIME SINCE NEW OR OVERHAULc. SERIAL NUMBER
EH-60A A005-01253 Days
b. MAKE OR TYPE d. ACFT HRS LAST OIL CHANGEb. SERIAL NUMBER
HELICOPTER, UTILITY INTERMEDIATE GEARBOX 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
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:
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
8199.8
8524475 1399 0
e. ACFT HRS INSTALLEDc. TIME SINCE NEW OR OVERHAULc. SERIAL NUMBER
EH-60A 856006 Days
b. MAKE OR TYPE d. ACFT HRS LAST OIL CHANGEb. SERIAL NUMBER
HELICOPTER, UTILITY AUXILIARY POWER UNIT Hrs
a. NOMENCLATURE AND TYPEa. NOMENCLATUREFREQUENCY
COMPONENT
3.2.SAMPLEEND ITEM
1.
Page 1 of 1
a b
SUBMITTED
c a b
SAMPLE DATE PIDSAMPLELAST OILEND ITEM
RESULTSDATE RESULTS RECEIVED7. 8.6. REASON FORHOURS5.4.
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:
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 6726.6 5972
e. ACFT HRS INSTALLEDc. TIME SINCE NEW OR OVERHAULc. SERIAL NUMBER
EH-60A A00601066 Days
b. MAKE OR TYPE d. ACFT HRS LAST OIL CHANGEb. SERIAL NUMBER
HELICOPTER, UTILITY TAIL ROTOR GEARBOX ASSY 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
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:
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
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)
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.
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
B3031442370410-02820-0541650011431226SERVO, PRIMARY MAIN ROTOR
2823
UNCLASSIFIED For Official use Only (FOUO)
UNCLASSIFIED For Official use Only (FOUO)
REMARKS
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
26-Sep-1986
5 K78286D
1151 0 0 0 0
0
HELICOPTER, UTILITY 1520010820686 EH-60A
8524475
002 ~ ~
0 0 0
06H06
78286 0 0 0 0 799
A2710102870361-03001-0451615010812775SHAFT ASSY, T/R DRV SEC 1
0
UNCLASSIFIED For Official use Only (FOUO)
UNCLASSIFIED For Official use Only (FOUO)
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.
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 07-Apr-2017
07-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
82106 0 0 3069 0 799
B30311137274000-10311650011431226SERVO, PRIMARY MAIN ROTOR
3069
UNCLASSIFIED For Official use Only (FOUO)
UNCLASSIFIED For Official use Only (FOUO)
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
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
0.3USAACE, FT.RUCKER, AL
ALL UH-60A SERIES AIRCRAFTENGINE ANTI-ICE (AISBV)
H-60-12-ASAM-10MWO:
Priority Mnt Level
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
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
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
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:
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
ENGINE ASSY, TURBINE 8524475GE-E-3073691. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
ENGINE ASSY, TURBINE 8524475GE-E-3079271. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
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
thomas.m.lilly16-Dec-1999
0.5ESRA FTCKY(T.GRODE)
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
thomas.m.lilly16-Dec-1999
0.5ESRA FTCKY(T.GRODE)
ALL AH-64 AND UH-60 SERIESAIRCRAFT - ONE TIME INSPECTIONOF T700-GE-700/701/701C ENGINES
UH-60-99-ASAM-11MWO:
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
FUEL CONTROL 8524475UDAJ12191. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 24 of 24
05-Sep-2012 OM
donna.k.moss10-Sep-2012
0.5USAACE, FT.RUCKER, AL
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
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
5.0USAACE, FT.RUCKER, AL
PLASTIC MEDIA BLAST (PMB) ANDOXIDE FLAKE RESIDUE
H-60-13-ASAM-04MWO:
Priority Mnt Level
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
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
thomas.m.lilly25-Aug-2010
0.5USAACE, FT.RUCKER, AL(LW2720)
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
thomas.m.lilly25-Aug-2010
0.5USAACE, FT.RUCKER, AL(LW2720)
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
thomas.m.lilly25-Aug-2010
1.0USAACE, FT.RUCKER, AL(LW2720)
