1. nomenclature 2. model 3. aircraft serial …€¦ · date mwo pid hrs and mwo title applying or...

PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN

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

8724660EH-60AHELICOPTER, UTILITY

3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE

of 4

DR25-Jan-2007

NOORGANIZATIONNO PID

0.1 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

KR13-Apr-2001

USAACE,FT.RUCKER,AL.

80.001-Nov-2002

LILLY, THOMASM

SEALED LEAD ACID BATTERY (SLAB)SYSTEM AND RELOCATION OFUTILITY LIGHT POWER

1-1520-237-50-77MWO:

Mnt LevelPriority

DM01-Sep-1991

DYNCORP 2.001-Sep-2001

LILLY, THOMASM

IMPROVED ENGINE COWLINGRELEASE HANDLE ASSEMBLY

1-1520-237-50-64MWO:

Mnt LevelPriority

FR02-Nov-2009


0.102-Aug-2013

STALEY,JENNIFER M

SINGLE INSTALLATION OF ATTITUDEHEADING REFERENCE UNIO (AHRU)

1-1520-237-20-2MWO:

Mnt LevelPriority

DM22-Feb-1991

DYNCORP 780.002-Dec-1991

LILLY, THOMASM

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

1-1520-237-50-59MWO:

Mnt LevelPriority

DR05-Jan-2010


120.002-Sep-2010

P, GINSTALLATION OF BLUE FORCETRACKING (BFT) ON EH60HELICOPTERS

EH-60-001MWO:

Mnt LevelPriority

DR01-Jul-2008


30.002-Sep-2010

P, GINSTALLATION OF ELECTRONIC DATAMANAGEMENT SYSTEM (EDM) FORBLUE FORCE TRACKING (BFT)

RSN LSF01106MWO:

Mnt LevelPriority

DR11-Aug-2000


LILLY, THOMASM

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

1-1520-237-50-79MWO:

Mnt LevelPriority

DN01-Feb-1993


LILLY, THOMASM

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

1-1520-237-50-67MWO:

Mnt LevelPriority

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

DA FORM 2408-5, AUG 2004 EQUIPMENT MODIFICATION RECORD

PIDMWODATE HRS





of 4

DU31-May-1995


LILLY, THOMASM

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

1-1520-237-50-73MWO:

Mnt LevelPriority

DR02-Aug-2001


LILLY, THOMASM

INSTALLATION OF THE AN/ARN-123VOR/ILS RECEIVER IN UH-60 SERIESHELICOPTER RECEIVER (NSN: 5821-01-478-6865) (EIC: N/A)

1-1520-237-50-83MWO:

Mnt LevelPriority

DN31-Oct-1996


LILLY, THOMASM

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

1-1520-237-50-74MWO:

Mnt LevelPriority

DN15-Nov-1990

DYNCORP 4.011-Jan-1994

LILLY, THOMASM

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

1-1520-237-50-61MWO:

Mnt LevelPriority

DN01-Mar-1989

DYNCORP 5.011-Jan-1994

LILLY, THOMASM

INCORPORATION OF IMPROVEDTIEDOWN FITTINGS

1-1520-237-50-53MWO:

Mnt LevelPriority

DU10-Aug-1987

SIKORSKY 1.013-Nov-1987

LILLY, THOMASM

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

55-1520-237-50-46MWO:

Mnt LevelPriority

DR21-Jun-2004

NOORGANIZATION

0.013-Nov-1987

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

DN01-Oct-1988

TRACOR 12.014-Aug-1989

LILLY, THOMASM

EH-60A INSTALLATION OF AFCSINLINE FILDER

55-1520-237-55-6MWO:

Mnt LevelPriority

DN01-May-1994

DYNCORP 128.014-Mar-1994

LILLY, THOMASM

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

1-1520-237-50-66MWO:

Mnt LevelPriority



PIDMWODATE HRS





of 4

DN01-Aug-1991

DYNCORP 3.517-Jun-1990

LILLY, THOMASM

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

Mnt LevelPriority

DN15-Jan-1991

DYNCORP 15.021-Jun-1992

LILLY, THOMASM

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

55-1520-237-50-58MWO:

Mnt LevelPriority

DN15-Jan-1989

DYNCORP 11.024-Jul-1989

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

1-5945-237-50-1MWO:

Mnt LevelPriority

DR15-Jul-1985

PCW 0.526-Oct-1994

K, CMODIFICATION OF DIRECTIONALCONTROL CABLE SYSTEM (UH-60A &EH-60A HELICOPTERS) NATIONALSTOCK NUMBER (NSN) 1520-01-035-0266 & 1520-01-082-0686

55-1520-237-50-34MWO:

Mnt LevelPriority

DN23-Jan-1989

DYNCORP 0.526-Oct-1994

LILLY, THOMASM

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

55-1520-237-50-44MWO:

Mnt LevelPriority

DN30-Apr-1997

DYNCORP 52.028-Nov-2001

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

1-1520-237-50-56MWO:

Mnt LevelPriority

DN30-Jun-2004


51.128-Sep-2009

LILLY, THOMASM

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

1-1520-237-50-92MWO:

Mnt LevelPriority

DN24-Mar-1988

DYCORP 2.029-Dec-1988

LILLY, THOMASM

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

55-1520-237-50-47MWO:

Mnt LevelPriority

DM15-Nov-1989

DYNCORP 22.030-May-1990

LILLY, THOMASM

MODIFICATION OF DOWEL PINRETENTION MAIN GEARBOX

55-1520-237-50-43MWO:

Mnt LevelPriority



PIDMWODATE HRS





of 4

DN17-Jan-1989


LILLY, THOMASM

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

55-1520-237-50-52MWO:

Mnt LevelPriority

DN09-Jun-1988


E, AINCORPORATION OF STABILATORAMPLIFIER IMPROVEMENTS(INCLUDES MODIFICATION OFSTABILIZATION TEST SET) (UH-60AHELICOPTERS)

55-1520-237-50-42MWO:

Mnt LevelPriority



NUMBER PIDENTRY

ORGANIZATION LOCATION8.7.

DATE6.

REMARKS4. 5.

EH-60A 8724660HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL

Page 1 of 73

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREGERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-84-01- NOTAPPLICABLE TO THIS AIRCRAFT (PCW4663)

05-Nov-1984 1

NAVPRO

thomas.m.lilly

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-84-01-NOTAPPLICABLE TO THIS AIRCRAFT (PCW 4663)

05-Nov-1984 2

NAVPRO

thomas.m.lilly

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-84-03-APPLIES TOUH-60AAIRCRAFT SERIAL NUMBER 77-22714THROUGH 82-23671 (PCW 4663)

05-Nov-1984 3

NAVPRO

thomas.m.lilly

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/840272 DATED 5NOVEMBER 1984 UH-60A-84-APPLIES TO UH-60A AIRCRAFT SERIAL NUMBER 77-22714THROUGH 83-23895 (PCW 4663)

05-Nov-1984 4

NAVPRO

thomas.m.lilly

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-84-05-MAINTENANCEMANDATORY, RECORDING AND REPORTINGNONE. (PCW4663)

05-Nov-1984 5

NAVPRO

thomas.m.lilly

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED GYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-8406-APPLIES TO UH-60A AIRCRAFT SERIAL NUMBER 77-22714THOUGH 83-23875. (PCW4663)

05-Nov-1984 6

NAVPRO

thomas.m.lilly

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-84-07-NOTAPPLICABLE TO THIS AIRCRAFT (PCW4663)

05-Nov-1984 7

NAVPRO

thomas.m.lilly


05-Nov-1984 8

NAVPRO

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 73


05-Nov-1984 9

NAVPRO

thomas.m.lilly

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-84-10 APPLIES TOUH-60A AIRCRAFT SERIAL NUMBER 72-22714THROUGH 83-23882 - ONE TIME INSPECTIONOF WHENEVER PYLON IS FOLDED (PCW4663)

05-Nov-1984 10

NAVPRO

thomas.m.lilly

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-84-11 APPLIES TOUH-60A AIRCRAFT SERIAL (PCW4663)

05-Nov-1984 11

NAVPRO

thomas.m.lilly

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84.272 DATED 5NOVEMBER 1984 UH-60-60A-84-12 APPLIES TOUH-60A AIRCRAFT SERIAL NUMBER 72-22714THROUGH 83-23875 (PCW4663)

05-Nov-1984 12

NAVPRO

thomas.m.lilly

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/840171 DATED 5NOVEMBER 1984 UH-60A-85-17 APPLICABLETO UH-60A AIRCRAFT SERIAL NUMBER 77-22714 THROUGH 85-24405 (PCW VM4663)

05-Nov-1984 13

NAVPRO

DK237781

NAVPROSAFETY OF FLIGHT MESSAGES THAT ARENOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER A1984 UH-60A-85-16 APPLICABLETO UH-A60A AIRCRAFT SERIAL NUMBER 77-22714 THROUGH 85-24405 (PCW VM4663)

05-Nov-1984 14

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-85-14 APPLICABLETO UH-60A AIRCRAFT SERIAL NUMBER 77-22714 THROUGH 85-24405 (PCW4663)

05-Nov-1984 15

NAVPRO

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05-Nov-1984 16

NAVPRO

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NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 3 of 73


05-Nov-1984 17

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/840272 DATED 5NOVEMBER 1984 UH-60A-85-11 APPLICABLETO UH-60A AIRCRAFT SERIAL NUMBER 77-22714 THROUGH 85-24405 (PCW4663)

05-Nov-1984 18

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/840272 DATED 5NOVEMBER 1984 UH-60A-85-10 APPLICABLETO UH-60A AIRCRAFT SERIAL NUMBER 77-22714 THROUGH 85-24405 (PCW4663)

05-Nov-1984 19

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-85-09 NOTAPPLICABLE TO THIS AIRCRAFT (PCW4663)

05-Nov-1984 20

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-85-08 NOTAPPLICABLE TO THIS AIRCRAFT (PCW 4663)

05-Nov-1984 21

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-85-07 (PCW4663)

05-Nov-1984 22

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-85-06 APPLIES TOUH60A AIRCRAFT SERIAL NUMBER 77-22714THROUGH 84-24016 (PCW4663)

05-Nov-1984 23

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-85-04 APPLIES TOUH60A AIRCRAFT SERAL NUMBER 77-22714THROUGH 84-23978 (PCW4663)

05-Nov-1984 24

NAVPRO

DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 4 of 73

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-27 DATED 5NOVEMBER 1984 UH-60A-85-03 APPLIES TOUH-60A AIRCRAFT SERIAL NUMBER 77-22714THROUGH 84-23978 (PCW4663)

05-Nov-1984 25

NAVPRO

DK237781


05-Nov-1984 26

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NUMBER 77-22714 THROUGH 84-23978(PCW4663)

05-Nov-1984 27

NAVPRO

DK237781


05-Nov-1984 28

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84 AIRCRAFTSERIAL NUMBER 77-22714 THROUGH 83-23895(PCW4663)

05-Nov-1984 29

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NUMBER 84-23970 (PCW4663)

05-Nov-1984 30

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-84-13 APPLIES TOUH-60A AIRCRAFT SERAIL NUMBER 72-22714THROUGH 83-23895 (PCW4663)

05-Nov-1984 31

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-87-11 NOTAPPLICABLE TO THIS AIRCRAFT (PCWVM4663)

06-Nov-1984 1

NAVPRO

DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 5 of 73


06-Nov-1984 2

NAVPRO

DK237781


06-Nov-1984 3

NAVPRO

DK237781

NAOVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-85-02 NOTAPPLICABLE TO THIS AIRCRAFT (PCWVM4663)

06-Nov-1984 4

NAVPRO

DK237781


06-Nov-1984 5

NAVPRO

DK237781


06-Nov-1984 6

NAVPRO

DK237781


06-Nov-1984 7

NAVPRO

DK237781


06-Nov-1984 8

NAVPRO

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06-Nov-1984 9

NAVPRO

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NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 6 of 73


06-Nov-1984 10

NAVPRO

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06-Nov-1984 11

NAVPRO

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06-Nov-1984 12

NAVPRO

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06-Nov-1984 13

NAVPRO

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06-Nov-1984 14

NAVPRO

DK237781


06-Nov-1984 15

NAVPRO

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06-Nov-1984 16

NAVPRO

DK237781


06-Nov-1984 17

NAVPRO

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NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 7 of 73


06-Nov-1984 18

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-86-11 NOTAPPLICABLE TO THIS AIRCRAFT (SEE MSG UH-A60A-86-07) (PCW VM4663)

06-Nov-1984 19

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-86-10 APPLIES TOUH-60A AIRCRAFT SERIAL NUMBER 77-22714THROUGH 84.24016 (PCW VM4663)

06-Nov-1984 20

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-86-08 APPLIES TOUH-60A AIRCRAFT SERIAL NUMBER 7-22714THROUGH 86-24487 (PCW VM4663)

06-Nov-1984 21

NAVPRO

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06-Nov-1984 22

NAVPRO

DK237781


06-Nov-1984 23

NAVPRO

DK237781


06-Nov-1984 24

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60-86-04 APPLIES TOUH60A AIRCRAFT SERIAL NUMBER 77-22714THROUGH 86-24429 (PCW VM4663)

06-Nov-1984 25

NAVPRO

DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 8 of 73


06-Nov-1984 26

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-86-02 APPLIES TOUH-60A AIRCRAFT AIRCRAFT SERIAL NUMBER77-22714 THROUGH 86-24490 (PCW VM4663)

06-Nov-1984 27

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-86-01 APPLIES TOUH-60A APPLIES TO UH-60A AIRCRAFTSERIAL NUMBER 77-22714 THOUGH 85-24429(PCW VM4663)

06-Nov-1984 28

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-85-27 (PCW VM4663)

06-Nov-1984 29

NAVPRO

DK237781


06-Nov-1984 30

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MESSAGES THATARE NOT APPLICABLE LISTED/LISTED FORREFERENCE PURPOSES AS DIRECTED BYNAVPRO LTR 4855 SER QAV/84-272 DATED 5NOVEMBER 1984 UH-60A-85-25 APPLIES THUH-60A AIRCRAFT SERIAL NUMBER 77-22714THROUGH 85-24430 (PCW VM4663)

06-Nov-1984 31

NAVPRO

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06-Nov-1984 32

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DK237781


06-Nov-1984 33

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NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 9 of 73

NAVPRONOTE: SAFETY OF FLIGHT MASSAGES THATNAVPRO ARE NOT APPLICABLELISTED/LISTED FOR REFERENCE PURPOSESAS DIRECTED BY NAVPRO LTR 4855 SERQAV/84-272 DATED 5 NOVEMBER 1984 UH-60A-85-22 NOT APPLICABLE TO THIS AIRCRAFT(PCW VM4663)

06-Nov-1984 34

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MASSAGES THATNAVPRO ARE NOT APPLICABLELISTED/LISTED FOR REFERENCE PURPOSESAS DIRECTED BY NAVPRO LTR 4855 SERQAV/84-272 DATED 5 NOVEMBER 1984 UH60A-85-21 NOT APPLICABLE TO THIS AIRCRAFT(PCW VM4663)

06-Nov-1984 35

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MASSAGES THATNAVPRO ARE NOT APPLICABLELISTED/LISTED FOR REFERENCE PURPOSESAS DIRECTED BY NAVPRO LTR 4855 SERQAV/84-272 DATED 5 NOVEMBER 1984 UH-60A-85-20 SURPERSEDED BY SOF MSG UH-60A-85-21 (PCW VM4663)

06-Nov-1984 36

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MASSAGES THATNAVPRO ARE NOT APPLICABLELISTED/LISTED FOR REFERENCE PURPOSESAS DIRECTED BY NAVPRO LTR 4855 SERQAV/84-272 DATED 5 NOVEMBER 1984 UH-60A-85-18 APPLIES TO UH60A AIRCRAFT SERIALNUMBER 77-22714 THROUGH 85-24405 AND 85-24406 (PCW VM4663)

06-Nov-1984 37

NAVPRO

DK237781

NAVPRONOTE: SAFETY OF FLIGHT MASSAGES THATNAVPRO ARE NOT APPLICABLELISTED/LISTED FOR REFERENCE PURPOSESAS DIRECTED BY NAVPRO LTR 4855 SERQAV/84-272 DATED 5 NOVEMBER 1984 UH-60A-85-19 APPLIES TO UH-60A AIRCRAFT SERIALNUMBER 77-22714 THROUGH 85-24405 (PCWVM4663)

