1. nomenclature 2. model 3. aircraft serial number
Post on 11-Jul-2022
13 Views
Preview:
TRANSCRIPT
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
8524465EH-60AHELICOPTER, UTILITY
3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE
Page 1 of 4
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
OM17-Mar-1988
SIKORSKY WPB(T SPEARS)
1.002-Jun-1988
LILLY, THOMASM
ALL UH-60A/EH-60A AIRCRAFT, ONETIME INSPECTION OF THE TAILROTOR GEARBOX OUTPUT SHAFT
UH-60-88-02MWO:
Mnt LevelPriority
DN30-Apr-1987
SIKORSKY WPB(T SPEARS)
1.004-JUN-1988
LILLY, THOMASM
INCORPORATION OF WIRE STRIKEPROTECTION SYSTEM (WSPS) (UH-60A HELICOPTER)
55-1520-237-50-24MWO:
Mnt LevelPriority
DR25-Jan-2007
USAACE, FT.RUCKER, AL(RJ0827)
1.005-JUN-2010
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
DN30-Jun-2004
USAACE, FT.RUCKER, AL(RJ0827)
1.005-JUN-2010
LILLY, THOMASM
MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE DOPPLERGPS NAVIGATION SET (DGNS)
1-1520-237-50-92MWO:
Mnt LevelPriority
DN15-Jan-1989
LSSI(R.GILBERT)
12.005-NOV-1992
LILLY, THOMASM
INCORPORATION OFELECTROMAGENTIC INTERFERENCE(EMI) PROTECTION FOR LEFT ANDRIGHT RELAY PANELS (UH-60A/EH-60A HELICOPTERS)
1-5945-237-50-1MWO:
Mnt LevelPriority
DR15-Jul-1985
LSSI(J. VAUGHN) 1.005-NOV-1992
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
DN16-Oct-1989
LSSI(R GILBERT) 20.005-NOV-1992
LILLY, THOMASM
MODIFICATION OF FLIGHT CONTROLMIXER ASSEMBLY (UH-60A/EH-60AHELICOPTERS)
55-1520-237-50-49MWO:
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.
8524465EH-60AHELICOPTER, UTILITY
3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE
Page 2 of 4
OE30-Apr-1986
SIKORSKYACFT.(JAMESKRETZ)
2.007-AUG-1986
LILLY, THOMASM
RELOCATION OF THE AUTOMATICFLIGHT CONTROL SYSTEM (AFCS)PANEL
55-1520-237-20-1MWO:
Mnt LevelPriority
DN15-Jan-1991
LSSI(R.GILBERT) 8.007-OCT-1992
LILLY, THOMASM
INCORPORATION OF ENGINE DRIVESHAFT BALANCING PROCEDURE (UH-60A/EH-60A HELICOPTERS)
55-1520-237-50-58MWO:
Mnt LevelPriority
DN09-Jun-1988
LSSI(M GROSS) 1.009-JUN-1988
LILLY, THOMASM
INCORPORATION OF STABILATORAMPLIFIER IMPROVEMENTS(INCLUDES MODIFICATION OFSTABILIZATION TEST SET) (UH-60AHELICOPTERS)
55-1520-237-50-42MWO:
Mnt LevelPriority
DN01-May-1994
LSSI/OLR(D.WILLIAMS)
140.011-MAY-1995
LILLY, THOMASM
INCORPORATION OF IMPROVED FIREEXTINGUISHER CIRCUIT ANDHELLFIRE CONNECTOR (UH-60 A/LAND EH-60A)
1-1520-237-50-66MWO:
Mnt LevelPriority
DM21-Jun-2006
CSC,FT.CAMPBELLFT.RUCKER,AL )(RJ0827)
160.014-Sep-2009
LILLY, THOMASM
INSTALLATION INSTRUCTIONS FORTHE BLUE FORCE TRACKING ON UH-60A/L HELICOPTERS (NSN 1520-01-035-0266) (NSN 1520-01-298-4532)
1-1520-237-50-BFT60-001MWO:
Mnt LevelPriority
DR03-Dec-2005
CSC, FT.CAMPBELL FT.RUCKER, AL(RJ0827)
1.014-Sep-2009
LILLY, THOMASM
INSTALLATION OF ELECTRONIC DATAMANAGEMENT (EDM) SYSTEM FORBLUE FORCE TRACKING
1-1520-237-50-EDMMWO:
Mnt LevelPriority
DM15-Nov-1989
LSSI(M GROSS) 1.015-NOV-1989
LILLY, THOMASM
MODIFICATION OF DOWEL PINRETENTION MAIN GEARBOX
55-1520-237-50-43MWO:
Mnt LevelPriority
DN17-Jan-1989
LSSI(M GROSS) 1.016-AUG-1989
LILLY, THOMASM
MODIFICATION OF BEARINGRETAINER SPRING CLIP, TAIL ROTORSERVO (UH/EH-60A HELICOPTERS)
55-1520-237-50-52MWO:
Mnt LevelPriority
DN01-Oct-1988
TRACOR FLIGHTSYST. INC.(RFERGUSON)
10.016-AUG-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.
8524465EH-60AHELICOPTER, UTILITY
3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE
Page 3 of 4
DN01-Oct-1990
LSSI(M. GROSS) 1.016-AUG-1989
LILLY, THOMASM
INCORPORATION OF ENGINEQUADRANT SECONDARY STOP TONO. 1 AND NO. 2 ENGINE POWERCONTROL LEVERS (UH-60AHELICOPTERS)
55-1520-237-50-39MWO:
Mnt LevelPriority
DU31-May-1995
LMLM/OLR(WFANE)
16.019-JUL-1995
LILLY, THOMASM
MODIFICATION OF THE ENGINE TRIMBALANCE HARDWARE (EH/UH-60AAND UH-60L HELICOPTERS)
1-1520-237-50-73MWO:
Mnt LevelPriority
DN30-Apr-1997
AMCOM 2/OLR(SS9694)
1.019-JUN-2000
LILLY, THOMASM
INSTALLATION OF THE AVIATOR'SNIGHT VISION IMAGING SYSTEM(ANVIS) LIGHTING UPDATE EH/UH-60A/L
1-1520-237-50-56MWO:
Mnt LevelPriority
DU10-Aug-1987
LSSI/OLR(GGOODWIN)
12.019-OCT-1987
LILLY, THOMASM
INCORPORATION OF STABILATORSLEW-UP SWITCH (UH-60AHELICOPTER)
55-1520-237-50-46MWO:
Mnt LevelPriority
DN23-Jan-1989
LSSI(M. GROSS) 1.023-JAN-1989
LILLY, THOMASM
MODIFICATION OF MAIN ROTOR HEADANTI-FLAP BRACKETS (UH-60A ANDEH-60A HELICOPTERS)
55-1520-237-50-44MWO:
Mnt LevelPriority
FR02-Nov-2009
USAACE 2.023-Nov-2013
WILLIAMS,OLIVIA D
SINGLE INSTALLATION OF ATTITUDEHEADING REFERENCE UNIO (AHRU)
1-1520-237-20-2MWO:
Mnt LevelPriority
DN24-Aug-1992
MANAGEMENTTECHNOLOGIESMANTEC(L.BELL)
2.525-AUG-1995
LILLY, THOMASM
MODIFICATION OFCOUNTERMEASURE SYSTEMS,SPECIAL PURPOSE AN/ALQ151(V)2
32-5865-012-55-2MWO:
Mnt LevelPriority
DN24-Aug-1992
MANAGEMENTTECHNOLOGIESMANTEC(L.BELL)
2.825-AUG-1995
LILLY, THOMASM
MODIFICATION OF MX10842/ALQ P/N5108067-1
32-5999-002-55-1MWO:
Mnt LevelPriority
DN01-Feb-1993
LSSI(R. DIXON) 1.027-MAR-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
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.
8524465EH-60AHELICOPTER, UTILITY
3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE
Page 4 of 4
DM22-Feb-1991
LSSI(R. DIXON) 1.027-MAR-1995
LILLY, THOMASM
INCORPORATE ELECTRO-MAGNETICENVIRONMENT (EME) PROTECTIONPROVISIONS ON DELIVERED UH-60A/LAND EH-60A HELICOPTERS
1-1520-237-50-59MWO:
Mnt LevelPriority
DN15-Nov-1990
LSSI(R. DIXON) 1.027-MAR-1995
LILLY, THOMASM
INSTALLATION OF IMPROVEDTIEDOWN RING EYEBOLT (UH-60A/LAND EH-60A)
1-1520-237-50-61MWO:
Mnt LevelPriority
DM01-Sep-1991
LSSI(R. DIXON) 1.027-MAR-1995
LILLY, THOMASM
IMPROVED ENGINE COWLINGRELEASE HANDLE ASSEMBLY
1-1520-237-50-64MWO:
Mnt LevelPriority
DU30-Mar-1987
LSSI(W PANYE) 3.028-APR-1987
LILLY, THOMASM
MODIFICATION OF MAIN ROTORBLADE DE-ICE DISRUPTOR HARNESSAND TAIL ROTOR SLIP RINGHARNESS (UH-60A HELICOPTERS)
55-1520-237-50-36MWO:
Mnt LevelPriority
DN31-Oct-1996
ATCOM/OLTLM212302 FT.DRUM NY(TM8902)
20.028-APR-1997
LILLY, THOMASM
INSTALLATION OF REDUCEDDIAMETER BALLISTIC TOLERANTFUEL LINES (UH-60A/L AND EH-60AHELICOPTERS)
1-1520-237-50-74MWO:
Mnt LevelPriority
DN01-Aug-1991
LSSI/OLR(B.BARON)
30.028-DEC-1990
LILLY, THOMASM
STAB GROUNDING STRAP55-1520-237-50-54MWO:
Mnt LevelPriority
DR13-Apr-2001
USAAVNC, FT.RUCKER, AL(LW2720)
90.028-OCT-2002
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
DR11-Aug-2000
AMCOM/OLRLM2 FT DRUM,NY(SB SILES)
4.029-JUL-1999
LILLY, THOMASM
INSTALLATION OF THEPILOT/COPILOT SEATS MA-16(IMPROVED) INERTIA REEL IN ALL UH-60 HELICOPTERS
1-1520-237-50-79MWO:
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 1 of 61
SIKORSKY AIRCRAFTAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG. 70400-0003REV. E. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD. A. AFT CONTROL SERVOINPUT ROD HAS BEEN LENGTHENED 1/2TURN. B. LATERAL CONTROL SERVO INPUTROD NO CHANGE REQUIRED. C. FORWARDCONTROL INPUT ROD HAS BEEN SHORTENED1/2 TURN. NOTE: WHEN AIRCRAFT RIGGING ISBIASED RIGGING PIN HOLES ARETEMORAIRLY LOST AT THE ABOVE 3 POINTS(UNKNOWN/R/CLERK LW2720)
20-Feb-1986 1
STRATFORD, CT
thomas.m.lilly
SIKORSKY AIRCRAFTUH-60A-84-02-TB55-1520-237-20-48---ONE TIMEINSPECTION OF WIRE HARNESS ROUTINGFORE FEEDER HARNESS BETWEEN NO. 1AND NO.2 JUNCTION BOXES COMPLIED WITH(UNKNOWN/R/CLERK LW2720)
04-Aug-1986 2
STRATFORD, CT
thomas.m.lilly
SIKORSKY AIRCRAFTUH-60A-84-07 TB55-1520-237-20-53---INSPECTION OF ENGINE OUTPUT SHAFT P/N70361-08004-042 AND 043 COMPLIED WITHMS9724-08 BOLTS INSTALLED ANDINSPECTED PER UH-60A-84-07 NA TO THISAIRCRAFT--UH 60A-84-08 TB55-1520-237-20-50ONE TIME INSPECTION AEROQUIP CARGOHOOK PRESSURE CARTRIDGE ASSY P/NFE7590-65 COMPLIED WITH(UNKNOWN/R/CLERK LW2720)
05-Aug-1986 1
STRATFORD, CT
thomas.m.lilly
SIKORSKY AIRCRAFTS.O.F. MSG. UH-60A-86-07--REQUIREMENTFOR UNGROUNDING COMPLIED WITH (JAMESKURTZ)
07-Aug-1986 1
STRATFORD, CT
thomas.m.lilly
SIKORSKY AIRCRAFTCOMPLIED WTH S.O.F. MSG.#2201101Z DTDFEB.86 UH-60A-86-02---ONE TIME INSPECTIONOF TAIL ROTOR DRIVESHAFT NUTS.(CHARLES WESCOTHER)
07-Aug-1986 2
STRATFORD, CT
thomas.m.lilly
SIKORSKY AIRCRAFTCOMPLIED WITH S.O.F. MSG. #231740Z DTDFEB.86 UH-60A-86-03---REVISION TO S.O.F.MSG UH-60A-86-02 (CHARLES WESCOTHER)
07-Aug-1986 3
STRATFORE, CT
thomas.m.lilly
SIKORSKY AIRCRAFTCOMPLIED WITH S.O.F MSG.#072355Z DTDMAY 1986 UH-60A-86-08---REPLACEMENT OFSTABILATOR ACTUATORS P/N 70400-06641-110 (CHARLES WESCOTHER)
07-Aug-1986 4
STRATFORD, CT
thomas.m.lilly
SIKORSKY AIRCRAFTCOMPLIED WITH S.O.F MSG. 301500Z DTSOCT. 86 UH-60A-86-19----UH-60A REPETITVEINSP. OF EYEBOLT P/N 70209-02136-102(CHARLES WESCOTHER)
07-Aug-1986 5
STRATFORD, CT
thomas.m.lilly
SIKORSKY AIRCRAFTCOMPLIED WIHT S.O.F. MSG.#122200Z DTDMAR.86 UH-60A-86-05 IMMEDIATE GROUNDINGOF UH-60/EH-60 SERIES AIRCRAFT. (CHARLESWESCOTHER)
07-Aug-1986 6
STRATFORD, CT
thomas.m.lilly
SIKORSKY AIRCRAFTCOMPLIED WITH S.O.F. MSG.#171600Z DTDAPR.86 UH-60A-86-06 STABILATOR AUTOFLIGHT CONTROL PANEL RETROFIT.(LARSON)
08-Aug-1986 1
STRATFORD, CT
thomas.m.lilly
SIKORKSY AIRCRAFTS.O.F. MSG. 291415Z DTD. JULY 1986 UH-60A-86-13----UH-60 SERIES AIRCRAFT, REMOVALOF AN310-8 NUTS. (JAMES KURTZ)
10-Sep-1986 1
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 2 of 61
SIKORSKYCOMPLIED WITH S.O.F. MSG. 19130OZ STDAUGUST 1986 UH-60A-86-15-UH EH-60ASERIES AIRCRAFT, REVISION TO REMOVALOF AN310-8 NUTS, NSN 5310-00-167-1289(JAMES KURTZ)
10-Sep-1986 2
STRATFORD, CT
thomas.m.lilly
SIKORSKY AIRCRAFTUH-60A-85-02---SAFETY OF FLIGHTMAINTENANCE MANDATORY MESSAGE TOCHANGE THE AUTOROTATION RPM LIMITSCOMPLIED WITH (UNKNOWN/R/CLERKLW2720)
12-Sep-1986 1
STRATFORD, CT
thomas.m.lilly
SIKORSKY AIRCRAFTUH-60A-86-21 TB55-1520-238-20-85 ONE TIMEINSPECTION OF CREW SEATS FORLONGITUDINAL MOVEMENTS OF LOCK PINADJUSTMENT COMPLIED WITH (JAMESKURTZ)
15-Dec-1986 1
STRATFORD, CT
thomas.m.lilly
LARSON AASFACFT ASSIGNED TO AASF VARNING---D.W.LARSON AASF VARNE SANDSTON, VA(UNKNOWN/R.CLERK LW2720)
12-Feb-1987 1
SANDSTON, VA
thomas.m.lilly
LARSONTB55-1520-237-20-79---REPL. OF ENG DESWIRLCLAMSP NA THIS ACFT DW LARSO(UNKNOWN/R.CLERK)
09-Mar-1987 1
VARNGE SAMPSTON,VA
thomas.m.lilly
DW LARSONSOF MSG UH-60A-87-03 TB55-1520-237-23-20-89---ONE TIME INSP & RECURRING INSP OFFIRST THREE TAIL ROTOR DRIVE SHAFTSPLINE COUPLINGS COMPLIED WITH(UNKNONW/R.CLERK LW2720)
18-Mar-1987 1
AASF VAARNGSANDSTON, VA
thomas.m.lilly
AASF VAARNGSOF MSG UH-60-87-04--REVISION TO INSP OFEYEBOLT-COMPLIED WITH (LARSON)
03-Apr-1987 1
SANDSTON, VA
thomas.m.lilly
LARSONSOF MSG UH-60-87-06--TB55-1520-237-50-02--ONE TIME AND RECURRING INSPECTIONS OILCOOLER SPLINES-COMPLIED WITH--DW(UNKNOWN/R.CLERK/LW2720)
16-May-1987 1
AASF VAARNG,SANDSTON, VA
thomas.m.lilly
AASF VAARNGSOF MSG UH-60-87-07--TB55-1520-237-20-90-ONE TIME AND RECURRING INSP OF LAT. ANDLONG. LINK ASSY FOR CRACKED BEARINGSINNER RACE. COMPLIED WITH (LARSON)
16-May-1987 2
SANDSTON, VA
thomas.m.lilly
AASF VARNGSOF MSG UH-60A-87-08 TB55-1520-237-20-91--ONE TIME INSP OF MIDSECTIONBELLCRANKS=COMPLIES WITH (LARSON)
14-Jul-1987 1
SANDSTON, VA
thomas.m.lilly
AASFS-O-F MESSAGE UH-60A-88-01 TB55-1520-237-20-95--ONE TIME INSPECTION OF CERTAINSERIAL NUMBER TAIL ROTOR BLADE ASSY'S.COMPLIED WITH (H.T. EUBANK)
16-Feb-1988 1
VARNG SANDSTON, VA
thomas.m.lilly
SIKORSKY AIRCRAFTE.I. E70-702-20-2018---CARGO DOOR ROLLERASSEMBLY COMPLIED WITH AT SIKORSKYAIRCRAFT, W.P.B. (TOMMIE)
09-Jun-1988 1
W.P.B. FT.
thomas.m.lilly
SIKORSKY AIRCRAFTSOF UH-60A-88-03---MAINTENANCEMANDATORY LIFE EXTENSION OF MAINMODULE SHAFT COMPLIED WITH ATSIKORSKY AIRCRAFT, W.P.B., FL (BEANS)
09-Jun-1988 2
W.P.B.
thomas.m.lilly
SIKORSKY AIRCRAFTTB55-1520-237-20-79--INSPECTION ANDREPLACEMENT OF ENGINE DESWIRL DUCTCLAMPS COMPLIED WITH AT SIKORSKYAIRCRAFT, (BEANS)
09-Jun-1988 3
W.P.B.
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 3 of 61
SIKORSKY AIRCRAFTP.M.I. 88-081-TRANSMISSION MAIN MODULELOG AND CARD COMPLIED WITH (BEANS)
10-Jun-1988 1
W.P.B., FL
thomas.m.lilly
SIKORSKY AIRCRAFTNOTE: THE FOLLOWING RETROFIT MOD KITSHAVE BEEN INSTALLED PER MODIFICATIONF00159 TO CONTRACT DAAJ09-85-C-A006:70070-30038-015/016--HIRSS MOD INSTALL;700700-20139-013-ECU DUCT MOD; 70070-20142-011--MOD KIT PANEL; 70070-20144-011---MOD KIT ECM CRADLE; 70070-20146-011/012---MOD KIT FLOOR INSTALL;70070-20151-012--CARGO DOOR SEAL MOD; 70070-20154-011--DIPLEX SHELF INSTALL;70070-55090-012/011--MOD KIT ECU SYSTEM; 70070-55094-011-MODKIT ECM ANTENNA; 70070-55119-011--MODHARNESS ASSY. DIPLEXER; 70070-55123-011--MOD KIT JUNCTION BOXES; 70070-55125-011-ICS SYSTEM MOD; 70070-60074-011---MOD KITHSI WLG; 70070-60077-011--MOD KIT BUSCABLE; 70070-60082-011-MOD INV. HOSE;COMPLIED WITH AT SIKORSKY AIRCRAFT,WEST PALM BEACH FL. 70070-60083-011--NPUGROND WIRE (TOMMIE BARNES)
10-Jun-1988 2
QUALITY ASSURANCE
thomas.m.lilly
CA AVCRAD,SOF UH-60-88-08, REV TO UH-60-88-06 C/W(JOHN NESHA)
01-Aug-1988 1
FRESNO, CA
thomas.m.lilly
AVCRADSOF GEN-88-02 ONE TIME INSP FOR CORRECTINTERNAL PORTABLE FIRE EXT C/W AL(LARRY)
21-Sep-1988 1
FRESNO, CA
thomas.m.lilly
AVCRADSOF UH-60-88-11--RESCINDS NEED TO CARRYCIRCL RED X ON -13 OF EH 60A ACFT SOF UIH-60-86-18 C/W (THOMAS GREIL)
18-Oct-1988 1
FRESNO, CA
thomas.m.lilly
AVCRAD, CASOF MSG#UH-60-88-12--NOT APPLICABLE TOEH-60A AIRCRAFT (THOMAS CREWS)
02-Nov-1988 1
FRESNO, CA
thomas.m.lilly
AVCRAD, CASOF MSG #UH-60-85-05---MAINTENANCEMANDITORY, RECORDING REPORTING NONE(THOMAS CREWS)
17-Nov-1988 1
FRESNO, CA
thomas.m.lilly
AVCRAD, CASOF MSG# UH-60-85-22 NA TO THIS ACFT(THOMAS CREWS)
17-Nov-1988 2
FRESNO, CA
thomas.m.lilly
AVCRAD, CASOF MSG# UH-60-86-09 PREVISOUSLY C/W,NOT ENTERED ON -15 (-5) (THOMAS CREWS)
17-Nov-1988 3
FRESNOC, CA
thomas.m.lilly
AVCRAD, CASOF MSG# UH-60-86-18 MSG RECINDED BYSOF MSG# UH-60-88-11 ON EH-60A (THOMASCREWS)
17-Nov-1988 4
FRESNO, CA
thomas.m.lilly
AVCRAD, CASOF MSG# UH-60-87-01-PREVIOUSLY C/W,NOT ENTERED ON -15 (-5) (THOMAS CREWS)
17-Nov-1988 5
FRESNO, CA
thomas.m.lilly
AVCRAD, CASOF MSG# UH-60-87-02 TB NUMBER CHANGEPREVIOUSLY C/W (THOMAS CREWS)
17-Nov-1988 6
FRESNO, CA
thomas.m.lilly
AVCRAD, CASOF MSG# UH-60-87-05 PREVIOUSLY C/W(THOMAS CREWS)
17-Nov-1988 7
FRESNO, CA
thomas.m.lilly
AVCRAD, CASOF MSG# UH-60-87-12-PREVIOUSLY C/W,NOT ENTERED ON -15 (-5) (THOMAS CREWS)
17-Nov-1988 8
FRESNO, 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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 4 of 61
AVCRAD, CASOF MSG# UH-60-88-04-REVISION TO 88-02C/W (THOMAS CREWS)
17-Nov-1988 9
FRESNO, CA
thomas.m.lilly
AVCRAD, CASOF MSG# UH-60-88-09-ONE TIME INSP OFARA CREW SEATS FOR LOOSE CLEVISSCREWS C/W AT 146 ACFT HRS (THOMASCREWS)
17-Nov-1988 10
FRESNO, CA
thomas.m.lilly
AVCRAD, CASOF MSG# UH-60-88-13 ONE TIME INSP OFMAIN ROTOR BLADE PINS FOR BROKEN ORMISSING SEGMENTS C/W AT 146.3 ACFT HRS(THOMAS CREWS)
01-Dec-1988 1
FRESNO, CA
thomas.m.lilly
AVCRAD, CASOF MSG# UH-60-88-14--NOT APPLICABLE TOEH-60A AIRCRAFT (THOMAS CREWS)
10-Dec-1988 1
FRESNO, CA
thomas.m.lilly
AVCRAD, FATSOF MSG# UH-60-82-03-CHECK ENGINE OILSIGHT GAGE PRIOR TO 1ST ENGINE STARTAND AFTER EACH FLIGHT C/W (CLIFFBARNES)
10-Jan-1989 1
FRESNO, CA
thomas.m.lilly
AVCRAD,SOF MSG# UH-60-82-18 INSP OF M/R SPINDLEDROOP STOP BEARING AND BEARINGSUPPORT FOR CRACKS C/W (CLIFF BARNES)
10-Jan-1989 2
FRESNO, CA
thomas.m.lilly
AVCRAD,SOF MSG#UH-60A-89-03--ONETIME INSP OFMAIN ROTOR SPINDLES ALL P/N'S CW BY(THOMAS CREWS)
12-Jul-1989 1
FRESNO, CA
thomas.m.lilly
AVCRAD,SOF MSG# UHJ-60A-89-04-CHANGE TO 89.03C/W BY (THOMAS CREWS)
12-Jul-1989 2
FRESNO, CA
thomas.m.lilly
AVCRAD, FATSOF MSG# UH-60A-89-05 ONETIME INSP OFWSPS FOR CONTACT ON WIRE BUNDLE C.WBY CA AVCRAD (THOMAS CREWS)
17-Jul-1989 1
FRESNOC, CA
thomas.m.lilly
TFSI, MOJAVE AIRPORTONE TIME INSP OF R/H RELAY PANEL ASSYSAND L/H RELAY PANEL ASSYS FOR SUSPECTGROUNDING MODULES. C/W 158.2 ACFTHOURS R/H PANEL S/N P-507, L/H PANEL S/NP-1233 EH-60 MAINT SUPERVISOR (RONALDCONWAY)
28-Jul-1989 1
MOJAVE CA
thomas.m.lilly
TFSI, MOJAVE AIRPORTALL H-60 SERIES ACFT REVISION TO RIGHT &LEFT HAND RLAY PANEL C/W L@ 158.2 HRS.EH-60 MAINT SPERICAL (UNKNOWN/LW272R.CLERK)
11-Aug-1989 1
MOJAVE, CA
thomas.m.lilly
TFSI, MOJAVE AIRPORTALL H-60 SERIES ACFT. ONETIME INSP OFFUEL BOOST PUMP HOSE ATTACHMENT C.W@ 158.2 HRS., EH-60 MAINT SUPERVISER(UNKNOWN.LW2720 R.CLERK)
11-Aug-1989 2
MOJAVE, CA
thomas.m.lilly
TFSI, MOJAVE AIRPORTALL H-60-SERIES ACFT CORRECTION OFRETIREMENT LIFE SCHEDULE FOR H-60RETIRMENT LIFE SCHEDULE C/W @ 158.2HRS. EH-60 MAINT SUPERVISOR(UNKNOWN/LW2720 R/CLERK)
17-Aug-1989 1
MOJAVE, CA
thomas.m.lilly
TFSI MOJAVE AIRPORTSOF-MSG-UH-60-89-10 REVISION TO 89-01-, 89-02 ALL H-60 SERIES ACFT ONE TIMEINSPECTIOIN OF G/G ROTOR STARERSHROUDS APPL CABLE CW #19 #2 ENGINESTO BE COMPLIED WITH AT SPECIFIC LIMITS.158.2 HRS. EH-60A MAINT SUPERVISOR(UNKNOWN/LW2720 R.CLERK)
19-Sep-1989 1
MOJAVE, 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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 5 of 61
TFSI MOJAVE AIRPORTSOF MSG UH-60-89-11-ALL H-60 SERIES ACFTONE TIME INSPECTION OF OIL COOLER AXIALFAN C/W @ 1582 HRS IPS LEVEL FORE/AFT .27VERT .8. EH-60A MAINT SUPERVISOR(UNKNOWN/LW2720 R.CLERK)
14-Nov-1989 1
MOJAVE, CA
thomas.m.lilly
TFSI MOJAVESOF MSG UH-60A-89-12 ALL H-60 SERIESACFT, ONE TIME INSPECTION OF OIL COOLERAXIAL FAN C/W @ 158.2 HRS EH-60A MAINTSUPERVISOR (UNKNOWN/LW2720 R.CLERK)
30-Nov-1989 1
MOJAVE AIRPORT
thomas.m.lilly
TFSI MOJAVESOF MSG UH-60-89-13--ALL H-60 SERIESACFT, RESTRICTIONS AGAINST USINGFIGHTING ASSY P/N 70700-20433-045 FORRAPPELING PARACHUTING ANDTRASNPORTABILITY TIEDOWN OPERATIONC/W @ 158.2 HRS. EH-60 MAINT SUPERVISOR(UNKNOWN/LW2720 R.CLERK)
11-Dec-1989 1
MOJAVE AIRPORT CA
thomas.m.lilly
AVCRAD CAUH-60-90-01(TB-55-1520-237-20-113) ONE TIMEINSP AND RECURRING OF MAIN ROTORBLADE EXPANDABLE PIN. C/W AT 198.4 ACFTHRS. @ (CHRIS WACHTER)
19-Apr-1990 1
FRESNO CA
thomas.m.lilly
D CO 3/25 AHBTB-55-1520-237-20-110 ONE TIME INSP OF OILCOOLER AXIAL FAN FOR SUSPECT SERIALNUMBER AND PART NUMBERS COMPLETED04 JUNE 90 AT 235.6 ACFT HRS (WELCH)
04-Jun-1990 1
FORT DRUM, NY
thomas.m.lilly
D CO 3/25 AHBSOF MSG UH-60-90-02 ONE TIME ANDRECURRING INSP OF T/R PITCH BEAMRETAINING NUT AND WASHER C/W 249.9ACFT HRS (WELCH)
13-Aug-1990 1
FORT DRUM , NY
thomas.m.lilly
D 3/25 AHBTB55-1520-237-20-118 ONE TIME INSPECTIONOF TAIL ROTOR PITCH BEAM RETAININGWASHER AND PITCH BEAM RETAINING NUTAND EMPHASIZED RECURRING VISUALINSPECTION COMPLETED 06 SEPT. 90 AT249.9 ACFT. HRS. (WELCH)
13-Aug-1990 2
FT. DRUM, NY
thomas.m.lilly
D 3/25 AHBTB55-1520-237-20-113 INSPECTION FORDEFECTIVE ICERATE INDICATOR COMPLETED25 SEPT 90 AT 261.1 ACFT HRS. (WELCH)
11-Sep-1990 1
FT. DRUM, NY
thomas.m.lilly
OCMSEC ST. LOUIS, MOOCM/ACE PERFORMED AT 0129 A/C HRS. ATFT. DRUM, NY BY ACE TEAM MEMBER FAVSCOM OCMSEC ST. LOUIS MO(UNKNOWN/LW2720 R.CLERK)
19-Sep-1990 1
FT.DRUM, NY
thomas.m.lilly
D 3/25 AHBTB55-1520-237-20-104-NEW OVERHAULRETIREMENT LIFE SCHEDULE FOR H-60COMPLIED WITH (MELT)
16-Oct-1990 1
FT. DRUM, NY
thomas.m.lilly
D3.25 AHBTB55-1520-237-20-111 ONE TIME INSPECTIONOF UPPER PRESSURE PLATE AND SPINDLETO HUB ATTACHMENT BOLT FOR PROPERLENGTH COMPLIED WITH 10 OCT 90 AT 267.6ACFT HRS. (MELT)
16-Oct-1990 2
FT. DRUM, NY
thomas.m.lilly
D CO 3/25 AHBUH-60-91-ASAM-02 RECURRING EROSIONINSPECTION OF MAIN ROTOR BLADES TIPCAPS FOR ACFT INVOLVED IN OPERATIONDERSET SHIELD (BANVILLE)
15-Jan-1991 1
FT. DRUM, NY
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 6 of 61
DCO 3/25 AHBUH-60-91-ASAM-03 EXTENDED TBO'S ON OILCOOLER BLOWER AND TAIL ROTOR PITCHCHANGE SHAFT BEARIND FOR ACFTINVOLVED IN OPERATION DESERT SHIELD(BANVILLE)
15-Jan-1991 2
FT. DRUM, NY
thomas.m.lilly
D CO 3-25TH AHBUH-60-91-ASAM-04-LIFE LIMITS EXTENTEDFOR O.P. DERSERT STORM N/A THIS STATION(JARO)
21-Feb-1991 1
FT. DRUM, NY
thomas.m.lilly
D CO 3-25TH AHBUH-60-91-ASAM-05-ONE TIME INSP OF ALLUH60 FOR FOUR (4) UNSERVICEABLE MAINROTOR SPINDLE ASSY (JARO)
21-Feb-1991 2
FT. DRUM, NY
thomas.m.lilly
D CO. 3-25TH AHBTB 55-1520-237-70-122 ONE TIME INSP. OF M/RSPINDLE FOR CERTAIN SERIAL NUMBERS (DJARO)
21-Feb-1991 3
FT. DRUM N.Y
thomas.m.lilly
D CO 3-25-AHBTB55-1520-237-20-119-ONE TIMEREPLACEMENT AND 30HR SPECIAL INSP OFTAIL ROTOR PITCH BEAM RETAININGWASHER C/W 292.8 HRS. (MELT)
08-Mar-1991 1
FT. DRUM, NY
thomas.m.lilly
D CO 3-25 AHBUH-60-91-ASAM-01--ONE TIMEREPLACEMEANT AND 30HR INSPECTION OFTAIL ROTOR PITCH BEAM RETAININGWASHER (WALSHER)
12-Mar-1991 1
FT. DRUM, NY
thomas.m.lilly
D CO 3-25-AHBUH-60-91-ASAM-06-ONE TIME INSP OF CARGOHOOK INTERNAL WIRE BUNDLE C/W(BARNVILLE)
22-Mar-1991 1
FT. DRUM, NY
thomas.m.lilly
DCO 3/25 AHBUH-60-91-ASAM-08-ONE TIME INSP OF FIREEXTINGUISHING SYSTEM C/W (WINKLE)
27-Mar-1991 1
FT. DRUM,NY
thomas.m.lilly
DCO 3/25 AHBGEN-91-ASAM-03-AUTHORIZATION FORINSTALLATION AND USING CRYPTOGRAPHICCOMPUTER (BARNVILLE)
16-Apr-1991 1
FT. DRUM,NY
thomas.m.lilly
DCO 3/25 AHBUH-60-91-ASAM-09 -30HR SPECIAL INSP OFM/R SPINDLE ELASTOMERIC BEARINGS(WINKLE)
21-May-1991 1
FT. DRUM, NY
thomas.m.lilly
AVSCOM OCMSECOCM/ACE PERFORMED AT 0295 A/C HRS. ATFT. DRUM, NY BY ACE TEAM MEMBER MADENAVSCOM OCMSEC. ST. LOUIS, MO(UNKNOWN/LW2720)
02-Aug-1991 1
ST. LOUIS, MO
thomas.m.lilly
LSI, DOL AVIMUH-60-99-ASAM-09-ONE TIME INSP OF BLADEPINS COMPLETED 1085.9 ACFT HRS. (BRUCE)
12-Aug-1991 1
FT. DRUM, NY
thomas.m.lilly
D CO 3/25 AHBI/A/W UH-60-92-ASAM-01--ONE TIME S/NCHECK OF ALL MAIN ROTOR SPINLDE ASSY(BANVILLE)
07-Jan-1992 1
FT. DRUM, NY
thomas.m.lilly
D CO 3/25 AHBI/A/W TB1-1520-237-30-2-INSP OF ALL H-60ACFT INVOLVED IN DESERT STORM N/A THISACFT (BANVILLE)
05-Mar-1992 1
FT. DRUM, NY
thomas.m.lilly
D CO 3/25 AHBUH-60-92-ASAM-02--ONE TIME INSP OF NO1 &NO.2 FOR THIS SHAFT C/W (BANVILLE)
12-May-1992 1
FT. DRUM, NY
thomas.m.lilly
AVSCOM OCMSECOCM/ACE PERFORMED AT 0389 A/C HRS. ATFT. DRUM, NY ACE TEAM MEMBER 0 AVSCOMOCMSEC ST. LOUIS MO (UNKNOWN/LW2720 R.CLERK)
24-Jun-1992 1
ST. LOUIS
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 7 of 61
D CO 3/25 AHBUH-60-92-ASAM-03-PURPOSE TO INSTITUTENEW ENGINE CLEANING PROCEDURES TOPREVENT DIRT BUILDUP (KEVIN YOAKUM)
04-Sep-1992 1
FT. DRUM, NY
thomas.m.lilly
D CO 3-25 AHBUH-60-92-ASAM-04-AS OF 1 JUL 92 CLEAN AIRACT PROHIBITS INTENTIONAL RELEASE OFCFC/FREON DURING MAINTENCE OFREFRIGERATION AND AIR CONDITIONINGSYSTEMS (KEVIN YOAKUM)
04-Sep-1992 2
FT. DRUM, NY
thomas.m.lilly
DCO 3-25 AHBUH-60-92-ASAM-05-INSPECTION ANDREPLACEMENT OF M/R BLADE EXPANDABLEPINS TO ELIMINATE 10HR/14DAYSINSPECTION OF PINS PER UH-60-90-01 (KEVINYOAKUM)
08-Sep-1992 1
FT.DRUM, NY
thomas.m.lilly
D CO 3-25TH AHBUH-60-92-ASAM-06-ONE TIME INSPECTIONFOR PROPER HARDWARE ON PEDALADJUSTER ASSEMBLY C/W (KEVIN YOAKUM)
28-Sep-1992 1
FT. DRUM, NY
thomas.m.lilly
LSSIMWO 55-1520-237-50-58-ENGINE DRIVESHAFTBALANCING PROCDURES COMPLIED WITH BY(GILBERT)
07-Oct-1992 1
LSSI 343 CFT
thomas.m.lilly
DCO 3-25 TH AHBUH-60-93-ASAM-01 ONE TIME OPERATIONALCHECK OF THE XMSN AND GEARBOX CHIPDETECTOR SYSTEMS COMPLETED THISDATED AT 440.9 ACFT HRS (KEVIN YOAKUM)
14-Oct-1992 1
FT. DRUM, NY
thomas.m.lilly
DCO 25TH AVN REGTUH-60-93-ASAM-04--ONE TIME INSPECTIONFOR PROPER HAND WANE ON THE PEDALADJ ASSY P/N 70400-01613 COMPLETED 15DEC 92 AT 447.8 ACFT HRS (LANGENWATER)
15-Dec-1992 1
FT. DRUM, NY
thomas.m.lilly
DCO 25TH AVN REGTUH-60-93-ASAM-06-ONE TIME INSPECTION OFT/R PITCH BEAMS TO REMOVED SUSPECTS/N'S COMPLETED 22 DEC 92 AT 447.8 ACFTHRS BY (KEVIN LANGEWATER)
22-Dec-1992 1
FT. DRUM, NY
thomas.m.lilly
DCO 3/25 AHBUH-60-93-ASAM-07 H-60 HELICOPTERREVISION OF COROSION LIMITS FOR TAILROTOR GEAR BOX SERVO MAOUNTING BORE(KEVIN YOAKUM)
31-Dec-1992 1
FT. DRUM, NY
thomas.m.lilly
DCO 3-25 AHB FT.DRUM, NY
UH-60-93-ASAM-10-ONE TIME ANDRECURRING INSPECTION /CLEANING OF THEEXTERNAL STORES SUPPORT SYSTEMSESSS NOT INSTALLED ON THIS AIRCRAFT(TORRES)
16-Apr-1993 1
FT. DRUM, NY
thomas.m.lilly
D CO 3-25 AHBUH-60-93-ASAM-11-INSPECT AND REPLACEARA CREW RESTRAINT BOCKLE CROTCHASSEMBLIES C.W (TORRES)
16-Apr-1993 2
FT. DRUM, NY
thomas.m.lilly
DCO 3-25 AHBUH-60-93-ASAM-08-TO BIAS TAIL ROTORRIGGING THREE DEGRESS COMPLIED WITH30 APR 93, 492.6 ACFT HRS (EGLY)
03-May-1993 1
FT. DRUM, NY
thomas.m.lilly
DCO 3-25 AHBUH-60-93-ASAM-12-ABRUPT CHANGE IN MAINROTOR TRACK/ VIBRATION COMPLIED WITH492.6 ACFT HRS (EGLY)
03-May-1993 2
FT. DRUM, NY
thomas.m.lilly
DCO 3-25 AHBUH-60-93-ASAM-02-T700GG ROTOR CLEANINGAND SINGLE ENGINE OPERATIONINFORMATION COMPLIED WITH 492.6 ACFTHRS (EGLY)
11-May-1993 1
FT. DRUM, NY
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 8 of 61
DCO 3-25 AHBUH-60-93-ASAM-03--INSP AND REPLACEMENTOF MAIN ROTOR EXPAN. PIN COMPLIED WITH447.8 ACFT HRS. (EGLY)
11-May-1993 2
FT. DRUM, NY
thomas.m.lilly
DCO 3-25 AHBUH-60-93-ASAM-09-ONE TIME INSP TODETERMINE COMPLIANCE WITH SYSTEMMWO'S 492.6 ACFT HRS. (EGLY)
11-May-1993 3
FT. DRUM, NY
thomas.m.lilly
E CO 25TH AVN REGTUH-60-93-ASAM-13--ALL H-60 ACFT WITHEXTERNAL STORES SUPPORT SYTEM ANDEXTENEDE RANGE FUEL SYSTEM KITS (HUFF)
10-Jun-1993 1
FT. DRUM, NY
thomas.m.lilly
ECO 25TH AVN REGTUH-60-93-ASAM-13-ALL H-60 ACFT WITH ESSS& EFFS INST INSP. EJECTOR RACK (HUFF)
22-Jun-1993 1
FT. DRUM, NY
thomas.m.lilly
ECO 25TH AVN REGTUH-60-93-ASAM-14-AND ASAM-15 INSP OFESSS AND ERFS COMPLIED WITH ON 23 JUN93 AT 499.8 ACFT HRS. (HUFF)
23-Jun-1993 1
FT. DRUM, NY
thomas.m.lilly
FT. DRUM, NYACE/ACCE PERFORMED AT 500 A/C HRS(HUFF)
12-Jul-1993 1
FT. DRUM, NY
thomas.m.lilly
ECO 25TH AVN REGTUH-60-93-ASAM-05--ONE TIME INSP OF T/RDRIVESHAFT VISCOUS DAMPER BEARINGSCOMPLETED 16 JUL 93 499.8 ACFT HRS(HUFF)
16-Jul-1993 1
FT. DRUM, NY
thomas.m.lilly
ECO 25TH AVN REGTUH-60-93-ASAM-16--ONE TIME INSP OF HYOPUMP 70652-02300-050-KNURLEDBLEED/RELEIF KNOB SECURING PINCOMPLETED 29 JUL 1993 499.8 HRS (HUFF)
29-Jul-1993 1
FT. DRUM, NY
thomas.m.lilly
ECO 25TH AVN REGTPMSII COMP 499.8 ACFT HRS (HUFF) 24-Oct-1993 1
FT. DRUM, NY
thomas.m.lilly
E 25 AVN RGTUH-60-94-ASAM-01--ONE TIME INSP OFMASTER FAULT PANELS C/W FOR NVGREQUIREMENTS (HUFF)
03-Dec-1993 1
FT. DRUM,
thomas.m.lilly
D CO 3-25 AHBUH-60-94-ASAM-02 (TB1-1520-237-20-149) INSPOF BUCKLE/CROTCH ASSY. C/W AT 510.8 HRS(KYOAKUM)
24-Jan-1994 1
FT. DRUM, NY
thomas.m.lilly
D CO 3-25 AHBUH-60-94-ASAM-03 TB1-1520-237-20-151 INSPOF M/R SPINDLES AND THRUST BEARINGSC/W AT 510.8 ACFT HRS (KYOAKUM)
24-Jan-1994 2
FT. DRUM, NY
thomas.m.lilly
D CO 3-25 AHBUH-60-94-ASAM-04 REISSUE OF ONE TIMEINSP. TO REMOVE SUSPECT TAIL ROTORPITCH BEAMS (UNKNOWN/LW2720 R.CLERK)
02-Feb-1994 1
FT. DRUM, NY
thomas.m.lilly
D CO 3-25 AHBTHIS IS A REISSUE OF UH-60-93-ASAM-06 C/W513.4 ACFT HRS. (UNKNOWN/LW2720R.CLERK)
02-Feb-1994 2
FT. DRUM ,NY
thomas.m.lilly
DCO 3-25 AHBUH-60-94-ASAM-05-ALL H-60 ACFT DUE TIMEREMOVAL OF TAIL G/B W/TAIL G/B OUTPUTSHAFT, P/N 70358-06620-101 FOR REWORKTB1-1520-237-20-152 C/W AT 518.9 ACFT HRS.(ROSS)
12-Feb-1994 1
FT. DRUM, NY
thomas.m.lilly
D CO 3-25 AHBUH-60-94-ASAM-07-CHANGE TO H-60OVERHAUL AND RETIREMENT TABLE TB1-1520-237-20-154 C/W AT 522.7 ACFT HRS(UNKNOWN/LW2720 R.CLERK)
11-Mar-1994 1
FT. DRUM, NY
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 9 of 61
D CO 3-25 AHBUH-60-94-ASAM-08-REVISION TO UH-60-94-ASAM-07 CHANGE TO H-60 OVERHAULRETIREMENT TABLE TB1-1520-237-20-154 C/WAT 522.7 ACFT HRS (UNKNOWN/LW2720R.CLERK)
14-Mar-1994 1
FT. DRUM, NY
thomas.m.lilly
D CO 3-25 AHBUH-60-94-ASAM-09--ALL H-60 ACFT, REMOVALOF CERTAIN PRIMARY SERVO ASSY TB1-1520-237-20-155 C/W AT 544.7 ACFT. HRS (ROSS)
18-Apr-1994 1
FT. DRUM, NY
thomas.m.lilly
FT. DRUM, NYACE/AACE PERFORMED AT 0603 A/C HRS(ROSS)
27-Sep-1994 1
FT. DRUM, NY
thomas.m.lilly
D CO 3-25 AHBUH-60-95-ASAM-01-TB1-1520-237-20-157 UH-60/EH-60, HOIST AND RECOVERY OF UH-60/EH-60 FIXED PROVSIONAED HELICOPTER C/WAT 950.6 ACFT HRS. (ROSS)
20-Oct-1994 1
FT. DRUM, NY
thomas.m.lilly
DCO 3-25 AHBUH-60-95-ASAM-02 TB1-1520-237-20-159 ALL H-60 AIRCRAFT REQUIREMENT TO OPERATETHE FUEL TANK SUBMERGED BOOST PUMPS.ON AT ALL TIMES WITH ALL FUELS PARINGGROUND AND FLIGHTS OPERATIONS C/W AT950.6 ACFT HRS (ROSS)
20-Oct-1994 2
FT. DRUM, NY
thomas.m.lilly
D CO 3-25 AHBUH-60-95-ASAM-03 TB1-1520-237-20-158-ALL H-60 ACFT. RESHIMMING REQUIREMENT OF T/RBLADE PIVOT BEARING AND ONE TIME INSP.FOR SPECIFIED S/N T/R BLADES UH-60-95-ASAM-04 REDUCTION OF TORQUES OF SELF-RETAINING PIVOT BOLTS (ROSS)
27-Oct-1994 1
FT. DRUM, NY
thomas.m.lilly
D C0-3.25-AHBUH-60-95-ASAM-05 THREE PART INSPPROCEDURE FOR ALL H-60 BLACKHAWKHELICOPTERS EXCEPT MK-60K. FORHISTORICAL RECORD INSP., ULTRASONICINSP. OF T/R GEARBOX OUTPUT SHAFT P/N70358-06620-101 AND REMOVAL OF T/RGEARBOXES WITH SHAFTS REQUIRINGREWORK. (ROSS)
06-Dec-1994 1
FT. DRUM, NY
thomas.m.lilly
DCO 3-25 AHBUH-60-95-ASAM-05-TB1-1520-237-20-163 ALL H-60 ACFT, CHANGE IN RETIRMENT LIFE OFSERVO BEAM RAILS C/W AT 604.4 ACFT HRS.(HAASE)
25-Jan-1995 1
FT. DRUM, NY
thomas.m.lilly
DOL AVIMUH-60-95-ASAM-04 ALL UH-60 ACFTREDUCTION OF TORQUE OF SELF-RETAININGPIVOT BOLTS TB1-1520-237-20-160 (LAISDELL)
26-Jan-1995 1
FT. DRUM, NY
thomas.m.lilly
