1. NOMENCLATURE 2. MODEL 3. AIRCRAFT SERIAL NUMBER

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





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



PIDMWODATE HRS





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



PIDMWODATE HRS





Page 4 of 4

DM22-Feb-1991


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


LILLY, THOMASM

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

1-1520-237-50-61MWO:

Mnt LevelPriority

DM01-Sep-1991


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



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


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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REMARKS4. 5.


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


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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


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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


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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


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DATE6.

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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


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REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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 [email protected] 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


NUMBER PIDENTRY


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REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


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REMARKS4. 5.


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


NUMBER PIDENTRY


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REMARKS4. 5.


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


NUMBER PIDENTRY


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REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


mary.b.hodge

USAACEMEC F124091 AUTHORIZATION GRANTED TOINSTALL HUD TDT AMPLIFIER DISCONNECTSIAW MEO A6206 REV. A

25-Mar-2011 1


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


shelia.d.cook


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 37 of 61

USAACEDELAYED ENTRY: ACFT INDUCTED INTOULLS-A(E) ON 16-MAR-11 AT 5966.3 ACFT HRS.

06-Apr-2011 1


dean.a.keirn

USAACEOPERATING WITHIN LIMITATIONS ANDRESTRICTIONS OF AWR 1681 DTD 10 MAY 10.(6010.7 ACFT HRS) (MH1534).

14-Apr-2011 1


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


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


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


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


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


mae.p.belford

USAAACEH-60-11-ASAM-13, ENGINE AIR INLET VALVE @6130.1 AC HRS

09-Jul-2011 1


frances.j.jackson

USAACEH-60-11-SOF-01, DISCREPANT SELF LOKCINGDOUBLE HEXAGON NUTS @6130.1 AC HRS

10-Jul-2011 1


frances.j.jackson

USAACEH-60-11-AMAN-15, IVHMS ACCELEROMETERS@ 6139.9 AC HRS

14-Jul-2011 1


frances.j.jackson

USAACEH-60-11-ASAM-14, ENGINE COWLING REPAIRRESTRICTIONS @ 6161.4 AC HRS

20-Jul-2011 1


frances.j.jackson


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 38 of 61

USAACEDELAYED ENTRY MEC F123536 DATED 14 MAR11 REQUEST ATUHORIZATION TO REPAIRRIGHT BEADED PANEL. PERMISSIONGRANTED.

04-Aug-2011 1


frances.j.jackson

USAACEDELAYED ENTRY MEC F127804 DATED 06 JUN11; REQUEST AUTHORZATION AS OWHETHER AIRCRAFT MAY REMAIN INSERCVICE. PERMISSION GRANTED.

04-Aug-2011 3


frances.j.jackson

USAACEDELAYED ENTRY MEC F124091 DATED 24 MAR11; REQUEST AUTHORIZATIO TO INSTLALLHUB TGT. PERMISSION GRANTED

04-Aug-2011 4


frances.j.jackson

USAACEDELAYED ENTRY MEC F72883 DATED 27 FEB08; REQUEST EVAL AND APPROVAL TOREPAIR CRACK AREA. PERMISSIONGRANTED.

05-Aug-2011 1


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


frances.j.jackson

USAACEAIRCRAFT NO LONGER OPERATING IAW MEOA6055 AT AIRCRAFT HRS: 6220.1.

02-Sep-2011 1


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


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


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


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


debra.r.chancellor

USAACEACFT OPERATING IAW AWR 1639 REV 3 DTD 1JUN 11 LIMITATIONS AND RESTRICTIONS INAWR.

16-Sep-2011 2


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


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


mary.b.hodge

USAACET/R TENSION CHECK COMPLETED @ 6229.8ACFT HRS. L/H 144 R/H 144 @ 26.9 DEGREESCELSIUS.

23-Sep-2011 1


mary.b.hodge


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


mary.b.hodge

USAACECOMPLIED WITH H-60-12-SOF-01 @ 6268 ACFTHRS.

08-Oct-2011 1


vickie.l.meadows

USAACEH-60-12-SOF-02 (TAIL ROTOR INTERMEDIATEGEARBOX) C/W AT 6268.0 ACFT HRS.

11-Oct-2011 1


debra.r.chancellor

USAACEH-60-12-SOF-03 (TAIL ROTOR INTERMEDIATEGEARBOX) C/W AT 6279.1 ACFT HRS. (AFS545).

14-Oct-2011 1


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


mae.p.belford

USAACEH-60-11-AMAM-19 (IMMC LCF CHG 62REQUIREMENTS )C/W @ 6298.6 ACFT HRS

22-Oct-2011 1


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


patrick.a.newton

USAACEAIRCRAFT NO LONGER OPERATING IAW AWR1529 REV, 1 DATED 07 OCT 10 @ 6325.0 ACFTHRS.

28-Oct-2011 1


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


claudia.f.anderson

USAACEAIRCRAFT NO LONGER OPEATING IAW AWR1455 R1 DATED 23 OCT 09 @ 6330.3 ACFTHRS.

03-Nov-2011 1


claudia.f.anderson

USAACEAIRCRAFT OPEATING IAW AWR 1455 REV 2DATED 31 OCT 2011 @ 6330.3 ACFT HRS.

03-Nov-2011 2


claudia.f.anderson

USAACEAIRCRAFT NO LONGER OPERATING IAW AWR1455 R2 DATED 31 OCT 11 @ 6377.7 ACFT HRS.

21-Nov-2011 1


claudia.f.anderson


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 40 of 61

USAACEAIRCRAFT OPERATING IAW AWR 1455 R3DATED 10 NOV 11 @ 6377.7 ACFT HRS.

21-Nov-2011 2


claudia.f.anderson

USAACEAIRCRAFT OPERATING IAW AWR 1153, R6,DATED 18 NOV 11, ON 06 DEC 2011 @ 6404.6ACFT HRS.

05-Dec-2011 2


claudia.f.anderson

USAACEAIRCRAFT OPERATING UNDER THERESTRICTIONS AND GUIDLINES OF MEOA5826 REV B

06-Dec-2011 1


olivia.d.williams

USAACEH-60-12-ASAM-02 DRAG BEAMREPLACEMENT @ 6405.6 ACFT HRS.