REDESIGNED PLANETARY GEARCARRIER RETIREMENT LIFE.(TB1027)
H-60-10-AMAM-02MWO:
Priority Mnt Level
21-Mar-2013 FM
jessica.n.kennedy23-Mar-2013
3.0USAACE, FT.RUCKER, AL
PLASTIC MEDIA BLAST (PMB) ANDOXIDE FLAKE RESIDUE
H-60-13-ASAM-04MWO:
Priority Mnt Level
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
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
QTY REQNOMENCLATURE:ITEM NO
1GYRO, DIRECTIONAL - CN-998/ASN-43
U UUUUUUUU UU0
3
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1SIGNAL DATA CONVERTER - CV-3338A/ASN-128B
U UUUUUUUU UU1
4
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1MOUNTING FOR KIT-1A/1C/TSEC - MT-3949A/U
U UUUUUUUU UU1
5
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RECEIVER - R-2139/ARN-123(V)
U UUUUUUUU UU1
6
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1MOUNTING - MT-4834/ARN-123(V)
U UUUUUUUU UU1
7
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1COMMAND INSTR SYS PROCESSOR - 70600-01038-101
U UUUUUUUU UU1
8
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1MOUNTING RACK - 70600-01038-102
U UUUUUUUU UU1
9
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1SAS AMPLIFIER - 70901-02908-104
U UUUUUUUU UU1
10
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RATE GYRO ASSEMBLY - 70600-01047-041
U UUUUUUUU UU1
11
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RATE GYRO - TRU-2A/A
U UUUUUUUU UU1
12
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
3MOUNT FOR TSEC/KY58 - S1660-60036-001
U UUUUUUUU UU3
13
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
3BATTERY FOR KY 58 - BA-1372/U
U UUUUUUUU UU0
14
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
3INTERFACE ADAPTER (KY-58) - Z-AHQ/TSEC
U UUUUUUUU UU0
15
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
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
SECTION I COCKPITEH-60A_BASELINE
4. EQUIPMENT CHECKLIST
8524475 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
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
QTY REQNOMENCLATURE:ITEM NO
1AMPLIFIER IMPEDANCE - AM-4859A/ARN-89
U UUUUUUUU UU1
17
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1#2 VHF-FM ANTENNA COUPLER - 70600-01010-104
U UUUUUUUU UU0
18
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1VHF/AM ANTENNA FILTER - 70600-01012-102
U UUUUUUUU UU1
19
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2VHF/AM ANTENNA FILTER - 70600-01011-103
U UUUUUUUU UU2
20
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2ANTENNA - AS-3831/APN-209(V)
U UUUUUUUU UU2
21
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1GLIDE SLOPE ANTENNA - 70600-01043-101
U UUUUUUUU UU1
22
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
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
QTY REQNOMENCLATURE:ITEM NO
2FIRST AID KIT - 6545-00-919-6650
U UUUUUUUU UU0
24
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1FIRE EXTINGUISHER - FR23-4-11848
U UUUUUUUU UU0
25
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2BAROMETERIC ALTIMETER - AAU-32/A
U UUUUUUUU UU2
26
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2CREW SEAT - D3801-2
U UUUUUUUU UU3
27
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2AIRCRAFT CLOCK - ABU-11A
U UUUUUUUU UU2
28
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RECEIVER/TRANSMITTER - RT-1477/ARC-201
U UUUUUUUU UU0
29
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2INTERPHONE CONTROL - C6533/ARC
U UUUUUUUU UU2
30
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
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
SECTION I COCKPITEH-60A_BASELINE
4. EQUIPMENT CHECKLIST
8524475 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
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
QTY REQNOMENCLATURE:ITEM NO
1INDICATOR ALTIMETER - ID-1917C/APN-209
U UUUUUUUU UU1
32
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1CONTROL RADIO SET - C-7392/ARN-89
U UUUUUUUU UU1
33
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1CONTROL - C-10604(V)6/ARN-186
U UUUUUUUU UU0
34