06-Nov-1984 38

NAVPRO

DK237781

D COUH-60-95-ASAM-07 (TB 1-1520-237-20-167)INSPECTION OF ALL GUNNER/TROOP SEATSATTENUATION WIRES AND ATTENUATORROLLER BEARINGS COMPLIED WITH AT ACFTHRS BY SGT WRGHT TI (JW2180)

10-Aug-1985 1

APO, AE

DK237781

D CO 2-501 AVNUH-60-98-ASAM-02 (TB1-1520-237-20-197 ALL H-60 ACFT WITH PUSHRODS PN 70400-08155-050 AND 051 MANUFACTURED BY VERSATILEMACHINING INC. CAGE CODE 65522 C/W AT1365.4 BY SGT THOMAS (JT9273)

09-Oct-1987 1

APO AE 09165

DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 10 of 73

SIKORSKYAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG. 70400-0003REV.E. SYSTEM CONTROLS HAVE B EENBIASED IN ACCORD A. AFT CONTROL SERVOINPUT ROD HAS BEEN LENGTHENED 1/2TURN B. LATERL CONTROL SERVO INPUTTURN B. LATERAL CONTROL SERVO INPUTTOD HAS BEEN SHORTENED 1/8 TURN. C.FORWARD CONTROL SERVO INPUT ROD HASBEEN SHORTENED 1/2 TURN. NOTE: WHENAIRCRAFT RIGGING IS BAISED RIGGING PINHOLES ARE TEMPORARILY LOST AT TGEABOVE 3 POINTS (PCW VM4663)

24-Oct-1987 1

STRADFORD, CT

DK237781

NAVPROWAIVER (W0075) - AUTHORIZES DELIVERY OFAIRCRAFT WITH UNQUALIFIED 70902-02001-046 STABILATOR AMPLIFIERS INSTALLED(PCW VM4663)

24-Oct-1987 2

NAVPRO

DK237781

NAVPROWAIVER (W0072R20 - AUTHORIZES DELIVERYOF AIRCRAFT WITH 70209-02136-102EYEBOLTS INSTALLED (MAINTENANCECRANE AND TIE DOWN RING MOUNTINGSYSTEM (PCW VM4663)

24-Oct-1987 3

NAVPRO

DK237781

NAVPROWAIVER(W0066) - AUTHORIZES USE OF MAINNAVPRO ROTOR SPINDLE MAIN ROTORBLADE CUFF, MAIN ROTOR HUB, MAIN ROTORCONTROL HORN AND MAIN ROTOR SHAFT,PENDING COMPLETION OF QUALIFICATIONTESTING (PCW VM4663)

24-Oct-1987 4

NAVPRO

DK237781

NAVPROWAIVER (W0060R1) - AUTHORIZES USE OFNAVPRO MAIN ROTOR SPINDLE, MAIN ROTORBLADE CUFF, MAIN ROTOR HUB, MAIN ROTORCONTROL HORN AND MAIN ROTOR SHAFT,PENDING COMPLETION OF QUALIFICATIONTESTING (PCW VM4663)

24-Oct-1987 5

NAVPRO

DK237781

NAVPROWAIVER (W0043) - AUTHORIZES USE OF ARC-186 PRIOR TO APPROVAL OFELECTROMAGNETIC COMPATIBILITY (EMC)TESTING (PCW VM4663)

24-Oct-1987 6

NAVPRO

DK237781

NAVPROWAIVER (W0037)- AUTHORIZES USE OFUNQUALIFIED ANTENNA COUPLERS AND LOWPASS FILTERS. (PCW VM4663)

24-Oct-1987 7

NAVPRO

DK237781

NAVPRONOTE: THE FOLLOWING APPLICABLEWAIVERS ARE LISTED FOR REFERENCEPURPOSSES AS DIRECTED BY NAVPRO LTR4855 SER, QAV/84-272 DATED 5 NOVEMBER1984 (PCW VM4663)

24-Oct-1987 8

NAVPRO

DK237781

NAVPROWAIVER (W0067) - AUTHORIZES DELIVERY OFAIRCRAFT WITH UNQUALIFIED COMPONENTSINSTALLED PRIOR TO COMPLETION OFQUALIFICATION TESTING. (PCW VM4663)

24-Oct-1987 9

NAVPRO

DK237781

SIKORSKYUH-60A-87-09 (55-1520-237-50-46)INSTALLATION OF CYCLIC STABILATOR SLEWSWITCH COMPLIED WITH. (PCW VM4663)

13-Nov-1987 1

STRATFORD, CT

DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 11 of 73

SIKORSKYCOMPLIED WITH THE SOF MSG UH-60A-86-21 (TB 55-1520-238-20-85) ONE TIME INSPECTIONOF CREW SEATS FOR LONGITUDINALMOVEMENT OF LOCKPIN ADJUSTMENT (PCWVM4663)

13-Nov-1987 2

STRATFORD, CT

DK237781

SIKORSKYUH-60A-84-02 ( TB 55-1520-237-20-48) ONEINSPECTION OF WIRE HARNESS ROUTINGFOR FEEDER HARDNESS B (PCW)

13-Nov-1987 3

STRATFORD, CT

DK237781

SIKORSKYUH-60A-83-12 (TB 55-1520-237-20-46)INSPECTION OF TAIL ROTOR ASSY FOR BENTSERVO VALVE INPUT STEM COMPLIED WITH(PCW VM4663)

13-Nov-1987 4

STRARFORD, CT

DK237781

SIKORSKYCOMPLIED WITH SOF MSG UH-60A 87-08UH60/EH-60A AIRCRAFT INSPECTION OF MIDSECTION BELLCRANK ASSY (PCW VM4663)

19-Nov-1987 1

STRATFORD, CT

DK237781

SIKORSKYUH-60A-87-07 (TB 55-1520-237-20-90)INSPECTION OF TWO LONGITUDINAL LINKASSY AND CLEVIS ASSY FOR CRACKEDINNER RACE (PCW VM4663)

19-Nov-1987 2

STRATFORD, CT

DK237781

TFSIALL UH-EH-60 AIRCRAFT ONE TIMEINSPECTION OF THE TAIL ROTOR GEARBOXOUTPUT SHAFT COMPLIED WITH AT 37 A/CHRS NO DEFECTS (PCW VM4663)

31-Jan-1988 1

MAHAVE, AIRPORT, CA

DK237781

SIKORSKYSOF MSG UH-60A-87-12 ONE TIMEINSPECTION OF DEFECTIVE T700-GE-700.701ENGINE POWER TURBIN MODULES COMPLIESWITH (PCW VM4663)

02-Feb-1988 1

STRATFORD, CT

DK237781

TFSIALL H-60 SERIES AIRCRAFT INSPECTION FORCERTAIN SERIAL NUMBER TAIL ROTORBLADE ASSYS COMPLIED WITH AT 37.0 ACFTHRS. EH-60 MAINT SNS FOUND A009-02930(PCW VM4663)

17-Feb-1988 1

MAHAVE AIRPORT, CA

DK237781

TFSIALL UH-EH-60 AIRCRAFT ONE TIMEINSPECTION OF THE TAIL ROTOR GEARBOXOUTPUT SHAFT COMPLIED WITH AT 37 A/CHRS NO DEFECTS (PCW VM4663)

31-Mar-1988 1

MAHAVE AIRPORT, CA

DK237781

TFSIALL H-60 ACFT LFE EXTENSION OF THE H-60ACFT MAIN MODULE SHAFT COMPLIED WITHAT 37 A/C HRS S/N A265-1326 SHAFT PN 70351-08131-046 S/N B253-01998 (PCW VM4663)

23-May-1988 1

MAHAVE AIRPORT, CA

DK237781

TFSIUH-60-88-05: ALL H-60 SERIES AIRCRAFT TFSIINITIATION OF AUXILIARY POWER UNITMAXIMUM ALLOWABLE OPERATIVE TIME(MOAT) IN TERMS OF APU OPERATING HOURSAND APU START COMPLIED WITH 66.8 HRS(PCW VM4663)

27-Jun-1988 1

MAHAVE AIRPORT, CA

DK237781

SIKORSKYMWO 55-1520-237-55/5 INSTALLATION OF 4-PROLL ABSORBER COMPLIED WITH 13JUL 88(PCW VM4663)

13-Jul-1988 1

STRATFORD CT

DK237781

B COMP 70TH TRANSUH-60-88-06 TB 55-1520-237-20-99 OVERHAULLIFE FOR TRANSMISSION OIL COOLERBLOWER CW (PCW VM4663)

21-Jul-1988 1

70TH TRANS APO NY09094

DK237781


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DATE6.

REMARKS4. 5.


Page 12 of 73

4/2 AVUM TRP ACRUH-60-88-07 REVISION OF UH-60-88-05 APU(MOAT) HURLY/START-TRACKING C/W AT 74.9ACFT HRS THIS DATE (PCW VM4663)

01-Aug-1988 1

APO NY 09092

DK237781

AVUM TRPSOF MSG UH-60A-88-07 REVISION OF UH-60-88-05 C/W THIS DATE AT 74.9 ACFT HRS (PCWVM4663)

01-Aug-1988 2

APO NY 09092-0216

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60-88-04 WAS FOUND THIS DATETO BE NOT C/W DURING REVIEW OFRECORDS. FOF MSG UH60-88-04 C/W THISAT74.9 A/C HRS. (PCW VM4663)

03-Aug-1988 1

APO NY 09092

DK127781

4/2 AVUM TRP ACRUH-60-88-08 REVISION OF UH-60-88-06 C/WTHIS DATE AT 74.9 A/C HRS. (PCW VM4663)

03-Aug-1988 2

APO NY 09092

DK237781

AVSCOM OCM SECOCM/ACE PERFORMED AT 75 AC HRS AT GEBY ACE TEAM MEMBER J (PCW VM4663)

10-Aug-1988 1

ST. LOUIS MO

DK237781

CCADSOF MSG UH-60-88-09 ONE TIME INSP OFPILOTS & CO-PILOTS SEAT CLEVIS SCREWSC/W 17 AUG 88 AT 84.3 A/C HRS (PCW VM4663)

23-Sep-1988 1

APO NY 09092

DK237781

CCADSOF MSG UH-60-88-09 ONE TIME INSP OFPORTABLE FIRE EXTINGUISHER C/W 29 SEP88 AT 129.9 ACFT HRS. (PCW VM4663)

03-Oct-1988 1

APO NY 09092

DK237781

4/2 AVUM TRPSOF MSG UH-60-88-10 NON APPLICABLE THISACFT (PCW VM4663)

12-Nov-1988 1

ACR APO NY 09092

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60-88-12 NOT APPLICABLE THISACFT (PCW VM4663)

12-Nov-1988 2

APO,NY 09092

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60-88-11 REVISION TO UH-60-86-18 FOR RAPELLING OPS C/W THIS DATE 21OCT 88 AT 141.8 A/C HRS (PCW VM4663)

12-Nov-1988 3

APO ,NY 09092

DK237781

4/2 AVUM TRP ACRSOF MSG GEN-03 REVISION TO GEN-88-02P/C/W AT 148. 3 5 OST 88, ENTERED THIS DATE(PCW VM4663)

10-Dec-1988 1

APO, NY 09092

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60-88-14 ONE TIME INSP FORMWO COMPLIANCE ON H/S HOIST N/A THISACFT (PCW VM4663)

10-Dec-1988 2

APO, NY 09092

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60-88-13 ONE TIME INSP OF M/RBLADE EXPANDABLE PIN C/W 28 NOV 88 AT148.3 A/C HRS (PCW VM4663)

10-Dec-1988 3

APO, NY 09092

DK237781

4/2 AVUMSOF MSG UH-60A-89-01 ONE TIMEINSPECTION OF T700-G-E-700 ENGINE GASGENERATOR STATOR SHROUDS, C/W 13FEB89 AT 169.1 ACFT HRS (PCW VM4663)

14-Feb-1989 1

TRP ACR APO NY 09092

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60A-89-02 CORRECTION TO SOFMSG UH-60A-89-01 C/W AT 169.1 ACFT HRS(PCW VM4663)

15-Feb-1989 1

APO NY 09092

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60A-89-03 ONE TIME INSP OF M/RSPINDLES C/W 4 APR 89 AT 194.7 A/C HRS(PCW VM4663)

04-Apr-1989 1

APO, NY

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60A-89-05 ONE TIME INSP OFWIRE STRIKE PROTECTION SYSTEM C/W 14JUN 89 AT 213.2 ACFT2 HRS (PCW VM4663)

15-Jun-1989 1

APO, NY 09092

DK237781


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DATE6.

REMARKS4. 5.


Page 13 of 73

NAVPROOCM/ACE PERFORMED AT 230 A/C HRS ATFEUCHT, GER B Y ACE TEAM MEMBER C.(PCW VM4663)

06-Jul-1989 1

NAVPRO

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60-89-04 REVISION TO ONE TIMEINSP OF ALL MAIN ROTOR SPINDLES C/W 4APR 89 AT 194.7 ACFT HRS. (PCW VM4663)

10-Jul-1989 1

APO, NY 09092

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60-89-06 ONE TIME INSPECTIONOF R/H AND L/H RELAY PANELS FORSUSPECT GROUNDING MODULES C/W 20 JUL89 AT 229.8 ACFT HRS. (PCW VM4663)

20-Jul-1989 1

APO, NY 09092

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60-89-09 CORRECTION OFRETIREMENT LIFE SCHEDULE FOR H-60RETIREMENT LIFE COMPONENTS C/W 18 AUG89 AT 249.3 ACFT HRS. (PCW VM4663)

18-Aug-1989 1

APO, NY 09092

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60-89-07 REVISION TO SOF MSGUH-60-89-06 C/W 11 AUG 89 AT 249.3 ACFTHRS. (PCW VM4663)

18-Aug-1989 2

APO, NY 09092

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60-89-08, ONE TIME INSP OF 4/2AVUM TRP ACRFUEL BOOST PUMPS C/W 18AUG 89 AT 249.3 A/C HRS. (PCW VM4663)

19-Aug-1989 1

APO, NY 09092

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60-89-10 ONE TIME INSP OF GASGENERATOR SERIAL NUMBER C/W 22 SEP 89AT 259.5 ACFT HRS. (PCW VM4663)

28-Sep-1989 1

APO,NY 09092

DK237781

4/2 AVUM TRP ACRTB 55-1520-237-20-104 NEW OVERHAULRETIREMENT LIFE SCHEDULE FOR H-60RETIRMENT LFE COMPONENTS C/W 31 OCT89AT 227.1 ACFT HRS. (PCW VM 4663)

31-Oct-1989 1

APO, NY 09092

DK237781

4/2 QVUM TRP ACRSOF MSG UH-60-89-11 ONE TIME INSP OF OILCOOLER AXIAL FAN C/W 13 NOV 89 AT 277.1ACFT HRS (PCW VM4663)

14-Nov-1989 1

APO, NY 09092

DK237781

4/2 AVUM TRP ACRDF ANTENNA INSULATOR INSTALLATION FORLIFTING OF DE-ICE RESTRICTION COMPLETED18 NOV 89 AT 277.0 ACFT HRS. (PCW VM4663)

21-Nov-1989 1

APO, NY 09092

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60-89-12 ONE TIME SN AND PNCK OF OIL COOLER ASSY C/W 28 NOV 89 AT279.6 (PCW VM4663)

28-Nov-1989 1

APO, NY 09092

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60-89-13 RESTRICTION AGAINSTUSING FITTING PN 70700-20433-045 FORRAPELLING PARACHUTING ANDTRANSPORTABILITY TIESOWN OPERATIONC/W 6 DEC 89 281.7 ACFT HRS. (PCW VM4663)

06-Dec-1989 1

APO, NY 09092

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60-90-01 ONE TIEMANDRECURRING INSPECTION OF M/R BLADEEXPANDABLE LPINS C/W 18 APR 90 AT354.7ACFT. HRS. (PCW VM 4663)

23-Apr-1990 1

LOWE AHP, FT.RUCKER, AL.

DK237781

OCM/ACEPCM/ACE PERFORMED AT 396 A/C HRS ATFEUCAT GE BY ACE TEAM MEMBER ----W---ST. LOUIS , MO (PCW VM4663)

02-Jul-1990 1

ST.LOUIS MO

DK237781

4/2 AVUM TRP ACRSOF MSG UH-60-9-0-02 ONE TIME INSPECTIONOF TAIL ROTOR PITCH BEAM RETAININGWASHER AND PITCH BEAM RETAINING NUTAND EMPHASIZED RECURRING VISUALINSPECTION C/W 15 AUG 90 AT 421.4(PCWVM4663)

22-Aug-1990 1

APO, NY 09092

DK237781


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DATE6.