DCO 3/25 AHBUH-60-95-SOF -02 --TB1-1520-237-20-161 ONETIME VISUAL INSP OF ALL H-60 M/R/B CUFFSC/W AT 604.4 ACFT HRS. (HASSE)
15-Feb-1995 1
FT. DRUM, NY
thomas.m.lilly
SIKORSKY AIRCRAFTUH-60-95-SOF-01TB1-1520-237-20-162--ULTRASONIC INSP OF T/R/G/B OUTPUT SHAFTP/N 70358-06620-101 COMPLETED @ 611.9ACFT HRS. ON T/R G/B/ SER #A006-00996(SIKORSKY)
15-Mar-1995 1
FORT DRUM, NY
thomas.m.lilly
CCO 3/25 AHBCM/ACE PERFORMED AT 612 A/C HRS. AT FT.DRUM, NY BY ACE TEAM MEMBER M ATCOMOCM SECTION ST. LOUIS, MO (MOORE)
27-Jun-1995 1
FORT DRUM, NY
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 10 of 61
E CO 25TH AVN REGTUH-60-95-ASAM-06---TB1-1520-237-20-168-ONETIME INSP FOR CRACKED MAIN XSNM BEAMSUPPER DECK SKIN CRACKS, FRAME CRACKSC/W 611.9 ACFT HRS. (HAASE)
12-Jul-1995 1
FT. DRUM, NY
thomas.m.lilly
E CO. 25TH AVN REGTUH-60-95-ASAM-07-ONE TIME INSP OF ALLGUNNER TROOP SEATS UPPER ATTEN WIRESAND ROLLER BRNGS FOR DAMAGE, WEAR,FREEDOM OF MOVEMENT AND PRESENCE OFCRESCENT BUSHING AND INSPPILOT/COPILOT SEATS FOR PROPER ICSCORD ROUTING COMPLIED WITH 611.9 ACFTHRS. (HASSE)
12-Jul-1995 2
FT. DRUM, NY
thomas.m.lilly
E CO 25TH AVN REGTTAIL ROTOR BIASED IAW TM 1-1520-237-23-5FOR REPL OF T/R G/B BK A 5.500 B 5.875 BL A5.500 B5.875 YA 6.250 B6.625 RA 6.250 B6.625611.9 ACFT HRS (GASSE)
31-Aug-1995 1
FT. DRUM, NY
thomas.m.lilly
DCO 3-25 AHBSOF UH-60-96-01-CHANGE IN RET. LIFE OFFWD BELLCRANK SUPPORT ASSY MFD BYHICKSVILLE MACHINE WKS AND REMOVALOF SPECIFIED SERIAL NUM. FWD BELLCRANKSUPPORT ASSY C/W AT 623.4 ACFT HRS.(KILMARTIN)
07-Nov-1995 1
FT. DRUM, NY
thomas.m.lilly
D 3-25 AHBUH-60-96-ASAM-02 TB1-1520-237-20-171-ONETIME INSPECTION FOR SUSPECT MAINROTOR SHAFT BOLTS ALL H-60 ACFTCOMPLETED AT 625.2 ACFT HRS. (JS5031)
30-Nov-1995 1
FT. DRUM, NY
thomas.m.lilly
D CO 3-25 AHBUH-60-96-ASAM-01 TB1-1520-237-20-170REPLACEMENT OF BOLTS IN IMPROVEDFLIGHT CONTROL SYSTEM. N/A THIS ACFT(JS8453)
01-Dec-1995 1
FT. DRUM, NY
thomas.m.lilly
DCO 3-25 AHBUH-60-95-ASAM-08-T-700-GE700AND T700-GE701 PROVIDE INFO TO IDENTIFY ENGINESWITH UNDAMPED G/G TURBINE BLADES C/W625.2 A/C HRS. (ROSS)
05-Dec-1995 1
FT. DRUM, NY
thomas.m.lilly
D . CO 3-25 AHBSOF-UH-60-96-02 TECHNICAL, INTERIMCHANGE TO RETIRMENT LIFE OF INBD RETPLATES SNC 1234-001-THR C1234-150 ANDRMVL OF SN FM0001 THR FM00142 C/W 625.2ACFT HRS SOF UH-60-96-03 TB1-1520-237-20-174 TECHNICAL, INTERIM CHANGE TORETIREMENT LIFE OF M/R/B CUFF PN70150-09109-041 WITH SN FM0080 THRU FM0679 C/WAT 625.2 ACFT HRS. (STEVENS)
06-Dec-1995 1
FT.DRUM, NY
thomas.m.lilly
D CO 3-25 AHBUH-60-SOF-96-04-REMOVAL OF SPECIFICSERIAL NUMBER AFT BELLCRANK SUPPORTASSY TB1-1520-237-20-175 COMPLIED WITHTHIS DATED AT 627 ACFT HOURS. (SHAFFER)
14-Dec-1995 1
FT. DRUM, NY
thomas.m.lilly
D CO 3-25 AHBUH-60-96-ASAM-03 REVISION TO ONE TIMEINSPECTION FOR SUSPECT MAIN ROTORSHAFT NUT BOLTS ON ALL H-60 ACFTCOMPLIED WITH AT 625.2 ACFT HRS. (JS8453)
01-Feb-1996 1
FT. DRUM, NY
thomas.m.lilly
D CO 3-25 AHBUH-60-96-ASAM-04 TB1-1520-237-20-176REDUCTION IN MAX ALLOWABLE LOAD ON(FRIES) FAST ROPE INSERTION EXTRACTIONSYSTEM N/A THIS ACFT (JS5031)
01-Feb-1996 2
FT. DRUM, NY
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 11 of 61
D CO 2-10TH AVN REGTUH-60-96-ASAM-05-ONE TIME INSP FOR FWDBELLCRANK SUPPORT ASSEMBLIES MADEBY HICKSVILLE MACHINE WORK INCREASESERVICE LIFE FROM 500 HRS TO 1800 HRSREVISED TB1-1520-237-20-172 COMPLIEDWITH THIS DATE AT 653 ACFT HRS. (JS8453)
19-Jul-1996 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10TH AVN REGTUH-60-96-ASAM-07 TB1-1520-237-20-179- TB1-1520-250-20-4-ONE TIME INSP OF CERTAIN M/RSPINDLE RETAINING RODS COMPLIED WITHAT 703 ACFT HRS (JS8453)
23-Aug-1996 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10TH AVN REGTUH-60-96-ASAM-06 TB1-1520-237-20-143-INFORMATIONAL ALL H-60 ACFT UH-60A MAINROTOR SPINDLE CRACK (JS8453)
05-Sep-1996 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10TH AVN REGTUH-60-96-ASAM-09 INSP OF STAB ACTUATORCLEVIS, DUE NLT THE NEXT SCHEDULED PMS-2 OR AS SOON AS PRACTIC AL C/W AT 706AC HRS (JS8453)
16-Sep-1996 1
FT. DRUM ,NY
thomas.m.lilly
D CO 2-10TH AVN REGTUH-60-96-ASAM-10 MANDATORYREPLACEMENT OF SLEEVE BEARING IN ALLELASTOMERIC BEARING ASSEMBLIESDURING ALL RECURRING PMS-II C/W AT 706ACFT HRS (JS8453)
16-Sep-1996 2
FT.DRUM, NY
thomas.m.lilly
D CO 2-10TH AVNUH-60-96-ASAM-09 INSP OF STAB ACTUATORCLEVIS DUE NLT THE NEXT SCHEDULED PMS-2 OR AS SOON AS PRACTICAL. C/W AT 1461.1ACFT HRS. (JS8453)
16-Sep-1996 3
FT. DRUM, NY
thomas.m.lilly
D CO 2-10TH AVN REGTACFT HISTORICAL RECORDS TRANSCRIBEDTO ULLS-A SYS THIS DATE AT 706 ACFT HRSIN ACCORDANCE WITH INSTRUCTIONSPROVIDED BY THE PRECONVERSION TEAM.(JS8453)
17-Sep-1996 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVN REGTUH-60-96-ASAM-11--TB1-1520-237-20-8-TB1-1520-237-20-183 CHANGE IN RETIREMENT LIFEOF FENN MANUFACTURED MAIN ROTORBLADE CUFFS FROM 75HRS TO 450HRSCOMPLETED AT 706.0 ACFT HRS. (JS5031)
25-Sep-1996 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVN REGTUH-60-97-ASAM-01--MAINTENACE MADATORYALL H-60 BLACKHAWK HELICOPTERSINSPECTION OF ALL MAIN ROTOR HUBASSYS. (WM2099)
07-Oct-1996 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVN REGTUH-60-97-ASAM-02-MAINTENACE MANDATORYALL UH-60A/L AND EH-60 HELICOPTERS, ONETIME INSPECTION OF TAIL DRIVE FLEXIBLECOUPLING CONNECTIONS (WW2099)
15-Oct-1996 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVN REGTUH-60-97-ASAM-03 MAINTENANCEMANDATORY ALL UH-60A/L AND EH-60AAIRCRAFT WITH T700-GE-700 ENGINES-REPLACEMENT OF UNDAMPED GASGENERATOR ROTOR/STATOR ASSY (WW2099)
28-Oct-1996 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10TH AVN REGT.UH-60-97-ASAM-04, TB1-1520-237-20-186 ANDTB1-1520-20-250-20-11, CHANGE INRETIRMENT LIFE OF MAIN ROTOR BLADECUFF MANUFACTURED BY FENNMANUFACTURING COMPLIED WITH AT 708.2ACFT. HRS. (JO7550)
26-Dec-1996 1
FT. DRUM, NY
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 12 of 61
D CO 2-10TH AVN REGT.UH-60-SOF-97-01, TECHNICAL, REMOVAL OFCERTAIN REWORKED MAIN ROTORSWASHPLATE ASSY, ALL UH-60A/L AND EH-60A HELICOPTERS WITH CERTAIN S/NVERIFIED BY RECORDS CHECK. (DK2698)
14-Jan-1997 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10TH AVN REGT.UH-60-97-ASAM-05, MAINTENANCEMANDATORY, ALL UH-60A/L, EH-60AAIRCRAFT, ONE-TIME INSPECTION FORREMOVAL AND REWORK OF CERTAINVISCOUS DAMPER BEARING SUPPORTASSY'S TB1-1520-237-23-3 (DK2698)
14-Jan-1997 2
FT. DRUM, NY
thomas.m.lilly
D CO 2-10TH AVNUH-60-97-ASAM-06, MAINTENANCEMANDATORY, ALL UH-60A/L, EH-60AAIRCRAFT WITH THE LATERAL BELLCRANKASSY. P/N 70400-08150-045, MANUFACTUREDBY "PURDY MACHINE COMPANY" REMOVALREQUIRED IF IN EXCESS OF 360 TSN HRS,AND OR 30 DAYS OF MESSAGE RECEIPT(DK2698)
14-Jan-1997 3
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVN REGTUH-60-97-ASAM-07, MAINTENACEMANDATORY, ALL H-60 AIRCRAFT,REPLACEMENT OF SPECIFIC SERIALNUMBERED MANUFACTURED TAIL ROTORSERVO CYLINDER ASSY'S PN2227000-9, 13-17.TB1-1520-237-20-188 (DK2698)
14-Jan-1997 4
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVN REGTUH-60-97-ASAM-08, MAINTENACEMANDATORY, ALL H-60 AIRCRAFT WITH THECONNECTING LINK ASSY PN 70400-08155-056,MANUFACTURED BY "PURDY MACHINECOMPANY" TB1-1520-237-20-187 (DK2698)
14-Jan-1997 5
FT. DRUM, NY
thomas.m.lilly
D CO 2-10TH AVN REGTUH-60-97-ASAM-09, MAINTENACEMANDATORY, ONE TIME INSPECTION FORSPECIFIC SERIAL NUMBERS ON P/N70351-08186-043 MAIN ROTOR SHAFT EXTENSIONASSY'S WITH CAGE CODE NUMBERS 15152OR 82001. THIS MESSAGE REDUCED LIFETIME TOO 2100 HRS (DK2698)
23-Jan-1997 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVIATIONREGIMENT
UH-60-97-ASAM-10, MAINTENANCEMANDATORY, UH-60A/EH-60A INSP FORSUSPECT MAIN SUPPORT BRIDGE ASSY'S S/N0121AI THRU 0168AI, REDUCTION INRETIREMENT LIFE. (DK2698)
13-Feb-1997 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVN REGTUH-60-97-ASAM-11 INCREASE IN RETIREMENTLIFE OR CERTAIN SIX LUG M/R BLADE CUFFS.C/W AT 788.5 ACFTS HRS (JS6288)
21-Mar-1997 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVN REGTUH-60-97-ASAM-12, INFORMATIONAL, THISRESCINDS SOF MESSAGE 96-02 FOR FENNMANUFACTURED INBOARD RETENTIONPLATES S/N FM00001 THROUGH FM 00142.INCREASE RETIRMENT LIFE TO 12,000 ACFTHOURS. (JB3106)
14-Apr-1997 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVN REGTH-60-97-ASAM-13, ALL H-60 ACFT, ONE TIMEINSP OF M/R SPINDLE BEARING SLEEVECOMPLETED ON 06 JUN 97 (JS6288)
06-Jun-1997 1
FT. DRUM, NY
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 13 of 61
D CO 2-10 AVN REGTJACE INSPECTION PERFORMED AT 863 ACFTHRS BY (M) JACE TEAM MEMBER MWO/OLRATCOM ST. LOUIS MO (JS5031)
10-Jul-1997 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVN REGTUH-60-97-ASAM-14 TB1-1520-237-20-195 ONETIME INSP OF BELLCRANK P/N 70400-08158-101 FOR SUSPECT CAGE CODE 1W160(JS5031)
14-Aug-1997 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVNUH-60--97-ASAM-15 TB1-1520-237-20-196 ONETIME INSP OF M/R P/C LINK ROD END P/N70101-08202-101 FOR CAGE 40137 (JS5031)
14-Aug-1997 2
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVN REGTUH-60-97-ASAM-16 TB1-1520-237-20-198 ONETIME INSP OF SWASHPLATE LINKAGE CLEVISCONNECTORS P/N 770400-08151-050 FORSUSPECT CAGE (2A622) MFG BY AIRBORNEAPPAREL. (JS5031)
14-Aug-1997 3
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVN REGTUH-60-97-ASAM-17 TB1-1520-237-20-199-INSPOF ALL H-60 SERIES WITH THE INTERNALRESCUE HOIST BRACKET ASSEMBLY P/N70800-02508-046 INSTALLED (JS5031)
15-Aug-1997 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVN REGTUH-60-97-ASAM-18 TB1-1520-237-20-201 ONETIME VISUAL INSPECTION OF M/RSWASHPLATE ASSY'S FOR SUSPECT SN'S(JS5031)
10-Sep-1997 1
FT. DRUM, NY
thomas.m.lilly
2-10 AVN REGTUH-60-97-ASAM-19--ONE TIME INSPECTION OFANVIS/HUD POWER SUPPLY (JS3106)
30-Sep-1997 1
FT. DRUM, NY
thomas.m.lilly
D CO-2-10 AVN FT.DRUM, NY
UH-60-98-ASAM-01 REVISION OF SERVICELIFE OF CERTAIN M/R SHAFT EXTENSIONS,FROM 2100 TO 14000 HOURS N/A THIS ACFT(JK5511)
02-Oct-1997 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVN REGTUH-60-98-ASAM-02 ONE TIME INSP FORSUSPECT PUSH RODS P/N 70400-08155-050/051 MANUFACTURED BY VERSATILEMACHINING WITH CAGE CODE 6S522COMPLIED WITH ON THIS DATE (JG4714)
09-Oct-1997 1
FT. DRUM, NY
thomas.m.lilly
2-10TH AVNUH-60-98-ASAM-03 ONE TIME INSP. OFSWASHPLATE LINK ASSY. C/W 973.9 ACFTHRS (EK3084)
04-Nov-1997 1
FT. DRUM, NY
thomas.m.lilly
C-CO 10TH AVNJACE COMPLETED AT 989 A/C HRS BY JACEMEMBER LL AMCOM OLR/MWO BRANCH(UNKNOWN/LW2720 R/CLERK)
08-Jan-1998 1
FT. DRUM, NY
thomas.m.lilly
C-CO 10TH AVNUH-60-98-ASAM-04 INSP OF OVERHAULEDPRIMARY YAW BOOST, COLLECTIVE BOOSTAND TAIL SERVOS FOR LOOSE HACK BOLTSC/W 984.1 ACFT HRS. (UNKNOWN/LW2720R/CLERK)
11-Mar-1998 1
FT. DRUM, NY
thomas.m.lilly
C-CO 10TH AVNUH-60-98-ASAM-05-INSP OF SWASHPLATELINK ASSY FOR P/N 70400-08110-054/061 TEKCAGE CODE 05780 C/W 985.1 ACFT HRS.(UNKNOWN/LW2720 R/CLERK)
20-May-1998 1
FT. DRUM, NY
thomas.m.lilly
C-CO 10TH AVNPMS2 COMPLETED AT 988.6 A/C HRS NEXTPMS2 DUE AT 1488.6 A/C HRS. (KAMMEYER)
27-Aug-1998 1
FT. DRUM, NY
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 14 of 61
C CO 2/10 AVN REGTUH-60-98-ASAM-07-ONETIME INSP OF ALL H-60 ACFT FOR SUSPECT LEFT TIE RODPN70400-08115-043 CAGE CODE 3R021 C/W AT996.6 ACFT HRS. (ARNOLD)
18-Sep-1998 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10TH AVN REGTUH-60-99-ASAM-03-ALL UH/EH-60A, ONE TIMEINSP OF ALL T700-GE-700 ENGINE RECORDSC/W THIS DATE AT 1000.00 HRS (KAMMEYER)
09-Nov-1998 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVN REGTUH-60-99-ASAM-01-ALL H-60 ACFTRESTORATION OF FULL SERVICE LIFE OF THESWASHPLATE LINK ASSY. P/N 70400-08110-054/061 MANUFACTURED BY TEK (CAGECODEE65780) C/W THIS DATE AT 998.7 ACFTHRS. (BRUCE)
11-Nov-1998 1
FT. DRUM ,NY
thomas.m.lilly
D CO 2-10 AVN REGTUH-60-99-ASAM-02--ONE TIME INSPECTION OFEXTERNAL RESCUE HOISTS MANUFACTUREDBY BREEZE-EASTERN, MSG C/W THIS DATE @998.7 ACFT HRS (BRUCE)
11-Nov-1998 2
FT. DRUM, NY
thomas.m.lilly
D CO 2-10TH AVN REGTUH-60-99-ASAM-04 ALL H-60, T700-GE-701/701C ENGINE ODV RELATED FLAMEOUTS(INFORMATIONAL) COMPLIED WITH AT 1000.0ACFT HRS. (KAMMEYER)
01-Dec-1998 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10TH AVNUH-60-99-ASAM-05--ALL H-60, ONE TIME INSPOF THE MAIN ROTOR SPINDLE BEARINGASSY FOR EXISTENCE OF SLEEVE BEARINGCOMPLIED WITH AT 1003.4 ACFT HRS(KAMMEYER)
13-Dec-1998 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10TH AVN REGTUH-60-99-ASAM-06--ALL H-60, ONE TIME INSPAND REVISED RETIRMENT LIFE OF MAINROTOR PITCH HORNS COMPLIED AT 1003.4ACFT HRS. (BRUCE)
14-Dec-1998 1
FT DRUM , NY
thomas.m.lilly
LMLMJACE COMPLETED AT 1045 ACFT HRS BYJACE MEMBER G AMCOM OLR/MWO BRANCH(EH9090)
21-Jan-1999 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10TH AVN REGTUH-60-99-ASAM-07 ALL H-60, ONE TIME INSPAND REVISED SCHEDULING OF MAIN ROTORHUB NDI COMPLIED AT 1019.3 ACFT HRS.(BRUCE)
06-Apr-1999 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVN REGTUH-60-99-ASAM-08-ALL H-60 ACFT, REVISEDRETIRMENT LIFE OF BELLCRANK SUPPORTASSY. 042/043/045 COMPLETED 1059.9 ACFTHRS. (BRUCE)
20-Jul-1999 1
FT. DRUM, NY
thomas.m.lilly
D.CO 2-10 AVN REGTH-60-99-ASAM-10---ALL H-60 ACFT, ONE TIMEINSP OF R/H CROSSFEED BREAKAWAY FUELVALVE W/PART #70307-03006-103 COMPLETEDAT 1085.9 ACFT. HRS. (BRUCE)
24-Aug-1999 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10TH AVN REGT.UH-60-99-ASAM-12 INSPECTION INTERVALCHANGE FOR HAMILTON STANDARD HMU'SP/N'S GO1, G04, G06, G09 AND G11 ON T700-GE-700 ENGINES C/W AT 1087.9 ACFT HRS.(BRISTON)
25-Aug-1999 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10TH AVN REGTUH-60-99-ASAM-11-ONE TIME INSPECTION OFT700-GE-700/701 ENGINES COMPLETED AT1085.9 ACFT HRS. (COLE)
25-Aug-1999 2
FT. DRUM, NY
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 15 of 61
D CO 2-10TH AVNUH-60-00-ASAM-01--ALL H-60 ACFT, REVISEUH-60-99-ASAM-07 TO INCREASE INSPINTERVAL ON M/R HUB COMPLETED WITH AT1111.1 ACFT HRS. (COLE)
19-Nov-1999 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVNUH-60-00-ASAM-03-ALL H-60 AIRCRAFTINSPECTION AND REMOVAL OF SUSPECTSERVO ASSEMBLIES COMPLIED WITH AT1132.0 ACFT HRS. (DH)
18-Jan-2000 1
FT. DRUM, NY
thomas.m.lilly
DOL AVIMAUTHORIZATION GRANTED TO REPLACE THEINBD AND OUTBD BUSHINGS IN FWDSUPPORT BELLCRANK ASSY I/A/W DMWR 55-1520-237 AND LAR LTR DTD 11 FEB 00 C/W AT1132.0 ACFT HRS (FLUENT)
11-Feb-2000 1
FT. DRUM, NY
thomas.m.lilly
DOL AVIM LSIUH-60-00-ASAM-04---INSPECTION OF TAILLANDING GEAR STRUT FOR SPECIFIC S/N,WITHIN NEXT 10 FLT HRS NLT 08 MAR 2000C/W AT 1132 HRS (TB0588)
28-Feb-2000 1
FT. DRUM, NY
thomas.m.lilly
DOL AVIM LSIACFT M/R RIGGING HAS BEEN CHECKED ANDNO ADJUSTMENT HAVE BEEN MADE AT THISTIME, SEE ATTACHED RIGGING SHEET FORRIGGING INFORMATION C/W AT 1132.0 ACFTHRS. (FLUENT)
01-Mar-2000 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVNUH60-00-ASAM-05-ALL H-60 SEIRES AIRCRAFTTAIL NUMBER 77-22715-9026367 INSP OF FIREEXTINGUISHER WIRING I/A/W TM1-1520-237-23ACFT HRS. 1152.1 COMPLETED (TN8278)
19-May-2000 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVNUH-60-00-ASAM-06--INSP FIRE EXTINGUISHERWIRING IAW CHANGE #1 TO TB1-1520-237-20-219 ACFT HRS. 1183.0 N/A TO ACFT. (KB3648)
22-Jun-2000 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10-AVNSOF UH-60-00-01-ALL H-60 ACFT, INITIAL ANDRECURRING INSP OF MAIN ROTOR SPINDLELUGS C/W AT 1184.0 ACFT HRS 13 JUL 00(MB4060)
13-Jul-2000 1
FT. DRUM, NY
thomas.m.lilly
DCO 2-10SOF UH-60-00-02 ALL H-60 ACFT , REMOVALOF INPUT MODULE GENE BOX ASSEMBLIESWITH POTENTIALLY CRACKERS BEVELGEARS C/W AT 1189.8 HRS (KK3148)
04-Aug-2000 1
FT. DRUM, NY
thomas.m.lilly
LMLMACE COMPLETED AT 1184 ACFT HRS BY ACEMEMBER L AMCOM OLR/MWO BRANCH(EH9090)
11-Aug-2000 1
FT. DRUM, NY
thomas.m.lilly
DCO 2-10 AVNUH-60-00-ASAM-07--ONE TIME INSP OF WIREHARNESS CONNECTING THE N 01 & NO. 2JUNCTION BOXES ACFT HRS. 1205.0 NATOACFT (CA0465)
02-Sep-2000 1
FT. DRUM, NY
thomas.m.lilly
DCO 2-10 AVNSOF UH-60-01-01-INITIAL AND RECURRINGINSP OF TH EMLG DRAG BEAM ASSY ANDDECREASE TORQUE ON THE JACK PAD NUTC/W @ 1221.2 AFT HRS. (DH6343)
07-Nov-2000 1
FT. DRUM, NY
thomas.m.lilly
D CO 2-10 AVNSOF-UH-60-01-02--ALL H-60 ACFT UPDATE TOSOF UH-60-01-01 EXTENDING OF DATE TO BECOMPLETED C/W 1221.2 ACFT HRS. (RB3433)
28-Dec-2000 1
FT. DRUM, NY
thomas.m.lilly
DCO 2-10 AVNSOF UH-60-01-03 ALL H-60 ACFT INSPECTIONOF LATERAL SERVO BELLCRANK ASSY FORCERTAIN P/N AND CAGE C/W 1224.2 ACFTHRS. (RB3433)
05-Jan-2001 1
FT. DRUM, NY
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 16 of 61
DCO 2-10 AVNSOF UH-60-01-04--ALL H-60 ACFT INSPECTIONFOR INSTALLATION OF FUEL MONITORINGSYSTEM C/W 1224.2 ACFT HRS. (RB3433)
05-Jan-2001 2
FT. DRUM, NY
thomas.m.lilly
DCO 2-10 AVNSOF UH-60-01-06--ALL H-60 SERIES ACFT,INSPECTION OF ALL SAS ACTUATORS C/W @1246.3 ACFT HRS. (KK3198)
26-Mar-2001 1
FT. DRUM, NY
thomas.m.lilly
USAAVNCACFT RECEIVED FROM FT. DRUM, NY I/A/WTWX 171843Z JAN 01. ACFT HRS. 1251.5 ATDEPARTURE, 1256.2 AT ARRIVAL AT FT.RUCKER. ACCEPTANCE INSP COMPLETED BYUSAAVNC PERSONNEL AT FT. DRUM PRIORTO DELIVERY (LW2720)
29-Mar-2001 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNCONE TIME & RECURRING ISNP OF BOOSTSERVO & PILOT ASSIST MODULEMANIFOLDBASE PLATE FOR LOOSE MOUNTBOLTS I/A/W DPC UH60-00-01 C/W AT 1256.2(LW2720)
05-Apr-2001 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNCACFT DECONFIGURED I/A/W CECOM FLIGHTACTIVITY CHECKLIST. EQUIPMENT REMOVEDINCLUDES: AN/ALQ-151(V)2 MISSIONEQUIPMENT PACKAGE, AN/ASN-132INTEGRATED INERTIAL NAVIGATION SYSTEM(IINS), ACFT SURVIVABILTY EQUIPMENT (ASE), ENVIRONMENTAL CONTROL SYSTEM (ECS),MISSION ANTENNA(S) AND WAVEGUIDEASSEMBLIES. SUBJECT CHECKLIST LOCATEDIN THE BACK OF THIS HISTORICAL RECORD.(LW2720)
09-Apr-2001 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNCTHE FOLLOWING LIST OF MODIFICATIONSCOMPLETED AT 1256.2 ACFT. HRS. I/A/WLOCAL DOCUMENTS FOR SCHOOL FLEETTRAINING: INSTL OF FUEL FLAG, INSTL OFBUZZ NUMBER, INSTL OF HIGH VISIBILITYPAINT SCHEME (LW2720)
09-Apr-2001 2
FT. RUCKER, AL
thomas.m.lilly
USAAVNCACFT. OPERATING UNDER AWORTHINESSRELEASE DTD 21NOV00. ACFT WILL OPERATEAS UH60A WHILE ASSIGNED TO USAAVNC.(LW2720)
09-Apr-2001 3
FT. RUCKER, AL
thomas.m.lilly
USAAVNCTB1-1520-237-20-232 SOF UH-60-01-07, INSP OFM/R FLT CONTROL SELF LOCKING BOLTSCW30-MAY-01 ACFT HOURS 1360.8 (LW2720)
30-May-2001 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNCTB1-1520-237-20-232 SOF UH-60-01-08,REVISION TO SOF UH-60-01-07, INSP OF M/RFLT CONTROL SELF LOCKING BOLTS CW 10-JUN-2001 AT 1409.5 ACFT. HRS. (LW2720)
10-Jun-2001 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNC,INSPECTION AND IDENTIFICATION OFAIRCRAFT WITH RECIVER TRANSMITTERSWHICH REQUIRE UPGRADES IAW GEM-MIM-01-005-DUE NLT 13 JULY 2001. COMPLETED AT09 JULY 2001, ACFT HRS. 1449.0 (LW2720/R.CLERK)
11-Jul-2001 1
FT. RUCKER, AL
thomas.m.lilly
DYNCORPOCM/ ACE PERFORMED AT 1488.0 ACFT HRS.BY TEAM MEMBER R. AMCOM PROJECT OLRFT. C. KY (T. STEGMAN 0568)
30-Aug-2001 1
FT. CAMPBELL, 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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 17 of 61
USAAVNC#2 CROSSFEED BREAKAWAY VALVEREPLACED I/A/W TB1-1520-237-20-213COMPLETED AT 1488 ACFT HRS (LW2720R/CLERK)
22-Oct-2001 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNCTB1-1520-237-20-241 (SOF UH-60-02-03), ONETIME INSP OF FLIGHT CONTROLS SYSTEM,PITCH TRIM ASSY. C/W 1488 (LW2720R/CLERK)
11-Dec-2001 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNC,TB1-1520-237-20-242 (SOF UH- 60-02-04), INSPOF APU FUEL LINES FOR PROPER GROMMETAT APU SHROUD ASSY. C/W AT 1488.0 ACFTHRS. (LW2720 R/CLERK)
25-Jan-2002 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNCTB1-1520-237-20-246 (UH-60-02-ASAM-02)INITIAL AND RECURRING INSPECTION OF THECONTROL ROD JAMNUT. C/W AT 1488.0 ACFTHRS. (LW2720 R/CLERK)
10-Feb-2002 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNCTB1-1520-237-20-216 (UH-60-00-ASAM-02),CYCLIC STICK WIRING BUNDLE RELOCATION.C/W AT 1488 ACFT HRS. (LW2720 R/CLERK)
15-Feb-2002 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNCPMSII PHASE 3 COMPLETED AT 1488.0 ACFTHRS. NEXT PMSII PHASE 4 DUE AT 1988.0ACFT HRS. (LW2720 R/CLERK)
22-Feb-2002 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNCTB1-1520-237-20-244 (UH-60-2-ASAM-04)RESTRAINT SYSTEM INSPECTION.C/W @ 1488ACFT HRS (JB2761 R/CLERK)
20-Mar-2002 1
FT.RUCKER,AL
thomas.m.lilly
USAAVNCTB1-1520-237-20-252 (UH-60-02-ASAM-06)COLLECTIVE AND YAW BOOST SERVOASSEMBLIES SWAGE PIN COLLARS C/W AT1517.3 ACFT HRS. (JS4089 R/CLERK)
19-Apr-2002 1
FT.RUCKER,AL
thomas.m.lilly
DYNCOPROCM/ACE PERFORMED AT 1641 ACFT/ HRS.BY TEAM MEMBER R AMCOM PROJECT OLRFT. C. KY (T.STEGMAN TS0568)
13-Jun-2002 1
FT. CAMPBELL, KY
thomas.m.lilly
USAAVNCTB 1-1520-237-20-256 (UH-60-02-ASAM-08),INSP OF AN/ARC-220 WIRING FOR CHAFING.C/W AT 1641.6 ACFT HRS. N/A THIS ACFT.(LW2720 R/CLERK)
14-Jun-2002 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNCTB1-1520-237-20-257 (UH-60-02-ASAM-09), INSPOF T/R QUADRANT INSTALLATIONHARDWARE. C/W AT 1642.1 ACFT HRS.(LW2720 R/CLERK)
14-Jun-2002 2
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. (DK1063)
11-Jul-2002 1
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 1896.8 ACFT HRS (LW2720 R/CLERK)
24-Sep-2002 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNCUH-60-03-ASAM-01, FWD BELLCRANKSUPPORT RETIREMENT LIFE. S/N B367-02110.C/W AT 1979 ACFT HRS (LW2720 R/CLERK)
09-Dec-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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 18 of 61
USAAVNCUH-60-03-ASAM-02, T/R SERVO RETIREMENTLIFE S/N B300-01014. C/W AT 1979 ACFT HRS(LW2720 R/CLERK)
09-Dec-2002 2
FT. RUCKER, AL
thomas.m.lilly
USAAVNCGEN-03-ASAM-01 SINGLE CHANNEL GROUNDAND AIRBORNE RADIO (SINGCGARS) ARC-201BATTERY BOX. C/W AT 1985 ACFT HRS(LW2720 R/CLERK)
18-Dec-2002 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNCTB1-1520-237-20-245 (UH-60-02-ASAM-03)INSPECTION OF ENGINE CONTROLQUADRANT POWER CONTROL LEVER (PCL)WIRING. C/W @ 1984.8 ACFT HRS (VK3955,R/CLERK)
06-Feb-2003 1
FT RUCKER, AL
thomas.m.lilly
USAAVNCAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG 70400-00003REV E SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD A.AFT CONTROL SERVOINPUT ROD HAS (NO CHANGE) B. LATERALCONTROL SERVO INPUT ROD HAS BEEN(SHORTNED 1/4 TURN) C. FORWARDCONTROL SERVO INPUT ROD HAS (NOCHANGE) AT 1984.8 ACFT HRS (VK3955,R/CLERK)
28-Feb-2003 1
FT RUCKER, AL
thomas.m.lilly
USAAVNCPMS-2 PHASE #4 COMPLETED AT 1984.8 ACFTHRS. NEXT PMS-2 PHASE #5 DUE AT 2484.8ACFT HRS. (VK3955, R/CLERK)
05-Mar-2003 1
FT RUCKER, AL
thomas.m.lilly
USAAVNCOCM/ACE PERFORMED AT 2189 A/C HRS. BYTEAM MEMBER J AMCOM/OLR FTCKY(FS6922)
13-Jun-2003 1
FT. RUCKER, AL
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. (DD3948)
19-Jun-2003 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNCSOF UH-60-04-01, INSP. OF FORWARDBELLCRANK SUPPORT INSTALLATIONHARDWARE C/W AT 2265.2 ACFT. HRS.(MF4187 R/SPEC.)
02-Oct-2003 1
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 AT2265.2 ACFT HRS. (JH5095, R/SPEC)
02-Dec-2003 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNCAWOR REL 13MAY02(2) INSTALLATION OFTHE PROVISIONS FOR THE INSTALLATION OFTHE DOPPLER/GPS AN/ASN-128B C/W THISDATE AT 2265.2 ACFT HRS. (JH5095, R/SPEC)
02-Dec-2003 2
FT. RUCKER, AL
thomas.m.lilly
USAAVNCAWOR REL 13MAY02(3) INSTALLATION OFTHE PROVISIONS FOR THE INSTALLATION OFA CARGO HOOK C/W THIS DATE AT 2265.2ACFT HRS. (JH5095, R/SPEC)
03-Dec-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
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 19 of 61
USAAVNCUH-60-04-ASAM-01 GLARE SHIELD LIGHTINGCIRCUIT BREAKER REPLACEMENT C/W AT2265.2 ACFT HRS. (VK3955, R/SPEC)
31-Mar-2004 1
FT RUCKER, AL
thomas.m.lilly
USAAVNCUH-60-04-ASAM-02 INSP OF T/R D/SHAFTFLANGE NUT C/W AT 2265.2 ACFT HRS.(VK3955, R/SPEC)
02-Apr-2004 1
FT RUCKER, AL
thomas.m.lilly
AMCOM/OLR FTCKYOCM/ACE PERFORMED AT 2265 A/C HRS BYTEAM MEMBER J (FS6922)
14-May-2004 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNCSOF UH-60-04-02 DISABLING OF COCKPITAIRBAG SYSTEM C/W @ 2265.2 ACFT HRS(VK3955, R/SPEC)
10-Jun-2004 1
FT RUCKER, AL
thomas.m.lilly
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 70400-0225-046 HASBEEN SHORTENED 1/2 TURN. B. ACFTCONTROL SERVO INPUT ROD P/N 70400-02258-045 HAS BEEN LENGTHENED 1/2 TURN. C.FORWARD CONTROL SERVO INPUT ROD P/N70400-02258-047 HAS BEEN SHORTENED 1/2TURN AT 2265.7 ACFT. HRS. (MF4187 R/SPEC.)
27-Jul-2004 1
FT. RUCKER, AL.
thomas.m.lilly
USAAVNCUH-60-04-ASAM-04, REVISION TO UH-60-04-ASAM-03, FUEL SYSTEM INTEGRITY CHECKSC/W AT 2265.7 ACFT. HRS. (MF4187 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 2265.7 ACFT. HRS. (MF4187 R/SPEC.)
14-Aug-2004 1
FT. RUCKER, AL.
thomas.m.lilly
USAAVNCUH-60-04-ASAM-05, RESTRAINT SYSTEMINSPECTION C/W AT 2269.2 ACFT. HRS.(MF4187 R/SPEC.)
28-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 @ 2269.2 ACFT. HRS. NEXTPHASE #5 DUE @ 2684.8 ACFT. HRS. (MF4187R/SPEC.)
22-Oct-2004 1
FT. RUCKER, AL.
thomas.m.lilly
USAAVNCACFT OPERATING UNDER AWR 1220. A COPYOF THIS AWR IS LOCATED IN THEHISTORICAL RECORDS (MF4187 R/SPEC.)
28-Oct-2004 1
FT. RUCKER, AL.
thomas.m.lilly
USAAVNCIMPLEMENTATION OF 700 HOUR ESM IAWAWR DTD 38 OCT, R-1 C/W AT 2269.2 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 2269.2ACFT. HRS. (MF4187 R/SPEC.)
11-Jan-2005 1
FT. RUCKER, AL.
thomas.m.lilly
USAAVNCAIRCRAFT PLACED IN INTERMEDIATESTORAGE AT 2269.2 ACFT. HRS. FROM 12 OCT04 THRU 22 JAN 05. (MF4817 R/SPEC.)
22-Jan-2005 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 2279.9ACFT. HRS. (MF4187 R/SPEC.)
16-Feb-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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 20 of 61
USAAVNCUH-60-05-ASAM-02 BLUE FORCE TRACKER(BFT) N/A THIS ACFT. C/W AT 2308.2 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) N/A THIS ACFT. C/WAT 2333.8 ACFT. HRS. (MF4187 R/SPEC.)
15-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 2362.9ACFT. HRS. (MF4187 R/SPEC.)
25-Mar-2005 1
FT. RUCKER, AL.
thomas.m.lilly
USAAVNCUH-60-05-ASAM-03 AIRCREW RESTRAINTSYSTEM COMPATIBILITY C/W AT 2399.4 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 2402.4 ACFT HRS.(MF4187 R/SPEC.)
09-Apr-2005 1
FT. RUCKER, AL.
thomas.m.lilly
USAAVNCBIRD STRIKE ABOVE PLT COCKPIT AREA AT2403.4 ACFT. HRS. VISUAL INSP. CONDUCTEDFOUND NO VISIBLE EVIDENCE OF BIRDSTRIKE AND NO DAMAGE NOTED (MF4187R/SPEC.)
09-Apr-2005 2
FT. RUCKER, AL.
thomas.m.lilly
USAAVNCUH-60-05-ASAM-06 TROOP SEAT RESTRAINTBUCKLE COMPLETD AT 2474.1 ACFT HRS.(MF4187 R/SPEC.)
29-Apr-2005 1
FT. RUCKER, AL.
thomas.m.lilly
USAAVNCUH-60-05-ASAM-07, AIR INTRUSION OFHYDRAULIC SYSTEM COMPLETED AT 2477.1ACFT HRS. (TB1027 R/SPEC)
01-May-2005 1
FT. RUCKER, AL.
thomas.m.lilly
DYNCORPOCM/ACE PERFORMED AT 2514.6 ACFT. HRS.BY TEAM MEMBER N. AMCOM PROJECT OLR.(MC0697)
27-May-2005 1
FT. CAMPBELL
thomas.m.lilly
USAAVNCT/R BIAS MEASUREMENTS COMPLETED I/A/WTM1-1520-237-23, PARA 11-4-6.RED:5.284/4.942, YELLOW:5.215/4.877,BLUE:4.572/4.239, BLACK:4.443/4.108. (MF4187R/SPEC.)
21-Jul-2005 1
FT. RUCKER, AL.
thomas.m.lilly
USAAVNCACFT. OPERATING UNDER (AWR 1262) FORSPECIFIED UH-60A HELICOPTERS TOCONDUCT FLIGHTS WITH EXPERIMENTAL G-AXIS SEALS AT 2674.8 ACFT, HRS. (MF4187R/SPEC.)
26-Jul-2005 1
FT. RUCKER, AL.
thomas.m.lilly
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 1/2 TURN. B. AFTCONTROL SERVO INPUT ROD P/N 70400-02258-045 HAS BEEN LENGTHENED 1/2 TURN. C.FORWARD CONTROL SERVO INPUT ROD P/N70400-02258-047 HAS BEEN SHORTENED 1/2TURN. *****NOTE******* WHEN AIRCRAFTRIGGING IS BIASED RIGGING PIN HOLES ARETEMPORARILY LOST AT THE ABOVE 3POINTS. C/W AT 2674.8 ACFT. HRS. (MF4187R/SPEC.)
29-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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 21 of 61
USAAVNCUH-60-05-ASAM-01 REVISION OF FUELSYSTEM INTEGRITY CHECKS C/W AT 2674.8ACFT. HRS. (PART 2) (MF4187 R/SPEC.)
02-Aug-2005 1
FT. RUCKER, AL.
thomas.m.lilly
USAAVNCUH-60-05-ASAM-09 CRASHWORTHYEXTERNAL FUEL SYSTEM (CEFS)INSTALLATION BOLTS C/W AT 2674.8 ACFT.HRS. (MF4187 R/SPEC.)
02-Aug-2005 2
FT. RUCKER, AL.
thomas.m.lilly
USAAVNC700 HR. PHASE #5 COMPLETED AT 2674.8ACFT. HRS. NEXT 700 HR. PHASE #6 DUE AT3374.8 ACFT. HRS. (MF4187 R/SPEC.)
03-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 2803.5ACFT. HRS. (MF4187 R/SPEC.)
15-Oct-2005 1
FT. RUCKER, AL.
thomas.m.lilly
USAAVNCACFT. OPERATING UNDER AIRWORTHNESSRELEASE DTD 06 OCT 05 TO CONDUCT ESMOPERATIONAL EVALUATION AAT THEUSAAVNC, FT. RUCKER, AL. (AWR 1220)(MF4187 R/SPEC.)
19-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 2817.6 ACFT. HRS. PMIINTERVAL INCREASED FROM 700 TO 720 HRSI/A/W 1220 NEXT PHASE #6 DUE AT 3394.8ACFT. HRS. (MF4187 R/SPEC.)