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1CONTROL - C-11466A/ARC-201
U UUUUUUUU UU0
35
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1COMPARATOR SIGNAL DATA - CM482/ARC186(V)
U UUUUUUUU UU1
36
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
3MOUNT - MT-6051/ARC-186
U UUUUUUUU UU3
37
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RECEIVER/TRANSMITTER - RT-1296A/APX-100
U UUUUUUUU UU1
38
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1CIVIL NAVIGATION CONTROL - C-10048/ARN-123(V)
U UUUUUUUU UU1
39
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1COMPASS SET CONTROLLER - C-8021E/ASN-75
U UUUUUUUU UU1
40
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RADIO RETRANSMISSION PANEL -70550-01008-042
U UUUUUUUU UU1
41
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1MAGNETIC COMPASS - MS17983-4
U UUUUUUUU UU1
42
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2OUTSIDE AIR TEMP INDICATOR - MS28028-1
U UUUUUUUU UU2
43
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1ARMOUR WING PANEL - 70500-01152-093
U UUUUUUUU UU0
44
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1ARMOUR WING PANEL - 70500-01152-094
U UUUUUUUU UU0
45
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
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
SECTION I COCKPITEH-60A_BASELINE
4. EQUIPMENT CHECKLIST
8524475 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
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
QTY REQNOMENCLATURE:ITEM NO
1CONTROL-INDICATOR ASN-132 C-11097/ASN-132
U UUUUUUUU UU0
47
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1SIGNAL DATA CONVERTER ASN-132CV-3739/ASN-132
U UUUUUUUU UU0
48
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1MOUNT FOR ASN-132 MT-4915/A
U UUUUUUUU UU0
49
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1DATA PROCESS SET AN/UYK-64(V)2
U UUUUUUUU UU0
50
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1TACAN RECEIVER/TRANSMITTER RT-1159/A
U UUUUUUUU UU0
51
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1ELECTRONIC SEQUENCE UNIT, 163290-100-E
U UUUUUUUU UU1
52
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RADAR DETECTION SET SIGNAL AN/APR39
U UUUUUUUU UU0
53
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1IR JAMMER COUNTERMEASURES SET AN/ALQ-144(V)
U UUUUUUUU UU0
54
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1DISPENSER GENERAL PURPOSE AIRCRAFT M130
U UUUUUUUU UU0
55
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
3SECURE SPEECH UNIT TSEC/KY-58
U UUUUUUUU UU0
56
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
3CONTROL INDICATOR (KY-58) C-8157/ARC
U UUUUUUUU UU0
57
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1KY-100 AIRTERM 0N616736-1
U UUUUUUUU UU0
58
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1CONTROL DISPLAY UNIT C-12346/URC
U UUUUUUUU UU0
59
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
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
Page 5 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
1 ACFT ARRIVED IN THIS CONFIGURATION3
BATTERY FOR KY 58 - BA-1372/U
1 ACFT ARRIVED IN THIS CONFIGURATION14
INTERFACE ADAPTER (KY-58)- Z-AHQ/TSEC
1 ACFT ARRIVED IN THIS CONFIGURATION15
REMOTE CONTROL UNIT (KY-58) - Z-AHP/YSEC
1 ACFT ARRIVED IN THIS CONFIGURATION16
#2 VHF-FM ANTENNACOUPLER - 70600-01010-104
1 ACFT ARRIVED IN THIS CONFIGURATION18
FIRST AID KIT - 6545-00-919-6650
1 ACFT ARRIVED IN THIS CONFIGURATION24
FIRE EXTINGUISHER - FR23-4-11848
1 ACFT ARRIVED IN THIS CONFIGURATION25
CREW SEAT - D3801-21 ACFT ARRIVED IN THIS CONFIGURATION27
RECEIVER/TRANSMITTER - RT-1477/ARC-201
1 ACFT ARRIVED IN THIS CONFIGURATION29
REVERSE OF DA FORM 2408-17, NOV 1991
Page 6 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
CONTROL - C-10604(V)6/ARN-186
1 ACFT ARRIVED IN THIS CONFIGURATION34
CONTROL - C-11466A/ARC-2011 ACFT ARRIVED IN THIS CONFIGURATION35
ARMOUR WING PANEL - 70500-01152-093
1 ACFT ARRIVED IN THIS CONFIGURATION44
ARMOUR WING PANEL - 70500-01152-094
1 ACFT ARRIVED IN THIS CONFIGURATION45