REMARKS4. 5.


Page 14 of 73

H COONE TIME INSPECION OF 2408-16S FORSPINDLE ASSAMVLIES I/A/W UH-60-91-ASAM-05 AND TB 55-1520-237-20-122 COMPLIEDWITH AT 5607.1 ACFT HRS. 21 FEB 91 (PCWVM4663)

21-Feb-1991 1

APO, NY

DK237781

H CO 3RD AVNUH-60-01-ASAM-02 ( TB 55-1520-237-20-120)RECURRING ERROSION INSP OF M/R BLADESTIP CAPS (ACFT IN DESERT SHIELD) N/A THISACFT (PCW VM4663)

28-Mar-1991 1

APO, NY

DK237781

H COONE TIME INSP OF CAFGO HOOK INTERNALWIRE BUNDLE ROUTING I/A/W UH-60-91-ASAM-06 AND TB1 1520-237-20-124 N/A TO THISAIRFRAME. (PCW VM4663)

28-Mar-1991 2

APO, NY

DK237781

H COUH-60-91-ASAM-01/TB 55-1520-237-20-119 ONETIME REPLACEMENT OF T/R PITCH BEAMRETAINING NUT WASHER AND 30 HRINSPECTION (SPECIAL) COMPLETED ON 28MAR 91 AT 520.9 ACFT (PCW VM4663)

28-Mar-1991 3

APO, NY

DK237781

H COUH-60-91-ASAM-04 ( TB 55-1520-37-20-123)ACFT OPERATION IN SWA (DESERT STORM)TO PROVICE GUIDANCE FOR SITUATIONSREQUIRING EXCEEDING THE RETLIREMENT(FINITE) LIFE OF CERTAIN COMPONENTS N/ATHIS ACFT (PCW VM4663)

28-Mar-1991 4

APO, NY

DK237781

H COUH-60-91-ASAM-08/TB 1-1520-237-20-125 ONETIME INSPECTION OF FIRE EXTINGUISHERSYSTEM COMPLETED ON 3 APR 91 AT 520.9ACFT HRS. (PCW VM4663)

03-Apr-1991 1

APO, NY

DK237781

H COTB 55/1520-237-20-111. ONE TIME INSP OFUPPER PRESSURE PLATE AND SPINDLE TOHUB ATTACHMENT BOLT COMPLETED 3 APRIL91 (PCW VM4663)

03-Apr-1991 2

APO, NY

DK237781

OCM/ACEOCM/ACE PERFORMED AT 530 A/C HRS ATGIEBELSTADT, GE BY ACE TEAM MEMBER 0

03-Jun-1991 1

ST.LOUIS MO

DK237781

H COUH-60-91-ASAM-10/TB 1-1520-237-20-127 ONETIME INSPECTION AND REPLACEMENT OFMAIN LANDING GEAR, BRAKE ASSEMBLYPISTON INSULATORS COMPLETED 15 AUG 91AT 545.4 ACFT HRS. (PCW VM4663)

12-Sep-1991 1

APO, NY

DK237781

G COUH-60-92-ASAM-01/TB 1-1520-237-20-129 INSPOF DA FORM 2408-16S FOR THREE (3)UNSERVICEABLE SPINDLE ASSEMBLIESCOMPLETED 13 JAN 92 AT 570.3 ACFT HRS(PCW VM4663)

17-Jan-1992 1

APO, NY

DK237781

H COUH-60-91-ASAM-09/TB 1-1520-237-20-126CHANGE TO INSPECTION PROCEDURES FORM/R SPINDLES AND ELASTOMERIC BEARINGSCOMPLIED WITH 29 MAY 91 AT 529.7 ACFT HRS(PCW VM4663)

17-Jan-1992 2

APO, NY

DK237781

C CO 7/227 AVN REGTUH-60-93-ASAM-08 PITCH BIAS TAIL ROTORRIGGING THREE DEGRESS COMPLIED AT689.4 ACFT HRS (PCW VM4663)

19-Jan-1992 1

APO AE 09165

DK237781

C CO 7-227 AVN REGTACCEPTED ACFT FROM B CO 790TH TRANSBN (AVIM) AT 573.8 ACFT HRS 26FEB 92 (PCWVM4663)

26-Feb-1992 1

APO NY 09165

DK237781


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DATE6.

REMARKS4. 5.


Page 15 of 73

OCM/ACEOCM/ACE PERFORMED AT 622.0 ACFT HRS ATHANAU , GE BY ACE TEAM MEMBER ----A----(PCW VM4663)

12-Jun-1992 1

ST.LOUIS, MO

DK237781

C CO 7/227TH AVNREGT

ONE TIME INSPECTION OF MR BLADEEXPANABLE PINS COMPLIED ON 25 AUG 92 AT955.9 ACFT HRS (PCW VM 4663)

19-Aug-1992 1

APO AE 09165

DK237781

C CO 7/227 AVN REGTUN-60-92-ASAM-06 ONE TIME INSP FORPROPER HARDWARE ON THE PEDALADJUSTER ASSY COMPLETED 649.2 ACFTHRS 07 OCT 92 (PCW VM4663)

07-Oct-1992 1

APO AE 09165

DK237781

C CO7/227 AVN REGTUH-60-93-ASAM-01 ONE TIME OPERATIONALCHECK OF THE TRANSMISSION ANDGEARBOX CHIP DETECTOR SYSTEMCOMPLIED AT 658.7 ACFT HRS (PCW VM4663)

07-Oct-1992 2

APO AE 09165

DK237781

C CO 7/227 AVN REGTONETIME INSP OF COLLECTIVE BIAS TUBEINSTALLATION I/A/W AN=MSAT-I-LEAN ATCOMUH-60 LAR DATE 05 NOV 92 COMPLETED 07NOV 92 AT 665.3 ACFT HRS (PCW VM4663)

07-Nov-1992 1

APO AE 09165

DK237781

C CO 7/227TH AVNUH-60A-93-ASAM-11 ONE TIME INSPECTIONOF PILOTS BUCKLE & CROTCH STRAP ASSYCOMPLIED WITH 740.3 ACFT HRS SSGMARTINEZ P (PM0823)

15-Apr-1993 1

APO AE 09165

DK237781

C CO 7/227TH AVN REGTUH-60A-93-ASAM-10 ONE TIME INSPECTIONOF ESSS VALVES & PNEUMATIC LINESCOMPLIED WITH @ 740.3 ACFT HRS SSGMARTINES P (PM0823)

15-Apr-1993 2

APO AE 09165

DK237781

C CO 7/227TH AVNREGT

UH-60A-93-ASAM-09-ONE TIME INSPECETIONTO DETERMINE COMPLAINCE WITH SYSMWO'S COMPLIED WITH @ 740.3 ACFT HRSSSG MARTINEZ P (PM0823)

15-Apr-1993 3

APO AE 09165

DK237781

C CO 7/227TH AVN REGTLATE ENTRY: UH-60A-93-ASAM-08 PITCH BIASON TAIL ROTOR RIGGING THREE DEGREESCOMPLIED AT 743.3 ACFT HRS ON 22 APR 93SSG MARTINEZ P DIMENSION (INCHES)BEFORE BIAS AFTER BIAS DIFFERENCE BLK:3.97/4.29/.320, BLU: 3.99/4.32/.330, YLL;4.59/4.92..330 RED:4.62/4.93/.310 (PM0823)

23-Apr-1993 1

APO AE 09165

DK237781

C CO 7/227TH AVN REGTUH-60-93-ASAM-12 COMPLIED WITH ACFT HRS743.3 SSG MARTINEZ PEDRO (DR4202)

23-Apr-1993 2

APO AE 09165

DK237781

C CO 7/227TH AVN REGTBRIEFING OF UH-60-93-ASAM-13 COMPLIED AT755.0 ACFT HRS 8 JUN 93 SSG MARTINEZ P(PM0823)

08-Jun-1993 1

APO AE 09165

DK237781

C CO 7/227TH AVNUH-60-93-ASAM-14 INSPECTION OF ERFSEJECTOR RACKS COMPLETED AT ---ACFTHRS BY (DR4202)

18-Jun-1993 1

APO AE 09165

DK237781

C CO 7/227TH AVN REGTUH-60-93-ASAM-16 ONE TIME INSPECTION OFHYDRAULIC PUMP MODULE KNORLEDBLEED/RELIEF KNOB SCURING PIN COMPLIED778.6 ACFT HRS BY: SSG NARK P. ABARE(DR4202)

02-Aug-1993 1

APO AE 09165

DK237781

C CO 7/227 AVN REGTUH-60-94-ASAM-01 NVG COMPATIBILTY OFMASTER WARNING PANELS. COMPLIED AT834.3 ACFT HRS (RS3214)

17-Nov-1993 1

APO AE 09165

DK237781


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DATE6.

REMARKS4. 5.


Page 16 of 73

C CO 7/227 AVN FEGTUH-60-94-ASAM-03 REFURBISHMENT OF MAINROTOR SPINDLE AND THRUST BEARINGSCOMPLETED AT 841.5 ACFT HRS C/W 12 OCT981.2 ACFT HRS( RS 3214)

13-Jan-1994 1

APO AE 09165

DK237781

C CO 7/227 AVN REGTUH-60-94-ASAM-02 BUCKLE/CROTCH ASSYCOMPLIED AT 839.5 ACFT HRS (RS3214)

13-Jan-1994 2

APO AE 09165

DK237781

C CO 7/227 AVN REGTUH-60-94-ASAM-04 ONETIME INSP OF T/RPITCH BEAM ASSY COMPLETED AT 847.3ACFT HRS (RS3214)

02-Feb-1994 1

APO AE 09165

DK237781

C CO 7/227 AVN REGTUH-60-94-ASAM-06 COCKPITSTANDARDIZATION OF PILOT AND COPILOTRESTRAINT SYSTEM COMPLETED AT 851.3ACFT HRS

11-Feb-1994 1

APO AE 09165

DK237781

C CO 7/227 AVN REGTUH-60-94-ASAM-05 REPLACEMENT OF THE T/RGEAR BOX WITH -101 OUTPUT SHAFT ASSYCOMPLETED AT 851.3 ACFT HRS (RS3214)

11-Feb-1994 2

APO AE 09165

DK237781

C CO 7/227 AVN REGTUH-60-94-ASAM-07 CHANGE TO OVERHAULAND RETIREMENT TABLE AND CORRECTIONOF HISTORICAL RECORDS COMPLETED AT865.8 ACFT HRS(RS3214)

07-Mar-1994 1

APO AE

DK237781

C CO 7.227 AVN REGTUH-60-94-ASAM-08 REVISION OF ASAM 07 TOBE COMPLIED WITH BY 20 APR 94 OR 893.2ACFT HRS (RS3214)

06-Apr-1994 1

APO AE 09165

DK237781

C CO 7/227TH AVNUH-60-94-ASAM-09 REMOVAL OF CERTAINPRIMARY SERVOS ASSY COMPLTED AT 893.2ACFT HRS (RW3928)

06-Apr-1994 2

APO AE 09165

DK237781

C CO 7.227 AVN REGTUH-60-94-ASAM-10 REVISION TO UH60-940ASAM-03 COMPLETED AT 923.7 ACFT HRS(RW3928)

12-Apr-1994 1

APO AE 09165

DK237781

C CO 7.227 AVN REGTUH-60-94-ASAM-11 MAIN ROTOR BLADE DEICEMAT RESISTANCE MEASUREMENTS TESTMETHOD. COMPLETED AT 923.7 ACFT HRS(RW3928)

13-Apr-1994 1

APO AE 09165

DK237781

C CO 7/227 AVN REGTUH-60-94-ASAM-12 AUTHORIZATION FOR UH-60 AIRCRAFT TO BE UTILIZES FOR EXTERNALLOAD OPERATION LIMITED A MAXZIMUM 9000POUND STATIC WEIGHT AND ACORRESPONDING MAXIMUM EXTERNAL LOADOPERATION GROSS WEIGHT OF 23000POUNDS. DOES NOT APPLY TO THIS ACFT(RW3928)

11-Jul-1994 1

APO AE 09165

DK237781

C CO 7/227 AVNOCM/ACE PERFORMED AT 988 ACFT HOURSBY ACE TEAM MEMBER L AVSCOM OCMSECST. LOUIS MO THIS RECORD WAS BROUGHTFORWARD FROM HAND WRITTEN ENTRIESACFT HOUR BELIEVED TO BE INCORRECT(MM2015)

05-Aug-1994 1

HANAU GERMANY

DK237781

A CO 70TH TRANENGINE LIFE IMPOSED ON CERTAINCOMPONENTS I/A/W TB 1-2840-248-20-18DATED 31 MAY 1994 COMPLIED WITH (MN2015)

04-Oct-1994 1

MANHEIM GERMANY

DK237781

A CO 70TH TRANSUH-60-95-ASAM-02 REQUIREMENT TOOPERATE FUEL BOOST PUMPS DURNING ALLFROUND AND FLIGHT OPERATIONS WITH ALLTYPES OF FUEL

05-Oct-1994 1

MANHEIM GERMANY

DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 17 of 73

A9/227TH ASBTB1-2840-248-20-18 DATED 31 MAY 1994 LIFELIMITS FOR T700/701 ENGINE COMPONENTSCOMPLIED WITH (MM2015)

06-Oct-1994 1

HANAY GERMANY

DK237781

A CO 9/227TH ASBUH-60-95-ASAM-01 AERIAL RECOVERY USINGFORWARD FUSELAGE MOUNTED TIRDOWNPOINTS. ESSS HARD POINT ACFT COMPLIEDWITH 07 OCT 94 (MM2015)

07-Oct-1994 1

HANAU ARMY AIRFIELD

DK237781

A CO 70TH TRANSPHASE #2 COMPLETED AT 981.2 ACFT HOURSPHASE #3 DUE AT 1481.2 ACFT HOURS(MM2015)

18-Oct-1994 1

MANHEIM GERMANY

DK237781

A CO 70TH TRANSUH-60-95-ASAM-02 REQUIREMENT TOOPERATE FUEL BOOST PUMPSCONTUNUOUSY WITH ALL TYPES OF FUELCOMPLIED WITH (MM2015)

18-Oct-1994 2

MANHEIM GERMANY.