19-Oct-2005 2
FT. RUCKER, AL.
thomas.m.lilly
USAAVNC#2 CROSSFEED BREAKAWAY VALVEREPLACED I/A/W TB1-1520-237-20-213COMPLETED AT 2927.8 ACFT HRS (TB1027R/SPEC)
13-Dec-2005 1
FT. RUCKER, AL.
thomas.m.lilly
USAAVNC,UH-60-06-ASAM-01 TAIL LANDING GEARSTRUT C/W AT 2958.8__ACFT. HRS. (CA3091,R/SPEC)
10-Jan-2006 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNC,T/R BIAS MEASUREMENTS COMPLETED AT2960.7 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED 4.8310/5.1350; BLUE 4.1290/4.4340;YELLOW 4.7675/5.0725; BLACK 4.1070/4.4110(CA3091, R/SPEC)
19-Jan-2006 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNC,T/R CABLE TENSION CHECK COMPLETED @20` C R/H 157; LH 158 TRAVEL .040-3.453 @2960.7 ACFT HRS. (CA3091, R/SPEC)
22-Jan-2006 1
FT. RUCKER, AL
thomas.m.lilly
USAAVNC,T/R BIAS MEASUREMENTS COMPLETED @2960.7 ACFT HRS. I/A/W TM1-1520-237-23,PARA 11-4-6 RED: 4.831/5.111; BLUE:4.150/4.430; YELLOW: 4.7625/5.042; BLACK:4.1215/4.401 (CA3091/R/SPEC)
22-Jan-2006 2
FT. RUCKER, AL
thomas.m.lilly
USAAVNC,T/R CABLE TENSION CHECK COMPLETED @20` C RH 157 LH 158 TRAVEL .040-3.453(CA3091/ R.SPEC)
22-Jan-2006 3
FT. RUCKER, AL
thomas.m.lilly
USAAVNC,ACFT CONTINUES TO OPERATE UNDER AWR1153, JP-8+100 FUEL, R2 DTD 30JAN06(CA3091, R/SPEC)
30-Jan-2006 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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 22 of 61
USAAVNCT/R BIAS MEASUREMENTS COMPLETED @3032.8 ACFT HRS. I/A/W TM1-1520-237-23,PARA 11-4-6 RED: 5105.0/4777.0; BLUE:4436.0/4092.5; YELLOW: 4997.5/4673.0; BLACK:4420.5/4074.5 (JT0967 R/SPEC.)
25-Feb-2006 1
FT. RUCKER, AL.
thomas.m.lilly
USAAWCC/W UH-60-05-ASAM-11 WIRING HARNESSCHAFFING @ 3051.9 ACFT HRS. (JT0967R/SPEC.)
11-Mar-2006 1
FT. RUCKER, AL.
thomas.m.lilly
DYNCORP PROJECTOLR
OCM/ACE PERFORMED AT 3053.9 ACFT. HRS.BY TEAM MEMBER QQ AMCOM PROJECT OLR(LS2032, L. SANDERS)
14-Mar-2006 1
FT. CAMPBELL, KY.
thomas.m.lilly
USAAWCACFT OPERATING UNDER AWR 1292HELICPOTERS EQUIPPED WITH THE DOPPLERGLOBAL POSITIONING SYSTEM NAFL SYS3171.3 ACFT HRS. (JT0967 R/SPEC)
16-Mar-2006 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCUH-60-06-ASAM-02 MAIN ROTOR (M/R) RIGIDCONNECTING LINK/PITCH CONTROLASSEMBLIES C/W AT 3141.2 ACFT. HRS.(JT0967 R/SPEC.)
11-Apr-2006 1
FT. RUCKER, AL.
thomas.m.lilly
USAAWCAWR # 927 DTD 06 JUN 03 FOR AN/ASN-128BDOPPLER/GPS NAVIGATION SYSTEM, JUMPSEAT INSTALLED OR MISSION SEAT RE-LOCATED, SEALED LEAD BATTERY (SLAB)SYSTEM AND CARGO HOOK INSTALLED.(JT0967 R/SPEC)
13-Apr-2006 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCONE TIME INSP OF CONSOLE CIRCUIT BREAKPANEL ASSEMBLIES FOR WATERPENETRATION IAW ACLC EMAIL DTD 17 MAR06. C/W 3148.7 ACFT HRS. (JT0967 R/SPEC.)
15-Apr-2006 1
FT. RUCKER, AL.
thomas.m.lilly
USAAWCM/R RIG CHECK COMPLETED @ 3164.8 ACFTHRS. NO ADJUSTMENTS MADE. (JT0967R/SPEC.)
09-May-2006 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCACFT OPERATING UNDER AWR 1292HELICPOTERS EQUIPPED WITH THE DOPPLERGLOBAL POSITIONING SYSTEM NAFL SYS3171.3 ACFT HRS. (JT0967 R/SPEC)
16-May-2006 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCACFT OPERATING UNDER AWR 1262 DTD 05MAY 06, TO CONDUCT FLIGHTS WITHEXPERIMENTAL G-AXIS SEALS. (JT0967R/SPEC.)
17-May-2006 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCUH-60-06-ASAM-03 SWASHPLATE DUPLEXBEARING C/W @ 3214.6 ACFT HRS. (JT0967R/SPEC.)
16-Jun-2006 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCAWR 1251 AIRCRAFT OPERATING UNDERAWR DTD 16MAR05 FOR INSTALLATION OFEYEBOLTS ON UH-60A/L HEILCOPTERBIFILAR ARMS TO SECURE SAFETYHARNESSES (JT0967 R/SPEC.)
19-Jun-2006 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCUH-60-06-ASAM-04 COCKPIT AIRBAG SYSTEM(CABS) ELECTRONIC CRASH SENSOR UNIT(ECSU) DRAIN PLUGS COMPLETED AT 3231.0ACFT HRS. (JT0967 R/SPEC.)
22-Jun-2006 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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 23 of 61
USAAWCUH-60-06-SOF-02 DISABLING OF COCKPITAIRBAG SYSTEM (CABS) C/W AT 3231.0 ACFT.HRS. (JT0967 R/SPEC.)
22-Jun-2006 2
FT. RUCKER, AL
thomas.m.lilly
USAAWCUH-60-06-ASAM-05 BLUE FORCE TRACKERHARDWARE INSTALLATION C/W @ 3294.0ACFT HRS. INSPECTION INDICATED ON 2408-13-1 THAT THIS DOES NOT APPLY TO THISACFT. (JT0967 R/SPEC.)
21-Jul-2006 1
FT RUCKER, AL
thomas.m.lilly
USAAWCBIRD STRIKE TO YELLOW M/R BLADE AT 3349ACFT. HRS. INSP. CONDUCTED AND FOUNDNO DAMAGE TO ACFT (JT0967 R/SPEC.)
17-Aug-2006 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCUH-60-07-ASAM-01 REQUIREMENTS OF UH-60-07-ASAM-01, (REROUTING OF WHITEENGINE/AIRFRAME HARNESS ASSEMBLY)COMPLIED WITH @ 3394.1 ACFT HRS. (MF4187R/SPEC.)
04-Dec-2006 1
FT. RUCKER, AL.
thomas.m.lilly
USAAWCGEN-MIM-06-001 INSPECTION OF T700 SERIESENGINE OIL FILLER ASSEMBLY C/W AT 3394.1ACFT. HRS. (MF4187 R/SPEC.)
07-Dec-2006 1
FT. RUCKER, AL.
thomas.m.lilly
USAAWCT/R BIAS MEASUREMENTS COMPETED AT3394.1 ACFT. HRS. I/A/W TM1-1520-237-23,PARA 11-4-6. RED: 4.819/5.153, YELLOW:4.800/5.137, BLUE: 4.197/4.535,BLACK:4.212/4.550. (MF4187 R/SPEC.)
07-Dec-2006 2
FT. RUCKER, AL.
thomas.m.lilly
USAAWCT/R BIAS MEASUREMENTS COMPLETED @3394.1 ACFT HRS. I/A/W TM1-1520-237-23,PARA 11-4-6 RED:4.819/5.153; BLUE:4.197/5.535; YELLOW: 4.800/5.137; BLACK:4.212/5.550 (TB1027 R/SPEC)
08-Dec-2006 1
FT. RUCKER, AL.
thomas.m.lilly
USAAWCT/R CABLE TENSION CK COMPLETED AT3394.1 ACFT HRS. R/H 115; L/H 115 @ 50DEGREES FAREINHEIGHT (TB1027 R/SPEC)
08-Dec-2006 2
FT. RUCKER, AL.
thomas.m.lilly
USAAWC720 HR. PMI #6 COMPLETED @ 3394.1 ACFT.HRS. NEXT PMI#7 DUE @ 4114.1 ACFT. HRS.(MF4187 R/SPEC.)
13-Dec-2006 1
FT. RUCKER, AL.
thomas.m.lilly
USAAWC#2 CROSSFEED BREAKAWAY VALVEREPLACED I/A/W TB1-1520-237-20-213 THISDATE @ 3394.1 ACFT HRS. (JT0967 R/SPEC.)
14-Dec-2006 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCUH-60-07-ASAM-02 REVISION TO UH-60-07-ASAM-01, REROUTING OF WHITEENGINE/AIRFRAME HARNESS ASSEMBLYCOMPLETED AT 3396.1 ACFT HRS. (MF4187R/SPEC.)
22-Dec-2006 1
FT. RUCKER, AL.
thomas.m.lilly
USAAWCT/R CABLE TENSION CHECK COMPETED AT3394.1 ACFT. HRS. R/H=115, L/H=115, 50*C.(MF4187 R/SPEC.)
29-Dec-2006 1
FT. RUCKER, AL.
thomas.m.lilly
USAAWCT/R CABLE TENSION CHECK COMPETED AT3395.1 ACFT. HRS. R/H=150, L/H=150, 20*C.(MF4187 R/SPEC.)
29-Dec-2006 2
FT. RUCKER, AL.
thomas.m.lilly
USAAWCUH-60-07-ASAM-04 AUTOROTATIONALCHARTS COMPLETED AT 3394.1 ACFT HRS.(MF4817 R/SPEC.)
29-Dec-2006 3
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 24 of 61
USAAWCT/R BIAS MEASUREMENTS COMPETED AT3397.1 ACFT. HRS. I/A/W TM1-1520-237-23,PARA 11-4-6. RED: 4.819/5.153, YELLOW:4.800/5.137, BLUE: 4.197/4.538,BLACK:4.212/4.550. (MF4187 R/SPEC.)
29-Dec-2006 4
FT. RUCKER, AL.
thomas.m.lilly
USAAWCAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG 70400-00003REV.D. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD. A AFT CONTROL SERVOINPUT ROD P/N 70400-02258-045 HAS BEENLENGTHENED 3/4 TURN. B LATERALCONTROL SERVO INPUT ROD P/N 70400-02258-046 HAS BEEN LENGTHENED 1/8 TURN. CFORWARD CONTROL SERVO INPUT ROD P/N70400-0225/-047 HAS BEEN SHOSRTENED 3/4TURN. NOTEL WHEN AIRCRAFT RIGGING ISBIASED RIGGING PIN HOLES ARETEMPORARILY LOST AT THE ABOVE 3 POINTSAT 3394.1 AC FT. HRS. (MF4187 R/SPEC.)
29-Dec-2006 5
FT. RUCKER, AL.
thomas.m.lilly
USAAWCUH-60-07-ASAM-03 YAW AND COLLECTIVEBOOST SERVOS ROLL PIN COMPLETED AT3396.1 ACFT HRS. (MF4187 R/SPEC.)
03-Jan-2007 1
FT. RUCKER, AL.
thomas.m.lilly
USAAWCACFT OPERATING UNDER AWR 1153 (R3)(JP8+100 FUEL), DTD 19DEC06. 3403.0 ACFTHRS. (JT0967 R/SPEC)
09-Jan-2007 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCUH-60-07-ASAM-05 ARC-220/KY-100 START-UPPROCEDURES (N/A THIS ACFT., KY-100 NOTINSTALLED) AT 4496.0 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 3432.8ACFT. HRS. (M. BELFORD 1137)
07-Feb-2007 1
FT. RUCKER, AL.
thomas.m.lilly
USAAWCUH-60-07-AMAM-01 COMMON MISSILEWARNING SYSTEM (CMWS) N/A THIS ACFT.@3520.8 ACFT. HRS. (JT0967 R/SPEC)
27-Mar-2007 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCUH-60-07-ASAM-07 INSTALLATION OF STATICBONDING JUMPERS, N/A TO THIS ACFT. C/WAT 3611.6 ACFT. HRS. (JT0967 R/SPEC)
11-May-2007 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCACFT OPERATING UNDER AWR 1292 DTD 27APR 07; HELICPOTERS EQUIPPED WITH THEDOPPLER GLOBAL POSITIONING SYSTEMNAFL SYS 3629.3 ACFT HRS. (JT0967 R/SPEC)
16-May-2007 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCAWR 1251 AIRCRAFT OPERATING UNDERAWR DTD 16 MAR 07 FOR INSTALLATION OFEYEBOLTS ON UH-60A/L HEILCOPTERBIFILAR ARMS TO SECURE SAFETYHARNESSES (JT0967 R/SPEC)
16-May-2007 2
FT. RUCKER, AL
thomas.m.lilly
DYNCORP OLROCM/ACE PERFORMED AT 3743 ACFT HRS BYTEAM MEMBER R. AMCOM PROJECT OLR.(TS0568)
25-Jun-2007 1
FT. CAMPBELL, KY
thomas.m.lilly
USAAWCACFT. OPERATING UNDER AWR 1220, REV. 3,DTD. 27JUL07. IMPLEMENTATION OF 720HOUR (ESM) REQUIREMENTS AT 3790.8 ACFT.HRS. (JT0967 R/SPEC)
01-Aug-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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 25 of 61
USAAWCMULTIPLE BIRD STRIKES ACROSS AIRFRAME.INSP AIRFRAME, INL.ETS, ROTORS: NODAMAGE FOUND... 3925.7 ACFT HRS. (JT0967R/SPEC)
29-Sep-2007 1
FT. RUCKER, AL
thomas.m.lilly
USAACETB1-1520-237-23, CHG 8 IGB CHIP DETECTORINOPERABLE. CHIP DETECTOR REPLACED.(JT0967)
31-Oct-2007 1
LOWE AHP
thomas.m.lilly
USAAWCH-60-08-AMAM-01 MAIN LANDING GEARSHOCK STRUTS C/W AT 4017.5 ACFT. HRS.(JT0967 R/SPEC)
03-Nov-2007 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCINITIAL INSP OF H-60-08-ASAM-03 CHANGESTO CURRENT FUEL SYSTEM INTEGRITYCHECKS C/W AT 4046.5 ACFT. HRS. (JT0967R/SPEC)
16-Nov-2007 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCH-60-08-ASAM-02 POWER AVAILABLECONTROL CABLE C/W AT 4049.5 ACFT. HRS.(JT0967 R/SPEC)
18-Nov-2007 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCH-60-08-ASAM-04 PILOT'S LOWER SEAT RAILCHAFING ELECTRICAL HARNESS C/W @4061.9 ACFT HRS. (JT0967 R/SPEC)
27-Nov-2007 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCH-60-08-ASAM-03 CHANGES TO CURRENTFUEL SYSTEM INTEGRITY CHECKS C/W AT4069.7 ACFT. HRS. (JT0967 R/SPEC)
01-Dec-2007 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCH-60-08-AMAM-02 TAIL ROTOR OUTBOARDRETENTION PLATE SHIMS C/W @ 4069.7 ACFTHRS. (JT0967 R/SPEC)
03-Dec-2007 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCH-60-08-ASAM-05 TAIL ROTOR QUADRANTSPRING CAPSULE ASSEMBLY C/W AT 4094.7ACFT. HRS. (JT0967 R/SPEC)
15-Dec-2007 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCH-60-08-AMAM-05 GOODRICH INTERNALRESCUE HOISTS COMPLETED @ 4110.9 ACFTHRS. NA TO THIS ACFT. (TB1027 R/SPEC)
31-Jan-2008 1
FT. RUCKER, AL.
thomas.m.lilly
USAAWCH-60-08-AMAM-06 COMMON MISSILEWARNING SYSTEM (CMWS) SEQUENCERSC/W AT 4110.9 ACFT HRS. AFS558 (RC1002)
26-Feb-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCT/R CABLE TENSION CK C/W @ 4110.9 ACFTHRS, L/H=166, R/H=165, @ 82*F (MR0958)
28-Feb-2008 1
FT RUCKER, AL
thomas.m.lilly
USAAWCH-60-08-AMAM-04 H-60-08-AMAM-04 COCKPITDOOR JETTISONABLE WINDOWS C/W AT4110.9 ACFT HRS. (RC1002)
03-Mar-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCT/R BIAS MEASUREMENTS COMPETED AT4110.9 ACFT. HRS. I/A/W TM1-1520-237-23,PARA 11-4-6. RED: 4.718/5.045, YELLOW:4.716/5.046, BLUE: 4.070/4.395,BLACK:4.071/4.396. (RC1002)
03-Mar-2008 2
FT. RUCKER, AL
thomas.m.lilly
USAAWCAIRCRAFT 8524465 HAS A CRACK ABOUT ONEINCH LONG ON THE FORWARD LEFT FRONTCORNER OF THE SHEAR DECK IN THE AFTSECTION OF THE TAILCONE. REPAIRED IAWSIKORSKY REPARI SE-0871T021 AND MECF72883. DTD 27 FEB 08 (RC1002)
04-Mar-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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 26 of 61
USAAWCH-60-08-ASAM-06 M/R PYLON SLIDINGFORWARD FAIRING C/W AT 4110.9 ACFT HRS.AFS643 (RC1002)
07-Mar-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCH-60-08-SOF-01 MAIN ROTOR BLADEEXPANDABLE PIN INSPECTION CHANGE C/WAT 4110.9 ACFT HRS. AFS558 (RC1002)
12-Mar-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCM/R RIG CHECK COMPLETED @ 4110.9 ACFTHRS. PRIMARY SERVO CONTROL ROD BIAS:FWD: NO CHANGE, AFT: NO CHANGE, LAT: 1FLATSHORTING. (RC1002)
19-Mar-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCT/R CABLE TENSION CHECK COMPETED AT4110.9 ACFT. HRS. R/H=165, L/H=166, 82*F.(RC1002)
20-Mar-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCT/R BIAS MEASUREMENTS COMPETED AT4110.9 ACFT. HRS. I/A/W TM1-1520-237-23,PARA 11-4-6. RED: 4.718/5.045/.327, YELLOW:4.716/5.046/.330, BLUE: 4.070/4.395/.325,BLACK:4.071/4.396/.325. (MR0958)
20-Mar-2008 2
FT RUCKER, AL
thomas.m.lilly
USAAWCUH-60-08-ASAM-01 TROOP/GUNNER SEATUPPER ENERGY ATTENUATING WIRES N/ATHIS ACFT. AT 4110.9 ACFT. HRS. AFS595(RC1002)
21-Mar-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAAWC720 HR PMI #7 COMPLETED @ 4110.9 ACFTHRS. NEXT PMI #8 DUE @ 4830.9 ACFT HRS.(RC1002)
25-Mar-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCAIRCRAFT NO LONGER OPERATING IAW AWRDATED 19 DEC 06. (JP-8+100 FUEL) AFS514(JT0967 R/SPEC)
10-Apr-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCH-60-08-AMAM-07 AN/ASN-128B/D DOPPLERGPS NAVIGATION SET (DGNS) C.W @ 4164.5ACFT HRS. (JT0967 R/SPEC)
20-Apr-2008 1
FT. RUCKER, AL
thomas.m.lilly
DYNCOPR INTLOCM/ACE PERFORMED AT 4184 ACFT HRS BYTEAM MEMBER R (TS0568)
30-Apr-2008 1
FT. CAMPBELL, KY,AMCOM RASM-E
thomas.m.lilly
USAAWCM/R RIG CHECK COMPLETED @ 4184.2 ACFTHRS. NO ADJUSTMENTS MADE. (BH0315)
03-May-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCACFT. OPERATING UNDER AWR 1220, REV. 3,DTD. 27JUL07. IMPLEMENTATION OF 720HOUR (ESM) REQUIREMENTS SUPERCEDEDBY AWR 1220 DTD 22 MAY 08 @ 4253.1 ACFT.HRS (BH0315)
04-Jun-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAAWCOPERATE ACFT IAW AIRWORTHINESSRELEASE (AWR 1220 R-4 DTD 22 MAY 08) TOCONDUCT A MODIFIED SCHEDULEDMAINTENANCE AT THE UNITED STATES ARMYAVIATION WARFIGHTING CENTER. (BH0315)
04-Jun-2008 2
FT. RUCKER, AL
thomas.m.lilly
USAAWCH-60-08-AMAM-08 FLIGHT CONTROL RIGGINGC/W @ 4255.6 ACFT HRS. (BH0315)
07-Jun-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAACEAIRCRAFT OPERATING UNDERLIMITATIONS/RESTRICTIONS OF AWR 1514DTD 31 JULY 08 AT 4301.3 ACFT HRS (BH0315)
31-Jul-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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 27 of 61
USAACEM/R RIG CHECK COMPLETED AT 4301.1 ACFTHRS. NO ADJUSTMENTS NOTED. (BH0315)
10-Aug-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAACET/R BIAS MEASRUEMENTS COMPLETED AT4301.3 ACFT HRS I/A/W TM 1-1520-237-23 PARA11-4-6. YELLOW: 4.817/5.124/.307, BLUE:4.163/4.472/.309, RED: 4.817/5.123/.306, BLACK:4.160/4.467/.307 (BH0315)
11-Aug-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAACET/R CBALE TENSION CHECK COMPLETED AT4311.1 ACFT HRS. L/H=145, R/H=145 @ 23°C(BH0315)
21-Aug-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-08-ASAM-11 FLIGHT CONTROLINSPECTION COMPLIED WITH AT 4311.1 ACFTHRS (BH0315)
21-Aug-2008 2
FT. RUCKER, AL
thomas.m.lilly
USAACEPOSSIBLE BIRD STRIKE TO UNDERSIDE OFNOSE. INSPECTION COMPLETED AND NODAMAGE FOUND AT 4327.7 ACFT HRS.(BH0315)
27-Aug-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAACEONE TIME FCC REQUIRED PRIOR TO FIRSTFLIGHT WITH NEW EQUIPMENT INSTALLEDIAW AWR 1514 DTD 31 JULY 08 NOTAPPLICABLE TO THIS AIRCRAFT. (BH0315)
28-Aug-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAACEAIRCRAFT OPERATING UNDERLIMITATIONS/RESTRICTIONS OF AWR 1262DTD 02 JUN 08 AT 4359.3 ACFT HRS (BH0315)
15-Sep-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH60-08-ASAM-12 PARKER AEROSPACETURBINE STARTER (ATS) COMPLIED WITH AT4365.2 ACFT HRS. (BH0315)
21-Sep-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-08-ASAM-13 FIRE EXTINGUISHING TUBEUNION RING COMPLIED WITH AT 4365.5 ACFTHRS. (BH0315)
23-Sep-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAACEACFT. OPERATING UNDER AWR 1251, DTD. 16MAR 07, SUPERCEDED BY AWR 1251, REV. 2DTD 01 SEP 08 @ 4366.0 ACFT. HRS (BH0315)
24-Sep-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAACEOPERATE ACFT IAW AIRWORTHINESSRELEASE (AWR 1251, REV.4, DTD 01 SEP 08)FOR OPERATION OF H-60 HCPTS WITHEYEBOLTS INSTALLED ON BIFILAR ARMS TOSECURE SAFETY HARNESSES. (BH0315)
24-Sep-2008 2
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-08-ASAM-14 ENGINE HARNESSESCOMPLIED WITH AT 4403.5 ACFT HRS(BH0315)
11-Oct-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-09-SOF-01 HYDRO-MECHANICAL UNITCOMPLIED WITH AT 4430.2 ACFT HRS(BH0315)
23-Oct-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH60-09-SOF-02 (IRCMS) NOT APPLICABLE TOTHIS AIRCRAFT AT 4469.5 ACFT HRS (BH0315)
08-Nov-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAACET/R BIAS MEASUREMENTS COMPLETED AT4469.5 ACFT HRS IAW TM 1-1520-237-20 PARA11-4-6. RED: 5.118/4.761/.357, YELLOW:5.021/4.664/.357, BLUE: 4.547/4.231/.316,BLACK: 4.535/4.225/.310 (BH0315)
09-Nov-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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 28 of 61
USAACEH-60-09-SOF-03 (POSSIBLE RETIREMENT LIFEOVERFLIGHT) COMPLIED WITH AT 4495.1ACFT HRS (BH0315)
20-Nov-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAACEOPERATE ACFT IAW AIRWIRTHINESSRELEASE (AWR 1479, DTD 04 JAN 08),"IMPROVED MAIN TRANSMISSIONPLANETARY CARRIER ASSY", @ 4518.8 ACFTHRS. (BH0315)
25-Nov-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAACECOMPLIED WITH REQUIREMENTS OFPARAGRAPH 7.3-7.10 OF H-60-08-ASAM-10 AT4548.7 ACFT HRS. (BH0315)
17-Dec-2008 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-09-ASAM-01 COMPLIED WITH AT 4571.8ACFT HRS (MARKED AS N/A) (BH0315)
13-Jan-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-09-ASAM-04 (RESCUE HOIST MARK 44MOD 0 CARTRIDGE ACTIVATION DEVICE)COMPLIED WITH AT 4668.4 ACFT HRS (N/ATHIS ACFT) (BH0315)
01-Mar-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-09-ASAM-05 (UPDATE TO LIFE LIMITCHANGE FOR TAIL ROTOR QUADRANTSPRING CAPSULES) COMPLIED WITH AT4748.8 ACFT HRS (BH0315)
01-Apr-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-09-ASAM-07 (FIRE EXTINGUISHERWIRING BREAKAWAY THREAD) COMPLIEDWITH AT 4756.2 ACFT HRS (BH0315)
12-Apr-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEACFT NO LONGER OPERATING UNDER AWR1292 DATED 27 APR 07 (AWR 1292) REV. 3,ASN-128D) (JC6208)
05-May-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEACFT OPERATING UNDER AWR 1292 DATED26 MAR 09. REV. 4.(DGNS) (JC6208)
05-May-2009 2
FT. RUCKER, AL
thomas.m.lilly
USAACEI/A/W ETM 1-1520-237-23-6 WP 039100, L/HUPPER CARGO DOOR TRACK UPPERVERTICAL ROLLER TRACKS, HORIZONTALANGLE, FORWARD VICINITY DOOR JAM, HASSROLLER WEAR DIVOT MEASURING .12" INDEPTH. REQUESTING MEC REPAIR.REMAINING THICKNESS IS .38". (JC6208)
06-May-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEACFT OPERATING UNDER MEC #F92347-UPPER CARGO DOOR TRACK IS BEYONDLIMITSPER THE MANUAL BY .002. REQUESTPERMISION TO INSTALL WEAR STRIP ON L/HUPPER TRACKS P/N: 70217-02702-049 TOREINFORCE AREA WHERE CARGO DOORROLLERS REST WHEN DOORS ARE CLOSEDIN LOCK POSITION. WOULD BE IDENTICAL TOR/H SIDE STRIP AND BONDING PROCEDUREWOULD BE THE SAME 0.025 STAINLESSSTEEL WEAR STRIP WILL BE TAPERED ANDGLUED USING HYSOL 9309. PERMISSIONGRANTED. (RJ0827, R/SPEC)
08-May-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEREPLACED WALKING BEAM REMOVED SN:B346-00159 & INSTALLED SN: D346-00056 @4805.0 ACFT HRS.(AFS 648) (KJ0605)
12-May-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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 29 of 61
USAACEH-60-09-ASAM-09 FIRE EXTINGUISHER WIRING(BREAKAWAY THREAD) COMPLETED AT4805.0 ACFT HRS. (JC6208)
13-May-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEL/H CARGO DOOR TRACK REPAIRED I/A/WMEC F92347 @ 4805.0 ACFT HOURS DURING720 HR. PHASE (JC6208)
18-May-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEOPERATE AIRCRAFT WITHIN LIMITS ANDRESTRICTIONS OF AIRWORTHINESSRELEASE, AWR 1505 DTD 18 MAY 09 AT 4805.0ACFT HRS (BH0315 R/SPEC)
18-May-2009 2
FT. RUCKER, AL
thomas.m.lilly
USAACET/R BIAS MEASUREMENTS COMPLETED AT4805.0 ACFT HRS IAW TM 1-1520-237-20 PARA11-4-6. RED: 5.152/4.830/.322, YELLOW:5.154/4.835/.322, BLUE: 4.517/4.197/.320,BLACK: 4.524/4.197/.320 (JC6208)
19-May-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEM/R RIG CHECK COMPLETED AT 4805.0 ACFTHRS. NO ADJUSTMENTS MADE. (JC6208)
19-May-2009 2
FT. RUCKER,AL
thomas.m.lilly
USAACET/R CABLETENSION CHECK COMPLETED AT4805.0 ACFT HRS. L/H=149, R/H=149 @ 20°C(JC6208)
20-May-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-09-ASAM-08 ENGINE COWLING WEIGHTRESTRICTION COMPLETED AT 4805.0 ACFTHRS. INSP. COMPLETE 300 LB WEIGHT LIMIT.(JC6208)
21-May-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACE720 HR PMI #8 COMPLETED @4805.0 ACFTHRS. NEXT PMI # 9 DUE @ 5525 ACFT HOURS.(JC6208)
22-May-2009 1
FT. RUCKER, AL
thomas.m.lilly
CSCOCM/ACE PERFORMED AT 4815.5 ACFT HRSBY TEAM MEMBER DD AMCOM AFMA (JB9001)
04-Jun-2009 1
FT CAMPBELL, KY
thomas.m.lilly
USAACEACFT NO LONGER OPERATING UNDER AWR1262 REV 5, DTD 02 JUN 08 TERMINATED ASOF 01 JUN 09. SEALS NOW ACCEPTED FORARMY USE. (RJ0827, R/SPEC)
16-Jun-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-09-ASAM-11 CARGO DOOR WINDOWEMERGENCY JETTISON HANDLE INSP C/W AT4815.5 ACFT HRS (RJ0827, R/SPEC)
30-Jun-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACE1-1520-237-23-9 FUEL CELL CORRISIONINSPECTION OF UH-60, EH-60 AND HH-60-SERIES HELICOPTERS C/W AT 4815.5 ACFTHRS (RJ0827, R/SPEC)
13-Jul-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACE1-1520-237-23-10 INSTALLATIN OF UH-60, EH-60 SND HH-60 SERIES HELICOPTER FORBODY PLUG CORROSION INSPECTION C/W AT4815.5 ACFT HRS (RJ0827, R/SPEC)
13-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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 30 of 61
USAACEMEC # F95203- 308 BEAM HAS GOUGESLOCATED NEAR AFT HILOCK. REQUESTINGTO USE TYPICAL BLENDING AND NDIPROCEDURES ON THE GOUGES AND CUTS.PROCEDURE WAS PREVIOSLY COMPLETED(REF MEC F83894). TAB DAMAGE WASBLENDED AND NO CRACKS WERE FOUNDWITH NDI- LIGHTLY BLEND REMAININGGOUGES TO ROUND OUT TRANSITION AREASTO REDUCE STRESS RISERS. MANUFACTUREAND INSTALL BRIDGING STRAP PER SE-A70326-308. (RJ0827, R/SPEC)
14-Jul-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACET/R BIAS MEASUREMENTS COMPLETED AT4815.5 ACFT HRS IAW TM 1-1520-237-20 PARA11-4-6. RED:5.197/4.860 , YELLOW:5.155/4.820 ,BLUE:4.496/4.158 , BLACK: 4.574/4.242(RJ0827, R/SPEC)
22-Jul-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACET/R CABLE TENSION CK COMPLETED @4815.5 ACFT HRS L/H: 169, R/H 170 @ 31'C(RJ0827, R/SPEC)
06-Aug-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACET/R BIAS MEASUREMENTS COMPLETED AT4815.5 ACFT HRS IAW TM 1-1520-237-20 PARA11-4-6. RED:5.199/4.885 , YELLOW:5.176/4.855 ,BLUE:4.555/4.240 , BLACK: 4.557/4.246(RJ0827, R/SPEC)
07-Aug-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEM/R RIG CK COMPLETED @ 4815.5 ACFT HRS-THE FOLLOWING ADJ WERE MADE: FWD: 1/2SHORT, AFT:1/2 LONG, LAT: 4 1/2 SHORT.(RJ0827, R/SPEC)
07-Aug-2009 2
FT. RUCKER, AL
thomas.m.lilly
USAACEACFT GROUNDED FOR H-60-09-ASAM-07 ANDH-60-09-ASAM-09 NOT COMPLIED WITH.COMPLETED BY AFS 727 AT 4833.7 ACFT HRS.(RJ0827, R/SPEC)
14-Aug-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACECOMPLY WITH REQUIREMENTS OF GEN-09-AMAM-ULLS-A (E) - N/A TO THIS ACFT DUE TOUNIT NOT CURRENTLY USING ULLS-A (E)(4781.1 ACFT HRS) (RJ0827, R/SPEC)
26-Aug-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACECOMPLIED WITH REQUIREMENTS OF H-60-09-AMAM-06 AT 4872.2 ACFT HRS. CARGO HOOKCARTRIDGE ACTUATED DEVICE (CAD) LIFEREDUCTION. AFS793 (JB2761 R/SPEC)
27-Aug-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 97372 IS LOCATED IN THEHISTORICAL RECORDS. (RJ0827, R/SPEC)
27-Aug-2009 2
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 4876.8 ACFT HRS. (JB2761R/SPEC)
28-Aug-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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 31 of 61
USAACET/R BIAS MEASUREMENTS COMPLETED AT4930.0 ACFT HRS IAW TM 1-1520-237-20 PARA11-4-6. RED:5.1950/4.8460 ,YELLOW:5.1980/408435 , BLUE:4.4445/4.1180 ,BLACK:4.4500/4.1355 (RJ0827, R/SPEC)
14-Sep-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-09-AMAM-07 HALON HAND-HELD FIREEXTINGUISHERS (HHFE) C/W AT 4937.3 ACFTHRS (RJ0827, R/SPEC)
17-Sep-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEACFT NO LONGER OPERATING UNDER AWR1514, DTD 31 JUL 08 BECAUSE ACFT ISEQUIPPED WITH 128B GPS (5015.1 ACFT HRS)(RJ0827, R/SPEC)
21-Oct-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEACFT NO LONGER OPERATING UNDERLIMITATIONS AND RESTRICTIONS SPECIFIEDIN AWR 1292, DTD 26 MAR 09. REV 4 (DGNS)DUE TO ACFT BEING EQUIPPED WITH 128BDPLR/ GPS (ACFT HRS 5015.1) (RJ0827,R/SPEC)
21-Oct-2009 2
FT. RUCKER, AL
thomas.m.lilly
USAACET/R CABLE TENSION CHECK COMPLETED AT5024.0 ACFT HRS. L/H-120, R/H-120 AT 60*F.(MB1137)
24-Oct-2009 1
FT. RUCKER, AL.
thomas.m.lilly
USAACET/R BIAS MEASUREMENTS COMPLETED AT5024.0 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 5.052/4.720, YELLOW: 5.023/4.686,BLUE: 4.363/4.028, BLACK: 4.300/3.965.(MB1137)
24-Oct-2009 2
FT. RUCKER, AL.
thomas.m.lilly
USAACET/R BIAS MEASUREMENTS COMPLETED AT5024.0 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 4.787/5.138, YELLOW: 4.762/5.090,BLUE: 4.102/4.432, BLACK: 4.050/4.405.(MB1137)
24-Oct-2009 3
FT. RUCKER, AL.
thomas.m.lilly
USAACET/R BIAS MEASUREMENTS COMPLETED AT5024.0 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:5.133/4.797, YELLOW: 5.151/4.821,BLUE:4.439/4.101, BLACK: 4.446/4.116.(MB1137)
24-Oct-2009 4
FT. RUCKER, AL.
thomas.m.lilly
USAACET/R CABLE TENSION CHECK COMPLETED AT5024.0 ACFT HRS. R/H-129, L/H-130, AT 18*C.(MB1137)
24-Oct-2009 5
FT. RUCKER, AL.
thomas.m.lilly
USAACET/R BIAS MEASUREMENTS COMPLETED AT5024.0 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 5.053/4.716, YELLOW: 5.044/4.707,BLUE: 4.328/3.996, BLACK: 4.291/3.959.(MB1137)
25-Oct-2009 1
FT. RUCKER, AL.
thomas.m.lilly
USAACET/R CABLE TENSION CK COMPLETED AT5033.9 ACFT HRS L/H: 120 R/H: 120 @ 20'C/68'F(RJ0827, R/SPEC)
29-Oct-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACET/R BIAS MEASUREMENTS COMPLETED AT5033.9 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 5.022/4.692, YELLOW:5.045/4.649 ,BLUE:4.295/3.965 , BLACK:4.379/4.019.(RJ0827, R/SPEC)
29-Oct-2009 2
FT. RUCKER, AL
thomas.m.lilly
USAACET/R CABLE TENSION CK COMPLETED AT5033.9 ACFT HRS L/H: 114 R/H: 114 AT20'C/68'F (RJ0827, R/SPEC)
29-Oct-2009 3
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 32 of 61
USAACET/R CABLE TENSION CK COMPLETED AT5033.9 ACFT HRS- L/H:137 R/H:136 AT 78'F(RJ0827, R/SPEC)
30-Oct-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACET/R CABLE TENSION CK COMPLETED AT5033.9 ACFT HRS L/H: 115 R/H:125 AT 15'C.(RJ0827, R/SPEC)
31-Oct-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACET/R BIAS MEASUREMENTS COMPLETED AT5033.9 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:5.126/4.793 , YELLOW:5.055/4.722 ,BLUE:4.405/4.0373, BLACK:4.419/4.077 .(RJ0827, R/SPEC)
31-Oct-2009 2
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-10-AMAM-04 ASN-128B/C DOPPLERGLOBAL POSITIONING SYSTEM GPSNAVIGATION SET COMPLETED AT 5048.5ACFT HRS. (RJ0827, R/SPEC)
10-Nov-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-10-ASAM-03 FIRE BOTTLE DISCHARGELINES AND NOZZLES COMPLETED AT 5059.2ACFT HRS. (RJ0827, R/SPEC)
14-Nov-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEACFT OPERATING UNDER AWR 1445, R2 DTD20MAR09, AFCS. 5070 ACFT HRS (DK1063)
19-Nov-2009 1
FT. RUCKER, AL.
thomas.m.lilly
USAACEH-60-10-ASAM-04 STABILITY AUGMENTATIONSYSTEM (SAS) LINKS C/W AT 5070.1 ACFTHRS (RJ0827)
19-Nov-2009 2
FT. RUCKER, AL
thomas.m.lilly
USAACET/R BIAS MEASUREMENTS COMPLETED AT5080.7 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:50168/40849 , YELLOW:5.150/4.827,BLUE:4.432/4.113, BLACK:4.509/4.190 (RJ0827)
21-Nov-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACET/R BIAS MEASUREMENTS COMPLETED AT5080.9 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:4.688/4.398 , YELLOW:4.648/4.355 ,BLUE:3.986/3.694, BLACK:3.989/3.692 (RJ0827)
23-Nov-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACET/R BIAS MEASUREMENTS COMPLETED AT5090.3 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:5.159/4.855 , YELLOW:5.095/4.792 ,BLUE:4.412/4.110, BLACK:4.433/4.132 (RJ0827)
30-Nov-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACET/R CABLE TENSION CK COMPLETED @5090.3 ACFT HRS- R/H: 129 L/H: 130 AT 17'C(RJ0827)
01-Dec-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEACFT OPERATING UNDER AWR 1505 R 3 DTD21 OCT 09 (RJ0827)
08-Dec-2009 1
FT. RUCKER, AL
thomas.m.lilly
USAACEACFT NO LONGER OPERATING UNDER AWR1479, DTD 04 JAN 08 (IMPROVED MAINTRANSMISSION PLANETARY CARRIER ASSY)(RJ0827)
01-Jan-2010 1
FT. RUCKER, AL
thomas.m.lilly
USAACET/R BIAS MEASUREMENTS COMPLETED AT5165.5 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:5.1175/4.7810 ,YELLOW:5.0710/4.7360 , BLUE: 4.4080/4.0770,BLACK: 4.4200/4.0890 (RJ0827, R/SPEC)
15-Jan-2010 1
FT. RUCKER, AL
thomas.m.lilly
USAACEACFT NO LONGER OPERATING UNDER MEOA6055 (REPLACED RED M/R DROOP STOPBUSHING) AT 5465.5 ACFT HRS (RJ0827,R/SPEC)
17-Jan-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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 33 of 61
USAACEGEN-10-AMAM-02 DISTRIBUTION OF NEWACFT ELECTRONIC LOGBOOK, N/A THISLOCATION, C/W AT 5185.6 ACFT HRS. (RJ0827,R/SPEC)
26-Jan-2010 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-10-AMAM-11 OIL SAMPLING CHANGESCOMPLETED AT 5198.4 ACFT. HRS. (RJ0827,R/SPEC)
01-Feb-2010 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-10-ASAM-06 AUTO-IGNITION ANDTRANSIENT DROOP IMPROVEMENT TDIMODIFICATION COMPLETED AT 5215.8 ACFTHRS. (RJ0827, R/SPEC)
09-Feb-2010 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-10-AMAM-05 ULLSA IMMC LCF CHANGE60B C/W AT 5227.5 ACFT HRS. (RJ0827,R/SPEC)
13-Feb-2010 1
FT. RUCKER, AL
thomas.m.lilly
USAACEMEO - A6055- FT RUCKER MAINTENANCE HASREQUESTED THAT DE-BONDED M/R DROOPSTOP BUSHINGS BE ALLOWED TO STAY INSERVICE UNTIL THE NEXT PMI AT WHICH TIMETHEY WILL BE REPLACED. TM 1-1520-237-23AND TM 1-1520-280-23 STATES THAT NODISPLACEMENT OR DISBONDING ISALLOWED. AED HAS REVIEWED THEREQUEST AND BASED ON STRUCTURALANALYSIS OF THE DROOP STOP PIN THEREQUEST IS AUTHOURIZED. SEE COPY OFMEO IN THE BACK OF THIS HISTORICALBOOK. (RJ0827, R/SPEC)
22-Feb-2010 1
FT. RUCKER, AL
thomas.m.lilly
USAACEAWR 1251 R2 SUPERCEDED, ACFT NOWOPERATING UNDER AWR 1251 REV. 3 DTD26FEB 10. (5256.2 ACFT HRS) (EYEBOLTS)(RJ0827)
02-Mar-2010 1
FT. RUCKER, AL
thomas.m.lilly
USAACEM-MOD FILTER BUTTON POPPED AT 5361.5ACFT HRS. REPLACED FILTER-MOC OK.(RJ0827)
09-Apr-2010 1
FT. RUCKER, AL
thomas.m.lilly
USAACEAWR 1445 DTD 20 MAR 2009 REV 2 (AFCS) ISNOT APPLICABLE @ 5407.8 ACFT HRS.(VM4663)
22-Apr-2010 1
FT RUCKER, AL
thomas.m.lilly
USAACEOPERATING UNDER LIMITATION ANDRESTRICTIONS SPECIFIED IN ASR 1455 REV 1.DTD 23 OCT 09 (CAPS) @ 5407.8 ACFT HRS.(VM4663)
22-Apr-2010 2
FT RUCKER, AL
thomas.m.lilly
USAACEH-60-10-AMAM-12 (IMPROVED DRAG BEAM)C/W AT 5426.1 ACFT HRS (RJ0827)
04-May-2010 1
FT. RUCKER, AL
thomas.m.lilly
USAACEACFT NO LONGER OPERATING UNDER AWR927 DTD 06 JUN 03- AWR WAS SUPERCEDEDBY AWR 1681 ACFT NOW OPERATING IAWWITH AWR 1681 DTD 10 MAY 10 (5479.0 ACFTHRS) (RJ0827)
19-May-2010 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-10-ASAM-07 STABILATOR HINGEFITTINGS C/W AT 5479.0 ACFT HRS (RJ0827)
20-May-2010 1
FT. RUCKER,A L
thomas.m.lilly
USAACEACFT OPERATING WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1514 DTD01 JUL 10 (ACFT HRS 5482.2) (RJ0827)
25-May-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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 34 of 61
USAACEACFT OPERATING WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1529 DTD07 OCT 09. ( ACFT HRS 5482.2) (RJ0827)
25-May-2010 2
FT. RUCKER,AL
thomas.m.lilly
USAACEAWR 1220 DTD 22 MAY 08 R4 (ENHANCEDSCHEDULED MAINTENANCE) SUPERCEDEDBY AWR 1220 R5 DTD 28 MAY 10 . ACFT NOWOPERATING AS PRESCRIBED IN REVISEDAWR. (5482.2 ACFT HRS) (RJ0827)
02-Jun-2010 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-10-ASAM-08 APU AND APU FIREWALLC/W AT 5482.5 ACFT HRS (RJ0827)
09-Jun-2010 1
FT. RUCKER, AL
thomas.m.lilly
USAACEH-60-10-SOF-02 SPINDLE LUG NDI ANDRETIREMENT LIFE CHANGES C/W AT 5502.0ACFT HRS (RJ0827)
22-Jun-2010 1
FT. RUCKER, AL
thomas.m.lilly
CSCOCM / ACE PERFORMED AT 5505 ACFT HRSBY TEAM MEMBER DD AMCOM / RASM-E(JB9001)
25-Jun-2010 1
FT. CAMPBELL, KY
thomas.m.lilly
USAACEU-60-10-AMAM-16 (COMMON MISSLEWARNING SYSTEM GUARDED DISPENXESWITCH) IS NOT APPLICABLE TO THIS A/C5505 ACFT HRS (VM4663)
25-Jun-2010 2
FT RUCKER, AL
thomas.m.lilly
USAACEH-60-09-ASAM-11 CARGO DOOR WINDOWEMERGENCY JETTISON HANDLE INSP C/W AT5505 (VM4663)
27-Jun-2010 1
FT RUCKER, AL
thomas.m.lilly
USAACEONE TIME INSP ON T/R QUADRANT MICROSWITCH FOR JAM NUT SAGETIES INSTALLED.C/W @ 5506.6 ACFT HRS. (VM4663)
02-Jul-2010 1
FT RUCKER, AL
thomas.m.lilly
USAACEMEC F111786 - RIGHT 34.5 CHANNELCRACKED JUST AFT OF FS308. COMPLETEREPAIR IAW AJM-BL34-1B, TM 1-1520-237-23-6AND TM 1-1520-204-23 AND ADJUST 34.5CHANNEL SPLICE LOCATION TO STA 320.AUTHORIZED BY DAMON N. HAY AT 5512.4ACFT HRS ON 14 JUL 10. (RC1002)
14-Jul-2010 1
FT. RUCKER, AL
thomas.m.lilly
USAACET/R CABLE TENSION CHECK COMPLETED AT5512.4 ACFT HRS. L/H=185. R/H=185 AT 33*C.(MB1137)
19-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 2
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEPHASE INSPECTION #9 COMPLETED AT 5512.4ACFT HRS. NEXT PHASE IS #10 ST 6232.4ACFT HRS. (MB1137)
23-Jul-2010 1
FT. RUCKER, AL.