CONTROL-INDICATOR ASN-132 C-11097/ASN-132
1 ACFT ARRIVED IN THIS CONFIGURATION47
SIGNAL DATA CONVERTERASN-132CV-3739/ASN-132
1 ACFT ARRIVED IN THIS CONFIGURATION48
MOUNT FOR ASN-132 MT-4915/A
1 ACFT ARRIVED IN THIS CONFIGURATION49
DATA PROCESS SET AN/UYK-64(V)2
1 ACFT ARRIVED IN THIS CONFIGURATION50
TACANRECEIVER/TRANSMITTER RT-1159/A
1 ACFT ARRIVED IN THIS CONFIGURATION51
RADAR DETECTION SETSIGNAL AN/APR39
1 ACFT ARRIVED IN THIS CONFIGURATION53
IR JAMMERCOUNTERMEASURES SETAN/ALQ-144(V)
1 ACFT ARRIVED IN THIS CONFIGURATION54
REVERSE OF DA FORM 2408-17, NOV 1991
Page 7 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
DISPENSER GENERALPURPOSE AIRCRAFT M130
1 ACFT ARRIVED IN THIS CONFIGURATION55
SECURE SPEECH UNITTSEC/KY-58
1 ACFT ARRIVED IN THIS CONFIGURATION56
CONTROL INDICATOR (KY-58)C-8157/ARC
1 ACFT ARRIVED IN THIS CONFIGURATION57
KY-100 AIRTERM 0N616736-11 ACFT ARRIVED IN THIS CONFIGURATION58
CONTROL DISPLAY UNIT C-12346/URC
1 ACFT ARRIVED IN THIS CONFIGURATION59
REVERSE OF DA FORM 2408-17, NOV 1991
SECTION II CABINEH-60A_BASELINE
4. EQUIPMENT CHECKLIST
8524475 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
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
QTY REQNOMENCLATURE:ITEM NO
1BEARING, DISTANCE, HEADING INDICATOR - ID2301/U
U UUUUUUUU UU0
2
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1MARKER BEACON ANTENNA - 70600-02011-103
U UUUUUUUU UU1
3
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1FM HOMING ANTENNA ASSY - 70600-02017-104
U UUUUUUUU UU1
4
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1FM HOMING ANTENNA ASSY - 70600-02017-105
U UUUUUUUU UU1
5
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1FIRST AID KIT - 6545-00919-6650
U UUUUUUUU UU0
6
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1FIRE EXTINGUISHER - FR23-4-11848
U UUUUUUUU UU0
7
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1CRASH AXE - 56D6221
U UUUUUUUU UU1
8
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1HAND SET - H-250/U
U UUUUUUUU UU1
9
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1SLAB BATTERY - D8565/11-1
U UUUUUUUU UU1
10
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1INTERPHONE CONTROL - C6533/ARC
U UUUUUUUU UU3
11
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1ADAPTER FUEL DRAIN - 70307-03018-102
U UUUUUUUU UU0
12
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
4LOCK ASSY BLADE TIEDOWN - 70700-20369-041
U UUUUUUUU UU0
13
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2PLUG ASSY INTAKE - HIRSS SUPP - 70700-20515-041/042
U UUUUUUUU UU0
14
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2PLUG ASSY EXHAUST - HIRSS - 70700-20515-043
U UUUUUUUU UU0
15
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
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
SECTION II CABINEH-60A_BASELINE
4. EQUIPMENT CHECKLIST
8524475 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
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
QTY REQNOMENCLATURE:ITEM NO
1COVER ASSY OIL COOLER - 70700-20511-041
U UUUUUUUU UU0
17
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1BLADE FOLD SET - 70700-20412-011
U UUUUUUUU UU0
18
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2COVER PITOT TUBE - 70700-20460-041
U UUUUUUUU UU0
19
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1TROOP SEATS - 70500-02151-045
U UUUUUUUU UU0
20
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2COVER ENGINE INLET - 83DSCC-D006
U UUUUUUUU UU0
21
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1FITTING ASSEMBLY - L/H - 70751-02023-043
U UUUUUUUU UU0
22
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1FITTING ASSEMBLY - R/H - 70751-02023-044
U UUUUUUUU UU0
23
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1ICS WALK-AROUND CORD - 70602-02023-044
U UUUUUUUU UU0
24
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1PORTABLE INSP. FLOOD LIGHT - 15-0366-1
U UUUUUUUU UU0
25
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1HYD. PUMP HANDLE - 15400-50126
U UUUUUUUU UU1
26
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2EQUIPMENT LOGBOOK - MIL-D-43064