DK237781

A CO 9/227TH ASBUH-60-95-ASAM-03 INSPECTION OF T/R PIVOTBEARINGS AND RE-SHIM OF CERTAIN T/RBLADES COMPLIED WITH THIS DATE (MM2015)

02-Nov-1994 1

HANAU GERMANY

DK237781

A CO 9/227TH ASBUH-60-95-ASAM-04 INSP OF FLIGHT CONTROLPIVOT BOLTS. C/W THIS DATE (MM2015)

16-Nov-1994 1

APO AE 09165

DK237781

A CO 9/227TH ASBUH-60-95-SOF-01 INSP OF AND REPLACEMENTOF T/R G/B W/ OUTPUT SHAFT PN -101 INSP31MAR95) REPLACEMENT DUE NLT 1183.2ACFT HOURS OR 31 DEC 95 (MM2015)

01-Dec-1994 1

APO AE 09165

DK237781

SIKORSKY ACFTUH-60-95-SOF-01 ULTRASONIC INSP OF T/RG/B WITH P/N 101 OUTPUT SHAFT C/W THISDATE (PASSED) G/B DUE REPLACEMENT AT1183.9 ACFT HRS OR 31 DEC 95 (MM2015)

11-Jan-1995 1

APO AE

DK237781

A CO 9/227TH ASBUH-60-95-ASAM-05 RETIREMENT LIFECHANGE OF CERTAIN PN SERBEAM RAILISAND INSP OF THEIR BARREL NUTS (MM2015)

30-Jan-1995 1

APO AE 09165

DK237781

D COSAFETY OF FLIGHT, UH-60-95-SOF-02 ALLEH/UH/WH-60 A/L AIRCRAFT CHANGE TORETIREMENT LIFE FOR CERTAIN MAIN ROTORBLADE CUFFS (UH-60-1-1520-237-20-161)(PW3928)

15-Feb-1995 1

APO, AE

DK237781

D COONE TIME INSPECTION FOR CRACKED MAINTRANSMISSION BEAMS, UPPER DECK SKINCRACKS, AND FRAME CRACKS ANDIMPLEMENTATION OF A RECURRING 100HOUR INSPECTION COMPLETED AT 1008.2ACFT HOURS ON 28 JUN 1995 IAW UH-60-ASAM-06 (TB 1-1520-237-20-168) A. ESSELMANSSG (AE4964)

28-Jun-1995 1

APO, AE

DK237781

D COONE TIME INSPECTION TO REMOVE SUSPECTTAIL ROTOR PITCH CHANGE SHAFTSACCOMPLISHED ON 20 SEP 95 AT 1045.7 ACFTHRS IAW TB 1-1520-237-20-166 A. ESSELLMAN,SSG (AE4964)

20-Sep-1995 1

APO, AE

DK237781

D COUH-60-95-ASAM-08 GAS GENERATOR TURBINEROTOR BLADE INFORMATION COMPLIEDWITH AT ACFT HRS ON 22 SEP 95 BY SGT J.WRIGHT TI. (JW2180)

25-Sep-1995 1

APO, AE

DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 18 of 73

D COUH-60-96-ASAM-01 REPLACEMENT OFSPECIFIC PIVIOT BOLTS AND NUTS FOR ALLEH/UH/WH-60L AND WH-60K ACFT. DOES NOTAPPLY TO THIS ACFT. BY SGT J WRIGHT TI ATACFT HRS (JW2180)

20-Oct-1995 1

APO, AE

DK237781

D COCHANGE TO RETIREMENT LIFE OF FORWARDBELLCRANK ASSY COMPLETED IAW UH-60-SOF-96-01 (TB 1-1520-237-20-172) AT 1064.3ACFT HRS ON 06 NOV 95. J. ANDUJO, SSG(JA9937)

06-Nov-1995 1

APO, AE

DK237781

D COUH-60-96-SOF-02 ONE-TIME INSPECTION FORSUSPECT T/R INBOARD RETENTION PLATESCOMPLETED ON 27 NOV 95 AT 1068.0AIRCRAFT HOURS, (TB 1-1520-237-20-173). A.ESSELLMAN, SSG (AE4964)

28-Nov-1995 1

APO, AE

DK237781

D COUH-60-96-SOF-03 (TB 1-1520-237-20-174)CHANGE IN RETIREMENT LIFE OF CERTAINMAIN ROTOR BLADE CUFFS COMPLIED WITHAT 1069.3 ACFT. HRS ON DEC 95 BY SGTJAMES P WRIGHT TI. (JW2180)

07-Dec-1995 1

APO, AE

DK237781

D COUH-60-96-SOF-04 ONE-TIME INSPECTION OFAIRCRAFT RECORDS FOR SUSPECT AFTBELLCRANK SUPPORTS COMPLIED WITH AT1070L7 AIRCRAFT HOURS, ON 13 DEC 95(DA6661)

13-Dec-1995 1

APO, AE

DK237781

D COUH-60-96-ASAM-04 (TB 1-1520-238-20-176)REVISION OF FIRES SYSTEM AIRWORTHINESSRELEASE; N/A TO THIS (JW2180)

14-Mar-1996 1

APO, AE

DK237781

D COLATE ENTRY UH-60-96-ASAM-02 ONE TIMEINSPECTION AND REMOVAL OF SUSPECTMAIN ROTOR SHAFT NUT BOLTS COMPLIEDWITH 05 DEC 95 AT 1069.3 ACFT HRS J.(JW2180)

18-Apr-1996 1

APO, AE

DK237781

D COUH-60-96-ASAM-05(REVISED TB 1-150-237-20-D CO 7/227TH AVN 172) RECORDS CHECK FORINSTALLATION OF FWD VELLCRANKSUPPORT ASSY S/N 1316 HMW1 THRU 1316HMW560 RETIREMENT LIFE CHANGED TO 1800HRS C/W AT 1279.4 ACFT HRS (DA6661)

14-Jul-1996 1

APO, AE

DK237781

D COUH-60-96-ASAM-08 (TB 1-1520-237-20-178) ALLH-60 SERIES ACFT INCREASED FATIQUE LIFEOF CERTIAN TAIL ROTOR INBOARDRETENTION PLATED N/A THIS ACFT AT 1314.7ACFT HOURS ON 26 AUG 96 SGT J. WRIGHT TI(JW2180)

26-Aug-1996 1

APO, AE

DK237781

D COUH-60-96-ASAM-06 INFORMATIONAL, ALL H-60SERIES ACFT RITERATES TB 1-1520-237-20-143/UH-60-93-ASAM-12 UH-60A MAIN ROTORSPINDLE CRACK AT 1314.7 (JW2180)

26-Aug-1996 2

APO, AE

DJ237781

D COUH-60-96-ASAM-07 (TB 1-1520-237-20-179/TB 1-1520-250-20-4) ONE TIME RECORDS CHECKFOR CERTAIN INSTALLED SPINCLERETENTION RODS COMPLIED WITH AT 1314.7ACFT HOURS ON 26 AUF 96 BY SGT J. WRIGHTTI (JW2180)

26-Aug-1996 3

APO, AE

DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 19 of 73

D COAWR DATED 1 JUN 95 AUTHORIZATION TOOPERATE ALL UH-60A/L /EH-60A AIRCRAFTWITH THE RT1518/ARC-164 H QII RADIOINSTALLED C/W AT 1323.8 ACFT HRS BY SSGD. ALEXANDER (DA6661)

26-Aug-1996 4

APO, AE

DK237781

D CO 2/501 AVN REGTUH-60-97-ASAM-02 (TB 1-1520-237-20-184)VISUAL INSPECTION OF T/R D/S FLEXCOUPLINGS FOR PROPER CONNECTION ANDINSTALLATIONS OF AHRDWARE C/W AT 1323.1ACFT HRS (RC3061)

06-Nov-1996 1

APO AE 09165

DK237781

D CO 2/501 AVN REGTUH-60-97-SOF -01 (TB 1-1520-237-20-185)HISTORICAL RECORDS REVIEW FOR CERTAINM/R SWASHPLATE SERIAL NUMBERS C/W AT1326.4 ACFT HRS BY SGT R CITARELLA(RC3061)

04-Dec-1996 1

APO AE 09165 HANAUGE

DK237781

D COUH-60-97-ASAM-01(TB 1-1520-237-20-181)INSPECTION OF M/R HUB ASSY FOR PROPEREDGE BREAK AT THE 11 O-CLOCK DAMPERATTAACHMENT POINT C/W AT 1326.4ACFTHRS (RC3061)

12-Dec-1996 1

APO, AE

DK237781

OCM SECTIONOCM/ACE PERFORMED AT 1326.4 ACFT HRSAT HANAU GERMANY (AB6076)

18-Dec-1996 1

ST.LOUIS, MO

DK237781

D CO 2/501 AVN REGTUH-60-97-ASAM-03 (TB 1-2840-248-*20-19) ALLUH-60A/E H-60A AIRCRAFT WITH T700-GE-700ENGINES, REPLACEMENT OF DAMPEDNEDGAS GENERATOR ROTOR/STATOR ASSY C/WBY SFT J. WRIGHT AT 1326.4 ACFT HRS 27DEC 96 (JW2180)

06-Jan-1997 1


DK237781

D CO 2/501 AVN REGTUH-60-97-ASAM-04 (TB 1-1520-237-20-186)INCREASE IN RETIREMENT LIFE OF CERTAINMR BLADE CUFF C/W AT 1326.4 ACFT HRS(DA6661)

07-Jan-1997 1


DK237781

D COUH-60-97-ASAM-05(TB 1-1520-250-23-1) ONETIME INSPECTION OF ALL VISCOUS DAMPERBEARING SUPPORT ASSYS C/W AT 1326.4ACFT HRS ON 10 JAN 97 BY SGT. J. WRIGHT TI(JW2180)

10-Jan-1997 1

HANAU, GE

DK237781

D CO 2/501 AVN REGTUH-60-97-ASAM-06 (TB1-1520-237-20-189)DECREASE IN RETIREMENT LIFE OF CERTAINLATERAL ABELL CRANKS C/W AT 1326.4 ACFTHRS BY SSG J MITSCH (JM1943)

10-Jan-1997 2


DK237781

D CO 2/501 AVN REGTUH-60-97-ASAM-08 (TB 1-1520-237-20-187) ONETIME VISUAL INSP OF CEONNECTING LINK PN70400-08155-056 CW AT 13263.4 ACFT HRS BYD. ALEXANDER (DA6661)

13-Jan-1997 1


DK237781

D CO 2/501 AVN REGTUH-60-97-ASAM-07 (TB A-1520-237-20-188) ONETIME INSPECTION OF T/R SERVO ASSY FORREPLACEMSNT C/W AT 1326.4 ACFT HRS BYSSG. G. DAVIS (GD8614)

15-Jan-1997 1


DK237781

D CO 2/501 AVN REGTUH-60-97-ASAM-09 (TB 1-1520-237-20-190-(TB1-1520-250-20-15) ONE TIME VISUAL INSPECTIONOF MAIN ROTOR SHAFT EXTENSION FORCERTAIN DAGE CODE/SER # C/W AT 1326.4HRS ON 03 FEB 97 BY SGT J. WRIGHT TI(JW2180)

05-Feb-1997 1

APO AE 09165

DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 20 of 73

D CO 2/501 AVN REGTUH-60-97-ASAM-10 (TB 1-1520-237-20-191)RETIREMENT LIFE FOR CERTAIN SER # MAINSUPPORT BRIDGE ASSY C/W AT 1326.4 ACFTHRS (DA6661)

21-Feb-1997 1


DK237781

D CO 2/501 AVN REGTUH-60-97-*ASAM-11 (TB 1-1520-237-20-192)RETIREMENT LIFE INCREASED FOR THE MAINROTOR BLADE CUFF C/W AT 1331.8 ACFT HRS(DA6661)

18-Mar-1997 1


DK237781

D COMIM-GEN-97-02 ADVISORY MSG OFR VSWRADJUSTMENT ON AN/APX-100(V) IFFTRANSPONDER ENTERED BY SSG J. MITSCHTI (JM1943)

04-Apr-1997 1

APO, AE

DK237781

D COUH-60-MIM-97-01 ADVISORY MSG FORMANUAL CHANGE TO THE 30HR SPECIALINSP OF ENG OUTPUT SHAFT P/N 043ENTERED BY SSG J. MITSCH T. I. (JM1843)

04-Apr-1997 2

APO, AE

DK237781

D COUH-60-MIM-97-02 ADVISORY MSG FORMANUAL CHANGE TO THE STABILATORACTUATOR ASSY REPAIR PROCEDURESENTERED BY SSG J. MITSCH T.T. (JM1943)

04-Apr-1997 3

APO, AE

DK237781

D COSOUM-ATCOM-97-02 ADVISORY MSG FOEAIRCRAFT REFUEL NOZZLES CCRMANUFACTURED BY CARTER GROUNDREFUEL COMPANY ENTERED BY SSG J.MITSCH T.I. (JM1943)

04-Apr-1997 4

APO, AE

DK237781

D COINFORMATION MSG FOR ALL ARMY ACFTUSING AN/AVS-7 SYSTEMS N/A THIS ACFT BYSSG. J. MITSCH T.I. (JM1943)

04-Apr-1997 5

APO, AE

DK237781

D CO 2/501 AVN REGTGEN-97-ASAM-02 ALL ACFT W/HYDRA 70ROCKET SUSPESION CLARIFICATION N/A THISACFT BY SSG J. MITCH TI (JM1943)

04-Apr-1997 6


DK237781

D CO 2/501 AVN REGTGEN-ASAM-97-03 ALL H-60 ACFT CHANGE OFPROCEDURES FOR LOADING THECRYPTODEYS IN NAVSTAR AN/ASN-147 GPSRECEIVERS NA TO THIS AIRCRAFT BY JMITSCH SSG TI (JM1943)

04-Apr-1997 7


DK237781

2-501 AVN REGTUH-60-97-ASAM-12 RESTORATION OF SERVICELIFE OF THE T/R INBOARD RETENTIONPLATES P/N 70358-06612-042 MFGBY FEEN N/ATHIS ACFT (JM1943)

28-Apr-1997 1

APO AE 09165

DK237781

D COUH-60-97-ASAM-13 (TB 1-1520-237-20-194) ALLH-60 ACFT ONE-TIME INSP OF M/R SPINDLESPHERICAL ELASTBEARINGS FOR INNERSLEEVE BEARING P/N SB 5203-202 C/W AT1335.5 ACFT HRS BY SSG J. MITSCH T.I.(DA6661)

09-Jun-1997 1

APO, AE

DK237781

D COUH-60-97-ASAM-16 ALL H-AA60 ACFT WITHSWASHPLATE LINKAGE CLEVIS CONNECTORP/N 70400-08151-050 MANUFACTURED BYAIRBORNE APPAREL CAGE CODE 2A622 C/WAT 06 AUG 97 BY SGT J. THOMAS T.I. 1345.4ACFT HRS (JT9273)

06-Aug-1997 1

APO AE

DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 21 of 73

D COUH-60-97-ASAM-15 ALL H-60 ACFT WITHBEARING ROD ENDS P/N 70101-08202-101MANUFACTURED BY ISLAND ENGINEERINGCAGE CODE 40137 C/W AT 06 AUG 97 AT1345.4 ACFT HRS BY SGT J. THOMAS T.I.(JT9273)

06-Aug-1997 2

APO, AE 09165

DK237781

D CO 2/501 AVN REGTU-60-97-ASAM-14, ALL H-60 ACFT WITHBELLCRANK SUPPORT PN 70400-08158-101MANUFACTURED MY AMERICA QN GENEREALCAGE CODE 1W160 C/W AT 06 AUG 97 1345.4ACFT HRS BY BY SGT J. THOMAS (JT9273)

06-Aug-1997 3

APO AE 09165

DK237781

ATCOM OLR/MWOBRANCH

JACE/INSPECTION PERFORMED AT 1347.4 ACHOURS AT HANAU GERMANY BY TEAMMEMBERS LAST FOUR OF PID UNREADABLEON HAND WRITTEN RECORDS (ME 0000)

27-Aug-1997 1

ST OUIS M.O

DK237781

D CO 2-501 AVNUH-60-97-ASAM-18 (TB 1-1520-237-20-201)VISUAL CK OF THE SWASHPLATE ASSY CW AT1352.3 ACFT HRS (DA6661)

15-Sep-1997 1

APO AE 09165

DK237781

D CO 2-501 AVNUH-60-97-ASAM-19 (TB 1-1520-237-20-204) ONETIME INSP OF ALL AN/AVS-7 SYSTEMS TOVERIFY INSTALLATION OF THE CORRECTPOWER SUPPLY COMPONENT NA THIS ACFTACFT HRS (DA6661)

02-Oct-1997 1

APO AE 09165

DK237781

D CO 2-501 AVNUH-60-98-ASAM-01 INCREASE IN RET. LIFE OFSHAFT EXTENTION WITH P/N 70351-08186-043WITH CAGE CODE 15152 OR 082001 C/W AT1362.9 ACFT HRS BY SSG J MITS (JM1943)

03-Oct-1997 1

APO AE 09165

DK237781

D CO 2-501 AVNSOF UH-60-98-01 RICK MANAGEMENT OF 230GALLON EXTERNAL TANKS FLIGHTOPERATION C/W (DA661)

02-Feb-1998 1

APO AE 09165

DK237781

D CO 2-501 AVNUH-60-98-ASAM-04 ( TB 1-1520-237-20-205)ONE TIME INSP OF PRIMARY SERVOCOLLECTIVE COOST SERVO, YAW BOOSTSERVO AND T/R SERVO FOR A CCAD REWORKSTICKER C/W AT 1424.6 ACFT HRS

11-Mar-1998 1

APO AE 09165

DK237781

D CO 2-501 AVNUH-60-98-ASAM-05 VISUAL CHECK OFSWASHPLATE PN 70400-08110-054/061 CAGECODE 65780 AND TEK4 OR TEK9 C/W AT 1441.4ACFT HRS NA THIS ACFT (JM1943)

14-Sep-1998 1

APO AE 09165

DK237781

A CO 127 ASBUH-60-98-ASAM-07 ALL H-60 AIRCRAFT ONETIME INSP OF LEFT TIE ROD FOR P/N 70400-08115-043 CAGE CODE 3R021 C/W @ 1441.4ACFT HRS (WT4342)

16-Sep-1998 1

APO AE 09165

DK237781

A CO 127 ASBPHASE #3 COMPLETED AT 1441.4 ACFT HRSNEXT PHASE #4 DUE AT 1941.4 ACFT HRS(WT4342)

01-Oct-1998 1

APO AE 09165

DK237781

A CO 127 ASBLATE ENTRY UH-60-98-ASAM-03 ONE TIMEINSP OF SWASHPLATE LINK PN 70400-08110-54 WITH TEK MFG CW AT 1376.3 ACFT HRS(JM1943)

