1. NOMENCLATURE 2. MODEL 3. AIRCRAFT SERIAL ... UTILITY EH-60A 8624564 1. NOMENCLATURE 2. MODEL 3....

PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN

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

8624564EH-60AHELICOPTER, UTILITY

3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE

of 4

DR25-Jan-2007

(NOORGANIZATION/PID)

0.0 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

DR21-Jun-2004

USAAWC, FT.RUCKER, AL(RJ0827)

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

DU10-Aug-1987

DYNCORP OLR,FT. HOOD, TX(G.P 'P/C/W')

6.001-AUG-1987

LILLY, THOMASM

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

55-1520-237-50-46MWO:

Mnt LevelPriority

DO04-Apr-1986

LSMAC CA-AVCRAD (E.G.)

5.001-NOV-1989

LILLY, THOMASM

INSTALLATION OF MODIFIED OILSHIELDS

55-1520-237-50-53MWO:

Mnt LevelPriority

DN15-Jan-1989

LSMAC, CA-AVCRAD (E.G.)

12.001-NOV-1989

LILLY, THOMASM

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

1-5945-237-50-1MWO:

Mnt LevelPriority

DM21-Jun-2006

CSC, USAACE,FT. RUCKER, AL

200.004-Mar-2010

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

DM22-Feb-1991

DYNCORP OLR,FT. HOOD, TX.(HENRY K)

832.005-MAR-1993

LILLY, THOMASM

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

1-1520-237-50-59MWO:

Mnt LevelPriority

DM01-Sep-1991


2.005-MAR-1993

LILLY, THOMASM

IMPROVED ENGINE COWLINGRELEASE HANDLE ASSEMBLY

1-1520-237-50-64MWO:

Mnt LevelPriority

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

DA FORM 2408-5, AUG 2004 EQUIPMENT MODIFICATION RECORD

PIDMWODATE HRS





of 4

DN01-Aug-1991


3.505-MAR-1993

LILLY, THOMASM

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

Mnt LevelPriority

DN16-Oct-1989


24.005-MAR-1993

LILLY, THOMASM

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

55-1520-237-50-49MWO:

Mnt LevelPriority

DN09-Jun-1988

PROJECT OLRLSSI (D.S.)

124.008-NOV-1990

LILLY, THOMASM

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

55-1520-237-50-42MWO:

Mnt LevelPriority

DM15-Nov-1989

PROJECT OLRLSSI (D.S.)

22.008-NOV-1990

LILLY, THOMASM

MODIFICATION OF DOWEL PINRETENTION MAIN GEARBOX

55-1520-237-50-43MWO:

Mnt LevelPriority

DN01-Oct-1988

TRAEOK,AEROSPACE(JAMES H.)

11.008-SEP-1989

LILLY, THOMASM

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

55-1520-237-55-6MWO:

Mnt LevelPriority

DN30-Apr-1997

LM2/OLR(S.SCOTT)

60.008-SEP-1999

LILLY, THOMASM

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

1-1520-237-50-56MWO:

Mnt LevelPriority

DN31-Oct-1996

LM2/OLR(S.SCOTT)

30.008-SEP-1999

LILLY, THOMASM

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

1-1520-237-50-74MWO:

Mnt LevelPriority

DR11-Aug-2000

LM2/OLR(S.SCOTT)

6.011-JUN-1999

LILLY, THOMASM

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

1-1520-237-50-79MWO:

Mnt LevelPriority

DN15-Nov-1990

DYNCORP OLR,FT. HOOD, TX(F.C.)

4.014-DEC-1992

LILLY, THOMASM

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

1-1520-237-50-61MWO:

Mnt LevelPriority



PIDMWODATE HRS





of 4

DN01-May-1994

LSSI,PROJ.OLR.(J.L.)

140.014-DEC-1994

LILLY, THOMASM

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

1-1520-237-50-66MWO:

Mnt LevelPriority

OT14-May-1987

SIKORSKY,78286(BRENDAWALSH)

1.014-MAR-1987

LILLY, THOMASM

INSPECTION OF TAIL ROTORDRIVESHAFT SPLINE COUPLINGS

55-1520-237-20-89MWO:

Mnt LevelPriority

DN24-Mar-1988

DYNCORP OLR,FT. HOOD, TX(G.P 'P/C/W')

67.015-APR-1988

LILLY, THOMASM

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

55-1520-237-50-47MWO:

Mnt LevelPriority

DN17-Jun-1989

DYNCORP OLRFT. HOOD.TX(G.P 'P/C/W')

6.015-JUN-1991

LILLY, THOMASM

INCOROPORATION OF EXHAUSTEXTENDER DOUBLERS

55-1520-237-50-51MWO:

Mnt LevelPriority

DR05-Jan-2010

CSC, FTRUCKER, AL

200.020-May-2010

J, BINSTALLATION OF BLUE FORCETRACKING (BFT) ON EH60HELICOPTERS

EH-60-001MWO:

Mnt LevelPriority

DR01-Jul-2008

CSC, FTRUCKER, AL

39.020-May-2010

J, BINSTALLATION OF ELECTRONIC DATAMANAGEMENT SYSTEM (EDM) FORBLUE FORCE TRACKING (BFT)

RSN LSF01106MWO:

Mnt LevelPriority

DR03-Dec-2005

CSC/USAACE,FT. RCUKER, AL.(JB2761)

39.020-MAY-2010

LILLY, THOMASM

INSTALLATION OF ELECTRONIC DATAMANAGEMENT (EDM) SYSTEM FORBLUE FORCE TRACKING

1-1520-237-50-EDMMWO:

Mnt LevelPriority

DU31-May-1995

LM2/OLR(CSMITH)

16.020-NOV-1995

LILLY, THOMASM

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

1-1520-237-50-73MWO:

Mnt LevelPriority

DN30-Jun-2004

USAAWC, FT.RUCKER, AL(RJ0827)

90.025-Jul-2011

LILLY, THOMASM

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

1-1520-237-50-92MWO:

Mnt LevelPriority

FR02-Nov-2009

USAACE 16.025-Jun-2013

STRICKLAND,WILLIAM A

SINGLE INSTALLATION OF ATTITUDEHEADING REFERENCE UNIO (AHRU)

1-1520-237-20-2MWO:

Mnt LevelPriority



PIDMWODATE HRS





of 4

DR13-Apr-2001

USAATTC, FT.RUCKER, AL.(AFS201, SNOLIN, 2938)

80.027-MAY-2004

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

DN01-Feb-1993

LSSI,PROJ.OLR.(JL)

400.030-AUG-1994

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



NUMBER PIDENTRY

ORGANIZATION LOCATION8.7.

DATE6.

REMARKS4. 5.

EH-60A 8624564HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL

Page 1 of 64

NO ORGANIZATIONNOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR., 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 (JB2761 'PCW')

05-Nov-1984 1

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONOH-60A-84-01 NOT APPLICCABLE TO THISACFT (JB2761 'PCW')

05-Nov-1984 2

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONUH-60A-84-03 APPLIES TO UH-60A AIRCRAFTSERIAL NUMBER 77-22714 THROUGH 82-23671(JB2761 'PCW')

05-Nov-1984 3

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 4

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONUH-60A-84-05- MAINTENANCE MANDATORY,RECORDING, AND REPORTING NONE (JB2761'PCW')

05-Nov-1984 5

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 6

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONUH-60A-84-10 APPLIES TO UH-60A AIRCRAFTSERIAL NUMBER 77-22714 THROUGH 82-23882ONE TIME INSPECTION OR WHENEVER PYLONIS FOLDED (JB2761 'PCW')

05-Nov-1984 7

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 8

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 9

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 10

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONUH-60A-84-14 APPLIES TO UH-60A AIRCRAFTSERIAL NUMBER 84-23970 (JB2761 'PCW')

05-Nov-1984 11

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 12

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 13

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 14

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 15

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 16

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 17

(NO LOCATION)

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 64


05-Nov-1984 18

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONUH-60A-85-07 NOT APLICABLE TO THISAIRCRAFT (JB2761 'PCW')

05-Nov-1984 19

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONUH-60A-85-08- NOT APPLICABLE TO THISAIRCRAFT (JB2761 'PCW')

05-Nov-1984 20

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 21

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 22

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 23

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 24

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 25

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 26

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 27

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 28

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 29

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONUH-60A-85-18 APPLIES TO UH-60A AIRCRAFTSERIAL NUMBER 77-22714 THROUGH 85-24403, 85-24405, AND 85-24406 (JB2761 'PCW')

05-Nov-1984 30

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 31

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONUH-60A-85-20 SUPERSEDED BY S.O.F. MSG UH-60A-85-21 (JB2761 'PCW')

05-Nov-1984 32

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 33

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 34

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 35

(NO LOCATION)

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 3 of 64


05-Nov-1984 36

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 37

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 38

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 39

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 40

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 41

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 42

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 43

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 44

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONUH-60A-84-07 NOT APPLICABLE TO THISAIRCRAFT (JB2761 'PCW')

05-Nov-1984 45

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 46

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 47

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 48

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONUH-60A-86-10- APPLIES TO UH-60A AIRCRAFTSERIAL NUMBER 77-22714 THROUGH 84-24016(JB2761 'PCW')

05-Nov-1984 49

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 50

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONUH-60A-86-11 NOT APPLICABLE TO THISAIRCRAFT 9SEE MSG. UH-60A-86-07) (JB2761'PCW')

05-Nov-1984 51

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 52

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 53

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 54

(NO LOCATION)

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 4 of 64


05-Nov-1984 55

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 56

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 57

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 58

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 59

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 60

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 61

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 62

(NO LOCATION)

thomas.m.lilly


05-Nov-1984 63

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONNOTE: WAIVERS THAT ARE APPLICABLELISTED FOR REFERENCE PURPOSES ASDIRECTED BY NAVPRO LTR., 4855 SER QAV/84-272 DATED 5 NOVEMBER 1984 (JB2761 'PCW')

05-Nov-1984 64

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONWAIVER (WOO37)- AUTHORIZATION FORDELIVERY OF UNQUALIFIED ANTENNACOUPLERS AND LOW PASS FILTERS ANDINSTALLATION OF ARC-186 RADIO SETS (AIRCRAFT 570 AND SUBSEQUENT) (JB2761'PCW')

05-Nov-1984 65

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONWAIVER (WOO43)- AUTHORIATION FORDELIVERY OF AIRCRAFT WITH ARC-186 RADIOSETS PRIOR TO APPROVAL OFELECTOMAGNETIC COMPATABILITY (EMC)TESTING (JB2761 'PCW')

05-Nov-1984 66

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONWAIVER (W0056)- USE OF ALTERNATESOURCE WINDSHIELD ANTI-ICECONTROLLERS (JB2761 'PCW')

05-Nov-1984 67

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONWAIVER (W0060R1)- ACCEPTANCE OFAIRCRAFT, MAIN ROTOR SPINDLE, MAINROTOR BLADE CUFF, MAIN ROTOR HUB, MAINROTOR CONTROL HORN AND MAIN ROTORSHAFT (JB2761 'PCW')

05-Nov-1984 68

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONWAIVER (W0066)- ANVIS COMPATIBLELIGHTING SYSTEM COMPONENTS (JB2761'PCW')

05-Nov-1984 69

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONWAIVER (W0063)- UNQUALIFIEDENVIRONMENTAL CONTROL SYSTEM (ECS)UNIT (JB2761 'PCW')

05-Nov-1984 70

(NO LOCATION)

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 5 of 64

NO ORGANIZATIONWAIVER (W0067)- DELIVERY OF EH-60AAIRCRAFT WITH UNQUALIFIED CONPONENTSINSTALLED (JB2761 'PCW')

05-Nov-1984 71

(NO LOCATION)

thomas.m.lilly

NO ORGANIZATIONWAIVER (W0072) - EYE BOLTS- MAINTENANCECRANE AND TIE DOWN RING SYSTEMS(JB2761 'PCW')

05-Nov-1984 72

(NO LOCATION)

thomas.m.lilly

SIKORSKY AIRCRAFTUH-60A-83-12 (TB 55-1520-237-20-46)INSPECTION OF TAIL ROTOR ASSY FOR BENTSERVO VALVE INPUT STEM COMPLIED WITH(JAMES KRETZ)

21-Jan-1987 1

STRATFORD, CT

thomas.m.lilly

SIKORSKY AIRCRAFTAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG. 70400-0003 REV.E. SYSTEMS CONTROLS HAVE BEEN BIASEDIN ACCORD. A. AFT CONTROL SERVO INPUTROD HAS BEEN LENGTHENED 1/2 TURN. B.LATERAL CONTROL SERVO INPUT ROD HASBEEN SHORTENED 1/4 TURN. C. FORWARDCONTROL SERVO INPUT ROD HAS BEENSHORTENED 1/2 TURN. NOTE: WHENAIRCRAFT RIGGING IS BIASED RIGGING ISBIASED RIGGING PIN HOLES ARETEMPORARILY LOST AT THE ABOVE 3 POINTS.(JAMES KRETZ)

22-Jan-1987 1

STRATFORD, CT

thomas.m.lilly

SIKORSKY AIRCRAFTUH-60A-84-02 (TB 55-1520-237-20-48) ONE TIMEINSPECTION OF WIRE HARNESS ROUTINGFOR FEEDER HARNESS BETWEEN NO. 1 ANDNO. 2 JUNCTION BOXES COMPLIED WITH.(JAMES KRETZ)

31-Jan-1987 1

STRATFORD, CT

thomas.m.lilly

102ND USARASFREMOVED BEARING DISTANCE HEADINGINDICATOR, ID-2301/U, PER MSG #270800Z,FEB 87 (EC3971)

01-Feb-1987 1

SCOTT AFB, IL

thomas.m.lilly

SIKORSKY AIRCRAFTUH-60A-85-02 SAFETY OF FLIGHTMAINTENANCE MANDATORY TO CHANGE THEAUTOROTATION RPM LIMITS COMPLIED WITH(JAMES KRETZ)

10-Feb-1987 1

STRATFORD, CT

thomas.m.lilly

SIKORSKY AIRCRAFTUH-60A-86-21 (TB 55-1520-238-20-85 ONE TIMEINSPECTION OF CREW SEATS FORLONGITUDINAL MOVEMENT OF LOCK PINADJUSTMENT COMPLIED WITH (JAMESKRETZ)

13-Feb-1987 1

STRATFORD, CT

thomas.m.lilly

SIKORSKY AIRCRAFTCOMPLIED WITH S.O.F. MSG 132215Z MAR. 87(UH-60A-87-03) TB 55-1520-237-20-89 -ONETIME AND RECURRING INSPECTIONS ON THEFIRST THREE TAIL ROTOR DRIVESHAFTSPLINE COUPLINGS. (BRENDA WALSH)

14-Mar-1987 1

STRATFORD, CT

thomas.m.lilly

SIKORSKY AIRCRAFTCOMPLIED WITH S.O.F. MSG 242300Z MARCH87 (UH-60A-87-04) -UH-06A/EH-60A AIRCRAFT,REVISION TO INSPECTION OF EYEBOLT P/N70209-02136-102 (SSMITH)

27-Mar-1987 1

STRATFORD, CT

thomas.m.lilly

102ND USARASFSOF MSG UH-60A-87-01 ONE TIME TORQUEVLAADATION OF ENGINE FUEL PRESSUREINDICATOR. COMPLIED WITH (BR6249)

01-Apr-1987 1

SCOTT AFB IL

thomas.m.lilly

102ND USARASFSOF MSG UH-60A-87-02 CORRECTION OF MSGUH-60A-87-01 TB NUMBER COMPLIED WITH(BR6249)

01-Apr-1987 2

SCOTT AFB, IL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 6 of 64

102ND USARASFSOF MSG UH-60A-87-05 STABILSTOROPERATION PROCEDURES, ACFT HAS BEENRESTRICTED PER THIS SOF MGS. (BR6249)

16-Apr-1987 1

SCOTT AFB, IL

thomas.m.lilly

102ND USARASFSOF MSG UH-60A-87-06, TB 55-1520-237-50-2,ONE TIME AND RECURRING INSPECTION OFOIL COOLER SPLINES AND INSTALLATION OFSPLINES WEAR INDICATOR, COMPLIED WITH42.5 HRS LONG AXIS .10 VERTICAL AXIS .10OIL COOLERS/N 02870057. (BR6249)

04-May-1987 1

SCOTT AFB, IL

thomas.m.lilly

102ND USARASFSOF MSG UH-60A-87-07, TB 55-1520-237-20-90,ONE TIME AND RECURRING INSPECTION OF 2LONGITUDINAL LINK ASSEMBLIES AND ONELATERAL CLEVIS ASSEMBLY FOR INNERRACE BEARING CRACKS COMPLIED WITH(BR6249)

26-May-1987 1

SCOTT AFB, IL

thomas.m.lilly

102ND USARASFGENERAL SOF MSG (GEN-87-02), TB 55-1500-200-20-25, LOCAL PURCHASE OF TIMECHANGE AIRCRAFT COMPONENTS/PARTSCOMPLIED WITH 87-07-07 (BR6249)

07-Jul-1987 1

SCOTT AFB, IL

thomas.m.lilly

102ND USARASFSOF MSG UH-60A-87-08, TB 55-1520-237-20-91,ONE TIME INSPECTION OF MIDSECTIONBELLCRANK ASSEMBLIES COMPLIED WITH(BR6249)

08-Jul-1987 1

SCOTT AFB, IL

thomas.m.lilly

102ND USARASFOCM/ACE PERFORMED AT 56 ACFT HRS BYACE TEAM MEMBER N. EASTMAN, AVSCOMOCMSEC, ST LOUIS MO (BR6249)

23-Aug-1987 1

SCOTT AFB, IL

thomas.m.lilly

102ND USARASFSOF MSG UH-60A-87-10, TB 55-1520-237-20-92ONE TIME INSPECTION OF INPUT FLANGEASSEMBLY. COMPLIED WITH (AZ6716)

18-Oct-1987 1

SCOTT AFB, IL

thomas.m.lilly

102ND USARASFSOF MSG UH-60A-87-11 TB 55-1520-237-20-94,ONE TIME INSPECTION OF CARGO DOORUPPER AND LOWER ROLLER SUPPORTASSEMBLIES. COMPLIED WITH 87-11-04(AZ6716)

04-Nov-1987 1

SCOTT AFB, IL

thomas.m.lilly

102ND USARASFSOF MSG UH-60A-87-09, MWO 55-1520-237-50-46, INSTALLATION OF CYCLIC STABILATORSLEW UP SWITCH PROVISION FOR LEARINGOF SOF MSG UH-60A-87-05. COMPLIED WITH87-11-27. (AZ6716)

27-Nov-1987 1

SCOTT AFB, IL

thomas.m.lilly

102ND USARASFSOF MSG UH-60A-87-12, ONE TIMEINSPECTION FOR DEFECTIVE T700-GE-700/701ENGINE POWER TURBINE MODULES C/W 87-12-03 (AZ6716)

03-Dec-1987 1

SCOTT AFB, IL

thomas.m.lilly

102ND USARASFSOF MSG UH-60A-88-01 ONE TIMEINSPECTION FOR CERTAIN SERIAL NUMBERTAIL ROTOR BLADE ASSEMBLIES C/W 88-02-17 (NB4724)

17-Feb-1988 1

SCOTT AFB, IL

thomas.m.lilly

102ND USAFASF55-1520-237-20-96 (UH-60-88-02) INSP OF TAILROTOR GEARBOX OUTPUT SHAFT.C/W 88-03-23 (BR6249)

23-Mar-1988 1

SCOTT AFB, IL

thomas.m.lilly

USAAVNDTA,55-1520-237-20-102 (UH-60-88-13) INSP. OF M/RBLADE EXPENDABLE RETENTION PIN FORMISSING SEGMENTS C/W (B ARMSTRONG,CIV)

21-Nov-1988 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 7 of 64

USAAVNDTASIKORSKY MOD KIT 70070-20154-011, SELFINSTALLATION, UHF DIPLEXER, APPLIED. (BARMSTRONG, CIV)

01-Dec-1988 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNDTASIKORSKY MOD KIT 70070-20151-012, RHCARGO DOOR SEAL, APPLIED (BARMSTRONG, CIV)

01-Dec-1988 2

FT. RUCKER, AL

thomas.m.lilly

USAAVNDTASIKORSKY MOD KIT 70070-20151-011, SEALINSTALLATION & INTERIOR, APPLIED. (BARMSTRONG, CIV)

09-Dec-1988 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNDTASIKORSKY MOD KIT 70070-20151-013, DUCTINSTALLATION (LHS), APPLIED (BARMSTRONG, CIV)

16-Dec-1988 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNDTAEXTERNAL STORES SUPPORT SYSTEM (ESSS)REMOVED (B ARMSTRONG, CIV)

08-Jan-1989 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNDTASIKORSKY MOD KIT 70070-55119-011,HARNESS ASSEMBLY, DIPLEXER, APPLIED (BARMSTRONG, CIV)

09-Jan-1989 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNDTAS.O.F. MESSAGE UH-60-86-18, RAPPLEINGOPERATIONS, SEE S.O.F. MGS EH-60-88-11. (BARMSTRONG, CIV)

09-Jan-1989 2

FT. RUCKER, AL

thomas.m.lilly

USAAVNDTAS.O.F. MESSAGE UH-60-88-07 C/W, SEE S.O.F.MESSAGE UH-60-88-05. (B ARMSTRONG, CIV)

09-Jan-1989 3

FT. RUCKER, AL

thomas.m.lilly

USAAVNDTAS.O.F.MESSAGE UH-60-88-08 ACFT REVISIONTO OVERHAUL LIFE FOR THE XMSN OILCOOLER, PCW. (SEE ACFT 2408-16) (BARMSTRONG, CIV)

09-Jan-1989 4

FT. RUCKER, AL

thomas.m.lilly

USAAVNDTAS.O.F. MESSAGE UH-60-84-05, MAINT.MANDATORY RECORDING, REPORTING NONE.(B ARMSTRONG, CIV)

09-Jan-1989 5

FT. RUCKER, AL

thomas.m.lilly

USAAVNDTAUH-60-88-12, NA TO EH-60 (B ARMSTRONG,CIV)

09-Jan-1989 6

FT. RUCKER, AL

thomas.m.lilly

USAAVNDTAUH-60-88-14, NA TO EH-60 (B ARMSTRONG,CIV)

09-Jan-1989 7

FT. RUCKER, AL

thomas.m.lilly

TFSI MOJAVE AIRPORTUH-60-89-01 ONETIME INSPECTION OF T700-GE-700 ENGINE GAS GENERATOR STATORSHROUD CW 393.9 HRS EH-60 MAINTSUPERVISOR (FSI36 O.C.)

17-Feb-1989 1

MOJAVE CA 93501

thomas.m.lilly

TFSIUH-60-89-02, CORRECTION TO 89-01, ONETIME INSPECTION OF T700-GE-700 ENGINEGAS GENERATOR STATOR SHROUD C/W 393.9HRS EH-60 MAINT SUPERVISOR (FSI36 O.C.)

17-Feb-1989 2

MAJAVE AIRPORT,MAJAVE, CA

thomas.m.lilly

NO ORGANIZATIONSOF MSG # UH-60-89-04 CHANGE TO 89-03 C/WBY CA AVORAD FAT 95727 (CA AV ORADW71MAA QC-6)

03-Mar-1989 1

FAT 95727

thomas.m.lilly

SIKORSKY ACFTUH-60-85-05- NA THIS ACFT POU'S INSTALLED.RESTRICTION ENTERED IN OPERATORSMANUEL (JB2761 'PCW')

30-Mar-1989 1

SIKORSKY ACFT

thomas.m.lilly

SIKORSKY ACFTUH-60-86-21, ONE TIME INSP OF CREW SEATSFOR LONGITUDINAL MOVEMENT OF LOCKPINS ADJ. C/W BY SIKORSKY ACFT 13 FEB 87REF AUTOMATED 2408-15 (JB2761 'PCW')

30-Mar-1989 2

SIKORSKY ACFT

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 8 of 64

TFSISOF MSG # UH-60-89-03 ONE TIMEINSPECTION OF ALL MAIN ROTOR SPINDLES.ALL PART NUMBERS C/W @ 393.9 HRS EH-60MAINT SUPERVISOR (FSI36 O.C.)

03-Apr-1989 1

MAJAVE AIRPORT,MAJAVE, CA

thomas.m.lilly

CA AVCRADSOF MSG # UH-60A-89-06 ONETIME INSP OFR/H / L/H RELAYS FOR SUSPECT GROUNDINGMODULES C/W BY CAAVCRAD FAT 93727 (CAAVORAD W71MAA QC6)

28-Aug-1989 1

FAT 93727

thomas.m.lilly

CA AVCRADSOF MSG # UH-60A-89-07 CHANGE TO 8906C/W (THOMAS R. CORED (TI))

28-Aug-1989 2

FAT 93727

thomas.m.lilly

CA AVCRADSOF MSG# UH-60A-89-09 CORRECTION OFRETIREMENT LIFE SCHEDULE C/W BY CAAVCRAD FAT 93727 (THOMAS R. CORED (TI))

28-Aug-1989 3

FAT 93727

thomas.m.lilly

CA AVCRADSOF MSG #UH-60A-89-12 SERIAL NUMBERCHECK ON AXIAL FAN SHAFT C/W 427.8 HRSBY CA AVCRAD FAT (CA AVORAD W71MAA QC-6)

28-Nov-1989 1

FAT 93727

thomas.m.lilly

CA AVCRADSOF MSG #UH-60A-89-05 ONE TIME INSP OFWSPS FOR CONTACT WITH WIRING UNDERPYLON COVER C/W 427.8 HRS BY CA AVCRADFAT 93727 (CA AVORAD W71MAA QC-6)

17-Jan-1990 1

FAT 93727

thomas.m.lilly

CA AVCRADSOF MSG # UH-60A-89-08 ONETIME INSP OFFUEL BOOST HOSE ATTACHMENT C/W 427.8HRS BY CA AVCRAD FAT (CA AVORADW71MAA QC-6)

19-Jan-1990 1

FAT 93727

thomas.m.lilly

CA AVCRADSOF MSG # UH-60A-89-10 CORRECTION TOINSP CRITERIA ON SOF 89-01-02 C/W 427.8HRS BY CA AVCRAD FAT (CA AVORADW71MAA QC-6)

19-Jan-1990 2

FAT 93727

thomas.m.lilly

CA AVCRADSOF MSG #UH-60A-89-11 CORRECTION TO 89-10 C/W (CA AVORAD W71MAA QC-6)

19-Jan-1990 3

FAT 93727

thomas.m.lilly

SVC CO 4-1 AVNSOF MSG UH-60-90-01 ONE TIME INSPECTIONOF MAIN TOROT BLADE EXPANDABLE PINSCONPLETED 12 APR 90, 476.4 ACFT HRS,(JB2761 'PCW')

13-Apr-1990 1

FT RILEY, KS 66442

thomas.m.lilly

NO ORGANIZATIONDF ANTENNA HOUSING INSULATORSREPLACED WITH P/N 1951-1-4116-4 TOCOMPLY WITH AWR DATED 21 SEP 89 (JB2761'PCW')

18-May-1990 1

(NO LOCATION)

thomas.m.lilly

TEROTEKPMS-2 INSP COMPLETED AT 501.0 ACFT HRS(JB2761 'PCW')

22-Jun-1990 1

FT. RILEY, KS,66442

thomas.m.lilly

OCMSECOCM/ACE PERFORMED AT 515 ACFT HRS ATFT RILEY KS BY ACE TEAM MEMBER S.PARKER, AVSCOM (S.PARKER)

27-Jul-1990 1

ST LOUIS, MO

thomas.m.lilly

D LO 4-1 AVN REGTSOF MSG UH-60-90-02 ONE TIME INSP OF TAILROTOR PITCH BEAM RETENTION HARDWARECOMPLETED (JB2761 'PCW')

20-Aug-1990 1

FT RILEY, KS 66442

thomas.m.lilly

DYNCORP OLR1-1520-237-20-121 INSTALLATION OF GPS(TRIMBLE TRIMPACK) (L MATHER)

23-Apr-1991 1

KKME, SA APO 09734

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 9 of 64

C. CO 4-1 AVN REGTSOF MSG UH-60-91-AMSAV-08 TB 1520-237-20-125 ONE TIME INSP OF FIRE EXTINGUISHERSYSTEM COMPLETED 23 JUL 91 AT 725.6 ACFTHR (JB2761 'PCW')

23-Jul-1991 1

FT. RILEY KS 66442

thomas.m.lilly

OCM SECOCM/ACE PERFORMED AT 726 ACFT HRS ATFT. RILEY KS BY ACE TEAM MEMBER W RIGHTAVSCOM OCM SEC (W RIGHT)

10-Sep-1991 1

ST. LOUIS, MO

thomas.m.lilly

C. CO 4-1 AVNUH-60-91-ASAM-01 ONE TIME REPLACEMENTOF THE T/R PITCH BEAM RETAINING NUTWASHER COMPLIED WITH 2 MAR 91 AT 688.2ACFT HRS (JB2761 'PCW')

11-Oct-1991 1

FT. RILEY, KS 66442

thomas.m.lilly

C.CO 4-1 AVNUH-60-91-ASAM-02 MAIN ROTOR TIP CAPRECURRING EROSION PROTECTIONINSPECTION (JB2761 'PCW')

11-Oct-1991 2

FT. RILEY, KS 66442

thomas.m.lilly

C. CO4-1 AVNUH-60-91-ASAM-03 TBO HOURS EXTENDEDFROM 2000 TO 3000 HOURS FOR THE OILCOOLER AND T/R PITCH CHANGE SHAFT FOROPERATION DESERT STORM (JB2761 'PCW')

11-Oct-1991 3

FT. RILEY, KS 66442

thomas.m.lilly

C.CO 4-1 AVNUH-60-91-ASAM-04 GUIDANCE FOREXCEEDING RETIREMENT LIFE OF CERTAINCOMPONENTS DURING DESERT STORM(S.KENNETH)

11-Oct-1991 4

FT RILEY, KS 66442

thomas.m.lilly

C CO 4-1 AVNUH-60-61-ASAM-05 ONE TIME SERIAL NUMBERCHECK OF M/R SPINDLES COMPLIED WITH 26AUG 91 AT 726.0 ACFT HRS (S.KENNETH)

11-Oct-1991 5

FT RILEY, KS 66442

thomas.m.lilly

C CO 4-1 AVNUH-60-91-ASAM-06 CARGO HOOK WIREBUNDLE ROUTING DOES NOT APPLY TO ACFT(S.KENNETH)

11-Oct-1991 6

FT RILEY, KS 66442

thomas.m.lilly

C CO 3-1 AVNUH-60-91-ASAM-07 MAIN TRANSMISSION PARTNUMBER UPDATE FOR NEW TRANSMISSIONS.(S.KENNETH)

11-Oct-1991 7

FT RILEY, KS

thomas.m.lilly

C CO 4-1 AVNUH-60-91-ASAM-09 CHANGES TO INSPECTIONPROCEDURES OF M/R ELASTOMERICBEARING (S.KENNETH)

11-Oct-1991 8

FT RILEY, KS

thomas.m.lilly

C CO 4-1 AVNUH-60-91-ASAM-10 ONE TIME INSP AND/ORREPLACEMENT OF MAIN GEAR BRAKEASSEMBLY COMPLIED WITH 23 JUL 91 AT725.6 ACFT HRS (S.KENNETH)

11-Oct-1991 9

FT RILEY, KS

thomas.m.lilly

C CO 4-1 AVNUH-60-91-ASAM-11 REQUIREMENT TOOPERATE AIRCRAFT WITH FUEL BOOSTPUMPS ON WHILE BURING JP4 FUEL.(S.KENNETH)

11-Oct-1991 10

FT RILEY, KS 66442

thomas.m.lilly

C CO 4-1 AVNUH-60-92-ASAM-01 INSPECTION FOR THREEUNSERVICEABLE SPINDLES I/A/W TB 1-1520-237-20-129 C/W AT 810.4 ACFT HRS(S.KENNETH)

08-Jan-1992 1

FT RILEY, KS 66442

thomas.m.lilly

C CO 4/1 AVNUH-60-92-ASAM-02 ALL EVEN SERIALNUMBERED UH-60A/L BLACKHAWKAIRCRAFT, ONE TIME INSP FOR ENGINEOUTPUT SHAFT BOLT TORQUE ANDVIBRATION LEVEL COMPLIED WITH AT 871.3ACFT HOURS ON 14 MAY 92 (T.GRATH)

14-May-1992 1

FT RILEY, KS 66442

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 10 of 64

C CO 4-1 AVNUH-60-92-ASAM-03 T700-GE-700 GASGENERATOR ROTOR TURBINE BLADEFAILURES/ENGINE CLEANING, ENGINE LIFELIMITED OCMPONENTS TRACKING, ANDSINGLE ENGINE FLIGHT PLANNINGPROCEDURES. (RV)

10-Jun-1992 1

FT RILEY, KS 66442

thomas.m.lilly

C CO 4-1 AVNUH-60-92-ASAM-04 ALL EH-60 AIRCRAFT, USEOF RECOVERY/RECYCLE EQUIPMENT ON ALLAIR CONDITIONING OR REFRIGERANTSYSTEMS HAT USE CFC/FREON. (RV)

30-Jul-1992 1

FT RILEY, KS 66442

thomas.m.lilly

DYNCORP (PROJECTOLR)

MSG#UH-60-92-ASAM-06(TB 1-1520-237-20-134)ALL H-60 ARMY ACFT ONE TIME INSP FORPROPER HARDWARE ON THE PEDALADJUSTER ASSY COMPLIED WITH 28 SEP 92AT 942.4 ACFT HRS (D.COSTER)

28-Sep-1992 1

FT HOOD, TX 76540

thomas.m.lilly

DYNCORP, PROJECTOLR

MSG UH-60-92-ASAM-05 (TB 1-1520-237-20-130)INSP & REPLACEMENT OF MAIN ROTORBLADE EXPANDABLE PINS PREVIOUSLYCOMPLIED WITH BY C CO 4-1 AVN FT RILEY,KS 66442 (GEORGE LEMIRE)

13-Oct-1992 1

FT HOOD, TX 76540

thomas.m.lilly

DYNCORP (PROJECTOLR)

UH-60-93-ASAM-01(TB 1-1520-237-135) ONETIME OPERATIONAL CHECK OF THERANSMISSION AND GEARBOX CHIPDETECTOR SYSTEMS NOT REQUIRED I/A/WATCOM MEMORANDUM DTD 30 OCT 92(D.COSTER)

02-Nov-1992 1

FT HOOD, TX 76540

thomas.m.lilly

TSARCOM OCM SECOCM/ACT PERFORMED AT 942 A/C HRS, ATKILLEEN MUNI ARPT, TX BY ACE TEAMMEMBER P (J.BAKER)

13-Nov-1992 1

ST LOUIS, MO

thomas.m.lilly

DYNCORP PROJ OLRMSG#UH-60-93-ASAM-03(TB 1-1520-237-20-130)REVISION TO UH-60-92-ASAM-05 INSP &REPLACEMENT OF M/R BLADE EXPANDABLEPINS COMPLIED WITH AT 942.4 ACFT HRS(GEORGE LEMIRE)

18-Nov-1992 1

FT HOOD, TX 76543

thomas.m.lilly

DYNCORP, PROJECTOLR

MSG#UH-60-93-ASAM-04(TB 1-1520-237-20-134)REVISION TO UH-60-92-ASAM-06 INSP &REPLACEMENT OF IMPROPER HARDWARE ONTHE PEDAL ADJUSTER ASSY. COMPLIED WITH3 DEC 92 AT 942.4 ACFT HRS - NOTAPPLICABLE (GEORGE LEMIRE)

03-Dec-1992 1

FT HOOD, TX 76544

thomas.m.lilly

DYNCORP, PROJECTOLR

MSG#UH-60-93-ASAM-06(TB 1-1520-237-20-136)ONE TIME INSPECTION FOR SUSPECT TAILROTOR PITCH BEAM COMPLETED 21 DEC 92AT 942.4 ACFT HRS (GEORGE LEMIRE)

21-Dec-1992 1

FT HOOD, TX 76544

thomas.m.lilly

DYNCORP PROJECTOLR

MSG#UH-60-93-ASAM-08(TB 1-1520-237-20-138)BIAS TAIL ROTOR RIGGING THREE DEGREESCOMPLIED WITH 14 JAN 93 AT 842.4 ACFTHRS. (GEORGE LEMIRE)

14-Jan-1993 1

FT HOOD, TX 76544

thomas.m.lilly

F CO 1ST AVNUH-60-95-ASAM-95 CHANGE TO RETIREMENTLIFE FOR SERVICE BEAM RAILS PARTNUMBER 70209-22103-050152-034-056 (D.S.)