07-Dec-2011 1


claudia.f.anderson

USAACEH-60-11-ASAM-13 (INLET ANTI-ICE VALVE)COMLETED AT 6462.1 ACFT HRS.

14-Jan-2012 1


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


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


mae.p.belford

USAACEACFT OPERATING IAW AWR 1800 DTD 30 NOV11 AT 6474.0 ACFT HRS.

19-Jan-2012 3


mae.p.belford

USAACEH-60-12-SOF-04 - (BREEZE EASTERNEXTERNAL HOIST) COMPLIED WITH AT 6543.7AIRCRAFT HOURS.

18-Feb-2012 1


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


thomas.e.mitchell

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

27-Feb-2012 1


dean.a.keirn

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

28-Feb-2012 1


dean.a.keirn

USAACECOMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-17 @ 6579.7 ACFT HRS.

07-Mar-2012 1


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


thomas.e.mitchell


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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


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


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


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


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


thomas.e.mitchell

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

20-Mar-2012 1


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


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


thomas.e.mitchell

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

03-Apr-2012 1


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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


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


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


dean.a.keirn

USAACEMEC F145525, AUTHORIZATION GRANTEDFOR CCAD DFT TO REPLACE LH STA 265FRAME. 6671.0 ACFT HRS.

04-May-2012 1


dean.a.keirn

USAACEMEC F145528, AUTHORIZATION GRANTEDFOR CCAD DFT TO REPLACE RH STA 265FRAME. 6671.0 ACFT HRS.

04-May-2012 2


dean.a.keirn

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

08-May-2012 1


dean.a.keirn

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

25-May-2012 1


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


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


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


thomas.e.mitchell


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


dean.a.keirn

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

01-Aug-2012 1


dean.a.keirn

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

01-Aug-2012 2


dean.a.keirn

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

02-Aug-2012 1


dean.a.keirn

USAACEINSP H-60-12-AMAM-09, HYDRAULIC LINECHAFE DUE TO MISSING CLAMPS,COMPLETED, FAILED, AND CORRECTEDDEFICIENCIES 22AUG12 @ 6671 ACFT HRS

22-Aug-2012 1


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


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


dean.a.keirn

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

31-Aug-2012 1


dean.a.keirn

USAACEH-60-12-AMAM-15 (TRIM ACTUATORS),COMPLIED WITH AND COMPLETED 31AUG12@ 6671.0 ACFT HRS.

31-Aug-2012 2


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


jessica.l.wendel

USAACEH-60-12-ASAM-11, HYDRO-MECHANICAL UNIT(HMU), INSP COMP-FAILED 06SEP12 @ 6671.0ACFT HRS

06-Sep-2012 2


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


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


jessica.n.kennedy


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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


jessica.l.wendel

USAACEDELAYED ENTRY: ACFT DATE OFMANUFACTURE IS FEB 86

02-Oct-2012 1


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


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


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


dean.a.keirn

USAACEH-60-13-AMAM-02 (AHRS) C/W @ 6697.5 ACFTHRS. (HARNESS FAILED. HARNESS WASREPOSITIONED)

08-Nov-2012 1


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


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


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


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


jessica.l.wendel

USAACEH-60-13-AMAM-04 (LCF CHANGE 63)COMPLETED 10JAN13 @ 6730 ACFT HRS

10-Jan-2013 1


jessica.l.wendel

USAACEH-60-13-AMAM-05 (MLG BRAKES) COMPLETED-BOTH PASS-25 JAN 2013 @ 6730.0 ACFT HRS

25-Jan-2013 1


jessica.l.wendel


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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


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


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


jessica.l.wendel

USAACEH-60-13-AMAM-06 (CEFS) COMPLETED - CEFSNOT INSTALLED; AMAM-06 NOT APPLICABLE12FEB2013 @ 6748.1 ACFT HRS

12-Feb-2013 1


jessica.l.wendel

USAACEH-60-13-ASAM-03 (MR SPINDLE ANTI-FLAPASSEMBLIES) COMPLIED WITH 27FEB2013 @6765.1 ACFT HRS

27-Feb-2013 1


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


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


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


kathleen.m.jungell

USAACEH-60-13-ASAM-04 (PLASTIC MEDIA BLAST ANDOXIDE FLAKE RESIDUE) COMPLETED26MAR2013 @ 6807.4 ACFT HRS

26-Mar-2013 1


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


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


anthony.s.speigner

USAACEH-60-13-ASAM-05 ELECTRIC RESCUE HOISTCOMPLETED 09 APR 2013 AT 6822.4 ACFT.HRS.

09-Apr-2013 1


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


dean.a.keirn

USAACEH-60-13-ASAM-06 (PMI CHECKLIST CHANGES)COMP @ 6876.5 ACFT HRS. (AFS 76)

10-May-2013 1


kathleen.m.jungell

USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-SOF-01 THIS DATE AT 6907.7 ACFT HRS.

31-May-2013 1


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


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


marilyn.l.jones

USAACECOMPLETED TAIL ROTOR CABLE TENSIONCHECK: L-140 IN LBS, R-140 IN LBS, 26DEGREES CELCIUS. MR109846

05-Aug-2013 1


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


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


christina.l.negron

USAACEMEC F170635, AUTHORIZATION GRANTED TOREPAIR RH TAIL STRUT ACCESS OPENINGCRACK IN UPPER FWD CORNER. 6939.7 ACFTHRS.

14-Aug-2013 1


dean.a.keirn

USAACEDAGR SERIAL NUMBER IS 214674 @ 6939.7ACFT HRS. IAW PROPERTY ADMINISTATOR @PHASE

19-Aug-2013 1


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


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


vickie.l.meadows


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


vickie.l.meadows

USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-01 (FLIGHT CONTROL RIGGINGPROCEDURES)@ 6939.7 ACFT HRS.

26-Aug-2013 1


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


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


vickie.l.meadows

USAACEPMI- PHASE #11 COMPLETED AT 6939.7 ACFTHRS. PMI- PHASE #12 DUE AT 7659.7 ACFTHRS.