03-Nov-1998 1

APO AE 09165

DK237781

A CO 127 ASBJACE INSPECTION PERFORMED AT 1452.9 A/CHOURS AT HANUA GERMANY BY MEMBER CC(IK3963)

09-Nov-1998 1

APO AE 09165

DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 22 of 73

A CO 127 ASBUH-60-99-ASAM 02 INSPECTION OF RESCUEHOIST AND HOIST BRACKERS NA THIS ACFTCOMPLIED WITH AT 1452 ACFT HRS (JI7391)

10-Nov-1998 1

APO AE 09165

DK237781

A CO 127 ASBUH-60-99-ASAM-01 SWASHPLATE LINKS TOFULL TBO N/A THIS ACFT COM WITH AT 1452ACFT HRS

10-Nov-1998 2

APO AE 09165

DK237781

A CO 127 ASB17 NOV 98 LATE ENTRY T/R PITCH BIAS ONTAIL ROTOR RIGGING COMPLETED THISPHASE #3 AC HRS 1441.4 BEFORE BIASAFTER BIAS DIFFERENCE BLK;4.416/4.053/.363 BLU: 4.386/4.072/.314, YEL:5.106/4.750/.326, RED: 5.082/4.750/.332(WT4342)

17-Nov-1998 1

APO AE 09165

DK237781

A CO 127 ASBUH-60-99-ASAM-03 ALL UH-60A/EH60AHELICOPTER ONE TIME INSP OF ALL T700-GE-700 ENG RECORDS COMPLETED AT 1452.9ACFT HRS

03-Dec-1998 1

APO AE 09165

DK237781

A CO 127TH ASBUH-60-99-ASAM-06 ALL H60 A/C INSP ANDREVISED RETIREMENT LIFE OF M/R PITCHHORNS P/N 70102-08111-047 COMP 1452.9 A/CHRS (WT4342)

14-Dec-1998 1

APO AE 09165

DK237781

D CO 2-501 AVNUH-60-99-ASAM-07 AA H60 ACFT INSP OF MR DCO 2-501 AVN HUB ASSY (LV5775)

07-Apr-1999 1

APO AE 09165

DK237781

D CO 2-501 AVNUH-60-99-ASAM-08 H60 ACFT REVISEDRETIREMENT LIFE OF BELLCRANK SUPPORTASSY P/N 70400-08162-042/043/45MANUFACTURED BY AIR INDUSTRIES (CAGE8L513) NA THIS ACFT (LV5775)

25-Jun-1999 1

APO AE 09165

DK237781

D CO 2-501 AVNUH-60-99-ASAM-09 ONE TIME INSP OF THE M/RBLADE EXP PIN PART # 07103-08107-101/102/103 CW AT 1505.5 ACFT HRS (ST5114)

03-Aug-1999 1

APO AE 09165

DK237781

D CO 2-501 AVNUH-60-99-ASAM-11 ( TB 1-2840-240-20-13) ONETIME INSPECTION OF T700GE700/701CENGINES COMPLIED WITH AT 1505 ACFT HRSENG SERIAL NUMBERS GE-E-306213 GE-E306092 (FH5454)

03-Aug-1999 2

APO AE 09165

DK237781

D CO 2-501 AVNUH-60-99-ASAM-09 ONE TIME INSP OF MAINROTOR BLADE PINS P/N70110308107.101/102/103 COMPLIED WITH AT1505.5 ACFT HRS BLADE PIN SERIAL NUMBERAVK-04827X, AVK-04275X, AVK-04568X, AVK-04260X, AVK-04267X, AVK-03785, AVK-04253X(FH5454)

03-Aug-1999 3

APO AE 09165

DK237781

D CO 2-501 AVNOUT OF SEQUENCE UH-60-99-ASAM-10 ALLHG ACFT INSP OF #2 CROSSFEED BRAKAWAYVALVE COMPLIED WITH AT 1515.5 ACFT HRS(RF7757)

17-Aug-1999 1

APO AE 09165

DK237781

D CO 2-501 AVNUH-60-99-ASAM-12 ADDITION OF 250 HR INSPOF P-3 BELLOWS O-RING LEAKING ONCERTAIN HMU'S #1 ENG HMU P/N N/A #2 ENGHMU P/N 4046T52G06 ADDED TO DA FROM2408-18 COMPLIED WITH AT 1515.5 ACFT HRS(WH9843)

24-Aug-1999 1

APO AE 09165

DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 23 of 73

AMCOM-E-OLRJACE/CPCE PERFORMED AT 1517.0 AACFTHRS AT HANAU GERMANY BY MEMBERS S9CC(IK3963)

03-Sep-1999 1

HUNTSVILLE, AL

DK237781

D CO 2-501UH-60-00-ASAM-01 ALL H60 ACFT REVISIONTO UH-60-99-ASAM-07 OF MR HUB ASSY CWAT 1535.4 ACFT HRS (LV5775)

17-Nov-1999 1

APO AE 09165

DK237781

D CO 2-501 AVNUH-60-00-ASAM-02 ALL H60 ACFT CYCLICSTICK WIRING BUNDLE RELOCATIONCOMPLIED WITH AT 1537.4 ACFT HRS (RF7757)

17-Dec-1999 1

APO AE 09165

DK237781

D CO 2-501 AVNUH-60-00-ASAM-03 ALL H60 ACFT INSPECTAND REMOVAL OF SUSPECT PRIMARY SERVOASSY (TB 1-1520-237-20-217) CW AT 1538.9ACFT HRS (RF7757)

03-Jan-2000 1

APO AE 09165

DK237781

D CO 2-501 AVNLATE ENTRY UH-60-99-ASAM-04INFORMATIONAL ALL EH , MH UH-L , K ACFTT700-GE-701C ENG ODV RELATEDFLAMEOUTS NA THIS ACFT (RF7757)

11-Feb-2000 1

APO AE 09165

DK237781

D CO 2-501 AVNLATE ENTRY: UH-60-99-ASAM-04-INFORMATIONAL , ALL EH MH UH-60L K ACFTTA700-GE-701C ENG ODV RELATEDFLAMEOUTS NA THIS ACFT (RF7757)

11-Feb-2000 2

APO AE 09165

DK237781

D CO 2-501 AVNUH-60-00-ASAM-04 H-60 ACFT INSP TAIL L/GSHOCK STRUT ASSY FOR MISSING BEARINGRETENTION PIN. C/W AT 1583.2 ACFT HRS(CI2567)

23-Feb-2000 1

DAPO AE 09165

DK237781

AMCOM-E OLRACD/CPCE PERFORMED AT 1603.1 ACFT HRSAT HANAU GERMANY BY MEMBERS S4CC(IK3963)

08-May-2000 1

HUNTSVILLE AL

DK237781

AMCOM-E-OLRACD/CPCE PERFORMED AT 1603.1 ACFT HRSAT HANAU GERMANY BY MEMBERS S4CC(IK3963)

08-May-2000 2

HUNTSVILLE, AL

DK237781

D CO 2-501-AVNUH-60-00-ASAM-05 H-60 ACFT INSP OF FIREEXT WIRING (CHANGE 1 TO TB 1-1520-237-20-219) CW AT 1606.0 ACFT HRS (006402)

19-May-2000 1

APO AE 09165

DK237781

D CO 2.501 AVNUH-60-00-ASAM-06 H-6 ACAFT INSP OF FIREEXT WIRING ( CHANGE 1 TO TB 1-1520-237-20-219) C/W AT 1617.9 ACFT HRS (006402)

23-Jun-2000 1

APO AE 09165

DK237781

D CO 2-501 AVNLATE ENTRY SOF UH-60-00-01 INITIAL ANDRECURRING INSP OF MR SPINDLE LUGSCOMPLIED WITH AT 1623.9 ACFT HRS ( TB A-1520-237-20-221) RR 3090)

13-Jul-2000 1

APO AE 09165

DK237781

D CO 2.501 AVNLATE ENTRY SOF UH-60-00-02 INSP INPUTMODULE GEARBOX ASSY RECORDS IAW TB 1-1520-237-20-222 COMPLIED WITH AT 1623.9ACFT HRS (ST51114)

03-Aug-2000 1

APO AE 09165

DK237781

D CO 2-501 AVNSOF UH-60-01-05, ALL H-60 SERIES AIRCRAFTREVISION TO UH-60-00-01 INSP MR SPINDLES(TB 1-1520-237-20-230 CW AT 1604.4 ACFT HRS(LV5775)

09-Mar-2001 1

APO AE 09165

DK237781

D CO 2-501 AVNSOF UH-60-01-09 ONETIME INSP OF MR BLADEEXPANABLE PINS (TB1-1520-237-20-233 ) CW@ 000.00 ACFT HRS (0000)

11-Jun-2001 1

APO AE HANAU GE

DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 24 of 73

D CO 2-501 AVNSOF UH-60-01-09 ALL H-60 ACFT, ONE TIMEINSPECTION OF ALL M/R BLADE EXPAND PINCW 1689.4 ACFT HRS (LV5775)

11-Jul-2001 1

APO AE 09165

DK237781

D CO 2-501 AVNSOF UH-60-01-10 ONE TIME INSP OF MRBLADE EXPANDABLE PINS (TB 1-1520-237-20-234 ) C/W AT 1689.4 ACFT HRS (RF4246)

17-Jul-2001 1

APO AE 09165

DK237781

A CO 127TH ASBSOF UH-60-01-AS, ALL H-60 ACFT INSP OF M/RBLADE EXPANDABLE PINS (TB 1-1520-237-20-236) CW AT (RB6542)

24-Aug-2001 1

APO AE 09165

DK237781

A CO 127TH ASBSOF UH-60-01-11, ALL H-60 ACFT INSP OF MRHUB ASSY (TB 1-1520-237-20-235) (RB6542)

24-Aug-2001 2

APO AE 09165

DK237781

D CO 2-501 AVNASAM UH-60-02-01, INSP T/R PADDLE FAIRINGASSY (TB 1-1520-237-20-239 CW AT 1711.9ACFT HRS (ME1125)

15-Nov-2001 1

APO AE 09165

DK237781

D CO 2-501 AVNSOF UH-60-02-01, INSP OIL COOLER FANSHAFT ASSY FWD MOUNT FLANGE (TB 1-1520-237-20-240) CW AT 1711.9 ACFT HRS (006422)

19-Nov-2001 1

APO AE 09165

DK237781

D CO 2-501 AVNSOF UH-60-02-02, H-60 MAIN ROTOR HUB SUB-ASSY REWORK AT 1712.7 ACFT HRS (RB6542)

10-Dec-2001 1

APO AE 09165

DK237781

D CO 2-501 AVNSOF UH-60-02-03 ALL H-60 SERIES AIRCRAFTONETIME INSPECTION OF THE FLIGHTCONTROL SYSTEM . PITCH TRIM ASSY AT1712.7 ACFT HRS (RB6542)

11-Dec-2001 1

APO AE 09165

DK237781

D CO 2-501 AVNSOF UH-60-02-04, ALL H-60 SERIES AIRCRAFTINSPECTION OF APU FUEL LINES GROMMET(TB 1-1520-237-20-242) AT 1712.9 ACFT HRS(LH1760)

02-Jan-2002 1

APO AE 09165

DK237781

D CO 2-501 AVNSOF/UH-60-02-05 ALL H-60 SERIES AIRCRAFTINSPECTION OF MR BLADE EXPANDABLEPINS (TB 1-1520-237-20-243) CW AT 1712.9ACFT HRS

08-Feb-2002 1

APO AE 09165

DK237781

D CO 2-501 AVNASAM/UH-60-02-02 ALL H-60 SERIESAIRCRAFT, INITIAL AND RECURRINGINSPECTION OF CONTROL ROD JAMNUT (TB 1-1520-237-20-246) CW AT 1712.9 ACFT HRS(JJ0485)

12-Feb-2002 1

APO AE 09165

DK237781

D COSOF UH-60-02-06, REVISION TO MAIN ROTORHUB NONDESTRUCTIVE INSPECTIONPROCEDURES (NDI) C/W @ 1720.2 ACFT HRS(LH1760)

16-Feb-2002 1

APO, AE

DK237781

D COUH-60-00-ASAM-05 ONE TIME INSP OF M/RSPINDLE THRUST BEARING (RR3090)

02-Apr-2002 1

APO, AE

DK237781

D COUH-60-00-ASAM-07 ONE TIME INSP OF WIREHARNESSES CONNECTING THE #1 AND #2JUNCTION BOXES (TB 1-1520-237-20-224) N/ATO THIS ACFT (RF4246)

16-Apr-2002 1

APO, AE

DK237781

D COUH-60-02-ASAM-07 ALL H-60 SERIES ACFT,TORQUE FACTOR CHARTS DISCREPANCY C/W@ 1720.2 ACFT HRS (LH1760)

30-Apr-2002 1

APO, AE 09165

DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 25 of 73

D COUH-60-02-ASAM-06, ALL H-60 SERIES ACFTCOLL AND YAW BOOST SERVO ASSY SWAGEPIN COLLARS INSP (TB 1 1520-237-20-252) C/W@ 1720.2 ACFT HRS (RF4246)

30-Apr-2002 2

APO, AE

DK237781

D COSOF UH-60-02-07 ALL UH-60A. EH-60A, UH-60QSERIES ACFT MAIN MODULE PLANETARYCARRIER ASSEMBLY C/W @ 1720.2 ACFT HRS(LH1760)

14-May-2002 1

APO, AE

DK237781

D CO 2.51 ST AVN BNSOF UH-60-02-09 ALL UH-60A , EH-60A, UH60QMAIN MODULE PLANETARY CARRIER AASSYC/W @ 1720.2 ACFT HRS (LH1760)

21-May-2002 1

APO AE 09165

DK237781

AMCOM PROJECT/OLRUH-60-02-SOF-11 ONE TIME INSPECTION OFMAIN ROTOR BLADE CUFF ASSY NOTCOMPLIED WITH SUPERCEDED BY UH-60-02-SOF-12 1721.1 ACFT HRS (PG4153)

12-Aug-2002 1

EAST HAAF, GA 31409

DK237781

AMCOM PROJECT/OLRUH-60-02-SOF-12 REVISON TO UH-60-02-SOF-11 ONE TIME INSPECTION OF MAIN ROTORBLADE CUFF ASSY COMPLIED WITH AT 1721.2ACFT HRS (PG4153)

10-Sep-2002 1

HAAF, GA 31409

DK237781

AMCOM PROJECT/OLRAIRCRAFT DE-CPNFIGURED AT 1721.2 ACFTHRS

13-Sep-2002 1

HAAF, GA 31409

DK237781

USAACEACFT OPERATING UNDER AWOR REL DTD 13MAY 02 FOR SPECIFIED EH60 ACFT TOOPERATE WITH ALL MISSION EQUIPMENTREMOVED AND SELECTED EQUIPMENTINSTALLED (SEE AWOR REL) THIS AWOR RELSUPERCEDES AWOR RELS WITH SAMESUBJECT DTD 15 JAN 02, 06 JUN 01 AND 21NOV 00 (MF4187)

17-Sep-2002 1


DK237881

USAACEACFT ARRIVED AT USAAVNC, FT. RUCKER, AL.ON 17 SEP 02 WITH 1725.7 ACFT HRS. FROMGERMANY, ACFT WENT TO HAAF, SAVANNAH,GA. FOR EH DE-MOD. NO ACCEPTANCE INSPWAS COMPLETED BY DYNCORP PERSONNELFROM THIS LOCATION. (MF4187)

17-Sep-2002 2


DK237781

USAACETB1-1520-237-20-261 (UH-60-02-ASAM-11)INSPECT AN/ARC-220 WIRING FOR CHAFINGC/W AT 1725.7 ACFT HRS. (JM1943)

24-Sep-2002 1


DK237781

USAACEAWOR REL 13 MAY 02 (3) INSTALLATION OFTHE PROVISIONS FOR THE INSTALLATION OFA CARGO HOOK C/W THIS DATE AT 1726.5ACFT HRS. (VM4663)

01-Nov-2002 1


DK237781

USAACEAWOR REL 13 MAY 02 (2) INSTALLATION OFTHE PROVISIONS FOR THE INSTALLATION OFTHE DOPPLER/GPS AN/ASN-128B C/W THISDATE AT 1726.5 ACFT HRS. (VM4663)

01-Nov-2002 2


DK237781

USAACEAWOR REL 13 MAY 02 (1) INSTALLATION OFTHE PROVISIONS FOR THE INSTALLATION OFTHE ANVIS/HUD AN/AVS-7 C/W THIS DATE AT1726.5 ACFT HRS. (VM4663)