26-Jan-1993 1

FT. RILEY, KS. 66442

thomas.m.lilly

DYNCORPPROJECT/OLR

PMS-2 (PE#2) INSPECTION COMPLETED AT942.4 ACFT HRS, 27JAN93. [NEXT PMS-2 #3WILL BE AT 1442.4 ACFT HRS] (G.LEMIRE CIV.INSPECTOR)

27-Jan-1993 1

FT. HOOD, TX76544

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 11 of 64

DYNCORP, PROJECTOLR

PMS-2(PE#2) INSPECTON COMPLETED AT942.4 ACFT HRS 27 JAN 93 (G.LEMIRE)

27-Jan-1993 2

FT HOOD, TX 76544

thomas.m.lilly

DYNCORP, PROJECTOLR

TB 1-1520-237-30-2 DESERT STORMREDEPLOYMENT SPECIAL INSPECTION ANDCLEANING REQUIREMENT UH-60A/L AND EH-60 ACFT COMPLETED AT 942.4 ACFT HRS 27JAN 93. (G.LEMIRE)

27-Jan-1993 3

FT HOOD, TX 76544

thomas.m.lilly

DYNCORP, PROJECTOLR

TB 1-1500-200-20-30 DESERT STORMREDEPLOYMENT CLEANING REQUIREMENTCOMPLETED AT 942.4 ACFT HRS 27 JAN 93(G.LEMIRE)

27-Jan-1993 4

FT HOOD, TX 76544

thomas.m.lilly

C CO 4-1 ANV REGTUH-60-93-ASAM-09 ONE TIME INSP FOR MWOCOMPLIANCE COMPLETED @ 957.6 ACFT HRS(CD)

14-Apr-1993 1

FT RILEY, KS 66442

thomas.m.lilly

C CO 4-1 AVN REGTUH-60-93-ASAM-11 ONE TIME INSP OF CREWESTRAINT ASSY COMPLETED @ 957.6 ACFTHRS (CD)

14-Apr-1993 2

FT RILEY, KS 66442

thomas.m.lilly

C CO 4-1 AVN REGTUH-60-93-ASAM-12 READING OF UH-60-93-ASAM-12 ENTERED ON 2408-13-1, COMPLIEDWITH AT 966.9 ACFT HRS (DV)

28-Apr-1993 1

FT RILEY, KS 66442

thomas.m.lilly

C CO 4-1 AVN REGTUH-60-93-ASAM-16 ONE TIME INSP OFHYDRAULIC PUMP BLEED VALVE KNOBS FORSECURITY COMPLIED WITH @ 1019.4 ACFTHRS (CD)

05-Aug-1993 1

FT RILEY, KS 66442

thomas.m.lilly

C CO 4-1 AVN REGTUH-60-93-ASAM-17 POSSIBLE ORQUEFLUCTUATIONS & TQ REDUCTION DUE TOHIGH INTENSITY RADIO TRANSMISSIONSAREA(HIRTA) (NOTE: N/A TO THIS ACFT) (DD)

13-Sep-1993 1

FT RILEY, KS 66442

thomas.m.lilly

C CO 4-1 AVN REGTUH-60-94-ASAM-01 INSP OF MASTERWARNING PANEL FOR P/N 70550-01108-107(DD)

18-Nov-1993 1

FT RILEY, KS 66442

thomas.m.lilly

C CO 4-1 AVNUH-60A-94-ASAM-01 INSP OF MASTERWARNING PANEL P/N 70550-01108-107COMPLIED WITH 1099.9 ACFT HRS (JD)

02-Dec-1993 1

FT RILEY, KS 66442

thomas.m.lilly

NO ORGANIZATIONACE/AACE PERFORMED AT 1100 A/C HRS ATFT RILEY, KS BY ACE TEAM MEMBER LAVSCOM ACE/OCM (DAVE CASLEY)

06-Dec-1993 1

FT RILEY, KS

thomas.m.lilly

C CO 4-1 AVNUH-60A-94-ASAM-02 INSP OF SEAT BELTLANYARD PULL TYPE BUCLKE/CROTCH ASSYFOR P/N D-4495-08 SN#2413 SN#2346COMPLIED WITH 14 JAN 94 (DD)

04-Jan-1994 1

FT RILEY, KS 66442

thomas.m.lilly

C CO 4-1 AVNUH-60-94-ASAM-04 INSPECTION OF T/R PITCHBEAM FOR SUSPECTED SERIAL NOCOMPLIED WITH 1104.5 HRS (G JOHNSON)

03-Feb-1994 1

FT RILEY, KS 66442

thomas.m.lilly

CCO 4-1 AVNTB1-1520-237-20-151 ONE TIMEREFURBISHMENT OF M/R SPINDLES ANDREPLACEMENT OF CERTAIN M/R THRUSTBEARINGS. (JB2761 R/SPEC PCW BY GJ)

14-Feb-1994 1

FT. RILEY,KS 66442

thomas.m.lilly

CCO 4-1 AVN FT.TB1-1520-237-20-150 (UH-60-94-ASAM-06) INSPOF PILOTS SEAT RESTRAIN SYS. C/W @ 1104ACFT HRS. BY SSG. MARTINEZ. ,P. (JB2761R/SPEC PCW BY GJ)

16-Feb-1994 1

FT. RILEY, KS 66442

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 12 of 64

CCO 4-1 AVNTB1-1520-237-20-152 (UH-60-94-ASAM-05) ONETIME REMOVAL OF T/R GEARBOXES WITHOUTPUT SHAFT P/N 70358-06620-101 FORREWORK. (JB2761 R/SPEC PCW BY SV)

16-Feb-1994 2

FT.RILEY, KS 66442

thomas.m.lilly

CCO 4-1` AVNTB1-1520-237-20-154 (UH-60-94-ASAM-07 MAOTCHANGES C/W @ 1106 ACFT HRS. (JB2761R/SPEC PCW BY FJ)

24-Mar-1994 1

FT. RILEY, KS66442

thomas.m.lilly

CCO4-1 AVN REGT FT.UH-60-94-ASAM-08 REVISION TO UH-60-94-ASAM-07 C/W @ 1106 ACFT HRS. ROBERT J.HALIGOWSKI (R. HALIGOWSKI)

24-Mar-1994 2

FT. RILEY,KS 66442

thomas.m.lilly

CCO 4-1 AVN REGT.UH-60-94-ASAM-09 REMOVAL OF CERTAINPRIMARY SERVO ASSYT C/W AT 1118.3 ACFTHRS. (R.J. HALLIGOWSKI)

08-Apr-1994 1

FT. RILEY, KS 66442

thomas.m.lilly

CCO 4-1 AVN REGTUH-60-94-ASAM-10 A REVISION TO UH-60-94-ASAM-03 ONE TIME REFURBISHMENT OFMAIN ROTOR SPINDLE AND REPLACEMENTOF CERTAIN M/R THRUST BEARINGS C/W AT1125.8 ACFT HRS. (R. WEEKS)

14-Apr-1994 1

FT. RILEY, KS

thomas.m.lilly

ATCOM OCM/ACE TEAM3

OCM/ACE & AACE PERFORMED AT 1149 ACFTHRS BY TEAM MEMBER P ATCOM OCM/ACEST. LOUIS (R.A. & R. HENDRIX)

03-Aug-1994 1

FT. RILEY, KS.

thomas.m.lilly

F CO 1ST AVNUH-60-95-ASAM-01 HOISTING AND ARIALRECOVERY OF UH-60/EH60 ESSS FIXEDPROVISION HELICOPETERS N/A THIS ACFTC/W 1148.7 ACFT HRS (H. GARDNER)

14-Oct-1994 1

FT. RILEY, KS

thomas.m.lilly

FCO 1ST AVNUH 60-95-ASAM-02 REQUIREMENT TOOPERATE THE FUEL TANK SUBMERGEDBOOST PUMPS ON AT ALL TIMES WITH ALLFUELS DURING GROUND FLT OPERATIONS,ACFT C/W 1148 ACFT HRS (SJ & D.SYDOW)

14-Oct-1994 2

FT. RILEY, KS.

thomas.m.lilly

FC 1ST AVNUH-60-95-ASAM-003 SHIMMING OF TAILROTOR PIVOT BEARINGS WHICH CONTAINCOMPOSITE PIVOT BEARING RETAINERS (T1-1520-237-20-158) (M.G.)

07-Nov-1994 1

FT. RILEY,KS 6642

thomas.m.lilly

FCO 1ST AVNUH-60-05-ASAM-04 REDUCTION OF TORQUEOF SELT RETAINING PIVOT BOLTS (TB1-1520-237-20-160) (TB1-1520-250-20-2) (M.G.)

10-Nov-1994 1


thomas.m.lilly

FCO 1ST AVNSOF UH-60-95-01 ONE TIME INSP OF RECORDSOF ALL TAIL ROTOR GEARBOXS TO IDENTIFYGEARBOX OUTPUT SHAFTS PN 70358-06620-101 (M.G.)

15-Dec-1994 1

FT. RILEY, KS 66442

thomas.m.lilly

F CO 1ST AVNSOF UH-60-95-02 CHANGE TO RETIREMENTLIFE FOR CERTAIN M.E BVLADE CUFFS, C/WWITH 1148.7 ACFT HRS. TB1-1520-237-20-161(M.G.)

15-Feb-1995 1


thomas.m.lilly

F CO 1ST AVNUH-60-ASAM-06 ONE TIME INSP FORCRACKED MAINTRANS BEARINGS UPPERDECK SKIN FRAME CRACKS ANDIMPLENTATION OF 100 HR RECURRING INSPTB1-1520-237-20-163 (M.G.)

20-Jun-1995 1

FT. RILEY, KS 66442

thomas.m.lilly

F CO 1ST AVNUH-60-95-ASAM-07 EXPLICIT SHIMMINGPROCEDURES FOR ALLENTVATION ROLLERSINSP TB1-1520-237-20-163 (M.G.)

20-Jun-1995 2


thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 13 of 64

UNC AVIATIONUH-60-96-01 (TB1-1520-237-20-160)REPLACEMENT OF IMPOROVED FLIGHTCONTROL BOLTS. (J.H.)

23-Oct-1995 1

LAKEHURST N.J

thomas.m.lilly

UNC AVIATIONSOF UH-60-96-01 (TB1-1520-237-20-172)CHANGE IN RETIREMENT LIFE AND REMOVALOF CERTAIN S/N FWD BELLCRANK SUPPORT.(J.H.)

08-Nov-1995 1

LAKEHURST N.J.

thomas.m.lilly

UNC AVIATIONSOF UH-60-96-03 (TB1-1520-237-209174)INSPECTON OF M/R BALDE CUFF S/N (J.H)

09-Dec-1995 1

LAKEHURST N.J.

thomas.m.lilly

UNC AVIATION NAVCSOF UH-60-96-02 (TB1-1520-237-20-173) ONETIME UNSP T/R INBD RETENTION PLATE (JFLESCHE CIV TI)

19-Mar-1996 1

LAKEHURST, N.J.

thomas.m.lilly

UNC AVIATIONSOF UH60-96-04 (TB1-1520-237-20-175) INSP OFAFT BELLCRANK . (J FLESCHE TI)

26-Mar-1996 1

LAKEHURST, N.J.

thomas.m.lilly

UNC AVIATIONUH-60-96-ASAM-05 (TB101520-237-20-177INCREASE IN FATIGUE LIFE OF FWD SUPPORTASSY. (J FLESCHE TI)

10-Jul-1996 1

LAKEHURST, N.J.

thomas.m.lilly

UNC AVIATIONUH-60-96-ASAM-08 (TB1-1520-237-20-178)INCREASE IN FATIGUE LIFE OF INBO T/RRETENTION PLATE (J FLESCHE TI)

29-Aug-1996 1

LAKEHURST, N.J.

thomas.m.lilly

UNC AVIATIONUH-60-96-ASAM-01 (TB1-1520-237-20-182)SPINDLE AND ELASTOMERIC BRG. INSP @PHASE (J FLESCHE TI)

12-Sep-1996 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-97-ASAM-01 (TB1-1520-237-20-181)VISUAL INSP JOF M/R HUB (J FLESCHE)

24-Oct-1996 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-97-ASAM-02 (TB1-1520-237-20-184) T/RFLEX COUPLING INSP (J FLESCHE)

30-Oct-1996 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-97-ASAM-03 (TB1-2840-248-19)REPLACEMENT OF UNPAMPERED GAS GENROTOR (J FLESCHE)

11-Nov-1996 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-97-01 (TB1-1520-237-20-185) S/N CHECKOF SWASHPLATE (J FLESCHE)

03-Dec-1996 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-97-ASAM-07 (TB1-1520-237-20-188) REPLOF SPECIFIC S/N T/R SERVOS (J FLESCHE)

15-Jan-1997 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-97-ASAM-06 (TB1-1520-237-20-189)LATERAL BELLCRANK ASSY S/N CHECK (JFLESCHE)

22-Jan-1997 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-97-ASAM-05 (TB1-1520-237-23-2)REWORK VISCOUS DAMPERS (J FLESCHE)

22-Jan-1997 2

LAKEHURST,N.J.

thomas.m.lilly

W4GV20UH-60-97-ASAM-08(TB1-1520-237-20-181) INSPCONNECTING LINK SN (J FLESCHE)

22-Jan-1997 3

LAKEHURST,N.J.

thomas.m.lilly

W4GV20UH-60-97-ASAM-09 (TB1-1520-237-20-190 M/RSHAFT EXTENSION S/N CHECK (J FLESCHE)

24-Jan-1997 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-97-ASAM-10 (TB1-1520-237-20-191)CHANGE IN RETIREMENT LIFE MAIR BRIDGE(J FLESCHE)

14-Feb-1997 1

LAKEHURST, N.J.

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 14 of 64

W4GV20UH-60-97-ASAM-11 (TB1-1520-237-20-192)INCRFEASE IN FATIGUE LIFE FOR M/R BLADECUFF 70150-09109-041 AND 043. (G HILL)

03-Mar-1997 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-97-ASAM-13 (TB1-1520-237-20-194) INSPOF M/R SPINDLE SPHERICAL BENRING FOREXISTENCE OF INNER SLEEVE BEARING (G.HILL)

16-Jun-1997 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20JACE INSP PERFORMED AT 1210 ACFT AHRSAT NAES LAKEHURST, N.J. BY JACE JATEAMMEMBER 'M' AT COM OLR/MWO BRANCH ST.LOUIS, L, MO. (C MOORE 9437)

24-Jul-1997 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-97-ASAM-14 (TB1-1520-237-20-195)ONETIME INSP 2 REPLACEMENT OFBELLCRAND SUPPORT MFG. BY AMERICANGENERAL CAGE 1W160 (G. HILL)

22-Aug-1997 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-97-ASAM-15 (TB1-1520-237-20-196) ONETIME INSP AND REPLACEMENT OF LOWERPITCH LINK BEARING ROD END P/N 70101-08202-101 BY ISLAND ENG (G.HILL)

22-Aug-1997 2

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-97-ASAM-16 (TAB1-1520-237-198) ONETIME UNSP FOR SWASHPLATE LINKAGE,CLEVISCONNECTOR P/N 70400-08151-050 BYAIRBORNE APPAREL CAGE 2A622 (G. HILL)

22-Aug-1997 3

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-92-ASAM-18 (TB1-1520-237-201)REMOVAL OF CERTAIN S/N SWASHPLATES(G.HILL)

15-Sep-1997 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-97-ASAM-19 (TB1-1520-237-20-204) ONETIME INSP JOF ANVIS/HUD POWERS SUPPLY(G. HILL)

01-Oct-1997 1

LAKEHURST,N.J.

thomas.m.lilly

W4GV20UH-60-98-ASAM-02 (TB1-1520-237-20-197)REPLACEMENT OF PUSH RODS P/N 70400-08155-0500R051 MANF. BY VERSATILEMACHINE CODE 6S552 (G. HILL)

14-Oct-1997 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-98-ASAM-17 (TB1-1520-237-20-197) INSPOF INTERNAL RESCOE HOIST BRACKET ASSYALUMINUM STRUCTURAL PLATE ASSY(G.HILL)

28-Oct-1997 1

LAKEHURST,N.J.

thomas.m.lilly

W4GV20UH-60-98-ASAM-03 (TB1-1520-237-20-203) UH60 ACFT WITH SWASHPLATE LINK ASSY P/N70400-08110-054 MANF BY TRK CAAGE 65780FOR REPLACEMENT (G.HILL)

12-Nov-1997 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH60-98-ASAM-05 (TB1-1520-237-20-203) INSPALL ACFT. WITH SWASHPLATE LINK ASSY PN70400-08110-054-061 MANF. BY TEK CAGECODE 65780 FOR REPLACEMENT (G. HILL)

06-Mar-1998 1

LAKEHURST, N.J.

thomas.m.lilly

LM LMJACE/CPCL COMPL AT 1224 A/C HRS BY JACEMEMBER LL AM COM MWO BRANCH (E.CHECKS)

12-Mar-1998 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-98-ASAM-04 (TB1-1520-237-20-205) INSPFOR LOOSE HUCK BOLTS ON OVER HAVPRMARY, YAW, COLLCTIVE AND T/R SERVOFOR REPLACEMENT (G. HILL)

19-Mar-1998 1

LAKEHURST, N.J.

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 15 of 64

W4GV20UH-60-98-ASAM-07 (TB1-1520-237-20-206) ONETIME INSP OF LEFT TIE ROD ASSY PN 70400-18115-043 MANF. BY ARGEN CORD CAGE8R021 (G.HILL)

21-Sep-1998 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-99-ASAM-01 (TB1-1520-237-20-208)RESTORATION OF FULL SERVICE LIFE OFSWASHPLATE LINK P/N 70400-08110-054-061MANF BY TEK 65780 (G.HILL)

05-Nov-1998 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-99-ASAM-02 (TB1-1520-237-20-207) INSPOF ALL U60 ACFT WEITH PROVISION FOREXTERNAL HOISTAND ALL HOIST MANF. BYBREEZE EASTERN (G.HILL)

09-Nov-1998 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-99-ASAM-03 (TB1-2840-248-20-22-209)ONE TIME INSP OF 700GE700 ENGINES FORCOMPONENT TIME IN SERVICE (G.HILL)

04-Dec-1998 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-ASAM-04 INFORMATIONAL ON ENG.O.DV RELATER FLAME OUTS ON T700GE-701CENGINES (G.HILL)

22-Dec-1998 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-ASAM-05 (TB1-1520-237-20-209)ONETIME INSP JOF M/R SPINDLE BEARING FOREXISTENCE OF INNER SLEEVE BEARING (G.HILL)

22-Dec-1998 2

LAKEHURST, N.J.;

thomas.m.lilly

W4GV20UH-60-ASAM-06 (TB1-1520-237-20-210) ONETIME INSP AND REVISED RETIREMENT LIFEOF M/R PITCH HORN P/N 70102-08111-047 BYSERIAL # (G. HILL)

22-Dec-1998 3

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-99-ASAM-08 (TB-1-1520-237-20-211)REVISED RETIRE MENTLIFE OF BVELLCRANKSUPPORT ASSY P/N 70400-08162-042/043/045CAGE 8L513 (G.HILL)

18-Jun-1999 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-99-ASAM-07 (TB-1-1520-237-212) INSPOF M/R HUB ASSY FOR CRACKS ATSPECIFIED AREAS AND RECURRING INSP (G.HILL)

09-Jul-1999 1

LAKE HURST, N.J.

thomas.m.lilly

W4GV20UH-60-99-ASAM-09 (TB 1-1520-237-20-214) ONETIME INSP O FAIL M/R EXPANDABLE BLADEPINS FOR SHOTS IN OUTER SEGMENTS ANDREPLACEMENT OF 101 PINS (G.HILL)

02-Aug-1999 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-99-ASAM-10 (TB1-1520-237-20-213)INSPAND PREVENTIVE MAINTENANCE ON II 2CROSSFEED BREAK ASAY VALVE P/N 70307-03006-103 (G. HILL)

04-Aug-1999 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-99-ASAM-11 (TB1-2840-248-20-23) ONETIME INSP OF T 700 GE 700/701/701C ENGINESFOR PROPER TIME CHANGE ITEMS. (G.HILL)

16-Aug-1999 1

LAKEHURST, N.J.

thomas.m.lilly

104GV20 NAESUH-60-99-ASAM-02. INTERVAL CHG FORHAMILTON STANDARD HMUP/N:4046T52G01/G04/G06/G09/G11 (JM4586)

24-Aug-1999 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-00-ASAM-01 (TB1-1520-237-20-215)REVISION TO UH-60-99-ASAM-07-ON INSPOFM/R HUB ASSY. (G. HILL)

15-Nov-1999 1

LAKEHURST, N.J.

thomas.m.lilly

AMCOM OLR/MSOBRANCH

JACE COMPLETED AT 1234 ACFT HRS BYJACE MEMBER G . (EH9090)

22-Dec-1999 1

LAKEHURST N.J.

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 16 of 64

CFA-W4GU20UH-60-00-ASAM-03 (TB1-1520-237-20-217) ONETIME INSP AND REMOVAL OF SUSPECTPRIMARY SERVO ASSY. (GH3283)

04-Jan-2000 1

NAES LAKEHURST, N.J.

thomas.m.lilly

CFA-W4GV20.UH-60-00-ASAM-02, TB1-1520-237-20-216 ONETIME INSP OF CYCLIC STICK WIRE HARNESFOR CHAFFING. (JM4586)

05-Jan-2000 1


thomas.m.lilly

W4GV20UH-60-00-ASAM-04 (TB1-1520-237-218) INSP.TAIL LANDING GEAR SHOCK STRUT ASSYFOR MISSING BEARING RETENTION PINS.(GH3283)

08-Mar-2000 1


thomas.m.lilly

LULMACE COMPLETED AT 1241 ACFT HRS BY ACEMEMBER L AMCOM OLR/MWO BRANCH.(EH9080)

20-Apr-2000 1

LAKEHURST, N.J.

thomas.m.lilly

W4GV20UH-60-00-ASAM-05 (TB1-1520-237-20-219) ONETIME INSP OF FIRE EXTINGUISHER WIRING.(GH3283)

17-May-2000 1

NAES LAKEHURST N.J.

thomas.m.lilly

AMCOM/OLR LM2 TEAM12101

INSP IAW UH-60 PM MEMORANDUM SUBJECT:INSP OF MWO 1-1520-237-50-55 MODIFIEDAIRCRAFT DATED 21SEPT98 C/W AT 1241.8ACFT HRS. (B.P 0067)

05-Jun-2000 1

LAKEHURST N.J.

thomas.m.lilly

W4GV20UH-60-00-ASAM-06 (TB1-1520-237-20-219)UPDATE CHANGE 1 TO INSP OF FIREEXTINGUSHER WIRING. (GH3283)

29-Jun-2000 1


thomas.m.lilly

W4GV20SOF UH-60-00-01 (TB1-1520-237-20-221) INITIALAND RECURRING INSP OF MAIN ROTORSPINDLE LUGS FOR CRACKS. (GH3283)

15-Jul-2000 1


thomas.m.lilly

W4GV20SOF UH-60-00-02 (TB1-1520-237-20-222)REMOVAL OF INPUT MODULE GEARBOXASSY. WITH POTENTIALLY CRACKED BEVELGEARS. (GH3283)

04-Aug-2000 1

NAES LAKEHURST N.J.

thomas.m.lilly

USAAVNCACFT RECEIVED FROM CECOM FLIGHTFACILITY, LAKEHURST, NJ (W4GV20) I/A/WTWX 141433Z JUL 00. ACFT HRS 1244.6 ATDEPARTURE, 1252.0 AT ARRIVAL AT FT.RUCKER. (DK1063)

10-Aug-2000 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-96-ASAM-03 TB1-1520-237-20-171 INSP.OF M/R SHAFT NUT BOLT C/W AT 1252.0 ACFTHRS. (RS4443 R/CLERK)

16-Aug-2000 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCONE TIME & RECURRING INSP OF BOOSTSERVO & PILOT ASSIST MODULE MANIFOLDBASE PLATE FOR LOOSE MOUNT BOLTS IAWDYN PROCESS CONTROL # UH60-00-01 C/W AT1252.0 ACFT HRS. (RS4443 R/CLERK)

16-Aug-2000 2

FT. RUCKER, AL

thomas.m.lilly

USAAVNCAIRCRAFT OPERATING UNDER AWR FORSPECIFIED EH-60A HELICOPTERS TO BEOPERATED WITH ALL MISSION EQUIPMENTREMOVED AND SINGLE CHANNEL GROUNDAND AIRBORNE RADIO SYSTEM (SINCGARS),AVIATOR NIGHT VISION IMAGING SYSTEMHEAD UP DISPLAY (ANVIS-7/HUD), AN/ASN-128B DOPPLER/GPS NAVIGATION SYSTEMAND JUMP SEAT INSTALLED (AWR 890).DATED 08MAY00. ACFT WILL OPERATE AS AUH-60A PER PARA 4.F OF THE AWR. (RS4443R/CLERK)

17-Aug-2000 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 17 of 64

USAAVNCAIRCRAFT OPERATING UNDER AWR FOREMERGENCY LOCATOR TRANSMITTER (ELT)DATED 05FEB99. (RS4443 R/CLERK)

17-Aug-2000 2

FT. RUCKER, AL

thomas.m.lilly

USAAVNCTHE FOLLOWING LIST OF MODIFICATIONSCOMPLETED AT ACCEPTANCE AT 1252.0 ACFTHRS I/A/W LOCAL DOCUMENTS FOR SCHOOLFLEET TRAINING: INSTL OF FUEL FLAG, INSTLOF ELT MOUNT, INSTL OF PHENOLIC BLOCKAT FWD END OF M/R PYLON TRACK, INSTL OFAPU VENT SCREEN, INSTL OF BUZZNUMBERS, INSTL OF HIGH VISIBILITY PAINTSCHEME. (DK1063)

18-Aug-2000 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCTB1-1520-237-20-224 (UH-60-00-ASAM-07) ONETIME INSPECTION OF WIRE HARNESSESCONNECTING THE #1 & #2 JUNCTION BOXESC/W AT 1260.4 ACFT HRS. [N/A FOR THIS ACFT](RS4443 R/CLERK)

02-Sep-2000 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCTB1-1520-237-20-225 (SOF UH-60-01-01) INITIALAND RECURRING INSP OF THE MLG DRAGBEAM ASSY AND DECREASE TORQUE ON THEJACKPAD NUT C/W AT 1378.9 ACFT HRS.(RS4443 R/CLERK)

06-Nov-2000 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCUH-60-01-02 (TB1-1520-237-20-225) REVISIONTO SOF UH-60-01-01 TB1-1520-237-20-225INITIAL AND RECURRING INSPECTION OF THEMAIN LANDING GEAR DRAG BEAM ASSY. ANDDECREASE TORQUE ON THE JACKPAD NUTC/W AT 1436.0 ACFT HRS. (RS4443 R/CLERK)

02-Jan-2001 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCSOF UH-60-01-04 TB1-1520-237-20-228 RISKMANAGEMENT OF 230 GALLON EXTERNALTANK FLIGHT OPERATIONS C/W AT 1442.4ACFT HRS. (RS4443 R/CLERK)

09-Jan-2001 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCTB1-1520-237-20-167 (IP2860 R/CLERK) 07-Feb-2001 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNC#2 CROSSFEED BREAKAWAY VALVEREPLACED I/A/W TB1-1520-237-20-213 THISDATE AT 1442.4 ACFT HRS (IP2860, R/CLERK)

21-Feb-2001 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCTB1-1520-237-20-233 (SOF UH-60-01-09) ONETIME INSP OF M/R BLD EXPANDABLEPINS.C/W @ 1442.4 ACFT HRS (IP2860R/CLERK)

11-Jun-2001 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCTB 1-1520-237-20-232 (SOF UH-60-01-08) INSPOF M/R FLIGHT CONTROL SELF-LOCKINGBOLTS. (IP2860 R/CLERK)

13-Jun-2001 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCTHE FOLLOWING LIST OF MODIFICATIONSCOMPLETED AT 1442.4 ACFT HRS I/A/WLOCAL DOCUMENTS FOR SCHOOL FLEETTRAINING: INSTALLATION OF HANDLE, M/RPYLON SLIDING COVER, INSTALLATIOIN OFSCREEN, CABIN HEAT INLET, INSTALLATIONOF SCREEN OVER BATTERY VENT. (IP2860,R/CLERK)

05-Jul-2001 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 18 of 64

USAAVNCGEN-MIM-01-005 IDENTIFICATION OFRECEIVER TRANSMITTERS (R/T) REQUIRINGECP-II SOFTWARE UPDATES C/W AT 1442.4ACFT. HRS. (MA4187 R/CLERK)

09-Jul-2001 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCTB1-1520-250-20-2 (UH-60-95-ASAM-04)REDUCTION OF TORQUE OF SELF RETAININGBOLTS AND COR LETTER DATED 22 NOV 94C/W @ 1442.4 ACFT HRS (IP2860 R/CLERK)

13-Jul-2001 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCTB1-1520-237-20-180 (UH-60-96-ASAM-09)VISUAL INSP STABILATOR ACTUATORCLEVISES FOR APPLICATION OF EPOXYPRIMER. C/W AT 1442.4 ACFT HRS (IP2860R/CLERK)

17-Jul-2001 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCTB1-1520-237-20-151 (UH-60-94-ASAM-03) ONETIME REFURBISHMENT OF M/R SPINDLE ANDREPL OF CERTAIN M/R THRUST BRNGS C/W @1442.4 ACFT HRS (IP2860, R/CLERK)

18-Jul-2001 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCPMS-2 PHASE #3 COMPLETED AT 1442.4 ACFTHRS. PMS-2 PHASE #4 DUE AT 1942,4 ACFTHRS. (TB1027 R/CLK)

18-Jul-2001 2

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCOCM/ACE PERFORMED AT 1512 ACFT HRS BYTEAM MEMBER "R". AMCOM PROJECT OLR.FT. CAMPBELL, KY. (TS0568)

18-Sep-2001 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCTB1-1520-237-20-241 (SOF UH-60-02-03), ONETIME INSP OF FLIGHT CONTROL SYSTEM,PITCH TRIM ASSY. C/W @ 1616.4 ACFT HRS(IP2860,R/CLERK)

10-Dec-2001 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCTB1-1520-237-20-242 (SOF UH-60-02-04),INSPECT APU FUEL LINES FOR PROPERGROMMET AT APU SHROUD ASSY. C/W AT1676.2 ACFT HRS (IP2860)

24-Jan-2002 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCTB 1-1520-237-20-246 (UH-60-02-ASAM-02)INITIAL AND RECURRING INSPECTION OF THECONTROL ROD JAMNUT C/W @ 1702.7 ACFTHRS (JB2761 R/CLERK)

08-Feb-2002 1

FT. RUCKER,AL

thomas.m.lilly

USAAVNCTB1-1520-237-20-244 (UH-60-2-ASAM-04)RESTRAINT SYSTEM INSPECTION. C/W AT1790.3 ACFT HRS ON 21 MAR 02 (VB3955R/CLERK)

22-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 AT1837.6 ACFT HRS. (JS4089 R/CLERK)

20-Apr-2002 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCTB1-1520-237-20-256 (UH-60-02-ASAM-08) INSPOF AN/ARC-220 WIRING FOR CHAFING. N/ATHIS ACFT. C/W AT 1919.2 ACFT HRS (IP2860,R/CLERK)

13-Jun-2002 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNC,TB1-1520-237-20-257 (UH-60-02-ASAM-09) INSPOF T/R QUADRANT HARDWAREINSTALLATION. C/W @ 1924.0 ACFT HRS(IP2860, R/CLERK)

15-Jun-2002 1

FT. RUCKER, AL

thomas.m.lilly

DYNCORPOCM/ACE PERFORMED AT 1935 ACFT HRS BYTEAM MEMBER R AMCOM PROJECT OLR FT.C. KY (T.STEGMAN, TS0568)

09-Jul-2002 1

FT. CAMPBELL, KY

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 19 of 64

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

USAAVNCPMS-2 #4 COMPLETED AT 1934.7 ACFT HRS.PMS-2 #5 DUE AT 2434.7 ACFT HRS (IP2860,R/CLERK)

27-Jul-2002 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNC,TB1-1520-237-20-245 (UH-60-02-ASAM-03)INSPECTION OF ENGINE CONTROLQUADRANT POWER CONTROL LEVER (PCL)WIRING. C/W AT 1934.7 ACFT HRS (IP2860,R/CLERK)

03-Sep-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 1964.4 ACFT HRS. (IP28960, R/CLERK)

24-Sep-2002 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCBIRD FEATHERS FOUND ON FRONT CENTERTOP OF ACCESS PANEL. TI BIRD STRIKE INSPDUE FOR FEATHERS FOUND ON FRONT OFTOP CENTER ACCESS PANEL. INSP OK. NODAMAGE FOUND AT 1993.5 ACFT HRS.(VK3955, R/CLERK)

10-Oct-2002 1

FT RUCKER, AL

thomas.m.lilly

USAAVNCUH-60-03-ASAM-01 FWD BELLCRANKSUPPORT ASSY RETIREMENT LIFE C/W AT2086.5 ACFT HRS. (IP2860, R/CLERK)

09-Dec-2002 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCUH-60-03-ASAM-02 TAIL ROTOR SERVO ASSYRETIREMENT LIFE C/W AT 2086.5 ACFT HRS.(IP2860, R/CLERK)

09-Dec-2002 2

FT. RUCKER, AL

thomas.m.lilly

USAAVNC#1 ENGINE FLAME OUT ON GROUND WHENADVANCING PCL TO FLY. TIGHTENED LOOSECANNON PLUG, W4P3 YELLOW CABLE ON #1ENG ECU & C/W T/S PROC. 3.1. TEST FLIGHTPORTION OF T/S PROC. 3.1 REQUIRED #1 ENG.(IP2860, R/CLERK)

16-Dec-2002 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNC,GEN-03-ASAM-01 (SINCGARS) ARC-201BATTERY BOX C/W AT 2119 ACFT HRS (IP2860,R/CLERK)

18-Dec-2002 1

FT. RUCKER, AL

thomas.m.lilly

DYNCORP PROJECTOLR FT. C. KY

OCM/ACE PERFORMED AT 2350 ACFT HRS BYTEAM MEMBER QQ AMCOM. (LS2032 L.SANDERS)

04-Apr-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. (JB2761 R/SPEC)

19-Jun-2003 1

FT.RUCKER,AL

thomas.m.lilly

USAAVNCPMS 2 PHASE INSP #5 COMPLETED THIS DATE@ 2420.5 ACFT HRS. NEXT PHASE #6 DUE @2920.5. (JB2761 R/SPEC)

21-Jul-2003 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 20 of 64

USAAVNCSOF UH-60-04-01, INSP OF FORWARDBELLCRANK SUPPORT INSTALLATIONHARDWARE. C/W AT 2556.1 ACFT HRS (LW2720R/SPEC)

01-Oct-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 FORWARD CONTROLSERVO INPUT ROD HAS BEEN SHORTENED1/2 TURN IN B. AFT CONTROL SERVO INPUTROD HAS BEEN LENGTHENED 1/2 TURN OUTAT 2577.1 ACFT HRS (LW2720 R/SPEC)

25-Oct-2003 1

FT. RUCKER, AL

thomas.m.lilly

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

07-Jan-2004 1

FT.RUCKER,AL

thomas.m.lilly

USAAVNCBLUE MAIN ROTOR TIP CAP SHOWSEVIDENCE OF BIRD STRIKE ON POST FLIGHTTIP CAP DAMAGED ON TOP. {ACTION TAKEN:DAMAGED ON TIP CAP LEADING EDGE} BIRDSTRIKE INSP DUE FOR BLUE M/R TIP CAPSSHOWS EVIDENCE OF A BIRD STRIKE{ACTION TAKEN: DAMAGED TAKEN:DAMAGED ON TIP CAP LEADING EDGE}(LW2720 R/SPEC)

24-Mar-2004 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCUH-60-04-ASAM-02 INSP OF T/R D/SHAFTFLANGE NUT C/W AT ACFT HRS. 2819.1(LW2720 R/SPEC)

02-Apr-2004 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCBLUE MAIN ROTOR TIP CAP SHOWSEVIDENCE OF BIRD STRIKE ON POST FLIGHTTIP CAP DAMAGED ON TOP. {ACTION TAKEN:DAMAGED ON TIP CAP LEADING EDGE} BIRDSTRIKE INSP DUE FOR BLUE M/R TIP CAPSSHOWS EVIDENCE OF A BIRD STRIKE{ACTION TAKEN: DAMAGED TAKEN:DAMAGED ON TIP CAP LEADING EDGE}(LW2720 R/SPEC)

24-Apr-2004 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCUH-60-04-ASAM-01, GLARE SHIELD LIGHTINGCIRCUIT BREAKER REPLACEMENT, C/W AT2880.5 ACFT HRS. (AFS201, S NOLIN, 2938,R/SPEC)

25-May-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAATTCAWOR REL 06JUN03(01) INSTALLATION OFTHE PROVISIONS FOR THE INSTALLATION OFTHE ANVIS/HUD AN/AVS-7 C/W THIS DATE AT2880.5 ACFT HRS. (RH0333, S NOLIN, 2938,R/SPEC)

25-May-2004 2

FT. RUCKER, AL.

thomas.m.lilly

USAATTCAWOR REL 06JUN03(02) INSTALLATION OFTHE PROVISIONS FOT HE INSTALLATION OFTHE DOPPLER/GPS AN/ASN-128B C/W THISDATE AT 2880.5 ACFT HRS. (RH0333, S NOLIN,2938, R/SPEC)

25-May-2004 3

FT. RUCKER, AL.

thomas.m.lilly

USAATTCAWOR REL 06JUN03(3) INSTALLATION OF THEPROVISIONS FOR THE INSTALLATION OF ACARGO HOOK C/W THIS DATE AT 2880.5 ACFTHRS. (RH0333, S NOLIN, 2938, R/SPEC)

25-May-2004 4

FT. RUCKER, AL.

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 21 of 64

USAAVNCUH-60-04-02, DISABLING OF COCKPIT AIRBAGSYSTEM (CABS) C/W AT 2880.5 ACFT HRS.(AFS222, S NOLIN, 2938, R/SPEC)

10-Jun-2004 1

FT. RUCKER, AL.

thomas.m.lilly

AMCOM/OLROCM/ACE PEFORMED AT 2907 ACFT HRS BYTEAM MEMBER J. (FS6922, S NOLIN, 2938,R/SPEC)

06-Jul-2004 1

FT. C KY.

thomas.m.lilly

USAAVNCAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG. 70400-00003REV. E. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD. A FORWARD CONTROLSERVO INPUT ROD HAS BEEN SHORTENED1/2 TURN IN B. AFT CONTROL SERVO INPUTROD HAS BEEN LENGTHENED 1/2 TURN OUTC. LATERAL HAS NO CHANGE AT 2908.1 ACFTHRS. (S NOLIN, 2938, R/SPEC)

15-Jul-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-04-ASAM-03 FUEL SYSTEM INTEGRITYCHECKS C/W AT 2916.6 ACFT HRS. (AFS132, SNOLIN, 2938, R/SPEC)

05-Aug-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNC#2 CROSSFEED BREAKAWAY VALVEREPLACED I/A/W TB 1-1520-237-20-213 THISDATE AT 2916.6 ACFT HRS. (AFS132, S NOLIN,2938, R/SPEC)

13-Aug-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 2916.6 ACFT HRS. (AFS152, S NOLIN,2938, R/SPEC)

13-Aug-2004 2

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCSOF UH-60-04-04 TECHNICAL, RCS CSGLD-1860 (R1), H-60 MAIN ROTOR HUBSUBASSEMBLY REWORK, UH-60-04-SOF-04C/W AT 2916.6 ACFT HRS. (AFS009, S NOLIN,2938, R/SPEC)

16-Aug-2004 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 FORWARD CONTROLSERVO INPUT ROD HAS NO CHANGE. B. AFTCONTROL SERVO INPUT ROD HAS NOCHANGE. C. LATERAL HAS 1/2 TURN RIGHT AT2916.6 ACFT HRS. (S NOLIN, 2938, R/SPEC)

18-Aug-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCPHASE INSP #6 COMPLETED @ 2916.6 ACFTHRS. NEXT PHASE #7 DUE @ 3416.6 ACFTHRS. (AFS132, S NOLIN, 2938, R/SPEC)

19-Aug-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-04-ASAM-05, RESTRAINT SYSTEMINSPECTION C/W @ 2943.7 ACFT HRS (VK3955,R/SPEC)

27-Sep-2004 1

FT RUCKER, AL

thomas.m.lilly

USAAVNC,CO-PILOTS WINDSHIELD APPEARS TO HAVEHIT BY A BAT OR SMALL BIRD. INSP.COMPLETED NO DAMAGE NOTED AT 2990.4ACFT. HRS. (MF4187 R/SPEC.)

14-Oct-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCRIGHT SIDE OF TAIL PYLON HAS REMAINS OFBIRD. ALSO SOME FEATHERS OF LEFT SIDESTEP FAIRING AT 3005.4 ACFT. HRS. BIRDSTRIKE INSP. COMPLETED NO DAMAGENOTED. (MF4187 R/SPEC.)

16-Oct-2004 1

FT. RUCKER, AL.