U UUUUUUUU UU1
27
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1COMPUTER LOGBOOK
U UUUUUUUU UU1
28
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1WEIGHT AND BALANCE HANDBOOK - TM 55-1500-342-23
U UUUUUUUU UU1
29
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
4TIEDOWN ASSEMBLY, TOW - 70700-20433-045
U UUUUUUUU UU0
30
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
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
Page 3 of 5SERIAL NUMBER MODEL AREA NAME
8524475 EH-60A_BASELIN SECTION II CABINEH-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
INERTIAL NAVIGATION SET -AN/ASN-141
1 ACFT ARRIVED IN THIS CONFIGURATION1
BEARING, DISTANCE,HEADING INDICATOR -ID2301/U
1 ACFT ARRIVED IN THIS CONFIGURATION2
FIRST AID KIT - 6545-00919-6650
1 ACFT ARRIVED IN THIS CONFIGURATION6
FIRE EXTINGUISHER - FR23-4-11848
1 ACFT ARRIVED IN THIS CONFIGURATION7
INTERPHONE CONTROL -C6533/ARC
1 ACFT ARRIVED IN THIS CONFIGURATION11
ADAPTER FUEL DRAIN - 70307-03018-102
1 ACFT ARRIVED IN THIS CONFIGURATION12
LOCK ASSY BLADE TIEDOWN- 70700-20369-041
1 ACFT ARRIVED IN THIS CONFIGURATION13
PLUG ASSY INTAKE - HIRSSSUPP - 70700-20515-041/042
1 ACFT ARRIVED IN THIS CONFIGURATION14
PLUG ASSY EXHAUST - HIRSS- 70700-20515-043
1 ACFT ARRIVED IN THIS CONFIGURATION15
PLUG ASSY APU EXHAUST -70700-20509-041
1 ACFT ARRIVED IN THIS CONFIGURATION16
REVERSE OF DA FORM 2408-17, NOV 1991
Page 4 of 5SERIAL NUMBER MODEL AREA NAME
8524475 EH-60A_BASELIN SECTION II CABINEH-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
COVER ASSY OIL COOLER -70700-20511-041
1 ACFT ARRIVED IN THIS CONFIGURATION17
BLADE FOLD SET - 70700-20412-011
1 ACFT ARRIVED IN THIS CONFIGURATION18
COVER PITOT TUBE - 70700-20460-041
1 ACFT ARRIVED IN THIS CONFIGURATION19
TROOP SEATS - 70500-02151-045
1 ACFT ARRIVED IN THIS CONFIGURATION20
COVER ENGINE INLET -83DSCC-D006
1 ACFT ARRIVED IN THIS CONFIGURATION21
FITTING ASSEMBLY - L/H -70751-02023-043
1 ACFT ARRIVED IN THIS CONFIGURATION22
FITTING ASSEMBLY - R/H -70751-02023-044
1 ACFT ARRIVED IN THIS CONFIGURATION23
ICS WALK-AROUND CORD -70602-02023-044
1 ACFT ARRIVED IN THIS CONFIGURATION24
PORTABLE INSP. FLOODLIGHT - 15-0366-1
1 ACFT ARRIVED IN THIS CONFIGURATION25
EQUIPMENT LOGBOOK - MIL-D-43064
1 ACFT ARRIVED IN THIS CONFIGURATION27
TIEDOWN ASSEMBLY, TOW -70700-20433-045
1 ACFT ARRIVED IN THIS CONFIGURATION30
REVERSE OF DA FORM 2408-17, NOV 1991
Page 5 of 5SERIAL NUMBER MODEL AREA NAME
8524475 EH-60A_BASELIN SECTION II CABINEH-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
REVERSE OF DA FORM 2408-17, NOV 1991
SECTION III TRANSITION SECTIONEH-60A_BASELINE
4. EQUIPMENT CHECKLIST
8524475 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
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
QTY REQNOMENCLATURE:ITEM NO
2IFF ANTENNA - 70600-02010-103
U UUUUUUUU UU2
2
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1UHF/AM ANTENNA 70600-03002-104
U UUUUUUUU UU1
3
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1PUMP FUEL SAMPLER - 82829/4P156-3
U UUUUUUUU UU0
4
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1COMPENSATOR MAGNETIC FLUX - CN-405/ASN
U UUUUUUUU UU1
5
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1COMPASS TRANSMITTER - T-611/ASN
U UUUUUUUU UU1
6
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1GPS ANTENNA 22433-40
U UUUUUUUU UU1
7
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1HF AMPLIFIER COUPLER AM-7531/URC
U UUUUUUUU UU0
8
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RECEIVER/TRANSMITTER RT-1749/URC
U UUUUUUUU UU0
9
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
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
Page 2 of 2SERIAL NUMBER MODEL AREA NAME
8524475 EH-60A_BASELIN SECTION III TRANSITION SECTIONEH-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
PUMP FUEL SAMPLER -82829/4P156-3
1 ACFT ARRIVED IN THIS CONFIGURATION4
HF AMPLIFIER COUPLER AM-7531/URC
1 ACFT ARRIVED IN THIS CONFIGURATION8
RECEIVER/TRANSMITTER RT-1749/URC