thomas.m.lilly
USAACET/R BIAS MEASUREMENTS COMPLETED AT5512.4 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 4.745/5.074, YELLOW: 4.708/5.042,BLUE: 4.075/4.408, BLACK: 4.029/4.368.(MB1137)
24-Jul-2010 1
FT. RUCKER, AL.
thomas.m.lilly
USAACET/R CABLE TENSION CHECK COMPLETED AT5512.4 ACFT HRS. LH=185, R/H=185 AT 33*.(MB1137)
24-Jul-2010 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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 35 of 61
USAACEMAIN ROTOR RIG CHECK COMPLETED AT5512.4 ACFT HRS. FWD=SHORTENED 1 FLAT,AFT= LENGTHENED 1 FLAT, LAT= NOADJUSTMENT. (MB1137)
26-Jul-2010 1
FT. RUCKER, AL.
thomas.m.lilly
USAACEH-60-10-AMAM-05 COMPLIED WITH AT 5513.9ACFT HRS. (TRI MAX 30 EXTINGUISHER NOTINSTALLED) (RJ0827)
29-Jul-2010 1
FT. RUCKER, AL.
thomas.m.lilly
USAACEH-60-10-ASAM-11 COMMON COMPONENTRETIREMENT CHANGE ITEMS UPDATE C/W AT5522.5 ACFT HRS (TP1634)
03-Aug-2010 1
FT. RUCKER, AL.
thomas.m.lilly
USAACEAWR 1514 DTD 01 JUL 10 SUPERCEDED BYAWR 1514 REV.1 DTD 03 AUG. 10 @ 5523.9ACFT HRS (TP1634) (A FS64)
03-Aug-2010 2
FT. RUCKER, AL.
thomas.m.lilly
USAACET/R CABLE TENSION CHECK COMP AT 5521.5ACFT HRS L/H 166, RH 167 26*C. (TP1634)
04-Aug-2010 1
FT. RUCKER, AL.
thomas.m.lilly
USAACEH-60-10-ASAM-12 T700 SERIES ENGINESCOMMON COMPONENT RETIREMENT CHANGETIMES C/W AT 5532.2 ACFT HRS. (RJ0827)
10-Aug-2010 1
FT. RUCKER, AL.
thomas.m.lilly
USAACET/R CABLE TENSION CK COMPLETED AT5532.2 ACFT HRS- L/H: 165 R/H: 166 AT 26'C.(RJ0827)
10-Aug-2010 2
FT. RUCKER, AL.
thomas.m.lilly
USAACEH-60-10-ASAM-15 IMPROVE EXTERNALSTORES SUPPORT SYSTEM (ESSS) FUEL;SYSTEM VENT ELBOW C/W AT 5532.2 ACFTHRS (RJ0827)
10-Aug-2010 3
FT. RUCKER, AL.
thomas.m.lilly
USAACEACFT OPERATING UNDER LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1455 DTD23 OCT 10 (5551.3 ACFT HRS) (RJ0827)
14-Aug-2010 1
FT. RUCKER, AL.
thomas.m.lilly
USAACEH-60-10-ASAM-16 RESCUE HOIST CABLE CUTHARNESS CONNECTOR C/W AT 5611.3 ACFTHRS (NO HOIST INSTALLED) (RJ0827)
13-Sep-2010 1
FT. RUCKER, AL.
thomas.m.lilly
USAACEACFT OPERATING UNDER LIMITATIONS ANDRESTRICTIONS OF AWR 1639 DTD 28 MAY 10(5611.3 ACFT HRS) (RJ0827)
14-Sep-2010 1
FT. RUCKER, AL.
thomas.m.lilly
USAACEACFT OPERATING WITHIN LIMITATIONS ANDRESTRICTIONS OF AWR 1529, R.1 DTD07OCT10 (FOGS) (5662.0 HRS) SUPERCEDESAWR DTD 07 OCT 09. (RJ0827)
07-Oct-2010 1
FT. RUCKER, AL.
thomas.m.lilly
USAACEH-60-11-AMAM-04 H-60-11-AMAM-04 ULLS-A(E)(IMMC) (LCF CHANGE 61) C/W AT 5724.0 ACFTHRS (N/A TO THIS ACFT/IVHMS NOTINSTALLED) (RJ0827)
27-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 5724.0ACFT HRS (N/A IMDS/IVHMS NOT INSTALLED)(RJ0827)
27-Oct-2010 2
LOWE AHP
thomas.m.lilly
USAACEACFT NO LONGER OPERATING UNDER AWR1455 REV 1, DTD 23 OCT 09- N/A "B" CAPFOUND NOT INSTALLED (5736.0 ACFT HRS(RJ0827)
05-Nov-2010 1
LOWE AHP
thomas.m.lilly
USAACEACFT NO LONGER OPERATING UNDER AWR1455, DTD 23 OCT 10- N/A "B" CAP FOUNDNOT INSTALLED (5736.0 ACFT HRS (RJ0827)
05-Nov-2010 2
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 36 of 61
USAACEM/MOD FILTER BUTTON POPPED AT 5766.1ACFT HRS.XSMN SERVICEABILITY CKCOMPLETED30 MIN GROUND ROUND AND 30MIN HOVER COMPLETED RESINPECTION OFMAIN AND INPUT MOD CHIP DETECTORSCOMPLETED- NO CHIPS FOUND. (RJ0827)
17-Nov-2010 1
LOWE AHP
thomas.m.lilly
USAACEACFT OPERATING WITHIN LIMITATIONS ANDRESTRICTIONS OF AWR 1455, DTD 23OCT09(5777.0 ACFT HRS) (RJ0827)
20-Nov-2010 1
LOWE AHP
thomas.m.lilly
USAACEH-60-11-ASAM-03 HAMILTON STANDARDHYDRO-MECHANICAL UNITS (HMU) C/W AT5777.0 ACFT HRS- N/A TO THIS ACFT (RJ0827)
24-Nov-2010 1
LOWE AHP
thomas.m.lilly
USAACEH-60-11-ASAM-04 AN/ARN-153 TCN-500 TACANRECEIVER BEARING ERROR C/W AT 5784.7ACFT HRS (N/A ACFT NOT EQUIPPED)(RJ0827)
03-Dec-2010 1
LOWE AHP
thomas.m.lilly
USAACEH-60-11-ASAM-06 CYCLIC STICK STOP BOLTSC/W AT 5867.7 ACFT HRS. (SC2006 ( AFS 36))
04-Feb-2011 1
LOWE AHP
thomas.m.lilly
USAACEMEO - A6055 C/W AT 5867.7 ACFT HRS.REPLACED BUSHING IAW 1-1520-237-23-7 WP0565 AND WP 0564. (SC2006 ( AFS 36))
04-Feb-2011 2
LOWE AHP
thomas.m.lilly
USAACECOLLECTIVE BOOST LINK ASSY REPLACEDAT 5867.7 ACFT HRS. (SC2006 ( AFS 36))
04-Feb-2011 3
LOWE AHP
thomas.m.lilly
USAACET/R BIAS MEASUREMENTS COMPLETED AT5867.7 ACFT HRS RED: 5.110 - 4.753 = .347,YELLOW: 5.059 - 4.715 = .344, BLUE: 4.401 -4.096 = .305, BLACK: 4.346 - 4.041 = .305(SC2006)
05-Feb-2011 1
LOWE AHP
thomas.m.lilly
USAACE120 HOUR INSP AND 360 HR INSP C/W AT5867.7 ACFT HRS. (SC2006)
05-Feb-2011 2
LOWE AHP
thomas.m.lilly
USAACEH-60-11-AMAM-06 MEDICAL CAROUSELREFURBISHMENT C/W AT 5868.2 ACFT HRS.N/A NOT INSTALLED. (SC2006 ( AFS 83))
07-Feb-2011 1
LOWE AHP
thomas.m.lilly
USAACEH-60-11-ASAM-08 LOS/IFF ANTENNA ANDIVHLLMS ACCELEROMETER CONNECTORSSAFETY WIRE C/W AT 5889.5 AIRCRFT HOURS.(LW2720 R/SPEC)
12-Feb-2011 1
FT. RUCKER, AL
thomas.m.lilly
USAACEMAIN MOD CHIP LIGHT ILLUMINATED ONBATTERY NBIT. CHIP DETECTOR WORKSHEETSAYS OLD STYLE. CHECKED & FOUND NBITINSTALLED. (SC2006 (AFS747))
03-Mar-2011 1
FT. RUCKER, AL
thomas.m.lilly
USAACEACFT OPERATING WITHIN LIMITATIONS ANDRESTRICTIONS OF AWR 1505 REV 3 DTD 21OCT 09 (5966.3 ACFT HRS) (MH1534)
15-Mar-2011 1
LOWE AHP, FT.RUCKER, AL.
mary.b.hodge
USAACEMEC F124091 AUTHORIZATION GRANTED TOINSTALL HUD TDT AMPLIFIER DISCONNECTSIAW MEO A6206 REV. A
25-Mar-2011 1
LOWE AHP, FT.RUCKER, AL.
olivia.d.williams
USAACEH-60-11-ASAM-09 (INTERNAL AUXILIARY FUELTRANSFER SYSTEM) IAFTS COMPLIED WITHAT 5982.1 ACFT HRS. IAFTS NOT INSTALLED.(AFS 767)
28-Mar-2011 1
LOWE AHP, FT.RUCKER, AL.
shelia.d.cook
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 37 of 61
USAACEDELAYED ENTRY: ACFT INDUCTED INTOULLS-A(E) ON 16-MAR-11 AT 5966.3 ACFT HRS.
06-Apr-2011 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEOPERATING WITHIN LIMITATIONS ANDRESTRICTIONS OF AWR 1681 DTD 10 MAY 10.(6010.7 ACFT HRS) (MH1534).
14-Apr-2011 1
LOWE AHP, FT.RUCKER, AL.
mary.b.hodge
USAACEH-60-11-AMAM-11, AIRWORTHINESS RELEASESTATUS UPDATE C/W AT 6,043.4 ACFT HRS.AFFECTED AWR'S NO LONGER APPLY. AFS594 (SC2006)
26-Apr-2011 1
LOWE AHP, FT.RUCKER, AL.
shelia.d.cook
SES-IAIRCRAFT PAINT STRIPPED BY PLASTICMEDIA BLASTING.
17-May-2011 1
HSV, AL
HO666422
SES-IAIRCRAFT PRIMED WITH ONE COAT MIL-PRF-2377J, PAINTED WITH ONE COAT MIL-DTL-64159 TYPE II.
19-May-2011 1
HSV, AL
HO666422
SESIC/W H-60-AMAM-11-09 @ 6052.6 ACF HRS (DAFORM 2408-19-3 ENGINE COMPONENTOPERATING HOUR RECORD.
20-May-2011 1
HSV, AL
HO666422
USAACE23 MAY 11 - IMPENDING BY PASS BUTTONPOPPED DURING FLIGHT AT 6052.6 ACFT HRS.REPLACES MAIN MODULE S/N A26500531 OILFILTER IAW 0057 00. TSN ON XSMN 5889 HRS.PID (FJ021809).
23-May-2011 1
LOWE AHP, FT.RUCKER, AL.
frances.j.jackson
CSCOCM/ACE PERFORMED AT 6067.3 ACFT HRSBY TEAM MEMBER R. AFMA RASM-E.
03-Jun-2011 1
FT.CAMPBELL, KY.42223
dean.a.keirn
USAACEH-60-11-AMAM-13 EXTERNAL RESCUE HOISTMOUNT FITTING COMPLETED AT 6070.3 ACFTHRS. NA TO THIS ACFT. (TB1027)
08-Jun-2011 1
LOWE AHP, FT.RUCKER, AL.
tony.barnes
USAACEM/MOD FILTER BUTTON POPPED AT 6096.8A/C HRS. WTH TSN 5932.8 HRS / INSPECTEDAND REPLACED FILTER BUTTON CW TM 1-1520-237-7. (FJ1809)
22-Jun-2011 1
LOWE AHP, FT.RUCKER, AL.
frances.j.jackson
USAACEACFT NO LONGER OPERATING UNDER MEOA6055 DUE TO REPLACEMENT OF BLACK M/RSTOP BUSHING. COMPLETED AT 6220.1 ACFTHRS.
30-Jun-2011 1
LOWE AHP, FT.RUCKER, AL.
mae.p.belford
USAAACEH-60-11-ASAM-13, ENGINE AIR INLET VALVE @6130.1 AC HRS
09-Jul-2011 1
LOWE AHP, FT.RUCKER, AL.
frances.j.jackson
USAACEH-60-11-SOF-01, DISCREPANT SELF LOKCINGDOUBLE HEXAGON NUTS @6130.1 AC HRS
10-Jul-2011 1
LOWE AHP, FT.RUCKER, AL.
frances.j.jackson
USAACEH-60-11-AMAN-15, IVHMS ACCELEROMETERS@ 6139.9 AC HRS
14-Jul-2011 1
LOWE AHP, FT.RUCKER, AL.
frances.j.jackson
USAACEH-60-11-ASAM-14, ENGINE COWLING REPAIRRESTRICTIONS @ 6161.4 AC HRS
20-Jul-2011 1
LOWE AHP, FT.RUCKER, AL.
frances.j.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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 38 of 61
USAACEDELAYED ENTRY MEC F123536 DATED 14 MAR11 REQUEST ATUHORIZATION TO REPAIRRIGHT BEADED PANEL. PERMISSIONGRANTED.
04-Aug-2011 1
LOWE AHP, FT.RUCKER, AL.
frances.j.jackson
USAACEDELAYED ENTRY MEC F127804 DATED 06 JUN11; REQUEST AUTHORZATION AS OWHETHER AIRCRAFT MAY REMAIN INSERCVICE. PERMISSION GRANTED.
04-Aug-2011 3
LOWE AHP, FT.RUCKER, AL.
frances.j.jackson
USAACEDELAYED ENTRY MEC F124091 DATED 24 MAR11; REQUEST AUTHORIZATIO TO INSTLALLHUB TGT. PERMISSION GRANTED
04-Aug-2011 4
LOWE AHP, FT.RUCKER, AL.
frances.j.jackson
USAACEDELAYED ENTRY MEC F72883 DATED 27 FEB08; REQUEST EVAL AND APPROVAL TOREPAIR CRACK AREA. PERMISSIONGRANTED.
05-Aug-2011 1
LOWE AHP, FT.RUCKER, AL.
frances.j.jackson
USAACEDELAYED ENTRY MEC F92347 DATED 08 MAY09; REQUEST PERMISSION TO INSTALL AWEAR STRIP ON L/H UPPER TRACK.PERMISSION GRANTED
05-Aug-2011 2
LOWE AHP, FT.RUCKER, AL.
frances.j.jackson
USAACEAIRCRAFT NO LONGER OPERATING IAW MEOA6055 AT AIRCRAFT HRS: 6220.1.
02-Sep-2011 1
LOWE AHP, FT.RUCKER, AL.
debra.r.chancellor
USAACEMAIN ROTOR RG CHECK PRIMARY SERVOCONTROL ROD BIAS FWD: NO ADJUSTMENT;AFT: NO ADJUSTMENT; LAT 1/2 FLAT IN.
08-Sep-2011 1
LOWE AHP, FT.RUCKER, AL.
claudia.f.anderson
USAACE720 HOUR PHASE # 10 COMPLETED AT 6220.1ACFT HRS. NEXT PHASE # 11 IS DUE AT6940.1 ACFT HRS.
09-Sep-2011 1
LOWE AHP, FT.RUCKER, AL.
debra.r.chancellor
USAACET/R CABLE TENSION CHECK COMPLETED AT6220.1 ACFT HRS. L/H 145 R/H 145 TEMP 25.2DEGREES CELSIUS.
10-Sep-2011 1
LOWE AHP, FT.RUCKER, AL.
debra.r.chancellor
USAACET/R BIAS MEASUREMENTS COMPLETED AT6220.1 ACFT HRS. YELLOW 4.720-5.049=0.329RED 4.822 5.152=0.330 BLUE 4.154 4.486=0.332BLACK 4.037 4.371=0.334
10-Sep-2011 2
LOWE AHP, FT.RUCKER, AL.
debra.r.chancellor
USAACEACFT OPERATING IAW AWR 1639 REV 3 DTD 1JUN 11 LIMITATIONS AND RESTRICTIONS INAWR.
16-Sep-2011 2
LOWE AHP, FT.RUCKER, AL.
frances.j.jackson
USAACEMAIN TRANSMISSION SN: A26500531 AT TSN:6058 OIL FILTER BUTTON POPPED.COMPLETED SERVICEABILITY INSP (OK) IAWIETM 1-1520-210-23-7 WP 0626. (ACFT HRS:6222.4)
18-Sep-2011 1
LOWE AHP, FT.RUCKER, AL.
debra.r.chancellor
USAACEMAIN TRANSMISSION, SN: A26500531, OILFILTER BUTTON POPPED @ 6222..4 ACFT HRSW/TSN: 6058. SERVICEABILITY CK. INSTALLED1ST STAGE FILTER
18-Sep-2011 2
LOWE AHP, FT.RUCKER, AL.
mary.b.hodge
USAACET/R TENSION CHECK COMPLETED @ 6229.8ACFT HRS. L/H 144 R/H 144 @ 26.9 DEGREESCELSIUS.
23-Sep-2011 1
LOWE AHP, FT.RUCKER, AL.
mary.b.hodge
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 39 of 61
USAACEH-60-11-AMAM-20, AN/ASN-128D DOPPLERAND AMPS SOFTWARE UPGRADE INSPCOMPLETED @ 6228.3 ACFT HRS. (AFS 594).
23-Sep-2011 2
LOWE AHP, FT.RUCKER, AL.
mary.b.hodge
USAACECOMPLIED WITH H-60-12-SOF-01 @ 6268 ACFTHRS.
08-Oct-2011 1
LOWE AHP, FT.RUCKER, AL.
vickie.l.meadows
USAACEH-60-12-SOF-02 (TAIL ROTOR INTERMEDIATEGEARBOX) C/W AT 6268.0 ACFT HRS.
11-Oct-2011 1
LOWE AHP, FT.RUCKER, AL.
debra.r.chancellor
USAACEH-60-12-SOF-03 (TAIL ROTOR INTERMEDIATEGEARBOX) C/W AT 6279.1 ACFT HRS. (AFS545).
14-Oct-2011 1
LOWE AHP, FT.RUCKER, AL.
bryan.w.hollis
USAACEAIRCRAFT BEING OPERATED I/A/W MEOA6055 REV.B DUE TO YELLOW M/R LEADDROOP STOP BUSHING DE-BONDED.REPLACEMENT OF DROOP STOP BUSHINGREQIRED AT THE NEXT PMI DUE AT 6580.1AIRCRAFT HOURS.
20-Oct-2011 1
LOWE AHP, FT.RUCKER, AL.
mae.p.belford
USAACEH-60-11-AMAM-19 (IMMC LCF CHG 62REQUIREMENTS )C/W @ 6298.6 ACFT HRS
22-Oct-2011 1
LOWE AHP, FT.RUCKER, AL.
janice.m.bruce
USAACEAWR 1505 REV 3 SUPERCEDED BY AWR 1505REV 4 DTD 21 OCT 11 @ 6298.6 ACFT HRS.ACFT NOW OPERATING WITHIN LIMITATIONSAND RESTRICTIONS SPECIFIED IN AWR 1505REV 4.
22-Oct-2011 2
LOWE AHP, FT.RUCKER, AL.
patrick.a.newton
USAACEAIRCRAFT NO LONGER OPERATING IAW AWR1529 REV, 1 DATED 07 OCT 10 @ 6325.0 ACFTHRS.
28-Oct-2011 1
LOWE AHP, FT.RUCKER, AL.
claudia.f.anderson
USAACEAIRCRAFT OPERATING IAW AWR 1529 REV 2DATED 07 OCT 11 @ 6325.0 ACFT HRS.
28-Oct-2011 2
2810LOWE AHP, FT.RUCKER, AL.
claudia.f.anderson
USAACEH-60-12-AMAM-03, TRANSPONDER ANDCOMMON MISSILE WARNING SYSTEM C/W @6325.0 ACFT HRS. (CMWS MWO NOTINSTALLED)
31-Oct-2011 1
LOWE AHP, FT.RUCKER, AL.
claudia.f.anderson
USAACEAIRCRAFT NO LONGER OPEATING IAW AWR1455 R1 DATED 23 OCT 09 @ 6330.3 ACFTHRS.
03-Nov-2011 1
LOWE AHP, FT.RUCKER, AL.
claudia.f.anderson
USAACEAIRCRAFT OPEATING IAW AWR 1455 REV 2DATED 31 OCT 2011 @ 6330.3 ACFT HRS.
03-Nov-2011 2
LOWE AHP, FT.RUCKER, AL.
claudia.f.anderson
USAACEAIRCRAFT NO LONGER OPERATING IAW AWR1455 R2 DATED 31 OCT 11 @ 6377.7 ACFT HRS.
21-Nov-2011 1
LOWE AHP, FT.RUCKER, AL.
claudia.f.anderson
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 40 of 61
USAACEAIRCRAFT OPERATING IAW AWR 1455 R3DATED 10 NOV 11 @ 6377.7 ACFT HRS.
21-Nov-2011 2
LOWE AHP, FT.RUCKER, AL.
claudia.f.anderson
USAACEAIRCRAFT OPERATING IAW AWR 1153, R6,DATED 18 NOV 11, ON 06 DEC 2011 @ 6404.6ACFT HRS.
05-Dec-2011 2
LOWE AHP, FT.RUCKER, AL.
claudia.f.anderson
USAACEAIRCRAFT OPERATING UNDER THERESTRICTIONS AND GUIDLINES OF MEOA5826 REV B
06-Dec-2011 1
LOWE AHP, FT.RUCKER, AL.
olivia.d.williams
USAACEH-60-12-ASAM-02 DRAG BEAMREPLACEMENT @ 6405.6 ACFT HRS.
07-Dec-2011 1
LOWE AHP, FT.RUCKER, AL.
claudia.f.anderson
USAACEH-60-11-ASAM-13 (INLET ANTI-ICE VALVE)COMLETED AT 6462.1 ACFT HRS.
14-Jan-2012 1
LOWE AHP, FT.RUCKER, AL.
olivia.d.williams
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
USAACEAWR 1639 R3, DTD 1 JUN 11 SUPERCEDED BYAWR 1800 DTD 30 NOV 11 AT 6474.0 ACFTHRS.
19-Jan-2012 2
LOWE AHP, FT.RUCKER, AL.
mae.p.belford
USAACEACFT OPERATING IAW AWR 1800 DTD 30 NOV11 AT 6474.0 ACFT HRS.
19-Jan-2012 3
LOWE AHP, FT.RUCKER, AL.
mae.p.belford
USAACEH-60-12-SOF-04 - (BREEZE EASTERNEXTERNAL HOIST) COMPLIED WITH AT 6543.7AIRCRAFT HOURS.
18-Feb-2012 1
LOWE AHP, FT.RUCKER, AL.
thomas.e.mitchell
USAACEH-60-12-ASAM-06 (UPPER BULKHEAD FUELSYSTEM BREAKAWAY VALVE AND FIREEXTINGUISHING SYSTEM DIRECTIONALVALVE) COMPLIED WITH ON 23 FEB 2012 AT6550.7 AIRCRAFT HOURS.
23-Feb-2012 1
LOWE AHP, FT.RUCKER, AL.
thomas.e.mitchell
USAACEACFT OPERATING UNDER AWR 1251, R4 DTD22FEB12, EYEBOLTS ON BIFILAR ARMS,SUPERSEDING 1251 R3.
27-Feb-2012 1
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
USAACECOMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-17 @ 6579.7 ACFT HRS.
07-Mar-2012 1
LOWE AHP, FT.RUCKER, AL.
vickie.l.meadows
USAACEAIRCRAFT NO LONGER BEING OPERATEDI/A/W MEO A6055 REV.B DUE TO YELLOW M/RLEAD DROOP STOP BUSHING. INSPECTIONOF DROOP STOP BUSHING COMPLETED AT6579.7 AIRCRAFT HOURS.
08-Mar-2012 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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 41 of 61
USAACEAIRCRAFT NO LONGER BEING OPERATEDI/A/W MEO A6055 REV.B DUE TO RED LEADBUSHING. REPLACED RED LEAD DROOPSTOP BUSHING COMPLETED AT 6579.7AIRCRAFT HOURS.
08-Mar-2012 2
LOWE AHP, FT.RUCKER, AL.
thomas.e.mitchell
USAACET/R CABLE ADJUSTMENT DUE FOR FAIL TAILROTOR COMPLETE RIG COMPLETED INCONJUNCTION WITH T/R COMPLETE RIG.ADJUSTED RIGHT SIDE (155 LBS) ADJUSTEDLEFT SIDE (155 LBS) AT 26 DEGREES (C), AT6579.7 AIRCRAFT HOURS. (LN026882,TW027341)
08-Mar-2012 3
LOWE AHP, FT.RUCKER, AL.
thomas.e.mitchell
USAACET/R BIAS DUE: COMPLETED AT 6579.7AIRCRAFT HOURS: MEASUREMENT: BLACK:3.882-4.217=0.335, YELLOW: 4.570-4.906=0.336,BLUE: 3.956-4.292=0.336, RED: 4.695-5.028=0.333, MR# 114688.
08-Mar-2012 4
LOWE AHP, FT.RUCKER, AL.
thomas.e.mitchell
USAACET/R BIAS COMPLETE RIG DUE: COMPLETEDAT 6579.7 AIRCRAFT HOURS, CHECKEDFOUND OK IAW 237-23-9 WP 11051,MEASUREMENT: BLACK: 3.882-4.217=0.335,YELLOW: 4.570-4.906=0.336, BLUE: 3.956-4.292=0.336, RED: 4.695-5.028=0.333, MR#114688. (LN026882,JT027338, TW027341)
09-Mar-2012 1
LOWE AHP, FT.RUCKER, AL.
thomas.e.mitchell
USAACECABLE TENSION CHECK COMPLETED AT6589.6 AIRCRAFT HOURS: L/H=150 LBSR/H=140 LBS TEMP=21 DEGREES (C).(RG022045,JB022017).
15-Mar-2012 1
LOWE AHP, FT.RUCKER, AL.
thomas.e.mitchell
USAACET/R BIAS DUE: COMPLETED AT 6589.6AIRCRAFT HOURS: MEASUREMENT: BLACK:4.46-4.13=0.33, YELLOW: 5.12-4.79=0.33, BLUE:4.51-4.18=0.33, RED: 5.18-4.85=0.33, MR#118978.
15-Mar-2012 3
LOWE AHP, FT.RUCKER, AL.
thomas.e.mitchell
USAACEACFT OPERATING IAW AWR 1648, R2 DTD09MAR12, MAGNUS LAPTOPS, SUPERSEDINGR1.
20-Mar-2012 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACET/R BIAS DUE: COMPLETED AT 6603.5AIRCRAFT HOURS: MEASUREMENT: BLACK:3.882-4.217=0.335, YELLOW: 4.570-4.906=0.336,BLUE: 3.956-4.292=0.336, RED: 4.695-5.028=0.333, MR# 114688. (SJ011449)
20-Mar-2012 2
LOWE AHP, FT.RUCKER, AL.
thomas.e.mitchell
USAACEMAIN MOD S/N 26500531, WITH TSN OF 6454HOURS: TRANSMISSION FILTER IMPENDINGBYPASS INDICATOR IS NO LONGERIMPENDING (AZ603137) AT 6618.2 AIRCRAFTHOURS. (ACTION TAKEN): REPLACED MAINMOD OIL FILTERS IAW WP 657,656,626 NODEBRIS AND NO CHIPS FOUND.(MA027101,CC027323)
22-Mar-2012 1
LOWE AHP, FT.RUCKER, AL.
thomas.e.mitchell
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
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 42 of 61
USAACEMEC F144295, AUTHORIZATION GRANTEDFOR CCAD DFT TO REPLACE THE RH BEADEDPANEL WITH THE FOLLOWING KITS: 1680-01-513-6988, Plating Kit, R/H Beaded Panel andassociated kits, 1680-01-551-8404, Stringer Kit,R/H, 1680-01-551-8406, Window Kit, R/H, 1680-01-551-8403, Reinforce Kit, R/H BL 34.5. ACFTHRS: 6671.0.
16-Apr-2012 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEMEC F144296, AUTHORIZATION GRANTEDFOR CCAD DFT TO REPLACE THE LH BEADEDPANEL WITH THE FOLLOWING KITS: 1680-01-513-6990, Plating Kit, L/H Beaded Panel andassociated kits, 1680-01-551-7983, Stringer Kit,L/H. 1680-01-552-0092, Window Kit, L/H. 1680-01-551-8405, Reinforce Kit, L/H BL 34.5. ACFTHRS: 6671.0.
16-Apr-2012 2
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEOCM/ACE PERFORMED AT 6671 AIRCRAFTHOURS BY TEAM MEMBERS QQ AND PENTERED BY JW807912 FROM L-3 RASM-E.
19-Apr-2012 1
LOWE AHP, FT.RUCKER, AL.
debra.r.chancellor
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
USAACEMEC F145525, AUTHORIZATION GRANTEDFOR CCAD DFT TO REPLACE LH STA 265FRAME. 6671.0 ACFT HRS.
04-May-2012 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEMEC F145528, AUTHORIZATION GRANTEDFOR CCAD DFT TO REPLACE RH STA 265FRAME. 6671.0 ACFT HRS.
04-May-2012 2
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
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
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
USAACEH-60-12-ASAM-07 - ELECTRICAL WIRINGCHAFE, COMPLIED WITH @ 6671.0 AIRCRAFTHOURS ON 12 JUL 2012. R/SPEC. (TM027105)USAACE, FT. RUCKER, AL.
12-Jul-2012 1
LOWE AHP, FT.RUCKER, AL.
thomas.e.mitchell
USAACEH-60-12-AMAM-12 - MAINTENANCEMANDATORY, ALL H-60-A/K/L SERIESAIRCRAFT, RESCINDED COMMONCOMPONENT REMOVAL DATE COMPLIEDWITH AT 6671.0 AIRCRAFT HOURS ON THISDATE. RESCINDS H-60-10-ASAM-11. R/SPEC.(TM027105) USAACE, FT. RUCKER, AL.
13-Jul-2012 1
LOWE AHP, FT.RUCKER, AL.
thomas.e.mitchell
USAACEH-60-11-ASAM-08 - (CARGO HOOK MANUALRELEASE SPRING ASSEMBLY) COMPLIEDWITH ON 23 JUL 2012 @ 6671.0 AIRCRAFTHOURS BY (WS01493). R/SPEC. (TM027105)USAACE, FT. RUCKER, AL.
23-Jul-2012 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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 43 of 61
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
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
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
USAACEINSP H-60-12-AMAM-09, HYDRAULIC LINECHAFE DUE TO MISSING CLAMPS,COMPLETED, FAILED, AND CORRECTEDDEFICIENCIES 22AUG12 @ 6671 ACFT HRS
22-Aug-2012 1
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-09 (BREEZE EASTERN EXTERNALRESCUE HOIST CARTRIDGE ACTUATEDDEVICE (CAD) ELECTRICAL CONNECTOR), @6671.0 ACFT HRS
23-Aug-2012 1
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
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
USAACEH-60-12-AMAM-15 (TRIM ACTUATORS),COMPLIED WITH AND COMPLETED 31AUG12@ 6671.0 ACFT HRS.
31-Aug-2012 2
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
USAACEH-60-12-ASAM-10, ENGINE ANTI-ICE/STARTBLEED VALVES (AISBV), INSP COMP PASSED06SEP12 @ 6671.0 ACFT HRS
06-Sep-2012 1
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
USAACEH-60-12-ASAM-11, HYDRO-MECHANICAL UNIT(HMU), INSP COMP-FAILED 06SEP12 @ 6671.0ACFT HRS
06-Sep-2012 2
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
USAACEMAIN ROTOR RIG COMPLETED (CD022187)WITH THE FOLLOWING ADJUSTMENTS: FWD-SHORTENED 1 FLAT AFT- LENGTHENED 1FLAT LAT- SHORTENED 3 FLATS
17-Sep-2012 1
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
USAACETAIL ROTOR BIAS DIMENSION READINGS:RED: 4.794/5.123=.333, YELLOW:4.7605/5.0985=.338, BLUE: 4.098/4.427=.329,BLACK: 4.07/4.4=.330. COMPLETED AT 6671.0ACFT HRS.
20-Sep-2012 1
LOWE AHP, FT.RUCKER, AL.
jessica.n.kennedy
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 44 of 61
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
USAACEH-60-12-AMAM-16, MAIN ROTOR SPINDLE SUB-COMPONENT TRACKING REQUIREMENTS,INSP COMPLIED WITH 24SEP12 @ 6671.0 ACFTHRS
24-Sep-2012 1
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
USAACEDELAYED ENTRY: ACFT DATE OFMANUFACTURE IS FEB 86
02-Oct-2012 1
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
USAACEMEC F154149, AUTHORIZATION GRANTEDFOR A DEVIATION OF THE PEDAL ADJUSTACCESS COVER INSTALLATION PN 70209-01013-101/102. BOLT PN AN3-3A MAY BE USEDIN LIEU OF SCREW MS27039-1-07.
15-Oct-2012 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACET/R CABLE TENSION CHECK COMP (GOOD) -READINGS R-120 L-122 @ 8.9°C TENS.MR#109407 30OCT12 @ 6681.2 ACFT HRS
30-Oct-2012 1
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
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) C/W @ 6697.5 ACFTHRS. (HARNESS FAILED. HARNESS WASREPOSITIONED)
08-Nov-2012 1
LOWE AHP, FT.RUCKER, AL.
mary.b.hodge
USAACET/R CABLE TENSION CHECK COMPLETED,PASSED L/H-135LBS R/H-135LBS @ 21°CTENSIONMETER MR# 122358 28NOV12 @6723.9 ACFT HRS
28-Nov-2012 1
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
USAACETAIL ROTOR BIAS COMPLETED AT 6723.9ACFT HRS. RED: 4.791/5.101/.310/0.4/3.0BLACK: 4.084/4.385/.301/0.4/3.0 YELLOW:4.740/5.048/.308/0.4/3.0 BLUE:4.075/4.390/.315/0.4/3.0
28-Nov-2012 2
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
USAACEH-60-13-AMAM-03 DIGITAL ENGINE CONTROLUNIT (DECU) / ELECTRONIC DIGITAL ENGINECONTROL UNIT (EDECU) TURBINE GAS TEMP(TGT) BIAS INSP COMPLETED 03DEC12 @6728.8 ACFT HRS
03-Dec-2012 1
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
USAACEH-60-13-ASAM-01 (ANTI-COLLISION LIGHTSPOWER SUPPLY) C/W-PASS-POWER SUPPLYSN: B1802-06077 03DEC12 @ 6728.8 ACFT HRS
03-Dec-2012 2
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
USAACEH-60-13-AMAM-04 (LCF CHANGE 63)COMPLETED 10JAN13 @ 6730 ACFT HRS
10-Jan-2013 1
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
USAACEH-60-13-AMAM-05 (MLG BRAKES) COMPLETED-BOTH PASS-25 JAN 2013 @ 6730.0 ACFT HRS
25-Jan-2013 1
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 45 of 61
USAACETAIL ROTOR BIAS COMPLETED 29 JAN 2013COLOL/DIM. A/DIM. B/DIFFERENCE/BLADESET DEG/BLADE FINAL DEG RED .785 5.122.337 3.1 3.1 YELLOW 4.72 4.404 .312 3.1 3.1BLACK 4.077 4.411 .334 3.1 3.0 BLUE 4.092 -4.404 - .312 - 3.1 - 3.0 PROTRACTOR MR#100967
29-Jan-2013 1
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
USAACET/R CABLE TENSION CHECK COMPLETED 30JAN 2013 @ 6734.0 ACFT HRS - FAILED - MR#87703, TEMP: 22°C L/H: 126 R/H: 130ADJUSTED TO L/H: 140 R/H: 138
30-Jan-2013 1
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
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
USAACET/R CABLE TENSION CHECK COMPLETE,CHECK GOOD, LH:123 RH:122 MR#122358 @12°C MR#112082 04FEB2013 @ 6743.0 ACFTHRS
04-Feb-2013 2
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
USAACEH-60-13-AMAM-06 (CEFS) COMPLETED - CEFSNOT INSTALLED; AMAM-06 NOT APPLICABLE12FEB2013 @ 6748.1 ACFT HRS
12-Feb-2013 1
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
USAACEH-60-13-ASAM-03 (MR SPINDLE ANTI-FLAPASSEMBLIES) COMPLIED WITH 27FEB2013 @6765.1 ACFT HRS
27-Feb-2013 1
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
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
USAACEM/R RIG COMPLETED @ 6765.1 ACFT HRS IAWH-60-13-AMAM-01 ADDENDUM 1: T/R CABLETENSION CK - L/H: 133 R/H: 130 @ 14.3°C T/RBIAS MEASUREMENTS: RED - 0.8 / 4.809 /5.144 / .336 / 3.0; BLK - 1.0 / 4.087 / 4.423 / .336 /3.0; YEL - 0.8 / 4.762 / 5.097 / .335 / 3.1; BLU - 0.9/ 4.109 / 4.448 / .339 / 3.1 NO ADJUSTEMENTSTO PRIMARY SERVO CONTROL ROD BIAS
01-Mar-2013 2
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
USAACEENG ASSY SN: GE-E-306281 - COMPONENTCTS = HR(SN: CAO01300) CTS = 4345 / 22309 /9203 / 11191 - CHIP LIGHT FLICKERED -TROUBLESHOOTING PROC 46 COMP -CLEANED AND INSP CHIP DETECTORS ANDSCREENS REPLACED OIL FILTER IAW TM 1-2840-248-23 WP 0055 PROCEDURE 46
15-Mar-2013 1
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACEH-60-13-ASAM-04 (PLASTIC MEDIA BLAST ANDOXIDE FLAKE RESIDUE) COMPLETED26MAR2013 @ 6807.4 ACFT HRS
26-Mar-2013 1
LOWE AHP, FT.RUCKER, AL.
jessica.l.wendel
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
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 46 of 61
USAACEH-60-13-AMAM-07- ALL H-60 SERIES AICRAFT,LOAD DEMAND SPINDLE (LDS) CABLECLEARANCE C/W @ 6808.9 AIRCRAFTHOURS. ON 29 MAR 2013
01-Apr-2013 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACEH-60-13-ASAM-05 ELECTRIC RESCUE HOISTCOMPLETED 09 APR 2013 AT 6822.4 ACFT.HRS.
09-Apr-2013 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
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
USAACEH-60-13-ASAM-06 (PMI CHECKLIST CHANGES)COMP @ 6876.5 ACFT HRS. (AFS 76)
10-May-2013 1
LOWE AHP, FT.RUCKER, AL.
kathleen.m.jungell
USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-SOF-01 THIS DATE AT 6907.7 ACFT HRS.
31-May-2013 1
LOWE AHP, FT.RUCKER, AL.
janice.m.bruce
USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-11 (MAIN XMSN FILTER BOWLHARDWARE REPLACEMENT) (AFS 594) AT6929.1 ACFT HRS.
08-Jul-2013 1
LOWE AHP, FT.RUCKER, AL.
marilyn.l.jones
USAACEGEN-13-AMAM-04 AN/APN-209 RADARALTIMETER SET COMPONENT TRACKINGCOMPLETED AT 6934.2 ACFT HRS.(AFS 594).
16-Jul-2013 1
LOWE AHP, FT.RUCKER, AL.
marilyn.l.jones
USAACECOMPLETED TAIL ROTOR CABLE TENSIONCHECK: L-140 IN LBS, R-140 IN LBS, 26DEGREES CELCIUS. MR109846
05-Aug-2013 1
LOWE AHP, FT.RUCKER, AL.
vickie.l.meadows
USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-12-ASAM-01 (TAIL ROTOR OUTPUT BEVELGEAR NONDESTRUCTIVE INSPECTION @6939.7 ACFT HRS. T/R G/B S/N A006-03029AND BEVEL GEARSHAFT S/N A320-02502.
12-Aug-2013 1
LOWE AHP, FT.RUCKER, AL.
vickie.l.meadows
USAACEREPLACED DRAG BEAM SN: IA00747, IAW H-60-12-ASAM-02, AT 6940 ACFT HRS. NEW SN:C1397-00201.
13-Aug-2013 1
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
USAACEMEC F170635, AUTHORIZATION GRANTED TOREPAIR RH TAIL STRUT ACCESS OPENINGCRACK IN UPPER FWD CORNER. 6939.7 ACFTHRS.
14-Aug-2013 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEDAGR SERIAL NUMBER IS 214674 @ 6939.7ACFT HRS. IAW PROPERTY ADMINISTATOR @PHASE
19-Aug-2013 1
LOWE AHP, FT.RUCKER, AL.
vickie.l.meadows
USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-01 (TAIL ROTOR OUTPUT BEVEL GEARNONDESTRUCTIVE INSPECTION) @ 6939.7ACFT HRS. T/R G/B IS A006-03029 AND BEVELGEAR IS A320-02502.
20-Aug-2013 1
LOWE AHP, FT.RUCKER, AL.
vickie.l.meadows
USAACEREPLACED L/H DRAG BEAM ASSEMBLY, P/N70250-12057-047 IAW H-60-12-ASAM-02 @6939.7 ACFT HRS
21-Aug-2013 1
LOWE AHP, FT.RUCKER, AL.
vickie.l.meadows
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 47 of 61
USAACEM/R ROTOR RIG C/W. PRIMARY SERVOCONTROL RODS ARE BAISED AS FOLLOWS:FWD ADDTIONAL ADJUSTMENTS 1 FLAT IN.AFT ADDITIONAL ADJUSTMENTS- 1 FLAT OUT.LAT ADDITIONAL ADJUSTMENTS- 3 FLATS IN.@ 6943.7 ACFT HRS.
24-Aug-2013 1
LOWE AHP, FT.RUCKER, AL.
vickie.l.meadows
USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-01 (FLIGHT CONTROL RIGGINGPROCEDURES)@ 6939.7 ACFT HRS.
26-Aug-2013 1
LOWE AHP, FT.RUCKER, AL.
vickie.l.meadows
USAACET/R CABLE TENSION IS L-140 LBS, R-140 LBS@ 26 DEG CELCIUS @ 6939.7 ACFT HRS.
26-Aug-2013 2
LOWE AHP, FT.RUCKER, AL.
vickie.l.meadows
USAACET/R BIAS CHECK COMPLETED AT 6943.7 ACFTHRS. COLOR/DIM A/DIMB/DIFFERENCE/BLADE SET DEG/BLADE FINALDEG RED 4.754 5.063 .309 -0.5 3.0 YELLOW4.715 5.021 .306 -0.1 3.0 BLUE 4.045 4.378 0.3330.0 3.0 BLACK 4.054 4.363 0.309 0.1 3.0
26-Aug-2013 3
LOWE AHP, FT.RUCKER, AL.
vickie.l.meadows
USAACEPMI- PHASE #11 COMPLETED AT 6939.7 ACFTHRS. PMI- PHASE #12 DUE AT 7659.7 ACFTHRS.
28-Aug-2013 1
LOWE AHP, FT.RUCKER, AL.
tony.barnes
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
USAACEH-60-13-AMAM-10 (ULLS-AE LCF CHANGE 64)COMPLETED 07 SEPT 2013 AT 6923.4 ACFT.HRS.
09-Sep-2013 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACET/R CABLE TENSION CHECK COMPLETED,MR#122358 TEMP: 24.5 DEGREES C L/H 135R/H AT 6950.1 ACFT. HRS.
09-Sep-2013 2
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
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
LOCKHEED MARTINOCM/ACE PERFORMED AT 7060.1 ACFT HRSBY TEAM MEMBER QQ.
31-Oct-2013 1
LOWE AHP, FT.RUCKER, AL.
louis.e.sanders
USAACEAWR 1529: ACFT OPERATING IAW AWR 1529,R3 DTD 30OCT13, DUAL AHRS, SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR.
31-Oct-2013 2
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACECOMPLY WITH REQUIREMENTS OF H-60-14-SOF-01(BREEZE EASTERN EXTERNALRESCUE HOIST INSTALLATION) @ 7060.1ACFT HRS
01-Nov-2013 1
LOWE AHP, FT.RUCKER, AL.
felicia.tolver
USAACEAWR 1529: ACFT IS NO LONGER OPERATINGIAW AWR 1529, ALL REVISIONS. ACFTRECONFIGURED FROM DUAL AHRS TOSINGLE AHRS. SEE AWR 1444.
23-Nov-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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 48 of 61
USAACEAWR 1444: ACFT OPERATING IAW AWR 1444,R6 DTD 11JUL13, SINGLE AHRS
23-Nov-2013 2
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEH-60-14-ASAM-02 (HEALTH USAGEMONITORING SYSTEM (HUMS)ACCELEROMETERS) C/W 23 NOV 13 AT 7091.7ACFT. HRS. N/A THIS ACFT.
25-Nov-2013 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACEAWR 1251: ACFT OPERATING IAW AWR 1251,R8 DTD 26NOV13, EYEBOLTS ON BIFILARARMS, SUPERSEDING ALL PRIOR VERSIONSOF THIS AWR.
25-Nov-2013 2
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-15 (CRASHWORTHY EXTERNAL FUELSYSTEM (CEFS) RIGHT HAND FUEL CELLCOVER PLATE) @ 7122.2 ACFT HRS. CEFSNOT INSTALLED ON THIS A/C
16-Dec-2013 1
LOWE AHP, FT.RUCKER, AL.
tony.barnes
USAACEH-60-14-AMAM-03 (DISCREPANT CONNECTINGLINKS) C/W 30 DEC 13 AT 7124.1 ACFT HRS,FOUND N/A THIS ACFT.
30-Dec-2013 1
LOWE AHP, FT.RUCKER, AL.
marissa.w.watkins
USAACEH-60-14-ASAM-03 (ENGINE INLET BARRIERFILTER(EIBF) BRACKET REMOVAL) C/W 13JAN 2014 AT 7128.1 ACFT. HRS.