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 22 of 64

USAAVNCACFT OPERATING UNDER AWR 1220. A COPYOF THIS AWR IS LOCATED IN THE HISTORICALRECORDS (JB2761 R/SPEC)

21-Oct-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCCHANGED FROM PMS-2 TO PMD ANDINTERVAL INCREASED FROM 500 TO 700 HRSI/A/W AWR 1220 ON THIS DATE @ 3014.3 ACFTHRS. NEXT PHASE # 7 DUE @3616.6 ACFTHRS. (JB2761 R/SPEC)

22-Oct-2004 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCIMPLEMENTATION OF 700 HOUR ESM IAW AWRDTD 28 OCT, R-1 P/C/W AT 3045.6 ACFT HRS.(D.WILLIAMS 0950)

05-Nov-2004 1

FT. RUCKER,AL

thomas.m.lilly

USAAVNCUH-60-05-ASAM-01, REVISION OF FUELSYSTEM INTEGRITY CHECKS (NLT 18JAN05)C/W AT 3112.3 ACFT HRS. (AFS017, S NOLIN,2938, R/SPEC)

11-Jan-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-05-ASAM-02 BLUE FORCE TRACKER(BFT) N/A THIS ACFT AT 3228.6 ACFT HRS.(AFS053, S NOLIN, 2938, R/SPEC)

03-Mar-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-05-SOF-01 REACTIVATION OF COCKPITAIRBAG SYSTEM (CABS) C/W AT 3260.6 ACFTHRS. (AFS017, S NOLIN, 2938, R/SPEC)

16-Mar-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-05-SOF-02 ENHANCED SCHEDULEDMAINTENANCE (ESM) PROGRAMIMPLEMENTION N/A THIS ACFT AT 3267.3 ACFTHRS. (AFS017, S NOLIN, 2938, R/SPEC)

25-Mar-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCOCM/ACE PERFORMED AT 3279 ACFT HRS BYTEAM MEMBER M AMCOM/OLR FT. CKY.(JB7079, S NOLIN, 2938, R/SPEC)

01-Apr-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-05-ASAM-03 AIRCREW RESTRAINTSYSTEM COMPATIBILITY C/W AT 3291.9 ACFTHRS. (AFS009, S NOLIN, 2938, 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 3291.9 ACFT HRS.(AFS152, S NOLIN, 2938, R/SPEC)

09-Apr-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-05-ASAM-06 TROOP SEAT RESTRAINTBUCKLE COMPLETD AT 3363.4 ACFT HRS.(AFS017, S NOLIN, 2938, R/SPEC)

03-May-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-05-ASAM-07 AIR INTRUSION OFHYDRAULIC SYSTEM COMPLETD AT 3401.8ACFT HRS. (JG4539, S NOLIN, 2938, R/SPEC)

13-May-2005 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 FORWARD CONTROLSERVO INPUT ROD HAS BEEN LENGTHENED1/2 TURN. B. AFT CONTROL SERVO INPUTROD HAS BEEN SHORTENED 1/2 TURN. C.LATERAL HAS BEEN LENGHTHENED 1/4TURN. C/W AT 3439.7 ACFT HRS. (S NOLIN,2938, R/SPEC)

17-Jul-2005 1

FT. RUCKER, AL.

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 23 of 64

USAAVNCAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG. 70400-00003REV. E. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD. A FORWARD CONTROLSERVO INPUT ROD HAS BEEN SHORTENED3/4 TURN. B. AFT CONTROL SERVO INPUTROD HAS BEEN LENGTHENED 3/4 TURN. C.LATERAL HAS BEEN LENGHTHENED 1/4TURN. C/W AT 3439.7 ACFT HRS. (S NOLIN,2938, R/SPEC)

24-Jul-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCUH-60-05-ASAM-09 CRASHWORTHYEXTERNAL FUEL SYSTEM (CEFS)INSTALLATION BOLTS C/W AT 3444.1 ACFT.HRS. (AFS133, S NOLIN, 2938, R/SPEC)

02-Aug-2005 1

FT. RUCKER, AL.

thomas.m.lilly

USAAVNCT/R BIAS MEASUREMENTS COMPLETED I/A/WTM1-1520-237-23, PARA 11-4-6. RED:5.120/4.820, YELLOW: 5.120/4.820, BLUE:4.352/4.052, BLACK: 4.352/4.052. (CC0814,R/SPEC)

12-Sep-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 3591.1ACFT. HRS. (CC0814, R/SPEC)

21-Oct-2005 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCAIRWORTHINESS RELEASE 1220 DTD 06-OCT-05 TO CONDUCT ESM OPERATIONALEVALUATION AT THE USAAVNC, FT RUCKER,AL COMPLETED AT 3595.1 HRS. PMI INTERVALINCREASED FROM 700 TO 720 HRS I/A/W 1220NEXT PHASE # 7 DUE AT 3636.6 ACFT HRS.(CC0814, R/SPEC)

21-Oct-2005 2

FT. RUCKER, AL

thomas.m.lilly

USAAVNCACFT OPERATING UNDER AIRWORTHINESSRELEASE 1220 DTD 06-OCT-05 TO CONDUCTESM OPERATIONAL EVALUATION AT THEUSAAVNC, FT. RUCKER, AL (AWR 1220)(CC0814, R/SPEC)

21-Oct-2005 3

FT. RUCKER, AL

thomas.m.lilly

USAAVNCUH-60-05-ASAM-11 WIRING HARNESSCHAFFING C/W AT3633.5 ACFT. HRS. (CC0814,R/SPEC)

30-Nov-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. (CC0814,R/SPEC)

30-Nov-2005 2

FT. RUCKER, AL

thomas.m.lilly

USAAVNCUH-60-05-ASAM-01 REVISION OF FUELSYSTEM INTEGRITY CHECKS (CC0814,R/SPEC)

08-Dec-2005 1

FT. RUCKER, AL

thomas.m.lilly

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

12-Dec-2005 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 24 of 64

USAAVNCAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG. 70400-00003REV. E. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD. A FORWARD CONTROLSERVO INPUT ROD HAS NO CHANGE. B. AFTCONTROL SERVO INPUT ROD HAS NOCHANGE. C. LATERAL HAS NO CHANGE AT3633.5 ACFT HRS. (CC0814, R/SPEC)

14-Dec-2005 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCUH-60-06-ASAM-01 TAIL LANDING GEARSTRUT C/W AT 3633.5 ACFT. HRS. (CC0814,R/SPEC)

14-Dec-2005 2

FT. RUCKER, AL

thomas.m.lilly

USAAVNCT/R BIAS MEASUREMENTS COMPLETED I/A/WTM1-1520-237-23, PARA 11-4-6. RED:5.224/4.890, YELLOW: 5.023/4.686, BLUE:4.476/4.146, BLACK: 4.592/4.256. (CC0814,R/SPEC)

16-Dec-2005 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNC720 PMI # 7 COMPLETED AT 3633.5 ACFT HRS.NEXT PMI # 8 DUE AT 4353.5 ACFT HRS.(CC0814, R/SPEC)

22-Dec-2005 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCT/R BIAS MEASUREMENTS COMPLETED I/A/WTM1-1520-237-23, PARA 11-4-6. RED:5.251/5.534, YELLOW: 5.170/5.453, BLUE:4.642/4.923, BLACK:4.513/4.795. (CC0814,R/SPEC)

25-Jan-2006 1

FT. RUCKER, AL

thomas.m.lilly

USAAVNCACFT CONTINUES TO OPERATE UNDER AWR1153, JP-8+100 FUEL, R2 DTD 30JAN06(CC0814, R/SPEC)

30-Jan-2006 1

FT. RUCKER, AL

thomas.m.lilly

USAACEAWR 927 AWR # 927 DTD 06 JUN 03 FORAN/ASN-128B DOPPLER/GPS NAVIGATIONSYSTEM, JUMP SEAT INSTALLED OR MISSIONSEAT RE-LOCATED, SEALED LEAD BATTERY(SLAB) SYSTEM AND CARGO HOOKINSTALLED. (3862.3 ACFT HRS) (KJ0605R/SPEC)

31-Mar-2006 1

FT. RUCKER, AL

thomas.m.lilly

AMCOMOLR/DYNCORPOCM/ACE PERFORMED AT 3877 ACFT HRS BYTEAM MEMBER J (CC0814)

06-Apr-2006 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCONE TIME INSPECTION OF CONSOLE CIRCUITBREAK PANEL ASSEMBLIES FOR WATERPENETRATION DUE IAW ACLC EMAIL DATED17MAR06 COMPLETED AT 3877 ACFT HRS.(CC0814)

06-Apr-2006 2

FT. RUCKER, AL

thomas.m.lilly

USAAWCUH-60-06-ASAM-02 MAIN ROTOR (M/R) RIGIDCONNECTING LINK/PITCH CONTROLASSEMBLIES C/W AT 3904.9 ACFT. HRS.(CC0814, R/SPEC)

14-Apr-2006 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG. 70400-00003REV. E. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD. A FORWARD CONTROLSERVO INPUT ROD HAS NO CHANGE. B. AFTCONTROL SERVO INPUT ROD HAS NOCHANGE. C. LATERAL HAS NO CHANGE AT3944.6 ACFT HRS. (CC0814, R/SPEC)

04-May-2006 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 25 of 64

USAAWCUH-60-06-ASAM-04 COCKPIT AIRBAG SYSTEM(CABS) ELECTRONIC CRASH SENSOR UNIT(ECSU) DRAIN PLUGS COMPLETED AT 4076.7ACFT HRS. (CC0814, R/SPEC)

22-Jun-2006 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCUH-60-06-SOF-02 DISABLING OF COCKPITAIRBAG SYSTEM (CABS) C/W AT 4076.7 ACFT.HRS. (M. BELFORD 1137)

22-Jun-2006 2

FT. RUCKER, AL.

thomas.m.lilly

USAAWCT/R BIAS MEASUREMENTS COMPLETED I/A/WTM1-1520-237-23, PARA 11-4-6. RED:4.923/4.610, YELLOW: 4.880/4.567, BLUE:4.306/3.993, BLACK:4.306/3.993. (CC0814,R/SPEC)

20-Jul-2006 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCUH-60-06-ASAM-05 BLUE FORCE TRACKERHARDWARE INSTALLATION C/W AT 4116.3ACFT HRS. (DOES NOT APPLY TO THIS ACFT)(CC0814, R/SPEC)

26-Jul-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 @ 4352.8 ACFT HRS. (TB1027R/SPEC)

10-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 4352.8 ACFT HRS. (TB1027R/SPEC)

21-Dec-2006 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCUH-60-07-ASAM-04 AUTOROTATIONALCHARTS COMPLETED AT 4352.8 ACFT HRS.(JT0967 R/SPEC)

03-Jan-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCUH-60-07-ASAM-03 YAW AND COLLECTIVEBOOST SERVOS ROLL PIN COMPLETED AT4352.8 ACFT HRS. (CC0814, R/SPEC)

08-Jan-2007 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 4352.8 ACFT HRS. (CC0814,R/SPEC)

22-Jan-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCUH-60-06-ASAM-02 MAIN ROTOR (M/R) RIGIDCONNECTING LINK/PITCH CONTROLASSEMBLIES C/W AT 4352.8 ACFT. HRS.(CC0814, R/SPEC)

23-Jan-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCACFT IS OPERATING UNDER THE AWR 1153 R-3 DTD 19DEC06, OPERATE WITH JP-8+100FUEL (CC0814, R/SPEC)

24-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 4352.8 ACFT. HRS. (JT0967R/SPEC)

26-Jan-2007 1

FT.RUCKER,AL

thomas.m.lilly

USAAWCT/R BIAS MEASUREMENTS COMPLETED I/A/WTM1-1520-237-23, PARA 11-4-6. RED:4.791/5124, YELLOW: 4.755/5.094, BLUE:4.111/4.446, BLACK:4.093/427 (TB1027 R/SPEC)

05-Feb-2007 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCT/R CABLE TENSION CHECK COMPLETED.L/H: 159 R/H: 159 LBS @ 19'C. (CC0814,R/SPEC)

05-Feb-2007 2

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 26 of 64

USAAWCM/R RIG CK COMPLETED AT 4352.8 ACFT HRSWITH NO CHANGES. (TB1027 R/SPEC)

05-Feb-2007 3

FT. RUCKER, AL.

thomas.m.lilly

USAAWCUH-60-07-ASAM-06 INTERNAL RESCUE HOISTCABLE (GUARD) DEFLECTOR C/W AT 4352.8ACFT. HRS. (JT0967 R/SPEC)

08-Feb-2007 1

FT. RUCKER AL

thomas.m.lilly

USAAWC720 HR PMI #8 COMPLETED @ 4352.8 ACFTHRS. NEXT PMI # 9 DUE @ 5072.8 ACFT HRS.(CC0814, R/SPEC)

09-Feb-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCUH-60-07-AMAM-01 COMMON MISSILEWARNING SYSTEM (CMWS) N/A THIS ACFT. @4425.2 ACFT. HRS. (RJ0827, R/SPEC)

27-Mar-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R BAIS MEASUREMENTS COMPLETED @4473.9 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:5.27/4.94, YELLOW:5.20/4.88,BLACK:4.46/4.13, BLUE:4.53/4.20. (RJ0827,R/SPEC)

07-Apr-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R CABLE TENSION CHECK COMPLETED @4496.2 ACFT HRS. L/H 164, R/H 164 @ 22'C.(RJ0827, R/SEPC)

19-Apr-2007 1

FT. RUCKER, AL

thomas.m.lilly

NO ORGANIZATIONT/R BIAS MEASUREMENTS COMPLETED @4496.2 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: (RJ0827, R/SPEC)

19-Apr-2007 2

(NO LOCATION)

thomas.m.lilly

USAAWCOCM/ACE PERFORMED @ 4497 ACFT HRS BYTEAM MEMBER R. AMCOM PROJECT OLR.(RJ0827, R/SPEC)

26-Apr-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCUH-60-07-ASAM-07 INSTALLATION OF STATICBONDING JUMPERS, N/A TO THIS ACFT. C/WAT 4542.1 ACFT. HRS. (RJ0827, R/SPEC)

12-May-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCACFT OPERATING UNDER AWR 1251, REV 1,DTD 16 MAR 07(INSTL OF EYEBOLTS ONBIFILAR FOR SAFETY HARNESS). @ 4564.0ACFT HRS. (RJ0827, R/SPEC)

17-May-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCACFT. OPERATING UNDER AWR 1220, REV. 3,DTD. 27JUL07. IMPLEMENTATION OF 720HOUR (ESM) REQUIREMENTS AT 4737.8 ACFT.HRS. (RJ0827, R/SPEC)

31-Jul-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCUH-60-07-ASAM-10 MAIN FUEL MANIFOLDCHAFING @ 4773.5 ACFT HRS. (RJ0827,R/SPEC)

21-Aug-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCHYD BAY INSP OF FLIGHT CONTROLHARDWARE COMPLETED @ 4777.7 ACFT HRS.(RJ0827, R/SPEC)

24-Aug-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCBIRD STRIKE INSPECTION COMPLETED @4867.7 ACFT HRS NO DAMAGE FOUND.(RJ0827, R/SPEC)

11-Oct-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCBIRD STRIKE INSPECTION COMPLETED ONRED M/R BLADE UNDERSIDE COMPLETED @4902.4 ACFT HRS. NO DAMAGE FOUND(RJ0827, R/SPEC)

23-Oct-2007 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 27 of 64

USAAWCBIRD FOUND IN #2 ENG INLET ON PREFLIGHT@ 4935.5 ACFT HRS, ENTIRE BIRD CARCASSFOUND ON INLET STATOR.#2 ENG WASH ANDTF EVAL TO DETERMINE SERVICABILITY,HITCHECK COMPLETED FOUND WITHIN LIMITS.(RJ0827, R/SPEC)

31-Oct-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-AMAM-01 MAIN LANDING GEARSHOCK STRUTS C/W AT 4956.2_ACFT. HRS.(RJ0827, R/SPEC)

11-Nov-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R BIAS MEASUREMENTS COMPLETED @4964.0 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:5.247/4.911, BLK:4.431/4.096,YELL:5.201/4.867, BLUE:4.538/4.204. (RJ0827,R/SPEC)

17-Nov-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R CABLE TENSION CHECK COMPLETED @4964.0 ACFT HRS R/H 118, L/H 120, 12'C(RJ0827, R/SPEC)

20-Nov-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R BIAS MEASUREMENTS COMPLETED I/A/WTM1-1520-237-23 PARA 11-4-6 BLK:3.963/3.667,YELLOW:4.766/4.485, BLUE:4.039/3.744,RED:4.746/3.458 (RJ0827, R/SPEC)

20-Nov-2007 2

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-ASAM-02 POWER AVAILABLECONTROL CABLE C/W AT 4964.7_ACFT. HRS.(RJ0827, R/SPEC)

25-Nov-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-ASAM-03 CHANGES TO CURRENTFUEL SYSTEM INTEGRITY CHECKS C/W AT4969.2 ACFT. HRS. (RJ0827, R/SPEC)

01-Dec-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R CABLE TENSION CHECK COMPLETED @4973.5 ACFT HRS. TENSION NOT STABALIZEDI/A/W 1-1520-237-23 WP1695, L/H:123, R/H:123@ 12'C (RJ0827, R/SPEC)

03-Dec-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-AMAM-02 TAIL ROTOR OUTBOARDRETENTION PLATE SHIMS @ 4971.4 ACFT HRS.(RJ0827, R/SPEC)

03-Dec-2007 2

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R CABLE TENSION CHECK COMPLETED @4982.8 ACFT HRS L/H 135, R/H 136 @ 22'C.(RJ0827, R/SPEC)

12-Dec-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-ASAM-05 TAIL ROTOR QUADRANTSPRING CAPSULE ASSEMBLY C/W AT 4989.5ACFT. HRS. (RJ0827, R/SPEC)

15-Dec-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R CABLE TENSION CHECK COMPLETED @4992.4 (CABLES STABALIZED) L/H 140, R/H 140@ 22'C (RJ0827, R/SPEC)

18-Dec-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-ASAM-04 PILOT**S LOWER SEAT RAILCHAFING ELECTRICAL HARNESS @ 4997.7ACFT HRS. (RJ0827, R/SPEC)

19-Dec-2007 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-AMAM-04 H-60-08-AMAM-04 COCKPITDOOR JETTISONABLE WINDOWS @ 5011.7ACFT HRS (RJ0827, R/SPEC)

17-Jan-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-SOF-01 M/R BLADE EXPANDABLE PININSPECTION CHANGE C/W AT 5016.2 ACFTHRS. (RJ0827, R/SPEC)

28-Jan-2008 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 28 of 64

USAAWCAIRCRAFT NO LONGER OPERATING IAW AWRDATED 19 DEC 06 (JP-8+100 FUEL) (ACFT HRS5025.9). AFS558 (RC1002)

31-Jan-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-AMAM-05 GOODRICH INTERNALRESCUE HOISTS N/A TO THIS ACFT (5028.7ACFT HRS) (RJ0827, R/SPEC)

02-Feb-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-AMAM-06 COMMON MISSILE WARNINGSYSTEM (CMWS) SEQUENCERS - N/A TO THISACFT (5037.2 ACFT HRS) (RJ0827, R/SPEC)

07-Feb-2008 1

FT. RUCKER, AL

thomas.m.lilly

DYNCORP OLROCM/ACE PERFORMED @ 5070 ACFT HRS BYTEAM MEMBER R (TS0568)

11-Mar-2008 1

FT. CAMPBELL KY

thomas.m.lilly

USAAWCH-60-08-ASAM-06 M/R PYLON SLIDINGFORWARD FAIRING C/W AT 5070.6 ACFT HRS(RJ0827, R/SPEC)

15-Mar-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-AMAM-07 AN/ASN-128B/D DOPPLERGPS NAVIGATION SET (DGNS) (5070.6 ACFTHRS) (RJ0827, R/SPEC)

29-Mar-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAACEAWR 927 AWR # 927 DTD 06 JUN 03 FORAN/ASN-128B DOPPLER/GPS NAVIGATIONSYSTEM, JUMP SEAT INSTALLED OR MISSIONSEAT RE-LOCATED, SEALED LEAD BATTERY(SLAB) SYSTEM AND CARGO HOOKINSTALLED. (KJ0605 R/SPEC)

31-Mar-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCUH-60-08-ASAM-01 TROOP/GUNNER SEATUPPER ENERGY ATTENUATING WIRES N/ATHIS ACFT. AT 5070.6 ACFT. HRS. (RJ0827,R/SPEC)

02-Apr-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWC1/4" CRACK IN FWD TANG OR TAB OF RH SIDE308 FRAME VERIFIED BY NDI- (12 MAR 08)REPAIRED IAW MEC# F73517 (08 APR-08 @5070.6 ACFT HRS) (RJ0827, R/SPEC)

08-Apr-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R BIAS MEASUREMENTS COMPLETED @5070.6 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:5.230/4.897, BLACK:4.42/4.10,YELLOW:5.200/4.880, BLUE:4.480/4.140.(RJ0827, R/SPEC)

18-Apr-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCM/R RIG CK COMPLETED @ 5070.6 ACFT HRS,THE FOLLOWING ADJ WERE MADE: FWD:1/2SHORT, AFT: 1/2 LENGTHENED, LAT: 1 FLATSHORTING (RJ0827, R/SPEC)

18-Apr-2008 2

FT. RUCKER, AL

thomas.m.lilly

USAAWC720 HR PMI #9 COMPLETED @ 5070.6 ACFTHRS. NEXT PMI # 10 DUE @ 5790.6 ACFT HRS.(RJ0827, R/SPEC)

22-Apr-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R BIAS MEASUREMENTS COMPLETED @5071.6 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:5.215/4.882, BLACK: 4.409/4.075,YELLOW: 5.152/4.811, BLUE: 4.422/4.093(RJ0827, R/SPEC)

23-Apr-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAWCT/R BIAS MEASUREMENTS COMPLETED @5072.1 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6, RED: 5.187/4.875, YELLOW:5.187/4.875,BLUE:4.437/4.125, BLACK 4.437/4.125 (RJ0827,R/SPEC)

24-Apr-2008 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 29 of 64

USAAWCT/R BIAS MEASUREMENTS COMPLETED @5072.1 ACFT HRS BLUE-4.48/4.15/.33, YELLOW- 5.22/4.88/.34, BLACK - 4.44/4.10/.34, RED -5.26/4.92/.32. (TB1027 R/SPEC)

26-Apr-2008 1

FT. RUCKER, AL.

thomas.m.lilly

USAAWCT/R BIAS MEASURMENTS COMPLETED @5074.6 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6, RED: 5.017/4.705, BLACK:4.306/3.994,BLUE:4.306/3.994, YELLOW:5.017/4.705(RJ0827, R/SPEC)

30-Apr-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCREQUEST FOR AUTHORIZATION TO DEVIATEFROM WP 1194 00 PG 1194 REGARDING NON-REPAIRABLE/REPLACEABLE WIRINGHARNESS P/N 70550-02129-112, TO FORGOREPLACEMENT UNTIL THE NEXT MAJORMAINT EVENT OR NEXT PMI-2 AND TOCONTINUE TO FLY BY REMOVING CABLESFROM THE SLIP RING, SEAL W/PROSEAL ANDADD ACFT TO LIST OF ACFT AWAITING PMIINSP TO REPLACE DE-ICE RING WITH NEWAND IMPOVED SLIP RING W/TEMOVABLE DE-ICE CABLES. APPROVED WITH MEC # F75887,SEE COPY OF MEC IN BACK OF HISTORICALRECORDS. ( (RJ0827, R/SPEC)

30-Apr-2008 2

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R CABLE TENSION CK DUE FOR REPL OFBOTH TAIL PYLON CABLES CK FAILED (5080.3ACFT HRS) L/H 133, R/H132 @ 16'C (RJ0827,R/SPEC)

14-May-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCT/R CABLE TENSION CK COMPLETED @5090.4 ACFT HRS STABALIZED I/A/W WP1695R/H:155, L/H:157 @ 27'C (RJ0827, R/SPEC)

20-May-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCMAINTAIN ACFT AS PRESCRIBED IN AWR 1220,DTD 22 MAY 08 R-4. (ENHANCED SCHEDULEDMAINTENANCE) (@ 5130.1 ACFT HRS.)(RJ0827, R/SPEC)

04-Jun-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAAWCH-60-08-AMAM-08 COMPLIED WITHREQUIREMENTS OF H-60-08-AMAM-08 FLIGHTCONTROL RIGGING UPDATE AT 5135.2 ACFTHRS. (RJ0827, R/SPEC)

07-Jun-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAACEOPERATE ACFT WITHIN LIMITATIONSSPECIFIED IN AWR 1251, DTD 16 MAR 07(EYEBOLTS INSTALLED ON BIFILAR ARMS)(AWR 1251, REV 1.) (RJ0827, R/SPEC)

20-Jun-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAACEM/R RIG CK COMPLETED @ 5168.7 ACFT HRS -NO ADJ MADE (RJ0827, R/SPEC)

10-Jul-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-08-ASAM-11 COMPLIED WITHREQUIREMENTS OF H-60-08-ASAM-11 FLIGHTCONTROL INSPECTION AT5205.9_ ACFT HRS.(RJ0827, R/SPEC)

24-Aug-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-08-ASAM-13 H-60-08-ASAM-13 FIREEXTENGUISHING TUBE UNION RINGCOMPLETED AT 5213.4 ACFT HRS. (RJ0827,R/SPEC)

24-Sep-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAACEACFT OPERATING UNDER REVISED AWR 1251REV 2 (EYEBOLTS INSTALLED ON BIFILARARMS) (@ 5334.4 ACFT HRS. (RJ0827, R/SPEC)

25-Sep-2008 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 30 of 64

USAACEH-60-08-ASAM-12 PARKER AEROSPACE AIRTURBINE STARTER (ATS) COMPLETED 5229.9(AFS 576) KJ (R/SPE C)

04-Oct-2008 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEH-60-09-SOF-01 HYDRO-MECHANICAL UNIT(HMU) H-60-09-SOF-01 COMPLETED AT 5274.9ACFT HRS. (RJ0827, R/SPEC)

23-Oct-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-09-SOF-02 H-60-09-SOF-02 AN/ALQ-144INFRARED COUNTERMEASURE SYSTEM(IRCMS) COMPLETED @ 5303.0 ACFT HRS.NOT INSTALLED ON THIS ACFT. (KJ0605R/SPEC (INSP. AFS 528))

08-Nov-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLIED WITH REQUIREMENTS OF H-60-09-SOF-03 (POSSIBLE RETIREMENT LIFEOVERFLIGHT) @ 5315.2 ACFT HRS. (KJ0605R/SPEC (INSP. AFS 512))

15-Nov-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAACEACFT OPERATING UNDER AWR 1479 DTD 04JAN 08, HCPTS WITH MAIN MOD P/N -075 & -076. EQUIPPED WITH IMPROVED PLANETARYCARRIER ASSY, P/N -046 @ 5334.4 ACFT HRS(KJ0605 R/SPEC)

26-Nov-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-08-ASAM-10 ELECTRICAL WIRE CHAFEISSUES C/W @ 5353.9 ACFT HRS. (JT0967R/SPEC)

13-Dec-2008 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-09-ASAM-01 (T701C GAS GENERATORASSEMBLIES) C/W @ 5297. ACFT HRS, N/ATHIS ACFT (JT0967)

13-Jan-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACET/R BIAS CHECK COMPLETED @ 5433.6 ACFTHRS. BLACK: 4.292, 3.958, 0.334 YELLOW:5.037, 4.706, 0.331 BLUE: 4.268, 3.939, 0.329,RED: 5.057, 4.725, .332, 0.332 (KJ0605 R/SPEC)

23-Jan-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-09-ASAM-04 UH-60, AVIATION SAFETYACTION MESSAGE (ASAM) MAINTE.MANDATORY, RESCUE HOIST MARK 44 MOD 0CARTRIDGE DEVICE. C/W (N/A THIS ACFT) @5517.5 ACFT HRS. (KJ0605 R/SPEC)

28-Feb-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLY WITH REQUIREMENTS OF H-60-09-ASAM-05 UPDATE TO LIFE LIMIT CHANGE FORTAIL ROTOR (TR) QUADRANT SPRINGCAPSULES NLT 03 APR 09 (COMPLIED WITH @5537.9 ACFT HRS.) (KJ0605)

05-Mar-2009 1

FT. RUCKER, AL

thomas.m.lilly

DYNCORPINTERNATIONALAMCOM RASM-E

OCM/ACE PERFORMED @ 5549.6 ACFT HRSBY TEAM MEMBER J (LH9501)

11-Mar-2009 1

FT. CAMPBELL, KY

thomas.m.lilly

USAACEH-60-09-ASAM-07 H-60-09-ASAM-07, FIREEXTINGUISHER WIRING (BREAKAWAYTHREAD) COMPLETED AT 5607.8 ACFT HRS.(JT0967 R/SPEC)

08-Apr-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEM/R RIG CK COMPLETED @ 5694.8 ACFT HRS-NO INFO GIVEN ABOUT ADJ. (JT0967 R/SPEC)

03-May-2009 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 31 of 64

USAACER/H INPUT MOD CHIP DETECTOR HOUSINGWAS ABLE TO SPIN FREELY. DURINGSUBSEQUENT INSP. THE HOUSING ACTUALLYCAME OUT OF THE MODULE. BELIEVE THATTHE PIN THAT HOLDS THE HOUSING INBROKE OFF ALLOWING HOUSING TO SPINFREELY. REQUEST PERMISSION TOREINSTALL CHI DETECTOR OUSING AND PINUSING SIKORSKY REPAIR PROCEDURE SE-3160T064, AND CONTINUE SERVICE OF ACFT.THIS REPAIR WOULD PREVENT THEREPLACEMENT OF THE MAIN TRANSMISSION.THERE DOES NOT APPEAR TO BE ANYDAMAGE TO THE INNER DIAMETER OF THEHOUSING. REQUEST TO REPAIR USINGSIKORSKY PROCEDURE SE-3160T064 ISGRANTED. MEC F92186 (AUTORIZED BYTAMMY S. GRIFFIN 06 MAY 09.) SEE COPY OFMEC IN BACK OF HISTORICAL RECORDS.(KJ0605)

06-May-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-09-ASAM-09 FIRE EXTINGUISHER WIRING(BREAKAWAY THREAD) COMPLETED AT5704.8 ACFT HRS. (JT0967 R/SPEC)

09-May-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-09-ASAM-08 ENGINE COWLING WEIGHTRESTRICTION COMPLETED AT 5658.0 ACFTHRS. (JT0967)

17-May-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEDURING PHASE INSP. THE REAR APUCOWLING WAS FOUND TO HAVE A CRACK 4INCHES BY 10 INCHES CREATING A VOID. THEVOID/CRACK EXCEEDS THE REPAIRABLEAREA AS DESCRIED IN TM 1-1520-237-23WHICH IS 20% OF THE TOTAL AREA. REQUESTDEVIATION TO REPAIR THE VOIDED/CRACKEDAREA USING THE PROCEDURES OUTLINED INTM 1-120-237-10 TO INCLUDE REPLACEMENTOF THE CORE MATERIAL IF REQUIRED.SIMILIAR REPAIRS HAVE BEEN AUTHORIZEDUNDER MEC F92481, F57997 & F93203.REQUEST TO REPAIRE AS OUTLINED ISGRANTED. MEC F94292 LOCATED IN REAR OFHISTORICAL RECORDS. TAMMY S. GRIFFIN(KJ0605)

22-Jun-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEMEC# F94401 - FUSELAGE STRUCTUREDEVIATION ON THE RIGHT HAND FORWARDENGINE COWLING FITTING. REPAIR, ADDDAILY INSPECTION AND REPLACE UPON NEWPART RECEIPT WITHOUT DELAY. MECLOCATED IN REAR OF HISTORICAL RECORDS.TAMMY S. GRIFFIN (JT0967)

25-Jun-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEMEC# F94459 - FUSELAGE STRUCTUREDEVIATION ON THE LEFT HAND FORWARDENGINE COWLING FITTING. REPAIR, ADDDAILY INSPECTION AND REPLACE UPON NEWPART RECEIPT WITHOUT DELAY. MECLOCATED IN REAR OF HISTORICAL RECORDS.TAMMY S. GRIFFIN (KJ0605 R/SPEC)

25-Jun-2009 2

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 32 of 64

USAACEH-60-09-ASAM-11 CARGO DOOR WINDOWEMERGENCY JETTISON HANDLE INSP C/W AT5775.0 ACFT HRS. (MB1137)

01-Jul-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACET/R CABLE TENSION CK.W/ L/H164, R/H 165 @26°C. @ 5775 ACFT HRS. (JB2761 R/SPEC)

06-Jul-2009 1

FT. RUCKER, AL.

thomas.m.lilly

USAACET/R BIAS CHECK COMPLETED @ 5775.5 ACFTHRS. BLACK: 4.079/4.407=0.328, YELLOW:4.843/5.170=.327, BLUE: 4.058/4.392=.334 RED:4.825/5.156=.331, (JB2761 R/SPEC)

06-Jul-2009 2

FT. RUCKER, AL.

thomas.m.lilly

USAACEAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG. 70400-00003REV. E. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD. A FORWARD CONTROLSERVO INPUT ROD HAS 3 FLATS OUT. B. AFTCONTROL SERVO INPUT ROD HAS 3 FLATS IN.C. LATERAL HAS3 FLATS OUT AT 5775 ACFTHRS. (JB2761 R/SPEC)

06-Jul-2009 3

FT. RUCKER, AL.

thomas.m.lilly

USAACEPHASE INSPECTION #10 COMPLETED AT5775.0 ACFT HRS. PHASE # 11 DUE AT 6495.0ACFT HRS. (MB1137)

09-Jul-2009 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEACFT GROUNDED FOR H-60-09-ASAM-07 ANDH-60-09-ASAM-09 NOT COMPLIED WITH.COMPLETED BY AFS594 @ 5846.7 ACFT HRS.(JT0967)

13-Aug-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLIED WITH REQUIREMENTS OF GEN-09-AMAM-03, ULLS-A(E) AT 5865.3 ACFT HRS.AFS543 NA DUE TO UNIT NOT CURRENTLYUTILIZING ULLS-A (E). (JT0967)

25-Aug-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-09-AMAM-04 H-60-09-AMAM-04 CO-PILOTSEAT INTERFERENCE WITH ARMY AIRBORNCOMMAND CONTROL SYSYEM (A2C2S)COMPLETED AT 5865.3 ACFT HRS. (JT0967)

26-Aug-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLIED WITH REQUIREMENTS OF H-60-09-AMAM-06 AT 5874.4 ACFT HRS. CARGO HOOKCARTRIDGE ACTUATED DEVICE (CAD) LIFEREDUCTION. AFS522 (JB2761 R/SPEC)

27-Aug-2009 1

FT. RUCKER, AL.

thomas.m.lilly

USAACET/R CABLE TENSION C/W @ 5874.4 ACFT HRS.L/H=170; R/H=170 @ 33°C. (JT0967)

03-Sep-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACET/R BIAS CHECK COMPLETED @ 5875.9 ACFTHRS. BLACK: 4.432/4.897; YELLOW:5.223/4.889; BLUE: 4.450/4.116; RED:5.205/4.873. (JT0967)

03-Sep-2009 2

FT. RUCKER, AL

thomas.m.lilly

USAACEM/R RIG CK COMPLETED @ 5879.9 ACFT HRS-ADJ. MADE: FWD - 4 FLAT CW; AFT - 4 FLATSCCW; LAT - 2 FLATS CW. (JT0967)

03-Sep-2009 3

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-09-AMAM-07 HALON HAND-HELD FIREEXTINGUISHERS (HHFE) C/W AT 5893.0 ACFTHRS. (JT0967)

17-Sep-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEOPERATE WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1607, REV .1. DTD 21 SEP 09. NA CDU NOT INSTALLED ONTHIS ACFT. 5913.1 ACFT HRS (JT0967)

26-Sep-2009 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 33 of 64

USAACET/R BIAS CHECK COMPLETED @ 5936.9 ACFTHRS. BLACK: 4.39/4.06; YELLOW: 5.20/4.87;BLUE: 4.39/4.06; RED: 5.20/4.87. (JT0967)

11-Oct-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-10-ASAM-01 HAMILTON-SUNDSTRANDHYDRO-MECHANICAL UNITS COMPLETED AT5444.0 ACFT HRS (PASS) (DW0950)

14-Oct-2009 1

FT. RUCKER, AL.

thomas.m.lilly

USAACET/R BIAS CHECK COMPLETED @ 5946.5 ACFTHRS. BLACK: 4.425/4.090/.335 YELLOW:5.181/4.838/.343 BLUE: 4.43/4.092/.338 RED:5.192/4.858/.334 (KJ0605 R/SPEC)

15-Oct-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACET/R CABLE TENSION CK - NOT STABILIZED @5946.5 - PREVIOUS RDGS: R/H:140, L/H:141, @19 * C (KJ0605 R/SPEC)

15-Oct-2009 2

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. (KJ0605)

15-Oct-2009 3

FT. RUCKER, AL

thomas.m.lilly

USAACET/R CABLE TENSION CK COMPLETED @5952.7 ACFT HRS. LH: 140 RH: 140 @ 22(KJ0605 R/SPEC)

20-Oct-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEACFT OPERATING WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1505 DTD13 FEB 09 REV-2 ( 5 MICRON METAL MESHHYD FILTER & HYD SYS SAMPLING VALVE. @5765.5 ACFT HRS. (KJ0605 R/SPEC)

26-Oct-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLIED WITH REQUIREMENTS OF H-60-10-AMAM-04, ASN-128 B/C DOPPLER GLOBALPOSITIONING SYSTEM GPS NAVIGATION SET,NLT 17 NOV 09 @ 6026.1 ACFT HRS. (MQ6211R/SPEC)

11-Nov-2009 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEH-60-10-ASAM-03 (FIRE BOTTLE DISCHARGELINES AND NOZZLES) C/W @ 6045.1 ACFTHRS. ( AFS 562) (KJ0605 R/SPEC)

14-Nov-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEMAIN MOD SN: A265-00675 WITH TSN: 5037 -FILTER BUTTON POPPED @ 6052.0 ACFT HRS.FILTERS REPLACED. (AFS791) (KJ0605R/SPEC)

17-Nov-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEMAIN MOD SN: A265-00675 WITH TSN: 5037 -FILTER BUTTON POPPED @ 6057 ACFT HRS.FILTERS REPLACED. (AFS791) (KJ0605R/SPEC)

18-Nov-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-10-ASAM-04 STABILITY AUGMENTATIONSYSTEM (SAS) LINKS C/W AT 6056.6 ACFT HRS(AFS 576) (KJ0605 R/SPEC)

18-Nov-2009 2

FT. RUCKER, AL

thomas.m.lilly

USAACEACFT OPERATING IAW AWR 1505 (R-3) DTD 21OCT 09. (5-MICRON METAL MESH HYD FILTER)@ 6089.7 ACFT HRS. (KJ0605 R/SPEC)

08-Dec-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLIED WITH REQUIREMENTS OF TB 1-1520-237-23-9 AND TB 1-1520-237-23-10 (FUELCELL CORROSION INSPECTION) AT 6101.4ACFT HRS. AFS638 (RC1002)

14-Dec-2009 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 34 of 64

USAACET/R CABLE TENSION CK COMPLETED @5952.7 ACFT HRS. LH: 136 RH: 137 @ 23* C.(RC1002)

15-Dec-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACET/R BIAS CHECK COMPLETED @ 6101.4 ACFTHRS. BLACK: 3.746/3.450/.296 YELLOW:4.520/4.229/.291 BLUE: 3.753/3.445/.308 RED:4.526/4.224/.302 (RC1002)

16-Dec-2009 1

FT. RUCKER, AL

thomas.m.lilly

USAACEMAIN ROTOR HEAD RIGGED SYSTEMCONTROLS HAVE BEEN BIASED IN ACCORD.A. AFT CONTROL SERVO INPUT ROD HASBEEN 1/2 TURN LONGER. B. LATERALCONTROL SERVO INPUT ROD HAS BEEN NOTBEEN CHANGED. C. FORWARD CONTROLSERVO INPUT ROD HAS BEEN 1/2 TURNSHORTER @ 6101.4 ACFT HRS. (RC1002)

16-Dec-2009 2

FT. RUCKER, AL

thomas.m.lilly

USAACEACFT NO LONGER OPERATING IAW AWR 1479DTD 04 JAN 08 (IMPROVED MAINTRANSMISSION PLANETARY CARRIER ASSY)@ 6103.9 ACFT HRS. (AFS 592) (KJ0605)

04-Jan-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACET/R BIAS CHECK COMPLETED @ 6135.0 ACFTHRS. BLACK: 4.415/4.085/.330 YELLOW:5.150/4.815/.335 BLUE: 4.420/4.086/.334 RED:5.110/4.775/.335 (KJ0605)