01-Nov-2002 3


DK237781

USAACEUH-60-03-ASAM-02 TAIL ROTOR SERVO ASSYRETIREMENT LIFE C/W AT 1780 ACFT HRS.(DK1063)

09-Dec-2002 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 26 of 73

USAACEUH-60-03-ASAM-01 FWD BELLCRANKSUPPORT ASSY RETIREMENT LIFE C/W AT1780.4 ACFT HRS. (MF4187)

09-Dec-2002 2


DK237781

USAACEGEN-03-ASAM-01 (SINCGARS) ARC-201BATTERY BOX AT 1800 ACFT HRS. (VM4663)

18-Dec-2002 1


DK237781

DYNCORP, OLROCM/ACE PERFORMED AT 1941 ACFT HRS BYTEAM MEMBER QQ AMCOM PROJECT OLR(LS2032 L. SANDERS)

24-Mar-2003 1

FT.CAMBPELL,KY

DK237781

USAACE#2 CROSSFEED BREAKAWAY VALVEREPLACED I/A/W TB1-1520-237-20-213 ON 24MAR 03 AT 1941 ACFT HRS (VM 4663)

24-Mar-2003 2


DK237781

USAACETB1-1520-237-20-229 (SOF UH-60-01-03)REMOVAL OF LATERAL SERVO BELLCRANKASSY MANUFACTURED BY PURDY MACHINECOMPANY, CAGE CODE 15152 (VM4663 R/C)

26-Mar-2003 1


DK237781

USAACETB1-1520-237-20-257 (UH-60-02-ASAM-09), INSPOF T/R QUADRANT INSTALLATIONHARDWARE. C/W AT 1941 ACFT HRS (LW2720R/SPEC)

26-Mar-2003 2


DK237781

USAACETB1-1520-237-20-244 (UH-60-02-ASAM-04)RESTRAINT SYSTEM INSPECTION C/W AT 1941ACFT HRS (LW2720 R/SPEC)

27-Mar-2003 1


DK237781

USAACEGEN-MIM-01-005 IDENTIFICATION OFRECEIVER TRANSMITTERS (R/T) REQUIRINGECP-II SOFTWARE UPDATES. (VM4663 R/C)

01-Apr-2003 1


DK237781

USAACEUH-60-01-02 (TB1-1520-237-20-227), REVISIONTO SOF UH-60-01-01 (TB1-1520-237-20-225)INITIAL AND RECURRING INSPECTION OF THEMAIN LANDING GEAR DRAG BEAM ASSY ANDDECREASE TORQUE ON THE JACKPAD NUTC/W AT1941 ACFT HRS (LW2720 R/SPEC)

03-Apr-2003 1


DK237781

USAACE(TB1-1520-237-20-232) SOF UH-60-01-07, INSPOF M/R FLT CONTROL SELF LOCKING BOLTS.C/W AT 1941 ACFT HRS. (LW2720 R/SPEC)

04-Apr-2003 1


DK237781

USAACETB1-1520-237-20-245 (UH-60-02-ASAM-03)INSPECTION OF ENGINGE CONTROLQUADRANT POWER LEVER (PCL) WIRING. C/W1941 ACFT HRS. (LW2720 R/SPEC)

04-Apr-2003 2


DK237781

USAACEPHASE #4 COMPLETED AT 1941 .4 ACFT HRS.NEXT PHASE #5 DUE AT 2441.4 ACFT HRS(LW2720 R/SPEC)

17-Apr-2003 1


DK237781

USAACEACFT OPERATING UNDER AWORTHINESSRELEASE DTD 06 JUN 03 (EH-60 DE-MOD)WHICH SUPERSEDES AWOR RELEASES DTD11 OCT 02, 13 MAY 02, 15 JAN 02, 06 JUN 01AND 21 NOV 00. A COPY OF THE AWOR REL ISLOCATED IN THE BACK OF THIS HISTORICALBOOK (VM4663)

18-Jun-2003 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 27 of 73

USAACESOF UH-60-04-01, INSP OF FORWARDBELLCRANK SUPPORT INSTALLATIONHARDWARE. C/W AT 2250.4 ACFT HRS (IP2860,R/SPEC.)

01-Oct-2003 1


DK237781

USAACEACFT OPERATING UNDER AWORTHINESSRELEASE #1153 DTD 31 DEC 03 (JP-8+100)(IP2860, R/SPEC)

06-Jan-2004 1


DK237781

USAACEDELAYED ENTRY: MEC F28576 REQUESTAUTHORIZATION TO ONE TIME REPAIRBEARING SPLIT LINERS AUTHORIZED BY:KEITH M CLANCY

03-Mar-2004 1


DK237781

USAACEAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH SA DWG. 70400-00003REV E. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD A) AFT CONTROL SERVOINPUT ROD HAS BEEN LENGTHENED 1-1/4TURN. B) LATERAL CONTROL SERVO INPUTROD HAS BEEN LENGTHENED 3/4 TURN. C)FORWARD CONTROL SERVO INPUT ROD HASBEEN SHORTENED 1-1/4 TURN AT 2441.1 ACFTHRS (IP2860, R/SPEC)

12-Mar-2004 1


DK237781

USAACEUH-60-04-ASAM-01 GLARE SHIELD LIGHTINGCIRCUIT BREAKER REPLACEMENT C/W AT2441.1 ACFT HRS. (IP2860, R/SPEC)

16-Mar-2004 1


DK237781

USAACEPMS-2 # 5 COMPLETED AT 2441.1 ACFT HRSPMS-2 #6 DUE AT 2941.1 ACFT HRS (IP2860,R/SPEC)

17-Mar-2004 1


DK237781

USAACEUH-60-04-ASAM-02 INSP OF T/R D/SHAFTFLANGE NUT C/W AT 2448.2 ACFT HRS. - NATHIS ACFT - HAS OVER 2000 HRS (IP2860,R/SPEC)

07-Apr-2004 1


DK237781

USAACE#2 ENG INLET INGESTED A BIRD - RMVD BIRDFROM SWIRL FRAME AND COMPLETED BIRDSTRIKE INSP - NO DAMAGE FOUND. (IP2860,R/SPEC)

29-Apr-2004 1


DK237781

AMCOM/OLR FTCKYOCM/ACE PERFORMED AT 2545 ACFT HRS BYTEAM MEMBER J (FS6922)

20-May-2004 1

FT. RUCKER, AL

DK237781

USAACESOF UH-60-04-02 DISABLING OF COCKPITAIRBAG SYSTEM C/W AT 2587.7 ACFT HRS(IP2860, R/SPEC)

10-Jun-2004 1


DK237781

USAACEUH-60-MIM-04-008 INSPECTION OF WIRINGAND REPAIR TO POWER WIRING ANDINSULATION SLEEVING OF AIRCRAFTRETRACTABLE LANDING LIGHT. C/W AT 2260.2ACFT HRS (VK3955, R/SPEC)

08-Jul-2004 1


DK237781

USAACESOF UH-60-04-04 TECHNICAL, RCS CSGLD-1860 (R1), H-60 MAIN ROTOR HUBSUBASSEMBLY REWORK, UH-60-60-04-04. CWAT 2344.3 ACFT HRS (IP2860, R/SPEC)

18-Aug-2004 1


DK237781

USAACEUH-60-04-ASAM-04, REVISION TO UH-60-04-ASAM-03, FUEL SYSTEM INTEGRITY CHECKSC/W AT 2744.3 ACFT HRS (IP2860, R/SPEC)

19-Aug-2004 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 28 of 73

USAACEUH-60-04-ASAM-05, RESTRAINT SYSTEMINSPECTION C/W AT 2817 ACFT HRS. (DK1063)

22-Sep-2004 1


DK237781

USAACEPHASE TYPE CHANGED FROM PMS-2 TO PMDAND INTERVAL INCREASED FROM 500 TO 700HRS I/A/W AWR 1220 @ 2905.5 ACFT HRS.NEXT PHASE #6 DUE AT 3141.1 ACFT HRS. (M.BELFORD1137)

22-Oct-2004 1


DK237781

USAACEIMPLEMENTATION OF 700 HOUR ESM IAW AWRDTD 28OCT, R-1 DUE NLT 05NOV04. P/C/W AT2920.5 ACFT HRS. (M. BELFORD1137)

05-Nov-2004 1


DK237781

USAACEUH-60-04-ASAM-03 FUEL SYSTEM INTEGRITYCHECKS C/W AT ACFT HRS. SUPERCEDED BYUH-60-05-ASAM-01 (CA3091 R/SPEC)

07-Jan-2005 1


DK237781

USAACEEH/UH-60A, UH-60-05-ASAM-01, REVISION OFFUEL SYSTEM INTEGRITY CHECKS.COMPLIED WITH AT 2995.8 ACFT HRS (M.BELFORD 1137)

11-Jan-2005 1


DK237781

USAACEUH-60-05-ASAM-02, BLUE FORCE TRACKER(BFT). NA THIS ACFT. COMPLETED AT 2995.8ACFT HRS. (M. BELFORD 1137)

02-Mar-2005 1


DK237781

USAACEUH-60-05-SOF-01, REACTIVATION OF COCKPITAIRBAG SYSTEM (CABS). NA THIS ACFT 2995.8ACFT HRS. (M. BELFORD 1137)

16-Mar-2005 1


DK237781

USAACEM/R RIG CHECK COMPLETED @ 2995.8 ACFTHRS. NO ADJUSTMENTS MADE. (CA3091)

16-Mar-2005 2


DK237781

USAACEUH-60-05-SOF-02 ENHANCED SCHEDULEDMAINTENANCE (ESM) PROGRAMIMPLEMENTION (CA3091, R/SPEC)

16-Mar-2005 3


DK237781

USAACEM/R RIG CHECK COMPLETED @ 2995.8 ACFTHRS. NO ADJUSTMENTS MADE. (CA3091)

28-Mar-2005 1


DK237781

USAACEACFT PLACED IN INTERMEDIATE STORAGE 28DEC 04. REMOVED FROM STORAGE AT 2995.2ACFT HRS. (M. BELFORD 1137)

30-Mar-2005 1


DK237781

USAACEOCM/ACE PERFORMED AT 2996 ACFT HRS BYTEAM MEMBER M. (M. BELFORD 1137)

07-Apr-2005 1


DK237781

USAACEM/R RIG CHECK COMPLETED AT 2996.3 ACFTHRS. NO ADJUSTMENTS MADE (M. BELFORD1137)

10-Apr-2005 1


DK237781

USAACEUH-60-05-ASAM-04, TAIL LANDING GEAR YOKEASSY. COMPLETED AT 2996.3 ACFT HRS. (M.BELFORD 1137)

11-Apr-2005 1


DK237781

USAACEM/R RIG CHECK COMPLETED AT 2966.3 ACFTHRS. NO ADJUSTMENTS MADE (M. BELFORD1137)

17-Apr-2005 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 29 of 73

USAACEUH-60-05-ASAM-03, AIRCREW RESTRAINTSYSTEM COMPATIBILITY. COMPLETED AT2998.3 ACFT HRS. (M. BELFORD 1137)

20-Apr-2005 1


DK237781

USAACEM/R RIG CHECK COMPLETED AT 2998.8 ACFTHRS. FWD-NO ADJUSTMENT, AFT-NOADJUSTMENT, LAT- 1/4 TURN. (M. BELFORD1137)

25-Apr-2005 1


DK237781

USAACEUH-60-05-ASAM-06, TROOP SEAT RESTRAINTBUCKLE COMPLETED AT 2999.5 ACFT HRS. (M.BELFORD 1137)

29-Apr-2005 1


DK237781

USAACEM/R RIG CHECK COMPLETED AT 2999.5 ACFTHRS. FWD-1/2 TURN SHORTENED, AFT-1/2TURN LENGTHENED, LAT- 1/4 TURNSHORTENED. (M. BELFORD 1137)

03-May-2005 1


DK237781

USAACEUH-60-05-ASAM-07 AIR INTRUSION OFHYDRAULIC SYSTEM COMPLETD AT 3035.9ACFT HRS. (D. WILLIAMS 0950)

26-May-2005 1


DK237781

USAACEUH-60-05-ASAM-01 REVISION OF FUELSYSTEM INTEGRITY CHECKS (NLT 15APR06)C/W AT 3132.9 ACFT HRS. (AFS274, S NOLIN,2938, R/SPEC)

26-Jul-2005 1


DK237781

USAACEACFT OPERATING UNDER AWR 1262.HELICOPTERS TO CONDUCT FLIGHT WITHEXPERIMENTAL G-AXIS SEALS. A COPY OFTHIS AWR IS LOCATED IN THE HISTORICALRECORDS. THE ENTRY PLACED IN 2408-13-1AT 3132.9 ACFT HRS (M. BELFORD 1137)

27-Jul-2005 1


DK237781

USAACEUH-60-05-ASAM-09 CRASHWORTHYEXTERNAL FUEL SYSTEM (CEFS)INSTALLATION BOLTS C/W AT 3132.9 ACFTHRS. (AFS284, S NOLIN, 2938, R/SPEC)

02-Aug-2005 1


DK237781

USSACEM/R RIG CHECK COMPLETED AT 3132.9 ACFTHRS. NO ADJUSTMENTS MADE. (AM4615, SNOLIN, 2938, R/SPEC)

11-Aug-2005 1


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED I/A/WTM1-1520-237-23, PARA 11-4-6. RED:4.775/5.055, YELLOW: 4.735/5.016, BLUE:4.1200/4.4000, BLACK: 4.0000/4.2865. (M.BELFORD 1137)

12-Aug-2005 1


DK237781

USAACEPHASE INSP #6 C/W AT 3132.9 ACFT HRS.NEXT INSP #7 DUE AT 3832.9 ACFT HRS.(AFS155, S NOLIN, 2938, R/SPEC)

12-Aug-2005 2


DK237781

USAACE#1 ENG G-AXIS SEAL REMOVED FORLEAKING. REPLACED SEAL AND REMOVEDAIRWORTHINESS RELEASE AT 3268.5 ACFTHRS (M. BELFORD 1137)

14-Oct-2005 1


DK237781

USAACEEH/UH-60A ONE TIME INSPECTION OFINSTALLATION OF TAIL LANDING GEARDEFLECTOR (WIRE CUTTER) IAW E-MAILINSTRUCTIONS FROM ACLC DTD 12 OCT 05.COMPLETED AT 3270.1 ACFT HRS. (M.BELFORD 1137)

15-Oct-2005 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 30 of 73

USAACEACFT OPERATING UNDER AIRWORTHINESSRELEASE TO CONDUCT ESM OPERATIONALEVALUATION AT THE USAAVNC, FT. RUCKER,AL (AWR 1220) (M. BELFORD 1137)

20-Oct-2005 1


DK237781

USAACEAIRWORTHINESS RELEASE 1220 DTD 06 OCT05 TO CONDUCT ESM OPERATIONALEVALUATION AT THE USAAVNC, FT. RUCKER,AL COMPLETED AT 3291.4 ACFT HRS. PMIINTERVAL INCREASED FROM 700 TO 720 HRSI/A/W 1220 NEXT PHASE #7 DUE AT 3852.9ACFT HRS (M. BELFORD 1137)

20-Oct-2005 2


DK237781

USAACEACFT OPERATING UNDER AWR 1220. A COPYOF THIS AWR IS LOCATED IN THE HISTORICALRECORDS (M. BELFORD 1137)

25-Oct-2005 1


DK237781

USAACE#2 CROSSFEED BREAKAWAY VALVEREPLACED I/A/W TB1-1520-237-20-213COMPLETED AT 3380.3 ACFT HRS (M.BELFORD 1137)

22-Nov-2005 1


DK237781

USAACEUH-60-06-ASAM-01, TAIL LANDING GEARSHOCK STRUT COMPLETED AT 3461.1 ACFTHRS. (M. BELFORD 1137)

07-Jan-2006 1


DK237781

USAACEACFT CONTINUES TO OPRATE UNDER AWR1153, JP-8+100 FUEL, R2 DTD 30JAN06. (M.BELFORD 1137)

31-Jan-2006 1


DK23781

DYNCORP, OLROCM/ACE PERFORMED AT 3585.6 ACFT HRSBY TEAM MEMBER QQ AMCOM PROJECT OLR.(LS 2032 L. SANDERS)

08-Mar-2006 1

FT.CAMPBELL,KY

DK23781

USAACEUH-60-05-ASAM-11, WIRING HARNESSCHAFFING COMPLETED AT 3585.6 ACFT HRS.(M. BELFORD 1137)

11-Mar-2006 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT3676.5 ACFT HRS. TEMP 22 DEGREES C. R/H155, L/H 154. (M. BELFORD 1137)