28-Aug-2013 1


tony.barnes

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

29-Aug-2013 1


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


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


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


dean.a.keirn

LOCKHEED MARTINOCM/ACE PERFORMED AT 7060.1 ACFT HRSBY TEAM MEMBER QQ.

31-Oct-2013 1


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


dean.a.keirn

USAACECOMPLY WITH REQUIREMENTS OF H-60-14-SOF-01(BREEZE EASTERN EXTERNALRESCUE HOIST INSTALLATION) @ 7060.1ACFT HRS

01-Nov-2013 1


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


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 48 of 61

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

23-Nov-2013 2


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


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


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


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


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


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


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


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


anthony.s.speigner

DCR RASM-COCM/ACE PERFORMED AT 7182.3 AIRCRAFTHOURS BY TEAM MEMBERS P AND QQ

17-Mar-2014 1


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


dean.a.keirn

USAACEH-60-14-AMAM-05 LIGITIMATE CODE FILECHANGE 65 REQUIREMENTS COMPLETED AT7182.3 ACFT HRS.

05-Apr-2014 1


vickie.l.meadows

USAACET/R CABLE TENSION CHECK COMPLETED 11JUN 14, L/H: 155, R/H: 155, TEMP: 28.7C.

13-Apr-2014 1


anthony.s.speigner


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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


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


anthony.s.speigner

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

29-Apr-2014 1


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


dean.a.keirn

USAACEH-60-14-AMAM-14 (IVHMS CABLING)REQUIREMENTS COMPLETED AT 7291.8 ACFTHRS (MWO NOT APPLIED)

28-May-2014 1


olivia.d.williams

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

04-Jun-2014 1


dean.a.keirn

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

06-Jun-2014 1


dean.a.keirn

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


anthony.s.speigner

USAACET/R CABLE TENSION CHECK COMPLETED 11JUN 2014, L/H: 155, R/H: 155, TEMP: 28.7C.

11-Jun-2014 2


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


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


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


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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


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


dean.a.keirn

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

31-Jul-2014 1


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


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


anthony.s.speigner

USAACEH-60-14-SOF-04 (OPERATORS ANDCREWMEMBERS CHECKLIST) C/W 27 AUG 14AT 7416.1 ACFRT. HRS.

27-Aug-2014 1


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


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


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


anthony.s.speigner

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

27-Oct-2014 1


dean.a.keirn

USAACEC/W H-60-15-SOF-01 (OIL COOLER FAN AXIALBEARING) ON 28OCT14 @ 7441.0 ACFT. HRS.

29-Oct-2014 1


frances.j.grace

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

03-Nov-2014 1


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 51 of 61

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

03-Nov-2014 2


dean.a.keirn

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

07-Nov-2014 1


dean.a.keirn

USAACEREQUIREMENTS OF H-60-14-AMAM-19 (ULLS-A(E), LCF, CHANGE 66) C/W @ 7460.4 ACFT HRS.

08-Nov-2014 1


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


frances.j.grace

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

25-Nov-2014 1


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


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


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


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


dean.a.keirn

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

11-Feb-2015 1


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


dean.a.keirn

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

27-Feb-2015 1


anthony.s.speigner

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

04-Mar-2015 1


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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


bryan.w.hollis

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

13-May-2015 1


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


bryan.w.hollis

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

28-May-2015 1


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


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


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


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


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


bryan.w.hollis

USAACEH-60-15-AMAM-14 LEGITIMATE CODE FILE(LCF) CHANGE 67 REQUIREMENTS C/W AT7654.8

25-Jul-2015 1


olivia.d.williams

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

28-Jul-2015 1


dean.a.keirn

DCR RASM-COCM/ACE PERFORMED AT 7655.8 AIRCRAFTHOURS BY TEAM MEMBER P

02-Sep-2015 1


jacob.a.weikart


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


nacona.l.hamilton

USAACEH-60-15AMAM-18 MEDVAC CAROUSEL C/W ON3OCT15

14-Oct-2015 1


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


marilyn.l.jones

USAACEACFT OPERATING IAW AWR 1965 R1, DATED16 SEPT 15 (APPLE IPAD DEVICES)SUPERSEDING ALL PRIOR REVISIONS

14-Oct-2015 3


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


nacona.l.hamilton

USAACEH-60-16-ASAM-01- INBOARD RETENTIONPLATE TORQUE CHECKS, COMPLIED WITH AT7659.6 ACFT HRS.

17-Nov-2015 1


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


christina.l.negron

USAACEACFT OPERATING IAW AWR 1251, R12 DTD30NOV15, EYEBOLTS ON BIFILAR,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.

01-Dec-2015 1


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


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


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


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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


dean.a.keirn

USAACEENTRY #1 DTD 07DEC15 SHOULD HAVEINCLUDED MR SPINDLE SN D001-11514

07-Dec-2015 2


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


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


christina.l.negron


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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


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


christina.l.negron

USAACEACFT OPERATING IAW AWR 1913 R1 DATED06 NOV 2015 (ACN ELECTRONIC LOGBOOK)

04-Jan-2016 1


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


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


chelsey.p.phillips

USAACEACFT NO LONGER OPERATING IAW AWR 1648(MAGNUS LAPTOP COMPUTER) AT ACFT HRS:7659.6 ACFT HRS.

05-Jan-2016 2


christina.l.negron

USAACEH-60-16-ASAM-02- DEFECTIVE FUEL HOSES,COMPLIED WITH AT 7659.6 ACFT HRS.PASSED.

06-Jan-2016 1


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


christina.l.negron

USAACEACFT OPERATING IAW AWR 1913, R1, DATED06 NOV 15 (ACN LOGBOOK). AT 7659.6 ACFTHRS.

07-Jan-2016 1


christina.l.negron


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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


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


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


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


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


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


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


brian.k.dow

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

17-Feb-2016 1


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


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


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


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


brian.k.dow

USAACEREPLACED NUMBER TWO CROSSFEEDVALVE ON 09 MAR 16 AT 7725.0 ACFT. HRS.