1 ACFT ARRIVED IN THIS CONFIGURATION9
REVERSE OF DA FORM 2408-17, NOV 1991
SECTION IV TAIL CONEEH-60A_BASELINE
4. EQUIPMENT CHECKLIST
8524475 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
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
QTY REQNOMENCLATURE:ITEM NO
1HF ANTENNA 4700516-30
U UUUUUUUU UU0
2
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
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
Page 2 of 2SERIAL NUMBER MODEL AREA NAME
8524475 EH-60A_BASELIN SECTION IV TAIL CONEEH-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
HF ANTENNA 4700516-301 ACFT ARRIVED IN THIS CONFIGURATION2
REVERSE OF DA FORM 2408-17, NOV 1991
SECTION V TAIL ROTOR PYLONEH-60A_BASELINE
4. EQUIPMENT CHECKLIST
8524475 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
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
QTY REQNOMENCLATURE:ITEM NO
1#1 VHF-FM ANTENNA - 70600-06002-105
U UUUUUUUU UU1
2
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
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
Page 2 of 2SERIAL NUMBER MODEL AREA NAME
8524475 EH-60A_BASELIN SECTION V TAIL ROTOR PYLONEH-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
REVERSE OF DA FORM 2408-17, NOV 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
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
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
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
thomas.m.lilly04-Dec-2003
1.0USAAVNC, FT.RUCKER, AL(MF4187)
ALL UH-60A, UH-60L, EH-60A,REMOVAL OF SPECIFIC SUSPECTREWORKED MAIN ROTORSWASHPLATE ASSEMBLIES
UH-60-97-ASAM-18MWO:
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)
UH-60-98-ASAM-03MWO:
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
UH-60-06-ASAM-03MWO:
Priority Mnt Level
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
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
5.0USAACE, FT.RUCKER, AL
PLASTIC MEDIA BLAST (PMB) ANDOXIDE FLAKE RESIDUE
H-60-13-ASAM-04MWO:
Priority Mnt Level
For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG
EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991
REMARKS
THIS T/R PITCH CHANGE SHAFT IS IN UNSERVICEABLE CONDITION, HAS 2 EA BUSHINGS DAMAGED BEYOND LIMITS. ACFT 8524475 IS BEING TURNED
IN.
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
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 07-Apr-2017
07-Apr-2017 CHRIST 334-503-3807
2 N W0U91TF
0 0 0 0 0 0 0 8876
8876 0 0
HELICOPTER, UTILITY 1520010820686 EH-60A
8524475
0 0 0 0 0
11C23 0 0
65780 2 0 2285 1048 710
2330294270400-06100-0421615011417532T/R PITCH CHANGE SHAFT
2285
UNCLASSIFIED For Official use Only (FOUO)
UNCLASSIFIED For Official use Only (FOUO)
UNIT UNIQUE INVENTORY ITEMSEH-60A_BASELINE
4. EQUIPMENT CHECKLIST
8524475 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
Page 1 of 2
1IFM APMLIFIER AM-7189A/ARC
U UUUUUUUU UU1
1
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2ATTITUDE AND HEADING REFERENCE UNIT (CN1716/A)
U UUUUUUUU UU1
2
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1MOUNT IFM AMP PN: MT-6592/ARC
U UUUUUUUU UU1
3
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1BFT ANTENNA GPS PN: S671575-863
U UUUUUUUU UU1
4
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1BFT ANTENNA L-BAND PN: S65-8282-301
U UUUUUUUU UU1
5
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
0IGNITION KEYS
U UUUUUUUU UU2
6
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1BFT PALLET ASSY PN: 080094-1
U UUUUUUUU UU 0
7
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
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
Page 2 of 2SERIAL NUMBER MODEL AREA NAME
8524475 EH-60A_BASELIN UNIT UNIQUE INVENTORY ITEMSEH-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
IFM APMLIFIER AM-7189A/ARC1 ACFT ARRIVED IN THIS CONFIGURATION1
ATTITUDE AND HEADINGREFERENCE UNIT (CN1716/A)
1 ACFT ARRIVED IN THIS CONFIGURATION2
IGNITION KEYS1 ACFT ARRIVED IN THIS CONFIGURATION6
BFT PALLET ASSY PN: 080094-1
2 ACFT ARRIVED IN THIS CONFIGURATION7
REVERSE OF DA FORM 2408-17, NOV 1991