21-Jan-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACECOMPLY WITH REQIREMENTS OF GEN-10-AMAM-02 (DISTRIBUTION OF NEW ULLS-A (E)AIRCRAFT ELECTRONIC LOGBOOK) NLT 05FEB 10. N/A THIS FACILITY @ 6147.7 ACFTHRS. (AFS592) (KJ0605)

25-Jan-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-10-AMAM-11 OIL SAMPLING CHANGESCOMPLETED AT 6165.8 ACFT. HRS. (AFS 592)(KJ0605)

02-Feb-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-10-ASAM-06 AUTO-IGNITION ANDTRANSIENT DROOP IMPROVEMENT TDIMODIFICATION COMPLETED AT 6186.4 ACFTHRS. (AFS9) (KJ0605)

10-Feb-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-10-AMAM-05 ULLSA IMMC LCF CHANGE60B C/W AT 6200.5 ACFT HRS. (AFS 793)(KJ0605)

13-Feb-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEACFT OPERATING IAW 1251 (R-3) DTD 26 FEB10 (EYEBOLTS) @ 6236.4 ACFT HRS. (KJ0605)

01-Mar-2010 1

FT. RUCKER, AL

thomas.m.lilly

AMCOM/RASM-EOCM/ACE PERFORMED @ 6243 ACFT HRS BYTEAM MEMBER DD (KJ0605)

03-Mar-2010 1

FT. CAMPBELL, KY

thomas.m.lilly

USAACEMEC# F94401 - FUSELAGE STRUCTUREDEVIATION ON THE RIGHT HAND FORWARDENGINE COWLING FITTING. (NO LONGERREQUIRED) - ACFT INSP & FOUND TO BEREPLACED @ 6240.1 ACFT HRS. (AFS 514 -WW4464) (KJ0605)

07-Mar-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEMEC# F94459 - FUSELAGE STRUCTUREDEVIATION ON THE LEFT HAND FORWARDENGINE COWLING FITTING. (NO LONGERREQUIRED) - ACFT INSP & FOUND TO BEREPLACED @ 6240.1 ACFT HRS. (AFS 514 -WW4464) (KJ0605)

07-Mar-2010 2

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 35 of 64

USAACEACFT OPERATING IAW MEO A6055 REV A. DUETO M/R DROOP STOP BUSHING DE-BONDED.REPLACEMENT REQUIRED AT NEXT PMI DUE@ 6495.0 ACFT HRS. (BLACK LEAD BUSHING)(KJ0605)

24-Mar-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACE#2 CROSSFEED BREAKAWAY VALVEREPLACED I/A/W TB1-1520-237-20-213 @6257.4 ACFT HRS. (KJ0605)

25-Mar-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEACFT OPERATING IAW MEC F107474 - L/HBEADED PANEL CRACKED IN 9 PLACES, 3 OFTHE CRACKS PROGRESS UNDER THE "PDOUBLER" BEADED PANEL TO BE REPLACEDUPON RECEIPT OF NEW KIT & ASSOCIATEDMOD KITS. (KJ0605)

16-Apr-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-10-AMAM-12 IMPROVED DRAG BEAM C/WAT 6295 ACFT HRS (JB2761 R/SPEC)

04-May-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEACFT NO LONGER OPERATING UNDER AWR#927. SUPERCEDED BY AWR 1681. ACFT HRS6295. (JB2761 R/SPEC)

18-May-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEAWR 1681 AWR DTD 10 MAY 10 FOR AN/ASN-128B DOPPLER/GPS NAVIGATION SYSTEM,JUMP SEAT INSTALLED OR MISSION SEAT RE-LOCATED, SEALED LEAD BATTERY (SLAB)SYSTEM AND CARGO HOOK INSTALLED.(6295.ACFT HRS) (JB2761 RSPEC)

18-May-2010 2

FT. RUCKER, AL.

thomas.m.lilly

USAACEIAW MEC F107474 - L/H BEADED PANELREPLACED THIS DATE @ 6295 ACFT HRS.(JB2761 R/SPEC)

18-May-2010 3

FT. RUCKER, AL.

thomas.m.lilly

USAACEACFT OPERATING UNDER LIMITATIONS ANDREGULATIONS SPECIFIED IN AWR 1639 DTD 26JAN 10 (BFT/EDM) @ 6295 ACFT HRS (JB2761R/SPEC)

20-May-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEH-60-10-ASAM-07 STABILATOR HINGEFITTINGS C/W AT 6295.5 ACFT HRS (JB2761R/SPEC)

22-May-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEM/MODULE ASSY BYPASS BUTON POPPED @6295 ACFT HRS. REPLACED FILT ELEMENTAND RESET IAW3657. (JB2761 R/SPEC)

24-May-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEACFT OPERATING IAW AWR 1220 (R-5) DTD 28MAY 10 (ESM) (KJ0605)

01-Jun-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-10-ASAM-08 APU AND APU FIREWALLC/W AT 6332.4 ACFT HRS. (AFS745) (KJ0605)

05-Jun-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEACFT OPERATING IAW AWR 1639 (R-2) DTD 28MAY 10 (BFT/EDM) (KJ0605)

14-Jun-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-10-SOF-02 SPINDLE LUG NDI ANDRETIREMENT LIFE CHANGES C/W AT 6377.5ACFT HRS. (AFS 594) (KJ0605 (R/SPEC))

22-Jun-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACEH-60-10-AMAM-16 COMMON MISSILE WARNINGSYSTEM GUARDED DISPENSE SWITCH C/W AT6394.4 ACFT HRS. (AFS 594) (KJ0605 (R/SPEC))

25-Jun-2010 1

FT. RUCKER, AL

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 36 of 64

USAACEMAIN MOD HOUSING TBO TIME EXTENDED1300 HOURS (ONE TIME EXTENSION FOR S/N:015152-1856) PER MEC F110769 DTD 22 JUN 10- AT 6377.5 ACFT HRS. TIME TO NEXT PMI 117.5ACFT HRS. (RJ0827, R/SPEC)

08-Jul-2010 1

FT. RUCKER, AL

thomas.m.lilly

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

19-Jul-2010 1

LOWE AHP, FT.RUCKER, AL.

dean.a.keirn

USAACEH-60-10-ASAM-11 COMMON COMPONENTRETIREMENT CHANGE TIMES UPDATE C/W AT6476.7 (AFS 545) (KJ0605 (R/SPEC))

02-Aug-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEH-60-10-ASAM-12 T700 SERIES ENGINESCOMMON COMPONENT RETIREMENT CHANGETIMES C/W AT 6489.8 ACFT HRS. (AFS594)(KJ0605(R/SPEC))

10-Aug-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEH-60-10-ASAM-15 IMPROVE EXTERNAL STORESUPPORT SYSTEM (ESSS) FUEL; SYSTEMVENT ELBOW C/W AT 6491.8 ACFT HRS. (AFS556) (KJ0605 (R/SPEC))

12-Aug-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEACFT NO LONGER OPERATING IAW MEODROOP STOP BUSHING DE-BONDED. (BLACKLEAD BUSHING REPLACED DURING PMI @6491.8 ACFT HRS. (AFS 577) (KJ0605 (R/SPEC))

23-Aug-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACET/R CABLE TENSION CHECK COMPLETED AT6491.8 ACFT HOURS L/H: 160 TR/H 160 @ 28*C(JC6208)

28-Aug-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACET/R BIAS COMPLETED @ 6491.8 ACFT HOURS.RED: 4.804/5.134 (.330) BLUE: 4.076/4.396 (.320)YELLOW: 4.720/5.050 (.330) BACK: 1.008/4.340(.332) (JC6208)

28-Aug-2010 2

FT. RUCKER, AL.

thomas.m.lilly

USAACEPHASE INSPECTION #11 COMPLETED AT6491.8 ACFTH RS. PHASE #12 DUE AT 7211.8ACFT HRS. ((SC2006), R/SPEC)

30-Aug-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEM/R RIG CHECK COMPLETED @ 6491.8 ACFTHOURS. FWD: SHORTEN 1 FLAT; AFTLENGTHEN 1 FLAT; LAT: LENGTHEN 2 FLAT(JC6208)

30-Aug-2010 2

FT. RUCKER, AL.

thomas.m.lilly

USAACEDURING PHASE INSPECTION WAS FOUNDSOMETIME IN THE PAST THREADEDFASTENER WERE INSTALLED IN THE RIGHTHAND 34.5 BEAM. AUTHORIZATION GRANTEDTO LEAVE FASTENERS IN PLACE AND KEEPAIRCRAFT SERVICE I/A/W MEC F114001. ACOPY OF THIS MEC IS LOCATED IN THEHISTORICAL RECORDS. ACFT HRS 6491.8(DW0950 R/SPEC.)

31-Aug-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACEH-60-10-ASAM-16 (RESCUE HOIST CABLE CUTHARNESS CONNECTOR) C/W AT 6496.4 ACFTHRS. *NO HOIST INSTALLED (AFS 77) (KJ0605(R/SPEC))

09-Sep-2010 1

FT. RUCKER, AL.

thomas.m.lilly

USAACET/R CABLE TENSION CK SOMPLETED @ 6501.4ACFT HRS. R/H: 154. L/H: 154 @ 25* C. (KJ0605)

11-Sep-2010 1

FT. RUCKER, AL.

thomas.m.lilly


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 37 of 64

USAACE,H-60-11-AMAM-03 H-60-11-AMAM-03 OILCOOLER FAN AXIAL BEARING C/W AT 6606.4ACFT HRS. NA IND/IVHMS NOT INSTL.(AFS594)

26-Oct-2010 1

FT. RUCKER, AL

thomas.m.lilly

USAACE,H-60-11-AMAM-04 H-60-11-AMAM-04 ULLS-A(E)(IMMC) (LCF CHANGE 61) C/W AT 6606.4 ACFTHRS. (NA) (AFS 594) (KJ0605 R/ SPEC)

26-Oct-2010 2

FT. RUCKER, AL.

thomas.m.lilly

USAACE, FT RUCKER,AL

H-60-11-AMAM-03 H-60-11-AMAM-03 OILCOOLER FAN AXIAL BEARING C/W AT 6606.4ACFT HRS. NA IMD/IVHMS NOT

26-Oct-2010 3

LOWE AHP

KJ0605

USAACE,ACFT OPERATING IAW AWR 1455 (R-1) DTD 23OCT 09. (BATTELLE CAUTION ADVISORY CAP)@ 6647.3 ACFT HRS. (KJ0605)

12-Nov-2010 1

FT. RUCKER, AL

thomas.m.lilly


MAIN MOD S/N: A265-00675 WITH TSN-5640 OILFILTER IMPENDING BYPASS BUTTON POPPED@ 6655 ACFT HRS. OIL FILTER REPLACED

17-Nov-2010 1

LOWE AHP

KJ0605


H-60-11-ASAM-03 HAMILTON STANDARDHYDRO-MECHANICAL UNITS (HMU) M/A BY P/N(AFS 594) #1 UDAJ0407, #2 UDA93539 @ 6671.8

29-Nov-2010 1

LOWE AHP

KJ0605


H-60-11-ASAM-04 AN/ARN-153 TCN-500 TACANRECEIVER BEARING ERROR C/W AT 6690.2ACFT HRS. (AFS 767) N/A ACFT NOTEQUIPPED

03-Dec-2010 1

LOWE AHP

KJ0605


T/R CABLE TENSION CK COMPLETED @6690.2 ACFT HRS. L/H 148, R/H 148 @ 18.7DEG C.

04-Dec-2010 1

LOWE AHP

KJ0605

USAACE, FT. RUCKER,AL

T/R CABEL TENSION CK COMPLETED @6690.2 ACFTR HRS. R/H 150 L/H 150 @ 18.8DEG C.

07-Dec-2010 1

LOWE AHP

KJ0605


H-60-11-ASAM-03 HAMILTON STANDARDHYDRO-MECHANICAL UNITS (HMU). # 1 HMUS/N UDAJ0407 REPALCED WITH HUM S/NUDAJ4513 @ 6771.3 ACFT HRS.

12-Jan-2011 1

LOWE AHP

KJ0605


H-60-11-AMAM-06 MEDICAL CAROUSELREFURBISHMENT C/W AT 6816.4 ACFT HRS.N/A THIS ACFT.

07-Feb-2011 1

LOWE AHP

JT0967


H-60-11-ASAM-08 LOS/ IFF ANTENNAA ANDIVHMS ACCELEROMETER CONNECTORSSAFETY WIRE C/W AT 6825 ACFT HRS.

13-Feb-2011 1

LOWE AHP

DW0950

USAACEAUTHORIZATION GRANTED TO INSTALL HUDTGT AMPLIFIER DISCONNECTS IAW MEOA6206 REV A. ACFT HRS: 6828.3

24-Feb-2011 1


melissa.gann


MEC F122582- AUTHORIZATION GRANTED TOINSTALL HUD THAT AMPLIFIER DISCONNECTSIAW MEO A62HRS C/W 6850.7 12MAR11 MECLOCATED NI REAR OF HISTORICAL RECORDS.

07-Mar-2011 1

LOWE AHP

JT0967

USAACEH-60-11-ASAM-06 CYCLIC STICK STOP BOLTSC/W AT 6850.7 ACFT HRS.

10-Mar-2011 1


jeanora.g.thompson


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 38 of 64

CSC, AFMA, RASM-EOGM/ACE PERFORMEEDE AT 6850.7 ACFTHRS. BY TEAM MEMBER R

11-Mar-2011 1

LOWE AHP

JT0967


360 HR SPECIAL INSP C/W @ 6850.7 ACFTHRS.

14-Mar-2011 1

LOWE AHP

JT0967


T/R RIG CK COMPLETED @ 6690.2 ACFT HRS.RED: 4.686/ 4.358/ .328 BLACK:3.935/3.605/.330 BLUE: 3.989/ 3.654/.335YELLOW: 4.685/ 4.350/.335

16-Mar-2011 1

LOWE AHP

JT0967


H-60-11-ASAM-09 C/W @ 6875.0 ACFT HRS.(IAFTS NOT INSTALLED)

29-Mar-2011 1

LOWE AHP

jeanora.g.thompson

USAACEDELAYED ENTRY: ACFT INDUCTED INTO ULLS-A(E) ON (18MAR11) AT 6858.1 ACFT HRS.

06-Apr-2011 1


dean.a.keirn

USAACEF107474 Left beaded panel cracked in 9 places,3 of the cracks progress under the "PDoubler",exceeding TM repair criteria.Requestauthorization to replace beaded panel withPlating kit, NSN 1680-01-513-6990 andassociated kits if available:Stringer Kit, NSN1680-01-551-7983, PN 70070-20167-027Windowkit, NSN 1680-01-551-8406, PN 70070-20527-013BL 34.5 kit, NSN 1680-01-551-8405, PN 70070-20572-013Request written guidence andprocedure for the replacement of the L/Hbeadedpanel. 1). Authorization is granted forFt. Rucker maintenance contractor toreplaceleft hand beaded panel with new beadedpanel kit, P/N 70070-20470-013 onaircraft8624564. 2). Replace the beaded panel per themod 50-5 kit in DMWR 1-1520-237 WP 0333,leftHand side only. The following kits shall beinstalled.Plating kit, NSN 1680-01-513-6990Stringer Kit, NSN 1680-01-551-7983Window kit, NSN 1680-01-551-8406.BL 34.5 kit,NSN 1680-01-551-8405 3). Airframe will be de-populated and internally shored per memo AED-U-11,except DO NOT jack to the dimensionsstated in AED-U-11. Jack only to asnugcondition (maximum 0.010 inch defelctionof cabin ceiling). 4). Any major deviation fromthe listed instructions, inconsistencies,ordamage caused during repair procedure, oradditional nonconformitiesdiscovered duringthis repair must be reported to AMRDEC LiasonEngineer andthe repairprocedure shall bediscontinued until each issue is resolved andfurtherdisposition is granted. John David BJenkins

15-Apr-2011 1


vickie.l.meadows

USAACEMAIN MOD FILTER BUTTON POPPED @ 6934.0ACFT HRS W/TSN: 5919. 1ST STAGE FILTERREPL AND BUTTON RESET. SERVICEABILITYCHECK C/W.

20-Apr-2011 1


jeanora.g.thompson


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 39 of 64

USAACEH-60-11-AMAM-11 - (AWR STATUS UPDATE)COMPLIED WITH @ 6942.2 ACFT HRS - NA TOA/C BY SERIAL NUMBER.

27-Apr-2011 1


jeanora.g.thompson

USAACEH-60-11-AMAM-09 (DA FORM 2408-19-3 ENGINERECORDS) C/W THIS DATE @ 6979.2 ACFTHRS.

17-May-2011 1


jeanora.g.thompson

USAACEM/R RIG CHECK COMPLETED @ 6979.2 ACFTHOURS. FWD: SHORTEN 1/2 FLAT; AFTLENGTHEN 1/2 FLAT; LAT: NO CHANGE.

25-May-2011 1


jeanora.g.thompson

USAACET/R RIG CK COMPLETED @ 6979.2 ACFT HRS.RED: 4.788/4.443/.45; BLACK: 4.008/3.671/.337;BLUE: 4.073/3.731/.342; YELLOW:4.710/4.371/.339.

27-May-2011 1


jeanora.g.thompson

USAACET/R CABLE TENSION CK COMPLETED @6979.2 ACFT HRS. L/H - 170, R/H - 170 @ NODEGREE NOTED... REPLY TO 743 STATESTHAT THE DEGREE IS 89.3°.

27-May-2011 2


jeanora.g.thompson

USAACEH-60-11-AMAM-13, EXTERNAL RESCUE HOISTFITTING N/A THIS AIRCRAFT - ACFT HRS. C/W7006.3

09-Jun-2011 1


jeanora.g.thompson

USAACEAWR 1529 R1: DTD 07 OCT 09 ACFTOPERATING IAW WITHIN LIMITATIONS &RESTRICTIONS (AHRU/AHRS) @ 7007.3 ACFTHRS.

15-Jun-2011 1


jeanora.g.thompson

USAACEACFT OPERATING IAW AWR 1514 (R-1) DTD03AUG10 (DGNS-P31) @ 7007.3 ACFT HRS.

15-Jun-2011 2


jeanora.g.thompson

USAACEIMPENDING BYPASS RILTER BUTTON POPPEDON SHUTDOWN W/TSN: 5996 ACFT HRS @7011.3. REPL FILTER AND RESET BUTTON.

27-Jun-2011 1


jeanora.g.thompson

USAACEAWR 1639 R3 - ACFT OPERATING UNDER AWR1639 R3 DTD 01JUN11 WHICH SUPERCEDESAWR 1639 R2 DTD 14JUN10.

01-Jul-2011 1


jeanora.g.thompson

USAACEH-60-11-ASAM-13, ENGINE AIR INLET ANTI-ICING VALVE VALVE C/W @ 7034.7 ACFT HRS.#1 FAIL, #2 FAIL.

09-Jul-2011 1


jeanora.g.thompson

USAACEH-60-11-SOF-01 (DISCREPANT SELF LOCKINGDOUBLE HEAGON NUTS) C/W @ 7034.7 ACFTHRS. ( AFS )

10-Jul-2011 1


jeanora.g.thompson


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 40 of 64

USAACEH-60-11-ASAM-14 (ENGINE COWLING REPAIRRESTRICTIONS) C/W @ 7034.7 ACFT HRS (AFS545 ). #1 PASS - #2 FAIL.

18-Jul-2011 1


jeanora.g.thompson

USAACEH-60-AMAM-14 - IMPROPER INTERNAL FUELTUBE SWAGING - NA THIS ACFT.

20-Jul-2011 1


jeanora.g.thompson

USAACEH-60-11-AMAM-08 - #1 AC PRIMARY WIRINGFEED NA THIS ACFT.

20-Jul-2011 2


jeanora.g.thompson

USAACEH-60-AMAM-07 - NO HAND HOLD LETTERING -NA THIS ACFT.

20-Jul-2011 3


jeanora.g.thompson

USAACEH-60-ASAM-10 - NO. 2 GPS ANTENNACONNECTOR - NA THIS ACFT.

20-Jul-2011 4


jeanora.g.thompson

USAACEH-60-ASAM-07 - TROOP SEAT LATCH ASSY -NA THIS ACFT.

20-Jul-2011 5


jeanora.g.thompson

USAACEH-60-11-AMAM-15 ( IVHMS ACCELEROMETERS)INSP COMP @ 7038.7 ACFT HRS. ACFT NOTIVHMS EQUIPPED (AFS594)

25-Jul-2011 1


jeanora.g.thompson

USAACEMEC F53651 - DELAYED ENTRY -AUTHORIZATION TO REPAIR: requesting toinstall temporary fabricated covers overexposed flight control tubes @ station 247-265until reciept of new panels and aircraft goesintoits next scheduled 720 hr inspection. Tammy SGriffin 08-SEP-06 (COPY OF MEC INHISTORICAL RECORDS)

11-Aug-2011 1


jeanora.g.thompson

USAACEMEC F57997 - DELAYED ENTRY -AUTHORIZATION TO REPAIR: VOID ON UPPERSIDE EXCEEDING THE REPAIR CRITERIA OFUH60 IETM OF 2". 16" X 12" EXTENDINGTHROUGH TO LOWER SIDE 19" X 12". TammyS Griffin 29-JAN-07 (COPY OF MEC INHISTORICAL RECORDS)

11-Aug-2011 2


jeanora.g.thompson

USAACEMEC F58066 - DELAYED ENTRY -AUTHORIZATION TO REPAIR: RIGHT BEADEDPANEL CRACKED.AUTHORITY TO REPLACEBEADED PANEL UTILIZING SHORING IN LIEUOFCRITERIA IN UH60 IETM. Tammy S Griffin 26-JAN-07 (COPY OF MEC IN HISTORICALRECORDS)

11-Aug-2011 3


jeanora.g.thompson


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 41 of 64

USAACEMEC F58072 - DELAYED ENTRY -AUTHORIZATION TO REPAIR: RED T/R BLADETIP CAP RIVET ATTACHMENT HOLES (RIB)ELONGATED AND ONE BROKEN REQUEST:AUTHORITY TO REPAIR IAW DMWR 1-1615-287,PARA 3-113.7, PAGES 3-56-3-60. Damon N Hay30-JAN-07 (COPY OF MEC IN HISTORICALRECORDS)

11-Aug-2011 4


jeanora.g.thompson

USAACEMEC F65448 - DELAYED ENTRY -AUTHORIZATION TO REPAIR:Droop stopbushing on red Spindle(A001-01596) and yellowspindle (A001-06003) have come unseated.Request authorization to deviate from WP 055600 and replace bushing without removing themr spindle or removing the mr blade. Tammy SGriffin 10-AUG-07 (COPY OF MEC INHISTORICAL RECORDS)

11-Aug-2011 5


jeanora.g.thompson

USAACEMEC F80460 - DELAYED ENTRY -AUTHORIZATION TO REPAIR: the #1 HIRSS itwas found to have play measured at .050".Tammy S Griffin 19-AUG-08 (COPY OF MEC INHISTORICAL RECORDS)

11-Aug-2011 6


jeanora.g.thompson

USAACEMEC F94459 - DELAYED ENTRY -AUTHORIZATION TO REPAIR: the left handfoward engine cowling fitting was found to havewear on the fitting where the slide lath restwhen the door is in closed position. Tammy SGriffin 25-JUN-09 (COPY OF MEC INHISTORICAL RECORDS)

11-Aug-2011 7


jeanora.g.thompson

USAACEMEC F94846 - DELAYED ENTRY -AUTHORIZATION TO REPAIR: The hydraulicpressure and return lines located in the tailcone near the tail landing gear strut has dents.Tammy S Griffin 07-JUL-09 (COPY OF MEC INHISTORICAL RECORDS)

11-Aug-2011 8


jeanora.g.thompson

USAACEMAIN MOD S/N: A265-00675 FILTER BUTTONPOPPED DURING GROUND RUN. TSN: 6079;ACFT HRS. 7094.2. SERVICEABILITY INSPCOMPLETED. NO PARTICLES FOUND,REPLACED 1ST STAGE FILTER & RESETBUTTON IAW 1-1520-237-23-7.

02-Sep-2011 1


jeanora.g.thompson

USAACEH-60-11-AMAM-20 - REQUIREMENTS OF H-60-11-AMAM-20 (AN/ASN-128D SOFTWAREUPGRADE) NLT 27 SEP 11 C/W @ 7126.9 ACFTHRS. (AFS545)

22-Sep-2011 1


jeanora.g.thompson

USAACECOMPLIED WITH H-60-11-AMAM-17 ( T/RINBOARD/OUTBOARD RETENTION PLATESHIMS) @ 7184.7 (INSP 648)

29-Sep-2011 1


vickie.l.meadows

USAACEH-60-12-SOF-01 - TAIL ROTOR INTERMEDIATEGEARBOX COMPLETED AT 7162.0 ACFT HRS.AS PER FORM 730

08-Oct-2011 1


olivia.d.williams

USAACEH-60-12-SOF-02 (TAIL ROTOR INTERMEDIATEGEARBOX) C/W AT 7162.0 ACFT HRS.

10-Oct-2011 1


debra.r.chancellor


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 42 of 64

USAACEH-60-12-SOF-03 (T/R I/G/B) C/W AT 7169.8 ACFTHRS. (AFS 472).

15-Oct-2011 1


bryan.w.hollis

USAACEAIRCRAFT OPERATING IAW AWR 1505, R4DATED 21OCT11 @ 7183.4 ACFT HRS.

22-Oct-2011 1


jeanora.g.thompson

USAACEACFT NO LONGER OPERATING IAW WITH AWR1505 R3. ACFT HRS. 7183.4

22-Oct-2011 2


jeanora.g.thompson

USAACEACFT OPERATING WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1529 R2DATED 7 OCT 2011. ((FOGS) -(SUPERCEDESAWR 1529 R1) AT 7183.7 ACFT HRS.

28-Oct-2011 1


jeanora.g.thompson

USAACEH-60-12-AMAM-03, TRANSPONDER ANDCOMMON MISSILE WARNING SYSTEM C/W @7183.7 AIRCRAFT HOURS. C/W, CMWS MWONOT INSTALLED.

31-Oct-2011 1


jeanora.g.thompson

USAACEMEC F107474 - ACFT OPERATING IAW MECF107474 - L/H BEADED PANEL CRACKED IN 9PLACES, 3 OF THE CRACKS PROGRESSUNDER THE "P DOUBLER" BEADED PANEL TOBE REPLACED UPON RECEIPT OF NEW KIT &ASSOCIATED MOD KITS. (#5 IN ENGINEERINGDISPOSITION NOT COMPLIED WITH.DOWNGRADE MEC WILL BE COMPLIED WITHDURING NEXT PHASE). 13-1 DTD 28OCT11, #1,STATUS X. TIPID: WM015630; MECH PID:WM01563.

01-Nov-2011 1


jeanora.g.thompson

USAACEOPERATE IAW AWR 1455 (R-2) DTD 31 OCT -SUPERCEDES AWR 1455 (R1)

01-Nov-2011 2


kathleen.m.jungell

USAACEH-60-12-ASAM-01 TAIL ROTOR OUTPUT BEVELGEAR NON-DESTRUCTIVE INSPECTION C/W @7184.7 ACFT HRS BY INSP 106

07-Nov-2011 1


vickie.l.meadows

USAACEACFT DATE OF MANUFACTURE IS JAN 1987 @7184.7 ACFT HRS @ PHASE # 12

08-Nov-2011 1


vickie.l.meadows

USAACEMEC F107474 A- ACFT OPERATING IAW MECF107474 - L/H BEADED PANEL CRACKED IN 9PLACES, 3 OF THE CRACKS PROGRESSUNDER THE "P DOUBLER" BEADED PANEL TOBE REPLACED UPON RECEIPT OF NEW KIT &ASSOCIATED MOD KITS. (#5 IN ENGINEERINGDISPOSITION NOT COMPLIED WITH.DOWNGRADE MEC WILL BE COMPLIED WITHDURING NEXT PHASE). 13-1 DTD 28OCT11, #1,STATUS X. TIPID: WM015630; MECH PID:WM01563.

09-Nov-2011 1


jeanora.g.thompson


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 43 of 64

USAACEMEC F107474A - ACFT OPERATING IAW MECF107474 - L/H BEADED PANEL CRACKED IN 9PLACES, 3 OF THE CRACKS PROGRESSUNDER THE "P DOUBLER" BEADED PANEL TOBE REPLACED UPON RECEIPT OF NEW KIT &ASSOCIATED MOD KITS.

09-Nov-2011 2


jeanora.g.thompson

USAACEIAW MEC F107474, STEP #5 IN ENGINEERINGDISPOSITION COMPLIED WITH. COMPLETED@ 7184.7 ACFT HRS. LC010652

17-Nov-2011 1


jessica.n.kennedy

USAACEDELAYED ENTRY: ACFT OPERATING WITHINLIMITATIONS AND RESTRICTIONS SPECIFIEDIN AWR 1153 R6 DATED 18 NOV 11 (JP-8+100FUEL).

18-Nov-2011 1


donna.k.moss

USAACEMAIN ROTOR RIG CHECK: PRIMARY SERVOCONTROL ROD IS BIASED AS FOLLOWS: FWDIS NO ADJUSTMENT, AFT IS NO ADJUSTMENTLAT IS NO ADJUSTMENT @ 7198.7 ACFT HRS.

01-Dec-2011 1


vickie.l.meadows

USAACEOPERATE IAW AWR 1455 (R-3) DTD 10 NOV 11 -SUPERCEDES AWR 1455 (R-2) DTD 31 OCT R-2

02-Dec-2011 1


kathleen.m.jungell

USAACET/R CABLE TENSION RECORDINGS: L/H: 135,R/H:135, @ 20° COMPLETED AT 7184.7 ACFTHRS.

02-Dec-2011 2


jessica.n.kennedy

USAACET/R BIAS READINGS: RED:4.856/5.179=.323,YELLOW:4.854/5.178=.324,BLACK:4.171/4.494=.323,BLUE:4.173/4.495=.322. COMPLETED AT 7184.7ACFT HRS.

02-Dec-2011 3


jessica.n.kennedy

USAACEH-60-12-ASAM-02 DRAG BEAMREPLACEMENT @ 7185.2 ACFT HRS.

06-Dec-2011 1


claudia.f.anderson

USAACECOMPLIED WITH H-60-12-ASAM-02 DRAGBEAM REPLACEMENT@ 7185.2 ACFT HRS.(INSPECTOR 27) RIGHT BAD OLD STYLE LEFTGOOD NEW STYLE

06-Dec-2011 2


vickie.l.meadows

USAACET/R BIAS READINGS: RED:5.062/4.753=.309,BLACK:4.358/4.054=.304,BLUE:4.364/4.062=.302,YELLOW:5.196/4.889=.307. COMPLETED AT7185.2 ACFT HRS.

05-Jan-2012 1


jessica.n.kennedy

USAACE720 HR PHASE INSPECTION # 12 ISCOMPLETED AT 7184.7 ACFT HRS. NEXT 720HR PHASE # 13 IS DUE @ 7904.7.

09-Jan-2012 1

QLOWE AHP, FT.RUCKER, AL.

vickie.l.meadows

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 1800 DTD 30NOV11 - ACFT OPERATINGUNDER AWR 1800 DTD 30NOV11. THIS AWRSUPERCEDES ACR 1639 R3 DTD 01JUN11.ACFT HRS. 7216.6.

19-Jan-2012 2


jeanora.g.thompson


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 44 of 64

USAACEINSP A670 A/C CABIN TUB WASH COMPLETED@ 7270.7 ACFT HRS.

21-Feb-2012 1


donna.k.moss

USAACEM/R RIG CHECK: PRIMARY SERVO CONTROLROD IS BIASED AS FOLLOWS: FWD: NOADJUSTMENT, AFT: NO ADJUSTMENT ANDLAT: NO ADJUSTMENT @ 7270.7 ACFT HRS.

25-Feb-2012 1


donna.k.moss

USAACET/R CABLE TENSION RECORDINGS: L/H 146,R/H 146 @ 21 ° COMPLETED @ 7270.7 ACFTHRS.

25-Feb-2012 2


donna.k.moss

USAACET/R BIAS READINGS: RED: 4.802/5.138=.336,BLACK: 4.063/4.394=.331, YELLOW:4.878/5.211=.333, BLUE: 4.110/4.444=.334COMPLETED @ 7270.7 ACFT HRS.

25-Feb-2012 3


donna.k.moss

USAACEACFT NO LONGER OPERATING IAW AWR 1251R3 (EYEBOLTS) @ 7270.7 ACFT HRS.DM026217

27-Feb-2012 1


donna.k.moss

USAACEACFT NOW OPERATING IAW AWR 1251 R4(EYEBOLTS) @ 7270.7 ACFT HRS. DM026217

27-Feb-2012 2


donna.k.moss

USAACET/R CABLE TENSION CHECK RECORDINGS:L/H 139, R/H 139 @ 20° @ 7270.7 ACFT HRS.

27-Feb-2012 3


donna.k.moss

USAACET/R BIAS READINGS: RED: 5.138-4.802=.336,BLACK: 4.394-4.063=.331, YELLOW: 5.211-4.878=.333, BLUE: 4.444-4.110=.334 @ 7270.7ACFT HRS.

27-Feb-2012 4


donna.k.moss

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

27-Feb-2012 5


dean.a.keirn

USAACEINSP A670 CABIN TUB INSPECTIONCOMPLETED ON 28 FEB 2012 @ 7270.7 ACFTHRS NEXT DUE 28 FEB 2016. DM026217

28-Feb-2012 1


donna.k.moss

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

28-Feb-2012 2


dean.a.keirn

USAACET/R CABLE TENSION CHECK C/W @ 7271.2ACFT HRS. L/H 117, R/H 118 @ 17° C.

06-Mar-2012 1


donna.k.moss

USAACET/R BIAS READINGS: BLACK: 4.300-3.968=.332,YELLOW: 5.019-4.724=.333, BLUE: 4.339-4.004=.335, RED: 5.057-4.724=.333 (MR#95678)COMPLIED WITH @ 7271.2 ACFT HRS.

06-Mar-2012 2


donna.k.moss

USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-06 (UPPER BULKHEAD FUEL SYSTEMBREAKAWAY VALVE AND FIREEXTINGUISHING SYSTEM DIRECTIONALVALVE) @ 7272.2 ACFT HRS.

10-Mar-2012 1


donna.k.moss


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 45 of 64

USAACE9/11 HOUR CABLE TENSION DUE AT 7280.7 +/-1 ACFT HOUR MEASUREMENTS WERE L/H:139LBS R/H: 139LBS @ 20 DEGREES CEL.COMPLETED L/H 145, R/H 145 @ 24° CEL (MR#87703 & MR# 118172) IAW WP1747.

13-Mar-2012 1


donna.k.moss

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

20-Mar-2012 1


dean.a.keirn

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

03-Apr-2012 1


dean.a.keirn

USAACERH ENG COWL LATCH TEMPORARILYREPAIRED IAW MEO A6241 REV A. MUST BEPERMANENT REPAIR NLT 90 DAYS (02JUL12)

03-Apr-2012 2


dean.a.keirn

USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-SOF-05 (CHANGE TO DEPOT REPAIREDLEGACY M/R BLADES) @ 7330.2 ACFT HRS(AFS 594). NOT APPLICABLE.

11-Apr-2012 1


donna.k.moss

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

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

USAACELOWER HALF OF L/H MLG WIRE STRIKE BENTAND DISTORTED INBOARD, (BREAKAWAY TIP).REMOVED FROM A/C 8223700 AND REPLACEDON A/C 8624564 @ 7496.0 ACFT HRS. ECODPERFORMED BY QC KEN PACE 020157.

12-Jun-2012 1


donna.k.moss

USAACEDELAYED ENTRY: ACFT BEING OPERATED IAWMEO A6055 REV C DUE TO M/R BLADE LEADDROOP STOP BUSHING DEBONDED.REPLACEMENT OF M/R BLADE DROOP STOPBUSHING REQUIRED AT NEXT 360 DUE AT7545.2 ACFT HRS.

20-Jun-2012 1


donna.k.moss

L-3 RASM-3OCM/ACE PERFORMED AT 7530.3 AIRCRAFTHOURS BY TEAM MEMBER P

29-Jun-2012 1


jacob.a.weikart

USAACEMEC F149079, AUTHORIZATION GRANTED TOEXTEND THE REPLACEMENT DATE OF THE RHENG COWL LATCH (AS INSTALLEDPREVIOUSLY BY MEO A6241 REV A) 90 DAYSFROM MEC APPROVAL DATE, NOW DUE07OCT12.

09-Jul-2012 1


dean.a.keirn

USAACECOMPLIED WITH H-60-12-AMAM-12 @ 7530.3ACFT HRS.

11-Jul-2012 1


donna.k.moss


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 46 of 64

USAACECOMPLIED WITH H-60-12-ASAM-08 CARGOHOOK MANUAL RELEASE SPRING @ 7537.2ACFT HRS. FAILED.

23-Jul-2012 1


donna.k.moss

USAACEMEC F150256, AUTHORIZATION GRANTED TOREPAIR THE TW YOKE WASHER DEBOND IAWMEO A6577. 7543.0 ACFT HRS.

26-Jul-2012 1


dean.a.keirn

USAACECOMPLIED WITH MEO A6055 REV C M/RBLADE LEAD DROOP STOP BUSHINGDEBONDED REPLACED BUSHINGS IAW TM1-1520-237-23 WP0565 (BLUE, BLACK ANDYELLOW LEAD BUSHINGS) @ 7543.0 ACFTHRS. (TI: RW015577, MECH: JM026097 &MA022051).

26-Jul-2012 2


donna.k.moss

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

USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-07 @ 7543.0 ACFT HRS. (ELECTRICALWIRING CHAFE)

08-Aug-2012 1


donna.k.moss

USAACET/R BIAS COMPLETED @ 7543.0 ACFT HRS:RED: 5.126/4.788=.338 BLUE: 4.365/4.030=.335,YELLOW: 5.189/4.851=.338, BLACK:4.368/4.028=.340

09-Aug-2012 1


brandi.n.keener

USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-09 (HYDRAULIC LINE CHAFE) @ 7543.0ACFT HRS.

10-Aug-2012 1


donna.k.moss

USAACECOMPLIED WITH H-60-11-ASAM-06(MANDATORY MAINTENANCE, UPPERBULKHEAD FUEL SYSTEM BREAKAWAYWALVE AND FIRE EXTINGUISHING SYSTEMDIRECTIONAL VALVE) @ 7543.0 ACFT HRS.

12-Aug-2012 1


donna.k.moss

USAACEMANUAL OPERATION COMPLETED MOC OKIAW H-60-12-ASAM-08 @ 7543.0 ACFT HRS. (TI:RM026470)

12-Aug-2012 2


donna.k.moss

USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-09 (BREEZE EASTERN EXTERNALRESCUE HOIST CARTRIDGE ACTUATEDDEVICE (CAD) ELECTRICAL CONNECTOR) @7567.9 ACFT HRS. N/A THIS ACFT. HOIST NOTINSTALLED.

22-Aug-2012 1


donna.k.moss


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 47 of 64

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

USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-10 @ 7610.0 ACFT HRS. PASSED.

08-Sep-2012 1


donna.k.moss

USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-11 (HMU) @ 7620.7 ACFT HRS. #2FAILED INSP.