09-Mar-2016 1


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


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


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


brian.k.dow

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

01-Jun-2016 1


dean.a.keirn

USAACEACFT NO LONGER OPERATING IAW 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


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


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


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


brian.k.dow

USAACE48 MONTH 2408-18 INSPECTION A670, CABINTUB INSPECTION COMPLETED ON 27 JUN2016 AT 7984.0 ACFT. HRS.

27-Jun-2016 1


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


brian.k.dow

URS RASM-COCM/ACE PERFORMED AT 8030.6 AIRCRAFTHOURS BY TEAM MEMBERS P AND WW

08-Aug-2016 1


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


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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


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


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


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


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


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


brian.k.dow

USAACEACFT OPERATING IAW AWR 1693, R3 DTD28JAN16, RESA, SUPERSEDING ALL PRIORVERSIONS OF THIS AWR.

19-Sep-2016 2


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


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


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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


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


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1455, R6 DTD14OCT16, BATTELLE CAP, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR AND ISAQ123.

26-Oct-2016 1


dean.a.keirn

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

26-Oct-2016 2


joanna.n.lucier

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

27-Oct-2016 1


dean.a.keirn

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

01-Nov-2016 1


dean.a.keirn

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

12-Dec-2016 1


dean.a.keirn

USAACECOMPLIED WITH REQUIREMENTS OF H-60-17-AMAM-01, LCF CHANGE 68 ON 20 DEC 2016.

20-Dec-2016 1


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


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


brian.k.dow


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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


brian.k.dow

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

08-Mar-2017 1


dean.a.keirn

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

22-Mar-2017 2


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


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


dean.a.keirn

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

04-Apr-2017 1


thomas.e.mitchell

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

24-Apr-2017 1


dean.a.keirn

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


brian.k.dow


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


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


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


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


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


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


H-60-16-AMAM-07 (TAIL ROTOR SERVOSAFETY CABLE) NOT COMPLIED WITH

14-Sep-2017 1

HUNTSVILLE

robert.e.bridges


H-60-17-ASAM-11 (FUEL HOSE BORESCOPEINSPECTION) NOT COMPLIED WITH

14-Sep-2017 2

HUNTSVILLE

robert.e.bridges


H-60-17-AMAM-11 (ESM-2 PROGRAMIMPLEMENTATION) NOT COMPLIED WITH

14-Sep-2017 3

HUNTSVILLE

robert.e.bridges


H-60-17-ASAM-14 NOT COMPLIED WITH 03-Oct-2017 1

HUNTSVILLE

james.m.aldrich


H-60-17-AMAM-13 NOT COMPLIED WITH 03-Oct-2017 2

HUNTSVILLE

james.m.aldrich


H-60-17-ASAM-15 NOT COMPLIED WITH 03-Oct-2017 3

HUNTSVILLE

james.m.aldrich


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


DA FORM 2408-15-2, OCT 1991 AIRCRAFT VIBRATION RECORD




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






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






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 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






Page 5 of 10

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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 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






Page 6 of 10

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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






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 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 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






Page 8 of 10

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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






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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






Page 10 of 10

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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



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-


11.

O/H OR

10.


8.


Page 3 of 17


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.


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.


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.


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.


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


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 4 of 17


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.


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.


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.


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.


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


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 5 of 17


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


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.


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 6 of 17


hr)


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.


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.


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


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


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 7 of 17


hr)

LEAKING OIL.


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.


Page 8 of 17

CAO01521

GE-E-3064856035T02G01COLD SECTION MODULEGE-C-006623

6693

6002

14455

18830

15030

13425

3564

3523

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 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


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 10 of 17


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


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


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 11 of 17


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



Page 12 of 17

CAO01521

GE-C-0066233065T21G01OUTPUT SHAFT ASSYGGTA6574

6693

2

14455

151

15830

6

3564

2

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







EH-60A



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 13 of 17

04A01G 3065T21G01 OUTPUT SHAFT ASSY GGTA6574

hr)

0000

0000FCAY98036064T34P02NO 1 BALL BEARING

COND

COND

0000

0000FCAY58725121T46P02NO 2 ROLLER

COND

COND


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


Page 14 of 17

CAO01521

GE-E-3064856055T20G05MTCHD ROTOR/STATORMRS08937

5359

4105

13436

16609

12367

10142

2990

2401

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 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


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


Page 16 of 17

CAO01521

GE-E-3064856064T98G01POWER TURBINE MODULEGEL807552

6194

5092

14099

6087

14415

19263

3361

2639

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 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


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.



Page 1 of 16

CAO02124

85244656035T00G01T700-GE-700 ENGINE ASSYGE-E-207925

7211

6067

16745

14182

16209

16594

3498

3352

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 2 of 16


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


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 3 of 16


hr)

2466

3595UDC019634046T25G01COOLER, OIL

COND

COND

5565

0COMH134424046T28G14ANTI-ICE VALVE

COND

COND


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:


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 4 of 16


hr)

12441, INDEX: 16366, OP HRS: 5793) (ACFT 8023417 @ 5938.4 ACFT HRS)


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


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)


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)


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)



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 5 of 16


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.


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


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.



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 6 of 16


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.


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


Page 7 of 16

CAO02124

GE-E-2079256035T02G01COLD SECTION MODULEGE-C-006931

7211

3524

16745

14688

16209

6463

3497

1752

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 8 of 16


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


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 9 of 16


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


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



Page 10 of 16

CAO02124

GE-C-0069313065T21G01OUTPUT SHAFT ASSYGGAY9202

7211

1232

16745

4642

16209

1979

3497

547

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







EH-60A



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 11 of 16

04A01G 3065T21G01 OUTPUT SHAFT ASSY GGAY9202

hr)

122945511970544

0000FCAV41216064T34P02NO 1 BALL BEARING

COND

COND

122945511970544

26251819889481702FCAD65405121T46P02NO 2 ROLLER

COND

COND



Page 12 of 16

CAO02124

GE-E-2079256055T20G05MTCHD ROTOR/STATORMRSG3498

6736

3212

16649

1438

15262

8199

3284

1511

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 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


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)



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 14 of 16

04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRSG3498

hr)


Page 15 of 16

CAO02124

GE-E-2079256064T98G01POWER TURBINE MODULEGE-L-807448

5274

1834

16183

10781

10717

5923

2568

1737

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 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


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


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


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




8.DUE


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




Page 3 of 3




8.DUE


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




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


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


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


ENGINE COMPONENT OPERATING HOURS RECORDDA FORM 2408-19-3, DEC 1991

James.Aldrich

Highlight

James.Aldrich

Highlight

T/T I HIST RCDR S/NSERIAL NO. OP HRSLCF-2LCF-1POSHOURSAIRCRAFT AIRCRAFT ENGINE SERIAL NO. 13.12.11. 14.10.9.8.7.6.