13-Jan-2014 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACET/R BIAS CHECK COMPLETED 19 JAN 14 AT7138.0 ACFT HRS: DIM A DIM B DIFFERENCEFINAL (DEG) RED 4.726 5.013 0.287 3.0 BLACK4.022 4.321 0.299 3.0 YELLOW 4.675 4.98 0.3053.0 BLUE 4.025 4.322 0.297 3.0 YELLOW 4.6754.98 0.305 3.0 BLUE 4.025 4.322 0.297 3.0
21-Jan-2014 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACET/R ROTOR BIAS CHECK COMPLETED 30 JAN14 AT 7147.0 ACFT HRS. DIM A DIM BDIFFERENCE FINAL (DEG) RED 4.742 5.0750.333 3.0 BLACK 4.019 4.35 0.331 3.0 YELLOW4.695 4.997 0.302 3.0 BLUE 4.028 4.336 0.308 3.0
31-Jan-2014 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACEH-60-14-AMAM-08 (AN/ASC-15E CIRCUITBREAKER PROTECTION) C/W 07 MAR 14 AT7182.3 ACFT. HRS.
08-Mar-2014 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
DCR RASM-COCM/ACE PERFORMED AT 7182.3 AIRCRAFTHOURS BY TEAM MEMBERS P AND QQ
17-Mar-2014 1
LOWE AHP, FT.RUCKER, AL.
jacob.a.weikart
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 LIGITIMATE CODE FILECHANGE 65 REQUIREMENTS COMPLETED AT7182.3 ACFT HRS.
05-Apr-2014 1
LOWE AHP, FT.RUCKER, AL.
vickie.l.meadows
USAACET/R CABLE TENSION CHECK COMPLETED 11JUN 14, L/H: 155, R/H: 155, TEMP: 28.7C.
13-Apr-2014 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 49 of 61
USAACEH-60-14-AMAM-10 HONTEK COATED MAINROTOR BLADE REMOVAL COMPLETED AT7187.7 ACFT. HRS. "N/A TO THIS AIRCRAFT.
15-Apr-2014 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACEH-60-14-AMAM-12 (MAIN ROTOR SPINDLE NUTRETIREMENT LIFE EXTENTION) C/W 23 APR 14AT 7218.7 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 7219.7 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
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 7291.8 ACFTHRS (MWO NOT APPLIED)
28-May-2014 1
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
USAACEM/R RIG CHECK COMPLETED 11 JUN 14, FWDADDITIONAL ADJUSTMENTS: 1/2 TURNSHORTEN, AFT ADDITIONAL ADJUSTMENTS:1/2 TURN LENGTHEN, LAT ADDITIONALADJUSTMENTS: NEUTRAL.
11-Jun-2014 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACET/R CABLE TENSION CHECK COMPLETED 11JUN 2014, L/H: 155, R/H: 155, TEMP: 28.7C.
11-Jun-2014 2
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACET/R BIAS COMPLETED 11 JUN 14. BLADE DIMA DIM B DIFF FINAL DEG. RED .3 4.743 5.065 3BLACK .3 4.022 4.341 3 YELLOW.7 4.675 4.981 3BLUE.64.0314.3563
13-Jun-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.
18-Jun-2014 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEPER ACLC, MEC F72415, DTD 04MAR08 NEEDSTO BE RECORDED ON THIS 2408-15. THIS MECNO LONGER APPLIES TO THIS AIRFRAME ASMAIN MOD A265-00600 WAS REMOVED17JUL08.
18-Jun-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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 50 of 61
USAACEH-60-14-SOF-03, DISCREPANT SELF-LOCKINGNUTS, C/W AT 7316.8 ACFT HRS. PASSED. AFSINSP. 151
25-Jun-2014 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACEH-60-14-AMAM-16, ATTITUDE HEADINGREFERENCE UNIT 2410 TRACKINGCOMPLETED ON 22 JUL 14 AT 7368.4 ACFT.HRS.
16-Jul-2014 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
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 1
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
USAACEH-60-14-ASAM-09 (ENGINE OUTPUT SHAFT)C/W 01 AUG 14 AT 7390.7 ACFT. HRS.
01-Aug-2014 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACET/R CABLE TENSION CHECK COMPLETED 13AUG 14 AT 7407.8 ACFT. HRS. I/A/W EM 0013WP 1747 AND PERFORMED ADJUSTMENTSI/A/W EM 0013 WP 1156 TENSIONMETER MR#126782 THERMOMETER MR # 122082 (CABLESSET AT L/H: 172, R/H: 172 @ 31 DEG C.)
15-Aug-2014 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACEH-60-14-SOF-04 (OPERATORS ANDCREWMEMBERS CHECKLIST) C/W 27 AUG 14AT 7416.1 ACFRT. HRS.
27-Aug-2014 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACET/R CABLE TENSION CK COMPLETED 05 OCT14, L/H: 130, R/H 130 @ 10.5 DEG C.
07-Oct-2014 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACET/R CABLE TENSION CHECK COMPLETED 08OCT 14 I/A/W EM 0013 WP 1747, FAILED, MR#109407, TEMP: 19.2 DEG C, L/H: 139, R/H: 139.
10-Oct-2014 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACET/R CABLE TENSION CHECK COMPLETEDPASSED L/H 142, R/H 142 @ 20.7 DEG CELMR#126782 MR#118174
16-Oct-2014 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
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
USAACEC/W H-60-15-SOF-01 (OIL COOLER FAN AXIALBEARING) ON 28OCT14 @ 7441.0 ACFT. HRS.
29-Oct-2014 1
LOWE AHP, FT.RUCKER, AL.
frances.j.grace
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
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 51 of 61
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
USAACEREQUIREMENTS OF H-60-14-AMAM-19 (ULLS-A(E), LCF, CHANGE 66) C/W @ 7460.4 ACFT HRS.
08-Nov-2014 1
LOWE AHP, FT.RUCKER, AL.
frances.j.grace
USAACEH-60-15-ASAM-01 - C/W H-60-15-ASAM-01, LEDCAUTION ADVISORY PANE @ 7486.5 ACFTHRS
20-Nov-2014 1
LOWE AHP, FT.RUCKER, AL.
frances.j.grace
USAACEACFT OPERATING IAW AWR 1251, R10 DTD26NOV14, EYEBOLTS, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.
25-Nov-2014 1
LOWE AHP, FT.RUCKER, AL.
anthony.s.speigner
USAACEH-60-15-AMAM-05 - C/W REQUIREMENTS OF H-60-15-AMAM-05, AHRS EMERGENCYPROCEDURES @ 7533.9 ACFT HRS.
12-Dec-2014 1
LOWE AHP, FT.RUCKER, AL.
frances.j.grace
USAACEMEO A6116 – AIRCRAFT OPERATING UNDERMEO A6116 INSTALLATION OF FUEL FLAGFOR E/UH-60 FLEET AT FT. RUCKER, AL.
27-Jan-2015 1
LOWE AHP, FT.RUCKER, AL.
frances.j.grace
USAACEMEO A6116 – CORRECTIVE ENTRY – DELAYEDENTRY - AIRCRAFT OPERATING UNDER MEOA6116 INSTALLATION OF FUEL FLAG FORE/UH-60 FLEET AT FT. RUCKER, AL. CURRENTACFT HRS: 7559.5
27-Jan-2015 2
LOWE AHP, FT.RUCKER, AL.
frances.j.grace
USAACEACFT OPERATING IAW AWR 1738, R2 DTD23JAN15, AN/APX-118 CXP, SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR ANDISAQ 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
USAACEACFT IS NO LONGER OPERATING IAW AWR1514, ALL VERSIONS. ACFT IS OPERATINGIAW AWR 1753, R5 DTD 30JAN15, DGNSAN/ASN-128B/D, SUPERSEDING ALL PRIORVERSIONS OF 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
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 52 of 61
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 REQUIREMENTS OF H-60-15-ASAM-03 (TROOP/GUNNER SEAT ENERGYATTENUATORS) AT 7635.1 ACFT HRS. H-60-15-ASAM-03 NOT APPLICABLE SINCETROOP/GUNNER SEAT NOT INSTALLED(AFS765).
13-Apr-2015 1
LOWE AHP, FT.RUCKER, AL.
bryan.w.hollis
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
USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-15-AMAM-10 (AV-DEC GASKET INSPECTION)AT 7653.3 ACFT HRS.
27-May-2015 1
LOWE AHP, FT.RUCKER, AL.
bryan.w.hollis
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
USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-15-AMAM-11 (MODE-S TRANSPONDERADDRESS REVIEW) AT 7653.3 ACFT HRS. APX-100 TRANSPONDER INSTALLED, H-60-15-AMAM-11 NOT APPLICABLE (AFS219).
28-May-2015 2
LOWE AHP, FT.RUCKER, AL.
bryan.w.hollis
USAACETRANS IMPD BYPASS BUTTON POPPED(XMSN S/N: A265-01063, W/TTSN: 4083.3 HRS)AT 7653.3 ACFT ON ACFT 8524465. REPLACEDM/MOD STAGE 1 AND 2 OF FILTER BOWL IAWEM0013 WP626 AT 7653.3 ACFT HRS.
02-Jun-2015 1
LOWE AHP, FT.RUCKER, AL.
bryan.w.hollis
USAACEFACFT 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
USAACEACFT OPERATING IAW AWR 1681, R5 DTD22JUN15, EH DE-MOD, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR AND AWR'S927 AND 890.
23-Jun-2015 2
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEM/R RIG CHECK COMPLETED AT 7653.3 ACFTHRS. ADJUSTMENTS MADE TO PRIMARYSERVO CONTROL ROD BIAS: FWD - 1.5 FLATS,AFT - 1.5 FLATS, LAT - NO ADJUSTMENTNEEDED.
05-Jul-2015 1
LOWE AHP, FT.RUCKER, AL.
bryan.w.hollis
USAACEH-60-15-AMAM-14 LEGITIMATE CODE FILE(LCF) CHANGE 67 REQUIREMENTS C/W AT7654.8
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
DCR RASM-COCM/ACE PERFORMED AT 7655.8 AIRCRAFTHOURS BY TEAM MEMBER P
02-Sep-2015 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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 53 of 61
USAACEH-60-15-SOF-02 FAST ROPEINSERTION/EXTRACTION SYSTEM (FRIES)RELEASE CABLE C/W ON 24 SEPT 15.AIRCRAFT HOURS 7655.8 N/A TO THISAIRCRAFT
25-Sep-2015 1
LOWE AHP, FT.RUCKER, AL.
nacona.l.hamilton
USAACEH-60-15AMAM-18 MEDVAC CAROUSEL C/W ON3OCT15
14-Oct-2015 1
LOWE AHP, FT.RUCKER, AL.
tony.a.lane
USAACEMEC # F304460 FUEL CHECKVALVES:.AUTHORIZATION GRANTED IAWMEC F304460 TO PERFORM THE FOLLOWING:1. INCREASE PRESSURE FROM 50 PSICALLED OUT UP TO BUT NOT EXCEEDING 60PSI. 2. REPORT BACK TO AED LE WHETHERTHE INCREASE IN PRESSURE WORKED ORFAILED. ACFT HRS.7658.6.
14-Oct-2015 2
LOWE AHP, FT.RUCKER, AL.
marilyn.l.jones
USAACEACFT OPERATING IAW AWR 1965 R1, DATED16 SEPT 15 (APPLE IPAD DEVICES)SUPERSEDING ALL PRIOR REVISIONS
14-Oct-2015 3
LOWE AHP, FT.RUCKER, AL.
nacona.l.hamilton
USAACEH-60-16-AMAM-01 (EIBF FRAMES) C/W ON 27OCT 15 AIRCRAFT HOURS 7658.6 N/A TO THISAIRCRAFT
27-Oct-2015 1
LOWE AHP, FT.RUCKER, AL.
nacona.l.hamilton
USAACEH-60-16-ASAM-01- INBOARD RETENTIONPLATE TORQUE CHECKS, COMPLIED WITH AT7659.6 ACFT HRS.
17-Nov-2015 1
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
USAACEH-60-16-AMAM-03- PERSONNEL LOCATOR SETREMOVAL, COMPLIED WITH AT 7659.6 ACFTHRS. NOT INSTALLED ON THIS ACFT.
24-Nov-2015 1
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
USAACEACFT OPERATING IAW AWR 1251, R12 DTD30NOV15, EYEBOLTS ON BIFILAR,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.
01-Dec-2015 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEMEC F306331, 7659.6 ACFT HRS,AUTHORIZATION GRANTED TO REPAIR PICYCLIC STICK YOKE HOUSING IAW DMWR 1-1680-323 DTD 30DEC11 PG 3-13, PARA 3-12.REMOVE MINIMAL MATERIAL NOT TO EXCEEDEXISTING DEPTH.
02-Dec-2015 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEMEC F306333, 7659.6 ACFT HRS,AUTHORIZATION GRANTED TO REPAIR CPCYCLIC STICK YOKE HOUSING IAW DMWR 1-1680-323 DTD 30DEC11 PG 3-13, PARA 3-12.REMOVE MINIMAL MATERIAL NOT TO EXCEEDEXISTING DEPTH.
02-Dec-2015 2
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEMEC F306446, 7659.6 ACFT HRS,AUTHORIZATION GRANTED TO REPAIR A 6 X 6I NCH VOID IN OIL COOLER DOOR IAW TM 1-1500-204-23-11 'SANDWICH CORE REPAIR(HONEYCOMB PLUG)' REFERENCING TABLE 7-1 USING THE PASTE ADHESIVE METHODPARA 7-5D.
02-Dec-2015 3
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 54 of 61
USAACEMEC F306451, 7659.6 ACFT HRS,AUTHORIZATION GRANTED TO REPAIR A 12 X14 INCH VOID IN TRANSITION COWL IAW TM 1-1500-204-23-11 'SANDWICH CORE REPAIR(HONEYCOMB PLUG)' REFERENCING TABLE 7-1 USING THE PASTE ADHESIVE METHODPARA 7-5D.
02-Dec-2015 4
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEMEC F306583, AUTHORIZATION GRANTED TOREPLACE THE BUSHING IAW DMWR 1-1615-377 WP 0021 DATED 24 APR 2014(REPLACEMENT OF SPINDLE DAMPERATTAHCMENT BUSHINGS) WITH THEEXCEPTION THAT IF THE BORES IN THESPINDLE LINER ASSEMBLY ARE DAMAGEDOR OUT OF TOLERANCES GIVEN IN THEDMWR THE MACHINIST WILL NOT MACHINEAND ROLLER BURNISH THESE BORES ANDTHE SHOP WILL NRTS THE SPINDLE LINERASSEMBLY. IF THE BORES HAVE BEENMACHINED TO AN OVERSIZE DIMENSIONGIVEN IN TABLE 2, THE SHOP SHALL CEASEWORK AND CONTACT THE UNDERSIGNEDFOR FURTHER DISPOSITION.
07-Dec-2015 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEENTRY #1 DTD 07DEC15 SHOULD HAVEINCLUDED MR SPINDLE SN D001-11514
07-Dec-2015 2
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEMEC F306860, 7659.6 ACFT HRS, DURING FUELCELL MAINTENANCE, UNABLE TO PURGEFUEL FEED SYSTEM DUE TO PRESSURERELIEF VALVE FAILING TO OPEN ON THE #1MAIN FUEL CHECK VALVE AT 50 PSI. VALVEWAS REMOVED AND CONNECTED DIRECTLYTO THE FUEL INTEGRITY TESTER ANDPRESSURE RELIEF VALVE OPENED JUSTBELOW 50 PSI. AUTHORIZATION GRANTED TORE-INSTALL CHECK VALVE AND RETEST THEPRESSURE RELIEF VALVE PER EM0013 TM 1-1520-BLACKHAWK. IF THE VALVE PASSESTHE TEST PER THE TM AFTER RE-INSTALLATION, LEAVE VALVE IN-SERVICE. IFTHE VALVE FAILS THE ON AIRCRAFT TEST,CONTACT THE UNDERSIGNED.
14-Dec-2015 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACEMEC F307262, AUTHORIZATION TO INSTALLOIL COOLER FAN (FAN AXIAL SN: D51201513)AT 7659.6 ACFT HRS. OIL COOLER MOUNTINSTALLATION WAS ADJUSTED USINGPEELABLE SHIMS BETWEEN MOUNTING FACEAND OIL COOLER MOUNTING FLANGES. OILCOOLER MUST BE RE-EVALUATED AT NEXT720 PHASE INSPECTION , IAW MEC.
22-Dec-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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 55 of 61
USAACEMAIN ROTOR RIGGING CHECK COMPLETEDAT 7659.6 ACFT HRS. BLADES ON. CONTROLPOSITION: LOW COLL ANGLE 90 DEG R 180DEG FWD 270 DEG L0 DEG AFT TOTAL DEGAVG DEG COLL. RANGE 7.7 -2.1 -10.0 -0.2 -4.6 -1.15 HIGH COLL ANGLE: 90 DEG R 180 DEGFWD 270 DEG L 0 DEG AFT TOTAL DEG AVGDEG COLL. RANGE 18.5 11.1 11.0 17.9 58.514.625 15.775 FWD CYCLIC ANGLE: 90 DEG R180 DEG FWD 270 DEG L 0 DEG AFT TOTALDEG AVG DEG COLL. RANGE -2.9 31.1 34.0AFT CYCLE ANGLE:90 DEG R 180 DEG FWD270 DEG L 0 DEG AFT TOTAL DEG AVG DEGCOLL. RANGE 24.8 5.1 19.7 LEFT CYCLEANGLE: 90 DEG R 180 DEG FWD 270 DEG L 0DEG AFT TOTAL DEG AVG DEG COLL. RANGE-9.1 6.0 15.1 RIGHT CYCLIC ANGLE: 90 DEG R180 DEG FWD 270 DEG L 0 DEG AFT TOTALDEG AVG DEG COLL. RANGE 6.3 -7.9 14.2
23-Dec-2015 1
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
USAACEMAIN ROTOR RIGGING CHECK COMPLETEDAT 7659.6 ACFT HRS. PRIMARY SERVOCONTROL ROD BIAS: FWD: NO CHANGE, AFT:NO CHANGE, LAT: LENGTHEN 1 FLAT.
23-Dec-2015 2
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
USAACETAIL ROTOR BIAS CHECK COMPLETED AT7659.6 ACFT HRS. NO ADJUSTMENTS WEREMADE. COLOR 1ST DEG 2ND DEG FINAL DEGRED 2.8 2.8 2.8 BLACK2.82.82.8 YELLOW2.9 2.92.9 BLUE 3.0 3.0 3.0
28-Dec-2015 1
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
USAACEACFT OPERATING IAW AWR 1913 R1 DATED06 NOV 2015 (ACN ELECTRONIC LOGBOOK)
04-Jan-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACETAIL ROTOR CABLE TENSION CHECKCOMPLETED AT 7659.6 ACFT HRS. L/H CABLE162 LBS, R/H CABLE 160 LBS,TENSIONOMETER MR # 126115 AT 21.5DEGREES CELCIUS, THERMOMETERMR#118177.
04-Jan-2016 2
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
USAACEACFT OPERATING IAW AWR 1738, R4 DATED28DEC15 (AN/APX-118 CXP). SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR ANDISAQ 116.
05-Jan-2016 1
LOWE AHP, FT.RUCKER, AL.
chelsey.p.phillips
USAACEACFT NO LONGER OPERATING IAW AWR 1648(MAGNUS LAPTOP COMPUTER) AT ACFT HRS:7659.6 ACFT HRS.
05-Jan-2016 2
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
USAACEH-60-16-ASAM-02- DEFECTIVE FUEL HOSES,COMPLIED WITH AT 7659.6 ACFT HRS.PASSED.
06-Jan-2016 1
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
USAACE720 HOUR PHASE #12 COMPLETED AT 7659.6ACFT HRS, THE NEXT 720 HOUR INSPECTION(#13) IS DUE AT 8379.6 ACFT HRS.
06-Jan-2016 2
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
USAACEACFT OPERATING IAW AWR 1913, R1, DATED06 NOV 15 (ACN LOGBOOK). AT 7659.6 ACFTHRS.
07-Jan-2016 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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 56 of 61
USAACEACFT OPERATING IN ACCORDANCE WITHMEO A5755 A, USE OF SOUNDPROOFING ONEH-60 FLEET AT FT. RUCKER.SOUNDPROOFING INSTALLED AT 7659.6 ACFTHRS.
07-Jan-2016 2
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
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 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACECOMPLETED CABLE TENSION CHECK, AT7660.1 ACFT HRS, LH:150 LBS, RH: 150 LBS,AT 23.4 DEGRESS C, TENSIONMETER MR#126115 , THEROMEMTER MR #118177
15-Jan-2016 1
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
USAACETAIL ROTOR CABLE TENSION CHECKCOMPLETED AT 7661.6 ACFT HRS. R/H CABLE160 LBS L/H CABLE 162 LBS TENSIONOMETERSN: 126115 AT 21.8 CELCIUS THERMOMETERSN: 118177
16-Jan-2016 1
LOWE AHP, FT.RUCKER, AL.
christina.l.negron
USAACET/R CABLE TENSION CHECK COMPLETED AT7669.0 ACFT. HRS. R/H 150, L/H 150 @ 20.5DEG C. MR# 131652 & 118174. NOADJUSTMENTS MADE.
01-Feb-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
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
USAACET/R CABLE TENSION CHECK COMPLETED AT7678.1 ACFT. HRS. ADJUSTED TO L/H 105, R/H105 @ 6.5 DEG. C
05-Feb-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACET/R CABLE TENSION CHECK COMPLETED AT7687.7 ACFT. HRS. FAILED. L/H 105, R/H 105, @1.2 DEG C. MR#131652
10-Feb-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
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
USAACET/R CABLE TENSION CHECK COMPLETED AT7696.7 ACFT. HRS. FAILED CHECK. NOTWITHIN 5 LBS WHEN COMPENSATED FORTEMP. NO ADJUSTMENTS REQUIRED. NEWREADINGS WERE WITHIN RANGE. READINGSWERE L/H 125, R/H 125 AT 18 DEG. C. M/RTHERMOMETER 118174, TENSIONOMETER131652.(LW012211)
23-Feb-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACET/R CABLE TENSION CHECK COMPLETED AT7706.3 ACFT. HRS. CHECK FAILED AT L/H 120,R/H 120 @ 13 DEG. C. TENSIONOMETER MR#131652, THERMOMETER MR# 118174.(KC021671)
25-Feb-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACEMEC F307262A, 7659.6 ACFT HRS, AXIAL FANSN D512-01513, AUTHORIZATION GRANTEDTO USE SHIM PN 70652-02151-102 NIIN 01-123-0379 SHIM IN LIEU OF SS52J0250X0750 SHIMSTOCK.
26-Feb-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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 57 of 61
USAACET/R CABLE TENSION CHECK COMPLETED AT7715.6 ACFT. HRS. R/H 123, L/H 123 @ 11 DEG.C.
02-Mar-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACEREPLACED NUMBER TWO CROSSFEEDVALVE ON 09 MAR 16 AT 7725.0 ACFT. HRS.
09-Mar-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
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
USAACECOMPLIED WITH H-60-16-AMAM-06, T-CLIPINSTALLATION ON 25 APR 2016 AT 7828.3ACFT. HRS. N/A THIS ACFT.
25-Apr-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACEACFT OPERATING IAW AWR 1800, R5 DTD 27APR 16, SINGLE EDM AND/OR BFT,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR AND AWR'S 1284, 1347, 1414 AND 1639.
16-May-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
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 AWR1505, 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 GEN-16-AMAM-04,TRANSPONDER BATTERY REPLACEMENT ON04 JUN 2016 AT 7952.6 ACFT. HRS.(NOT INSTL)
04-Jun-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACECOMPLIED WITH REQUIREMENTS OF H-60-16-AMAM-09, ULLS-A(E) COMPONENTSDUPLICATION COMPLETED ON 21 JUN 16 AT7970.0 ACFT. HRS.
21-Jun-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACECOMPLIED WITH REQUIREMENTS OF H-60-16-SOF-01, UPPER CABIN (STA) 379 FRAMECRACKING ON 22 JUN 16 AT 7973.2 ACFT HRS.
22-Jun-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACE48 MONTH 2408-18 INSPECTION A670, CABINTUB INSPECTION COMPLETED ON 27 JUN2016 AT 7984.0 ACFT. HRS.
27-Jun-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACET/R RIGGING CHECK COMPLETED ON 24 JUL2016 AT 8022.1 ACFT. HRS. RED T/R BLADEBIAS 3.0 DEGREES, YELLOW T/R BLADE BIAS3.0 DEGREES, BLACK T/R BLADE BIAS 2.9DEGREES, BLUE T/R BLADE BIAS 3.1DEGREES. M/R # 100893.
24-Jul-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
URS RASM-COCM/ACE PERFORMED AT 8030.6 AIRCRAFTHOURS BY TEAM MEMBERS P AND WW
08-Aug-2016 1
LOWE AHP, FT.RUCKER, AL.
jacob.a.weikart
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
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 58 of 61
USAACECOMPLIED WITH H-60-16-SOF-02, RESCUEHOIST OPERATIONAL RESTRICTIONS ON 15AUG 2016 AT 8035.1 ACFT. HRS.
15-Aug-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACECOMPLIED WITH H-60-ASAM-06, IMPROVEDT/R QUADRANT SUPPORT ON 23 AUG 16 AT8055.4 ACFT. HRS.. FAILED, NOT INSTALLED.
23-Aug-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACECORRECTIVE ENTRY: COMPLIED WITH H-60-16-ASAM-06, IMPROVED T/R QUADRANTSUPPORT ON 23 AUG 16 AT 8055.4 ACFT.HRS. FAILED. NOT INSTL.
23-Aug-2016 2
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACET/R RIG CHECK CHECK COMPLETED AT 8067ACFT. HRS. AVA M/R# 81252. RED T/R BLADEBIAS ANGLES MEAS. 3.0 / 20.6 M/R 127251,YELLOW T/R BLADE BIAS ANGLES MEAS. 3.0 /20.4 M/R 127251, BLACK T/R BLADE BIASANGLES MEAS. 3.0 / 20.4 M/R 127251, BLUET/R BLADE BIAS ANGLES MEAS. 3.0 / 20.4 M/R127251.
27-Aug-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACEH-60-16-AMAM-10, ULLS-A-(E) PHASE LCFUPDATE COMPLETED ON 04 SEP 16 AT 8070.5ACFT HRS.
04-Sep-2016 1
LOWE AHP, FT.RUCKER, AL.
olivia.d.williams
USAACEMEC F317139, 8075.9 ACFT. HRS., MAINTRANSMISSION S/N A26501063,AUTHORIZATION TO COMPLETEPROCEDURES IN BLACKHAWK NEWSLETTER, ISSUE 44 MAY/JUNE 2000 TODETERMINE XX ADDITIONAL QUARTS OF OIL(NO MORE THAN 3) TO STOP FLUCTUATION.AUTHORIZED BY JOHN DAVID JENKINS ON 09SEP 2016.
13-Sep-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACELATE CORRECTIVE ENTRY: MAIN MOD FILTERBUTTON POPPED ON TRANSMISSION S/NA265-01063 ON 23 AUG 2016 AT 8055.4 ACFT.HRS. WITH 4485 TSN. REPLACED MAINTRANSMISSION OIL FILTER ELEMENT ANDSERVICEABILITY INSPECTION C/W IAWEM0013 & WP#0626 00
19-Sep-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACEACFT OPERATING IAW AWR 1693, R3 DTD28JAN16, RESA, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.
19-Sep-2016 2
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
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 F317139A, 8075.9 ACFT HRS, XMSN SNA265-01063, TSN 4506, 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
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 59 of 61
USAACECOMPLIED WITH REQUIREMENTS OF H-60-17-ASAM-01, ULLS-A(E) CADS MODULE ON 06OCT 2016 AT 8077.0 ACFT. HRS.
06-Oct-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACEMEC F317139B, XMSN A265-01063, TSN 4506,TWO QUARTS OF OIL ADDED PER THEATTACHED TROUBLESHOOTING PROCEDURE(ADDENDUM A) DID NOT FULLY ALLEVIATETHE FLUCTUATION. MAINTENANCE HASREQUESTED TO ADD AN ADDITIONAL QUARTOIL FOR A TOTAL OF 3 QUARTS.AUTHORIZATION GRANTED TO ADDADDITIONAL QUART OF OIL, FOR A TOTAL OF3 QUARTS. CONTINUE WITHTROUBLESHOOTING PROCEDURE STEPSAFTER ADDITION OF OIL.
06-Oct-2016 2
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
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
USAACEACFT OPERATING IAW AWR 1455, R6 DTD14OCT16, BATTELLE CAP, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR AND ISAQ123.
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 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 REQUIREMENTS OF H-60-17-AMAM-01, LCF CHANGE 68 ON 20 DEC 2016.
20-Dec-2016 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACECOMPLIED WITH REQUIREMENTS OF H-60-17-SOF-01, RESCUE HOIST EMERGENCYPROCEDURES CHANGES ON 20 DEC 2016 AT8139.9 ACFT. HRS.
20-Dec-2016 2
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACECOMPLIED WITH REQUIREMENTS OF H-60-17-ASAM-04, AIRFRAME STRUCTURAL PARTS ON06 JAN 2017 AT 8139.9 ACFT. HRS.
06-Jan-2017 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 60 of 61
USAACET/R BIAS MEASUREMENTS ARE AS FOLLOWS:RED SET BIAS (MAINT) 3.0, VERIFY BIAS (QA)3.0, COLLECTIVE FULL UP PEDAL FULL LEFT(18.5 DEG MIN) 20.5, BLACK SET BIAS (MAINT)3.0, VERIFY BIAS (QA) 3.0, COLLECTIVE FULLUP PEDAL FULL LEFT (18.5 DEG MIN) 20.5,YELLOW SET BIAS (MAINT) 3.0, VERIFY BIAS(QA) 3.1, COLLECTIVE FULL UP PEDAL FULLLEFT (18.5 DEG MIN) 20.6, BLUE SET BIAS(MAINT) 3.0, VERIFY BIAS (QA) 3.0,COLLECTIVE FULL UP PEDAL FULL LEFT (18.5DEG MIN) 20.4.
04-Mar-2017 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACET/R CABLE TENSION CHECK COMPLETED ON04 MAR 2017 @ 8170.3 ACFT. HRS. L/H 161, R/H160 @ 70.2 DEG F. TENSIOMETER MR# 131652,THERMOMETER MR# 127737.
04-Mar-2017 2
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
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 2
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACECOMPLIED WITH H-60-17-AMAM-07, EXTERNALMOUNTED RESCUE HOIST (EMRH) ARMADAPTOR CORROSION CONTROL ON 24 MAR2017 AT 8208.1 ACFT. HRS. EMRH NOTINSTALLED.
24-Mar-2017 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
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
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
MAIN ROTOR RIG CHECK #1 (RED BLADEPOSITION) COMPLETED ON 11 MAY 2017.LOWCOLLECTIVE ANGLE: 90 DEG R, 7.93, 180 DEGFWD, -2.84, 270 DEG L, -10.89, 0 DEG AFT, 0.65,TOTAL DEG, -5.15, AVG DEG -1.2875. HIGHCOLLECTIVE ANGLE: 90 DEG R, 19.6,180 DEGFWD, 10.8, 270 DEG L , 9.25, 0 DEG AFT, 18,TOTAL DEG 57.65, AVG DEG , 14.4125. FWDCYCLIC ANGLE: 90 DEG R, -2.85, 270 DEG L,30.5, TOTAL DEG, 33.35, AFT CYCLE ANGLE:90 DEG R, 24.5, 270 DEG L,4.22, TOTAL DEG20.28, LEFT CYCLE ANGLE: 180 DEG FWD,9.54,0 DEG AFT, 5.55, TOTAL DEG. 15.09, RIGHTCYCLIC ANGLE: 180 DEG FWD, 5.86, 0 DEGAFT, 8.34, TOTAL DEG, 14.2.
11-May-2017 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
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 8524465HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL
Page 61 of 61
USAACEMEC F326174, 8244.7 ACFT HRS, LEFT SPLICESTRAP DOUBLER CRACKED STA 379 BL 45WL 206. CRACK STARTS IN RADIUS ANDPROGRESSES UNDERNEATH LOWER CARGODOOR TRACK FAIRING. AUTHORIZATIONGRANTED TO REPAIR IAW DMWR 1-1520-237-1DATED 9 SEP 2013 WP 0120 WITHEXCEPTIONS AS STATED IN MEC.
19-May-2017 1
LOWE AHP, FT.RUCKER, AL.
dean.a.keirn
USAACECOMPLIED WITH REQUIREMENTS OF H-60-17-ASAM-10, IMMSS HINGE PINS ON 20 JUN 2017AT 8278.9 ACFT. HRS. IMMSS NOT INSTALLED.
20-Jun-2017 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACECOMPLIED WITH REQUIREMENTS OF H-60-17-ASAM-12, IMMSS RETROFIT KIT, ON 31 JUL2017 AT 8300.7 ACFT. HRS.
31-Jul-2017 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
USAACECOMPLIED WITH REQUIREMENTS OF H-60-17-AMAM-12, AIRWORTHINESS RELEASEUPDATE ON 22 AUG 2017 AT 8340.5 ACFT.HRS.
22-Aug-2017 1
LOWE AHP, FT.RUCKER, AL.
brian.k.dow
SCIENCE ANDENGINEERINGSERVICES, LLC
ACFT TRANSFERRED TO BEST PROGRAM ON11-SEP-2017 AT 8345.2 ACFT HRS FROM LOWEFIELD, FT. RUCKER, AL. DATA PLATEINSTALLED
11-Sep-2017 1
HUNTSVILLE
robert.e.bridges
SCIENCE ANDENGINEERINGSERVICES, LLC
H-60-16-AMAM-07 (TAIL ROTOR SERVOSAFETY CABLE) NOT COMPLIED WITH
14-Sep-2017 1
HUNTSVILLE
robert.e.bridges
SCIENCE ANDENGINEERINGSERVICES, LLC
H-60-17-ASAM-11 (FUEL HOSE BORESCOPEINSPECTION) NOT COMPLIED WITH
14-Sep-2017 2
HUNTSVILLE
robert.e.bridges
SCIENCE ANDENGINEERINGSERVICES, LLC
H-60-17-AMAM-11 (ESM-2 PROGRAMIMPLEMENTATION) NOT COMPLIED WITH
14-Sep-2017 3
HUNTSVILLE
robert.e.bridges
SCIENCE ANDENGINEERINGSERVICES, LLC
H-60-17-ASAM-14 NOT COMPLIED WITH 03-Oct-2017 1
HUNTSVILLE
james.m.aldrich
SCIENCE ANDENGINEERINGSERVICES, LLC
H-60-17-AMAM-13 NOT COMPLIED WITH 03-Oct-2017 2
HUNTSVILLE
james.m.aldrich
SCIENCE ANDENGINEERINGSERVICES, LLC
H-60-17-ASAM-15 NOT COMPLIED WITH 03-Oct-2017 3
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.
8524465HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
Page 1 of 10
a b c d e f g
100HR15-Aug-1996 #1 ENGINE 0.450.000.00692.7
100HR15-Aug-1996 #2 ENGINE 0.040.000.00692.7
100HR15-Aug-1996 OIL COOLER 0.330.110.00692.7
100HR06-Aug-1997 #1 ENGINE 0.070.000.00703.0
100HR06-Aug-1997 #2 ENGINE 0.380.000.00703.0
100HR06-Aug-1997 OIL COOLER 0.050.300.00703.0
POST PMS II27-Aug-1998 #1 ENGINE 0.310.000.00988.6
POST PMS II27-Aug-1998 #2 ENGINE 0.330.000.00988.6
POST PMS II27-Aug-1998 OIL COOLER 0.200.080.00988.6
100HR09-Aug-1999 #1 ENGINE 0.230.000.001,085.9
100HR09-Aug-1999 #2 ENGINE 0.310.000.001,085.9
100HR09-Aug-1999 OIL COOLER 0.160.170.001,085.9
M/M REPLACE01-Mar-2000 #1 ENGINE 0.100.000.001,133.0
M/M REPLACE01-Mar-2000 #2 ENGINE 0.040.000.001,133.0
M/M REPLACE01-Mar-2000 OIL COOLER 0.500.630.001,133.0
100HR20-Jul-2000 #1 ENGINE 0.050.000.001,186.5
100HR20-Jul-2000 #2 ENGINE 0.300.000.001,186.5
100HR20-Jul-2000 OIL COOLER 0.640.300.001,186.5
100HR20-Jul-2000 TAIL ROTOR 0.000.120.001,186.5
100HR04-May-2001 L/H ENG 0.080.000.001,288.9
100HR04-May-2001 OIL COOLER 0.340.810.001,288.9
100HR04-May-2001 R/H ENG 0.130.000.001,288.9
100HR06-Jun-2001 L/H ENG 0.120.000.001,289.7
100HR06-Jun-2001 OIL COOLER 0.410.710.001,289.7
100HR06-Jun-2001 R/H ENG 0.190.000.001,289.7
SHAFT BALANCE COMPLETED TQ3508-Jul-2001 #2 OUTSHAF 0.000.100.001,448.5
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.
8524465HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
Page 2 of 10
a b c d e f g
VIBRATION CHECK DUE09-Jul-2001 DRI.SHAFT 0.000.040.001,449.0
PHASE INSPECTION26-Feb-2002 L/H DR/SHA 0.000.200.001,488.0
PHASE INSPECTION26-Feb-2002 OIL COOLER 0.900.260.001,488.0
PHASE INSPECTION26-Feb-2002 R/L DR/SHA 0.000.380.001,488.0
100 HR. INSP TQ=3302-Jun-2002 L/H ENG 0.000.460.001,591.8
100 HR. INSP02-Jun-2002 OIL COOLER 0.090.320.001,591.8
100 HR. INSP TQ=3402-Jun-2002 R/H ENG 0.000.420.001,591.8
TQ= 35 FOR REMOVAL/ REINSTALLATION ENG13-Jun-2002 R/H ENG 0.000.280.001,641.0
TQ= 35% 100 HR. INSP28-Jun-2002 L/H ENG 0.000.450.001,692.4
100 HR INSP.28-Jun-2002 OIL COOLER 0.340.120.001,692.4
100 HR. INSP. DID NOT HAVE TQ READINGS28-Jun-2002 R/H ENG 0.000.250.001,692.4
100 HR INSP10-Aug-2002 OIL COOLER 0.120.230.001,793.1
100 HR INSP TQ 3410-Aug-2002 L/H ENG 0.000.320.001,793.4
100 HR INSP TQ 3410-Aug-2002 R/H ENG 0.000.250.001,793.4
100 HR INSP TQ 3321-Sep-2002 L/H ENG 0.220.000.001,853.7
100 HR INSP21-Sep-2002 OIL COOLER 0.030.200.001,853.7
100 HR INSP TQ 3221-Sep-2002 R/H ENG 0.150.000.001,853.7
500 HR PHASE TQ=3807-Mar-2003 #1 ENG 0.050.000.001,984.8
500 HR PHASE TQ=3707-Mar-2003 #2 ENG 0.300.000.001,984.8
500 HR PHASE07-Mar-2003 OIL COOLER 0.150.450.001,984.8
100 HR INSP TQ=3519-Apr-2003 L/H ENG 0.080.000.002,086.0
100 HR INSP19-Apr-2003 OIL COOLER 0.140.320.002,086.0
100 HR INSP TQ=3419-Apr-2003 R/H ENG 0.300.000.002,086.0
100 HR INSP TQ= 3504-Jun-2003 L/H ENG 0.000.350.002,169.7
100 HR INSP TQ =3404-Jun-2003 R/H ENG 0.000.210.002,169.7
100 HR INSP TQ=3211-Jun-2003 L/H ENG 0.000.470.002,181.8
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.
8524465HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
Page 3 of 10
a b c d e f g
100 HR INSP11-Jun-2003 OIL COOLER 0.120.240.002,181.8
100 HR INSP TQ=3111-Jun-2003 R/H ENG 0.000.460.002,181.8
100 HR INSP TQ=3402-Jul-2003 L/H ENG 0.000.150.002,200.3
REMOVAL & REINSTALLATION OF ENG TQ=3715-Jul-2004 #1 ENG 0.280.000.002,265.2
REMOVAL & REINSTALLATION OF ENG TQ=3715-Jul-2004 #2 ENG 0.140.000.002,265.2
REMOVAL & REINSTALLATION OF ENG15-Jul-2004 OIL COOLER 0.180.750.002,265.2
BEARING REPLACEMENT26-Jan-2005 OIL COOLER 0.280.630.002,269.2
REM. & REINSTL.05-Feb-2005 OIL COOLER 0.280.630.002,272.2
120 HR. INSP. TQ. NOT LISTED03-Mar-2005 L/H ENG 0.170.000.002,308.2
120 HR. INSP.03-Mar-2005 OIL COOLER 0.300.680.002,308.2
120 HR. INSP. TQ. NOT LISTED03-Mar-2005 R/H ENG 0.140.000.002,308.2
120 HR. INSP. TQ=3816-Apr-2005 L/H ENG 0.420.000.002,429.5
120 HR.INSP.16-Apr-2005 OIL COOLER 0.310.400.002,429.5
120 HR. INSP. TQ=3716-Apr-2005 R/H ENG 0.110.000.002,429.5
REPL. OF #1 ENG FUEL PUMP12-May-2005 OIL COOLER 0.200.460.002,531.3
120 HR. INSP. TQ=3819-May-2005 L/H ENG 0.120.000.002,548.2
120 HR. INSP.19-May-2005 OIL COOLER 0.0048.000.002,548.2
120 HR. INSP. TQ=3819-May-2005 R/H ENG 0.130.000.002,548.2
OUT OF BAL. TQ=3820-May-2005 L/H ENG 0.120.000.002,548.2
120 HR. INSP. TQ=3429-Jun-2005 L/H ENG 0.160.000.002,667.7
120 HR. INSP.29-Jun-2005 OIL COOLER 0.280.110.002,667.7
120 HR. INSP. TQ=3629-Jun-2005 R/H ENG 0.060.000.002,667.7
REM. & REINSTL. TQ=3429-Jun-2005 L/H ENG 0.160.000.002,667.8
700 HR. PHASE #5 TQ=3604-Aug-2005 L/H ENG 0.090.000.002,674.8
700 HR. PHASE04-Aug-2005 OIL COOLER 0.130.110.002,674.8
700 HR. PHASE #5 TQ=3604-Aug-2005 R/H ENG 0.070.000.002,674.8
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.
8524465HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
Page 4 of 10
a b c d e f g
120 HR. INSP. TQ=3704-Oct-2005 L/H ENG 0.230.000.002,786.2
120 HR. INSP.04-Oct-2005 OIL COOLER 0.160.360.002,786.2
120 HR. INSP. TQ=3604-Oct-2005 R/H ENG 0.400.000.002,786.2
120 HR INSP TQ=39%06-Dec-2005 L/H ENG 0.050.000.002,915.2
120 HR INSP06-Dec-2005 OIL COOLER 0.170.410.002,915.2
120 HR INSP TQ=37%06-Dec-2005 R/H ENG 0.430.000.002,915.2
120 HR INSP TQ = 3727-Feb-2006 L/H ENG 0.090.000.003,032.8
120 HR INSP27-Feb-2006 OIL COOLER 0.120.300.003,032.8
120 HR INSP TQ = 3827-Feb-2006 R/H ENG 0.380.000.003,032.8
REPL SEAL TQ = 3703-Mar-2006 #2 ENG 0.250.000.003,040.4
120 HR INSP TQ=3619-Apr-2006 #1 ENG 0.170.000.003,154.4
120 HR INSP TQ = 3619-Apr-2006 #2 ENG 0.370.000.003,154.4
120 HR INSP19-Apr-2006 OIL COOLER 0.200.220.003,154.4
120 HR INSP TQ = 3812-Jul-2006 #1 ENG 0.220.000.003,272.6
120 HR INSP TQ = 3512-Jul-2006 #2 ENG 0.380.000.003,272.6
120 HR. INSP.12-Jul-2006 OIL COOLER 0.150.080.003,272.6
720 HR. PHASE #6 TQ=3615-Dec-2006 L/H ENG 0.290.000.003,394.1
720 HR. PHASE #615-Dec-2006 OIL COOLER 0.140.000.003,394.1
720 HR. PHASE #6 TQ=3715-Dec-2006 R/H ENG 0.250.000.003,394.1
REINSTALL OF SEC 2 T/R D/S NO 2ND NO. GV10-May-2007 OIL COOLER 0.000.420.003,610.9
120 HR INSP23-May-2007 #1 ENG 0.080.000.003,633.5
120 HR INSP23-May-2007 #2 ENG 0.230.000.003,633.5
120 HR INSP23-May-2007 OIL COOLER 0.000.490.003,633.5
120 HR MTP MOC NO TQ NOTED02-Jul-2007 #1 ENG 0.110.000.003,754.9
120 HR MTP MOC NO TQ NOTED02-Jul-2007 #2 ENG 0.200.000.003,754.9
120 HR MTP MOC02-Jul-2007 OIL COOLER 0.460.000.003,754.9
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.
8524465HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
Page 5 of 10
a b c d e f g
120 HR INSP NO TQ NOTED18-Sep-2007 #1 ENG 0.030.000.003,883.2
120 HR INSP NO TQ NOTED18-Sep-2007 #2 ENG 0.420.000.003,883.2
120 HR INSP18-Sep-2007 OIL COOLER 0.000.460.003,883.2
120 HR INSP NO TQ NOTED31-Oct-2007 #1 ENG 0.030.000.004,002.6
120 HR INSP NO TQ NOTED31-Oct-2007 #2 ENG 0.470.000.004,002.6
120 HR INSP31-Oct-2007 OIL COOLER 0.000.640.004,002.6
720 HR INSP NO TQ PROVIDED27-Mar-2008 #1 ENG 0.230.000.004,110.9
720 HR INSP NO TQ PROVIDED27-Mar-2008 #2 ENG 0.180.000.004,110.9
720 HR INSP NO TQ PROVIDED27-Mar-2008 OIL COOLER 0.000.370.004,110.9
120 HR MTP MOC - NO TQ NOTED29-May-2008 #1 ENG 0.120.000.004,233.6
120 HR MTP MOC - NO TQ NOTED29-May-2008 #2 ENG 0.360.000.004,233.6
120 HR MTP MOC - NO TQ NOTED29-May-2008 OIL COOLER 0.000.570.004,233.6
XMSN REPL & REINST - NO TQ NOTED14-Aug-2008 #1 ENG 0.240.000.004,301.3
XMSN REPL & REINST - NO TQ NOTED14-Aug-2008 #2 ENG 0.310.000.004,301.3
120 HR MTP MOC - NO TQ NOTED12-Sep-2008 #1 ENG 0.250.000.004,354.1
120 HR MTP MOC - NO TQ NOTED12-Sep-2008 #2 ENG 0.310.000.004,354.1
120 HR MTP MOC12-Sep-2008 OIL COOLER 0.000.610.004,354.1
120 HR MTP MOC - NO TQ NOTED10-Nov-2008 #1 ENG 0.120.000.004,469.5
120 HR MTP MOC - NO TQ NOTED10-Nov-2008 #2 ENG 0.290.000.004,469.5
120 HR MTP MOC10-Nov-2008 OIL COOLER 0.000.030.004,469.5
120 HR MTP MOC - NO TQ NOTED18-Jan-2009 #1 ENG 0.080.000.004,591.7
120 HR MTP MOC - NO TQ NOTED18-Jan-2009 #2 ENG 0.300.000.004,591.7
120 HR MTP MOC18-Jan-2009 OIL COOLER 0.000.860.004,591.7
120 HR MTP MOC18-Jan-2009 TAIL ROTOR 0.000.000.104,591.7
ENGINE REPLACEMENT06-Feb-2009 #2 ENG 0.220.000.004,634.4
120 HR MTP MOC - NO TQ NOTED15-Mar-2009 #1 ENG 0.140.000.004,709.2
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.