12-Sep-2012 1


donna.k.moss

USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-15 @ 7643.0 ACFT HRS. INSPECTIONCOMPLETE. YAW TRIM ACTUATOR P/N 181950-5, S/N B333-02009. NOT APPLICABLE BYSERIAL NUMBER. ROLL TRIM ACTUATOR P/NCUO9609220, S/N D332-00534. NOTAPPLICABLE BY PART NUMBER.(AFS594)

17-Sep-2012 1


donna.k.moss

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

USAACEENGINE COWLING LATCH FRAME REPAIR IAWMEO A6241A REPLACED @ 7662.2 ACFT HRS.ACFT NO LONGER OPERATING IAW MEOA6241A.

29-Sep-2012 1


donna.k.moss

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

15-Oct-2012 1


dean.a.keirn

USAACEACFT OPERATING IAW MEO A6055 REV C DUEBLUE M/R DROOP STOP LEAD BUSHINGDISBONDED @ 7703.3 ACFT HRS.

17-Oct-2012 1


donna.k.moss

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

USAACEMAIN MODULE TRANSMISSION REPLACEDACFT NO LONGER OPERATING IAW MECF92186.

07-Nov-2012 1


donna.k.moss

USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-02 (AHRS), INSPECTION COMPLETE.AHRS PASSES @ 7734.3 ACFT HRS. (AFS594)

13-Nov-2012 1


donna.k.moss


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 48 of 64

USAACETAIL ROTOR BIAS NUMBERS ENTERED IN TOHISTORICAL RECORDS - RED: 5.057" - 4.732" =0.325". BLACK: 4.376" - 4.040" = 0.336".YELLOW: 5.103" - 4.788" = 0.315". BLUE:4.367" - 4.035" = 0.332". FINAL BLADE ANGLESFOR ALL BLADES - 3.0 DEGRESS @ 7734.3ACFT HRS.

21-Nov-2012 1


donna.k.moss

USAACEM/R RIG CHECK COMPLETED. FWD/AFT/LATNO ADJUSTMENTS MADE. (JB020649)

21-Nov-2012 2


donna.k.moss

USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-01 (FLIGHT CONTROL RIGGINGPROCEDURES) @ 7734.3 ACFT HRS.

25-Nov-2012 1


donna.k.moss

USAACEMEC F157313, AUTHORIZATION GRANTED TOTEST #1 MAIN FUEL CHECK VALVE BYINCREASING THE PRESSURE IN STEP 28, WP1013, UP TO BUT NOT EXCEEDING 60 PSI.

28-Nov-2012 1


dean.a.keirn

USAACECOMPLIED WITH REQUIREMENT H-60-13-AMAM-03 (DIGITAL ENGINE CONTROLUNIT/ELECTRONICE DIGITAL ENGINECONTROL UNIT TURBINE GAS TEMPERATUREBIAS) @ 7734.3 ACFT HRS (AFS 594).

04-Dec-2012 1


donna.k.moss

USAACECOMPLIED WITH REQUIREMENT H-60-13-ASAM-01 (ANTI-COLLISION LIGHTS POWERSUPPLY) @ 7734.3 ACFT HRS (WS01135).

05-Dec-2012 1


donna.k.moss

USAACEACFT NO LONGER OPERATING IAW MEOA6055 REV C BLUE M/R DROOP STOPBUSHING REPLACED AT 7734.3 ACFT HRS.

06-Dec-2012 1


donna.k.moss

USAACEACFT BEING OPERATED IAW MEO A6055 FORM/R DROOP STOP BUSHING DISBONDED.REPLACEMENT DUE AT NEXT PMI @ 7904.7ACFT HRS.

15-Dec-2012 1


donna.k.moss

USAACE9-11 CABLE TENSION CHECK COMPLETED ,PASSED I/A/W TM1-1520-237-23 WP #1747 00 ,L/H=160 LBS. , R/H= 160 LBS. @ 19.5 DEGRESS" C " @ 7743.5 ACFT HRS.

18-Dec-2012 1


donna.k.moss

USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-04 (LCF CHANGE 63) @ 7753.4 ACFTHRS. (AFS 594)

10-Jan-2013 1


donna.k.moss

USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-05 (MLG BRAKES) @ 7755.6 ACFT HRS.BOTH ASSY'S PASS (AFS 594).

23-Jan-2013 1


donna.k.moss

USAACEDELAYED ENTRY - APPRPX. 1/2" DIAMETERHOLE RUBBED IN OUTER STIFFENER ANDCLIP (-159) NOT INSTALLED. AUTHORIZATIONGRANTED TO REPAIR AS OUTLINES IN MECF136600 DTD 17 NOV 11.

24-Jan-2013 1


olivia.d.williams

USAACEINITIATED CMWS/ATIRCM COMPONENTTRACKING IAW GEN-13-AMAM-02" COMPLIEDWITH @ 7780.2 ACFT HRS. NOT APPLICABLETO THIS ACFT.

31-Jan-2013 1


donna.k.moss


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 49 of 64

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

USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-06 (CEFS) @ 7796.6 ACFT HRS. NOTAPPLICABLE THIS ACFT.

12-Feb-2013 1


donna.k.moss

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

USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-03 (MR SPINDLE ANTI-FLAPASSEMBLIES) @ 7,846.2 ACFT HRS. ALL 4 M/RANTI-FLAP ASSEMBLIES PASS. (AFS 594)

01-Mar-2013 2


donna.k.moss


20-Mar-2013 1


vickie.l.meadows

USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-04 (PLASTIC MEDIA BLAST AND OXIDEFLAKE RESIDUE) @ 7887.1 ACFT HRS.

26-Mar-2013 1


donna.k.moss

USAACEMEC F65448 - DELAYED ENTRY -AUTHORIZATION TO REPAIR: DROOP STOPBUSHING ON RED SPINDLE (A001-01596) WASFOUND REMOVED THIS DATE. YELLOWSPINDLE SN: A001-06003 IS STILL INSTALLEDAS OF THIS DATE. ACFT STILL OPERATINGIAW MEC F65448.

27-Mar-2013 1


donna.k.moss

USAACEACFT NO LONGER OPERATING IAW MECF58072 T/R BLADES REPLACED 18 NOV 2011AND 31 JUL 2012 PER -16.

27-Mar-2013 2


donna.k.moss

USAACEACFT NO LONGER OPERATING IAW MECF110769 MAIN MODULE TRANSMISSIONREPLACED 07 NOV 2012.

27-Mar-2013 3


donna.k.moss

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


29-Mar-2013 2


vickie.l.meadows

USAACECOMPLIED WITH REQUIREMENTS OF H-64-13-AMAM-07 (LOAD DEMAND SPINDLE CABLECLEARANCE) AT 7889.9 ACFT HRS - PASSED.

03-Apr-2013 1


melissa.gann

USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-05 (ELECTRIC RESCUE HOIST) AT7889.9 ACFT HRS - NOT INSTALLED ON A/C.

08-Apr-2013 1


melissa.gann


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 50 of 64

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

USAACEDELAYED ENTRY: MEC F53651 IS NO LONGERAPPLICABLE. THE DEVIATION NO LONGEREXISTS. INSPECTION OF ACFT REVEALED THETEMPORARY FABRICATED PANEL IS NOLONGER INSTALLED, PROPERSOUNDPROOFING IS INSTALLED.

23-Apr-2013 1


dean.a.keirn

USAACECOMPLIED WITH H-60-13-ASAM-06 (PMICHECKLIST CHANGES) @ 7896.5 ACFT HRS.PASSED

08-May-2013 1


vickie.l.meadows

USAACEH-60-11-ASAM-06- PILOT'S CYCLIC STICKWIRE HARNESS-COMPLETED AT 7896.5 ACFTHRS.

15-May-2013 1


christina.l.negron

L-3 RASM-EOCM/ACE PERFORMED AT 7896.5 AIRCRAFTHOURS BY TEAM MEMBER P

16-May-2013 1


jacob.a.weikart

USAACEMEC F166771, AUTHORIZATION GRANTED TOREPAIR TRANSITION COWLING VOIDS. 7896.5ACFT HRS.

22-May-2013 1


dean.a.keirn

USAACEACFT NO LONGER OPERATING IAW MEOA6055 REV C; M/R DROOP STOP BUSHINGSREPLACED DURING PHASE AT 7896.5 ACFTHRS.

23-May-2013 1


melissa.gann

USAACEDAGR SERIAL NUBMER VERIFICATION C/W(S/N 219337) @ 7896.5 ACFT HRS.

29-May-2013 1


vickie.l.meadows

USAACECOMPLIED WITH THE REQUIRMENTS OF H-60-13-SOF-01 @ 7896.5 ACFT HRS.

06-Jun-2013 1


vickie.l.meadows

USAACEMAIN ROTOR RIGGING COMPLETED AT 7896.5ACFT HRS. FWD: 5 FLATS OUT, AFT: 5FLATS IN, LAT: 2 FLATS OUT.

07-Jun-2013 1


christina.l.negron

USAACET/R BIAS CHECK COMPLETED AT 7896.5 ACFTHRS. COLOR DIM A DIM BDIFFERENCE BLADE SET DEGBLADE FINAL SET DEGRED 4.7045.025 0.321 0.93.0BLACK 4.82 4.375 0.2930.1 3.0YELLOW4.639 5.004 0.3651.5 3.0BLUE4.061 4.375 0.3140.1 2.9

10-Jun-2013 1


christina.l.negron

USAACE720 HOUR PHASE # 13, COMPLETED AT 7896.5ACFT HRS. NEXT 720 HOUR PHASE (#14) ISDUE AT 8616.5 ACFT HRS.

12-Jun-2013 1


christina.l.negron


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 51 of 64

USAACEDATE OF MANUFACTURE TAKEN FROM THESERIAL NUMBER CHECK - JAN 87

12-Jun-2013 2


olivia.d.williams

USAACET/R CABLE TENSION CHECK COMPLETED AT7896.5 ACFT HRS. LEFT: 146 LBS, RIGHT: 145LBS, TEMP: 27 DEGREES C.

17-Jun-2013 1


christina.l.negron

USAACEMEC F168128, AUTHORIZATION GRANTED TOREPAIR VOID IN TRANSITION COWLING. 7899.1ACFT HRS.

24-Jun-2013 1


dean.a.keirn

USAACEAWR 1529: ACFT NO LONGER OPERATING IAWAWR 1529, ALL REVISIONS.L ACFTRECONFIGURED FROM DUAL AHRS TOSINGLE AHRS. SEE AWR 1444.

25-Jun-2013 1


melissa.gann

USAACEAWR 1444: ACFT OPERATING IAW AWR 1444,R5 DTD 21 JUN 13, SINGLE AHRS.

25-Jun-2013 2


melissa.gann

USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-11, MAIN TRANSMISSION FILTER BOWLHARDWARE REPLACEMENT, AT 7906.1 ACFTHRS.

03-Jul-2013 1


melissa.gann

USAACET/R CABLE TENSION CHECK COMPLETED AT7906.1 ACFT HRS. LEFT: 140 LBS, RIGHT: 140LBS AT 25.1° C.

03-Jul-2013 2


melissa.gann

USAACEAWR 1444: ACFT OPERATING IAW AWR 1444,R6 DTD 11JUL13, SINGLE AHRS,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR.

16-Jul-2013 1


dean.a.keirn

USAACECOMPLIED WITH REQUIREMENTS OF GEN-13-AMAM-04, AN/APN-209 RADAR ALTIMETERSET COMPNENT TRACKING, AT 7964.7 ACFTHRS.

29-Jul-2013 1


melissa.gann

USAACEACFT OPERATING UNDER MEO A5826B -REOCCURRING 40 HR INSP FOR HIRSS NO2.

05-Aug-2013 1


rhonda.e.jackson

USAACEH-60-13-ASAM-10 (WOODWARD HYDRO-MECHANICAL UNIT P3 TUBE) C/W AT 8019.1ACFT HRS. BOTH PASSED.

23-Aug-2013 1


rhonda.e.jackson

USAACET/R RIG CK COMPLETED AT 8019.1 ACFT HRS-BLADE READINGS ARE AS FOLLOWS: RED:2.9 YELLOW: 2.8 BLUE: 2.9 BLACK 2.9

28-Aug-2013 1


rhonda.e.jackson

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

29-Aug-2013 1


dean.a.keirn

USAACEH-60-13-AMAM-10 (ULLS-AE LCF CHANGE 64)C/W AT 8037.8 ACFT HRS.

07-Sep-2013 1


rhonda.e.jackson

USAACEMAIN ROTOR RIG C/W - NO ADJ MADE. 11-Sep-2013 1


rhonda.e.jackson


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 52 of 64

USAACEMAIN XSMN FILTER BUTTON FOUNDEXTENDED IN POST FLIGHT INSP. RESETFILTER BUTTON, REPLACED 1ST STAGEFILTER, DID SERVICEABILILTY CK

13-Sep-2013 1


rhonda.e.jackson

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

USAACECOMPLY WITH REQUIREMENTS OF H-60-14-SOF-01(BREEZE EASTERN EXTERNALRESCUE HOIST INSTALLATION) @8140.4 ACFTHRS. NA TO THIS ACFT.

02-Nov-2013 1


felicia.tolver

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

25-Nov-2013 1


dean.a.keirn

USACCECOMPLY WITH REQUIREMENTS OF H-60-14-ASAM-02 BY 08 DEC 13 (HUMS) ACFT HRS8193, NOT INSTALLED ON THIS ACFT.

26-Nov-2013 1


felicia.tolver

USAACECOMPLIED WITH H-60-12-ASAM-02REPLACED R/H DRAG BEAM ASSEMBLY, 70250-12057-048 IAW 1-1520-237-23 WP 446 00 @8186.8 ACFT HRS.

02-Dec-2013 1


vickie.l.meadows

USAACEH-60-14-ASAM-02 (HUMS) C/W AT 8193.4 ACFTHRS. N/A TO THIS ACFT

07-Dec-2013 1


rhonda.e.jackson

USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-15 (CRASHWORTHY EXTERNAL FUELSYSTEM (CEFS) RIGHT HAND FUEL CELLCOVER PLATE) CEFS NOT INSTALLED. H-60-13-AMAM-15 IS NOT APPLICABLE.(AFS 765) @8209.8 ACFT HRS.

13-Dec-2013 1


vickie.l.meadows

USAACEComplIED with requirements of H-60-14-AMAM-03 (DISCREPANT CONNECTING LINKS)RECORDS CHECK COMPLETE. H-60-14-AMAM-03 IS NOT APPLICABLE IAW PARA 7.1 (AFS765) @ 8212.8 ACFT HRS.

02-Jan-2014 1


vickie.l.meadows

USAACECOMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-03 (ENGINE INLET BARRIER FILTERBRACKET REMOVAL)INSP. COMPLETED IAW H-60-14-ASAM-03, BARRIER BRACKET NOTINSTALLED @ 8212.8 ACFT HRS.

03-Jan-2014 1


vickie.l.meadows

USAACEREQUIREMENTS OF H-60-14-SOF-02 T/R PITCHSHAFT BUSHING ASSY COMPLETED AT 8243.9ACFT HRS

26-Jan-2014 1


olivia.d.williams

USAACET/R BLADE BIAS CHECK COMPLETED AT8257.7 ACFT HRS. RED - 3.1 MR# 120212AND 126579YELLOW - 2.9 MR# 120212 AND126579BLACK - 2.8 MR# 120212 AND126579BLUE - 3.0 MR# 120212 AND 126579

12-Feb-2014 1


felicia.tolver

USAACET/R BLADE BIAS - RED - 3.1 MR90452T/RBLADE BIAS- YELLOW - 3.0 MR90452T/RBLADE BIAS- BLACK - 3.0 MR90452T/RBLADE BIAS BLUE - 3.0 MR90452

21-Feb-2014 1


felicia.tolver


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 53 of 64

USAACET/R BLADE BIAS - RED - 3.1/3.1 T/R BLADEBIAS- YELLOW - 2.8/2.9 T/R BLADE BIAS-BLACK - 3.0/3.1 T/R BLADE BIAS BLUE - 2.9/3.0

25-Feb-2014 1


felicia.tolver

USAACECOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-08 AIRCRAFT NOT OPERATED IAWAWR 1437. H-60-14-AMAM-08 IS NOTAPPLICABLE. (AFS 765) @ 8282.5

06-Mar-2014 1


vickie.l.meadows

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

27-Mar-2014 1


dean.a.keirn

USAACEH-60-14-AMAM-05 LEGITIMATE CODE FILECHANGE 65 REQUIREMENTS COMPLETED AT8341.8 ACFT HRS.

05-Apr-2014 1


janice.m.bruce

USAACEH-60-14-AMAM-10 HONTEK COATED MAINROTOR BLADE REMOVAL COMPLETED AT8358.9 ACFT HRS. N/A TO THIS ACFT.

12-Apr-2014 1


vickie.l.meadows

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

16-Apr-2014 1


dean.a.keirn

USAACEH-60-14-ASAM-06 CW @ 8381.5 ACFT HR 28-Apr-2014 1


mark.a.trehern

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

LOCKHEAD,MARTIN,FTCKY

ACE INSP COMPLETED AT 8381.5 ACFT HRSAT FT.RUCKER,AL. BY TEAM MEMBERS R&U.

14-May-2014 1


BS809374

USAACECOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-14 ( IVHMS CABLING) MWO NOTAPPLIED INSPECTION COMPLETED AT 8381.5ACFT HRS

28-May-2014 1


theresa.d.pollard

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

USAACEBFT DAGGER DISMOUNTED FOR SNINVENTORY. REMOUNTED BFT DAGGER IAWBFT FBCB2-BFT AVN @ 8412.4 ACFT HRS.

14-Jun-2014 1


vickie.l.meadows


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 54 of 64

USAACECOMPLIED WITH REQUIREMENTS OF H-60-14-SOF-03 (DISCREPANT HEXAGON NUTS)@8445.7 ACFT HRS

23-Jun-2014 1


VM4663

USAACECOMPLY WITH REQUIREMENTS OF H-60-14-AMAM-16 (ATTITUDE HEADING REFERENCEUNIT 2410 TRACKING) SINGLE AHRU'SINSTALLED. GYRO S/N 1277 ADDED TO THE2408-16 IAW H-60-14-AMAM-16. (AFS 765) @8482.2 ACFT HRS

22-Jul-2014 1


vickie.l.meadows

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

USAACECOMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-09 ENGINE OUTPUT SHAFT @ 8500.7ACFT HRS.

31-Jul-2014 2


vickie.l.meadows

USAACEMEC F188672, Authorization granted for theCCAD Depot Field Team to replace righthandbeaded panel with new beaded panel kit,P/N 70070-20470-012. Replace the beaded panelper the mod 50-5 kit in DMWR 1-1520-237 WP0333, Right Hand side only. The following kitsshall be installed: 1.a.)Plating kit, NSN 1680-01-513-6988 1.b.)Stringer Kit, NSN 1680-01-551-8404 1.c.)Window kit, NSN 1680-01-551-84061.d.)BL 34.5 Modification Kit(50-7), NSN1680-01-551-8403. 8515.6 ACFT HRS.

27-Aug-2014 1


dean.a.keirn

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-14-SOF-04 (OPERATORS ANDCREWMEMBERS CHECKLIST) AT 8534.5 ACFTHRS

29-Aug-2014 1


theresa.d.pollard

USAACECOMPLY WITH THE REQUIREMENTS OF H-60-14-ASAM-10 ( MAIN TRANSMISSIONPLANATARY CARRIER ASSY) @ 8547.2 ACFTHRS

11-Sep-2014 1


theresa.d.pollard

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

27-Oct-2014 1


dean.a.keirn

USAACECOMPLIED WITH H-60-15-SOF-01 (OIL COOLERFAN AXIAL BEARING) ON 28 OCT 14 AT 8611.0ACFT. HRS.

28-Oct-2014 1


brian.k.dow

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

03-Nov-2014 1


dean.a.keirn

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

03-Nov-2014 2


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 55 of 64

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

07-Nov-2014 1


dean.a.keirn

USAACECOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-19 (ULLS-A(E) LCF CHANGE 66) ON 08NOV 14 AT 8611.0 ACFT. HRS.

08-Nov-2014 1


brian.k.dow

USAACECOMPLIED WITH REQUIREMENTS OF H-60-15-ASAM-01, LED CAUTION ADVISORY PANEL ON19 NOV 14 AT 8611.0 ACFT. HRS.

19-Nov-2014 1


brian.k.dow

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

26-Nov-2014 1


brian.k.dow

USAACEH-60-15-AMAM-05, AHRS EMERGENCYPROCEDURES, COMPLIED WITH AT 8613.4ACFT HRS.

16-Dec-2014 1


christina.l.negron

USAACEMEC F194615, AUTHORIZATION GRANTED TOREPAIR THE TEE SECTION FLOOR SUPPORTAT LH STA 308 ASOUTLINED IN ATTACHEDPROCESS CONTROL 5732. 8613.4 ACFT HRS.

14-Jan-2015 1


dean.a.keirn

USAACEMEC F195096, AUTHORIZATION GRANTED FORCCAD DFT TO REPAIR STA 308 FWD LH INBDTAB CRACK IAW MEO A6089B. 8613.4 ACFTHRS.

30-Jan-2015 1


dean.a.keirn

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

04-Feb-2015 1


dean.a.keirn

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

11-Feb-2015 1


dean.a.keirn

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

19-Feb-2015 1


dean.a.keirn

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

04-Mar-2015 1


dean.a.keirn

USAACEH-60-15-AMAM-06- IDENTIFICATION OFSURVIVABILITY EQUIPMENT, COMPLIED WITHAT 8613.4 ACFT HRS.

24-Mar-2015 1


christina.l.negron

USAACEMEC F194615A, ORIGINAL ENGINEERINGDISPOSITION SHOULD STATE THE REPAIR ISFOR THE RH TEE CAP ANGLE AND NOT THELH TEE CAP ANGLE. 8613.4 ACFT HRS.

02-Apr-2015 1


dean.a.keirn

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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 56 of 64

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

13-May-2015 1


dean.a.keirn

DCR RASM-COCM/ACE PEFORMED AT 8613.4 AIRCRAFTHOURS BY TEAM MEMBERS P AND UU

22-May-2015 1


jacob.a.weikart

USAACEMEC F200541, AUTHORIZATION GRANTED TOREMOVE THE FOUR HI-LOCS NEEDED TO AIDIN SECURING THE DRILLBLOCK.AUTHORIZATION GRANTED FOR AMSSMACHINIST TO CLEAN UP TWO (QTY: 2)HOLES IN THE LOWER STA 308 FRAME.NOTES: 1. REMOVE MINIMAL MATERIAL TOCLEAN UP BORES. 2. MAINTAIN CURRENTEDGDE DISTANCE AS MUCH AS POSSIBLE. 3.ONCE HOLES ARE CLEANED UP, REPORTFINAL DIMINISIONS TO THE UNDER SIGNEDAND AN ADDENDUM WILL BE PROVIDED FORFINAL REPAIR.

27-May-2015 1


dean.a.keirn

USAACEH-60-15-AMAM-10- AV- DEC GASKETINSPECTION, COMPLIED WITH AT 8613.4 ACFTHRS. GASKET IS NOT INSTALLED.

27-May-2015 2


christina.l.negron

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

28-May-2015 1


dean.a.keirn

USAACEMEC F200541A, AFTER HOLE CLEAN UP,DIMENSIONS ARE AS FOLLOWS: THEFORWARD HOLE DIAMETER IS .3915" WITH ANEDGE DISTANCE OF .182" THE AFT HOLEDIAMETER IS .3915" WITH AN EDGE DISTANCEOF .182" AUTHORIZATION GRANTED TOFABRICATE AND INSTALL FREEZE PLUG(S).

01-Jun-2015 1


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 57 of 64

USAACEMEC F194615B, 8613.4 ACFT HRS, DURING THEREPAIR, IT WAS NOTED THAT DUE TO THETHICKNESS OF THE INBOARD NESTEDANGLE, THE TWO FASTENERS THAT PASSTHROUGH STA 308 COULD NOT BE INSTALLEDDUE TO CLEARANCE ISSUES.AUTHORIZATION GRANTED TO: 1. THEREMOVAL OF DAMAGED AREA OF EXTRUSIONWILL BE LONG ENOUGH TO CROSS STA308BEAM AND EXTEND AS NEEDED FOR THEINSTALLATION OF THREE (3) FASTENERS ONEACH SIDE OF STA 308.2. TWO (2) REPAIRANGLES TO BE FABRICATED TO FIT THEEXTRUSION SHAPE OF THE INBOARD SIDE,FROM 7075-0 MATERIAL .063" THICK ANDTHEN HEATED TREATED TO 7075-T6CONDITION. 3. LENGTH OF REPAIR ANGLESSHOULD BE AS NEEDED TO COMPLY WITHREFERENCE 1 (WP 0377) FOR EIGHT (8)FASTENERS ON EACH SIDE BEYOND CUT. 4.TWO REPAIR ANGLES SHOULD BEFABRICATED FROM 7075-0 MATERIAL .063"THICK AND THEN HEAT TREATED TO 7075-T6CONDITIONTO FIT THE EXTRUSION SHAPE OFTHE OUTBOARD SIDE. PART LENGTH SHOULDBE AS NEEDED TO ALLOW FOR EIGHT (8)FASTENERS ON EACH SIDE BEYOND CUT.(REF PROCESS CONTROL 5732 SHT 3 OF 5STEP 3C). NOTE: TWO (2) INBD REPAIRANGLES ARE TO BE INSTALLED ONE (1) ONFWD SIDE OF STATION 308 BEAM AND ONE (1)ON THE AFT SIDE OF THE STATION 308 BEAM.EXISTING TWO (2) LOCATION IN STATION 308BEAM ARE NOT TO BE PICKED UP IN INBD OROUTBD REPAIR ANGLES.5. TWO (2) RADIUSBLOCKS ARE TO BE FABRICATED FROM .125"THICK 7075-T6 MATERIAL. THE LENGTH ANDWIDTH OF RADIUS BLOCK TO BE ABLE TOPICK UP EXISTING FASTENER LOCATION INTHE STA 308 BEAM AND MAINTAIN MINIMUM1.5 ED.FOLLOW PROCESS CONTROL 5732,STEPS 3G ON SHT 3 OF 5 FOR FINISH.INSTALL ONE (1) RADIUS BLOCK ON THE FWDOUTBD SIDE OF STA 308 BEAM AND ONE (1)RADIUS BLOCK ON THE AFT OUTBD SIDE OFSTA 308 BEAM WHERE MEC F200541 AINSTALLED FREEZE PLUGS IN THE STA 308BEAM. INSTALL RADIUS BLOCKS PERPROCESS CONTROL 5732, STEPS 3 G THRU 3ION SHT 3 OF 5.

08-Jun-2015 1


dean.a.keirn

USAACEMEC F201273, AUTHORIZATION GRANTED FORAMSS MACHINIST TO CLEAN UP ONE (1)FIGURE 8 HOLE IN THE INBOARD FLANGE OFSTATION 315 BL 16.5.

12-Jun-2015 1


dean.a.keirn

USAACEMEC F201273A, STA 315 FLANGE, HOLE FINALDIAMETER (.3445"); FINAL E.D.( .145").AUTHORIZATION GRANTED TO FABRICATEAND INSTALL FREEZE PLUG(S) AS DIRECTEDIN MEC.

17-Jun-2015 1


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 58 of 64

USAACEMEC F194615C, 8613.4 ACFT HRS, ADDENDUMB DISPOSITION STATES TO HAVE EIGHT (8)FASTENERS ON EACH SIDE BEYONDCUT. THISSHOULD BE EIGHT (8) FASTENERS TOTAL ATEACH CUT AS FOLLOWS: FWD OF STA 308:FIVE (5) FASTENERS FWD OF CUT AND THREE(3) FASTENERS AFT OF CUT. AFT STA 308:THREE (3) FASTENERS FWD OF CUT AND FIVE(5) FASTENERS AFT OF CUT.

18-Jun-2015 1


dean.a.keirn

USAACEH-60-15-AMAM-11- MODE S TRANSPONDERADDRESS REVIEW, COMPLIED WITH AT 8613.4ACFT HRS. NOT INSTALLED.

18-Jun-2015 2


christina.l.negron

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

23-Jun-2015 1


dean.a.keirn

USAACEH-60-15-ASAM-03- TROOP/GUNNER SEATENERGY ATTENUATORS. COMPLIED WITH AT8613.4 ACFT HRS. PASSED.

27-Jun-2015 1


christina.l.negron

USAACE720 HOUR PHASE #14, WAS COMPLETED AT8613.4 ACFT HRS. THE NEXT 720 HOURPHASE (#15) IS DUE AT 9333.4 ACFT HRS.

30-Jun-2015 1


christina.l.negron

USAACEMAIN ROTOR RIGGING CHECK COMPLETEDAT 8613.4 ACFT HRS.CONTROL POSITION:LOWCOLL ANGLE90 DEG R 180 DEG FWD 270DEG L 0 DEG AFT TOTAL DEG AVGDEG COLL. RANGE 7.6 -1.4-9.7 0.2 -3.3 -0.825HIGH COLL ANGLE:90 DEG R 180 DEGFWD 270 DEG L 0 DEG AFT TOTALDEG AVG DEG COLL. RANGE 18.711.7 11.4 18.6 60.415.1 15.925FWD CYCLIC ANGLE:90 DEGR 180 DEG FWD 270 DEG L 0 DEG AFTTOTAL DEG AVG DEG COLL. RANGE -2.7 31.834.5AFT CYCLE ANGLE:90 DEG R 180 DEGFWD 270 DEG L 0 DEG AFT TOTALDEG AVG DEG COLL. RANGE 25.35.1 20.2LEFT CYCLEANGLE:90 DEG R 180 DEG FWD 270 DEGL 0 DEG AFT TOTAL DEG AVG DEGCOLL. RANGE -9.16.5 15.6RIGHT CYCLIC ANGLE:90DEG R 180 DEG FWD 270 DEG L 0 DEGAFT TOTAL DEG AVG DEG COLL.RANGE 6.5-7.9 14.4

01-Jul-2015 1


christina.l.negron

USAACEMAIN ROTOR RIGGING CHECK COMPLIEDWITH, AT 8613.4 ACFT HRS. PRIMARY SERVOCONTROL ROD BIAS: FWD; NO ADJUSTMENT,AFT: NO ADJUSTMENT, LAT: 2 FLATS IN.

01-Jul-2015 2


christina.l.negron


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 59 of 64

USAACETAIL ROTOR BIAS CHECK COMPLETED AT8613.4 ACFT HRS. COLOR DIM ADIM B DIFFERENCE SET DEG2ND DEG FINAL DEGREERED4.70 5.02 0.32 0.03.0 3.0BLACK 4.084.41 0.33 0.0 3.03.0YELLOW 4.67 4.990.32 0.0 3.03.0 BLUE 4.04 4.350.31 0 .0 3.03.0

02-Jul-2015 1


christina.l.negron

USAACETAIL ROTOR CABLE TENSION CHECKCOMPLETED AT 8613.4 ACFT HRS,COMPLETED IAW H-60-15-AMAM-03 . LEFTCABLE165 LBS RIGHT CABLE 165 LBS @ 28.5DEGREES CELCIUS THERMOMETER MR#118177 TENSIONMETER MR# 126115(CHECKED AT 5/32)

02-Jul-2015 2


christina.l.negron

USAACEMEC F300395, 8613.4 ACFT HRS,AUTHORIZATION GRANTED TO REPAIR THEPILOT'S RIGHT RAIL GUIDE FWD ISOLATORMOUNT IAW ENGINEERING INSTRUCTIONS INMEC.

22-Jul-2015 1


dean.a.keirn

USAACEMEC F300394, 8613.4 ACFT HRS,AUTHORIZATION GRANTED TO REPAIR CPLEFT RAIL GUIDE FWD ISOLATOR MOUNT IAWENGINEERING INSTRUCTIONS IN MEC.

22-Jul-2015 2


dean.a.keirn

USAACEMEC F300703, 8613.4 ACFT HRS,AUTHORIZATION GRANTED TO REPAIR CO-PILOTS SEAT RIGHT RAIL GUIDE FWDISOLATOR MOUNT IAW ENGINEERINSTRUCTIONS IN MEC.

24-Jul-2015 1


dean.a.keirn

USAACEH-60-15-AMAM-14 LEGITIMATE CODE FILE(LCF) CHANGE 67 REQUIREMENTS C/W AT8613.4

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

USAACEMEC F300697, 8613.4 ACFT HRS,AUTHORIZATION GRANTED TO REPAIRPILOTS SEAT LEFT RAIL GUIDE FWDISOLATOR MOUNT IAW ENGINEERINSTRUCTIONS IN MEC.

30-Jul-2015 1


dean.a.keirn

USAACETAIL ROTOR CABLE TENSION CHECKEDFAILED AND WAS ADJUSTED TO L/H 140 LBS.R/H 140 @ 28.5*C AT 8623.8 ACFT HRS.

06-Aug-2015 1


marilyn.l.jones

USAACETAIL ROTOR CABLE TENSION CHECKCOMPLETED AT 8633.8 ACFT HRS. STABILIZEDAT L/H:135*R/H: 135 AT 25.1 * C.

12-Aug-2015 1


marilyn.l.jones

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-15-AMAM-18 (MEDEVAC CAROUSEL) AT8745.1 ACFT HRS. N/A TO THIS ACFT -CAROUSEL NOT INSTALLED.

08-Oct-2015 1


marilyn.l.jones


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 60 of 64

USAACEAIRCRAFT NO LONGER OPERATING IAW AWR1965 (APPLE I-PAD DEVICES) SUPERCEDEDBY AWR 1965 R1 AT 8760.8 ACFT HRS.

14-Oct-2015 1


marilyn.l.jones

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-16-AMAM-01 (EIBF FRAMES) AT 8796.2 ACFTHRS.

27-Oct-2015 1


marilyn.l.jones

USAACEACFT OPERATING IAW AWR 1693, R2 DTD06JAN14, RESA.

30-Oct-2015 1


dean.a.keirn

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-16-ASAM-01 (INBOARD RETENTION PLATETORQUE CHECKS) AT 8817.1 ACFT HRS.

10-Nov-2015 1


marilyn.l.jones

USAACETAIL ROTOR CABLE TENSION CHECKCOMPLETED AT 8817.1 ACFT HRS. L/H-168, R/H- 166 AT 22*C.

19-Nov-2015 1


marilyn.l.jones

USAACETAIL ROTOR BIAS CHECK COMPLETED AT8817.1 ACFT HRS.RED: 5.06,4.74=.32YELLOW:5.03,4.69=.34BLACK: 4.36,4.08=.28BLUE:4.45,4.12=.33

20-Nov-2015 1


marilyn.l.jones

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

01-Dec-2015 1


dean.a.keirn

USAACETAIL ROTOR CABLE TENSION CHECKCOMPLETED AT 8827.4 ACFT HRS. FAILED.

03-Dec-2015 1


marilyn.l.jones

USAACETAIL ROTOR CABLE TENSION COMPLETED AT8839.8 ACFT HRS. FAILED. L/H-132, R/H- 130 @13 C*.

07-Dec-2015 1


marilyn.l.jones

USAACEMAIN TRANSMISSION IMPENDING FILTERBYPASS BUTTON POPPED AT 8,839.8 ACFTHRS.

09-Dec-2015 1


marilyn.l.jones

USAACEACFT NO LONGER OPERATING IAW AWR 1648R3 (MAGNUS LAPTOP).

22-Dec-2015 1


chelsey.p.phillips

USAACEACFT OPERATING IAW AWR 1913 R1 DATED06NOV15 (ACN ELECTRONIC LOGBOOK).

22-Dec-2015 2


chelsey.p.phillips

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

05-Jan-2016 1


chelsey.p.phillips

USAACETAIL ROTOR CABLE TENSION CHECKCOMPLETED AT 8847.1 ACFT. HRS. (FAILED)L/H: 136, R/H:135 @ 20.5 *C.

05-Jan-2016 2


marilyn.l.jones

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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 61 of 64

USAACECOMPLIED WITH THE REQUIREMENTS OF UH-60-16-ASAM-02 (DFH-DEFECTIVE FUEL HOSES)AT 8850.1 ACFT HRS. PASSED.

08-Jan-2016 2


marilyn.l.jones

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

29-Jan-2016 1


dean.a.keirn

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

02-Feb-2016 1


dean.a.keirn

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

17-Feb-2016 1


dean.a.keirn

USAACETAIL ROTOR BIAS CHECK COMPLETED AT8977.1 ACFT. HRS.RED:3.0 DEGREES.YELLOW:3.0 DEGREES.BLACK: 3.0 DEGREESBLUE: 3.0DEGREES

15-Mar-2016 1


matthew.c.jackson

USAACEMEC F310874, 9007.2 ACFT HRS,AUTHORIZATION GRANTED FOR CCAD DFT TOREPLACE THE LH FLOOR SUPPORT TEEANGLE IAW DMWR 1-1520-237.

05-Apr-2016 1


dean.a.keirn

USAACEMEC F310874A, 9007.2 ACFT HRS, ECOD FORREPAIR WAS SENT TO AMCOM ANDAPPROVED PENDING RECEIPT OF PARTS ANDSCHEDULING IN CCAD WORK FLOW.AIRCRAFT MAY REMAIN IN SERVICE UNTILPARTS ARE RECEIVED AND SCHEDULED WITHCCAD DFT TO BE REPAIRED. THISDEFERMENT OF REPAIR MAY NOT EXCEED326.2 AIRCRAFT HOURS.

08-Apr-2016 1


dean.a.keirn

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

13-Apr-2016 1


dean.a.keirn

USAACEMEC F3122701 , 9065.6 ACFT. HRS.AUTHORIZATION GRANTED TO REFERENCEMEO A6241'S PROCEDURE FOR TEMPORARYREPAIR (LH SIDE) UNTIL SUPPLY SYSTEM ISABLE TP PROVIDE REPLACEMENTS.

06-May-2016 1


marilyn.l.jones

USAACEMEC F307289:9065.6 ACFT. HRS.,AUTHORIZATION GRANTED TO WELD REPAIRCRACK PER AWS D17.1 AND TM 1-1500-204-23-SERIES USING WELDING ROD ER4043 ANDGRIND SMOOTH. FLUORESCENT PENETRANTWELD. MEC F307289 DATED 22-DEC-2015.

09-May-2016 1


marilyn.l.jones

USAACEACFT OPERATING IAW AWR 1800 R5 DATED 27APR 16 (EDM) AND/OR (BFT) AT 9077.7 ACFT.HRS. SUPERCEDING ALL PRIOR VERSIONS OFTHIS AWR.

13-May-2016 1


marilyn.l.jones

USAACECOMPLIED THE REQUIREMENTS OF H-60-16-AMAM-06 (T-CLIP INSTALLATION) AT 9077.7ACFT. HRS. N/A TO THIS ACFT.

13-May-2016 2


marilyn.l.jones


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 62 of 64

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

01-Jun-2016 1


dean.a.keirn

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

02-Jun-2016 1


dean.a.keirn

USAACEGEN-16-AMAM-04, AN/APX-123 TRANSPONDERBATTERY REPLACEMENT C/W AT 9101.1 ACFTHRS (AFS #66).

04-Jun-2016 1


dean.a.keirn

USAACEMEC F313599, 9101.1 ACFT HRS, LEFT SPLICESTRAP AND DOUBLER CRACKED STA379,BL45, WL206. CRACKS START IN FORWARDCORNER AND PROGRESS UNDERNEATH THELOWER CARGO DOOR TRACK FAIRINGASSEMBLY. AUTHORIZATION GRANTED TOREPAIR IAW DMWR 1-1520-237-1 WP 0120 00DATED 9 SEPT 2013 WITH EXCEPTIONS ASSTATED IN MEC.