(256)123-3456HUNTSVILLEK08DD23. UIC 5. TELEPHONE NUMBER4. LOCATION

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


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


EH-60A A265-01063 Days


HELICOPTER, UTILITY MAIN TRANSMISSION MODULE Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 1 of 1

a b

SUBMITTED

c a b



COMPONENTCHANGE

frances.j.grace13-Jun-2014NORMALBASELINE0.03730730013-Jun-2014


christina.l.negron26-Jan-2016ABNORMALROUTINE117.04089.67659.608-Jan-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:



0

480

7662.6

8524465 2398.2 7138


EH-60A A00603398 Days


HELICOPTER, UTILITY TAIL ROTOR GEARBOX ASSY Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 1 of 1

a b

SUBMITTED

c a b



COMPONENTCHANGE

anthony.s.speigner22-Jan-2014NORMALBASELINE0.01191713821-Jan-2014

anthony.s.speigner20-Feb-2014NORMALROUTINE42.01233718019-Feb-2014


christina.l.negron26-Jan-2016ABNORMALBASELINE2.51712.67659.608-Jan-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:



0

480

8055.4

8524465 578 0


EH-60A 886019 Days


HELICOPTER, UTILITY AUXILIARY POWER UNIT Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 1 of 1

a b

SUBMITTED

c a b



COMPONENTCHANGE

brian.k.dow25-Aug-2016NORMALBASELINE24.8258055.423-Aug-2016

brian.k.dow08-Aug-2017NORMALROUTINE256.6281.6831206-Aug-2017

9. REMARKS:



PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN -


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


EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1, OCT 1991

PIDMWODATE HRS



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


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



(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


COND COND

531501537465205A02H


COND COND

531501537465205A02H

24347660BLADE PIN, SOLID B9410922670103-08108-041 CCCC

COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


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


AND he SINCELIFE





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


COND COND

161501158578806H12


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



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE





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



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE




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



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE




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



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


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




AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 7 of 7Condition Change Components


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.


PIDMWODATE HRS



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



PIDMWODATE HRS



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



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



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






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


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.


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.



PIDMWODATE HRS



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


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


WOODWARD HYDRO-MECHANICALUNIT (HMU) P3 TUBE

H-60-13-ASAM-10MWO:

Priority Mnt Level



PIDMWODATE HRS



FUEL CONTROL 8524465154642141. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

05-Sep-2012 OM

jessica.n.kennedy05-Oct-2012


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


WOODWARD HYDRO-MECHANICALUNIT (HMU) P3 TUBE

H-60-13-ASAM-10MWO:

Priority Mnt Level



PIDMWODATE HRS



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



PIDMWODATE HRS



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



PIDMWODATE HRS



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



PIDMWODATE HRS



INPUT MODULE 8524465A264-003791. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

02-Aug-2000 OT


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



PIDMWODATE HRS



INPUT MODULE 8524465A264-021511. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

02-Aug-2000 OT


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



PIDMWODATE HRS



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)


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)


Priority Mnt Level



PIDMWODATE HRS



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



PIDMWODATE HRS



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



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE

PREVSER NO.ANDNOMENCLATURE P/N TIMEINST HRS

MENT DUEREPLACINST HRSNO.COMPONENT

NOMENREPLACE -

O/H ORCOMP6.

1615015033115MAIN TRANSMISSIONMODULE

70351-08100-076 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






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


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.


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.


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.



PIDMWODATE HRS



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



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



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






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


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.


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



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






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


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


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



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






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


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.


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.


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.


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


1GYRO, DIRECTIONAL - CN-998/ASN-43

U UUUUUUUU UU 00

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SIGNAL DATA CONVERTER - CV-3338A/ASN-128B

U UUUUUUUU UU 01

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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


1RECEIVER - R-2139/ARN-123(V)

U UUUUUUUU UU 11

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING - MT-4834/ARN-123(V)

U UUUUUUUU UU 11

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMMAND INSTR SYS PROCESSOR - 70600-01038-101

U UUUUUUUU UU 11

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING RACK - 70600-01038-102

U UUUUUUUU UU 11

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SAS AMPLIFIER - 70901-02908-104

U UUUUUUUU UU 11

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO ASSEMBLY - 70600-01047-041

U UUUUUUUU UU 11

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO - TRU-2A/A

U UUUUUUUU UU 11

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3MOUNT FOR TSEC/KY58 - S1660-60036-001

U UUUUUUUU UU 33

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3BATTERY FOR KY 58 - BA-1372/U

U UUUUUUUU UU 00

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3INTERFACE ADAPTER (KY-58) - Z-AHQ/TSEC

U UUUUUUUU UU 00

15

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

AIRCRAFT INVENTORY RECORDDA FORM 2408-17, NOV 1991



8524465 EH-60A


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


1AMPLIFIER IMPEDANCE - AM-4859A/ARN-89

U UUUUUUUU UU 11

17

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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


1VHF/AM ANTENNA FILTER - 70600-01012-102

U UUUUUUUU UU 11

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2VHF/AM ANTENNA FILTER - 70600-01011-103

U UUUUUUUU UU 22

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2ANTENNA - AS-3831/APN-209(V)

U UUUUUUUU UU 22

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GLIDE SLOPE ANTENNA - 70600-01043-101

U UUUUUUUU UU 11

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#2 VHF-FM, VHF-AM SENSE ANTENNA - 70600-01019-104

U UUUUUUUU UU 11

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2FIRST AID KIT - 6545-00-919-6650

U UUUUUUUU UU 00

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRE EXTINGUISHER - FR23-4-11848

U UUUUUUUU UU 00

25

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2BAROMETERIC ALTIMETER - AAU-32/A