12-Apr-2006 1


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT3676.5 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 4.951/5.231, YELLOW:4.835/5.115,BLUE: 4.177/4.457, BLACK:4.168/4.448. (M.BELFORD 1137)

12-Apr-2006 2


DK237781

USAACEUH-60-06-ASAM-02, MAIN ROTOR RIGIDCONNECTING LINK/PITCH CONROLASSEMBLIES. COMPLETED AT 3677.2 ACFTHRS. (M. BELFORD 1137)

14-Apr-2006 1


DK237781

USAACET/R CABLE TENSION CHECK DUE 3686.5HRS.+/- 1.5 HRS. (1ST. READING: TEMP 22*C,L/H-154, R/H -155). COMPLETED AT 3686.8ACFT HRS. 28* C. R/H 149, L/H 150. (M.BELFORD 1137)

21-Apr-2006 1


DK237781

USAACEACLC EMAIL DATED 27MAR2006, ONE TIMEINSPECTION OF LOWER CONSOLE CIRCUITBREAK PANEL ASSEMBLIES FOR WATERPENETRATION. COMPLETED AT 3686.8 ACFTHRS (M. BELFORD 1137)

23-Apr-2006 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 31 of 73

USAACET/R CABLE TENSION CKECK COMPLETED AT3687.6 ACFT HRS. TEMP 29*C. R/H 141, L/H 140.(M. BELFORD 1137)

23-Apr-2006 2


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT3687.6 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 5.034/5.314, YELLOW: 4.936/5.216,BLUE: 4.282/4.562, BLACK: 4.258/4.538. (M.BELFORD 1137)

23-Apr-2006 3


DK237781


24-Apr-2006 1


DK237781

USAACEMAIN ROTOR RIG CHECK COMPLETED AT3688.6 ACFT HRS. NO ADJUSTMENTS MADE.(M. BELFORD 1137)

24-Apr-2006 2


DK237781

USAACET/R CABLE TENSION CHECK NOTPERFORMED IAW TM1-1520-237-23-6, PARA 11-4-110.1.2.P, PG 11-4-505. COMPLETED AT3696.3ACFT HRS. R/H=143, L/H=144, 22 DEGREES C.(M. BELFORD 1137)

29-Apr-2006 1


DK237781

USAACET/R CABLE TENSION CHECK DUE AT 3697.6A/C HR + OR -1.5 HR (PREVIOUS READINGTEMP 29 DEGREES C L/H 140 R/H 141.COMPLETED CABLE TENSION CK. AT 3696.3ACFT HRS. L/H=130, R/H=135, 15 DEGREES C(M. BELFORD 1137)

29-Apr-2006 2


DK237781

USAACET/R CABLE TENSION CHECK FAILED.ADJUSTED T/R CABLE TENSION L/H=137,R/H=135, 20 DEGREES C. COMPLETED AT3696.3 ACFT HRS. (M. BELFORD 1137)

29-Apr-2006 3


DK237781

USAACEDUE CABLE TENSION CHECK @ 3706.3 HRS +/-1.5 HRS TEMP 22 DEGREES C R/H 143, L/H 144.FAILED TENSION CHECK. NO ADJUSTMENTREQUIRED. COMPLETED AT 3708.0 ACFT HRS.(M. BELFORD 1137)

06-May-2006 1


DK237781

USAACET/R CABLE TENSION CHECK DUE AT 3718.0 +OR - 1.5 HRS TEMP 31 DEGREE C R/H 175, L/H175. COMPLETED AT 3718.7 ACFT HRS. R/H142, L/H 141 AT 19 DEGREE C. (M. BELFORD1137)

11-May-2006 1


DK237781

USAACEUH-60-06-SOF-02 DISABLING OF COCKPITAIRBAG SYSTEM (CABS) C/W AT 3768.2 ACFTHRS. (M. BELFORD 1137)

22-Jun-2006 1


DK237781

USAACEUH-60-06-ASAM-04-COCKPIT AIRBAG SYSTEM(CABS) ELECTRONIC CRASH SENSOR UNIT(ECSU) DRAIN PLUGS. NA THIS ACFT AT 3768.2ACFT HRS. (M. BELFORD 1137)

22-Jun-2006 2


DK237781

USAACET/R CABLE TENSION CHECK REQUIRED FORCABLE DISCONNECTED AND RECONNECTEDAT QURDIANT. COMPLETED AT 3768.2 ACFTHRS. L/H=174, R/H=175, AT 104*F. (M. BELFORD1137)

23-Jun-2006 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 32 of 73

USAACECABLE TENSION CHECK DUE AT 3778.2 +/-1.5HOURS. COMPLETED AT 3778.4 ACFT HRS.L/H=135, R/H=135, AT 240 C. (M. BELFORD1137)

29-Jun-2006 1


DK237781

USAACEUH-60-06-ASAM-05 BLUE FORCE TRACKERHARDWARE INSTALLATION C/W AT 3808 ACFTHRS. (NA THIS ACFT) (DK1063 (AFS 167))

21-Jul-2006 1


DK237781

USAACEGEN-MIM-06-001 INSPECTION OF T700 SERIESENGINE OIL FILLER ASSEMBLY (M. BELFORD1137)

22-Aug-2006 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT3851.4 ACFT HRS. L/H=173, R/H=174,TEMP=30*C. (M. BELFORD1137)

29-Aug-2006 1


DK237781

USAACEM/R RIGGING CHECK OMPLETED AT 3851.4ACFT HRS. NO ADJUSTMENTS ALLOWED. (M.BELFORD 1137)

29-Aug-2006 2


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT3851.4 ACFT HRS. I/A/W TM1-1520-237-23,PARA 11-4-6. RED: 4.777/5.117, YELLOW:4.831/5.158, BLUE: 4.139/4.475, BLACK:4.075/4.415. (M. BELFORD 1137)

30-Aug-2006 1


DK237781

USAACEPHASE INSPECTION #7 COMPLETED AT 3851.4ACFT HRS. (M. BELFORD 1137)

31-Aug-2006 1


DK237781

USAACEDELAYED ENTRY: MEC F53582 REQUEST TOREAM AND REPAIR STABILATOR MOUNTFITTING AUTHORIZED BY: TAMMY S GRIFFIN

08-Sep-2006 1


DK237781

USAACEUH-60-07-ASAM-01 REQUIREMENTS OF UH-60-07-ASAM-01, (REROUTING OF WHITEENGINE/AIRFRAME HARNESS ASSEMBLY)COMPLIED WITH 4081.0 ACFT HRS. (M.BELFORD 1137)

09-Dec-2006 1


DK237781

USAACEUH-60-07-ASAM-02 REVISION TO UH-60-07-ASAM-01, REROUTING OF WHITEENGINE/AIRFRAME HARNESS ASSEMBLYCOMPLETED AT4118 ACFT HRS. (TB1027R/SPEC)

21-Dec-2006 1


DK237781

USAACEUH-60-07-ASAM-03 YAW AND COLLECTIVEBOOST SERVOS ROLL PIN COMPLETED AT4119.0 ACFT HRS. (M. BELFORD 1137)

29-Dec-2006 1


DK237781

USAACEUH-60-07-ASAM-04 AUTOROTATIONALCHARTS COMPLETED AT 4119.0 ACFT HRS (M.BELFORD 1137)

30-Dec-2006 1


DK237781

USAACEACFT OPERATING UNDER AWR 1153 (R3)(JP8+100 FUEL) DTD 19DEC06 AT 4152.8 ACFTHRS (M. BELFORD 1137)

22-Jan-2007 1


DK237781

USAACEUH-60-07-ASAM-05 ARC-220/KY-100 START-UPPROCEDURES (N/A THIS ACFT., KY-100 NOTINSTALLED) AT 4162.1 ACFT. HRS. (M.BELFORD 1137)

25-Jan-2007 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 33 of 73

USAACEUH-60-07-ASAM-06 INTERNAL RESCUE HOISTCABLE (GUARD) DEFLECTOR C/W AT 4210.8ACFT. HRS. (M. BELFORD 1137)

08-Feb-2007 1


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT4214.3 ACFT HRS I/A/W TM1-1520-237-23, PARA11-2-6. RED: 5.087/4.742, YELLOW:5.0995/4.7630, BLUE: 4.423/4.081, BLACK:4.3665/4.0255. (M. BELFORD 1137)

13-Feb-2007 1


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT4214.3 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 5.143/4.811, YELLOW: 5.124/4.790BLUE: 4.476/4.137, BLACK: 4.424/4.092. (M.BELFORD 1137)

14-Feb-2007 1


DK237781

USAACEMAIN ROTOR RIG CHECK COMPLETED AT4214.3 ACFT HRS. NO ADJUSTMENTS MADE.(M. BELFORD 1137)

14-Feb-2007 2


DK237781

USAACECABLE TENSION CHECK COMPLETED AT4215.3 ACFT HRS. TEMP-18*C, R/H-130, L/H-131. NO ADJUSTMENTS MADE. (M. BELFORD1137)

18-Feb-2007 1


DK237781

USAACEMAIN ROTOR SYSTEM RIG COMPLETED AT4215.3 ACFT HRS. FWD:3/4 SHORTER, AFT:3/4LONGER, LAT: NO CHANGE. (M. BELFORD1137)

18-Feb-2007 2


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT4215.3 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:5.207/4.874, YELLOW:5.170/4.832,BLUE:4.532/4.202, BLACK:4.499/4.165. (M.BELFORD 1137)

18-Feb-2007 3


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT4216.8 ACFT HRS. L/H:125, R/H:124,TEMP:+16*C. (M. BELFORD 1137)

21-Feb-2007 1


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT4216.8 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 5.148/4.868, YELLOW: 5.142/4.862,BLUE:4.461/4.181, BLACK:4.430/4.150. (M.BELFORD 1137)

21-Feb-2007 2


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT4227.0 ACFT HRS. TEMP=20*C, L=151, R=153(M. BELFORD 1137)

28-Feb-2007 1


DK237781

USAACEUH-60-07-AMAM-01 COMMON MISSILEWARNING SYSTEM (CMWS) N/A THIS ACFT @4272.9 ACFT. HRS. (M. BELFORD 1137)

27-Mar-2007 1


DK237781

USAACEMAIN ROTOR RIG CHECK COMPLETED AT4272.9 ACFT HRS. FWD=NO CHANGE, AFT=NOCHANGE, LAT=SHORTENED 1 TURN. (M.BELFORD 1137)

28-Mar-2007 1


DK237781

USAACEUH-60-07-ASAM-07 INSTALLATION OF STATICBONDING JUMPERS, N/A TO THIS ACFT. C/WAT 4431.3 ACFT. HRS. (MB1137)

11-May-2007 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 34 of 73

USAACEACFT OPERATING UNDER AWR 1251, REV 1,DTD 16 MAR 07 (INATL OF EYEBOLTS ONBIFILAR FOR SAFETY HARNESSES) 4441.1ACFT HRS. (M. BELFORD 1137)

17-May-2007 1


DK237781

USAACEM/R RIG CHECK COMPLETED. FAILED RIGCHECK. COMPLETED AT 4518.0 ACFT HRS. (M.BELFORD 1137)

03-Jul-2007 1


DK237781

USAACEOCM/ACE PERFORMED @ 4518 ACFT HRS BYTEAM MEMBER R AMCOM PROJECT OLR(TB1027 R/SPEC)

09-Jul-2007 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT4518.0 ACFT HRS. R/H=175, L/H=178, 32*C. (M.BELFORD 1137)

27-Jul-2007 1


DK237781

USAACEFAILED M/R RIG CHECK-COMPLETE M/RRIGGING PROCEDURE DUE. COMPLETED M/RRIG CHECK. FWD=LENGHTENED 1/2 TURN,AFT=SHORTENED 1/2 TURN, LAT=SHORTENED1/4 TURN. COMPLETED AT 4518.0 ACFT HRS.(M. BELFORD 1137)

27-Jul-2007 2


DK237781

USAACEACFT OPERATING UNDER AWR (1220) TOCONDUCT A MODIFIED ENHANCEDSCHEDULED (ESM) PROGRAM SCHEDULE(REV -3 ) @ 4518.0 ACFT HRS. (RJ0827,R/SPEC)

02-Aug-2007 1


DK237781

USAACE720 HOUR PHASE COMPLETED AT 4518.0ACFT HRS. NEXT PHASE # 9 COMPLETED AT5238.0 ACFT HRS (M. BELFORD 1137)

09-Aug-2007 1


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT4518.5 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:5.161/4.830, YELLOW: 5.229/4.893,BLUE:4.495/4.161, BLACK: 4.498/4.163. (M.BELFORD 1137)

16-Aug-2007 1


DK237781

USAACEH-60-08-AMAM-01 MAIN LANDING GEARSHOCK STRUTS C/W AT 4699.1 ACFT. HRS. (M.BELFORD 1137)

03-Nov-2007 1


DK237781

USAACEH-60-08-ASAM-02 POWER AVAILABLECONTROL CABLE C/W AT 4715.9 ACFT. HRS.(M. BELFORD 1137)

07-Nov-2007 1


DK237781

USAACEH-60-08-ASAM-04 PILOTS LOWER SEAT RAILCHAFING ELECTRICAL HARNESS COMPLETEDAT 4777.3 ACFT HRS. (M. BELFORD 1137)

29-Nov-2007 1


DK237781

USAACEH-60-08-AMAM-02 TAIL ROTOR OUTBOARDRETENTION PLATE SHIMS COMPLETED AT4790.0 ACFT HRS. (M. BELFORD 1137)

01-Dec-2007 1


DK237781

USAACEH-60-08-ASAM-03 CHANGES TO CURRENTFUEL SYSTEM INTEGRITY CHECKS C/W AT4790.0 ACFT HRS (M. BELFORD 1137)

02-Dec-2007 1


DK237781

USAACEH-60-08-ASAM-05 TAIL ROTOR QUADRANTSPRING CAPSULE ASSEMBLY C/W AT 4814.1ACFT. HRS. (M. BELFORD 1137)

15-Dec-2007 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 35 of 73

USAACE#2 CROSSFEED BREAKAWAY VALVEREPLACED I/A/W TB1-1520-237-20-213 AT4819.9 ACFT HRS (M. BELFORD 1137)

19-Dec-2007 1


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT4877.0 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED 4.896/5.236, YELLOW:4.995/5.335,BLUE: 4.187/4.527, BLACK: 4.07/4.41. (M.BELFORD 1137)

28-Jan-2008 1


DK237781

USAACET/R CABLE TENSION ADJUSTED TO R/H=145,L/H=143 AT 21*C. COMPLETED AT 4877.0 ACFTHRS. (M. BELFORD 1137)

28-Jan-2008 2


DK237781

USAACEH-60-08-SOF-01 MAIN ROTOR BLADEEXPANDABLE PIN INSPECTION CHANGECOMPLETED AT 4877.0 ACFT HRS. (M.BELFORD 1137)

30-Jan-2008 1


DK237781


31-Jan-2008 1


DK237781


31-Jan-2008 2


DK237781

USAACEAIRCRAFT NO LONGER OPERATING IAWLIMITATIONS AND RESTRICTIONS SPECIFIEDIN THE ARW 1153 (JP-8+100 FUEL)COMPLETED AT 4877.0 ACFT HRS. (M.BELFORD 1137)

01-Feb-2008 1


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT4877.0 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:4.734/5.062, YELLOW: 4.751/5.078,BLUE:4.203/4.531, BLACK: 4.093/4.421. (M.BELFORD 1137)

02-Feb-2008 1


DK237781

USAACEH-60-08-AMAM-05 GOODRICH INTERNALRESCUE HOISTS COMPLETED AT 4877.0 ACFTHRS. (M. BELFORD 1137)

04-Feb-2008 1


DK237781

USAACEH-60-08-AMAM-03 MIL-PRF-23699 HIGHTEMPERATURE STABILITY (HTS) OILCOMPLETED AT 4878.0 ACFT HRS. (M.BELFORD 1137)

09-Feb-2008 1


DK237781

USAACEH-60-08-AMAM-06 COMMON MISSILE WARNINGSYSTEM (CMWS) SEQUENCERS COMPLETEDAT 4878.0 ACFT HRS (M. BELFORD 1137)

10-Feb-2008 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT887.0 ACFT HRS. R/H=124, L/H=120 AT 10*C (M.BELFORD 1137)

13-Feb-2008 1


DK237781

USAACEH-60-08-AMAM-04 H-60-08-AMAM-04 COCKPITDOOR JETTISONABLE WINDOWS COMPLETEDAT 4887.5 ACFT HRS. (M. BELFORD 1137)