13-Jun-2016 1


dean.a.keirn

USAACE 18-Jun-2016 1


marilyn.l.jones

20-Jun-2016 1


USAACECOMPLIED WITH THE REQUIREMENTS OH H-60-16-SOF-01, UPPER CABIN FRAMECRACKING AT 9101.1 ACFT. HRS.

21-Jun-2016 1


marilyn.l.jones

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-16-AMAM-09 ULLS-A(E) AT 9109.6 ACFT. HRS.

24-Jun-2016 1


marilyn.l.jones

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

USAACEH-60-16-SOF-02 (RESCUE HOISTOPERATIONAL RESTRICTIONS) COMPLIEDWITH @ 9207 ACFT HRS. HOIST NOTINSTALLED.

15-Aug-2016 1


mary.b.hodge

USAACEH-60-16-ASAM-06 (IMPROVED TAIL ROTORQUADRANT SUPPORT) C/W @ 9231.2 ACFTHRS.

22-Aug-2016 1


mary.b.hodge

USAACE#2 CROSSFEED BREAKAWAY VALVEREPLACED @ 9238.6 ACFT HRS IAW EM 0013WP 1000.

27-Aug-2016 1


mary.b.hodge

USAACETAIL WHEEL YOKE SN: U5412 WASREPLACED WITH T/W YOKE SN: U5439 @9239.1 ACFT HRS.

31-Aug-2016 1


mary.b.hodge


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 63 of 64

USAACEH-60-16-AMAM-10 (ULLS PHASE LCFUPDATES) C/W @ 9239.1 ACFT HRS.

02-Sep-2016 1


mary.b.hodge

USAACEMAIN MOD SN: A26500669 FILTER BUTTONPOPPED @ 9250.9 ACFT HRS.SERVICEABILITY COMP AND BUTTON RESET.(1ST OCCURRENCE).

08-Sep-2016 1


mary.b.hodge

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

USAACEH-60-17-ASAM-01 (ULLS-AE CADS MODULE)C/W @ 9288.5 ACFT HRS.

05-Oct-2016 1


mary.b.hodge

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 ISAQ 123.

26-Oct-2016 1


dean.a.keirn

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

USAACEH-60-17-ASAM-02 (TAIL ROTOR SERVO PILOTINPUT ARM ASSEMBLY) C/W @ 9303.6 ACFTHRS.

23-Nov-2016 1


mary.b.hodge

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

12-Dec-2016 1


dean.a.keirn

USAACEH-60-17-AMAM-01 (ULLS-A(E) LCF CHANGE 68C/W @ 9303.6 ACFT HRS.

20-Dec-2016 1


mary.b.hodge

USAACEH-60-17-SOF-01 (RESCUE HOIST EMERGENCYCHANGES) N/A TO THIS ACFT.

20-Dec-2016 2


mary.b.hodge

USAACEH-60-17-ASAM-04 (AIRFRAME STRUCTURALPARTS) C/W @ 9603.6 ACFT HRS.

06-Jan-2017 1


mary.b.hodge

SCIENCE ANDENGINEERINGSERVICES LLC

ACFT TRANSFERRED TO BEST PROGRAM2/27/17 @ 9303.6 ACFT HOURS. DATA PLATEINSTALLED.

27-Feb-2017 1

HUNTSVILLE

james.r.harper


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 64 of 64

SCIENCE ANDENGINEERINGSERVICES LLC

H-60-17-ASAM-07 NOT COMPLIED WITH. 17-Mar-2017 1

HUNTSVILLE

james.r.harper

SESIH-60-17-AMAM-07 NOT COMPLIED WITH 24-Mar-2017 1

HUNTSVILLE

james.m.aldrich


DATE AC HRS SHAFT VERTICAL REASON FOR VIBRATION CHECKLONGITUDINALLATERALIPS READINGS4.

8624564HELICOPTER, UTILITYEH-60A

3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL

Page 1 of 10

a b c d e f g

120 HR. VIBE CHECK09-Jan-2016 #2 ENGINE 0.190.000.008,850.1

100 HOUR INSP.16-Mar-2000 LH ENG 0.060.000.001,240.7

100 HOUR INSP.16-Mar-2000 OIL COOLER 0.060.010.001,240.7

100 HOUR INSP.16-Mar-2000 RH ENG 0.090.000.001,240.7

100 HR INSP TQ=3616-Oct-2000 LH ENG 0.070.000.001,337.3

100 HR INSP TQ=3616-Oct-2000 OIL COOLER 0.030.330.001,337.3

100 HR INSP TQ=3516-Oct-2000 RH ENG 0.360.000.001,337.3

ENG R&R TQ=3715-Nov-2000 LH ENG 0.310.000.001,392.4

ENG R &R BAL CK TQ=3817-Nov-2000 LH ENG 0.440.000.001,393.4

100 HR INSP TQ=3424-Jul-2001 #1 ENG 0.150.000.001,442.4

100 HR INSP TQ=3424-Jul-2001 #2 ENG 0.220.000.001,442.4

100 HR INSP24-Jul-2001 OIL COOLER 0.070.200.001,442.4

100 HR INSP TQ=3903-Oct-2001 L/H ENG 0.370.000.001,545.1

100 HR INSP03-Oct-2001 OIL COOLER 0.140.260.001,545.1

100 HR INSP TQ=3803-Oct-2001 R/H ENG 0.380.000.001,545.1

100 HR INSP TQ=3626-Dec-2001 #1 ENG 0.280.000.001,644.7

100 HR INSP TQ=3726-Dec-2001 #2 ENG 0.440.000.001,644.7

100 HR INSP26-Dec-2001 OIL COOLER 0.110.470.001,644.7

100 HR INSP TQ=4027-Feb-2002 LEFT ENG 0.330.000.001,744.8

100 HR INSP27-Feb-2002 OIL COOLER 0.110.140.001,744.8

100 HR INSP TQ=3927-Feb-2002 RIGHT ENG 0.280.000.001,744.8

100 HR INSP TQ=3624-Apr-2002 #1 ENG 0.320.000.001,844.6

100 HR INSP TQ=3524-Apr-2002 #2 ENG 0.270.000.001,844.6

100 HR INSP24-Apr-2002 OIL COOLER 0.050.500.001,844.6

500 HR INSP TQ=3715-Aug-2002 #1 ENG 0.190.000.001,934.7

500 HR INSP TQ=3715-Aug-2002 #2 ENG 0.250.000.001,934.7


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




Page 2 of 10

a b c d e f g

500 HR INSP15-Aug-2002 OIL COOLER 0.050.010.001,934.7

#1 ENG REM. & REINST TQ=3622-Sep-2002 #1 ENG 0.100.000.001,953.1

100 HR INSP TQ=3715-Nov-2002 #1 ENG 0.140.000.002,039.4

100 HR INSP TQ=3515-Nov-2002 #2 ENG 0.070.000.002,039.4

100 HR INSP15-Nov-2002 OIL COOLER 0.030.140.002,039.4

100 HR INSP TQ = 3810-Jan-2003 L/H ENG 0.080.000.002,139.4

100 HR INSP10-Jan-2003 OIL COOLER 0.020.100.002,139.4

100 HR. INSP TQ=3710-Jan-2003 R/H ENG 0.110.000.002,139.4

100 HR. INSP TQ=3702-Mar-2003 L/H #1 ENG 0.130.000.002,238.7

100 HR INSP02-Mar-2003 OIL COOLER 0.030.120.002,238.7

100 HR. INSP TQ=3702-Mar-2003 R/H #2 ENG 0.350.000.002,238.7

100 HR INSP TQ=3830-Mar-2003 L/H #1 ENG 0.150.000.002,337.5

100 HR. INSP30-Mar-2003 OIL COOLER 0.130.020.002,337.5

100 HR INSP TQ=3830-Mar-2003 R/H #2 ENG 0.250.000.002,337.5

500 HR INSP PHASE #5 TQ=3628-Jul-2003 L/H ENG #1 0.130.000.002,420.5

500 HR INSP PHASE #528-Jul-2003 OIL COOLER 0.200.400.002,420.5

500 HR INSP PHASE #5 TQ=3528-Jul-2003 R/H ENG #2 0.260.000.002,420.5

100 HR INSP TQ= 3713-Sep-2003 L/H ENG #1 0.100.000.002,525.6

100 HR INSP13-Sep-2003 OIL COOLER 0.320.170.002,525.6

100 HR INSP TQ=3613-Sep-2003 R/H ENG #2 0.140.000.002,525.6

100 HR INSP TQ=3829-Oct-2003 L/H ENG 0.020.000.002,576.6

100 HR INSP29-Oct-2003 OIL COOLER 0.130.340.002,576.6

100 HR INSP TQ=3829-Oct-2003 R/H ENG 0.300.000.002,576.6

100 HR INSP12-Dec-2003 L/H ENG 0.120.000.002,626.1

100 HR INSP12-Dec-2003 OIL COOLER 0.250.420.002,626.1

100 HR INSP12-Dec-2003 R/H ENG 0.050.000.002,626.1






Page 3 of 10

a b c d e f g

100 HR INSP21-Feb-2004 OIL COOLER 0.150.110.002,728.4

100 HR INSP TQ=3821-Feb-2004 L/H ENG 0.120.000.002,728.8

100 HR INSP TQ=3821-Feb-2004 R/H ENG 0.060.000.002,728.8

100 HR INSP TQ = 3605-Apr-2004 L/H ENG 0.100.000.002,823.8


100 HR INSP TQ = 3605-Apr-2004 R/H ENG 0.090.000.002,823.8

PMS II #6. TQ= 35.21-Aug-2004 L/H ENG 0.050.000.002,916.6

PMS II #6.21-Aug-2004 OIL COOLER 0.140.240.002,916.6

PMS II #6. TQ= 35.21-Aug-2004 R/H ENG 0.170.000.002,916.6

T/R BALANCE CK TQ=3501-Nov-2004 L/H ENG 0.290.000.003,040.6

T/R BALANCE01-Nov-2004 OIL COOLER 0.110.030.003,040.6

T/R BALANCE CK TQ=3501-Nov-2004 R/H ENG 0.200.000.003,040.6

ENG REPLACEMENT. TQ= 37.07-Dec-2004 L/H ENG 0.400.000.003,086.6

ENG CDU REPLACEMENT.03-Jan-2005 OIL COOLER 0.060.250.003,108.7

120 HR INSP. TQ= 38.27-Jan-2005 L/H ENG 0.350.000.003,160.5

120 HR INSP.27-Jan-2005 OIL COOLER 0.250.100.003,160.5

120 HR INSP. TQ= 36.27-Jan-2005 R/H ENG 0.220.000.003,160.5

ENG REMOVE/REINSTALL. TQ NOT NOTED.05-Feb-2005 L/H ENG 0.430.000.003,174.5

350 HR INSP.22-Mar-2005 OIL COOLER 0.140.210.003,266.6

120 HR INSP. TQ= 36.03-Apr-2005 L/H ENG 0.240.000.003,279.7

120 HR INSP.03-Apr-2005 OIL COOLER 0.160.350.003,279.7

120 HR INSP. TQ= 36.03-Apr-2005 R/H ENG 0.250.000.003,279.7

120 HR INSP. TQ= 35.13-May-2005 L/H ENG 0.190.000.003,402.1

120 HR INSP.13-May-2005 OIL COOLER 0.070.250.003,402.1

120 HR INSP. TQ= 36.13-May-2005 R/H ENG 0.150.000.003,402.1

MAIN XMSN MOD REPLACED. TQ= 34.27-Jul-2005 L/H ENG 0.380.000.003,439.7






Page 4 of 10

a b c d e f g

(NO REMARK)27-Jul-2005 OIL COOLER 0.230.050.003,439.7

MAIN XMSN MOD REPLACED. TQ= 36.27-Jul-2005 R/H ENG 0.250.000.003,439.7

120 HR INSP, TQ=3621-Sep-2005 L/H ENG 0.310.000.003,525.9

120 HR INSP21-Sep-2005 OIL COOLER 0.080.110.003,525.9

120 HR INSP, TQ=3521-Sep-2005 R/H ENG 0.110.000.003,525.9

PHASE INSP #7, TQ=3926-Dec-2005 L/H ENG 0.310.000.003,633.5

PHASE INSP #726-Dec-2005 OIL COOLER 0.510.140.003,633.5

PHASE INSP #7, TQ=3826-Dec-2005 R/H ENG 0.110.000.003,633.5

BAL CK DUE. NO TQ NOTED.27-Jan-2006 OIL COOLER 0.160.730.003,656.0

120 HR INSP01-Mar-2006 LH ENG 0.420.000.003,756.2

120 HR INSP01-Mar-2006 OIL COOLER 0.510.190.003,756.2

120 HR INSP01-Mar-2006 RH ENG 0.100.000.003,756.2

120 HR INSP07-Apr-2006 L/H ENG 0.390.000.003,877.0


120 HR INSP07-Apr-2006 R/H ENG 0.070.000.003,877.0

120 HR INSP, TQ=3524-Jul-2006 L/H ENG 0.440.000.004,116.3

120 HR INSP24-Jul-2006 OIL COOLER 0.230.740.004,116.3

120 HR INSP, TQ=3524-Jul-2006 R/H ENG 0.090.000.004,116.3

120 HR INSP, TQ NOT PROVIDED15-Sep-2006 L/H ENG 0.430.000.004,237.6

120 HR INSP, VERT NOT PROVIDED15-Sep-2006 OIL COOLER 0.000.460.004,237.6

120 HR INSP, TQ NOT PROVIDED15-Sep-2006 R/H ENG 0.180.000.004,237.6

720 HR INSP. PHASE #8 TQ NOT PROVIDED14-Feb-2007 #1 ENG 0.220.000.004,352.8

720 HR INSP. PHASE #8 TQ NOT PROVIDED14-Feb-2007 #2 ENG 0.200.000.004,352.8

720 HR INSP. PHASE #814-Feb-2007 OIL COOLER 0.000.180.004,352.8

120 HR MTP NO TQ GVN09-Apr-2007 L/H ENG 0.480.000.004,473.9

120 HR MTP09-Apr-2007 OIL COOLER 0.000.430.004,473.9






Page 5 of 10

a b c d e f g

120 HR MTP NO TQ GVN09-Apr-2007 R/H ENG 0.180.000.004,473.9

120 HR MTP NO TQ06-Jun-2007 L/H ENG 0.060.000.004,596.2

120 HR MTP06-Jun-2007 OIL COOLER 0.000.290.004,596.2

120 HR MTP NO TQ06-Jun-2007 R/H ENG 0.370.000.004,596.2

120 HR MTP NO TQ GVN26-Jul-2007 L/H ENG 0.060.000.004,714.0

120 HR MTP26-Jul-2007 OIL COOLER 0.000.360.004,714.0

120 HR MTP NO TQ GVN26-Jul-2007 R/H ENG 0.190.000.004,714.0

120 HR MTP NO TQ GVN24-Sep-2007 L/H 0.210.000.004,834.2

120 HR MTP24-Sep-2007 OIL COOLER 0.000.010.004,834.2

120 HR MTP NO TQ GVN24-Sep-2007 R/H 0.320.000.004,834.2

VIBE CK NO TQ PROVIDED22-Apr-2008 L/H ENG 0.330.000.005,070.6

VIBE CK22-Apr-2008 OIL COOLER 0.000.720.005,070.6

VIBE CK NO TQ PROVIDED22-Apr-2008 R/H ENG 0.300.000.005,070.6

BALANCE DUE10-Aug-2008 L/H ENG 0.190.000.005,200.4

120 HR MTP TQ NOT PROVIDED19-Nov-2008 #1 L/H ENG 0.310.000.005,315.2

120 HR MTP TQ NOT PROVIDED19-Nov-2008 #2 R/H ENG 0.130.000.005,315.2

120 HR MTP TQ NOT PROVIDED19-Nov-2008 OIL COOLER 0.000.340.005,315.2

120 HR MTP25-Jan-2009 #1 L/H ENG 0.240.000.005,433.6

120 HR MTP25-Jan-2009 #2 R/H ENG 0.060.000.005,433.6

120 HR MTP25-Jan-2009 OIL COOLER 0.000.360.005,433.6

120 HR MTP25-Jan-2009 T/R 0.000.100.005,433.6

120 HR MTP NO TQ NOTED11-Mar-2009 #1 ENG 0.230.000.005,555.6

120 HR MTP NO TQ NOTED11-Mar-2009 #2 ENG 0.110.000.005,555.6

120 HR MTP11-Mar-2009 OIL COOLER 0.000.390.005,555.6

120 HR MTP11-Mar-2009 T/R 0.000.050.005,555.6

120 HR MTP NO TQ NOTED26-Apr-2009 #1 ENG 0.300.000.005,672.9






Page 6 of 10

a b c d e f g

120 HR MTP NO TQ NOTED26-Apr-2009 #2 ENG 0.100.000.005,672.9

120 HR MTP26-Apr-2009 OIL COOLER 0.000.400.005,672.9

120 HR MTP26-Apr-2009 TAIL ROTOR 0.000.090.005,672.9

POST PHASE #10 TQ CHECK NO TQ PROVIDED20-Jul-2009 #1 ENG 0.190.000.005,775.0

POST PHASE #10 TQ CHECK NO TQ PROVIDED20-Jul-2009 #2 ENG 0.290.000.005,775.0

POST PHASE #10 TQ CHECK NO TQ PROVIDED20-Jul-2009 OIL COOLER 0.000.570.005,775.0

120 HR MTP NO TQ NOTED23-Sep-2009 #1 ENG 0.260.000.005,913.1

120 HR MTP NO TQ NOTED23-Sep-2009 #2 ENG 0.360.000.005,913.1

120 HR MTP23-Sep-2009 OIL COOLER 0.000.260.005,913.1

120 HR MTP NO TQ NOTED08-Nov-2009 ENG #1 0.210.000.006,023.4

120 HR MTP NO TQ NOTED08-Nov-2009 ENG #2 0.210.000.006,023.4

120 HR MTP NO TQ NOTED08-Nov-2009 OIL COOLER 0.000.230.006,023.4

120 HR MTP NO TQ NOTED19-Jan-2010 #1 ENG 0.290.000.006,135.0

120 HR MTP NO TQ NOTED19-Jan-2010 #2 ENG 0.340.000.006,135.0

120 HR MTP19-Jan-2010 OIL COOLER 0.000.210.006,135.0

REPL OF T/R D/S SUPPORT BEARING07-Mar-2010 OIL COOLER 0.000.360.006,240.1

120 HR MTP; NO TQ PROVIDED29-Mar-2010 #1 ENGINE 0.190.000.006,257.4

120 HR MTP; NO TQ PROVIDED29-Mar-2010 #2 ENGINE 0.110.000.006,257.4

120 HR MTP; NO TQ PROVIDED29-Mar-2010 OIL COOLER 0.000.310.006,257.4

120 HR MTP: TQ=34%19-Jun-2010 #1 ENG 0.270.000.006,377.5

120 HR MTP: TQ=34%19-Jun-2010 #2 ENG 0.340.000.006,377.5

120 HR MTP:19-Jun-2010 OIL COOLER 0.000.290.006,377.5

120 HR MTP MOC03-Sep-2010 #1 ENG 0.220.000.006,491.8

120 HR MTP MOC03-Sep-2010 #2 0.200.000.006,491.8

120 HR MTP MOC03-Sep-2010 OIL COOLER 0.000.260.006,491.8

720 HR PHASE05-Sep-2010 #1 ENG 0.220.000.006,493.3






Page 7 of 10

a b c d e f g

720 HR PHASE05-Sep-2010 #2 ENG 0.200.000.006,493.3

720 HR PHASE05-Sep-2010 OIL COOLER 0.000.260.006,493.3

120 HR MTP20-Oct-2010 #1 ENG 0.250.000.006,612.5

120 MTP MOC28-Oct-2010 #2 ENG 0.130.000.006,612.5

120 HR MTP MOC28-Oct-2010 OIL COOLER 0.000.250.006,612.5

120 HR MTP MOC28-Oct-2010 #1 ENG 0.250.000.006,612.5

120 MTP MOC15-Dec-2010 # 1 ENG 0.290.000.006,737.1

120 HR MTP MOC15-Dec-2010 # 2 ENG 0.090.000.006,737.1

120 HR MTP MOC15-Dec-2010 OIL COOLER 0.000.450.006,737.1

120 HR MTP MOC NO TQ NOTED15-Mar-2011 # ENG 0.270.000.006,850.7

120 HR MTP MOC- NO TQ NOTED15-Mar-2011 # 2 ENG 0.370.000.006,850.7

120 HR MTP MOC15-Mar-2011 OIL COOLER 0.000.370.006,850.7

120 HR MTP - NO TQ NOTED12-May-2011 #1 ENG 0.300.000.006,973.4

120 HR MTP - NO TQ NOTED12-May-2011 #2 ENG 0.050.000.006,973.4

120 HR MTP12-May-2011 OIL COOLER 0.000.370.006,973.4

120 HR MTP12-May-2011 TAIL ROTOR 0.000.150.006,973.4

120 HR MTP - NO TQ NOTED27-Aug-2011 #1 ENG 0.290.000.007,091.6

120 HR MTP - NO TQ NOTED27-Aug-2011 #2 ENG 0.100.000.007,091.6

120 HR MTP27-Aug-2011 OIL COOLER 0.000.240.007,091.6

120 HR MTP120 HR MTP

27-Aug-2011 T/R 0.000.070.007,091.6

WEIGHT AND BALANCE ON T/R BLADES. TQ=10002-Sep-2011 T/R 0.000.090.007,094.2

REPL T/R BOOTS15-Sep-2011 T/R 0.000.140.007,114.2

120 HR VIBE CHECK03-Dec-2011 #1 ENG 0.130.000.007,184.7

120 HR VIBE CHECK03-Dec-2011 #2 ENG 0.090.000.007,184.7

120 HR VIBE CHECK03-Dec-2011 OIL COOLER 0.000.070.007,184.7

120 HR VIBE CHECK03-Dec-2011 T/R D/S 0.000.080.007,184.7






Page 8 of 10

a b c d e f g

T/R TRACK AND BALANCE DUE29-Feb-2012 T/R 0.000.060.007,270.7

120 HR MOC05-Apr-2012 #1 ENG 0.070.000.007,308.5

120 HR MOC05-Apr-2012 #2 ENG 0.430.000.007,308.5

120 HR MOC05-Apr-2012 OIL COOLER 0.000.100.007,308.5

120 HR MOC05-Apr-2012 T/R 0.000.080.007,308.5

120 HR VIBE CHECK12-May-2012 OIL COOLER 0.000.110.007,429.6

120 HR VIBE CHECK12-May-2012 #1 ENG 0.100.000.007,429.6

120 HR VIBE CHECK12-May-2012 #2 ENG 0.320.000.007,429.6

120 HR VIBE CHECK12-May-2012 T/R 0.000.150.007,429.6

360 HR INSP13-Aug-2012 #1 ENG 0.230.000.007,543.0

360 HR INSP13-Aug-2012 #2 ENG 0.150.000.007,543.0

360 HR INSP13-Aug-2012 OIL COOLER 0.000.120.007,543.0

360 HR INSP13-Aug-2012 T/R 0.000.110.007,543.0

T/R RIG11-Dec-2012 T/R 0.000.150.007,734.3

VIBE CHECK DUE11-Dec-2012 OIL COOLER 0.000.120.007,734.3

T/R BALANCE18-Dec-2012 T/R 0.000.060.007,744.0

120 HR MOC03-Feb-2013 #1 ENG 0.460.000.007,780.2

120 HR MOC03-Feb-2013 #2 ENG 0.450.000.007,780.2

120 HR MOC03-Feb-2013 OIL COOLER 0.090.000.007,780.2

120 HR MOC03-Feb-2013 T/R 0.000.140.007,780.2

POST PHASE15-Jun-2013 #1 ENG 0.320.000.007,896.5

POST PHASE15-Jun-2013 #2 ENG 0.260.000.007,896.5

POST PHASE15-Jun-2013 OIL COOLER 0.000.160.007,896.5

POST PHASE15-Jun-2013 T/R D/S 0.000.060.007,896.5

120 HR VIBE CK29-Aug-2013 #1 ENG 0.400.000.008,019.1

120 HR VIBE CK29-Aug-2013 #2ENG 0.100.000.008,019.1






Page 9 of 10

a b c d e f g

120 HR VIBE CK29-Aug-2013 OIL COOLER 0.000.140.008,019.1

120 HR VIBE CK29-Aug-2013 T/R 0.000.120.008,019.1

120 HR DRIVESHAFT BAL CHECK10-Dec-2013 #1 ENG 0.120.000.008,257.7

120 HR DRIVESHAFT BAL CHECK10-Dec-2013 #2 ENG 0.140.000.008,257.7

120 HR DRIVESHAFT BAL CHECK10-Dec-2013 OIL COOLER 0.000.100.008,257.7

120 HR DRIVESHAFT BAL CHECK10-Dec-2013 T/R 0.000.090.008,257.7

REM/REINSTALL T/R BLADE ASSY25-Feb-2014 TAIL ROTOR 0.000.130.008,266.8

REQUIRED WITH MTF IAW TM 1-1520-237 MTF26-Feb-2014 TAIL ROTOR 0.000.100.008,267.4

120 HR INSP28-May-2014 #1 ENG 0.040.000.008,381.5

120 HR INSP28-May-2014 #2 ENG 0.210.000.008,381.5

120 HR INSP28-May-2014 OIL COOLER 0.000.070.008,381.5

120 HR INSP28-May-2014 T/R 0.000.140.008,381.5

120 HR MTP30-Jul-2014 #1 ENG 0.050.000.008,500.7

120 HR MTP30-Jul-2014 #2ENG 0.030.000.008,500.7

120 HR MTP30-Jul-2014 T/R 0.000.110.008,500.7

120 HR MTP30-Jul-2014 OIL COOLER 0.000.050.008,500.7

120 HR INSP VIBE CHECK28-Jul-2015 #1 ENG 0.260.000.008,613.4

120 HR VIBE INSPECTION28-Jul-2015 #2 ENGINE 0.160.000.008,613.4

120 HR VIBE INSPECTION28-Jul-2015 OIL COOLER 0.000.340.008,613.4

120 HR VIBE INSPECTION28-Jul-2015 TAIL ROTOR 0.000.030.008,613.4

POST PHASE30-Jul-2015 #1 ENG 0.260.000.008,615.4

POST PHASE30-Jul-2015 #2 ENG 0.160.000.008,615.4

POST PHASE30-Jul-2015 OIL COOLER 0.340.000.008,615.4

POST PHASE30-Jul-2015 T/R D/S 0.000.030.008,615.4

120 HR VIBE CHECK02-Oct-2015 #1ENGINE 0.430.000.008,735.6

120 HR VIBE CHECK03-Oct-2015 #2 ENGINE 0.210.000.008,735.6






Page 10 of 10

a b c d e f g

120 HR VIBE CHECK03-Oct-2015 OIL COOLER 0.000.420.008,735.6

120 HR VIBE CHECK03-Oct-2015 TAIL ROTOR 0.000.020.008,735.6

120 HR. VIBE CHECK09-Jan-2016 #1 ENGINE 0.470.000.008,850.1

120 HR. VIBE CHECK09-Jan-2016 OIL COOLER 0.000.580.008,850.1

120 HR. VIBE INSPECTION15-Mar-2016 #1 ENGINE 0.340.000.008,977.1

120 HR. VIBE INSPECTION.15-Mar-2016 # 2 ENGINE 0.190.000.008,977.1

120 HE VIBE INSPECTION.15-Mar-2016 OIL COOLER 0.000.530.008,977.1

120 HR. VIBE INSPECTION.15-Mar-2016 TAIL ROTOR 0.000.090.008,977.1

120 HR. VIBE CHECK25-May-2016 #1 ENGINE 0.240.000.009,095.9

120 HR. VIBE CHECK.25-May-2016 #2 ENGINE 0.180.000.009,095.9

120 HR. VIBE CHECK25-May-2016 OIL COOLER 0.000.450.009,095.9

120 HR. VIBE CHECK25-May-2016 TAIL ROTOR 0.000.020.009,095.9

120 HR VIBE CK18-Aug-2016 #1 ENG 0.100.000.009,220.6

120 HR VIBE CK18-Aug-2016 #2 ENG 0.150.000.009,220.6

120 HR VIBE CK18-Aug-2016 OIL COOLER 0.000.480.009,220.6

120 HR VIBE CK18-Aug-2016 T/R D/S 0.000.080.009,220.6

5. REMARKS

marilyn.l.jones

UNABLE TO BALANCE TAIL ROTOR DURING THE 120 HR VIBE CHECK.09-Jan-2016

FT. RUCKER, AL.USAACE



of 12

CAO00502

86245646035T00G01T700-GE-700 ENGINE ASSYGE-E-307091

5172

4992

27256

21673

8764

12489

2907

3011

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 12

04A 6035T00G01 T700-GE-700 ENGINE ASSY GE-E-307091

hr)

456821526112212831

460820182109172279GE-C-0060976035T02G01COLD SECTIONMODULE

COND

COND

4568

246GGM95K9F6064T55G01COMBUSTION LINER

COND

COND

456821526112212831

2513563170141762MRS091016055T20G05MTCHDROTOR/STATOR ASSY

COND

COND

4568

2888AMDA44765043T24G14STAGE 1 NOZZLE

COND

COND

456821526112212831

43461079279692201GE-L-0065736064T98G01POWER TURBINEMODULE

COND

COND

4568

2845GED0371536035T01G01ACCESSORY MODULE

COND

COND

4568

2395SUPJ61096034T62P13PARTICLESEPARATOR BLOWER

COND

COND

4992

3227UDAJ03185074T79G07FUEL CONTROL

COND

COND

4568

3123APM110RS4076T64G01POU ASSY-O/S DRAINVALVE

COND

COND

456821526112212831

47482710974962727CAO005024046T26G03HISTORY RECORDER

COND

COND

4568

6554UDC017384046T25G01COOLER, OIL

COND

COND

4568

2153GRTB40675066T38G08ANTI-ICE VALVE

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 12


hr)

14. SIGNIFICANT HISTORICAL DATA

10/27/201012:00:00 AM

1 ENGINE REPAIRED 22 OCT 10 IAW DMWR 1-2840-248-& CHANGES ANDRECAPPED DTD 03 DEC 01 S//M. THORN AIRCRAFT DATE TECHNICAN

MT1154 CCAD CORPUS CHRISTI, TX

12/6/201512:00:00 AM

1 ENGINE INSTALLED ON ACFT 8624571 AT 8198 ACFT HRS WITH LCF1 2857LCF2 11319 TTI 21610 OP HRS 4629 H/R S/N CAO00502 READINGS = LCF12753 LCF2 7594 TTI 27193 OP HRS 4809

OW 01095 USAACE FT RUCKER,AL

1/27/201712:00:00 AM

1 REMOVED ECU SN: EMDE0153, WITH TSN: 1457, FROM ENG GE-E-307091,H.R SN: CAO00502, AT H.R. READINGS: 2907, LCF2: 8764, TTI: 27256, OP HRS:5172. ENG CUMULATIVE COUNTS: LCF1: 3001, LCF2: 12489, TTI: 21673, OP

christina.l.negron USAACE FT. RUCKER, AL

1/27/201712:00:00 AM

2 REMOVED ENG SN: GE-E-307091, FROM ACFT 8624571, AT 8535 ACFT HRS.H.R. SN: CAO00502, AT H.R. READINGS LCF1; 2907, LCF2: 8764, TTI: 27256,HRS: 5172. ENG CUMULATIVE COUNTS: LCF1: 3011,LCF2: 12489. TTI: 21873,HRS: 4992. REMOVAL IS DUE TO LEAKING AT AIR TUBE FROM MID FRAMESLIP JOINT. ****NOTE***THIS ENG IS T.W.O. FOR AN ECU.

christina.l.negron USAACE FT. RUCKER, AL

2/4/201712:00:00 AM

1 REMOVED FUEL CONTROL S/N: 13349774 WITH TSN: 1152 AS SERVICABLECOMPONENT. INSTALLED FUEL CONTROL S/N: UDAJ0318 WITH TSN: 3227AS UNSERVICABLE COMPONENT(FAILURE CODE 803) WITH ENGINE CUM.COUNTS: LCF1 3011, LCF2 12489, TTI 21673, HRS 4992 & H/R READINGS:LCF1 2907, LCF2 8764, TTI 27256, HRS 5172.(UN-INSTALLED ENGINE)

KG4191 USAACE FT. RUCKER, AL

2/6/201712:00:00 AM

1 INSTALLED ENG SN: GE-E-307091 W/TSN:4992 ON ACFT. 8624564 AT 9303.6ACFT. HRS. HISTORY RECORDER (SN:CAO00502) READINGS:2907,8764,27256,5172. ENGINE CUM. COUNTS: 3011,12489,21673,4992.

marilyn.l.jones USAACE FT. RUCKER, AL.


of 12

CAO00502

GE-E-3070916035T02G01COLD SECTION MODULEGE-C-006097

4748

4608

27109

20182

7496

10917

2727

2279

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 5 of 12

04A01 6035T02G01 COLD SECTION MODULE GE-C-006097

hr)

460820182109172279

32941815491962328SAP570615044T27G02POWER TAKEOFFDRIVE

COND

COND

460820182109172279

490130084130482975GLB003016035T77G10COMPRESSORROTOR ASSY

COND

COND

460820182109172279

19161233025621061GATHE9266035T88P04GAS GEN TURBINESHAFT

13832

11000

460820182109172279

0000WESR05935036T95P01INNER BALANCEPISTON SE

COND

COND

460820182109172279

0000BIWYAMA26035T79P04COMPRESSORDISCHARGE SE

COND

COND

460820182109172279

73528271935569FIAAKJ6H6035T83P01COMPRESSOR REARSHAFT

9013

5000

460820182109172279

0000TYV60285044T07P01NO 3 LABYRINTH

COND

COND

460820182109172279

30081457273551602FMC030605035T57P02VORTEX SPOILER

COND

COND

460820182109172279

34871178646911450GATK94445043T04P02TIE ROD,COMPRESSOR

11261

10000

460820182109172279

21231003768101638GATPW4714045T08P01RING, SPACERCOMPRESSOR

12625

10000

460820182109172279

0000GLHTM1TT6055T59P01COMPRESSORIMPELLER

9748

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 6 of 12

04A01 6035T02G01 COLD SECTION MODULE GE-C-006097

hr)

460820182109172279

0000GGTA40583065T21G01OUTPUT SHAFT ASSY

COND

COND

460820182109172279

0000GLHTM4446032T26G09STAGE 1 BLISK

9748

5000

460820182109172279

0000GLHTMLF36032T27P08STAGE 2 BLISK

11748

7000

460820182109172279

0000GLHTMT5P6038T08P04STAGE 3 & 4 BLISK

11748

7000

460820182109172279

0000GLHTML0T6038T09P04STAGE 5 BLISK

11748

7000

460820182109172279

3247358166031794MDAM46036038T48P02NO 3 BALL BEARING

COND

COND

460820182109172279

3751658857273FCAG49296064T15P03NO 4 ROLLER

COND

COND



of 12

CAO00502

GE-C-0060973065T21G01OUTPUT SHAFT ASSYGGTA4058

4748

0

27109

0

7496

0

2727

0

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 8 of 12

04A01G 3065T21G01 OUTPUT SHAFT ASSY GGTA4058

hr)

0000

0000FCAU15746064T34P02NO 1 BALL BEARING

COND

COND

0000

0000FCAT21095121T46P02NO 2 ROLLER

COND

COND



of 12

CAO00502

GE-E-3070916055T20G05MTCHD ROTOR/STATORMRS09101

4748

2513

27109

5631

7496

7014

2727

1762

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 10 of 12

04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRS09101

hr)

2513563170141762

2513563170141762GGA067636039T57G24STATOR GASGENERATOR

COND

COND

2513563170141762

37358301599142GATH8CME6064T86P01STAGE 2 TURBINE

9375

5000

2513563170141762

1455986936731200BCM246116064T81P01STG 1 FWD COOLINGPLATE

8293

5000

2513563170141762

2901282402135PAMEN5216064T82P01STG 1 AFT COOLINGPLATE

9458

5000

2513563170141762

941111712474723GFF59WKH6064T83P01STG 2 FWD COOLINGPLATE

8807

5000

2513563170141762

3061298461721816GFFP15796064T84P02STG 2 AFT COOLINGPLATE

6687

5000

2513563170141762

2513563170141762GGA091016039T54G13ROTOR GASGENERATOR

COND

COND



of 12

CAO00502

GE-E-3070916064T98G01POWER TURBINE MODULEGE-L-006573

4748

4346

27109

10792

7496

7969

2727

2201

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 12 of 12

04A03 6064T98G01 POWER TURBINE MODULE GE-L-006573

hr)

43461079279692201

43461079279692201GGA086825043T75G07POWER TURBINEROTOR

COND

COND

43461079279692201

3212848596142110GATFF0326038T34P02STAGE 4 TURBINE

6536

5000

43461079279692201

128011801835655GATHGF075125T92G01POWER TURBINESHAFT

8468

5000

43461079279692201

186531822147920MABC50715034T27P01NO 5 ROLLER

COND

COND

43461079279692201

1269102234607910MAB0S7836064T36P01NO 6 BALL BEARING

COND

COND



of 16

CAO00499

86245646035T00G01T700-GE-700 ENGINE ASSYGE-E-306766

7207

6252

13815

6454

20144

15052

4193

3254

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)

40625583110812327

381912746156701863GEC0077436035T02G01COLD SECTIONMODULE

COND

COND

2306

2347GGMFK8196064T55G01COMBUSTION LINER

COND

COND

56156178135742950

33941056060661810MRS074526055T20G05MTCHDROTOR/STATOR ASSY

COND

COND

2306

3593AMDA30485043T24G14STAGE 1 NOZZLE

COND

COND

52456091130062799

32691309096762290GEL0074676064T98G01POWER TURBINEMODULE

COND

COND

2306

2837GE-D-0065896035T01G01ACCESSORY MODULE

COND

COND

2306

0SUPK23676034T62P18PARTICLESEPARATOR BLOWER

COND

COND

5616

3306UDAJ37455074T79G07FUEL CONTROL

COND

COND

5219

6185APM687RS4076T64G01POU ASSY-O/S DRAINVALVE

COND

COND

3471

3096ECD012534046T29G13ELECTRICALCONTROL UNIT

COND

COND

2306466841251518

32611202992172457CAO004994046T26G03HISTORY 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)

2306

1562UDC037274046T25G06COOLER, OIL

COND

COND

3143

0COMH112044046T28G14ANTI-ICE VALVE

COND

COND


8/28/200512:00:00 AM

1 WUC: 04A P/N: 6035T00G01 S/N: GE-E-306766T700-GE-700 ENGINE ASSY, TURBINE28 AUG 08 - ENGINE REPAIRED ANDRETURNED TO SERVICE. REPLACED OUTPUT SHAFT AND PTO DRIVE ASSY,SEE C/S MOD GEC006766 DA FORM 2408-16-1. ENGINE CUMULATIVECOUNTS: LCF1-1668, LCF2-5398, TTI-4870, HRS-2601. H.R. CAO00499READINGS: LCF1-2607, LCF2-10490, TTI-12231, HRS-3556. DK1063, USSACE,

thomas.m.lilly USAACE FT. RUCKER, AL.

8/28/200512:00:00 AM

2 WUC: 04A P/N: 6035T00G01 S/N: GE-E-306766T700-GE-700 ENGINE ASSY, TURBINE28 AUG 08 - ENGINE REPAIRED ANDRETURNED TO SERVICE. REPLACED OUTPUT SHAFT AND PTO DRIVE ASSY,SEE C/S MOD GEC006766 DA FORM 2408-16-1. ENGINE CUMULATIVECOUNTS: LCF1-1668, LCF2-5398, TTI-4870, HRS-2601. H.R. CAO00499READINGS: LCF1-2607, LCF2-10490, TTI-12231, HRS-3556. DK1063, USSACE,

thomas.m.lilly USAACE FT. RUCKER, AL.