U UUUUUUUU UU 22

26

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2CREW SEAT - D3801-2

U UUUUUUUU UU 33

27

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2AIRCRAFT CLOCK - ABU-11A

U UUUUUUUU UU 22

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER/TRANSMITTER - RT-1477/ARC-201

U UUUUUUUU UU 00

29

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2INTERPHONE CONTROL - C6533/ARC

U UUUUUUUU UU 22

30

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8524465 EH-60A


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


1INDICATOR ALTIMETER - ID-1917C/APN-209

U UUUUUUUU UU 11

32

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL RADIO SET - C-7392/ARN-89

U UUUUUUUU UU 11

33

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL - C-10604(V)6/ARN-186

U UUUUUUUU UU 00

34

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL - C-11466A/ARC-201

U UUUUUUUU UU 00

35

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPARATOR SIGNAL DATA - CM482/ARC186(V)

U UUUUUUUU UU 11

36

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3MOUNT - MT-6051/ARC-186

U UUUUUUUU UU 33

37

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER/TRANSMITTER - RT-1296A/APX-100

U UUUUUUUU UU 01

38

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CIVIL NAVIGATION CONTROL - C-10048/ARN-123(V)

U UUUUUUUU UU 11

39

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS SET CONTROLLER - C-8021E/ASN-75

U UUUUUUUU UU 00

40

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RADIO RETRANSMISSION PANEL -70550-01008-042

U UUUUUUUU UU 11

41

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MAGNETIC COMPASS - MS17983-4

U UUUUUUUU UU 11

42

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2OUTSIDE AIR TEMP INDICATOR - MS28028-1

U UUUUUUUU UU 22

43

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOUR WING PANEL - 70500-01152-093

U UUUUUUUU UU 00

44

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOUR WING PANEL - 70500-01152-094

U UUUUUUUU UU 00

45

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8524465 EH-60A


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


1CONTROL-INDICATOR ASN-132 C-11097/ASN-132

U UUUUUUUU UU 00

47

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SIGNAL DATA CONVERTER ASN-132CV-3739/ASN-132

U UUUUUUUU UU 00

48

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT FOR ASN-132 MT-4915/A

U UUUUUUUU UU 00

49

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1DATA PROCESS SET AN/UYK-64(V)2

U UUUUUUUU UU 00

50

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1TACAN RECEIVER/TRANSMITTER RT-1159/A

U UUUUUUUU UU 00

51

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ELECTRONIC SEQUENCE UNIT, 163290-100-E

U UUUUUUUU UU 11

52

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RADAR DETECTION SET SIGNAL AN/APR39

U UUUUUUUU UU 00

53

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IR JAMMER COUNTERMEASURES SET AN/ALQ-144(V)

U UUUUUUUU UU 00

54

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1DISPENSER GENERAL PURPOSE AIRCRAFT M130

U UUUUUUUU UU 00

55

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3SECURE SPEECH UNIT TSEC/KY-58

U UUUUUUUU UU 00

56

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3CONTROL INDICATOR (KY-58) C-8157/ARC

U UUUUUUUU UU 00

57

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1KY-100 AIRTERM 0N616736-1

U UUUUUUUU UU 00

58

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL DISPLAY UNIT C-12346/URC

U UUUUUUUU UU 00

59

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER




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)


GYRO, DIRECTIONAL - CN-998/ASN-43


GYRO, DIRECTIONAL - CN-998/ASN-43


SIGNAL DATA CONVERTER -CV-3338A/ASN-128B

2 REMOVED PER GOVT REQUEST4

BATTERY FOR KY 58 - BA-1372/U


BATTERY FOR KY 58 - BA-1372/U


INTERFACE ADAPTER (KY-58)- Z-AHQ/TSEC


INTERFACE ADAPTER (KY-58)- Z-AHQ/TSEC


REMOTE CONTROL UNIT (KY-58) - Z-AHP/YSEC


REVERSE OF DA FORM 2408-17, NOV 1991




db c


CHECK CHECK

ba ad

5. VERIFICATION

c



REMOTE CONTROL UNIT (KY-58) - Z-AHP/YSEC


#2 VHF-FM ANTENNACOUPLER - 70600-01010-104


#2 VHF-FM ANTENNACOUPLER - 70600-01010-104


FIRST AID KIT - 6545-00-919-6650


FIRST AID KIT - 6545-00-919-6650


FIRE EXTINGUISHER - FR23-4-11848




CREW SEAT - D3801-21 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION27

CREW SEAT - D3801-22 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION27

RECEIVER/TRANSMITTER - RT-1477/ARC-201


RECEIVER/TRANSMITTER - RT-1477/ARC-201






db c


CHECK CHECK

ba ad

5. VERIFICATION

c



CONTROL - C-10604(V)6/ARN-186


CONTROL - C-10604(V)6/ARN-186


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


COMPASS SET CONTROLLER- C-8021E/ASN-75


ARMOUR WING PANEL - 70500-01152-093










db c


CHECK CHECK

ba ad

5. VERIFICATION

c





CONTROL-INDICATOR ASN-132 C-11097/ASN-132


CONTROL-INDICATOR ASN-132 C-11097/ASN-132


SIGNAL DATA CONVERTERASN-132CV-3739/ASN-132


SIGNAL DATA CONVERTERASN-132CV-3739/ASN-132


MOUNT FOR ASN-132 MT-4915/A


MOUNT FOR ASN-132 MT-4915/A


DATA PROCESS SET AN/UYK-64(V)2


DATA PROCESS SET AN/UYK-64(V)2


TACANRECEIVER/TRANSMITTER RT-1159/A


TACANRECEIVER/TRANSMITTER RT-1159/A






db c


CHECK CHECK

ba ad

5. VERIFICATION

c



1159/A

RADAR DETECTION SETSIGNAL AN/APR39


RADAR DETECTION SETSIGNAL AN/APR39


IR JAMMERCOUNTERMEASURES SETAN/ALQ-144(V)


IR JAMMERCOUNTERMEASURES SETAN/ALQ-144(V)