8524465HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
Page 6 of 10
a b c d e f g
120 HR MTP MOC - NO TQ NOTED15-Mar-2009 #2 ENG 0.400.000.004,709.2
120 HR MTP MOC15-Mar-2009 OIL COOLER 0.000.660.004,709.2
120 HR MTP MOC15-Mar-2009 TAIL ROTOR 0.170.000.004,709.2
REPLACEMENT OF BLACK T/R BOOT26-Mar-2009 TAIL ROTOR 0.110.000.004,743.8
720 HR PHASE NO TQ PROVIDED26-May-2009 ENG #1 0.340.000.004,805.0
720 HR PHASE NO TQ PROVIDED26-May-2009 ENG #2 0.210.000.004,805.0
720 PHASE NO TQ PROVIDED26-May-2009 OIL COOLER 0.000.030.004,805.0
120 HR MTP NO TQ PROVIDED12-Sep-2009 L/H ENG 0.360.000.004,930.0
120 HR MTP12-Sep-2009 OIL COOLER 0.000.080.004,930.0
120 HR MTP NO TQ PROVIDED12-Sep-2009 R/H ENG 0.290.000.004,930.0
120 HR MTP NO TQ PROVIDED07-Nov-2009 L/H ENG 0.070.000.005,048.5
120 HR MTP07-Nov-2009 OIL COOLER 0.000.150.005,048.5
120 HR MTP NO TQ PROVIDED07-Nov-2009 R/H ENG 0.330.000.005,048.5
120 HR MTP- TQ=35%18-Mar-2010 L/H ENG 0.390.000.005,287.7
120 HR MTP18-Mar-2010 OIL COOLER 0.000.300.005,287.7
120 HR MTP- TQ= 34%18-Mar-2010 R/H ENG 0.210.000.005,287.7
120 HR MTP TQ = 34%23-Apr-2010 #1 ENG 0.070.000.005,407.8
120 HR MTP TQ= 34%23-Apr-2010 #2 ENG 0.090.000.005,407.8
120 HR MTP23-Apr-2010 OIL COOLER 0.000.130.005,407.8
720 HR PHASE27-Jul-2010 #1 ENG 0.360.000.005,512.4
720 HR PHASE27-Jul-2010 #2 ENG 0.300.000.005,512.4
720 HR PHASE27-Jul-2010 OIL COOLER 0.000.200.005,512.4
120 HR MTP - NO TQ PROVIDED29-Sep-2010 L/H ENG 0.240.000.005,629.1
120 HR MTP29-Sep-2010 OIL COOLER 0.000.060.005,629.1
120 HR MTP - NO TQ PROVIDED29-Sep-2010 R/H ENG 0.220.000.005,629.1
120 MTP -NO TQ PROVIDED12-Nov-2010 L/H 0.270.000.005,755.9
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.
8524465HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
Page 7 of 10
a b c d e f g
120 HR MTP12-Nov-2010 OIL COOLER 0.000.130.005,755.9
120 HR MTP NO TQ PROVIDED12-Nov-2010 R/H ENG 0.180.000.005,755.9
120 HR MTP MOC DUE04-Feb-2011 #1 ENG 0.120.000.005,867.7
120 HR MTP MOC DUE04-Feb-2011 #2 ENG 0.230.000.005,867.7
120 HR MTP MOC DUE04-Feb-2011 OIL COOLER 0.110.000.005,867.7
120 HR INSP01-Apr-2011 # 1 ENGINE 0.080.000.005,990.7
120 HR INSP01-Apr-2011 # 2 ENGINE 0.260.000.005,990.7
120 HR INSP01-Apr-2011 OIL COOLER 0.000.170.005,990.7
120 HR INSP01-Apr-2011 TAIL ROTOR 0.000.060.005,990.7
720 HR INSP17-Sep-2011 # 1 ENG 0.190.000.006,220.1
720 HR INSP17-Sep-2011 # 2 ENG 0.190.000.006,220.1
720 HR INSP17-Sep-2011 OIL COOLER 0.000.300.006,220.1
720 HR INSP17-Sep-2011 TR 0.000.090.006,220.1
REPL OF BLUE T/R BLADE07-Oct-2011 TAIL ROTOR 0.000.170.006,268.0
120 VIBE06-Nov-2011 #1 ENG 0.230.000.006,343.8
120 VIBE06-Nov-2011 #2 ENG 0.280.000.006,343.8
120 VIBE06-Nov-2011 OIL COOLER 0.000.400.006,343.8
120 VIBE06-Nov-2011 T/R BAL 0.000.090.006,343.8
120 HR INSPECTION14-Jan-2012 #1 ENGINE 0.450.000.006,462.1
120 HR INSPECTION14-Jan-2012 #2 ENGINE 0.270.000.006,462.1
120 HR INSPECTION14-Jan-2012 OIL COOLER 0.000.300.006,462.1
REPLACED TAIL ROTOR BLACK DE-ICE CABLE09-Feb-2012 TAIL ROTOR 0.000.070.006,508.7
120 HOUR, #1 ENG DRIVESHAFT BALANCE DUE10-Mar-2012 #1 ENG 0.210.000.006,579.7
120 HOUR10-Mar-2012 OIL COOLER 0.000.260.006,579.7
120 HOUR10-Mar-2012 TAIL ROTOR 0.000.030.006,579.7
120 HOUR11-Mar-2012 #2 ENG 0.290.000.006,579.7
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.
8524465HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
Page 8 of 10
a b c d e f g
T/R BALANCE CHECK DUE (KO012557)15-Mar-2012 TAIL ROTOR 0.000.080.006,589.6
VIBE CHECK AFTER CCAD REBUILD10-Oct-2012 #1 ENG 0.160.000.006,671.0
VIBE CHECK AFTER CCAD REBUILD10-Oct-2012 #2 ENG 0.290.000.006,671.0
VIBE CHECK AFTER CCAD REBUILD10-Oct-2012 OIL COOLER 0.000.340.006,671.0
VIBE CHECK AFTER CCAD REBUILD10-Oct-2012 TAIL ROTOR 0.000.050.006,671.0
120 HR INSP09-Nov-2012 #1 ENG 0.080.000.006,699.1
120 HR INSP09-Nov-2012 #2 ENG 0.180.000.006,699.1
120 HR INSP09-Nov-2012 OIL COOLER 0.000.240.006,699.1
120 HR INSP09-Nov-2012 T/R D/S 0.000.200.006,699.1
REPL OF T/R BLADE EROSION STRIP27-Mar-2013 T/R 0.000.020.006,807.4
120 HR MTF VIB CHECK05-Apr-2013 # 1 ENG 0.260.000.006,819.2
120 HR MTF VIB CHECK05-Apr-2013 #2 ENG 0.120.000.006,819.2
120 HR MTF VIB CHECK05-Apr-2013 OIL COOLER 0.000.120.006,819.2
120 HR MTF VIB CHECK05-Apr-2013 T/R 0.000.060.006,812.2
REPL OF T/R BOOT10-Apr-2013 T/R 0.000.020.006,828.0
REPL OF T/R BOOT22-Apr-2013 T/R 0.000.090.006,837.8
120 HR MTF VIB CHECK28-Aug-2013 # 1 ENG 0.360.000.006,939.7
120 HR MTF VIB CHECK28-Aug-2013 #2 ENG 0.210.000.006,939.7
120 HR MTF VIB CHECK28-Aug-2013 OIL COOLER 0.000.400.0069,397.7
120 HR MTF VIB CHECK28-Aug-2013 T/R 0.000.030.006,939.7
120 HR. INSP.15-Jun-2014 #1 ENG 0.370.000.007,300.7
120 HR. INSP.15-Jun-2014 #2 ENG 0.320.000.007,300.7
120 HR. INSP.15-Jun-2014 OIL COOLER 0.000.490.007,300.7
120 HR. INSP.15-Jun-2014 T/R 0.000.030.007,300.7
120 HR INSP26-Aug-2014 #1 ENG 0.410.000.007,416.1
120 HR INSP26-Aug-2014 #2 ENG 0.220.000.007,416.1
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.
8524465HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
Page 9 of 10
a b c d e f g
120 HR INSP26-Aug-2014 OIL COOLER 0.000.240.007,416.1
120 HR INSP26-Aug-2014 T/R 0.000.100.007,416.1
120 HR INSP03-Jan-2015 #2 ENG 0.130.000.007,540.0
120 HR INSP03-Jan-2015 #1 ENG 0.380.000.007,540.0
120 HR INSP03-Jan-2015 OIL COOLER 0.000.510.007,540.0
120 HR INSP03-Jan-2015 T/R 0.000.100.007,540.0
REMOVAL/REINSTALLATION OR T/R BLADES13-Jan-2016 T/R 0.000.170.007,659.6
POST 720 HOUR PHASE23-Jan-2016 #1 ENG 0.230.000.007,662.1
POST 720 HOUR PHASE23-Jan-2016 #2 ENG 0.130.000.007,662.1
POST 720 HOUR PHASE23-Jan-2016 OIL COOLER 0.040.000.007,662.1
POST 720 HOUR PHASE23-Jan-2016 T/R D/S 0.000.120.007,662.1
REINSTALLATION OF ENGINE ON 14 FEB 1616-Feb-2016 #2 ENGINE 0.130.000.007,687.7
120 HR MTF VIB CHECK31-Mar-2016 #1 ENGINE 0.210.000.007,784.6
120 HR MTF VIB CHECK31-Mar-2016 #2 ENGINE 0.260.000.007,784.6
120 HR MTF VIB CHECK31-Mar-2016 OIL COOLER 0.000.050.007,784.6
120 HR MTF VIB CHECK31-Mar-2016 T/R 0.000.100.007,784.6
120 HR MTF VIB CHECK21-May-2016 #1 ENG 0.220.000.007,904.3
120 HR MTF VIB CHECK21-May-2016 #2 ENG 0.240.000.007,904.3
120 HR MTF VIB CHECK21-May-2016 OIL COOLER 0.000.100.007,904.3
120 HR MTF VIB CHECK21-May-2016 T/R 0.000.150.007,904.3
BLACK T/R BLADE EROSION STRIP REPAIR15-Jul-2016 T/R 0.000.060.008,008.9
120 HR MTF VIB CHECK26-Jul-2016 #1 ENG 0.200.000.008,022.1
120 HR MTF VIB CHECK26-Jul-2016 #2 ENG 0.240.000.008,022.1
120 HR MTF VIB CHECK26-Jul-2016 OIL COOLER 0.000.170.008,022.1
120 HR MTF VIB CHECK26-Jul-2016 T/R 0.000.100.008,022.1
T/R ABRASION STRIP REPLACEMENT31-Aug-2016 T/R 0.000.010.008,067.0
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.
8524465HELICOPTER, UTILITYEH-60A
3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL
Page 10 of 10
a b c d e f g
T/R BAL FOR REPL OF RED T/R BL DE-ICE H25-Oct-2016 T/R 0.000.100.008,077.0
BAL. AFTER RED T/R ABRASION STRIP REPAIR03-Dec-2016 T/R 0.000.050.008,133.7
120 HR MTF VIB CHECK08-Jan-2017 #1 ENG 0.180.000.008,139.9
120 HR MTF VIB CHECK08-Jan-2017 #2 ENG 0.200.000.008,139.9
120 HR MTF VIB CHECK08-Jan-2017 OIL COOLER 0.000.250.008,139.9
120 HR MTF VIB CHECK08-Jan-2017 T/R 0.000.040.008,139.9
T/R BALANCE CHECK04-Mar-2017 T/R 0.000.040.008,170.3
OUTPUT SHAFT BALANCE05-Mar-2017 #2 ENG 0.030.000.008,170.3
120 HR MTF VIB CHECK10-Jun-2017 #1 ENG 0.200.000.008,262.3
120 HR MTF VIB CHECK10-Jun-2017 #2 ENG 0.490.000.008,262.3
120 HR MTF VIB CHECK10-Jun-2017 OIL COOLER 0.000.060.008,262.3
120 HR MTF VIB CHECK10-Jun-2017 T/R 0.000.180.008,262.3
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 85-24465
The following Components are actually installed on the acft and are Unserviceable (Green Tag, or have
an entry on the 13-1) at the time of the BEST Program In-Process. They may or may not be installed in
ULLS-A and MCDS. They will remain in the state they arrived until at such time they are actually
removed from the aircraft. If removed during the BEST In-Process, the 2410’s will be included in this
folder.
COMPONENT ULLS-A P/N ULLS-A S/N
SERVO. PRIMARY MAIN ROTOR 70410-02820-054 B303-15553
ACFT 85-24465
The following Components were unable to have the S/N’s verified during the BEST Induction and S/N
check process. Either Data Plates were not installed, not legible, partially legible, painted over, S/N
painted on component, internal or were not accessible due to cowlings/fairings not being removed. All
of these components have been S/N matched against MCDS and if the records do not match between
ULLS-A and MCDS, then the 2410 Hotline will provide follow on guidance.
COMPONENT ULLS-A P/N ULLS-A S/N
INPUT MODULE 70351-08001-046 A264-00379
INPUT MODULE 70351-08001-046 A264-02151
ACCUMULATOR 3197170-5 8110170A
STABILATOR ACTUATOR 70400-06641-117 C292-07785
STABILATOR ACTUATOR DL2155M31MOD1 1958
AFT TIE ROD SUPPORT FITTING 70400-08112-045 A391-00966
Page 1 of 17
CAO01521
85244656035T00G01T700-GE-700 ENGINE ASSYGE-E-306485
6716
6900
14517
105988
15099
20045
3581
4089
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 17
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-306485
hr)
687910597199804075
600218830134253523GE-C-0066236035T02G01COLD SECTIONMODULE
COND
COND
6879
1277GGMER6616064T55G01COMBUSTION LINER
COND
COND
554510495165173501
410516609101422401MRS089376055T20G05MTCHDROTOR/STATOR ASSY
COND
COND
6879
3013AMDA36605043T24G14STAGE 1 NOZZLE
COND
COND
638010561185653872
50926087192632639GEL8075526064T98G01POWER TURBINEMODULE
COND
COND
2949
2308GE-D-0060746035T01G01ACCESSORY MODULE
COND
COND
6380
0K70406034T62P18PARTICLESEPARATOR BLOWER
COND
COND
4314
0154642144046T52G39FUEL CONTROL
COND
COND
5161
2643APM240RR4076T64G01POU ASSY-O/S DRAINVALVE
COND
COND
7155
1310EMDE04984046T29G13ELECTRICALCONTROL UNIT
COND
COND
29489567590971841
2762415849471330CAO015214046T26G03HISTORY 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 17
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-306485
hr)
3329
4200UDC014214046T25G01COOLER, OIL
COND
COND
4301
1415COMH73304046T28G14ANTI-ICE VALVE
COND
COND
14. SIGNIFICANT HISTORICAL DATA
7/25/200012:00:00 AM
1 25 JUL 00: TB 1-2840-248-23 DTD 04 AUG 99 AND TB 1-2840-248-20-2 DTD 30JUN 94 C/W AT CCAD, S/L. FUENTES, RECORDS CLERK.
thomas.m.lilly CCAD (NO LOCATION
7/25/200012:00:00 AM
2 25 JUL 00: TB 1-2840-248-23 DTD 04 AUG 99 AND TB 1-2840-20-2 DTD 30 JUN94 C/W AT CCAD, S/L. FUENTES, RECORDS CLERK.
thomas.m.lilly CCAD (NO LOCATION)
7/25/200012:00:00 AM
3 25 JUL 00: TB 1-2840-248-20-2 DTD 30 JUN 94 C/W AT CCAD. S/L. FUENTES,RECORDS CLERK.
thomas.m.lilly CCAD (NO LOCATION)
7/31/200012:00:00 AM
1 31JUL 00: CCAD - PT MOD REPAIRED, 25 JUL 00, IAW DMWR55-2840-248 &CHGS. S/L. FUENTES, RECORDS CLERK.
thomas.m.lilly CCAD (NO LOCATION)
7/31/200012:00:00 AM
2 31 JUL 00: CCAD- MATCHED GG ROTOR/STATOR ASSY REPAIRED, 25 JUL00, IAW DMWR 55-2840-248 & CHGS. STG 1 & STG 2 BLADE SETSINSTALLED W/DAMPERS. S/L. FUENTES, RECORDS CLERK.
thomas.m.lilly CCAD (NO LOCATION)
7/31/200012:00:00 AM
3 31 JUL 00: CCAD - PT MOD REPAIRED, 25 JUL 00, IAW DMWR 55-2840-248 &CHGS. S/L. FUENTES, RECORDS CLERK.
thomas.m.lilly CCAD (NO LOCATION)
4/16/200212:00:00 AM
1 16 APR 02: (ACFT AND) ENGINE INVOLVED IN TAIL ROTOR BLADE STRIKE.ENGINE INSPECTED AND RELEASED FOR CONTINUED USE I/A/W AMCOMLTR DTD 16 APRIL 2002, HISTORY RECORDER READING: LCF 1 1540, LCF 25629, TTI 5142 AND OP HRS:3090. TOTAL CUMULATIVE COUNTS ONENGINE: LCF 1 2051, LCF 2 9779, TTI 96659, AND OP HRS 3276. CO3789, 54THMED DET, FT. LEWIS, WA 98433
thomas.m.lilly 54TH MED DET FT. LEWIS, WA
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 17
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-306485
hr)
6/21/200612:00:00 AM
1 21 JUN 06: CCAD, C/S MOD REPAIRED, 19 JUNE 06, IAW DMWR 1-2840-248 &CHGS. FUEL INJECTORS CLEANED & FLOWED PER DMWR @ C/S TSN:3875, RECAPPED ON 19 JUNE 06, IAW AED P-3430B, DTD 03 01, S/O S.RODRIGUEZ RECORDS CLERK.
thomas.m.lilly CCAD (NO LOCATION)
1/14/200912:00:00 AM
1 14 JAN 09 - REPAIRED C/S MOD. S/N:GE-C-006480 AT LCF:2574, LCF2:10871,TTI:30517, HRS:3725 ON UNINSTALLED ENG. SN:GE-E-306485 W/CUM.COUNTS LCF1:3002, LCF2:13438, TTI:104369, HRS:4301. H/R SN:CAO01521READINGS AT LCF1:2491, LCF2:9288, TTI:12852, HRS:4115. (ES4206 ENG.SHOP) ENGINE RETURNED TO SERVICEABLE CONDITION. MF4187R/SPEC.; USAACE, FT. RUCKER, AL.
thomas.m.lilly USAACE FT. RUCKER, AL.
7/2/200912:00:00 AM
1 02 JUL 09 - ENGINE CHIP NO 1 ENGINE. CLEANED CHIP DETECTOR. APURUN. NO CHIP LIGHT PRESENT. INSPECT #1 CHIP DETECTOR AFTER 15MIN GROUND RUN - COMPLETED WITH NO CHIPS PRESENT. (AIRCRAFT8724671 AT 5095.6 ACFT HRS) HISTORY RECORDER SN: CAO01521READINGS ARE LCF1 - 2594, LCF2 - 9945, TTI - 12956, OP HRS - 4375.(RC1002) R/SPEC, USAACE, FT. RUCKER, AL.
thomas.m.lilly USAACE FT. RUCKER, AL.
9/15/200912:00:00 AM
1 15 SEP 09 - #1 ENG OIL FILTER BYPASS BUTTON POPPED. REPLACEDFILTER. AIRCRAFT 8724671 AT 5224.7 ACFT HRS. ENGINE COUNTS ARELCF1 - 3170, LCF2 - 14647, TTI - 104529, OP HRS - 4697. HISTORY RECORDERCOUNTS ARE LCF1 - 2659, LCF2 - 10497, TTI - 13012, OP HRS - 4511. (RC1002)R/SPEC, USAACE, FT. RUCKER, AL.
thomas.m.lilly USAACE FT. RUCKER, AL.
9/15/200912:00:00 AM
2 15 SEP 09 - #1 ENG OIL FILTER BYPASS BUTTON POPPED. REPLACEDFILTER. AIRCRAFT 8724671 AT 5224.7 ACFT HRS. ENGINE COUNTS ARELCF1 - 3170, LCF2 - 14647, TTI - 104529, OP HRS - 4697. HISTORY RECORDERCOUNTS ARE LCF1 - 2659, LCF2 - 10497, TTI - 13012, OP HRS - 4511. (RC1002)R/SPEC, USAACE, FT. RUCKER, AL.
thomas.m.lilly USAACE FT. RUCKER, AL.
3/12/201112:00:00 AM
1 REMOVED ENGINE S/N: GE-E-306485 W/TSN: 5545 FROM ACFT 8724671 @6044.9 ACFT HR. ENGINE CUMM CNTS: LCF1:3501 LCF2:16517,INDEX:104953, OP HRS:5545, ENGINE H/R READINGS S/N: CAO01521LCF1:2990, LCF2:12367, INDEX:13436, OP HRS:5359.
jessica.n.kennedy USAACE FT.RUCKER, AL
3/14/201112:00:00 AM
1 GG ROTOR S/N MRS09172 REMOVED FROM UNISTALLED ENG WITHLCF1:3766, LCF2:15003, INDEX:14531, OP HRS:7059. REMOVAL DUE TO TIMECHANGE ENG CUMM CNTS. LCF1:3501, LCF2:16517, INDEX:104953, OP
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 17
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-306485
hr)
HR:5545. H/R S/N:CAO01521 READINGS= LCF1: 2990, LCF2:12367,INDEX;6609, OP HOURS: 5359. INSTALLED GG ROTOR S/N: MRS08937 WITHLCF1:2401, LCF2; 10142, INDEX:16609, OP HRS: 4105
DW010950 USAACE FT.RUCKER, AL
3/17/201112:00:00 AM
1 INTSTALLATION ENGINE S/N: GEE306485 W/TSN: 5545 (AIRCRAFT HOURS12163) HISTORY RECORDER READINGS: LCF1: 2990, LCF2:12367, TTI: 13436,HOURS: 5359. ENG READINGS : LCF1-3501 LCF2-16517 TTI-104953 HOURS-5545. RECORD SPEC JK015371
jessica.n.kennedy USAACE FT. RUCKER, AL
3/17/201112:00:00 AM
2 INSTALLED ENGINE S/N: GEE306485 W/TSN: 5545 (AIRCRAFT HOURS12163) HISTORY RECORDER READINGS: LCF1: 2990, LCF2:12367, TTI: 13436,HOURS: 5359. ENG READINGS : LCF1-3501 LCF2-16517 TTI-104953 HOURS-5545. RECORD SPEC JK015371
jessica.n.kennedy USAACE FT. RUCKER, AL
8/1/201212:00:00 AM
1 REMOVED ENG S/N: GEE-306485 H/R READINGS OF LCF1: 3361 LCF2:14415TTI: 14099 OP HRS: 6194 ENG CUMM COUNTS: LCF1: 3872 LCF2: 18565 TTI:105616 OP HRS: 6380 FROM ACFT 8826017 AT 12963 ACFT HRS DUE TO TIME
rhonda.e.jackson USAACE FT. RUCKER, AL
8/6/201212:00:00 AM
1 PT MOD S/N GE-L-037287 REMOVED FROM UNINSTALLED EINGINE WITHLCF1 2854 LCF2 10646 TTI 20456 OP HRS 5026. REMOVAL DUE TO TIMECHANGE. ENG CUM CTS = LCF1 3872 LCF2 18565 TTI 105616 OP HRS 6380.H/R S/N CAO01521 READINGS = LCF1 3361 LCF2 14415 TTI 14099 OP HRS6194, INSTALLED PT MODULE S/N GEL807552 WITH LCF1 2639 LCF2 19263TTI 6087 OP HRS 5092.
olivia.d.williams USAACE FT RUCKER,AL
8/10/201212:00:00 AM
1 REMOVED PARTICLE SEP BLOWER S/N: SUS01664 W/TTSN: 4961 FROM ENGGE-E-306485 (ACFT 8826017 AT 12963 ACFT HRS) W/ ENG CUMM COUNTSLCF1:3361 LCF2:14415 TTI:14099 OP HRS:6194 H/R READINGS: LCF1: 3361LCF2: 14415 TTI:14099 OP HRS: 6194 DUE TO MISSING MORE THAN 50% OFPLATING ON IMPELLAR SHROUD. PART SEP BLOWER K7040 W/TTSN: 0
rhonda.e.jackson USAACE FT. RUCKER, AL
8/16/201212:00:00 AM
1 INSTALLED ENGINE GE-E306485 WITH H.R.(CAO01521) READINGS2990/12367/13436/5359. ENG CUM COUNTS 3872/18565/105616/6380.
vickie.l.meadows USAACE FT RUCKER, AL
8/16/201212:00:00 AM
2 INSTALLED ENGINE GE-E306485 WITH H.R.(CAO01521) READINGS2990/12367/13436/5359. ENG CUM COUNTS 3872/18565/105616/6380 ON A/CS.N 8826017 @ 12963.4 ACFT HRS.
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 6 of 17
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-306485
hr)
vickie.l.meadows USAACE FT RUCKER, AL
4/4/201412:00:00 AM
1 REPLACEMENT OF COLD SECTION, SN: GE-C-006780 EXTENDED 20 HRS TOBE DUE AT 6700 HRS ON ENGINE SN: GE-E-306485, W/ 7699 TSN & HRRDGS: LCF1: 3556, LCF2: 15012, TTI: 14455, OP HRS: 6675 ON ACFT 0067017AT 13433.9 ACFT HRS.
marissa.w.watkins USAACE FT. RUCKER, AL
4/15/201412:00:00 AM
1 REMOVED ENG SN: GE-E-306485 FROM ACFT 8826017 AT 13445.7 ACFT HRSW/ TSN: 7714 DUE TO COLD SECTON DUE TBO. CUMM ENG CTS: LCF1=4075, LCF2= 19980 TTI= 105972, OP HRS= 6879. HR SN: CAO01521 CUMMRDGS: LCF1= 3564, LCF2= 15030, TTI= 14455, OP HRS= 6693.
marissa.w.watkins USAACE FT. RUCKER, AL
5/5/201412:00:00 AM
1 COLD SECTION S/N GE-C-006480 REMOVED FROM UNINSTALLED ENGINEWITH LCF1 3647 LCF2 16613 TTI 32120 OP HRS 6303. REMOVAL DUE TOTIME CHANGE. ENGINE CUM CTS = LCF1 4075 LCF2 19980 TTI 105972 OPHRS 6879, H/R S/N CAO01521 READINGS = LCF1 3564 LCF2 15030 TTI 14455OP HRS 6693. COLD SECTION IGE-C-006623 INSTL WITH LCF1 3523 LCF213425 TTI 18830 OP HRS 6002.
olivia.d.williams USAACE FT RUCKER,AL
5/5/201412:00:00 AM
2 STAGE 1 NOZZEL S/N AMDA1590 REMOVED FROM UNISTALLED ENG WITHTTSN 6879. DUE TO CRACKED. INSTALLED AMDA3660 WITH TSN 3013. ENGCUM CTS = LCF1 4075 LCF2 19980 TTI 105972 OP HRS 6879. H/R S/NCAO01521 READINGS = LCF1 3564 LCF2 15030 TTI 14455 OP HRS 6693.
olivia.d.williams USAACE FT RUCKER,AL
5/5/201412:00:00 AM
3 COMBUSTION LINER S/N GGMP8578 REMOVED FROM UNISTALLED ENGWITH TTSN 6944. DUE TO SPRING BROKEN. INSTALLED GGMER661 WITHTSN 1277. ENG CUM CTS = LCF1 4075 LCF2 19980 TTI 105972 OP HRS 6879.H/R S/N CAO01521 READINGS = LCF1 3564 LCF2 15030 TTI 14455 OP HRS
olivia.d.williams USAACE FT RUCKER,AL
5/19/201412:00:00 AM
1 INSTALLED ON ACFT. 8524407 AT 10504 ACFT. HRS., WITH ENG METERREADINGS AS FOLLOWS, LCF-1: 4075, LCF-2: 19980, INDEX: 10592, OP HRS.:6879, HISTORY RECORDER S/N CAO01521 READINGS AS FOLLOWS, LCF-1:3564, LCF-2: 15030, INDEX: 14455, OP HRS.: 6693.
anthony.s.speigner USAACE FT. RUCKER, AL.
6/2/201412:00:00 AM
1 REMOVED FROM ACFT. 8524407 AT 10523 ACFT. HRS., WITH ENG.ACCUMULATIVE COUNTS AS FOLLOWS: LCF:1 4089, LCF-2: 20045, INDEX:105988, OP HRS.: 6900, AND HISTORY RECORDER READINGS AS FOLLOWS:LCF-1: 3578, LCF-2: 15095, INDEX: 14471, OP HRS: 6714, DUE TO ENGINE
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 7 of 17
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-306485
hr)
LEAKING OIL.
anthony.s.speigner USAACE FT. RUCKER, AL.
7/21/201412:00:00 AM
1 REPLACED OIL MANIFOLD, ENGINE RAN AND ACCEPTED ON TEST CELL,RETURNED TO SERVICE AT TTSN: 6900 HRS. HISTORY RECORDER SN:CAO1521, LCF 1: 03581, LCF 2: 15099, INDEX: 14517, OP HRS: 6716.
QC000000 USAACE(AMSS) FT. RUCKER, AL.
8/22/201412:00:00 AM
1 INSTALLED ENGINE S/N: GE-E-306485 WITH TTSN: 6900 ON ACFT 8524465AT 7416.1 ACFT HRS. HISTORY RECORDER READINGS: LCF1: 3581, LCF2:15099, TTI: 14517, OP HRS: 6716. ENGINE CUM CTS: LCF1: 4089, LCF2: 20045,TTI: 105988, OP HRS: 6900.
jeremy.g.strickland USAACE FT. RUCKER, AL.
7/7/201512:00:00 AM
1 REMOVED ECU S/N: EMDE0700, DUE TO TGT READS LOW, TSN 2681, LCF13674, LCF2 15318, TTI 14565, OP HRS 2681, ENG CUM CTS: LCF1 4182, LCF220264, TTI 106036, OP HRS 7155, H/R READINGS: LCF1 3674, LCF2 15318, TTI14565, OP HRS 6971.
jimmy.s.caylor USAACE FT.RUCKER,AL.
7/8/201512:00:00 AM
1 INSTALLED ECU S/N: EMDE0498, , TSN 1310, , ENG CUM CTS: LCF1 4182,LCF2 20264, TTI 106036, OP HRS 7155, H/R READINGS: LCF1 3674, LCF2 15318,TTI 14565, OP HRS 6971.
jimmy.s.caylor USAACE FT.RUCKER,AL.
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 8 of 17
CAO01521
GE-E-3064856035T02G01COLD SECTION MODULEGE-C-006623
6693
6002
14455
18830
15030
13425
3564
3523
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 9 of 17
04A01 6035T02G01 COLD SECTION MODULE GE-C-006623
hr)
600018679134193521
110452NRW970145056T66G02POWER TAKEOFFDRIVE
COND
COND
600018679134193251
600018679134193521GLB205736035T77G14COMPRESSORROTOR ASSY
COND
COND
600018679134193521
162515892924601GATCVNGR6035T88P04GAS GEN TURBINESHAFT
16066
11000
600018679134193521
0000WEST48045036T95P01INNER BALANCEPISTON SE
COND
COND
600018679134193521
0000MLEWF1776035T79P04COMPRESSORDISCHARGE SE
COND
COND
600018679134193521
2262108104526907FIAAJ6NM6035T83P01COMPRESSOR REARSHAFT
9429
5000
600018679134193521
0000VAEFY4775044T07P01NO 3 LABYRINTH
COND
COND
600018679134193521
21741445537001571BIWCM0495035T57P02VORTEX SPOILER
COND
COND
600018679134193521
2559384053111246GATHC1MC5043T04P02TIE ROD,COMPRESSOR
14132
10000
600018679134193521
23222252443711453GATMH2134045T08P01RING, SPACERCOMPRESSOR
14369
10000
600018679134193521
0000GLHTP87K6055T59P01COMPRESSORIMPELLER
11691
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 10 of 17
04A01 6035T02G01 COLD SECTION MODULE GE-C-006623
hr)
600018679134193521
0000GGTA65743065T21G01OUTPUT SHAFT ASSY
COND
COND
600018679134193521
0000GLHTNGN86032T26G09STAGE 1 BLISK
11691
5000
600018679134193521
0000GLHTPE2A6032T27P08STAGE 2 BLISK
13691
7000
600018679134193521
0000GLHTPE1F6038T08P04STAGE 3 & 4 BLISK
13691
7000
600018679134193521
0000GLHTPD476038T09P04STAGE 5 BLISK
13691
7000
600018679134193521
5079441439011415BARA90656043T45P01NO 3 BALL BEARING
COND
COND
600018679134193521
0000FCAAF7296064T15P03NO 4 ROLLER
COND
COND
14. SIGNIFICANT HISTORICAL DATA
7/26/200812:00:00 AM
1 WUC: 04A01 PN: 6035T02G01 PSN: GE-C-006623 COLD SECTIONMODULE26JUL08 - CCAD C/S MOD REPAIRED 22JUL08 IAW DMWR 1-2840-248 & CHANGES AND RECAPPED AED P3430B DTD 03DEC01. FUELINJECTORS CLEANED AND FLOWED PER DMWR AT C/S TSN 4240 ON22JUL08. /S/ S.DAVIS, AIRCRAFT DATA TECHNICIAN.
mae.p.belford CCAD (NO LOCATION)
9/9/200812:00:00 AM
1 WUC: 04A01 PN: 6035T02G01 PSN: GE-C-006623 COLD SECTIONMODULE09 SEP 08 - INSTALLED C/S MODULE S/N GEC006623 W/TSN 4242HRS ON ENGINE GE-E-307079 W/TTSN 4961 HRS. ENGINE CUMULATIVECTS: LCF-1: 2139, LCF-2: 12226, T/TI: 4656, OP HRS: 4961. H/R S/N ECD00607READINGS: LCF-1: 2139, LCF-2: 12226, T/TI: 4656, OP HRS: 4961. BH0315[R/SPEC], USAACE, FT. RUCKER, AL.
mae.p.belford USAACE FT. RUCKER, AL.
6/19/201212:00:00 AM
1 COLD SECTION RECAPPED ON 14 JUN 12 IAW DMWR 1-2840-248 &CHANGES. FUEL INJECTORS CLEANED AND FLOWED PER DMWR AT COLDSECTION MODULE TSN 6000
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 11 of 17
04A01 6035T02G01 COLD SECTION MODULE GE-C-006623
hr)
MT5543 CCAD CC,TX
5/5/201412:00:00 AM
1 COLD SECTION INSTALLED ON UNINSTALLED ENG WITH LCF1 3523 LCF213425 TTI 18830 OP HRS 6002. ENGINE CUM CTS =LCF1 4075LCF2 19980TTI 105972 OP HRS 6879. H/R READINGS S/N CAO01521 READING = LCF13564 LCF2 15830 TTI 14455 OP HRS 6693
olivia.d.williams USAACE FT RUCKER,AL
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 12 of 17
CAO01521
GE-C-0066233065T21G01OUTPUT SHAFT ASSYGGTA6574
6693
2
14455
151
15830
6
3564
2
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
EH-60A
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 13 of 17
04A01G 3065T21G01 OUTPUT SHAFT ASSY GGTA6574
hr)
0000
0000FCAY98036064T34P02NO 1 BALL BEARING
COND
COND
0000
0000FCAY58725121T46P02NO 2 ROLLER
COND
COND
14. SIGNIFICANT HISTORICAL DATA
6/19/201212:00:00 AM
1 OUTPUT SHAFT INSTALLED, INSPECTED, TEST AND FOUND SERVICEABLEON 14 JUN 12 IAW DMWR 1-2840-248 AND CHANGES
MT5543 CCAD CC,TX
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 14 of 17
CAO01521
GE-E-3064856055T20G05MTCHD ROTOR/STATORMRS08937
5359
4105
13436
16609
12367
10142
2990
2401
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 15 of 17
04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRS08937
hr)
410516609101422401
0000GATHJAGL6064T85P02STAGE 1 TURBINE
10359
5000
410516609101422401
23591382751761658GGA068106039T57G18STATOR GASGENERATOR
COND
COND
410516609101422401
2552887931143GATHHNWR6064T86P02STAGE 2 TURBINE
10104
5000
410516609101422401
18203451415710866GFF59PDP6064T81P01STG 1 FWD COOLINGPLATE
8539
5000
410516609101422401
6093662084448PAMEN5386064T82P01STG 1 AFT COOLINGPLATE
9750
5000
410516609101422401
8805752652555PAMET4836064T83P01STG 2 FWD COOLINGPLATE
9479
5000
410516609101422401
50064071261214GFF5CD5P6064T84P02STG 2 AFT COOLINGPLATE
9859
5000
410516609101422401
410516609101422401GGA089376039T54G13ROTOR GASGENERATOR
COND
COND
14. SIGNIFICANT HISTORICAL DATA
6/1/199912:00:00 AM
1 STAGE ONE AND TWO GG BLADE SETS CONTAIN NEW OR USED BLADESTHAT HAVE ALWAYS BEEN RUN WITH DAMPERS CCAD-C/W. UH-60-95-ASAM-08 AND 97-ASAM-03. RECORDS CLERK
QC000000 CCAD CCAD
12/10/201012:00:00 AM
1 TB1-2840-248-2 DTD 30JUN94 C/W AT CCAD AND LIFE LIMITS C/W I/A/WTM1-2840-248-23, TABLE 1-10
jessica.n.kennedy USAACE FT.RUCKER, AL
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 16 of 17
CAO01521
GE-E-3064856064T98G01POWER TURBINE MODULEGEL807552
6194
5092
14099
6087
14415
19263
3361
2639
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 17 of 17
04A03 6064T98G01 POWER TURBINE MODULE GEL807552
hr)
50926061192582637
50926061192582637GGAP55435043T75G07POWER TURBINEROTOR
COND
COND
50926061192582637
2670138548801025GATHCJFK6038T32P01STAGE 3 TURBINE
8524
5000
50926061192582637
0000GATHEPM66038T34P05STAGE 4 TURBINE
11194
5000
50926061192582637
0000GATHTW3W5125T92G01POWER TURBINESHAFT
11194
5000
50926061192582637
37441985177502267MDAA03125034T06P01NO 5 ROLLER
COND
COND
50926061192582637
449636598139542223MABY69016064T36P01NO 6 BALL BEARING
COND
COND
14. SIGNIFICANT HISTORICAL DATA
4/25/201212:00:00 AM
1 POWER TURBINE RECAPPED ON 20 APR 12 IAW DMWR 1-2840-248 &CHANGES. CP5495,
CP5495 CCAD CC, TEXAS
8/6/201212:00:00 AM
1 PT MODULE INSTALLED ON UNINSTALLED ENGINE ( GE-E-306485) WITHLCF1 2639 LCF2 19263 TTO 6087 OP HR S 5092. ENGINE CUM CTS = LCF1 3872LCF2 18565 TTI 105616 OP HRS 6380. ENG H/R S/N CAO01521 READINGS =LCF1 3361 LCF2 14415 OP HRS 14099 OP HRS 6194.
olivia.d.williams USAACE FT RUCKER,AL
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 1 of 16
CAO02124
85244656035T00G01T700-GE-700 ENGINE ASSYGE-E-207925
7211
6067
16745
14182
16209
16594
3498
3352
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 16
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-207925
hr)
606714182165943352
35241468864631752GE-C-0069316035T02G01COLD SECTIONMODULE
COND
COND
2466
3983GGMJ96296039T58G02COMBUSTION LINER
COND
COND
559214086156473139
3212143881991511MRSG34986055T20G05MTCHDROTOR/STATOR ASSY
COND
COND
2466
2964AMDA50335043T24G14STAGE 1 NOZZLE
COND
COND
413013620111022423
18341078159231737GE-L-8074486064T98G01POWER TURBINEMODULE
COND
COND
2466
2437GE-D-0067626035T01G01ACCESSORY MODULE
COND
COND
2466
1824SUSJ20346034T62P13PARTICLESEPARATOR BLOWER
COND
COND
4012
454154641514046T52G39FUEL CONTROL
COND
COND
2466
2850APM331RR4076T64G01POU ASSY-O/S DRAINVALVE
COND
COND
6326
441EMDE06114046T29G13ELECTRICALCONTROL UNIT
COND
COND
24661012049311409
36101268345461554CAO021244046T26G03HISTORY 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 16
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-207925
hr)
2466
3595UDC019634046T25G01COOLER, OIL
COND
COND
5565
0COMH134424046T28G14ANTI-ICE VALVE
COND
COND
14. SIGNIFICANT HISTORICAL DATA
10/29/201012:00:00 AM
1 29 OCT 2010- ENGINE ASSY S/N: GE-E-207925 INSTALLED ON ACFT AT6943.2 ACFT HRS. TTSN: 4165. CUM COUNTS: LCF1=2447, LCF2=11230,TTI=13630, HOURS=4165. H/R(CAO02124) READINGS: LCF1=2592,LCF2=10845, TTI=16193, HOURS=5310. (M. BELFORD 1137), USAACE, FT.
vickie.l.meadows USAACE, FT. RUCKER, AL.
10/1/201112:00:00 AM
1 REMOVED ENGINE SERIAL NUMBER GE-E-207925, W/TTSN: 4591 HRS,FROM AIRCRAFT 8724661 AT 7354.1 ACFT HRS. ENGINE CUMULATIVECOUNTS AT REMOVAL: LCF1 - 2644, LCF2 - 12743, TTI - 13752, OP HRS - 4591.HISTORY RECORDER (S/N:CAO02124) READINGS AT REMOVAL: LCF1 -2789, LCF2 - 12358, TTI - 16315, OP HRS - 5735. REASON FOR REMOVAL:SUSPECTED CRACKED TURBINE BLADE (BIRD STRIKE) (FC - 917).
bryan.w.hollis USAACE LOWE AHP
10/5/201112:00:00 AM
1 REMOVED R/H COMPRESSOR CASE TO INSPECT FOR 1ST STAGECOMPRESSOR BLADE SUSPECTED CRACK. NO DAMGE FOUND, ENGINERETURNED TO SERVICE. ENGINE CUMULATIVE COUNTS:2644/12743/13752/4591. H.R. CAO02124 READINGS: 2789/12358/16315/5735.(AFS533)
dean.a.keirn USAACE FT. RUCKER, AL.
10/5/201112:00:00 AM
2 INSTALLED # 2 ENGINE S/N: GE-E207925 ON ACFT: 8023417 AT 5886 ACFTHRS. ENG CUM CNTS: 2644/12743/13752/4591. H/R S/N: CAO02124:2789/12358/16315/5735.
shelia.d.cook USAACE FT RUCKER,AL.