4/26/200712:00:00 AM

1 WUC: 04A P/N: 6035T00G01 S/N: GE-E-306766T700-GE-700 ENGINE ASSY, TURBINE26APR07 CCAD ENGINE REPAIRED24APR 07 IAW DMWR 1-2840-248 & CHANGED AND RECAPPED AED P3430BDTD 03 DEC 01. FUEL INJECTORS CLEANED AND FLOWED PER DMWR ATC/S TSN 2306 ON 24APR07 S/SR. HERRERA, REOCRDS CLERK.

thomas.m.lilly CCAD (NO LOCATION)

3/15/201112:00:00 AM

1 15-MAR-11-RMVD ENGINE FROM ACFT 8624514 AT 7418 ACFT HRSA. TSN4062 HRS.(TGT PEAKS AT 971 DEGREES C) ENGINE CUMULITIVE COUNTS:LCF1=2327 LCF2=11081 TTI=5583 OPHRS=4062. HRS/NCAO00499CUMULATIVE READINGS:LCF1=3266 LCF2=6173 TTI=12944 OPHRS=5017

debra.r.chancellor USAACE FT RUCKER AL.

3/29/201112:00:00 AM

1 ENGINE SN: GE-E-306766 WITH TTSN: 4062 SENT TO TEST CELL FOR TGTPEAKED AT 971* C. DURING INSPECTION IT WAS DETERMINED THEENGINE DID NOT OVERHEAT BUT THERE WAS AN INDICATION PROBLEM.ENGINE RETURN TO SERVICEABLE CONDITION AFTER PASSING TESTCELL IN ALL AREAS. ENG CUM COUNTS ARE 2327/11081/5583/4062. H.R. SN:CAO00499 READINGS ARE 3266/16173/12/944/5017.

debra.r.chancellor USAACE FT. RUCKER, AL


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 4 of 16


hr)

4/4/201112:00:00 AM

1 INSTALLED ENG SN: GE-E-306766 WITH TSN: 4062 ON ACFT 8524480 @ 6919ACFT HRS. ENG CUMULATIVE CTS: LCF=2327, LCF2= 11081, TTI=5583, OPHRS=4062. H/R (CAO00499) LCF1=3266, LCF2=16173, TTI=12994, OP HRS=

kathleen.m.jungell USAACE FT. RUCKER, AL

4/25/201112:00:00 AM

1 REMOVED POU SN: APM816RT WITH TSN: 4726 ( INTERNAL FAILURE)FROM ENG SN: GE-E306766 WITH TSN: 4065 (8524480 @ 6919.0 ACFT HRS)ENG CUMULATIVE CTS: LCF1=2330 LCF2=11086 TTI=5583 OP HRS:4065 H/R (SN: CAO00499) RDGS: LCF1=3269 LCF2=16178 TTI=12994 OPHRS=5020 INSTALLED POU SN: APM852RS WITH TSN: 1283


4/27/201112:00:00 AM

1 REMOVED FUEL CONTROL SN: 15464082 , TSN: 406666 (LEAKING)INSTALLED FUEL CONTROL SN: J8002 WITH TSN: 3591ENG ASSY SN: GE-E-306766 WITH ENG CUMULATIVE CTS: LCF1=2330, LCF2=11086, TTI=5583, OPHRS=4066H/R (SN: CAO00499) RDGS: LCF1=3269, LCF2=16178, TTI=12994, OPHRS=5021


4/27/201112:00:00 AM

2 FUEL CONTROL SN: 15464082 REMOVED FROM ENG GE-E-306766 WITH TSN:4066 FROM ACFT 8524480 @ 6919 ACFT HRS. (LEAKING) INSTALLED FUELCONTROL SN: J8002 WITH TSN: 3591ENG CUMULATIVE CTS: LCF1=2330,LCF2=11086, TTI=5583, OP HRS=4066H/R (SN: CAO00499) RDGS: LCF1=3269,LCF2=16178, TTI=12994, OP HRS=5021


9/8/201212:00:00 AM

1 REMOVED FUEL CONTROL SN: J8002 WITH TSN: 4378 IAW H-60-12-ASAM-11FROM ENG ASSY SN: GE-E-306766 WITH ENG CUMULATIVE CTS: 2661 /12589 / 5931 / 4853 HR (SN: ECD01459) RDGS: 3600 / 17681 13292 / 5808


9/9/201212:00:00 AM

1 REINSTALLED FUEL CONTROL SN: J8002 WITH TSN: 4378 TSO: 787 OH'S: 1IAW H-60-12-ASAM-11 ON ENG ASSY SN: GE-E-306766 WITH ENGCUMULATIVE CTS: 2661 / 12589 / 5931 / 4853 HR (SN: ECD01459) RDGS: 3600/ 17681 13292 / 5808


1/16/201312:00:00 AM

1 16 JAN13 - REMOVED ANTI-ICE VALVE SN: COMH8907 TSN: 2372 (DUE TOCANNON PLUG FAILURE) FROM ENG ASSY SN: GE-E-307389 - ENGCUMULATIVE CTS = H/R (SN: ECD01459) RDGS: 4044 / 16704 / 11614 / 9237


1/16/201312:00:00 AM

2 16 JAN13 - INSTALLED ANTI-ICE VALVE SN: GRTU1762 TSN: 1514 ON ENGASSY SN: GE-E-307389 - ENG CUMULATIVE CTS = H/R (SN: ECD01459) RDGS:


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)12:00:00 AM ASSY SN: GE-E-307389 - ENG CUMULATIVE CTS = H/R (SN: ECD01459) RDGS:

4044 / 16704 / 11614 / 9237


1/16/201312:00:00 AM

3 16 JAN13 - INSTALLED ANTI-ICE VALVE SN: GRTU1762 TSN: 1514 ON ENGASSY SN: GE-E-307389 - ENG CUMULATIVE CTS = H/R (SN: ECD01459) RDGS:4044 / 16704 / 11614 / 9237


5/15/201312:00:00 AM

1 REMOVED POU S/N: APM852RS W/TTSN: 2437 FROM ENG GE-E-306766 ENGCUMM COUNTS- LCF1: 2786 LCF2: 12959 TTI: 6006 OP HRS: 5219 H/RREADINGS- LCF1: 3725 LCF2: 18051 TTI: 13367 OP HRS: 6174 DUE TOLEAKING. INSTALLED POU S/N: APM687RS W/TTSN: 6185.

rhonda.e.jackson USAACE FT. RUCKER, AL

7/16/201312:00:00 AM

1 REMOVED ENGINE ASSY GE-E-306766, FOR TIME CHANGE, WITHCUMALATIVE COUNTS: 2799/ 13006, 6091, 5245. H.R.(CAO00499)READINGS:3738, 18098, 13452, 6200.

vickie.l.meadows USAACE FT RUCKER, AL

7/18/201312:00:00 AM

1 REMOVED PT MOD S/N GE-L-006269 (DUE T/CHG) AT 5245 ENG HRS WITHTSN 6063 HRS. CUM CTS: LCF 1 2934, LCF 2 13041, TTI 12564, OP HRS 6063.ENG CUM CTS: LCF 1 2799, LCF 2 13006, TTI 6091, OP HRS 5245. HR S/NCAO00499 CUM READINGS: LCF 1 3738, LCF 2 18098, TTI 13452, OP HRS 6200.INSTALLED PT MOD S/N GE-L-007467 WITH CUM CTS: LCF 1 2290, LCF 29676, TTI 13090, OP HRS 3269.

tony.barnes USAACE FT. RUCKER, AL.

7/19/201312:00:00 AM

1 INSTALLED ENGINE ASSY GE-E-306766, WITH CUMALATIVE COUNTS: 2799/13006, 6091, 5245. H.R.(CAO00499)READINGS: 3738, 18098, 13452, 6200.

vickie.l.meadows USAACE FT RUCKER, AL

4/23/201412:00:00 AM

1 REMOVED FUEL CONTROL SN: J8002, WITH TSN: 4770, FROM ENG SN: GE-E-306766, HISTORY RECORDER SN: CA000499, H.R. READINGS: LCF1: 3738,LCF2: 18098, TTI: 13452, OP HRS: 6200, ENG CUMMULATIVE COUNTS: LCF1:2799, LCF2: 13006, TTI: 6091, OP HRS: 5245. (ACFT 8424480 AT 8072 ACFT HRS)

christina.l.negron USAACE FT RUCKER,AL.

4/23/201412:00:00 AM

2 REMOVED FUEL CONTROL SN: J8002, WITH TSN: 4770, FROM ENG SN: GE-E-306766, HISTORY RECORDER SN: CA000499, H.R. READINGS: LCF1: 3738,LCF2: 18098, TTI: 13452, OP HRS: 6200, ENG CUMMULATIVE COUNTS: LCF1:2799, LCF2: 13006, TTI: 6091, OP HRS: 5245. REMOVAL IS DUE TO INTERNALFAILURE.(ACFT 8424480 AT 8072 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 16


hr)


4/23/201412:00:00 AM

3 REMOVED FUEL CONTROL SN: J8002, WITH TSN: 4770, FROM ENG SN: GE-E-306766, HISTORY RECORDER SN: CA000499, H.R. READINGS: LCF1: 3738,LCF2: 18098, TTI: 13452, OP HRS: 6200, ENG CUMMULATIVE COUNTS: LCF1:2799, LCF2: 13006, TTI: 6091, OP HRS: 5245. REMOVAL IS DUE TO INTERNALFAILURE. INSTALLED FUEL CONTROL SN: UDA96531 WITH 3417.(ACFT8424480 AT 8072 ACFT HRS).


7/10/201412:00:00 AM

1 REMOVED FUEL CONTROL SN: UDA96531, FROM ENG SN: GE-E-306766,WITH H.R. SN: CAO00499, AND H.R. READINGS: LCF1: 3738, LCF2; 18098,ENG CUMULATIVE COUNTS: LCF1: 2799, LCF2: 13006, TTI: 6091, OP HRS:5245. REMOVAL IS DUE TO INTERNAL FAILURE (ENG WILL NOT START,FUEL PUMP NOT PRODUCING FUEL MIST AT EXHAUST).


7/10/201412:00:00 AM

2 REMOVED FUEL CONTROL SN: UDA96531, WITH TSN: 3417, FROM ENG SN:GE-E-306766, WITH H.R. SN: CAO00499, AND H.R. READINGS: LCF1: 3738,LCF2; 18098, ENG CUMULATIVE COUNTS: LCF1: 2799, LCF2: 13006, TTI: 6091,OP HRS: 5245. REMOVAL IS DUE TO INTERNAL FAILURE (ENG WILL NOTSTART, FUEL PUMP NOT PRODUCING FUEL MIST AT EXHAUST).


7/10/201412:00:00 AM

3 REMOVED FUEL CONTROL SN: UDA96531, WITH TSN: 3417, FROM ENG SN:GE-E-306766, WITH H.R. SN: CAO00499, AND H.R. READINGS: LCF1: 3738,LCF2; 18098, ENG CUMULATIVE COUNTS: LCF1: 2799, LCF2: 13006, TTI: 6091,OP HRS: 5245. REMOVAL IS DUE TO INTERNAL FAILURE (ENG WILL NOTSTART, FUEL PUMP NOT PRODUCING FUEL MIST AT EXHAUST). INSTALLEDFUEL CONTROL SN: UDAJ5462, WITH TSN: 6275, 1 PRIOR O/H, AND TSO: 0.


5/20/201512:00:00 AM

1 fuel control s/n: udaj5462 removed with ttsn: 6646 due to internal failure( will not lockout), from engine s/n: ge-e-306766 with cum counts: lcf1=2951, lcf2=13575, tti=6178,hours=5616. h/r (cao00499) readings: lcf1=3890, lcf2=18667, tti=13539, hours=6571.fuel control s/n: udaj3745 installed with ttsn: 3306, tso: 425, with 1 o/haul.

mae.p.belford USAACE FT. RUCKER, AL.

2/3/201712:00:00 AM

1 REMOVED ENG SN: GE-E-306766 W/TTSN: 6252 FROM ACFT 8524480 @ 9053.2ACFT HRS DUE TO "TBO". (ENG CUM COUNTS: 3254/15052/6454/6252)(H/RSN: CAO00499 READING: 4193/20144/13815/7207).

mary.b.hodge USAACE FT. RUCKER, AL

2/6/201712:00:00 AM

1 INSTALLED ENG SN: GE-E-306766 W/TSN:6252 ON ACFT. 8624564 AT 9303.6ACFT. HRS. HISTORY RECORDER (SN:CAO00499) READINGS:4193,20144,13815,7207. ENGINE CUM. COUNTS: 3254,15052,6454,6252.


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 16


hr)

4193,20144,13815,7207. ENGINE CUM. COUNTS: 3254,15052,6454,6252.

marilyn.l.jones USAACE FT. RUCKER,AL.


of 16

CAO00499

GE-E-3067666035T02G01COLD SECTION MODULEGEC007743

5017

3819

12944

12746

16173

15670

3266

1863

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 16

04A01 6035T02G01 COLD SECTION MODULE GEC007743

hr)

381612578156591859

43684668880813088SAP455805044T27G02POWER TAKEOFFDRIVE

COND

COND

381612578156591859

381612578156591859GLB004896035T77G10COMPRESSORROTOR ASSY

COND

COND

381612578156591859

0000WESR15935036T95P01INNER BALANCEPISTON SE

COND

COND

381612578156591859

0000BIWYBELT6035T79P04COMPRESSORDISCHARGE SE

COND

COND

381612578156591859

8805752652555FIAAPA296035T83P01COMPRESSOR REARSHAFT

9134

5000

381612578156591859

0000VAECB4365044T07P01NO 3 LABYRINTH

COND

COND

381612578156591859

3844909875892231BIWCC6195035T57P02VORTEX SPOILER

COND

COND

381612578156591859

20961256066681075GATHGJ245043T04P02TIE ROD,COMPRESSOR

12918

10000

381612578156591859

54635973104782438GAT4204H4045T08P01RING, SPACERCOMPRESSOR

9551

10000

381612578156591859

0000GLHTLL426055T59P01COMPRESSORIMPELLER

10014

5000

381612578156591859

24411063144101237GGAN31966039T56G02OUTPUT SHAFT ASSY

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 10 of 16

04A01 6035T02G01 COLD SECTION MODULE GEC007743

hr)

381612578156591859

0000GLHTM2T56032T26G09STAGE 1 BLISK

10014

5000

381612578156591859

0000GLHTN3P16032T27P08STAGE 2 BLISK

12014

7000

381612578156591859

0000GLHTN0E26038T08P04STAGE 3 & 4 BLISK

12014

7000

381612578156591859

0000GLHTMT6A6038T09P04STAGE 5 BLISK

12014

7000

381612578156591859

33761618246651749BARB15346043T45P01NO 3 BALL BEARING

COND

COND

381612578156591859

100075392278570FCAE75956064T15P03NO 4 ROLLER

COND

COND


1/18/201112:00:00 AM

1 CCAD C/S MOD REPAIRED 14JAN11 ISW DMWR 1-2840-248 & CHANGESAND RECAPPED DTD 03DEC01. FUEL INJECTORS CLEANED AND FLOWEDPER DMWR AT C/S TSN 3819 ON 14JAN11. /S/ C.PALUMBO, AIRCRAFT DATATECHNICIAN.

kathleen.m.jungell CCAD CORPUS CHRISTI


of 16

CAO00499

GEC0077436039T56G02OUTPUT SHAFT ASSYGGAN3196

5017

2444

12944

10799

16173

4421

3266

1241

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 12 of 16

04A01G 6039T56G02 OUTPUT SHAFT ASSY GGAN3196

hr)

24411063144101237

7329721085381FCAK06996064T34P01NO 1 BALL BEARING

COND

COND

24411063144101237

3523941861262078MDAL78695035T71P01NO 2 ROLLER

COND

COND


4/4/201112:00:00 AM

1 18JAN11 CCAD OUTPUT SHAFT REPAIRED 14 NJAN 11 IAW DMWR 1-2840-248 CHANGES AND RECAPPED DTD 03DEC01. /S/ C. PALUMBA, AIRCRAFTDATA TECHNICIAN



of 16

CAO00499

GE-E-3067666055T20G05MTCHD ROTOR/STATORMRS07452

6570

3394

13539

10560

18666

6066

3889

1810

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 14 of 16

04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRS07452

hr)

33941056060661810

941111712474723GATHDA1M6064T85P01STAGE 1 TURBINE

10629

5000

33941056060661810

33941056060661810GGA076866039T57G24STATOR GASGENERATOR

COND

COND

33941056060661810

879107482436699GATHEN086064T86P01STAGE 2 TURBINE

10691

5000

33941056060661810

19211263692411740GFFR83N36064T81P01STG 1 FWD COOLINGPLATE

9649

5000

33941056060661810

100189914033836GFF5A6CL6064T82P01STG 1 AFT COOLINGPLATE

10569

5000

33941056060661810

590992618217GFF5C00T6064T83P01STG 2 FWD COOLINGPLATE

10980

5000

33941056060661810

431323901205GFF5CPNJ6064T84P02STG 2 AFT COOLINGPLATE

11139

5000

33941056060661810

33941056060661810GGA074526039T54G13ROTOR GASGENERATOR

COND

COND


5/7/201512:00:00 AM

1 INSTALLED GG S/N MRS07452 AT 5615 ENG HRS W/TSN 3394, GG CUM CTS;1810, 6066,10560,OP HRS 3394, HR (CAO00499) 3889;18666;13539, OP HRS 6570,

theresa.d.pollard USAACE FT. RUCKER, AL


of 16

CAO00499

GE-E-3067666064T98G01POWER TURBINE MODULEGEL007467

6200

3269

13452

13090

18098

9676

3738

2290

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 GEL007467

hr)

32631290396562282

32631290396562282GGA071975043T75G07POWER TURBINEROTOR

COND

COND

32631290396562282

32631290396562282GAT597226038T32P01STAGE 3 TURBINE

7931

5000

32631290396562282

0000GATH9TJC6038T34P05STAGE 4 TURBINE

11194

5000

32631290396562282

24251735357451345GATLP8925125T92G01REPOWER TURBINESHAFT

8769

5000

32631290396562282

164938181662639MDAM99455034T06P01NO 5 ROLLER

COND

COND

32631290396562282

2728954641761471BARA60945034T04P01NO 6 BALL BEARING

COND

COND


7/18/201312:00:00 AM

1 INSTALLED PT MOD ON ENG S/N GE-E-306766 WITH TSN 3269 HRS AT 5245ENG HRS WITH CUM CTS: LCF 1 2290, LCF 2 9676, TTI 13090, OP HRS 3269.ENG CUM CTS: LCF 1 2799, LCF 2 13006, TTI 6091, OP HRS 5245. HR S/NCAO00499 CUM READINGS: LCF 1 3738, LCF 2 18098, TTI 13452, OP HRS 6200.

tony.barnes 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=

456

456

6722

447

1179

94

826063

APU

116305-302 8624564

4 456116305-302 826063AUXILIARY POWER UNIT 6722

15B 2835013692818

60206000

starts

RC RC4502902 SIF5448WHEEL, COMPRESSOR 6295 0

15B02B 2835014596002

60206000

starts

RC RC4501019 V62HD360WHEEL, TURBINE 6295 0

15B03 2835013638089

60206000

starts


For use of this form, see DA PAM 738-751; the proponent agency is DCS G-4

APD LC v1.00AUXILIARY POWER UNIT AND COMPONENT RECORDDA FORM 2408-16-2, MAR 2014

of 3

8624564HELICOPTER, 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 12 Feb 201714TM 1-1520-237-23&P14 DAY FLYABLE STORAGEENGINE RUN UP

29 Jan 2017D

A092 16 Mar 201730TM 11-6140-203-23 P30 DAY SLAB BATTERYINSPECTION (D8565/11-1)

14 Feb 2017D

A103 18 Feb 201730TM 1-1500-344-23AIRCRAFT WASH DUE 19 Jan 2017D

A110 9341.440TM 1-1520-237-PMSPMS 40 HOUR INSPECTION (ESMONLY)

9301.4H

A115 02 Feb 201730TM 1-1520-237-23&PLUBE REQUIRMENTS (ESMONLY)

03 Jan 2017D

A115 9343.640TM 1-1520-237-23&PLUBE REQUIRMENTS (ESMONLY)

9303.6H

A116 9333.4360H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE (ESM ONLY)

8973.4H

A116 15 Mar 201712H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE (ESM ONLY)

15 Mar 2016M

A117 9333.4360H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE(ESM ONLY)

8973.4H

A117 15 Mar 201712H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE(ESM ONLY)

15 Mar 2016M

A160 11 Mar 201790TM 1-1520-237-23&PESM 90 DAY CORROSIONINSPECTION

11 Dec 2016D

A210 9340.6120TM 1-1520-237-23&P120 HOUR INSPECTIONREQUIREMENTS (ESM ONLY)

9220.6H

A211 9333.4360H-60-10-AMAM-11APU OIL SAMPLE (ESM ONLY) 8973.4H

A211 15 Mar 201712H-60-10-AMAM-11APU OIL SAMPLE (ESM ONLY) 15 Mar 2016M

A213 9340.6120TB 1-1520-237-20-266ENGINE COMPRESSORCLEANING (ESM ONLY)

9220.6H

A295 9333.4360TM 1-1520-237-23&PSTABILATOR ACTUATOR ASSYLUBE (ESM ONLY)

8973.4H

A298 9333.4360TM 1-1520-237-23&PLUBE TAIL WHEEL BEARING 8973.4H

A298 12 Mar 201712TM 1-1520-237-23&PLUBE TAIL WHEEL BEARING 12 Mar 2016M

A299 9333.4360TM 1-1520-237-23&PSWASHPLATE LUBE (ESM ONLY) 8973.4H

A299 12 Mar 201712TM 1-1520-237-23&PSWASHPLATE LUBE (ESM ONLY) 12 Mar 2016M

A440 9333.4720TM 1-1520-237-23&PCLEAN TAIL WHEEL LOCKPIN 8613.4H

A470 10734.31500TM 1-1520-237-23&PREPLACE NUMBER TWOCROSSFEED VALVE

9234.3H

A471 10056.52160TM 1-1520-237-23&PREPLACE T/R SHAFT SUPPORTBEARINGS (FWD)

7896.5H

A472 10557.62160TM 1-1520-237-23&PREPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)

8397.6H

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

DA FORM 2408-18, OCT 1997 EQUIPMENT INSPECTION LIST

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

of 3




8.DUE


A473 10557.62160TM 1-1520-237-23&PREPLACE T/R SHAFT SUPPORTBEARINGS (AFT)

8397.6H

A476 10070.65000TM 1-1520-237-23&PREPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS

5070.6H

A477 10070.65000TM 1-1520-237-23&PREPLACEMENT OF STABILATORACTUATOR BOLTS

5070.6H

A480 10070.65000TM 1-1520-237-23&PREPLACE PIVOT BOLT 70400-08159-101,102,103,104

5070.6H

A485 10070.65000TM 1-1520-237-23&PREPLACE BELLCRANK BOLT70400-08159-105,106,107,108

5070.6H

A496 25 Apr 2017180TM 1-1520-237-23&PCF3BR FIRE EXTINGUISHERWEIGHT TEST INSPECTION

27 Oct 2016D

A501 07 Jul 2017180TM 1-1520-237-23&PMAIN ROTOR BLADE PRESSURECHECK

08 Jan 2017D

A502 26 Mar 2017180TM 1-1520-237-23&PINSPECT AND TEST GROUNDRECEPTACLE IAW TM 1-1500-204-23

27 Sep 2016D

A530 10 Aug 201712DA PAM 738-751AIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)

10 Aug 2016M

A532 30 Aug 201712TM 1-1500-204-23-4COMPASS SWING / RMI SWING 30 Aug 2016M

A533 26 Jun 201712TM 1-1520-237-23&PPITOT STATIC SYSTEMINSPECTION

26 Jun 2016M

A534 30 Jun 201712TM 1-1500-204-23-1FIRST AID KIT INSPECTION 30 Jun 2016M

A538 17 Aug 201712TM 1-1520-237-23&PFAT/OAT GAUGEINSPECTION/TEST

17 Aug 2016M

A553 01 Jul 201712AR 95-1ANNUAL WEIGHT AND BALANCEINVENTORY (365-1)

01 Jul 2016M

A580 17 Oct 201824TM 11-6140-203-23 PRETURN SLAB TO AVIM FORCAPACITY CHECK (EVERY 24MONTH)

17 Oct 2016M

A621 01 Jul 201724AR 95-1AIRCRAFT WEIGHING CLASS 1 01 Jul 2015M

A625 08 Nov 201860TM 11-6140-203-23 PREPLACEMENT OF SLABBATTERY (SLAB)

08 Nov 2013M

A630 01 Jul 2018114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 Jan 2009M

A633 01 Jul 2018114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #1,CARTRIDGE DODIC MH92

01 Jan 2009M

A638 01 Jul 2018114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #2,CARTRIDGE DODIC MH92

01 Jan 2009M

A640 01 Jul 2018114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE CARTRIDGE,31512AS105, 30903824-1

01 Jan 2009M

A648 15 Dec 2022180TM 1-1520-237-23&PREPLACE T/R SPRING CAPSULEASSY

15 Dec 2007M

A660 01 Aug 202172TB 9-1300-385REPLACE THRUSTEREMERGENCY RELEASE CARGOHOOK, MJ20

01 Aug 2015M




of 3




8.DUE


A665 17 Nov 201948H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215

17 Nov 2015M

A670 09 Apr 202048TM 1-1520-237-23&PCABIN TUB INSPECTION 09 Apr 2016M

A675 22 Nov 201948TM 1-1520-237-23&PFLIGHT CONTROL ROD INSP 22 Nov 2015M

A695 9333.4720H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

8613.4H

A695 06 May 201948H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

06 May 2015M

A755 17287.89000H-60-10-ASAM-11PC LINK TO SWASHPLATEBOLTS REPLACEMENT

8287.8H




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-307091

3. ENGINE SERIAL NUMBER2. ENGINE MODEL1. NOMENCLATURE

Page 1 of 1

07-Dec-2015 8624571 ENGINE REPLACED5000 107 103 198.2104629 848

04-Oct-2016 8624571 ENGINEREMOVED/REINSTALL

5000 102 96 198.7214987 845

24-Jan-2017 8624571 POST PHASE PMI 24500 106 103 198.4104989 845


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-306766

3. ENGINE SERIAL NUMBER2. ENGINE MODEL1. NOMENCLATURE

Page 1 of 1

27-Apr-2011 8524480 ENG REPL/TRACK &BLANCE

3000 109 103 198.8224065 845

26-Apr-2012 8524480 720 HOUR PMI-24000 103 100 198.2204514 845

24-Nov-2012 8524480 ENGINE REINSTALLED5000 105 104 19765040 848

18-Jul-2014 8524480 ATF 1.0 (POST PHASE)6000 99 95 198165246 841

22-May-2015 8524480 GG ROTORS REPLACED.5000 100 99 198.2165616 840

26-Aug-2015 8524480 ENGINE REINSTALLED4500 102 100 197.7165629.2 846

03-Jun-2016 8524480 720 HR INSP POST PHASE4000 104 100 197.92010058 843

03-Jun-2016 8524480 720 HR INSP POST PHASE4000 102 100 197.9205986 845

29-Oct-2016 8524480 NEW BASELINE6000 99 98 196.6126238 846

02-Dec-2008 8624514 PMI POST PHASE #116000 104 100.5 1100.142832 851

30-Oct-2009 8624514 REISNTALL OF ENG4000 106 102 199.7183259 847

29-Mar-2010 8624514 ECU REPLACEMENT4000 108 101 199.183570 848


T700 SERIES TURBINE ENGINE ANALYSIS CHECK RECORDDA FORM 2408-19-2, DEC 1991

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

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

17105 SESI

2. ORGANIZATION

CSGLD-1052

REQUIREMENT CONTROL SYMBOL(Julian)1. PERIOD ENDING DATE

Page 1 of 1

1GE-E-207851 ECD0211550452334110349272095098424018

2GE-E-306748 CAO019015555336212134326795098424018

1GE-E-306009 ECD03062438852415836183688008424021

1GE-E-306375 CAO0081060642540017183371286828424024

2GE-E-306513 CAO0075436912173213281242886828424024

1GEE-761436C LMDH7060205979345745101262957923304

1GEE-761436C LMDH7060205979345745101262957923304

2GEE767626 LMDH567032824328110062957923304

1GEE767410 LMDH1905103065099119845558223724

2GEE307957C LMDH43576063361182338845558223724

1GEE306276 ECD012633077147802762100841078223726

2GEE307093 CAO012033837100707617234641078223726


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

0

360

8636.7

8624564 9303.6 0

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

EH-60A A005-01332 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

jeanora.g.thompson17-Mar-2011NORMALROUTINE705.06853685317-Mar-2011

jeanora.g.thompson12-Dec-2011NORMALROUTINE0.07185718506-Dec-2011

donna.k.moss14-Aug-2012NORMALROUTINE359.07544754413-Aug-2012

melissa.gann18-Jun-2013ABNORMALROUTINE712.07897789714-Jun-2013

melissa.gann19-Jun-2013NOT_TESTEDOTHER0.07899789919-Jun-2013

melissa.gann01-Jul-2013NORMALLAB REQUES2.07901790128-Jun-2013

janice.m.bruce17-Sep-2013ABNORMALOTHER142.08041804116-Sep-2013

rhonda.e.jackson19-Sep-2013NORMALLAB REQUES151.08050805018-Sep-2013

olivia.d.williams18-Feb-2014NORMALROUTINE358.08257825715-Feb-2014

BASELINE0.58613.98613.931-Jul-2015

marilyn.l.jones14-Aug-2015NORMALLAB REQUES0.08636.78636.713-Aug-2015

marilyn.l.jones15-Mar-2016NORMALROUTINE340.48977.18977.115-Mar-2016

31JUL15-BASELINE POST PHASE. CN419218SEP 13 - A0AP SPECIAL REQUEST FOR CODE 'J' (DRAIN AND FLUSH AND RESAMPLE AFTER NEXT FLIGHT CYCLE) DUE TO FE FATIGUE 0.5-2 MICRONSTHROUGHOUT. FE CUTTING-1 MICRON; DIRT/SAND PRESENT AND RED OXIDES PRESENT.POST PHASE16SEP13- CHIP LIGHT18 JUN 13 - WATER19 JUN 13 - DRAINED DUE TO OIL LAB REQUEST.

9. REMARKS:

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

OIL ANALYSIS LOGDA FORM 2408-20, OCT 1997

0

360

8636.7

8624564 4479.6 8613


EH-60A A26500669 Days


HELICOPTER, UTILITY MAIN TRANSMISSION MODULE Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 1 of 1

a b

SUBMITTED

c a b



COMPONENTCHANGE

13-Aug-2015BASELINE0.53790.48613.931-Jul-2015

marilyn.l.jones14-Aug-2015NORMALLAB REQUES0.03812.78636.713-Aug-2015

marilyn.l.jones15-Mar-2016NORMALROUTINE340.44153.18977.115-Mar-2016

31 JUL 15- BASELINE, POST PHASE. CN4192

9. REMARKS:



0

360

8140.7

8624564 4986.6 9304


EH-60A A006-03133 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

mae.p.belford24-Jan-2011NORMALROUTINE6131.02671613120-Jan-2011

mae.p.belford26-Sep-2011NORMALROUTINE6487.03027648723-Sep-2011

mae.p.belford01-Jun-2012ABNORMALROUTINE6842.03382684231-May-2012

mae.p.belford07-Jun-2012NORMALLAB REQUES6845.03385684506-Jun-2012

mae.p.belford13-Nov-2012NORMALROUTINE7205.03745720509-Nov-2012

RG00082027-Aug-2013NORMALOTHER7422.03962742222-Aug-2013

RG00082025-Jun-2014ABNORMALSPECIAL7422.03962742202-Jun-2014

RG00082001-Jul-2014NORMALLAB REQUES7426.03966742626-Jun-2014

thomas.e.mitchell03-Jun-2015NORMALROUTINE359.34325.37785.801-Jun-2015

lashana.r.sasser17-May-2016NORMALBASELINE0.04680.78140.713-May-2016

13 MAY 16- BASELINE, ROUTINE POST PHASE. CN419201JUN12- ABNORMAL OIL SAMPLE. CODE C: DO NOT CHANGE OIL! SUBMIT RESAMPLE TO LAB AFTER NEXT FLIGHT CYCLE DUE TO HIGH PARTICLE.19MAY16 - OIL SAMPLE ORIGINALLY TAKEN ON THE 11MAY16, ENTER IN ERROR ON 2408-20; USAACE FT. RUCKER, AL LS027644

9. REMARKS:




Days

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


COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 1 of 1

a b

SUBMITTED

c a b



COMPONENTCHANGE

9. REMARKS:



PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN -


ACCUMULATOR 86245644288A1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 2 of 26

08-Dec-2003 DM

RR522810-Jan-2012

25.0CCAD/W0MUAAACCUMULATOR OVERHAUL1-1650-376MWO:

Priority Mnt Level


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

PIDMWODATE HRS



ANTI-ICE VALVE 8624564COMH112041. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 19 of 26

22-Jun-2011 OM

kathleen.m.jungell 26-Jun-2011

0.2USAACE, FT.RUCKER, AL

ANTI-ICE / START BLEED VALVEACTUATOR SHAFTS

H-60-11-ASAM-11MWO:

Priority Mnt Level

05-Sep-2012 OM

kathleen.m.jungell 07-Sep-2012

0.3USAACE, FT.RUCKER, AL(AFS 77)

ALL UH-60A SERIES AIRCRAFTENGINE ANTI-ICE (AISBV)

H-60-12-ASAM-10MWO:

Priority Mnt Level



REMARKS

INSTALLED WITH FAILURE CODE 381 (LEAKING) THIS AIRCRAFT IS GOING TO THE BEST PROJECT.

APD LF v1.00DA FORM 2410, JAN 97, IS OBSOLETEDA FORM 2410, MCDS

COMPONENT REMOVAL / REPAIR / INSTALL / GAIN / LOSS RECORD

For use of this form, see DA PAM 738-751; the proponent agency is DCS, G-4

SECTION I - MAINTENANCE ACTION

SECTION II - IDENTIFICATION

INSTALL REMOVE REPAIR GAIN/LOSS

5. MII 6. CAGE CODE 7. LANDINGS 8. NO. OF PREV

O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE

4. SERIAL NUMBER3. PART NUMBER2. NSN1. NOMENCLATURE

21. VERSION

d. OP HOURSc. TTIb. LCF 2a. LCF 1

17. COMPONENT CUMULATIVE COUNT / HOURS16. CONFIG CODE13. METER HRS

18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H

SECTION III - NEXT HIGHER ASSEMBLY (NHA) INSTALL / REMOVE INFORMATION

24. NHA PART NUMBER23. NHA NSN22. NHA NOMENCLATURE

25. NHA SERIAL NUMBER 26. NHA HOURS 27. START METER 28. METER HRS

31. WHEN DISCOVERED30. MALFUNCTION CODE29. HISTORY RECORDER SN

32. HISTORY RECORDER READING 33. NHA CUMULATIVE COUNT / HOURS

SECTION IV - GAIN / LOSS / REPAIR / ADMIN INFORMATION

d. OP HRSc. TTIb. LCF 2a. LCF 1d. OP HRSc. TTIb. LCF 2a. LCF 1

44. DATE

47. LOST / SHIPPED TO 48. LOCATION

45. PID AND TELEPHONE NUMBER 46. AKO USER NAME

43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL

38. ACTUAL FAILURE CODE 39. MAINTENANCE LEVEL

MWO

RECAP

40. MANHOURS 41. SRA 42. UIC

37. NEW NSN36. NEW PART NUMBER35. GAIN OR

LOSS CODE

34. INSPECTION ACTION CODES

X

W0U91T 16-Feb-2017

16-Feb-2017 MARILY 334-598-0670

4 N W0U91TF

0 0 0 0 0 0 0 9304

9304 0 0

HELICOPTER, UTILITY 1520010820686 EH-60A

8624564

0 0 0 0 0

11D01 0 0

78286 0 0 6755 0 381

B30309537B70410-02820-0541650011431226SERVO, PRIMARY MAIN ROTOR

6755

UNCLASSIFIED For Official use Only (FOUO)


REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

W0U91T 01-Feb-2017

01-Feb-2017 marily 334-598-0670

8 N W0U91TF

0 0 0 0 0 0 0 9304

9304 0 0


8624564

0 0 0 0 0

11D01 0 0

82106 0 0 1597 0 799

B30311712274000-10311650011431226SERVO, PRIMARY MAIN ROTOR

1597



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H








44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

W0U91T 08-Feb-2017

08-Feb-2017 ROSOND 334-598-0670

2 N W0U91TF

0 0 0 0 0 0 0 9304

9304 0 0


8624564

0 0 0 0 0

11D01 0 0

78286 0 0 3660 0 381

B3031529670410-02820-0541650011431226SERVO, PRIMARY MAIN ROTOR

3660



PIDMWODATE HRS



DRIVESHAFT ASSY ENGINE 8624564C845-072411. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 18 of 26

08-Aug-2005 OM

thomas.m.lilly25-Aug-2010

3.0USAACE, FT.RUCKER, AL(KJ0605)

ALL H-60 SERIES AIRCRAFT, ENGINEOUTPUT SHAFT

UH-60-05-ASAM-10MWO:

Priority Mnt Level



REMARKS

UPON INSPECTION FOUND TO BE CORRODED RB4325 6 DEC 16








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H








44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

06-Dec-2016 OW0950 334-503-2717 olivia.d.williams1

1 W0U911F

0 0 0 0 0 0 0

0 0

0 0 0 0 0

11C23 0 0

78286 0 2 0 1925 1212 170

E2330030970400-06100-0421615011417532T/R PITCH CHANGE SHAFT

1925



PIDMWODATE HRS



ENGINE ASSY, TURBINE 8624564GE-E-3067661. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 23 of 26

15-Feb-1987 OM

debra.r.chancellor24-Apr-2007

1.0CCAD, CORPC,TX 78419-5260(RH3098)

ONE TIME INSPECTION OF TORQUEFUEL DIFFER PRESSUREINDICATOR

55-2840-248-50-44MWO:

Priority Mnt Level

31-Jul-1989 OM


1.0CCAD, CORPC,TX 78419-5260(RH3098)

MODIFICATION OF GG ROTORASSEMBLY T700/701 REWORK T700ENGINES

55-2840-248-50-32MWO:

Priority Mnt Level

15-Aug-1990 OM


1.0CCAD, CORPC,TX 78419-5260(RH3098)

INSTALLATION OF SELF SEALADAPTER ASSEMBLY

55-2840-248-50-28MWO:

Priority Mnt Level

25-Jan-1991 DN


1.0CCAD, CORPC,TX 78419-5260(RH3098)

MODIFICATION OF POWER TAKEOFFDRIVE ASSEMBLY P/N 5044T27G01

55-2840-248-50-27MWO:

Priority Mnt Level

31-Mar-1993 DR


1.0CCAD, CORPC,TX 78419-5260(RH3098)

INSTALLATION OF PTO DRIVEASSEMBLY P/NS 5044T27G02 OR5056T66G02 (T700-GE-700 AND 701ENGINES)

1-2840-248-50-29MWO:

Priority Mnt Level

30-Jun-1994 OR


1.0CCAD, CORPC,TX 78419-5260(RH3098)

ONE TIME INSPECTION ANDCONVERSION OF FORMS ANDRECORDS FOR T700-GE-700, -701AND -701C SERIES GAS TURBINEENGINES

1-2840-248-20-2MWO:

Priority Mnt Level

13-May-1998 OI


1.0CCAD, CORPC,TX 78419-5260(RH3098)

ALL E/M/UH-60K/L AND AH-64AIRCRAFT, SUBJECT: T700-GE-701CENGINE ODV RELATED FLAMEOUTS


Priority Mnt Level

01-Dec-1998 OI


1.0CCAD, CORPC,TX 78419-5260(RH3098)

ALL EH/MH/UH-60L/K AND AH-64A/DAIRCRAFT, SUBJECT: T700-GE-701/701C ENGINE ODV RELATEDFLAMEOUTS


Priority Mnt Level

02-Aug-1999 FM


1.0CCAD, CORPC,TX 78419-5260(RH3098)

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


Priority Mnt Level


1.0CCAD, CORPC,TX 78419-5260(RH3098)

ALL H-60 SERIES AIRCRAFT,REROUTING OF WHITEENGINE/AIRFRAME HARNESSASSEMBLY




PIDMWODATE HRS



ENGINE ASSY, TURBINE 8624564GE-E-3067661. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 24 of 26

29-Nov-2006 OM

ASSEMBLY

Priority Mnt Level

19-Dec-2006 OM


1.0CCAD, CORPC,TX 78419-5260(RH3098)

ALL H-60 SERIES AIRCRAFT,REVISION TO UH-60-07-ASAM-01,REROUTING OF WHITEENGINE/AIRFRAME HARNESSASSEMBLY


Priority Mnt Level

13-Aug-2007 OM


1.0CCAD, CORPC,TX 78419-5260(RH3098)

ALL H-60 SERIES AIRCRAFT, MAINFUEL MANIFOLD CHAFING


Priority Mnt Level

20-Dec-2007 OM


1.0CCAD, CORPC,TX 78419-5260(RH3098)

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

debra.r.chancellor19-Sep-2008


ALL H-60 AND H-64 SERIESAIRCRAFT, SUSPECT ENGINEHARNESSES

H-60-08-ASAM-14MWO:

Priority Mnt Level

12-Jan-2009 FM

debra.r.chancellor14-Jan-2009


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

debra.r.chancellor07-Oct-2009


ALL H-60A AIRCRAFT, HAMILTON-SUNSTRAND HYDRO-MECHANICALUNITS

H-60-10-ASAM-01MWO:

Priority Mnt Level

30-Jul-2014 FM

anthony.s.speigner 31-Jul-2014

1.0USAACEHYDRO-MECHANICAL UNIT QUICKDISCOUNT PINS

H-60-14-ASAM-08MWO:

Priority Mnt Level



(ACFT HRS)

ji kgfdcba

RMVL HRSRMVL HRSCOMPO/HNOMENWUC O/HLOCATIONNSN

AND he SINCELIFE

PREVSER NO.ANDNOMENCLATURE P/N TIMEINST HRS MENT DUEREPLACINST HRSNO.COMPONENT

NOMEN REPLACE -O/H ORCOMP6.