DISPENSER GENERALPURPOSE AIRCRAFT M130


DISPENSER GENERALPURPOSE AIRCRAFT M130


SECURE SPEECH UNITTSEC/KY-58


SECURE SPEECH UNITTSEC/KY-58


CONTROL INDICATOR (KY-58)C-8157/ARC


CONTROL INDICATOR (KY-58)C-8157/ARC






db c


CHECK CHECK

ba ad

5. VERIFICATION

c



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


CONTROL DISPLAY UNIT C-12346/URC



SECTION II CABINEH-60A_BASELINE


8524465 EH-60A


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


1BEARING, DISTANCE, HEADING INDICATOR - ID2301/U

U UUUUUUUU UU 00

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MARKER BEACON ANTENNA - 70600-02011-103

U UUUUUUUU UU 11

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-104

U UUUUUUUU UU 11

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-105

U UUUUUUUU UU 11

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRST AID KIT - 6545-00919-6650

U UUUUUUUU UU 00

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRE EXTINGUISHER - FR23-4-11848

U UUUUUUUU UU 00

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CRASH AXE - 56D6221

U UUUUUUUU UU 11

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HAND SET - H-250/U

U UUUUUUUU UU 11

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SLAB BATTERY - D8565/11-1

U UUUUUUUU UU 11

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3INTERPHONE CONTROL - C6533/ARC

U UUUUUUUU UU 33

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ADAPTER FUEL DRAIN - 70307-03018-102

U UUUUUUUU UU 00

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


4LOCK ASSY BLADE TIEDOWN - 70700-20369-041

U UUUUUUUU UU 00

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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


2PLUG ASSY EXHAUST - HIRSS - 70700-20515-043

U UUUUUUUU UU 00

15

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER




SECTION II CABINEH-60A_BASELINE


8524465 EH-60A


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


1COVER ASSY OIL COOLER - 70700-20511-041

U UUUUUUUU UU 00

17

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BLADE FOLD SET - 70700-20412-011

U UUUUUUUU UU 00

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER PITOT TUBE - 70700-20460-041

U UUUUUUUU UU 00

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1TROOP SEATS - 70500-02151-045

U UUUUUUUU UU 00

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER ENGINE INLET - 83DSCC-D006

U UUUUUUUU UU 00

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FITTING ASSEMBLY - L/H - 70751-02023-043

U UUUUUUUU UU 00

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FITTING ASSEMBLY - R/H - 70751-02023-044

U UUUUUUUU UU 00

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ICS WALK-AROUND CORD - 70602-02023-044

U UUUUUUUU UU 00

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PORTABLE INSP. FLOOD LIGHT - 15-0366-1

U UUUUUUUU UU 00

25

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HYD. PUMP HANDLE - 15400-50126

U UUUUUUUU UU 11

26

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2EQUIPMENT LOGBOOK - MIL-D-43064

U UUUUUUUU UU 22

27

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPUTER LOGBOOK

U UUUUUUUU UU 01

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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


4TIEDOWN ASSEMBLY, TOW - 70700-20433-045

U UUUUUUUU UU 00

30

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8524465 EH-60A_BASELIN SECTION II CABINEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c





a. ITEM NUMBER

Nomenclature

INERTIAL NAVIGATION SET -AN/ASN-141


INERTIAL NAVIGATION SET -AN/ASN-141


BEARING, DISTANCE,HEADING INDICATOR -ID2301/U


BEARING, DISTANCE,HEADING INDICATOR -ID2301/U


FIRST AID KIT - 6545-00919-6650


FIRST AID KIT - 6545-00919-6650






ADAPTER FUEL DRAIN - 70307-03018-102


ADAPTER FUEL DRAIN - 70307-03018-102






db c


CHECK CHECK

ba ad

5. VERIFICATION

c



LOCK ASSY BLADE TIEDOWN- 70700-20369-041


LOCK ASSY BLADE TIEDOWN- 70700-20369-041


PLUG ASSY INTAKE - HIRSSSUPP - 70700-20515-041/042


PLUG ASSY INTAKE - HIRSSSUPP - 70700-20515-041/042


PLUG ASSY EXHAUST - HIRSS- 70700-20515-043


PLUG ASSY EXHAUST - HIRSS- 70700-20515-043


PLUG ASSY APU EXHAUST -70700-20509-041


PLUG ASSY APU EXHAUST -70700-20509-041


COVER ASSY OIL COOLER -70700-20511-041


COVER ASSY OIL COOLER -70700-20511-041


BLADE FOLD SET - 70700-20412-011






db c


CHECK CHECK

ba ad

5. VERIFICATION

c



BLADE FOLD SET - 70700-20412-011


COVER PITOT TUBE - 70700-20460-041


COVER PITOT TUBE - 70700-20460-041


TROOP SEATS - 70500-02151-045


TROOP SEATS - 70500-02151-045


COVER ENGINE INLET -83DSCC-D006


COVER ENGINE INLET -83DSCC-D006


FITTING ASSEMBLY - L/H -70751-02023-043


FITTING ASSEMBLY - L/H -70751-02023-043


FITTING ASSEMBLY - R/H -70751-02023-044






db c


CHECK CHECK

ba ad

5. VERIFICATION

c



FITTING ASSEMBLY - R/H -70751-02023-044


ICS WALK-AROUND CORD -70602-02023-044


ICS WALK-AROUND CORD -70602-02023-044


PORTABLE INSP. FLOODLIGHT - 15-0366-1


PORTABLE INSP. FLOODLIGHT - 15-0366-1


EQUIPMENT LOGBOOK - MIL-D-43064

1 AIRCRAFT ARRIVED IN CURRENT CONFIGURSATION27

COMPUTER LOGBOOK2 REMOVED PER GOVT REQUEST28

TIEDOWN ASSEMBLY, TOW -70700-20433-045


TIEDOWN ASSEMBLY, TOW -70700-20433-045



SECTION III TRANSITION SECTIONEH-60A_BASELINE


8524465 EH-60A


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


2IFF ANTENNA - 70600-02010-103

U UUUUUUUU UU 22

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF/AM ANTENNA 70600-03002-104

U UUUUUUUU UU 11

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PUMP FUEL SAMPLER - 82829/4P156-3

U UUUUUUUU UU 00

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPENSATOR MAGNETIC FLUX - CN-405/ASN