1/24/201212:00:00 AM
1 REMOVED ECU SN: EMDE0787 W/TTSN: 1453 FROM ENG SN: GE-E-207925 @4649 ENG HRS DUE TO TGT TEMP HIGH. (ENG ACCUM. READINGS: LCF1:2675, LCF2: 12826, TTI: 13803, OP HRS: 4649 )(HIST. REC SN: CAO02124COUNTS: LCF1: 2820, LCF2: 12441, INDEX: 16366, OP HRS: 5793) (ACFT8023417 @ 5938.4 ACFT HRS)
mary.b.hodge USAACE FT. RUCKER, AL
1/24/201212:00:00 AM
2 INSTALLED ECU SN: ECD01231 W/TSN: 4506 ON ENG SN: GE-E-207925 @4649 ENG HRS. (ENG ACCUM. READINGS: LCF1: 2675, LCF2: 12826, TTI:13803, OP HRS: 4649 )(HIST. REC SN: CAO02124 COUNTS: LCF1: 2820, LCF2:
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 16
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-207925
hr)
12441, INDEX: 16366, OP HRS: 5793) (ACFT 8023417 @ 5938.4 ACFT HRS)
mary.b.hodge USAACE FT. RUCKER, AL
5/13/201212:00:00 AM
1 REMOVED ANTI ICE VALVE (SN G7783) TSN 3454 FROM ENG (SN GE-E-207925) CUM CTS: 2764/13196/13849/4848 FOR INTERNAL FAILURE. HIS REC(SN CAO02124) READINGS 2909/12811/16412/5992. INSTALLED ANTI ICEVALVE (SN COMH9545) WITH TSN 849 @ 6136 ACFT HRS.
brandi.n.keener USAACE FT RUCKER, AL
12/15/201212:00:00 AM
0 TURBINE & COM[PRESSOR WHEELS NO CHANGE TSN 253 & SSN 1506, APU1197 TSN & 6651 SSN: METERS READ 285 & 1506 EVENTS
QC00000 HSPS SAN DIEGO, CA
8/15/201312:00:00 AM
1 REMOVED ANTI-ICE VALVE SN: COMH9545 W/TTSN: 1566 FROM ENG SN:GE-E-207925 @ 5565 ENG HRS DUE TO INTERNAL FAILURE. (HR SN:CAO02124 CUM CTS: 3268/15174/16649/6709)(ACFT 8023417 @ 6846.5 ACFT
mary.b.hodge USAACE FT. RUCKER, AL
8/15/201312:00:00 AM
2 INSTALLED ANTI-ICE VALVE SN: COMH13442 W/TSN: 0 ON ENG SN: GE-E-207925 @ 5565 ENG HRS. (HR SN: CAO02124 CUM CTS:3268/15174/16649/6709)(ACFT 8023417 @ 6846.5 ACFT HRS)
mary.b.hodge USAACE FT. RUCKER, AL
8/23/201312:00:00 AM
1 REMOVED ENG SN: GE-E-207925 W/TTSN: 5592 FROM ACFT 8023417 @6871.1 ACFT HRS DUE TO TBO. (ENG CUM CTS: 3139 /15647 /14086 /5592)(HIST REC. SN: CAO02124 CTS = 3284 /15262 /16649 /6736)
mary.b.hodge USAACE FT. RUCKER, AL
8/24/201312:00:00 AM
1 GG ROTOR SN: MRS07162 WITH TSN: 5609 (GG ROTOR CUMULATIVECOUNTS: LCF1-3017, LCF2-13583, TTI-37431, HOURS-5609) REMOVED FROM(GE-E-207925 @ 5592 ENG HOURS) (ENG CUMULATIVE COUNTS: LCF1:3139, LCF2: 15647, TTI: 14086, HOURS: 5592) (H.R. RECORDER (CAO2124)LCF1: 3284, LCF2: 15262, TTI: 16649, HOURS: 6736) FOR "TIME CHANGE"INSTALLED GG ROTOR SN: MRSG3498 WITH TSN: 3212 (GG ROTORCUMULATIVE COUNTS: LCF1: 1511, LCF2: 8199, TTI: 1438, HOURS: 3212)
loletia.v.williams USAACE FT. RUCKER, AL
8/25/201312:00:00 AM
1 ENGINE SN: GE-E-207925 WITH TSN: 5592 (ENG CUMULATIVE COUNTS:LCF1-3139, LCF2-15647, TTI-14086, HOURS-5592) (H.RECORDER SN:CAO02124: LCF1- 3284, LCF2-15262, TTI-16649, HOURS-6736) INSTALLED ON(8023417 @ 6871 AIRCRAFT HOURS)
loletia.v.williams 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 16
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-207925
hr)
5/6/201412:00:00 AM
1 REMOVED ECU SN: ECDO1231 W/TSN: 5888 HRS FROM ENG SN: GE-E-207925@ 6031 ENG HRS. (INTERNAL FAILURE) ENG CUMM. CTS. LCF1: 3328,LCF2: 16518, TTI: 14122, OP HRS: 6031. HIST. REC SN: CAO02124 READINGS:LCF1: 3473, LCF2: 16133, TTI: 16685, OP HRS: 7175. ACFT 8023417 @ 7297.5
frances.j.grace USAACE FT. RUCKER, AL
5/6/201412:00:00 AM
2 INSTALLED ECU SN: EMDE0498 W/TSN: 1015 HRS ON ENG SN: GE-E-207925@ 6031 ENG HRS. ENG CUMM. CTS. LCF1: 3328, LCF2: 16518, TTI: 14122, OPHRS: 6031. HIST. REC SN: CAO02124 READINGS: LCF1: 3473, LCF2: 16133,TTI: 16685, OP HRS: 7175. ACFT 8023417 @ 7297.5 ACFT HRS.
frances.j.grace USAACE FT. RUCKER, AL
6/26/201412:00:00 AM
1 REMOVED ENG SN: GE-E207925, FROM ACFT 8023417, AT 7326 ACFT HRS.HISTORY RECORDER SN: CAO02124, H.R. READINGS: LCF1: 3492, LCF 2:16192, TTI: 16735, OP HRS: 7206.
christina.l.negron USAACE FT RUCKER,AL.
6/26/201412:00:00 AM
2 REMOVED ENG SN: GE-E207925, FROM ACFT 8023417, AT 7326 ACFT HRS.HISTORY RECORDER SN: CAO02124, H.R. READINGS: LCF1: 3492, LCF 2:16192, TTI: 16735, OP HRS: 7206. ENG CUMULATIVE COUNTS: LCF1: 3347,LCF2: 16577, TTI: 14172, OP HRS: 6062. REMOVAL IS DUE TO HOLE INSWIRLFRAME AT THE 7 O'CLOCK POSITION.
christina.l.negron USAACE FT RUCKER,AL.
6/28/201412:00:00 AM
1 REPLACED SWIRL FRAME THIS DATE. ENG CUMULATIVE COUNTS: LCF1:3347, LCF2: 16577, TTI: 14172, OP HRS: 6062.
jeremy.g.strickland USAACE FT. RUCKER, AL.
7/11/201412:00:00 AM
1 ENTERED IN ERROR
UNKNOWN USAACE FT RUCKER,AL
8/14/201412:00:00 AM
1 ENTERED IN ERROR
olivia.d.williams USAACE FT RUCKER,AL
8/14/201412:00:00 AM
2 COLD SECTION S/N GE-C-006115 REMOVED FROM UNINSTALLED ENGINE(GE-E-207925) DUE TO LEAKING FROM SLIP FIT WITH LCF1 2458 LCF2 11381TTI 11825 OP HRS 5297. ENG CUM CTS = LCF1 3352 LCF2 16594 TTI 14182 OPHRS 6067, H/R S/N CAO02124 = LCF1 3498 LCF2 16209 TTI 16745 OP HRS 7211.
olivia.d.williams 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 6 of 16
04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-207925
hr)
8/14/201412:00:00 AM
3 COLD SECTION S/N GE-C-006931 INSTALLED ON UNINSTALLED ENGINEWITH LCF1 1752 LCF2 6463 TTI 14688 OP HRS 3524. ENGINE CUM CTS= LCF13352 LCF2 16594 TTI 14182 OP HRS 6067, H/R S/N CAO02124 READINGS =LCF1 3498 LCF2 16209 TTI 16745 OP HRS 7211.
olivia.d.williams USAACE FT RUCKER,AL
8/22/201412:00:00 AM
1 T700-GE-700 ENG. ASSY INSTALLED ON ACFT 8524465 AT 7416.1 ACFT HRS.WITH ENGNE CUMULATIVE COUNTS - LCF-3352;LCF2-16594; TTI-14182; OPHR-6067. H.R (CAO02124) READINGS = LCF1-3498; LCF2-16209; TTI=16745; OPHE-7211.
janice.m.bruce USAACE FT. RUCKER, AL
7/7/201512:00:00 AM
1 REMOVED ECU S/N: EMDE0498 W/TTSN: 1310 HRS FROM ENGINE S/N GE-E-207925 ON AIRCRAFT 8524465 AT 7653.6 ACFT HRS, REASON FORREMOVAL: CAUSES TGT TO LIMIT LOW 100 DEGREE. INSTALLED ECU S/N:EMDE0611 W/TTSN: 441 HRS ON ENGINE S/N: GE-E-207925 ON SAME ACFTAT SAME ACFT HRS AS LISTED ABOVE. HISTORY RECORDER (S/N:CAO02124) READINGS AT REMOVAL & INSTALLATION: LCF1 - 3602, LCF2 -16660, TTI - 16805, OP HRS - 7470. ENGINE CUMULATIVE CTS AT REMOVAL& INSTALLATION: LCF1 - 3456, LCF2 - 17045, TTI - 14242, OP HRS - 6326.
bryan.w.hollis USAACE FT. RUCKER, AL
2/11/201612:00:00 AM
1 EFFECTIVE THIS DATE, RECEIVED APU S/N: 886019 FOR AN OVERHAULREADINGS AT RECEIPT ARE: HOUR METER UNKNOWN, START METERUNKNOWN, TSN 1197, TSO 254, SSN 6651, SSO 1500. INITIATED NEW FORM.
QC00000 FRC EAST CHERRYPOINT, NC
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 7 of 16
CAO02124
GE-E-2079256035T02G01COLD SECTION MODULEGE-C-006931
7211
3524
16745
14688
16209
6463
3497
1752
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 8 of 16
04A01 6035T02G01 COLD SECTION MODULE GE-C-006931
hr)
35211459764541749
0000NRWA47715056T66G02POWER TAKEOFFDRIVE
COND
COND
35211459764541749
35211459764541749GLB208926035T77G14COMPRESSORROTOR ASSY
COND
COND
35211459764541749
273843883873918FIAID5496035T88P04GAS GEN TURBINESHAFT
15470
11000
35211459764541749
0000WEST48335036T95P01INNER BALANCEPISTON SE
COND
COND
35211459764541749
0000MMTF80416035T79P04COMPRESSORDISCHARGE SE
COND
COND
35211459764541749
3445866171461475GATGH4156035T83P01COMPRESSOR REARSHAFT
8763
5000
35211459764541749
0000VAEFA5655044T07P01NO 3 LABYRINTH
COND
COND
35211459764541749
794711123133843370ASV001805035T57P02VORTEX SPOILER
COND
COND
35211459764541749
84526682047513GATHJ8M85043T04P02TIE ROD,COMPRESSOR
16363
10000
35211459764541749
593823705168322963GATT85384045T08P01RING, SPACERCOMPRESSOR
11270
10000
35211459764541749
0000GLHTP7866055T59P01COMPRESSORIMPELLER
12208
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 9 of 16
04A01 6035T02G01 COLD SECTION MODULE GE-C-006931
hr)
35211459764541749
122945511970544GGAY92023065T21G01OUTPUT SHAFT ASSY
COND
COND
35211459764541749
0000GLHTNAA76032T26G09STAGE 1 BLISK
12208
5000
35211459764541749
0000GLHTPKDL6032T27P08STAGE 2 BLISK
14208
7000
35211459764541749
0000GLHTR0H76038T08P04STAGE 3 & 4 BLISK
14208
7000
35211459764541749
0000GLHTR20D6038T09P04STAGE 5 BLISK
14208
7000
35211459764541749
0000FCABA4446064T35P02NO 3 BALL BEARING
COND
COND
35211459764541749
109014062244549FCAH94746064T15P03NO 4 ROLLER
COND
COND
14. SIGNIFICANT HISTORICAL DATA
1/4/201312:00:00 AM
1 COLD SECTION MODULE RECAPPED ON 02 JAN 13 IAW DMWR 1-2840-248-&CHANGES. FACTORY NEW FUEL INJECTORS INSTALLED PER DMWR ATCOLD SECTION MODULE TSN 3524
CP5495 CCAD CC.TX
8/14/201412:00:00 AM
1 COLD SECTION INSTALLED ON UNINSTALLED ENGINE WITH LCF1 1752LCF2 6463 TTI 14688 OP HRS 3524. ENGINE CUM CTS= LCF1 3352 LCF2 16594TTI 14182 OP HRS 6067, H/R S/N CAO02124 READINGS = LCF1 3498 LCF216209 TTI 16745 OP HRS 7211. I
olivia.d.williams USAACE FT RUCKER,AL
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 10 of 16
CAO02124
GE-C-0069313065T21G01OUTPUT SHAFT ASSYGGAY9202
7211
1232
16745
4642
16209
1979
3497
547
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
EH-60A
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 11 of 16
04A01G 3065T21G01 OUTPUT SHAFT ASSY GGAY9202
hr)
122945511970544
0000FCAV41216064T34P02NO 1 BALL BEARING
COND
COND
122945511970544
26251819889481702FCAD65405121T46P02NO 2 ROLLER
COND
COND
14. SIGNIFICANT HISTORICAL DATA
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 12 of 16
CAO02124
GE-E-2079256055T20G05MTCHD ROTOR/STATORMRSG3498
6736
3212
16649
1438
15262
8199
3284
1511
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 13 of 16
04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRSG3498
hr)
3212143881991511
126549643376634GATH91AR6064T85P01STAGE 1 TURBINE
10471
5000
3212143881991511
3212143881991511GGAT24506039T57G24STATOR GASGENERATOR
COND
COND
3212143881991511
77021431456371GATHF8ME6064T86P01STAGE 2 TURBINE
10966
5000
3212143881991511
125882703828600PAMEU7846064T81P01STG 1 FWD COOLINGPLATE
10478
5000
3212143881991511
77021431456371GFF5AL5F6064T82P01STG 1 AFT COOLINGPLATE
10966
5000
3212143881991511
0000GFF5DHD06064T83P01STG 2 FWD COOLINGPLATE
11736
5000
3212143881991511
294291384117GFF5CH266064T84P02STG 2 AFT COOLINGPLATE
11442
5000
3212143881991511
3212143881991511GGAG34986039T54G13ROTOR GASGENERATOR
COND
COND
14. SIGNIFICANT HISTORICAL DATA
1/7/201312:00:00 AM
1 TB1-2840-248-20-2 DTD 30 JUN 94 C/W AT CCAD AND LIFE LIMITS C/W I/A/WTM1-2840-248-23, TABLE 1-10 1JUNE99 "STAGE ONE AND TWO GG BLADESETS CONTAIN NEW OR USED BLADES THAT HAVE ALWAYS BEEN RUNWITH DAMPERS"
ORTIZ CCAD CORPUS CHRISTI
8/24/201312:00:00 AM
1 GG ROTOR WITH TSN: 3212 (GG ROTOR CUMULATIVE COUNTS: LCF1: 1511,LCF2: 8199, TTI: 1438, HOURS: 3212)INSTALLED ON (GE-E-207925 @ 5592ENG HOURS) (ENG CUMULATIVE COUNTS: LCF1: 3139, LCF2: 15647, TTI:14086, HOURS: 5592) (H.R. RECORDER (CAO2124) LCF1: 3284, LCF2: 15262,TTI: 16649, HOURS: 6736)
loletia.v.williams 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 14 of 16
04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRSG3498
hr)
REVERSE OF DA FORM 2408-16-1, OCT 1991
Page 15 of 16
CAO02124
GE-E-2079256064T98G01POWER TURBINE MODULEGE-L-807448
5274
1834
16183
10781
10717
5923
2568
1737
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 16 of 16
04A03 6064T98G01 POWER TURBINE MODULE GE-L-807448
hr)
18311067859171735
18311067859171735GGAP39105043T75G07POWER TURBINEROTOR
COND
COND
18311067859171735
111339402615720GATH7RC66038T32P01STAGE 3 TURBINE
9158
5000
18311067859171735
0000GATHAT9D6038T34P05STAGE 4 TURBINE
10271
5000
18311067859171735
89631603836468GATHJ2F75125T92G01POWER TURBINESHAFT
9375
5000
18311067859171735
3851775526140FCAH46335034T27P02NO 5 ROLLER
COND
COND
18311067859171735
6588127726FCAN10026064T36P02NO 6 BALL BEARING
COND
COND
14. SIGNIFICANT HISTORICAL DATA
7/9/201012:00:00 AM
1 09JUL10 CCAD POWER TURBINE REPAIRED 08JUL10 IAW DMWR 1-2840-248& CHANGES AND RECAPPED DTD 03DEC01. /S/M. BENAVIDES. AIRCRAFTDATA TECHNICIAN.
vickie.l.meadows CCAD NO LOCATION
10/5/201112:00:00 AM
1 INSTALLED # 2 ENGINE S/N: GE-E207925 ON ACFT: 8023417 AT 5886 ACFTHRS. ENG CUM CNTS: 2644/12743/13752/4591. H/R S/N: CAO02124:2789/12358/16315/5735.
shelia.d.cook 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=
7
7
6658
7
1198
1
886019
APU
116305-302 8524465
3 7116305-302 886019AUXILIARY POWER UNIT 6658
15B 2835013692818
60006000
starts
RC RC4502902 SIF5727WHEEL, COMPRESSOR 6651 0
15B02B 2835014596002
60006000
starts
RC RC4503991 T411WHEEL, TURBINE 6651 0
15B03 2835013638089
60006000
starts
8. SIGNIFICANT HISTORICAL DATA
11-Feb-2016 1 EFFECTIVE THIS DATE, RECEIVED APU S/N: 886019 FOR AN OVERHAUL READINGS AT RECEIPT ARE:HOUR METER UNKNOWN, START METER UNKNOWN, TSN 1197, TSO 254, SSN 6651, SSO 1500. INITIATEDNEW FORM.
QC00000 FRC EAST CHERRY POINT, NC
07-Jul-2016 1 APU S/N: 886019, WAS OVERHAULED AND PROCESSED IN ACCORDANCE WITH DMWR 1-2835-209 ASSUPPLEMENTED BY NAVAIRDEPOT MCAS CHPT LES CP23-0-LL-173, REV C AND IS SERVICEABLE FORINSTALLATION AND CONTINUED SERVICE. THE FOLLOWING MAINTENANCE WAS PERFORMED.INSTALLED: NEW COMPRESSOR WHEEL S/N: SIF5727: NEW TURBINE WHEEL S/N: T411 AND FUELCONTROL S/N: 5-80-22. NEW METERS WERE INSTALLED AT THIS OVERHAUL. READINGS ATCOMPLETION: HOUR METER, 001, START METER 0007, TSN 1198, TSO 0001, SSN 6658, SSO 007.
AG3612 FRC EAST CHERRY POINT, NC
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
8524465HELICOPTER, 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 06 Sep 201714TM 1-1520-237-23&P14 DAY FLYABLE STORAGEENGINE RUN UP
23 Aug 2017D
A092 11 Sep 201730TM 11-6140-203-23 P30 DAY SLAB BATTERYINSPECTION (D8565/11-1)
12 Aug 2017D
A103 22 Aug 201730TM 1-1500-344-23AIRCRAFT WASH DUE 23 Jul 2017D
A110 8385.240TM 1-1520-237-PMSPMS 40 HOUR INSPECTION (ESMONLY)
8345.2H
A115 22 Sep 201730TM 1-1520-237-23&PLUBE REQUIRMENTS (ESMONLY)
23 Aug 2017D
A115 8385.240TM 1-1520-237-23&PLUBE REQUIRMENTS (ESMONLY)
8345.2H
A116 8502.1480H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE (ESM ONLY)
8022.1H
A116 26 Jul 201712H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE (ESM ONLY)
26 Jul 2016M
A117 8502.1480H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 8022.1H
A117 26 Jul 201712H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 26 Jul 2016M
A118 8825.2480H-60-10-AMAM-11MAIN GEARBOX OIL SAMPLE -ALL EXCEPT 073,074,075
8345.2H
A160 23 Sep 201790TM 1-1520-237-23&PESM 90 DAY CORROSIONINSPECTION
25 Jun 2017D
A210 8382.3120TM 1-1520-237-23&P120 HOUR INSPECTIONREQUIREMENTS (ESM ONLY)
8262.3H
A211 8792480H-60-10-AMAM-11APU OIL SAMPLE 8312H
A211 26 Jul 201812H-60-10-AMAM-11APU OIL SAMPLE 26 Jul 2017M
A213 8384.6120TB 1-1520-237-20-266ENGINE COMPRESSORCLEANING (ESM ONLY)
8264.6H
A295 8379.6360TM 1-1520-237-23&PSTABILATOR ACTUATOR ASSYLUBE (ESM ONLY)
8019.6H
A298 8815.5480TM 1-1520-237-23&PLUBRICATE TAIL WHEELBEARINGS
8335.5H
A298 23 Jul 201812TM 1-1520-237-23&PLUBRICATE TAIL WHEELBEARINGS
23 Jul 2017M
A299 8780.7480TM 1-1520-237-23&PLUBRICATE SWASHPLATE 8300.7H
A299 06 Jul 201812TM 1-1520-237-23&PLUBRICATE SWASHPLATE 06 Jul 2017M
A440 8139.6480TM 1-1520-237-23&PCLEAN TAIL WHEEL LOCKPIN 7659.6H
A470 92251500TM 1-1520-237-23&PREPLACE NUMBER TWOCROSSFEED VALVE
7725H
A471 8380.12160TM 1-1520-237-23&PREPLACE T/R SHAFT SUPPORTBEARINGS (FWD)
6220.1H
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
8524465HELICOPTER, 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.
A472 8380.12160TM 1-1520-237-23&PREPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)
6220.1H
A473 8380.12160TM 1-1520-237-23&PREPLACE T/R SHAFT SUPPORTBEARINGS (AFT)
6220.1H
A476 9998.65000TM 1-1520-237-23&PREPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS
4998.6H
A477 13030.65000TM 1-1520-237-23&PREPLACEMENT OF STABILATORACTUATOR BOLTS
8030.6H
A480 9998.65000TM 1-1520-237-23&PREPLACE PIVOT BOLT 70400-08159-101,102,103,104
4998.6H
A485 9998.65000TM 1-1520-237-23&PREPLACE BELLCRANK BOLT70400-08159-105,106,107,108
4998.6H
A496 23 Nov 2017180TM 1-1520-237-23&PCF3BR FIRE EXTINGUISHERWEIGHT TEST INSPECTION
27 May 2017D
A501 16 Jan 20186TM 1-1520-237-23&PMAIN ROTOR BLADE SPARPRESSURE CHECK
16 Jul 2017M
A502 22 Feb 2018180TM 1-1520-237-23&PINSPECT AND TEST GROUNDRECEPTACLE IAW TM 1-1500-204-23
26 Aug 2017D
A530 27 Sep 201712DA PAM 738-751AIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)
27 Sep 2016M
A532 03 Dec 201712TM 1-1500-204-23-4COMPASS SWING / RMI SWING 03 Dec 2016M
A533 06 Jan 201812TM 1-1520-237-23&PPITOT STATIC SYSTEMINSPECTION
06 Jan 2017M
A534 28 Jan 201812TM 1-1500-204-23-1FIRST AID KIT INSPECTION 28 Jan 2017M
A538 08 Sep 201712TM 1-1520-237-23&PFAT/OAT GAUGEINSPECTION/TEST
08 Sep 2016M
A553 01 Oct 201712AR 95-1ANNUAL WEIGHT AND BALANCEINVENTORY (365-1)
01 Oct 2016M
A580 02 Mar 201924TM 11-6140-203-23 PRETURN SLAB TO AVIM FORCAPACITY CHECK (EVERY 24MONTH)
02 Mar 2017M
A621 17 Oct 201824AR 95-1AIRCRAFT WEIGHING CLASS 1 17 Oct 2016M
A625 06 May 202160TM 11-6140-203-23 PREPLACEMENT OF SLABBATTERY (SLAB)
06 May 2016M
A630 01 Aug 2018114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #1,CARTRIDGE, DODIC MH92
01 Feb 2009M
A633 01 Dec 2019114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #1,CARTRIDGE DODIC MH92
01 Jun 2010M
A638 01 Dec 2019114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #2,CARTRIDGE DODIC MH92
01 Jun 2010M
A640 01 Aug 2018114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE CARTRIDGE,31512AS105, 30903824-1
01 Feb 2009M
A648 09 Feb 2018120TM 1-1520-237-23_PREPLACE T/R SPRING CAPSULEASSY
09 Feb 2008M
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
8524465HELICOPTER, 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.
A660 01 Dec 201772TB 9-1300-385REPLACE THRUSTEREMERGENCY RELEASE CARGOHOOK, MJ20
01 Dec 2011M
A665 22 Jan 201948H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215
22 Jan 2015M
A670 27 Jun 202048TM 1-1520-237-23&PCABIN TUB INSPECTION 27 Jun 2016M
A675 27 Jul 201748TM 1-1520-237-23&PFLIGHT CONTROL RODSINSPECTION
27 Jul 2013M
A695 8379.6720H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION
7659.6H
A695 06 Jan 202048H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION
06 Jan 2016M
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-306485
3. ENGINE SERIAL NUMBER2. ENGINE MODEL1. NOMENCLATURE
Page 1 of 1
20-May-2014 8524407 #2 ENG REPLACED6000 99 97 198126694 846
04-Oct-2014 8524465 ENG REPLACED5000 105 103 197.396901 845
09-Jul-2015 8524465 ECU REPLACED.5000 100 97 198.7207155 847
19-Jan-2016 8524465 MAX POWER CK PMS 25000 104 104 197.587166 843
06-Mar-2017 8524465 ENG REMOVAL /REINSTALLATION
6000 102 100 196.667683 845
17-May-2007 8724671 MAX PWR CHECK6000 92 87 197.6303787 843
07-Aug-2007 8724671 MAX PWR CHECK6000 91 92 0.9998.2224395 845
09-Aug-2007 8724671 120 HR INSP6000 91 92 0.9998.2223812 725
23-Sep-2008 8724671 120 HR INSP6000 94 94 198.1164027 844
18-Jan-2009 8724671 ENG INSTALLATION5000 106 105 197.634301 839
05-Feb-2009 8724671 REPLACE #1 ENG ECU4000 110 110 198.1-24314 848
30-May-2009 8724671 REPLACE #1 ENG ECU4000 104 103 198.3174476 846
05-Apr-2010 8724671 720 HOUR6000 97 97 197.9145021 868
05-Jun-2010 8724671 REPLACED # 1 ENGINE4000 100 100 198.5215625 848
12-Apr-2011 8826017 ENG REPLACED2000 108 102 198.4235580 851
09-Jul-2011 8826017 POST 7204000 97 97 198.9245643 846
09-Oct-2012 8826017 POST PHASE 720 HR PMI4000 104 102 198.3187219 849
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-207925
3. ENGINE SERIAL NUMBER2. ENGINE MODEL1. NOMENCLATURE
Page 1 of 1
05-Oct-2011 8023417 COLD SECTION REPLACED5000 106 100 198.8144591 849
01-Dec-2011 8023417 720 HR INSP4000 109 105 198124606 848
25-Jan-2012 8023417 ECU REPLACEMENT4000 110 104 199.1154649 849
10-May-2013 8023417 POST PHASE5000 107 100 198.7145323 842
26-Aug-2013 8023417 GG ROTOR REPLACEMENT4000 110 102 199165592 846
07-May-2014 8023417 ECU REPLACED5000 105 99 199166031 843
31-Jul-2014 8023417 POST PHASE4500 108 100 199106062 844
04-Oct-2014 8524465 ENG REPLACED5000 107 103 198.896068 839
09-Jul-2015 8524465 ECU REPLACED.5000 101 97 199.2206326 845
19-Jan-2016 8524465 MAX POWER CHECK PMS 25000 106 104 198.286339 843
15-Apr-2004 8724661 MAX POWER CHECK PMS 25000 103 103 197.293717 845
21-Sep-2006 8724661 RESET HIT BASELINE2500 109 108 197.7172545 850
29-Jan-2007 8724661 MAX POWER CHK6000 103 103 195.804435 844
29-Jan-2007 8724661 NO REMARKS6000 103 103 195.804435 844
03-Jun-2009 8724661 HIT CK WITHIN 53000 104 104 198.1214872 841
10-Aug-2009 8724661 REPL. ECU2000 103 103 198.9284935 846
04-Jan-2010 8724661 ENGREINSTALLED/ACCEPTANCE
5000 108 105 195.7-34993 844
04-Apr-2010 8724661 ENGINE REINSTALLATION4000 99 102 0.9697.3175121 844
09-Jul-2010 8724661 NEW ENG. INSTL.4000 103 98 198.8244012 848
19-Mar-2011 8724661 720 HR PHASE.4000 110 104 198.5154248 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
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
17258 SESI
2. ORGANIZATION
CSGLD-1052
REQUIREMENT CONTROL SYMBOL(Julian)1. PERIOD ENDING DATE
Page 1 of 2
1GE-E-306098 CAO0194574322864113503418488908424019
1GE-E-306098 CAO0194574322864113503418488908424019
2GE-E-307153 ECD008365764327709130330788908424019
2GE-E-307153 ECD008365764327709130330788908424019
1GE-E-306374 ECD01949417716436515124995458424028
2GE-E-306952 ECD019667862765116845308495458424028
1GE-E-207925 CAO0212481921685519691392883368524465
1GE-E-207925 CAO0212481731685519699392983378524465
1GE-E-207925 CAO0212481821685619767393483458524465
1GE-E-207925 CAO0212481821685619767393483458524465
2GE-E-306485 CAO0152176651484216722396283368524465
2GE-E-306485 CAO0152176661484216727396383378524465
2GE-E-306485 CAO0152176751484716755396883458524465
2GE-E-306485 CAO0152176751484716755396883458524465
1GE-E-306045 ECD009787442225516194234591708524472
1GE-E-306045 ECD009787442225516194234591708524472
1GE-E-306045 ECD009787442226416194234791708524472
1GE-E-306045 ECD009787442226416194234791708524472
1GE-E-306045 ECD009787442226416194234791708524472
2GE-E-307728 ECD025175491743012723249291708524472
2GE-E-307728 ECD025175491743012723249291708524472
2GE-E-307728 ECD025175491743012723249491708524472
2GE-E-307728 ECD025175491743012723249291708524472
2GE-E-307728 ECD025175491743012723249291708524472
1GE-E-307290 CAO0216182504322722310366994498624569
1GE-E-307290 CAO0216182504322722310366994498624569
1GE-E-307290 CAO0216182534322722312367194518624569
1GE-E-307290 CAO0216182544322722313367294538624569
1GE-E-307290 CAO0216182584322722314367394578624569
1GE-E-307290 CAO0216182604322722314367394598624569
1GE-E-307290 CAO0216182654322722317367694638624569
2GE-E-306644 CAO018044116406294911636194498624569
2GE-E-306644 CAO018044116406294911636194498624569
2GE-E-306644 CAO018044316406294941636394518624569
2GE-E-306644 CAO018044416406294981636494538624569
2GE-E-306644 CAO01804481640629503636694578624569
2GE-E-306644 CAO01804511640629506636794598624569
2GE-E-306644 CAO01804551640629511636994638624569
1GE-E-207306 ECD0075672432600512930335186748624574
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
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
17258 SESI
2. ORGANIZATION
CSGLD-1052
REQUIREMENT CONTROL SYMBOL(Julian)1. PERIOD ENDING DATE
Page 2 of 2
2GE-E-306258 ECD022906673953916496292286748624574
1GE-E-306845 ECD0132058931647719774369095988724659
2GE-E-306963 CAO0137679322577320800383295988724659
1GE-E-306153 CAO0167487302118020103451387028724667
2GE-E-307087 CAO0065381861134424520416187028724667
1GE-E-763887 LMDH97353082143916611176424250427019
2GEE767331 LMDH2438238794235206126324250427019
1GE-E-763650 LMDH933741871873610198202164097923296
2GE-E-955158 LMDH280734801215311036213364097923296
1GEE762410C LMDH941729146986225067298123553
2GEE761637C ECDH646128956255720367298123553
1GE-E-903226 LMDH615310693313243049143158123571
2GE-E-903287 LMDH621610512136239351043158123571
1GE-E-767053 LMDH9966178153313489103860858123607
1GE-E-306301C 12322647185856662558223687
2GEE991019 LMDH40868252426127233762558223687
1GEE767013C 27992482224243638223748
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
0
480
7662.6
8524465 2372.2 6940
e. ACFT HRS INSTALLEDc. TIME SINCE NEW OR OVERHAULc. SERIAL NUMBER
EH-60A A005-03106 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
anthony.s.speigner03-Sep-2013NORMALROUTINE0.0967694028-Aug-2013
anthony.s.speigner20-Feb-2014NORMALROUTINE240.01207718019-Feb-2014
frances.j.grace07-Jan-2015NORMALROUTINE602.61569.67542.607-Jan-2015
christina.l.negron26-Jan-2016ABNORMALROUTINE117.01686.67659.608-Jan-2016
brian.k.dow29-Jan-2016NORMALROUTINE3.01689.67662.628-Jan-2016
brian.k.dow28-Jul-2016NORMALROUTINE359.52049.18022.126-Jul-2016
08 JAN 16- ROUTINE, POST 720 HR PHASE. CN4192 ABNORMAL RESULT FOR WATER. DRAIN FLUSH AND RESAMPLE AFTER NEXT FLIGHT CYCLE. 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
480
8077
8524465 4775.2 7300
e. ACFT HRS INSTALLEDc. TIME SINCE NEW OR OVERHAULc. SERIAL NUMBER
EH-60A A265-01063 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
frances.j.grace13-Jun-2014NORMALBASELINE0.03730730013-Jun-2014
frances.j.grace07-Jan-2015NORMALROUTINE242.63972.67542.607-Jan-2015
christina.l.negron26-Jan-2016ABNORMALROUTINE117.04089.67659.608-Jan-2016
brian.k.dow29-Jan-2016NORMALROUTINE3.04092.67662.628-Jan-2016
brian.k.dow28-Jul-2016NORMALROUTINE359.54452.18022.126-Jul-2016
brian.k.dow04-Oct-2016NOT_TESTEDOTHER0.34507807704-Oct-2016
brian.k.dow28-Oct-2016NORMALBASELINE0.34507.38077.326-Oct-2016
08 JAN 16- ROUTINE, POST 720 HR PHASE. CN4192 ABNORMAL RESULT FOR WATER. RESAMPLE AFTER NEXT FLIGHT CYCLE. CN491204 OCT 16 - OIL DRAINED. NO SAMPLE TAKEN. USAACE FT. RUCKER, AL.BD011103
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
480
7662.6
8524465 2398.2 7138
e. ACFT HRS INSTALLEDc. TIME SINCE NEW OR OVERHAULc. SERIAL NUMBER
EH-60A A00603398 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
anthony.s.speigner22-Jan-2014NORMALBASELINE0.01191713821-Jan-2014
anthony.s.speigner20-Feb-2014NORMALROUTINE42.01233718019-Feb-2014
frances.j.grace07-Jan-2015NORMALROUTINE404.61595.67542.607-Jan-2015
christina.l.negron26-Jan-2016ABNORMALBASELINE2.51712.67659.608-Jan-2016
brian.k.dow29-Jan-2016NORMALROUTINE3.01715.67662.628-Jan-2016
brian.k.dow28-Jul-2016NORMALROUTINE359.52075.18022.126-Jul-2016
08 JAN 16- BASELINE. ROUTINE POST 720 HOUR PHASE. CN4192. ABNORMAL RESULT FOR WATER. DRAIN FLUSH AND RESAMPLE AFTER NEXT FLTCYCLE. CN4912
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
480
8055.4
8524465 578 0
e. ACFT HRS INSTALLEDc. TIME SINCE NEW OR OVERHAULc. SERIAL NUMBER
EH-60A 886019 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
brian.k.dow25-Aug-2016NORMALBASELINE24.8258055.423-Aug-2016
brian.k.dow08-Aug-2017NORMALROUTINE256.6281.6831206-Aug-2017
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
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
AFT BELLCRANK 8524465F345105121. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
19-Dec-2013 FT
christina.l.negron19-Aug-2014
2.0USAACE, FT.RUCKER, AL
AUTHORIZED USE OF RETAININGCOMPOUND CALLED OUT IN DMWT(8030-01-025-1692) IN BEARINGREPLACEMENT.
MEC 176646MWO:
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 8524465COMH73301. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
22-Jun-2011 OM
loletia.v.williams29-Jun-2011
2.0USAACE, FT.RUCKER, AL
ANTI-ICE / START BLEED VALVEACTUATOR SHAFTS
H-60-11-ASAM-11MWO:
Priority Mnt Level
05-Sep-2012 OM
vickie.l.meadows28-Sep-2012
5.0USAACE, FTRUCKER, 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
(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 8524465 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE
Condition Change Components Page 1 of 7
COND COND
156001113021502C12D
00TAIL CONE FITTING B497-0028470219-05001-044 CCCC
COND COND
162001231183103A01
07984FWD FIXED GEAR SHOCK BEM104770250-12051-045 CCCC
COND COND
162001231183103A01
02268FWD FIXED GEAR SHOCK IA0057670250-12051-045 CCCC
COND COND
162001421089003B01
26258162SHOCK ABSORBER (TAIL) BMC82770250-13101-044 CCCC
COND COND
165001285302405A01Z
49447695DAMPER ASSY, M/R A106-1032770106-08100-046 CCCC
COND COND
165001285302405A01Z
17908243DAMPER ASSY, M/R A1061431870106-08100-046 CCCC
COND COND
165001285302405A01Z
03116DAMPER ASSY, M/R R106-0110470106-08100-046 CCCC
COND COND
165001285302405A01Z
36868012DAMPER ASSY, M/R WG1060285170106-08100-046 CCCC
COND COND
531501537465205A02H
07269BLADE PIN, SOLID B941-2920070103-08108-041 CCCC
COND COND
531501537465205A02H
07269BLADE PIN, SOLID B941-2920670103-08108-041 CCCC
COND COND
531501537465205A02H
07660BLADE PIN, SOLID B941-3174870103-08108-041 CCCC
COND COND
531501537465205A02H
24347660BLADE PIN, SOLID B9410922670103-08108-041 CCCC
COND COND
531501537465205A02H
04805BLADE PIN, SOLID B9411676670103-08108-041 CCCC
COND COND
531501537465205A02H
06940BLADE PIN, SOLID B9412299470103-08108-041 CCCC
COND COND
531501537465205A02H
07930BLADE PIN, SOLID B9413504370103-08108-041 CCCC
COND COND
531501537465205A02H
07930BLADE PIN, SOLID B9413701370103-08108-041 CCCC
COND COND
161501199764605A03A
04184SWASHPLATE ASSY 015152-193570104-08000-050 CCCC
COND COND
161501503311506A
37307300MAIN TRANSMISSION MODUL A265-0106370351-08100-076 CCCC
COND COND
161501078571806A11
24931488ACCESSORY MODULE A258-0163070351-08080-043 CCCC
COND COND
161501078571806A11
00ACCESSORY MODULE A258-0214770351-08080-043 CCCC
COND COND
161501230621806E
28091488INPUT MODULE A264-0037970351-08001-046 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 8524465 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE
Condition Change Components Page 2 of 7
COND COND
161501230621806E
00INPUT MODULE A264-0215170351-08001-046 CCCC
COND COND
168001074515206F
9676940INTERMEDIATE GEARBOX A005-0310670357-06300-042 CCCC
COND COND
161501376508906G01
11917138TAIL ROTOR GEARBOX ASSY A0060339870358-06600-046 CCCC
COND COND
161501524780506H04
06580DRIVESHAFT ASSY ENGINE C8450888770361-08014-041 CCCC
COND COND
161501524780506H04
06940DRIVESHAFT ASSY ENGINE C8450949670361-08014-041 CCCC
COND COND
161501081277506H06
00SHAFT ASSY, T/R DRV SEC 1 A271-0094970361-03001-045 CCCC
COND COND
161501158951706H08
3597660SHAFT ASSY, T/R DRV SEC 2 WG300400015670361-03009-047 CCCC
COND COND
161501158952206H09
04805SHAFT ASSY, T/R SEC 3,4,5 WG30024-0016270361-05001-051 CCCC
COND COND
161501158952206H09
04805SHAFT ASSY, T/R SEC 3,4,5 WG30024-0062070361-05001-051 CCCC
COND COND
161501158952206H09
07660SHAFT ASSY, T/R SEC 3,4,5 WG300240032970361-05001-051 CCCC
COND COND
161501083295306H11
00SHAFT ASSY, T/R DRV SEC 6 A273-0090070361-05002-045 CCCC
COND COND
161501158578806H12
00SHAFT ASSY, T/R DRV SEC 7 A274-0101870361-06002-047 CCCC
COND COND
432001207722807A01
20908245PUMP MODULE ASSY, HYDR 246628A53023-06 CCCC
COND COND
432001207722807A01
8505479PUMP MODULE ASSY, HYDR 217966ABR70652-02300-050 CCCC
COND COND
432001207722807A01
9646940PUMP MODULE ASSY, HYDR 43238170652-02300-050 CCCC
COND COND
481001102247307B05A
05256VALVE, SOLENIOD 165103213850-3-1 CCCC
COND COND
481001102247307B05A
07709VALVE, SOLENIOD 239773213850-3-1 CCCC
COND COND
165001222431607B11
14386671ACCUMULATOR 8110170A3197170-5 CCCC
COND COND
168001604175408B20
5007660PANEL INDICATOR (PDU) 11151006848-50 CCCC
COND COND
168001342049608B20
03092PANEL INDICATOR (PDU) 524770450-01043-124 CCCC
COND COND
611501114969609A01
02631GENERATOR 84A173328B302-8-DM 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 8524465 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE
Condition Change Components Page 3 of 7
COND COND
611501114969609A01
23916200GENERATOR H84170550-02031-111 CCCC
COND COND
161501260074911C21
07660MIXER ASSEMBLY 438222070400-02300-046 CCCC
COND COND
168001261204411D25
24648031STABILATOR ACTUATOR C292-0778570400-06641-117 CCCC
COND COND
168001571757811D25
08031STABILATOR ACTUATOR 1958DL2155M31MOD1 CCCC
COND COND
599601316274311D26
04416STABILATOR AMPLIFIER A930-0350970902-02001-048 CCCC
COND COND
599601316274311D26
04417STABILATOR AMPLIFIER A930-0387470902-02001-048 CCCC
COND COND
299501496368615A04
2408337ENGINE SEQUENCING UNIT 36574504587 CCCC
COND COND
584101245909019E05A
7927662RECEIVER-TRANSMITTER, R 243BSM-C-967292 CCCC
COND COND
584101245909319E05C
7927662INDICATOR,HEIGHT 129NA3060591 CCCC
COND COND
660501503528419E06A
07359ATTITUDE HEADING REFERE 1627765100-20 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 8524465 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE
Time Change Components Page 4 of 7
20000 19998
156001081924402C15J
62226220TAIL PYLON FITTING A4860080270209-06051-043 RCRC
5100 11865
161501450483405A01A
06765HUB, M/R ROTOR ASSY D3080007370103-08112-047 RCRC
6400 9988
161501442692605A01I
40727660MAIN ROTOR SPINDLE ASSY A001-0519770102-08200-069 RCRC
14000 13961
161501074515105A01L
20241985MAIN ROTOR SHAFT EXTEND C286-0044970351-08186-043 RCRC
13000 13000
161501127738805A01T
55125512BIFILAR, M/R ROTOR ASSY A327-0111570107-08400-046 RCRC
12000 11195
161501083681206G01B
56104805O/B RETENTION PLATE (T/R) A257004670102-11101-042 RCRC
2520 9460
414001329342806H23
25206940FAN AXIAL D5120151370361-03005-107 01
13000 14429
156001129125607A24
62837712SAS ACTUATOR B1120779170410-02500-049 RCRC
13000 18176
156001129125607A24
24667642SAS ACTUATOR C1120022970410-02500-049 RCRC
13000 19037
156001129125607A24
16257662SAS ACTUATOR C1125196170410-02500-049 RCRC
2160 9101
161501141753211C23
12207660T/R PITCH CHANGE SHAFT 233-0482770400-06100-042 7192
24400 30408
165001143122611D01
14087416SERVO, PRIMARY MAIN ROT B303-11135274000-1031 RCRC
24400 30644
165001143122611D01
21018345SERVO, PRIMARY MAIN ROT B303-1555370410-02820-054 RCRC
24400 26749
165001143122611D01
45916940SERVO, PRIMARY MAIN ROT B3030183170410-02820-054 RCRC
13000 18227
1560011589685 usaace11D04
30188245AFT BELLCRANK F3451051270400-08102-045 RCRC
17000 17623
156001164416111D05
0623AFT TIE ROD SUPT FITTING A391-0096670400-08112-045 RCRC
2200 8780
168001164416011D06
06580AFT TIE ROD ASSY M392-1056470400-08111-042 RCRC
4400 12645
1560012868870 usaace11D07
08245AFT BELLCRANK SPT ASSY 3900308070400-08117-049 RCRC
11000 18300
304001287243811D08
07300LATERAL SWASHPLATE LINK 151520456170400-08151-061 RCRC
11000 17220
168001221286311D09
06220LATERAL SERVO BELLCRAN F3370402470400-08166-041 RCRC
11000 13928
168001158965311D11
50367964AFT WALKING BEAM C3460007870400-08104-048 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 8524465 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE
Time Change Components Page 5 of 7
4600 11900
156001289269711D13
07300LEFT TIE ROD ASSY 3440268570400-08115-046 RCRC
3500 10800
156001296948611D14
07300RIGHT TIE ROD ASSY 2880091870400-08114-051 RCRC
15000 21220
168001158965211D15
06220FORWARD BELLCRANK 152370400-08101-046 RCRC
5600 13845
1560012212619 usaace11D16
08245FWD BELLCRANK SPT ASSY B3670906570400-08162-042 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 6 of 7Time Change Components
7. SIGNIFICANT HISTORICAL DATA
11-Feb-1994 1 11 FEB 94- T/R BALANCE TO.13 IPS FOR REMOVAL/ REINSTALLATION 518.5 A/CHRS.
28-Aug-1998 2 28 AUG 98- REPLACEMENT TIME IN BLOCK 'K' OF 1489 A/C HRS IS FOR THESPINDLE NUT SEE DA FORM 2408-16 FOR EACH SPINDLE. SSG KURTIAK C.CO.10TH AVN REGT (AVIM) FT. DRUM N.Y 13662
28-Aug-1998 3 28 AUG 98- T/R BALANCE TO .13 IPS FOR REMOVAL/REINSTALLATION PNS2. SSGKURTIAK C. CO 10TH AVN REGT (AVIM) FT. DRUM, N.Y. 13602.
13-Apr-2001 4 13-APR-01: ALL ENTRIES CONVERTED TO ELAS AUTOMATED LOGBOOK 3000HRS I/A/W AVSCOM LTR DTD 23-JAN-91 FOR FT. RUCKER TRAINING FLEET ONLY.DK1063, R/SPEC; USAAVNC, FT. RUCKER, AL
01-Jun-2004 5 01 JUN 2004 - 2408-16 INITIATED I/A/W UH-60-MIM-04-006/007. AFS146, JH5095,REC/SPEC, USAAVNC, FT. RUCKER, AL.
04-Aug-2010 6 04-AUG-10- LEFT TIE ROD S/N E344-00254 MUST BE REMOVED FROM SERVICE IFREMOVED PRIOR TO 14000 ACFT HRS OR 14JUL12. T. POLLARD, 1634,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 7 of 7Condition Change Components
7. SIGNIFICANT HISTORICAL DATA
01-Jun-2004 7 01 JUN 2004 - 2408-16 INITIATED I/A/W UH-60-MIM-04-006/007. AFS146, JH5095,REC/SPEC, USAAVNC, FT. RUCKER, AL.
APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
CONTROL HORN ASSY 8524465A241-155451. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
10-Dec-1998 OM
mae.p.belford02-May-2007
0.5USAAWC, FT.RUCKER, AL(JT0967)
ALL H-60 SERIES AIRCRAFT,INSPECTION AND REVISEDRETIREMENT LIFE OF MAIN ROTORPITCH HORNS, P/N 70102-08111-047
UH-60-99-ASAM-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
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
FAN AXIAL 8524465D512015131. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
22-Dec-2015 FM
tammy.k.murphy22-Dec-2015
0.5USAACE FTRUCKER, AL
AUTHORIZATION TO INSTALLPEELABLE SHIMS BETWEEN FANAND FORWARD SUPPORT
F307262MWO:
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
(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 70361-03005-107 D51201513 06H234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE
Page 1 of 2
2520 9460
311001127300506H23A
02520BEARING, AXIAL FAN 7732210SFFC3 RCRC
2520 9460
311001127300506H23A
02520BEARING, AXIAL FAN 7733210SFFC3 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
09-Aug-2013 1 INSTALLED FAN AXIAL SN: D51201513, ON ACFT 8524465, AT 6940 ACFT HRS, WITH TSN: 2520, 1 PRIORO/H, AND TSO: 0.
christina.l.negron USAACE FT RUCKER,AL.
22-Dec-2015 1 MEC F307262, AUTHORIZATION TO INSTALL OIL COOLER FAN (FAN AXIAL SN: D51201513) AT 7659.6ACFT HRS. OIL COOLER MOUNT INSTALLATION WAS ADJUSTED USING PEELABLE SHIMS BETWEENMOUNTING FACE AND OIL COOLER MOUNTING FLANGES. OIL COOLER MUST BE RE-EVALUATED ATNEXT 720 PHASE INSPECTION , IAW MEC.
christina.l.negron USAACE FT. RUCKER, AL.
26-Feb-2016 1 MEC F307262A, 7659.6 ACFT HRS, AXIAL FAN SN D512-01513, AUTHORIZATION GRANTED TO USE SHIMPN 70652-02151-102 NIIN 01-123-0379 SHIM IN LIEU OF SS52J0250X0750 SHIM STOCK.
dean.a.keirn USAACE FT. RUCKER, AL.
APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
FUEL CONTROL 8524465154641511. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
23-Nov-2010 OM
thomas.m.lilly29-Nov-2010
0.5USAACE, FT.RUCKERL AL(MB1137)
ALL H-60A SERIES AIRCRAFT,HAMILTON STANDARD HYDRO-MECHANICAL UNITS (HMU)
H-60-11-ASAM-03MWO:
Priority Mnt Level
05-Sep-2012 OM
mary.b.hodge10-Sep-2012
0.5USAACE, FT.RUCKER, AL
ALL H-60A SERIES AIRCRAFT,HYDRO-MECHANICAL UNIT (HMU)
H-60-12-ASAM-11MWO:
Priority Mnt Level
19-Aug-2013 FN
mary.b.hodge22-Aug-2013
1.0USAACE, 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.
FUEL CONTROL 8524465154642141. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
05-Sep-2012 OM
jessica.n.kennedy05-Oct-2012
1.0USAACE, FT.RUCKER, AL
ALL H-60A SERIES AIRCRAFT,HYDRO-MECHANICAL UNIT (HMU)
H-60-12-ASAM-11MWO:
Priority Mnt Level
19-Aug-2013 FN
jessica.n.kennedy22-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.
FWD FIXED GEAR SHOCK 8524465IA005761. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
22-Dec-1998 OI
mae.p.belford27-Aug-2004
1.0USAAVNC, FT.RUCKER, AL.(MF4187)
CHANGES TO OVERHAUL ANDRETIREMENT SCHEDULE TM 1-1520-237-23-1AND AIRCRAFTCOMPONENTS REQUIRINGMAINTENANCE MANAGEMENT ANDHISTORICAL DATA REPORTS TB 1-1500-341-01
UH-60-MIM-99-001MWO:
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.
GEARSHAFT, BEVEL 8524465F320023611. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
17-Oct-2011 OM
vickie.l.meadows20-Aug-2013
0.0USAACETAIL ROTOR OUTPUT BEVEL GEARNON-DESTRUCTIVE INSPECTION
H-60-12-ASAM-01MWO:
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 8524465D308000731. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
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.
INPUT MODULE 8524465A264-003791. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
02-Aug-2000 OT
mae.p.belford22-Aug-2000
1.0AASF#1, HOPEHULL,AL.(XP4155)
ALL H-60 SERIES AIRCRAFT,REMOVAL OF INPUT MODULE GEARBOX ASSEMBLIESWITHPOTENTIALLY CRACKED BEVELGEARS
UH-60-00-02MWO:
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.
INPUT MODULE 8524465A264-021511. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
02-Aug-2000 OT
mae.p.belford04-Aug-2000
0.5D-CO 2-10 FT.DRUM, NY(KK3148)
ALL H-60 SERIES AIRCRAFT,REMOVAL OF INPUT MODULE GEARBOX ASSEMBLIESWITHPOTENTIALLY CRACKED BEVELGEARS
UH-60-00-02MWO:
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 ROTOR SHAFT EXTENDER 8524465C286-004491. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
22-Jan-1997 OM
mae.p.belford23-Jan-1997
1.0D.CO. 2/82 AVNFBNC (PCW-BA2721)
ALL H-60 AIRCRAFT WITH THE MAINROTOR SHAFT EXTENSIONASSEMBLY, P/N 70351-08186-043,MANUFACTURED BY FENNMANUFACTURING COMPANY (CAGECODE 82001) OR THE PURDYCORPORATION (CAGE CODE 15152)
UH-60-97-ASAM-09MWO:
Priority Mnt Level
01-Oct-1997 OM
mae.p.belford06-Oct-1997
0.1D.CO. 2/82 AVNFBNC (PCW-BA2721)
ALL H-60 AIRCRAFT, MAIN ROTORSHAFT EXTENSION ASSEMBLY, P/N70351-08186-043 MANUFACTUREDBY FENN MANUFACTURINGCOMPANY (CAGE CODE 82001) ORTHE PURDY CORPORATION (CAGECODE 15152)
UH-60-98-ASAM-01MWO:
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 ROTOR SPINDLE ASSY 8524465A001-051971. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
17-Sep-2012 OM
jessica.l.wendel24-Sep-2012
1.0USAACEMAIN ROTOR SPINDLE SUB-COMPONENT TRACKINGREQUIREMENTS
H-60-12-AMAM-16MWO:
Priority Mnt Level
26-Feb-2013 FM
jessica.l.wendel27-Feb-2013
0.5USAACEMAIN ROTOR SPINDLE ANTI-FLAPASSY (CORRECTION)
H-60-13-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.
MAIN TRANSMISSION MODULE 8524465A265-010631. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
30-Aug-2012 DR
JC168804-Sep-2013
621.0CCADRECAPITALIZATION REQURIMENTS1-1615-37,CHG 1MWO:
Priority Mnt Level
26-Mar-2014 FM
QC00000007-Jul-2014
1.0USAACE FT.RUCKER, AL.
MAIN TRANSMISSION FILTER BOWLAND CHIP DETECTOR ATTACHMENTHARDWARE
H-60-14-AMAM-09MWO:
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
(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 A265-01063 06A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE
Page 1 of 2
17000 24300
161501078571106A08
03730SWASHPLATE GUIDE F4250363770351-08227-041 RCRC
3000 8407
161501110149106A13
18933730HOUSING ASSY MGB 151520177870351-08110-045 RCRC
7600 14900
304001415838806A18
03730MAIN ROTOR SHAFT E2530446070351-08131-048 RCRC
12000 17407
161501497725706A19
18933730PLANETARY CARRIER ASSY A2400126770351-08175-046 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 2
7. SIGNIFICANT HISTORICAL DATA
03-Sep-2013 1 RECAPPED/OVERHAULED IAW DMWR 1-1615-371, C1. TSN: 3730, TSO: 0.
JC1688 CCAD CORPUS CHRISTI TX.
05-Jun-2014 1 INSTALLED ON ACFT. 8524465 AT 7300 ACFT. HRS., WITH TTSN: 3730, TTSO: 0.
anthony.s.speigner USAACE FT. RUCKER, AL.
02-Jun-2015 1 TRANS IMPD BYPASS BUTTON POPPED (XMSN S/N: A265-01063, W/TTSN: 4083.3 HRS) AT 7653.3 ACFTON ACFT 8524465. REPLACED M/MOD STAGE 1 AND 2 OF FILTER BOWL IAW EM0013 WP626 AT 7653.3ACFT HRS.
bryan.w.hollis USAACE FT. RUCKER, AL
23-Aug-2016 1 MAIN MOD FILTER BUTTON POPPED ON TRANSMISSION S/N A265-01063 AT 4485 TSN. REPLACED MAINTRANSMISSION OIL FILTER ELEMENT AND SERVICEABILITY INSPECTION C/W IAW EM0013 & WP#0626 00
brian.k.dow USAACE FT. RUCKER, AL.
30-Sep-2016 1 MEC F317139A, 8075.9 ACFT HRS, XMSN SN A265-01063, TSN 4506, AUTHORIZATION GRANTED TOPERFORM THE TROUBLE SHOOTING PROCEDURES IAW MAIN XMSN - NEWSLETTER ARTICLE(ATTACHED). ONCE TROUBLE SHOOTING PROCEDURES HAVE BEEN COMPLETED, REPORT FINDINGSTO THE UNDERSIGNED.
dean.a.keirn USAACE FT. RUCKER, AL.
06-Oct-2016 1 MEC F317139B, TWO QUARTS OF OIL ADDED PER THE ATTACHED TROUBLESHOOTING PROCEDURE(ADDENDUM A) DID NOT FULLY ALLEVIATE THE FLUCTUATION. MAINTENANCE HAS REQUESTED TOADD AN ADDITIONAL QUART OIL FOR A TOTAL OF 3 QUARTS. AUTHORIZATION GRANTED TO ADDADDITIONAL QUART OF OIL, FOR A TOTAL OF 3 QUARTS. CONTINUE WITH TROUBLESHOOTINGPROCEDURE STEPS AFTER ADDITION OF OIL.
dean.a.keirn USAACE FT. RUCKER, AL.
APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
MIXER ASSEMBLY 852446543822201. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
08-May-2015 DR
006-Aug-2015
15.0W0MUAA/CCADRECAPPEDDMWR 1-1615-282 CHG 1MWO:
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
(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 BEM1047 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE
Page 1 of 2
9000 16984
165001125090703A01A
00PISTON, MAIN L/GEAR STR BEM104770250-12067-102 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
27-Jun-2016 1 FWD FIXED GEAR SHOCK S/N BEM1047 INSTALLED ON ACFT 8524465 AT 7984 ACFT. HRS. WITH 0 TSN.AFS INSPECTOR 236.
brian.k.dow 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 IA00576 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE
Page 1 of 2
9000 11268
165001125090703A01A
00PISTON, MAIN L/GEAR STR IA0618570250-12067-102 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
27-Aug-2004 1 27 AUG 04 - INSTALLED M/L/G STRUT (NEW) ON ACFT. 8524465 AT 2267.7 ACFT HRS. (MF4187 R/SPEC.)USAAWC, FT. RUCKER, AL
mae.p.belford USAAWC 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.
1615014426926MAIN ROTOR SPINDLE ASSY 70102-08200-069 A001-05197 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE
Page 1 of 2
COND COND
161501161437305A01I02
11593083ELASTOMERIC BEARING B324-25291SB7001-048 CCCC
COND COND
311001158960705A01I02C
11593083THRUST BEARING B325-36756SB7002-048 CCCC
13000 16588
531001126944405A01I04
00M/R SPINDLE NUT C479-1146470102-08105-102 RCRC
6400 9988
530601460602005A01I06
00TIE ROD (M/R SPINDLE) C504-0163338023-10372-101 RCRC
10000 13588
161501214914005A01I07
00CONTROL HORN ASSY A241-1554570102-08111-047 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-May-2007 1 02 MAY 07 - INSTALLED M/R SPINDLE ASSY S/N: A001-005197 W/TSN 0 HRS ON ACFT 8524465 @ 3587.7ACFT HRS. JT0967 R/SPEC. USAAWC, FT. RUCKER, AL.
mae.p.belford USAAWC FT. RUCKER, AL
22-Dec-2010 1 SIGNIFICANT HISTORICAL DATA RETAINING NUT TORQUE: 130 FT. LBS. SIKORSHY AIRCRAFT
mae.p.belford SIKORSHY AIRCRAFT (NO LOCATION)
13-Sep-2012 1 INSTALLED ELASTOMERIC BEARING S/N B324-25291 WITH TSN-1159 AND THRUST BEARING S/N B325-36756 WITH TSN-1159 ON MAIN ROTOR SPINDLE S/N A001-05197 WITH TSN-3083 ON 8524465 @ 6671ACFT HRS.
vickie.l.meadows USAACE FT RUCKER, AL
23-Nov-2015 1 REMOVED M/R SPINDLE ASSY SN: A001-05197, AT 7660 ACFT HRS, WITH TSN: 4072. REMOVED FOR 720HOUR INSPECTION.
christina.l.negron USAACE FT. RUCKER,AL.
04-Dec-2015 1 COMPLETED 720HR INSPECTION AND RETURNED TO SERVICE. TTSN: 4072.
cynthia.moore USAACE (AMSS) FT. RUCKER, AL.
09-Dec-2015 1 INSTALLED ON ACFT. 8524465 AT 7660 ACFT. HRS. WITH TTSN: 4072.
rick.r.skinner USAACE FT. RUCKER, AL.
APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991
SECTION I COCKPITEH-60A_BASELINE
4. EQUIPMENT CHECKLIST
8524465 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
Page 1 of 10
1RECEIVER RADIO - R-1496A/ARN-89
U UUUUUUUU UU 11
1
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2DISPLACEMENT GYRO - CN-1314/A (9000C)
U UUUUUUUU UU 11
2
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1GYRO, DIRECTIONAL - CN-998/ASN-43
U UUUUUUUU UU 00
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 UU 01
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 UU 11
5
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RECEIVER - R-2139/ARN-123(V)
U UUUUUUUU UU 11
6
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1MOUNTING - MT-4834/ARN-123(V)
U UUUUUUUU UU 11
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 UU 11
8
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1MOUNTING RACK - 70600-01038-102
U UUUUUUUU UU 11
9
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1SAS AMPLIFIER - 70901-02908-104
U UUUUUUUU UU 11
10
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RATE GYRO ASSEMBLY - 70600-01047-041
U UUUUUUUU UU 11
11
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RATE GYRO - TRU-2A/A
U UUUUUUUU UU 11
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 UU 33
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 UU 00
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 UU 00
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
8524465 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
Page 2 of 10
3REMOTE CONTROL UNIT (KY-58) - Z-AHP/YSEC
U UUUUUUUU UU 00
16
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1AMPLIFIER IMPEDANCE - AM-4859A/ARN-89
U UUUUUUUU UU 11
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 UU 00
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 UU 11
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 UU 22
20
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2ANTENNA - AS-3831/APN-209(V)
U UUUUUUUU UU 22
21
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1GLIDE SLOPE ANTENNA - 70600-01043-101
U UUUUUUUU UU 11
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 UU 11
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 UU 00
24
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1FIRE EXTINGUISHER - FR23-4-11848
U UUUUUUUU UU 00
25
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2BAROMETERIC ALTIMETER - AAU-32/A
U UUUUUUUU UU 22
26
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2CREW SEAT - D3801-2
U UUUUUUUU UU 33
27
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2AIRCRAFT CLOCK - ABU-11A
U UUUUUUUU UU 22
28
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RECEIVER/TRANSMITTER - RT-1477/ARC-201
U UUUUUUUU UU 00
29
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2INTERPHONE CONTROL - C6533/ARC
U UUUUUUUU UU 22
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
8524465 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
Page 3 of 10
1RECEIVER/TRANSMITTER - RT-1115D/APN-209
U UUUUUUUU UU 11
31
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1INDICATOR ALTIMETER - ID-1917C/APN-209
U UUUUUUUU UU 11
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 UU 11
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 UU 00
34
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1CONTROL - C-11466A/ARC-201
U UUUUUUUU UU 00
35
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1COMPARATOR SIGNAL DATA - CM482/ARC186(V)
U UUUUUUUU UU 11
36
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
3MOUNT - MT-6051/ARC-186
U UUUUUUUU UU 33
37
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RECEIVER/TRANSMITTER - RT-1296A/APX-100
U UUUUUUUU UU 01
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 UU 11
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 UU 00
40
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RADIO RETRANSMISSION PANEL -70550-01008-042
U UUUUUUUU UU 11
41
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1MAGNETIC COMPASS - MS17983-4
U UUUUUUUU UU 11
42
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2OUTSIDE AIR TEMP INDICATOR - MS28028-1
U UUUUUUUU UU 22
43
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1ARMOUR WING PANEL - 70500-01152-093
U UUUUUUUU UU 00
44
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1ARMOUR WING PANEL - 70500-01152-094
U UUUUUUUU UU 00
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
8524465 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
Page 4 of 10
1STABILATOR/FLT CONT PNL - 70902-01070-048
U UUUUUUUU UU 11
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 UU 00
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 UU 00
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 UU 00
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 UU 00
50
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1TACAN RECEIVER/TRANSMITTER RT-1159/A
U UUUUUUUU UU 00
51
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1ELECTRONIC SEQUENCE UNIT, 163290-100-E
U UUUUUUUU UU 11
52
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RADAR DETECTION SET SIGNAL AN/APR39
U UUUUUUUU UU 00
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 UU 00
54
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1DISPENSER GENERAL PURPOSE AIRCRAFT M130
U UUUUUUUU UU 00
55
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
3SECURE SPEECH UNIT TSEC/KY-58
U UUUUUUUU UU 00
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 UU 00
57
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1KY-100 AIRTERM 0N616736-1
U UUUUUUUU UU 00
58
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1CONTROL DISPLAY UNIT C-12346/URC
U UUUUUUUU UU 00
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 10SERIAL NUMBER MODEL AREA NAME
8524465 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
robert.e.bridg1 CIV 11-Sep-2017
robert.e.bridg2 CIV 19-Oct-2017
b. LOCATION/REMARKSCHECK NO.
6. LOCATION OR REMARKS
a. ITEM NUMBER
Nomenclature
DISPLACEMENT GYRO - CN-1314/A (9000C)
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION2
DISPLACEMENT GYRO - CN-1314/A (9000C)
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION2
GYRO, DIRECTIONAL - CN-998/ASN-43
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION3
GYRO, DIRECTIONAL - CN-998/ASN-43
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION3
SIGNAL DATA CONVERTER -CV-3338A/ASN-128B
2 REMOVED PER GOVT REQUEST4
BATTERY FOR KY 58 - BA-1372/U
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION14
BATTERY FOR KY 58 - BA-1372/U
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION14
INTERFACE ADAPTER (KY-58)- Z-AHQ/TSEC
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION15
INTERFACE ADAPTER (KY-58)- Z-AHQ/TSEC
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION15
REMOTE CONTROL UNIT (KY-58) - Z-AHP/YSEC
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION16
REVERSE OF DA FORM 2408-17, NOV 1991
Page 6 of 10SERIAL NUMBER MODEL AREA NAME
8524465 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
robert.e.bridg1 CIV 11-Sep-2017
robert.e.bridg2 CIV 19-Oct-2017
REMOTE CONTROL UNIT (KY-58) - Z-AHP/YSEC
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION16
#2 VHF-FM ANTENNACOUPLER - 70600-01010-104
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION18
#2 VHF-FM ANTENNACOUPLER - 70600-01010-104
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION18
FIRST AID KIT - 6545-00-919-6650
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION24
FIRST AID KIT - 6545-00-919-6650
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION24
FIRE EXTINGUISHER - FR23-4-11848
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION25
FIRE EXTINGUISHER - FR23-4-11848
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION25
CREW SEAT - D3801-21 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION27
CREW SEAT - D3801-22 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION27
RECEIVER/TRANSMITTER - RT-1477/ARC-201
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION29
RECEIVER/TRANSMITTER - RT-1477/ARC-201
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION29
REVERSE OF DA FORM 2408-17, NOV 1991
Page 7 of 10SERIAL NUMBER MODEL AREA NAME
8524465 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
robert.e.bridg1 CIV 11-Sep-2017
robert.e.bridg2 CIV 19-Oct-2017
CONTROL - C-10604(V)6/ARN-186
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION34
CONTROL - C-10604(V)6/ARN-186
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION34
CONTROL - C-11466A/ARC-2011 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION35
CONTROL - C-11466A/ARC-2012 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION35
RECEIVER/TRANSMITTER - RT-1296A/APX-100
2 REMOVED PER GOVT REQUEST38
COMPASS SET CONTROLLER- C-8021E/ASN-75
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION40
COMPASS SET CONTROLLER- C-8021E/ASN-75
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION40
ARMOUR WING PANEL - 70500-01152-093
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION44
ARMOUR WING PANEL - 70500-01152-093
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION44
ARMOUR WING PANEL - 70500-01152-094
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION45
REVERSE OF DA FORM 2408-17, NOV 1991
Page 8 of 10SERIAL NUMBER MODEL AREA NAME
8524465 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
robert.e.bridg1 CIV 11-Sep-2017
robert.e.bridg2 CIV 19-Oct-2017
ARMOUR WING PANEL - 70500-01152-094
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION45
CONTROL-INDICATOR ASN-132 C-11097/ASN-132
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION47
CONTROL-INDICATOR ASN-132 C-11097/ASN-132
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION47
SIGNAL DATA CONVERTERASN-132CV-3739/ASN-132
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION48
SIGNAL DATA CONVERTERASN-132CV-3739/ASN-132
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION48
MOUNT FOR ASN-132 MT-4915/A
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION49
MOUNT FOR ASN-132 MT-4915/A
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION49
DATA PROCESS SET AN/UYK-64(V)2
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION50
DATA PROCESS SET AN/UYK-64(V)2
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION50
TACANRECEIVER/TRANSMITTER RT-1159/A
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION51
TACANRECEIVER/TRANSMITTER RT-1159/A
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION51
REVERSE OF DA FORM 2408-17, NOV 1991
Page 9 of 10SERIAL NUMBER MODEL AREA NAME
8524465 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
robert.e.bridg1 CIV 11-Sep-2017
robert.e.bridg2 CIV 19-Oct-2017
1159/A
RADAR DETECTION SETSIGNAL AN/APR39
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION53
RADAR DETECTION SETSIGNAL AN/APR39
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION53
IR JAMMERCOUNTERMEASURES SETAN/ALQ-144(V)
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION54
IR JAMMERCOUNTERMEASURES SETAN/ALQ-144(V)
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION54
DISPENSER GENERALPURPOSE AIRCRAFT M130
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION55
DISPENSER GENERALPURPOSE AIRCRAFT M130
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION55
SECURE SPEECH UNITTSEC/KY-58
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION56
SECURE SPEECH UNITTSEC/KY-58
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION56
CONTROL INDICATOR (KY-58)C-8157/ARC
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION57
CONTROL INDICATOR (KY-58)C-8157/ARC
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION57
REVERSE OF DA FORM 2408-17, NOV 1991
Page 10 of 10SERIAL NUMBER MODEL AREA NAME
8524465 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
robert.e.bridg1 CIV 11-Sep-2017
robert.e.bridg2 CIV 19-Oct-2017
KY-100 AIRTERM 0N616736-11 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION58
KY-100 AIRTERM 0N616736-12 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION58
CONTROL DISPLAY UNIT C-12346/URC
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION59
CONTROL DISPLAY UNIT C-12346/URC
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION59
REVERSE OF DA FORM 2408-17, NOV 1991
SECTION II CABINEH-60A_BASELINE
4. EQUIPMENT CHECKLIST
8524465 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
Page 1 of 6
1INERTIAL NAVIGATION SET - AN/ASN-141
U UUUUUUUU UU 00
1
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1BEARING, DISTANCE, HEADING INDICATOR - ID2301/U
U UUUUUUUU UU 00
2
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1MARKER BEACON ANTENNA - 70600-02011-103
U UUUUUUUU UU 11
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 UU 11
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 UU 11
5
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1FIRST AID KIT - 6545-00919-6650
U UUUUUUUU UU 00
6
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1FIRE EXTINGUISHER - FR23-4-11848
U UUUUUUUU UU 00
7
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1CRASH AXE - 56D6221
U UUUUUUUU UU 11
8
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1HAND SET - H-250/U
U UUUUUUUU UU 11
9
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1SLAB BATTERY - D8565/11-1
U UUUUUUUU UU 11
10
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
3INTERPHONE CONTROL - C6533/ARC
U UUUUUUUU UU 33
11
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1ADAPTER FUEL DRAIN - 70307-03018-102
U UUUUUUUU UU 00
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 UU 00
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 UU 00
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 UU 00
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
8524465 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
Page 2 of 6
1PLUG ASSY APU EXHAUST - 70700-20509-041
U UUUUUUUU UU 00
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 UU 00
17
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1BLADE FOLD SET - 70700-20412-011
U UUUUUUUU UU 00
18
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2COVER PITOT TUBE - 70700-20460-041
U UUUUUUUU UU 00
19
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1TROOP SEATS - 70500-02151-045
U UUUUUUUU UU 00
20
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2COVER ENGINE INLET - 83DSCC-D006
U UUUUUUUU UU 00
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 UU 00
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 UU 00
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 UU 00
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 UU 00
25
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1HYD. PUMP HANDLE - 15400-50126
U UUUUUUUU UU 11
26
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2EQUIPMENT LOGBOOK - MIL-D-43064
U UUUUUUUU UU 22
27
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1COMPUTER LOGBOOK
U UUUUUUUU UU 01
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 UU 11
29
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
4TIEDOWN ASSEMBLY, TOW - 70700-20433-045
U UUUUUUUU UU 00
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 6SERIAL NUMBER MODEL AREA NAME
8524465 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
robert.e.bridg1 CIV 11-Sep-2017
robert.e.bridg2 CIV 19-Oct-2017
b. LOCATION/REMARKSCHECK NO.
6. LOCATION OR REMARKS
a. ITEM NUMBER
Nomenclature
INERTIAL NAVIGATION SET -AN/ASN-141
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION1
INERTIAL NAVIGATION SET -AN/ASN-141
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION1
BEARING, DISTANCE,HEADING INDICATOR -ID2301/U
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION2
BEARING, DISTANCE,HEADING INDICATOR -ID2301/U
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION2
FIRST AID KIT - 6545-00919-6650
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION6
FIRST AID KIT - 6545-00919-6650
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION6
FIRE EXTINGUISHER - FR23-4-11848
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION7
FIRE EXTINGUISHER - FR23-4-11848
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION7
ADAPTER FUEL DRAIN - 70307-03018-102
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION12
ADAPTER FUEL DRAIN - 70307-03018-102
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION12
REVERSE OF DA FORM 2408-17, NOV 1991
Page 4 of 6SERIAL NUMBER MODEL AREA NAME
8524465 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
robert.e.bridg1 CIV 11-Sep-2017
robert.e.bridg2 CIV 19-Oct-2017
LOCK ASSY BLADE TIEDOWN- 70700-20369-041
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION13
LOCK ASSY BLADE TIEDOWN- 70700-20369-041
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION13
PLUG ASSY INTAKE - HIRSSSUPP - 70700-20515-041/042
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION14
PLUG ASSY INTAKE - HIRSSSUPP - 70700-20515-041/042
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION14
PLUG ASSY EXHAUST - HIRSS- 70700-20515-043
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION15
PLUG ASSY EXHAUST - HIRSS- 70700-20515-043
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION15
PLUG ASSY APU EXHAUST -70700-20509-041
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION16
PLUG ASSY APU EXHAUST -70700-20509-041
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION16
COVER ASSY OIL COOLER -70700-20511-041
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION17
COVER ASSY OIL COOLER -70700-20511-041
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION17
BLADE FOLD SET - 70700-20412-011
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION18
REVERSE OF DA FORM 2408-17, NOV 1991
Page 5 of 6SERIAL NUMBER MODEL AREA NAME
8524465 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
robert.e.bridg1 CIV 11-Sep-2017
robert.e.bridg2 CIV 19-Oct-2017
BLADE FOLD SET - 70700-20412-011
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION18
COVER PITOT TUBE - 70700-20460-041
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION19
COVER PITOT TUBE - 70700-20460-041
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION19
TROOP SEATS - 70500-02151-045
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION20
TROOP SEATS - 70500-02151-045
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION20
COVER ENGINE INLET -83DSCC-D006
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION21
COVER ENGINE INLET -83DSCC-D006
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION21
FITTING ASSEMBLY - L/H -70751-02023-043
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION22
FITTING ASSEMBLY - L/H -70751-02023-043
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION22
FITTING ASSEMBLY - R/H -70751-02023-044
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION23
REVERSE OF DA FORM 2408-17, NOV 1991
Page 6 of 6SERIAL NUMBER MODEL AREA NAME
8524465 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
robert.e.bridg1 CIV 11-Sep-2017
robert.e.bridg2 CIV 19-Oct-2017
FITTING ASSEMBLY - R/H -70751-02023-044
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION23
ICS WALK-AROUND CORD -70602-02023-044
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION24
ICS WALK-AROUND CORD -70602-02023-044
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION24
PORTABLE INSP. FLOODLIGHT - 15-0366-1
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION25
PORTABLE INSP. FLOODLIGHT - 15-0366-1
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION25
EQUIPMENT LOGBOOK - MIL-D-43064
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURSATION27
COMPUTER LOGBOOK2 REMOVED PER GOVT REQUEST28
TIEDOWN ASSEMBLY, TOW -70700-20433-045
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION30
TIEDOWN ASSEMBLY, TOW -70700-20433-045
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION30
REVERSE OF DA FORM 2408-17, NOV 1991
SECTION III TRANSITION SECTIONEH-60A_BASELINE
4. EQUIPMENT CHECKLIST
8524465 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
Page 1 of 2
1ANTENNA, LOOP - AS-2108A/ARN-89
U UUUUUUUU UU 11
1
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
2IFF ANTENNA - 70600-02010-103
U UUUUUUUU UU 22
2
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1UHF/AM ANTENNA 70600-03002-104
U UUUUUUUU UU 11
3
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1PUMP FUEL SAMPLER - 82829/4P156-3
U UUUUUUUU UU 00
4
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1COMPENSATOR MAGNETIC FLUX - CN-405/ASN
U UUUUUUUU UU 11
5
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1COMPASS TRANSMITTER - T-611/ASN
U UUUUUUUU UU 11
6
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1GPS ANTENNA 22433-40
U UUUUUUUU UU 11
7
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1HF AMPLIFIER COUPLER AM-7531/URC
U UUUUUUUU UU 00
8
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RECEIVER/TRANSMITTER RT-1749/URC
U UUUUUUUU UU 00
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
8524465 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
robert.e.bridg1 CIV 11-Sep-2017
robert.e.bridg2 CIV 19-Oct-2017
b. LOCATION/REMARKSCHECK NO.
6. LOCATION OR REMARKS
a. ITEM NUMBER
Nomenclature
PUMP FUEL SAMPLER -82829/4P156-3
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION4
PUMP FUEL SAMPLER -82829/4P156-3
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION4
HF AMPLIFIER COUPLER AM-7531/URC
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION8
HF AMPLIFIER COUPLER AM-7531/URC
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION8
RECEIVER/TRANSMITTER RT-1749/URC
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION9
RECEIVER/TRANSMITTER RT-1749/URC
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION9
REVERSE OF DA FORM 2408-17, NOV 1991
SECTION IV TAIL CONEEH-60A_BASELINE
4. EQUIPMENT CHECKLIST
8524465 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
Page 1 of 2
2VOR/LOC ANTENNA - 70600-05002-101
U UUUUUUUU UU 22
1
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1HF ANTENNA 4700516-30
U UUUUUUUU UU 00
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
8524465 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
robert.e.bridg1 CIV 11-Sep-2017
robert.e.bridg2 CIV 19-Oct-2017
b. LOCATION/REMARKSCHECK NO.
6. LOCATION OR REMARKS
a. ITEM NUMBER
Nomenclature
HF ANTENNA 4700516-301 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION2
HF ANTENNA 4700516-302 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION2
REVERSE OF DA FORM 2408-17, NOV 1991
SECTION V TAIL ROTOR PYLONEH-60A_BASELINE
4. EQUIPMENT CHECKLIST
8524465 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
Page 1 of 2
1TROOP COMMANDER ANTENNA - 70600-06001-104
U UUUUUUUU UU 11
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 UU 11
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
8524465 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
robert.e.bridg1 CIV 11-Sep-2017
robert.e.bridg2 CIV 19-Oct-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.
SHOCK ABSORBER (TAIL) 8524465BMC8271. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
15-Jun-2004 DM
BB420130-Oct-2012
10.0CCADTAIL LANDING GEAR SHOCK STRUTASSEMBLY; P/N 70250-13101-041, -042, -043, -044
1-1620-243MWO:
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 8524465015152-19351. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
02-Dec-1996 OT
mae.p.belford30-Apr-2008
0.5USAAWC, FT.RUCKER, AL(BH0315)
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
mae.p.belford30-Apr-2008
0.5USAAWC, FTRUCKER, AL(BH0315)
ALL UH-60A, UH-60L, EH-60A,REMOVAL OF SPECIFIC SUSPECTREWORKED MAIN ROTORSWASHPLATE ASSEMBLIES
UH-60-97-ASAM-18MWO:
Priority Mnt Level
12-Jun-2006 OM
mae.p.belford30-Apr-2008
2.0USAAWC, FT.RUCKER, AL(BH0315)
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
(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 015152-1935 05A03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE
Page 1 of 2
COND COND
161501087160205A03A01
34763476STATIONARY SWASHPLATE 015152-178370104-08010-044 CCCC
11000 15184
161501357508905A03A02
00ROTATING SWASHPLATE 015152-193570104-08001-045 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
30-Apr-2008 1 30 APR 08 - INSTALLED SWASHPLATE ASSY ON ACFT 8524465 @ 4184 ACFT HRS WITH TSN 00 HRS.BH0315. USAAWC, FT. RUCKER, AL.
mae.p.belford USAAWC FT. RUCKER, AL
APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
T700-GE-700 ENGINE ASSY 8524465GE-E-2079251. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 2
15-Feb-1987 OM
thomas.m.lilly27-Aug-2003
1.0CCAD N/A(PM6697)
ONE TIME INSPECTION OF TORQUEFUEL DIFFER PRESSUREINDICATOR
55-2840-248-50-44MWO:
Priority Mnt Level
31-Jul-1989 OM
thomas.m.lilly27-Aug-2003
33.0CCAD N/A(PM6697)
MODIFICATION OF GG ROTORASSEMBLY T700/701 REWORK T700ENGINES
55-2840-248-50-32MWO:
Priority Mnt Level
15-Aug-1990 OM
thomas.m.lilly27-Aug-2003
1.0CCAD N/A(PM6697)
INSTALLATION OF SELF SEALADAPTER ASSEMBLY
55-2840-248-50-28MWO:
Priority Mnt Level
25-Jan-1991 DN
thomas.m.lilly27-Aug-2003
20.0CCAD N/A(PM6697)
MODIFICATION OF POWER TAKEOFFDRIVE ASSEMBLY P/N 5044T27G01
55-2840-248-50-27MWO:
Priority Mnt Level
31-Mar-1993 DR
thomas.m.lilly27-Aug-2003
1.0CCAD N/A(PM6697)
INSTALLATION OF PTO DRIVEASSEMBLY P/NS 5044T27G02 OR5056T66G02 (T700-GE-700 AND 701ENGINES)
1-2840-248-50-29MWO:
Priority Mnt Level
08-Apr-1994 OU
thomas.m.lilly27-Aug-2003
1.0CCAD N/A(PM6697)
INSPECTION OF HMU TO GEARBOXFUEL LINE T701C FOR SERIALNUMBERS
1-2840-248-20-1MWO:
Priority Mnt Level
30-Dec-1994 FR
thomas.m.lilly27-Aug-2003
1.0CCAD N/A(PM6697)
YELLOW AND BLUE WIRE HARNESSINSULATION RESISTANCE CHECKFOR ALL AH-64A AIRCRAFT WITHT700-GE-701 ENGINES
1-2840-248-20-3MWO:
Priority Mnt Level
23-Dec-1997 FU
thomas.m.lilly27-Aug-2003
1.0CCAD N/A(PM6697)
PERIODIC INSPECTION ANDREPLACEMENT OF YELLOW ANDBLUE ENGINE HARNESS, RCSCSGLD-1860 (R1), ON ALL AH-64HELICOPTERS EQUIPPED WITH T700-GE-701 ENGINES
1-2840-248-20-20MWO:
Priority Mnt Level
05-Nov-1998 OM
thomas.m.lilly27-Aug-2003
1.0CCAD N/A(PM6697)
ALL UH-60A AND EH-60A SERIESHELICOPTERS, ONE TIMEINSPECTION OF ALL T700-GE-700ENGINE RECORDS
UH-60-99-ASAM-03MWO:
Priority Mnt Level
thomas.m.lilly27-Aug-2003
1.0CCAD N/A(PM6697)
ALL AH-64 AND UH-60 SERIESAIRCRAFT - ONE TIME INSPECTIONOF T700-GE-700/701/701C ENGINES
UH-60-99-ASAM-11MWO:
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.
T700-GE-700 ENGINE ASSY 8524465GE-E-2079251. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 2 of 2
02-Aug-1999 FM
Priority Mnt Level
20-Dec-2007 OM
thomas.m.lilly03-Jan-2008
4.0SSI, FT.BENNING, GA(AC3119)
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.lilly20-Jul-2010
0.4USAACE, FT.RUCKER, AL.(MB1137)
ALL H-60 AND H-64 SERIESAIRCRAFT, SUSPECT ENGINEHARNESSES
H-60-08-ASAM-14MWO:
Priority Mnt Level
12-Jan-2009 FM
thomas.m.lilly08-Jul-2010
0.5USAACE, FT.RUCKER, AL(MB1137)
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.lilly13-Oct-2009
1.0USAACE, FT.RUCKER, AL(JB2761)
ALL H-60A AIRCRAFT, HAMILTON-SUNSTRAND HYDRO-MECHANICALUNITS
H-60-10-ASAM-01MWO:
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.
T700-GE-700 ENGINE ASSY 8524465GE-E-3064851. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 2
15-Feb-1987 OM
thomas.m.lilly25-Jul-2000
0.5CCAD (LF3674)ONE TIME INSPECTION OF TORQUEFUEL DIFFER PRESSUREINDICATOR
55-2840-248-50-44MWO:
Priority Mnt Level
31-Jul-1989 OM
thomas.m.lilly25-Jul-2000
33.0CCAD (LF3674)MODIFICATION OF GG ROTORASSEMBLY T700/701 REWORK T700ENGINES
55-2840-248-50-32MWO:
Priority Mnt Level
15-Aug-1990 OM
thomas.m.lilly25-Jul-2000
1.0CCAD (LF3674)INSTALLATION OF SELF SEALADAPTER ASSEMBLY
55-2840-248-50-28MWO:
Priority Mnt Level
25-Jan-1991 DN
thomas.m.lilly25-Jul-2000
20.0CCAD (LF3674)MODIFICATION OF POWER TAKEOFFDRIVE ASSEMBLY P/N 5044T27G01
55-2840-248-50-27MWO:
Priority Mnt Level
31-Mar-1993 DR
thomas.m.lilly25-Jul-2000
1.5CCAD (LF3674)INSTALLATION OF PTO DRIVEASSEMBLY P/NS 5044T27G02 OR5056T66G02 (T700-GE-700 AND 701ENGINES)
1-2840-248-50-29MWO:
Priority Mnt Level
16-Aug-1999 OM
thomas.m.lilly25-Jul-2000
0.5CCAD (LF3674)ALL UH-60A, EH-60A AND UH-60QAIRCRAFT, SUBJECT: INSPECTIONINTERVAL CHANGE FOR HAMILTONSTANDARD HYDRO MECHANICALUNITS (HMU) P/NS 4046T52G01,4046T52G04, 4046T52G06,4046T52G09 AND 4046T52G11 USEDON THE T700-GE-700 ENGINE
UH-60-99-ASAM-12MWO:
Priority Mnt Level
16-Jul-2007 OM
thomas.m.lilly19-Jul-2007
0.5AC CO (MP8963)ALL H-60A SERIES AIRCRAFT,HAMILTON-SUNDSTRAND HYDRO-MECHANICAL UNITS (HMU'S)
UH-60-07-ASAM-08MWO:
Priority Mnt Level
13-Aug-2007 OM
thomas.m.lilly13-Aug-2007
0.5DS2 (RT0477)ALL H-60 SERIES AIRCRAFT, MAINFUEL MANIFOLD CHAFING
UH-60-07-ASAM-10MWO:
Priority Mnt Level
22-Sep-2008 OM
thomas.m.lilly04-Nov-2008
0.5AV CO (MP8963)ALL H-60 AND H-64 SERIESAIRCRAFT, SUSPECT ENGINEHARNESSES
H-60-08-ASAM-14MWO:
Priority Mnt Level
thomas.m.lilly18-Jan-2009
0.1USAACE FT.RUCKER, AL.(TB1027)
ALL H-60A/K/L AND AH-64 SERIESAIRCRAFT, T701C GAS GENERATOR(GG) ROTOR ASSEMBLIES
H-60-09-ASAM-01MWO:
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.
T700-GE-700 ENGINE ASSY 8524465GE-E-3064851. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 2 of 2
12-Jan-2009 FM
Priority Mnt Level
01-Oct-2009 OM
thomas.m.lilly09-Oct-2009
1.0USAACE, FT.RUCKER, AL(RC1002)
ALL H-60A AIRCRAFT, HAMILTON-SUNSTRAND HYDRO-MECHANICALUNITS
H-60-10-ASAM-01MWO:
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 8524465A006033981. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
21-Mar-2013 FM
QC00000018-Jan-2014
2.0USAACE, FT.RUCKER, AL
PLASTIC MEDIA BLAST (PMB) ANDOXIDE FLAKE RESIDUE
H-60-13-ASAM-04MWO:
Priority Mnt Level
25-Jul-2013 DR
JC168812-Aug-2013
200.8CCAD, CORPUSC, TX
H-60-12-ASAM-11-1615-279MWO:
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
(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 A00603398 06G014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE
Page 1 of 2
12000 15531
161501074515306G01C
36071191I/B RETENTION PLATE T/R C2590094170358-06612-042 RCRC
5000 12138
304001292161706G01D
01191GEARSHAFT, BEVEL F3200236170358-06620-102 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
12-Aug-2013 1 RECAPPED/OVERHAULED IAW DMWR 1-1615-279 TSN: 1191 TSO: 0
JC1688 CCAD CC, TX
18-Jan-2014 1 INSTALLED TAIL ROTOR GEARBOX ASSY S/N: A00603398 W/TSN: 1191 ON ACFT 8524465 @ 7138 ACFTHRS.
jessica.n.kennedy 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 70400-06100-042 233-04827 11C234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE
Page 1 of 2
2160 9104
311001113828811C23A
0504BRNG T/R PITCH CHG SHFT C840-13377SB1162-102 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
19-Dec-2013 1 INSTALLED T/R PITCH CHANGE SHAFT S/N 233-04827 WITH O/H-2, TSN-501 ON 8424024 @ 7367.1 ACFTHRS.
vickie.l.meadows USAACE FT RUCKER, AL
16-Dec-2015 1 REMOVED FROM ACFT. 8424024 AT 8086 ACFT. HRS. WITH TTSN: 1220, TSO: 719, 2 PREV. O/H. REMOVEDFOR LATERAL TRANSFER TO ACFT. 8524465.
rick.r.skinner USAACE FT. RUCKER, AL.
16-Dec-2015 2 INSTALLED ON ACFT. 8524465 AT 7660 ACFT. HRS. WITH TTSN: 1220, TSO: 719, 2 PREV. O/H.
rick.r.skinner USAACE FT. RUCKER, AL.
APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991
PIDMWODATE HRS
DATEORAPPLYINGMWO TITLEAND MAN -
8.NAME7.6. ORGANIZATION5.MWO NUMBER 9.4.
T/R PITCH CHANGE SHAFT 8524465233-048271. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER
Page 1 of 1
24-Jan-2014 FE
christina.l.negron24-Jan-2014
2.0USAACE, FTRUCKER, AL
TAIL ROTOR PITCH CHANGE SHAFTBUSHING
H-60-14-SOF-02MWO:
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
UNIT UNIQUE INVENTORY ITEMSEH-60A_BASELINE
4. EQUIPMENT CHECKLIST
8524465 EH-60A
3. AREA NAME 2. MODEL 1. SERIAL NUMBER
Page 1 of 3
2ATTITUDE AND HEADING REFERENCE UNIT (CN1716/A)
U UUUUUUUU UU 11
1
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1R-2594/ARN-147(V) RECEIVER
U UUUUUUUU UU 00
2
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1RT1836C/APX-118 TRANSPONDER
U UUUUUUUU UU 00
3
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1AN/APX-118 CONTROL
U UUUUUUUU UU 00
4
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1IFM AMPLIFIER AM-7189A/ARC
U UUUUUUUU UU 00
5
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1MOUNT IFM AMPLIFIER PN: MT-6592/ARC
U UUUUUUUU UU 11
6
1211109.8.7.6.5.4.3.2.1.CHECK NUMBER
QTY REQNOMENCLATURE:ITEM NO
1BFT ANTENNA GPS PN:S671575-863
U UUUUUUUU UU 11
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 3SERIAL NUMBER MODEL AREA NAME
8524465 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
robert.e.bridg1 CIV 11-Sep-2017
robert.e.bridg2 CIV 19-Oct-2017
b. LOCATION/REMARKSCHECK NO.
6. LOCATION OR REMARKS
a. ITEM NUMBER
Nomenclature
ATTITUDE AND HEADINGREFERENCE UNIT (CN1716/A)
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION1
ATTITUDE AND HEADINGREFERENCE UNIT (CN1716/A)
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION1
R-2594/ARN-147(V) RECEIVER1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION2
R-2594/ARN-147(V) RECEIVER2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION2
RT1836C/APX-118TRANSPONDER
1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION3
RT1836C/APX-118TRANSPONDER
2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION3
AN/APX-118 CONTROL1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION4
AN/APX-118 CONTROL2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION4
IFM AMPLIFIER AM-7189A/ARC1 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION5
IFM AMPLIFIER AM-7189A/ARC2 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION5
REVERSE OF DA FORM 2408-17, NOV 1991
Page 3 of 3SERIAL NUMBER MODEL AREA NAME
8524465 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
robert.e.bridg1 CIV 11-Sep-2017
robert.e.bridg2 CIV 19-Oct-2017
REVERSE OF DA FORM 2408-17, NOV 1991
top related