4140013293428FAN AXIAL 70361-03005-107 D51202190 06H234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

2520 11133

311001127300506H23A

01576BEARING, AXIAL FAN 9510210SFFC3 RCRC

2520 11133

311001127300506H23A

01576BEARING, AXIAL FAN 9514210SFFC3 RCRC

APD LC v2.00EDITION MAY 1967 IS OBSOLETE For use of this form, see DA PAM 738-751; the proponet agency is DCSLOG

AIRCRAFT COMPONENT HISTORICAL RECORDDA FORM 2408-16, OCT 1991

COMPO/H OR REPLACE -

NOMENCOMPONENT NO. INST HRS

REPLAC MENT DUEINST HRS TIMEP/NNOMENCLATURE

AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND

NSN LOCATION O/HWUC NOMEN O/H COMPRMVL HRS RMVL HRS

a b c d f g ki j

Page 2 of 2


26-Aug-2014 1 RECAPPED IAW DMWR 1-4140-228 TSN 1576, O/H 1

ET2508 CCAD/WOMUAA CC TX

23-Jan-2015 1 INSTALLED ON ACFT. 8624564 AT 8613 ACFT. HRS. WITH TTSN:1576, TSO: 0, 1 PREV. O/H.

rick.r.skinner USAACE FT. RUCKER, AL.

APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991

PIDMWODATE HRS



FUEL CONTROL 8624564UDAJ03181. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 26 of 26

23-Nov-2010 OM

kathleen.m.jungell 29-Nov-2010

0.5USAACE, FT.RUCKER, AL(RJ0827)

ALL H-60A SERIES AIRCRAFT,HAMILTON STANDARD HYDRO-MECHANICAL UNITS (HMU)

H-60-11-ASAM-03MWO:

Priority Mnt Level

19-Aug-2013 FM

tony.barnes22-Aug-2013

0.5USAACE FT.RUCKER, AL.

WOODWARD HYDRO-MECHANICALUNIT (HMU) P3 TUBE.

H-60-13-ASAM-10MWO:

Priority Mnt Level



PIDMWODATE HRS



INPUT MODULE 8624564A264-004771. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 13 of 26

02-Aug-2000 OT


1.0W4GV20, NAES,LAKEHURST, NJ(GH3283)

ALL H-60 SERIES AIRCRAFT,REMOVAL OF INPUT MODULE GEARBOX ASSEMBLIESWITHPOTENTIALLY CRACKED BEVELGEARS

UH-60-00-02MWO:

Priority Mnt Level



PIDMWODATE HRS



INPUT MODULE 8624564A264-025841. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 14 of 26

02-Aug-2000 OT


1.0W4GV20, NAES,LAKEHURST, NJ(GH3783)

ALL H-60 SERIES AIRCRAFT,REMOVAL OF INPUT MODULE GEARBOX ASSEMBLIESWITHPOTENTIALLY CRACKED BEVELGEARS

UH-60-00-02MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR PRIMARY SERVO 8624564B303-117121. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 16 of 26

18-Jun-2014 DR

AE973917-Oct-2016

25.0CCADRECAPPED1-1650-381MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SHAFT EXTENDER 8624564C286-004711. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 17 of 26

22-Jan-1997 OM

thomas.m.lilly01-Feb-1997

0.5W4GV20LAKEHURS, NJ(PCW/IP2860)

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

thomas.m.lilly30-Oct-1997

0.5W4GV20,LAKEHURST, NJ(PCW/IP2860)

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



(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 A26500669 06A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

17000 25277

161501078571106A08

3363789SWASHPLATE GUIDE F4250045970351-08227-041 RCRC

3000 11613

161501110149106A13

03789HOUSING ASSY MGB F2110040370351-08110-045 RCRC

7600 16213

304001415838806A18

03789MAIN ROTOR SHAFT E2530482870351-08131-048 RCRC

12000 19905

161501497725706A19

7083789PLANETARY CARRIER ASSY A2400197670351-08175-046 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


17-May-2011 1 OVERHAULED / RECAPPED IAW DMWR 1-1615-371, TSN: 3789, TSO: 0.

AM7203 CCAD CORPUS CHRISTI, TX

23-Jan-2015 1 INSTALLED MAIN TRANSMISSION SN: A26500669, ON ACFT 8624564, AT 8613 ACFT HRS, WITH TSN: 3789.


09-Dec-2015 1 MAIN TRANSMISSION IMPENDING FILTER BYPASS BUTTON POPPED AT 8,839.8 ACFT HRS.


26-Apr-2016 1 MEC F311659 AUTHORIZATION GRANTED TO COMPLETE WP 0626 MAIN TRANSMISSION SERVICEABILITYINSPECTION. IF NO PARTICLES ARE FOUND AFTER 30/30, AUTHORIZATION IS GRANTED TO KEEP THEMAIN TRANSMISSION IN SERVICE. MAIN MOD SN: A26500669 W/TSN: 4210. ACFT. HRS. 9033.4.


27-Apr-2016 1 TRANSMISSION FILTER BUTTON POPPED @ 9033.4 ACFT. HRS. W/TSN 4210 .


08-Sep-2016 1 MAIN MOD SN: A26500669 FILTER BUTTON POPPED @ 9250.9 ACFT HRS. SERVICEABILITY COMP ANDBUTTON RESET. (1ST OCCURRENCE).

mary.b.hodge USAACE FT. RUCKER, AL


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1620012311831FWD FIXED GEAR SHOCK 70250-12051-045 BEM0194 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

9000 16543

165001125090703A01A

00PISTON, MAIN L/GEAR STR BEM245070250-12067-102 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


08-Aug-2012 1 INSTALLED FWD FIXED GEAR SHOCK SN: BEM0194 WITH TSN: 0 ON ACFT 8624564 @ 7543.0 ACFT HRS.

donna.k.moss USAACE FT. RUCKER, AL


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1620012311831FWD FIXED GEAR SHOCK 70250-12051-045 C001-02604 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

9000 11002

165001125090703A01A

30694958PISTON, MAIN L/GEAR STR P0420170250-12067-102 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


26-Jan-2008 1 WUC: 03A01 P/N: 70250-12051-045 S/N: C001-02604 M/L/G STRUT26 JAN 08 - CCAD - OVERHAULED TSN: 4958, TSO: 0, CNTRL # 299007, EL9952, A/C DATA TECH, CCADCORPC CHRISTI TEXAS 78419-5260. RECAPPED IAW DMWR 1-1620-247, CHNG 1.

vickie.l.meadows CCAD CORPC CHRITI, TEXAS 78419-5260

03-Apr-2008 1 WUC: 03A01 P/N: 70250-12051-045 S/N: C001-02604 M/L/G STRUT03 APR 09 M/L/G STRUT S/N COO1-02604 W/TTSN: 4958 INSTALLED ON ACFT 8624564 @ 5071 ACFT HRS.RJ0827, R/SPEC, USAAWC, FT RUCKER, AL.

vickie.l.meadows USAAWC FT. RUCKER, AL.


PIDMWODATE HRS



PUMP MODULE, HYDRAULIC 8624564K2977ABR1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 25 of 26

29-Jul-2005 DM

OA0102-Oct-2013

56.0CCADRECAPPED1-4320-271MWO:

Priority Mnt Level



PIDMWODATE HRS



RIGHT TIE ROD ASSY 8624564D366-016231. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 21 of 26

20-Apr-2005 FM

25-Jun-20091.0USAACE, FT.

RUCKER, AL(JT0967)

H-60 SERIES HELICOPTERS, TIEROD ASSEMBLIES


Priority Mnt Level

01-Jun-2005 FM

25-Jun-20091.0USAACE, FT.

RUCKER, AL(JT0967)

H-60 SERIES AIRCRAFT, TIE RODASSEMBLY REINSPECTION


Priority Mnt Level



SECTION I COCKPITEH-60A_BASELINE

4. EQUIPMENT CHECKLIST

8624564 EH-60A

3. AREA NAME 2. MODEL 1. SERIAL NUMBER

Page 1 of 7

1RECEIVER RADIO - R-1496A/ARN-89

U UUUUUUUU UU1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER

QTY REQNOMENCLATURE:ITEM NO

2DISPLACEMENT GYRO - CN-1314/A (9000C)

U UUUUUUUU UU1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU0

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING FOR KIT-1A/1C/TSEC - MT-3949A/U

U UUUUUUUU UU1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMMAND INSTR SYS PROCESSOR - 70600-01038-101

U UUUUUUUU UU1

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING RACK - 70600-01038-102

U UUUUUUUU UU1

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SAS AMPLIFIER - 70901-02908-104

U UUUUUUUU UU1

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO ASSEMBLY - 70600-01047-041

U UUUUUUUU UU1

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO - TRU-2A/A

U UUUUUUUU UU1

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU3

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3BATTERY FOR KY 58 - BA-1372/U

U UUUUUUUU UU0

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU0

15

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

AIRCRAFT INVENTORY RECORDDA FORM 2408-17, NOV 1991



8624564 EH-60A


Page 2 of 7

3REMOTE CONTROL UNIT (KY-58) - Z-AHP/YSEC

U UUUUUUUU UU0

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU1

17

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#2 VHF-FM ANTENNA COUPLER - 70600-01010-104

U UUUUUUUU UU0

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU0

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU1

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU2

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GLIDE SLOPE ANTENNA - 70600-01043-101

U UUUUUUUU UU1

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU1

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU0

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRE EXTINGUISHER - FR23-4-11848

U UUUUUUUU UU0

25

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2BAROMETERIC ALTIMETER - AAU-32/A

U UUUUUUUU UU2

26

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2CREW SEAT - D3801-2

U UUUUUUUU UU2

27

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2AIRCRAFT CLOCK - ABU-11A

U UUUUUUUU UU2

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU0

29

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2INTERPHONE CONTROL - C6533/ARC

U UUUUUUUU UU2

30

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8624564 EH-60A


Page 3 of 7

1RECEIVER/TRANSMITTER - RT-1115D/APN-209

U UUUUUUUU UU1

31

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU1

32

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU1

33

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL - C-10604(V)6/ARN-184

U UUUUUUUU UU1

34

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL - C-11466A/ARC-201

U UUUUUUUU UU0

35

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPARATOR SIGNAL DATA - CM482/ARC186(V)

U UUUUUUUU UU1

36

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3MOUNT - MT-6051/ARC-186

U UUUUUUUU UU3

37

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU1

38

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU1

39

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU1

40

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RADIO RETRANSMISSION PANEL -70550-01008-042

U UUUUUUUU UU1

41

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MAGNETIC COMPASS - MS17983-4

U UUUUUUUU UU1

42

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2OUTSIDE AIR TEMP INDICATOR - MS28028-1

U UUUUUUUU UU2

43

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOR WING PANEL - 70500-01152-093

U UUUUUUUU UU0

44

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOR WING PANEL - 70500-01152-094

U UUUUUUUU UU0

45

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8624564 EH-60A


Page 4 of 7

1STABILATOR/FLT CONT PNL - 70902-01070-048

U UUUUUUUU UU1

46

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU0

47

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU0

48

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT FOR ASN-132 MT-4915/A

U UUUUUUUU UU0

49

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU0

50

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1TACAN RECEIVER/TRANSMITTER RT-1159/A

U UUUUUUUU UU0

51

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ELECTRONIC SEQUENCE UNIT, 163290-100-E

U UUUUUUUU UU1

52

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RADAR DETECTION SET SIGNAL AN/APR39

U UUUUUUUU UU0

53

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU0

54

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1DISPENSER GENERAL PURPOSE AIRCRAFT M130

U UUUUUUUU UU0

55

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3SECURE SPEECH UNIT TSEC/KY-58

U UUUUUUUU UU0

56

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU0

57

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1KY-100 AIRTERM 0N616736-1

U UUUUUUUU UU0

58

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL DISPLAY UNIT C-12346/URC

U UUUUUUUU UU0

59

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER




of 7SERIAL NUMBER MODEL AREA NAME

8624564 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

eddie.l.denne1 CIV 14-Mar-2017

b. LOCATION/REMARKSCHECK NO.

6. LOCATION OR REMARKS

a. ITEM NUMBER

Nomenclature

DISPLACEMENT GYRO - CN-1314/A (9000C)

1 AIRCRAFT ARRIVED IN THIS CONFIG2

GYRO, DIRECTIONAL - CN-998/ASN-43


BATTERY FOR KY 58 - BA-1372/U


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


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


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


VHF/AM ANTENNA FILTER -70600-01012-102


VHF/AM ANTENNA FILTER -70600-01011-103


FIRST AID KIT - 6545-00-919-6650


FIRE EXTINGUISHER - FR23-4-11848


REVERSE OF DA FORM 2408-17, NOV 1991




db c


CHECK CHECK

ba ad

5. VERIFICATION

c


RECEIVER/TRANSMITTER - RT-1477/ARC-201


CONTROL - C-11466A/ARC-2011 AIRCRAFT ARRIVED IN THIS CONFIG35

ARMOR WING PANEL - 70500-01152-093


ARMOR WING PANEL - 70500-01152-094


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


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


MOUNT FOR ASN-132 MT-4915/A


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


TACANRECEIVER/TRANSMITTER RT-1159/A


RADAR DETECTION SETSIGNAL AN/APR39


IR JAMMERCOUNTERMEASURES SETAN/ALQ-144(V)






db c


CHECK CHECK

ba ad

5. VERIFICATION

c


DISPENSER GENERALPURPOSE AIRCRAFT M130


SECURE SPEECH UNITTSEC/KY-58


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


KY-100 AIRTERM 0N616736-11 AIRCRAFT ARRIVED IN THIS CONFIG58

CONTROL DISPLAY UNIT C-12346/URC



SECTION II CABINEH-60A_BASELINE


8624564 EH-60A


Page 1 of 5

1INERTIAL NAVIGATION SET - AN/ASN-141

U UUUUUUUU UU0

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BEARING, DISTANCE, HEADING INDICATOR - ID2301/U

U UUUUUUUU UU0

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MARKER BEACON ANTENNA - 70600-02011-103

U UUUUUUUU UU1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-104

U UUUUUUUU UU1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-105

U UUUUUUUU UU1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRST AID KIT - 6545-00919-6650

U UUUUUUUU UU0

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRE EXTINGUISHER - FR23-4-11848

U UUUUUUUU UU0

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CRASH AXE - 56D6221

U UUUUUUUU UU0

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HAND SET - H-250/U

U UUUUUUUU UU1

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SLAB BATTERY - D8565/11-1

U UUUUUUUU UU1

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1INTERPHONE CONTROL - C6533/ARC

U UUUUUUUU UU3

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ADAPTER FUEL DRAIN - 70307-03018-102

U UUUUUUUU UU0

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


4LOCK ASSY BLADE TIEDOWN - 70700-20369-041

U UUUUUUUU UU0

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2PLUG ASSY INTAKE - HIRSS SUPP - 70700-20515-041/042

U UUUUUUUU UU0

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU0

15

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER




SECTION II CABINEH-60A_BASELINE


8624564 EH-60A


Page 2 of 5

1PLUG ASSY APU EXHAUST - 70700-20509-041

U UUUUUUUU UU0

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER ASSY OIL COOLER - 70700-20511-041

U UUUUUUUU UU0

17

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BLADE FOLD SET - 70700-20412-011

U UUUUUUUU UU0

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER PITOT TUBE - 70700-20460-041

U UUUUUUUU UU2

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1TROOP SEATS - 70500-02151-045

U UUUUUUUU UU0

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER ENGINE INLET - 83DSCC-D006

U UUUUUUUU UU2

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PINTLE MOUNT ASSY - L/H - 70751-02023-043

U UUUUUUUU UU0

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PINTLE MOUNT ASSY - R/H - 70751-02023-044

U UUUUUUUU UU0

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU0

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU0

25

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HYD. PUMP HANDLE - 15400-50126

U UUUUUUUU UU1

26

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2EQUIPMENT LOGBOOK - MIL-D-43064

U UUUUUUUU UU1

27

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPUTER LOGBOOK

U UUUUUUUU UU0

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1WEIGHT AND BALANCE HANDBOOK - TM 55-1500-342-23

U UUUUUUUU UU1

29

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


4TIEDOWN ASSEMBLY, TOW - 70700-20433-045

U UUUUUUUU UU0

30

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8624564 EH-60A_BASELIN SECTION II CABINEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c




a. ITEM NUMBER

Nomenclature

INERTIAL NAVIGATION SET -AN/ASN-141


BEARING, DISTANCE,HEADING INDICATOR -ID2301/U


FIRST AID KIT - 6545-00919-6650


FIRE EXTINGUISHER - FR23-4-11848


CRASH AXE - 56D62211 AIRCRAFT ARRIVED IN THIS CONFIG8

INTERPHONE CONTROL -C6533/ARC


ADAPTER FUEL DRAIN - 70307-03018-102


LOCK ASSY BLADE TIEDOWN- 70700-20369-041


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


PLUG ASSY EXHAUST - HIRSS- 70700-20515-043






db c


CHECK CHECK

ba ad

5. VERIFICATION

c


PLUG ASSY APU EXHAUST -70700-20509-041


COVER ASSY OIL COOLER -70700-20511-041


BLADE FOLD SET - 70700-20412-011


TROOP SEATS - 70500-02151-045


PINTLE MOUNT ASSY - L/H -70751-02023-043


PINTLE MOUNT ASSY - R/H -70751-02023-044


ICS WALK-AROUND CORD -70602-02023-044


PORTABLE INSP. FLOODLIGHT - 15-0366-1


EQUIPMENT LOGBOOK - MIL-D-43064


COMPUTER LOGBOOK1 AIRCRAFT ARRIVED IN THIS CONFIG28

TIEDOWN ASSEMBLY, TOW -70700-20433-045






db c


CHECK CHECK

ba ad

5. VERIFICATION

c



SECTION III TRANSITION SECTIONEH-60A_BASELINE


8624564 EH-60A


Page 1 of 2

1ANTENNA, LOOP - AS-2108A/ARN-89

U UUUUUUUU UU1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2IFF ANTENNA - 70600-02010-103

U UUUUUUUU UU2

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF/AM ANTENNA 70600-03002-104

U UUUUUUUU UU1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PUMP FUEL SAMPLER - 82829/4P156-3

U UUUUUUUU UU1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPENSATOR MAGNETIC FLUX - CN-405/ASN

U UUUUUUUU UU1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS TRANSMITTER - T-611/ASN

U UUUUUUUU UU1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GPS ANTENNA 22433-40

U UUUUUUUU UU1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF AMPLIFIER COUPLER AM-7531/URC

U UUUUUUUU UU0

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER/TRANSMITTER RT-1749/URC

U UUUUUUUU UU0

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8624564 EH-60A_BASELIN SECTION III TRANSITION SECTIONEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c




a. ITEM NUMBER

Nomenclature

HF AMPLIFIER COUPLER AM-7531/URC


RECEIVER/TRANSMITTER RT-1749/URC



SECTION IV TAIL CONEEH-60A_BASELINE


8624564 EH-60A


Page 1 of 2

2VOR/LOC ANTENNA - 70600-05002-101

U UUUUUUUU UU2

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF ANTENNA 4700516-30

U UUUUUUUU UU0

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8624564 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 THIS CONFIG2


SECTION V TAIL ROTOR PYLONEH-60A_BASELINE


8624564 EH-60A


Page 1 of 2

1TROOP COMMANDER ANTENNA - 70600-06001-104

U UUUUUUUU UU1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8624564 EH-60A_BASELIN SECTION V TAIL ROTOR PYLONEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c




a. ITEM NUMBER

Nomenclature


PIDMWODATE HRS



SERVO ASSY, TAIL ROTOR 8624564B300004171. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 15 of 26

15-Jul-2005 DM

CM56705917-May-2009

39.0CCAD/W0MUAATAIL ROTOR SERVO ASSEMBLY -P/N 2227000-13 (NSN: 1650-01-125-5430); P/N 2227000-17 (NSN: 1650-01-305-6954)

1-1650-384MWO:

Priority Mnt Level



REMARKS

INSTALLED UNSERVICEABLE, WILL NOT START








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H








44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

W0U91T 16-Feb-2017

16-Feb-2017 DEAN.A 334-598-0670

4 N W0U91TF

0 0 0 0 0 0 0 9304

9304 447 94


8624564

0 0 0 456 6722

15B 0 0

55820 4 0 1179 9 374

826063116305-3022835013692818AUXILIARY POWER UNIT

1179



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

03-Jul-2014 VM4663 334-598-0670

4 W0U92AF

0 0 0 0 0 0 0 8473

8473 0


8624564

0 0 0 0 0

11D26 0 0

78286 0 0 5255 0 799

P187270902-02001-0485996013162743STABILATOR AMPLIFIER

5255



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

13-Feb-2015 GP8475 252-464-7874 gregory.payne3

4 N65923D

0 0 0 0 4 0 6295 1085

1085 20 0

AUXILIARY POWER UNIT 2835013692818 116305-302

826063

0 0 0 0 0

15B02B 0

55820 0 0 0 0 0 799

SIF544845029022835014596002WHEEL, COMPRESSOR

0



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

13-Feb-2015 GP8475 252-464-7874 gregory.payne3

4 N65923D

0 0 0 0 4 0 6295 1085

1085 20 0

AUXILIARY POWER UNIT 2835013692818 116305-302

826063

0 0 0 0 0

15B03 0

55820 0 0 0 0 0 799

V62HD36045039912835013638089WHEEL, TURBINE

0



PIDMWODATE HRS



SWASHPLATE ASSY 8624564015152-13211. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 26

02-Dec-1996 OT


1.0USAAVNC, FT.RUCKER, AL(PCW SN2938)

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


0.5USAAVNC, FT.RUCKER, AL(PCW SN2938)

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


Priority Mnt Level

12-Jun-2006 OM

thomas.m.lilly12-Jun-2006

2.0USAAWC, FT.RUCKER, AL(CC0814)

ALL H-60 SERIES AIRCRAFT,SWASHPLATE DUPLEX BEARING


Priority Mnt Level



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011997646SWASHPLATE ASSY 70104-08000-050 015152-1321 05A03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

COND COND

161501087160205A03A01

40474047STATIONARY SWASHPLATE 015152-126870104-08010-044 CCCC

11000 13917

161501357508905A03A02

00ROTATING SWASHPLATE 015152-132170104-08001-045 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


10-Aug-2004 1 WUC: 05A03A P/N: 70104-08000-050 S/N: A015152-1321 SWASHPLATE ASSEMBLY10AUG04 - INSTALLED S/P ASSY SN: 015152-1321 WITH TTSN: 0 ON 8624564 AT 2917 ACFT HRS. AFS132, SNOLIN, 2938, R/SEPC USAAVNC, FT. RUCKER.

vickie.l.meadows USAAVNC FT. RUCKER, AL.


PIDMWODATE HRS



TAIL ROTOR BLADE ASSY 8624564A009025291. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 12 of 26

14-Nov-2001 OM

marlin.e.brandon24-Apr-2010

1.0CCAD/W0MUAA(AJ3147)

H-60 SERIES, INITIAL ANDRECURRING INSPECTION OF THETAIL ROTOR FAIRING ASSEMBLY


Priority Mnt Level

27-Feb-2004 DM

marlin.e.brandon24-Apr-2009

151.0CCAD/W0MUAA(AJ3147)

TAIL ROTOR BLADE ASSEMBLY P/N:70101-11200-044 (NSN 1615-01-088-3230)

1-1615-287MWO:

Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR GEARBOX ASSY 8624564A006-031331. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 6 of 26

21-Mar-2013 FM

QC0000023-Mar-2013

5.0USAACE,FT.RUCKER,AL.

PLASTIC MEDIA BLAST (PMB) ANDOXIDE FLAKE RESIDUE

H-60-13-ASAM-04MWO:

Priority Mnt Level



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1520010820686HELICOPTER, UTILITY EH-60A 8624564 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Time Change Components Page 1 of 3

20000 17314

156001081924402C15J

112998613TAIL PYLON FITTING A3300013770209-06051-043 RCRC

5100 13713

161501450483405A01A

08613HUB, M/R ROTOR ASSY D3080022370103-08112-047 RCRC

14000 14000

161501074515105A01L

00MAIN ROTOR SHAFT EXTEND C286-0047170351-08186-043 RCRC

13000 16778

161501127738805A01T

48358613BIFILAR, M/R ROTOR ASSY 015152-0034270107-08400-046 RCRC

10000 16582

161501430278205B02

27229304TAIL ROTOR BLADE ASSY A009-0872070101-11200-043 RCRC

10000 14445

161501113818805B02

48599304TAIL ROTOR BLADE ASSY A0090252970101-31000-043 RCRC

12000 13126

161501083681206G01B

44305556O/B RETENTION PLATE (T/R) A257-0046170102-11101-042 RCRC

2520 11133

414001329342806H23

15768613FAN AXIAL D5120219070361-03005-107 01

13000 15793

156001129125607A24

57168509SAS ACTUATOR B112-0871870410-02500-049 RCRC

13000 17066

156001129125607A24

52389304SAS ACTUATOR C1120238070410-02500-049 RCRC

13000 21613

156001129125607A24

08613SAS ACTUATOR C1120392470410-02500-049 RCRC

2160 10252

161501141753211C23

19259304T/R PITCH CHANGE SHAFT E2330030970400-06100-042 12122

11000 14407

165001305695411C25

58979304SERVO ASSY, TAIL ROTOR B3000041770410-06520-046 RCRC

24400 32107

165001143122611D01

15979304SERVO, PRIMARY MAIN ROT B303-11712274000-1031 RCRC

24400 26949

165001143122611D01

67559304SERVO, PRIMARY MAIN ROT B30309537B70410-02820-054 RCRC

24400 30044

165001143122611D01

36609304SERVO, PRIMARY MAIN ROT B3031529670410-02820-054 RCRC

13000 17371

156001158968511D04

42428613AFT BELLCRANK 3450294770400-08102-045 RCRC

17000 17000

156001164416111D05

00AFT TIE ROD SUPT FITTING A391-0105070400-08112-045 RCRC

2200 10940

168001164416011D06

08740AFT TIE ROD ASSY M3921058870400-08111-042 RCRC

4400 13013

156001286887011D07

08613AFT BELLCRANK SPT ASSY 3900285770400-08117-049 RCRC

11000 19613

304001287243811D08

08613LATERAL SWASHPLATE LINK 151520473170400-08151-061 RCRC



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE




Time Change Components Page 2 of 3

11000 19613

168001221286311D09

08613LATERAL SERVO BELLCRAN F337-0501770400-08166-041 RCRC

14000 14000

156001158947511D13

00LEFT TIE ROD ASSY E344-0059670400-08115-045 RCRC

20000 25775

156001329789211D14

19717746RIGHT TIE ROD ASSY D366-0162370400-08165-043 RCRC

15000 9373

168001158965211D15

142408613FORWARD BELLCRANK M355-0046870400-08101-046 RCRC

5600 13334

156001221261911D16

07734FWD BELLCRANK SPT ASSY B367-0567370400-08162-042 RCRC



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE




Condition Change Components Page 1 of 4

COND COND

156001113021502C12D

14511442TAIL CONE FITTING B497-0097470219-05001-044 CCCC

COND COND

162001231183103A01

07543FWD FIXED GEAR SHOCK BEM019470250-12051-045 CCCC

COND COND

162001231183103A01

49585071FWD FIXED GEAR SHOCK C001-0260470250-12051-045 CCCC

COND COND

162001421089003B01

39599304SHOCK ABSORBER (TAIL) WOMUAA-31210170250-13101-044 CCCC

COND COND

165001285302405A01Z

21887185DAMPER ASSY, M/R A106-0146570106-08100-046 CCCC

COND COND

165001285302405A01Z

35659160DAMPER ASSY, M/R A1060511070106-08100-046 CCCC

COND COND

165001285302405A01Z

14118581DAMPER ASSY, M/R A1060658270106-08100-046 CCCC

COND COND

165001285302405A01Z

05015DAMPER ASSY, M/R R106-0369970106-08100-046 CCCC

COND COND

531501537465205A02H

31259101BLADE PIN, SOLID B9411689770103-08108-041 CCCC

COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

161501199764605A03A

02917SWASHPLATE ASSY 015152-132170104-08000-050 CCCC

COND COND

161501503311506A

37898613MAIN TRANSMISSION MODUL A2650066970351-08100-076 CCCC

COND COND

161501078571806A11

21281442ACCESSORY MODULE A258-0380570351-08080-043 CCCC

COND COND

1615013838992 LH06A11

05217ACCESSORY MODULE A258-0733370351-08080-045 CCCC

COND COND

1615012306218 RH06E

00INPUT MODULE A264-0258470351-08001-046 CCCC



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE





COND COND

161501241611006E

17561149INPUT MODULE A264-0047770351-08001-047 CCCC

COND COND

168001074515206F

00INTERMEDIATE GEARBOX A005-0133270357-06300-042 CCCC

COND COND

161501376508906G01

49879304TAIL ROTOR GEARBOX ASSY A006-0313370358-06600-046 CCCC

COND COND

161501524780506H04

06492DRIVESHAFT ASSY ENGINE C845-0724170361-08014-041 CCCC

COND COND

161501524780506H04

07734DRIVESHAFT ASSY ENGINE C8450923070361-08014-041 CCCC

COND COND

161501081277506H06

00SHAFT ASSY, T/R DRV SEC 1 A271-0108270361-03001-045 CCCC

COND COND

161501158951706H08

08613SHAFT ASSY, T/R DRV SEC 2 WG30057-0007670361-03009-047 CCCC

COND COND

161501158952206H09

00SHAFT ASSY, T/R SEC 3,4,5 A272-0344370361-05001-051 CCCC

COND COND

161501158952206H09


COND COND

161501158952206H09


COND COND

161501083295306H11


COND COND

161501158578806H12


COND COND

432001207722807A01

9118210PUMP MODULE ASSY, HYDR K2977ABR53023-06 CCCC

COND COND

432001207722807A01

07810PUMP MODULE ASSY, HYDR K9817ABR53023-06 CCCC

COND COND

432001207722807A01

20068613PUMP MODULE ASSY, HYDR 197994ABR70652-02300-050 CCCC

COND COND

481001102247307B05A

04842VALVE, SOLENIOD 118683213850-3-1 CCCC

COND COND

481001102247307B05A

02642VALVE, SOLENIOD 37573213850-3-1 CCCC

COND COND

165001222431607B11

27729304ACCUMULATOR 4288A3197170-5 CCCC

COND COND

168001342049608B20

12827105PANEL INDICATOR (PDU) 3444100-601561-000 CCCC

COND COND

168001342049608B20

7093634PANEL INDICATOR (PDU) 898100-601561-000 CCCC

COND COND

611501114969609A01

20735206GENERATOR 3395E28B302-8-DM CCCC



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE





COND COND

161501260074911C21

08371MIXER ASSEMBLY TMD04643748170400-02300-046 CCCC

COND COND

168001261204411D25

41158370STABILATOR ACTUATOR B292-0288570400-06641-117 CCCC

COND COND

168001571757811D25

08799STABILATOR ACTUATOR 1536DL2155M31MOD1 CCCC

COND COND

599601316274311D26

19511935STABILATOR AMPLIFIER 255370902-02001-048 CCCC

COND COND

599601316274311D26

52558473STABILATOR AMPLIFIER P187270902-02001-048 CCCC

COND COND

299501496368615A04

602809ENGINE SEQUENCING UNIT 07594504587 CCCC

COND COND

589501518878319E04B

15157893SDC - DOPPLER NAVIGATION 1055P320A002-03 CCCC

COND COND

584101245909019E05A

5008773RECEIVER-TRANSMITTER, R 1111ANSM-C-967292 CCCC

COND COND

584101245909319E05C

07965INDICATOR,HEIGHT 1249FFA3060591 CCCC

COND COND

660501503528419E06A

08658ATTITUDE HEADING REFERE 1843765100-20 CCCC

COND COND

661001490516852A

12679304AUTOMAT FLT CONT COMPU 345-2234825050-1-001 CCCC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 4 of 4Condition Change Components






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 3 of 3Time Change Components


21-Jul-2008 1 21 JUL 08 LTR DTD 23 JAN 91 FOR FT. RUCKER TRAINING FEET ONLYINCREASING TBO TIME TO 3000 RESCINDED TBO TIME NOW AT 2520. RSJ0827,R/SPEC, USSACE, FT. RUCKER, AL.


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615013765089TAIL ROTOR GEARBOX ASSY 70358-06600-046 A006-03133 06G014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

12000 20998

161501074515306G01C

04681I/B RETENTION PLATE T/R FM391170358-06612-042 RCRC

5000 9317

304001292161706G01D

00GEARSHAFT, BEVEL F320-0039070358-06620-102 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


17-Mar-2006 1 17 MAR 2006-TEST INSPECTOR- TRANSMISSION HAS BEEN "FULL LOAD TESTED" AND ACCEPTED INACCORDANCE WITH CURRENT PROCEDURES.(SIK 554)

SIK554 NO ORGANIZATION NO LOCATION

17-Mar-2006 2 17 MAR 2006-THE ABOVE LISTED COMPONENT HAS BEEN INSPECTED AND FOUND TO BE ACCEPTABLE.(ASSEMBLY INSPECTOR VERIFY). (SIK 554)

SIK554 NO ORGANIZATION NO LOCATION

21-May-2006 1 21 MAY 2006- TAIL ROTOR GEARBOX S/N: A006-03133 INSTALLED ON ACFT 8724668 AT 3460.4 ACFT HRS.TTSN: 0. (M. BELFORD 1137), USAAVNC, FT. RUCKER, AL.

mae.p.belford USAACE FT. RUCKER, L.

06-Apr-2007 1 06 APR 07 - CHIP TAIL XMSN CAUTION LIGHT ILLUMINATED. NORMAL FUZZ FOUND ON DETECTOR,CLEANED I/A/W WP 0628-00 OF TM1-1520-237-23. JT0967 R/SPEC, USAAWC, FT. RUCKER, AL.

JT0967 USAAWC FT. RUCKER, AL.

03-Jun-2015 1 CHIP TAIL XMSN REMAINS ILLUMINATED AFTER COMPLETION OF CHECK. CHECKED AND FOUNDSERVICEABLE, INSPECT CHIP DETECTOR AND NO CHIPS NOTED. TTSN: 4325.

mae.p.belford USAACE, LOWE FIELD FT. RUCKER, AL

05-Dec-2015 1 TAIL ROTOR GEARBOX SN A006-03133 CHIP DETECTOR ILLUMINATED AT 8062 ACFT HOURS. TSN: 4602.NO CHIPS OF FUZZ FOUND PER EM 0013/WP 08800. REMOVED AND REPLACED T/R CHIP DETECTOR IAWEM 0013 WP 0698 00

chelsey.p.phillips USAACE FORT RUCKER, AL

06-Feb-2017 1 MEC F320867 DENIED.

dean.a.keirn USAACE FT. RUCKER, AL.


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011417532T/R PITCH CHANGE SHAFT 70400-06100-042 E23300309 11C234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

2160 10252

311001113828811C23A

0713BRNG T/R PITCH CHG SHFT C84012187SB1162-102 RCRC

COND COND

534001094578911C23C

713713CLEVIS, ROD END E233003090531201170400-06702-041 CCCC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


14-Oct-2015 1 INSTALLED ON ACFT. 8424018 AT 8825 ACFT. HRS., WITH TTSN: 1433.

anthony.s.speigner USAACE FT. RUCKER, AL

09-Sep-2016 1 REMOVED T/R PITCH CHANGE SHAFT SN: E23300309 FROM ACFT 8424018, AT 9317 ACFT HRS, WITH TSN:1925, 2 PRIOR O/H'S, AND TSO: 1212. REMOVAL IS DUE TO BUSHING TOO LARGE (OD).

christina.l.negron USAACE FT. RUCKER, AL.

15-Mar-2017 1 SN: E23300309 T/R PITCH CHANGE SHAFT TEMP INSTALLED AS UNSERVICEABLE F/C 190.

james.r.harper SES HUNTSVILLLE


UNIT UNIQUE INVENTORY ITEMSEH-60A_BASELINE


8624564 EH-60A


Page 1 of 2

U UUUUUUUU UU 1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8624564 EH-60A_BASELIN UNIT UNIQUE INVENTORY ITEMSEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c



a. ITEM NUMBER

Nomenclature


1. NOMENCLATURE 2. MODEL 3. AIRCRAFT SERIAL ... UTILITY EH-60A 8624564 1. NOMENCLATURE 2. MODEL 3....

Documents

Transcript of 1. NOMENCLATURE 2. MODEL 3. AIRCRAFT SERIAL ... UTILITY EH-60A 8624564 1. NOMENCLATURE 2. MODEL 3....