U UUUUUUUU UU 11

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS TRANSMITTER - T-611/ASN

U UUUUUUUU UU 11

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GPS ANTENNA 22433-40

U UUUUUUUU UU 11

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF AMPLIFIER COUPLER AM-7531/URC

U UUUUUUUU UU 00

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER/TRANSMITTER RT-1749/URC

U UUUUUUUU UU 00

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8524465 EH-60A_BASELIN SECTION III TRANSITION SECTIONEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c





a. ITEM NUMBER

Nomenclature

PUMP FUEL SAMPLER -82829/4P156-3


PUMP FUEL SAMPLER -82829/4P156-3


HF AMPLIFIER COUPLER AM-7531/URC


HF AMPLIFIER COUPLER AM-7531/URC


RECEIVER/TRANSMITTER RT-1749/URC


RECEIVER/TRANSMITTER RT-1749/URC



SECTION IV TAIL CONEEH-60A_BASELINE


8524465 EH-60A


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


1HF ANTENNA 4700516-30

U UUUUUUUU UU 00

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8524465 EH-60A_BASELIN SECTION IV TAIL CONEEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c





a. ITEM NUMBER

Nomenclature

HF ANTENNA 4700516-301 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION2

HF ANTENNA 4700516-302 AIRCRAFT ARRIVED IN CURRENT CONFIGURATION2


SECTION V TAIL ROTOR PYLONEH-60A_BASELINE


8524465 EH-60A


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


1#1 VHF-FM ANTENNA - 70600-06002-105

U UUUUUUUU UU 11

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8524465 EH-60A_BASELIN SECTION V TAIL ROTOR PYLONEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c





a. ITEM NUMBER

Nomenclature


PIDMWODATE HRS



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



PIDMWODATE HRS



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


0.5USAAWC, FTRUCKER, AL(BH0315)

ALL UH-60A, UH-60L, EH-60A,REMOVAL OF SPECIFIC SUSPECTREWORKED MAIN ROTORSWASHPLATE ASSEMBLIES


Priority Mnt Level

12-Jun-2006 OM


2.0USAAWC, FT.RUCKER, AL(BH0315)

ALL H-60 SERIES AIRCRAFT,SWASHPLATE DUPLEX BEARING


Priority Mnt Level



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



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






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


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.



PIDMWODATE HRS



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


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


1.0CCAD N/A(PM6697)

INSTALLATION OF SELF SEALADAPTER ASSEMBLY

55-2840-248-50-28MWO:

Priority Mnt Level

25-Jan-1991 DN


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


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


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


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


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


1.0CCAD N/A(PM6697)

ALL UH-60A AND EH-60A SERIESHELICOPTERS, ONE TIMEINSPECTION OF ALL T700-GE-700ENGINE RECORDS


Priority Mnt Level


1.0CCAD N/A(PM6697)

ALL AH-64 AND UH-60 SERIESAIRCRAFT - ONE TIME INSPECTIONOF T700-GE-700/701/701C ENGINES




PIDMWODATE HRS




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


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



PIDMWODATE HRS




Page 1 of 2

15-Feb-1987 OM


0.5CCAD (LF3674)ONE TIME INSPECTION OF TORQUEFUEL DIFFER PRESSUREINDICATOR

55-2840-248-50-44MWO:

Priority Mnt Level

31-Jul-1989 OM


33.0CCAD (LF3674)MODIFICATION OF GG ROTORASSEMBLY T700/701 REWORK T700ENGINES

55-2840-248-50-32MWO:

Priority Mnt Level

15-Aug-1990 OM


1.0CCAD (LF3674)INSTALLATION OF SELF SEALADAPTER ASSEMBLY

55-2840-248-50-28MWO:

Priority Mnt Level

25-Jan-1991 DN


20.0CCAD (LF3674)MODIFICATION OF POWER TAKEOFFDRIVE ASSEMBLY P/N 5044T27G01

55-2840-248-50-27MWO:

Priority Mnt Level

31-Mar-1993 DR


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


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


Priority Mnt Level

16-Jul-2007 OM


0.5AC CO (MP8963)ALL H-60A SERIES AIRCRAFT,HAMILTON-SUNDSTRAND HYDRO-MECHANICAL UNITS (HMU'S)


Priority Mnt Level

13-Aug-2007 OM


0.5DS2 (RT0477)ALL H-60 SERIES AIRCRAFT, MAINFUEL MANIFOLD CHAFING


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:



PIDMWODATE HRS




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



PIDMWODATE HRS



TAIL ROTOR GEARBOX ASSY 8524465A006033981. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

21-Mar-2013 FM

QC00000018-Jan-2014


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



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



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






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


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.



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



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






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


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.


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.


16-Dec-2015 2 INSTALLED ON ACFT. 8524465 AT 7660 ACFT. HRS. WITH TTSN: 1220, TSO: 719, 2 PREV. O/H.



PIDMWODATE HRS



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



UNIT UNIQUE INVENTORY ITEMSEH-60A_BASELINE


8524465 EH-60A


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


1R-2594/ARN-147(V) RECEIVER

U UUUUUUUU UU 00

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RT1836C/APX-118 TRANSPONDER

U UUUUUUUU UU 00

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1AN/APX-118 CONTROL

U UUUUUUUU UU 00

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IFM AMPLIFIER AM-7189A/ARC

U UUUUUUUU UU 00

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT IFM AMPLIFIER PN: MT-6592/ARC

U UUUUUUUU UU 11

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BFT ANTENNA GPS PN:S671575-863

U UUUUUUUU UU 11

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8524465 EH-60A_BASELIN UNIT UNIQUE INVENTORY ITEMSEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c





a. ITEM NUMBER

Nomenclature

ATTITUDE AND HEADINGREFERENCE UNIT (CN1716/A)


ATTITUDE AND HEADINGREFERENCE UNIT (CN1716/A)


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


RT1836C/APX-118TRANSPONDER


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



8524465 EH-60A_BASELIN UNIT UNIQUE INVENTORY ITEMSEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c




Documents

1. NOMENCLATURE 2. MODEL 3. AIRCRAFT SERIAL NUMBER