17-Feb-2008 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 36 of 73

USAACEH-60-08-ASAM-06 M/R PYLON SLIDINGFORWARD FAIRING C/W AT 4972.7 ACFT HRS.(M. BELFORD 1137)

15-Mar-2008 1


DK237781

USAACEOCM/ACE PERFORMED AT 4973 ACFT HRS BYTEAM MEMBER R. (M. BELFORD 1137)

17-Mar-2008 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT4972.7 ACFT HRS. L/H=135, R/H=135 AT 20*C.(M. BELFORD 1137)

24-Mar-2008 1


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT4973.7 ACFTR HRS I/A/W TM1-1520-237-23,PARA 11-4-6. RED: 4.793/5.093,YELLOW:4.794/5.094, BLUE: 4.134/4.434,BLACK: 4.085/4.385. (M. BELFORD 1137)

24-Mar-2008 2


DK237781

USAACEM/R RIG CHECK COMPLETED AT 4972.7 ACFTHRS. FWD=1/2 TURN SHORTENED, AFT=1/2TURN LENGTHENED. LAT=NO ADJUSTMENT(M. BELFORD 1137)

24-Mar-2008 3


DK237781

USAACEH-60-08-AMAM-07 AN/ASN-128B/D DOPPLERGPS NAVIGATION SET (DGNS) COMPLETED AT4972.7 ACFT HRS (M. BELFORD 1137)

29-Mar-2008 1


DK237781

USAACER/H 308 BEAM HAS A DISDRILLED #30 HOLETHROUGH THE BEAM WHICH EXTENDS 3/4THROUGH BEAM. REPAIRED 308 BEAM IAWMEC F74026A. COMPLETED AT 4972.7 ACFTHRS. (M. BELFORD 1137)

11-Apr-2008 1


DK237781

USAACERIGHT HAND BEADED PANEL HAS SEVENCRACKED BEADS IN A ROW WITH SOMEALREADY PATCHED. REPLACED R/H BEADEDPANEL I/A/W F74026. COMPLETED AT 4972.3ACFT HRS. (M. BELFORD 1137)

11-Apr-2008 2


DK237781

USAACET/R CABLE TENSION CK COMPLETED @4982.4 ACFT HRS L/H 144, R/H 141 @ 19DEGREES C (TB1027 R/SPEC)

18-Apr-2008 1


DK237781

USAACET/R CABLE TENSION SET TO LEFT-136, RIGHT-136 AT 19*C. COMPLETED AT 4982.7 ACFTHRS. (M. BELFORD 1137)

05-May-2008 1


DK237781

USAACECOPILOTS LOW COLL STOP BOLT SET TO .746IAW WP 1035. (M. BELFORD 1137)

07-May-2008 1


DK237781


07-May-2008 2


DK237781

USAACEM/R RIG CKECK COMPLETED AT 4482.7 ACFTHRS. FWD=SHORTENED 1/4 TURN,AFT=LENGTHENED 1/4 TURN,LAT=SHORTENED 1 TURN. (M. BELFORD 1137)

08-May-2008 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 37 of 73

USAACET/R BIAS MEASUREMENTS COMPLETED AT4987.2 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:5.152/4.842, YELLOW: 5.169/4.863,BLUE: 4.407/4.098, BLACK:4.426/4.120. (M.BELFORD 1137)

13-May-2008 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT4987.2 ACFT HRS. L=160, R=158 AT 26*C. (M.BELFORD 1137)

13-May-2008 2


DK237781

USAACEM/R RIG CHECK COMPLETED AT 4982.7 ACFTHRS. FWD=1/2 TURN SHORTENED, AFT=1/2TURN LENGTHENED, LAT=NO ADJUSTMENTRECORDED. (M. BELFORD 1137)

13-May-2008 3


DK237781


21-May-2008 1


DK237781

USAACEACFT OPERATING UNDER AWR (1220) TOCONDUCT A MODIFIED ENHANCEDSCHEDULED (ESM) PROGRAM SCHEDULE(REV -3 )@ 4518.0 ACFT HRS. SUPERCEDEDBY AWR 1220 DATED 22 MAY 2008 AT 5031.6ACFT HRS (M. BELFORD 1137)

04-Jun-2008 1


DK237781

USAACEH-60-08-AMAM-08 COMPLIED WITHREQUIREMENTS OF H-60-08-AMAM-08 FLIGHTCONTROL RIGGING UPDATE AT 5039.4 ACFTHRS (M. BELFORD 1137)

07-Jun-2008 1


DK237781

USAACEH-60-08-ASAM-11 COMPLIED WITHREQUIREMENTS OF H-60-08-ASAM-11 FLIGHTCONTROL INSPECTION AT 5228.4 ACFT HRS(M. BELFORD 1137)

25-Aug-2008 1


DK237781

USAACEBLUE M/R SPINDLE HUB INTERNAL LINER ISDISBONDED MORE THAN 25% I/A/W WPO548M/R HUB REQUIRES REPLACEMENT.REPAIRED IAW MECF80845. COMPLETED AT5228.4 ACFT HRS (M. BELFORD 1137)

29-Aug-2008 1


DK237781

USAACEOPERATE WITHIN LIMITATIONS ANDRESTRICTION SPECIFIED AWR 1251 DATED 01SEP 08 REV.2. COMPLETED AT 5235.5 ACFTHRS. (M. BELFORD 1137)

25-Sep-2008 1


DK237781

USAACEUH-60-08-ASAM-01 TROOP/GUNNER SEATUSAACE UPPER ENERGY ATTENUATINGWIRES N/A THIS ACFT. AT 5235.5 ACFT. HRS.(M. BELFORD 1137)

27-Sep-2008 1


DK237781

USAACER/H UPPER DOOR TRACK CRACKED AT FWDEND. REPAIRED TRACK I/A/W MEC-F82295.COMPLETED AT 5235.5 ACFT HRS. (M.BELFORD 1137)

03-Oct-2008 1


DK237781

USAACET/R QUADRANT SPRING CAPSULE SUPPORTBEARINGS WORN EXCESSIVELY. REPLACET/R QUADRANT SUPPORT AT 5235.5 ACFTHRS. (M. BELFORD 1137)

08-Oct-2008 1


DK237781

USAACEH-60-08-ASAM-12 PARKER AEROSPACE AIRTURBINE STARTER (ATS) COMPLETED 5235.5ACFT HRS (M. BELFORD 1137)

10-Oct-2008 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 38 of 73

USAACEH-60-08-ASAM-13 H-60-08-ASAM-13 FIREEXTINGUISHING TUBE UNION RINGCOMPLETED AT 5235.5 ACFT HRS. (M.BELFORD 1137)

14-Oct-2008 1


DK237781

USAACEL/H LOWER CARGO DOOR TRACK CENTERUSAACE INBOARD AND OUTBOARD WEARPADS WORN EXCESSIVELY. REPAIRED TRACKI/A/W MEC-F83056, WP0179 TM1-1520-237-23.COMPLETED AT 5235.5 ACFT HRS. (M.BELFORD 1137)

17-Oct-2008 1


DK237781

USAACET/R PYLON RIGHT HAND ATT. FITTING I/BBEARING HAS DAMAGE. REPLACED BEARINGPER MEC. F82919. COMPLETED AT 5235.5ACFT HRS. (M. BELFORD 1137)

21-Oct-2008 1


DK237781

USAACEH-60-08-ASAM-10 ELECTRICAL WIRE CHAFEISSUES COMPLETED AT 5235.5 ACFT HRS. (M.BELFORD 1137)

21-Oct-2008 2


DK237781

USAACEMAIN ROTOR COMPLETE RIG COMPLETED AT5235.5 ACFT HRS. NO ADJUSTMENTS MADE.(M. BELFORD 1137)

22-Oct-2008 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT5235.5 ACFT HRS. R/H=159, L/H=160 AT 19*C(M. BELFORD 1137)

23-Oct-2008 1


DK237781

USAACEH-60-09-SOF-01 HYDRO-MECHANICAL UNIT(HMU) H-60-09-SOF-01 COMPLETED AT 5235.5ACFT HRS. (M. BELFORD 1137)

23-Oct-2008 2


DK237781

USAACEPHASE INSPECTION #9 COMPLETED AT 5235.5ACFT HRS. (M. BELFORD 1137)

24-Oct-2008 1


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT5235.5 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 4.68/5.01, YELLOW: 4.68/5.01,BLUE: 4.13/4.46, BLACK: 4.13/4.46 (M.BELFORD 1137)

25-Oct-2008 1


DK237781


28-Oct-2008 1


DK237781


28-Oct-2008 2


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT5244.8 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 4.745/4.445, YELLOW: 4.770/4.476.BLUE: 4.30/3.733, BLACK: 4.053/3.743. (M.BELFORD 1137)

31-Oct-2008 1


DK237781


31-Oct-2008 2


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 39 of 73

USAACEH-60-09-SOF-02 H-60-09-SOF-02 AN/ALQ-144INFRARED COUNTERMEASURE SYSTEM(IRCMS) COMPLETED @ 5252.8 ACFT HRS. NATO THIS ACFT. (M. BELFORD 1137)

08-Nov-2008 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT5255.6 ACFT HRS. L/H=158, R/H=158 AT 32*.BELFORD 1137)

13-Nov-2008 1


DK237781

USAACEH-60-09-SOF-03 H-60-09-SOF-03 POSSIBLERETIREMENT LIFE OVERFLIGHT COMPLETEDAT 5269.2 ACFT HRS. (M. BELFORD 1137)

19-Nov-2008 1


DK237781

USAACEACFT OPERATE WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1479DATED 04 JAN 08 (IMPROVED PLANETARYCARRIER ASSY) COMPLETED AT 5292.1 ACFTHRS (M. BELFORD 1137)

25-Nov-2008 1


DK237781


17-Dec-2008 1


DK237781

USAACEH-60-09-ASAM-04 RESCUE HOIST MARK 44MOD 0 CARTRIDGE ACTIVATION DEVICE (CAD)N/A THIS ACFT AT 5482.4 ACFT HRS. BELFORD1137

28-Feb-2009 1


DK237781

USAACEQH-60-09-ASAM-05 UPDATE TO LIFE LIMITCHANGE FOR T/R QUADRANT SPRINGCAPSULES C/W AT 5496.4 ACFT HRS. (M.BELFORD 1137)

05-Mar-2009 1


DK237781

USAACEH-60-09-ASAM-07 H-60-09-ASAM-07, FIREEXTINGUISHER WIRING (BREAKAWAYTHREAD) COMPLETED AT 5595.2 ACFT HRS.(MB1137)

11-Apr-2009 1


DK237781

DYNCORP, OLROCM/ACE PERFORMED AT 5595 ACFT HRS BYTEAM MEMBER J AMCOM AFMA. (M. BELFORD1137)

13-Apr-2009 1

FT.CAMPBELL,KY

DK237781


13-Apr-2009 2


DK237781

USAACER/H 34.5 BEAM FWD END CORNER ANGLEBRACKET CRACKED. REPAIR COMPLETE.REMOVED 34.5 CRACK AREA I/A/W MECF91411. COMPLETED AT 5595.2 ACFT HRS.BELFORD 1137)

24-Apr-2009 1


DK237781

USAACELH BEADED PANEL CRACKED . REPAIRED IAWMEC F91407 AT 5595.2 ACFT HRS (M.BELFORD1137)

04-May-2009 1


DK237781

USAACEH-60-09-ASAM-09 FIRE EXTINGUISHER WIRING(BREAKAWAY THREAD) COMPLETED AT5595.2 ACFT HRS. (M. BELFORD 1137)

08-May-2009 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 40 of 73

USAACE#2 ENGINE (S/N:GE-E-207522) FUEL FILTERBUTTON POPPED. REPLACED FUEL FILTERRESET BUTTON. COMPLETED AT 5595.2 ACFTHRS. TTSN ON ENG 9463 (M. BELFORD 1137)

12-May-2009 1


DK237781

USAACEH-60-09-ASAM-08 ENGINE COWLING WEIGHTRESTRICTION COMPLETED AT 5596.2 ACFTHRS. (MB1137)

13-May-2009 1


DK237781

USAACEH-60-09-ASAM-11 H-60-09-ASAM-11 CARGODOOR WINDOW EMERGENCY JETTISONHANDLE INSP C/W AT 5710.5 ACFT HRS.(MB1137)

27-Jun-2009 1


DK237781

USAACEACFT GROUNDED FOR H-60-09-ASAM-07 ANDH-60-09-ASAM-09 NOT BEING C/WCOMPLETED AT 5783.2 (TP1634)

14-Aug-2009 1


DK237781

USAACEH-60-09-AMAM-04 H-60-09-AMAM-04 CO-PILOTSEAT INTERFERENCE WITH ARMY AIRBORNCOMMAND CONTROL SYSYEM (A2C2S)COMPLETED AT 5817.4 ACFT HRS. NA TO THISACFT (JT0967)

25-Aug-2009 1


DK237781

USAACEGEN-09-AMAM-03 ENHANCED ULLS-A(E)INTEGRATED MATERIAL MANAGEMENTCENTER (IMMC) LEGITMATE CODE (LCF)CHANGE 60 REQUIREMENTS (GEN-09-AMAM-03) COMPLETED @ 5821.4 ACFT HRS. NA TOTHIS ACFT. (TB1027 R/SPEC)

26-Aug-2009 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT5821.4 ACFT HRS. L/H=170, R/H=169 AT 96*(JT0967)

26-Aug-2009 2


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT5821.4 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 5.074/4.734; YELLOW: 6.368/5.031;BLUE: 4.378/4.040; BLACK: 4.375/4.030.(JT0967)

26-Aug-2009 3


DK237781

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 INHISTORICAL RECORDS (MB1137)

27-Aug-2009 1


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT5822.9 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 4.873/5.178, YELLOW: 4.889/5.181,BLUE: 4.450/4.746, BLACK: 4.092/4.397(MB1137)

27-Aug-2009 2


DK237781

USAACECOMPLIED WITH REQUIREMENTS OF H-60-09-AMAM-06 AT5822.4 ACFT HRS. CARGO HOOKCARTRIDGE ACTUATED DEVICE (CAD) LIFEREDUCTION. AFS522 (JB2761 R/SPEC)

27-Aug-2009 3


DK237781

USAACEH-60-09-AMAM-07 HALON HAND-HELD FIREEXTINGUISHERS (HHFE) C/W AT 5862.3 ACFTHRS. (MB1137)

16-Sep-2009 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 41 of 73

USAACEACFT OPERATING WITHIN LIMITATION ANDRESTRICTIONS SPECIFIED IN AWR 1514 DTD31 JUL 08 (TP1634)

28-Sep-2009 1


DK237781

USAACEAIRCRAFT OPERATING IAW MEO A6055 DUETO BLACK LEAD DROOP STOP BUSHINGDEBONDED. REPLACEMENT DUE AT NEXTPMI. 5955.5 ACFT HRS. (MB1137)

11-Oct-2009 1


DK237781

USAACEBLACK M/R BLADE LEAD DROOP STOPBUSHING DEBONDED. BLADE LEAD DROOPSTOP BUSHING INSPECTED IAW MEO A6055AT 5904.7 ACFT HRS. (MB1137)

11-Oct-2009 2


DK237781

USAACEAIRCRAFT OPERATING IAW MEO A6055 DUETO BLUE M/R DROOP STOP LEAD BUSHINGDEBONDED. REQUIRE REPLACEMENT ATNEXT PMI 5955.5 ACFT HRS. (MB1137)

21-Oct-2009 1


DK237781

USAACEBLUE M/R BLADE LEAD DROOP STOPBUSHING DEBONDED. BLADE LEAD DROOPSTOP BUSHING INSPECTED IAW MEO A6055AT 5910.1 ACFT HRS. (MB1137)

21-Oct-2009 2


DK237781

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 INHISTORICAL RECORDS (MB1137)

21-Oct-2009 3


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT5238.0 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 4.790/5.102, YELLOW:4.790/5.102,BLUE:4.00/4.312, BLACK: 4.00/4.312. (M.BELFORD 1137)

29-Oct-2009 1


DK237781

USAACER/H BEADED PANEL HAS SEVERAL CRACKEDBEADS IN A ROW WITH SOME ALREADYPATCHED. INSPECTION COMPLETED AT 5922.7ACFT HRS IAW MEC F74026 . NEXT DUE 02FEB 2010. (MB1137)

06-Nov-2009 1


DK237781

USAACEACFT NO LONGER OPERATING UNDER MEONO. A6055. BUSHINGS REPLACED AT PHASE10 AT 5922.7 ACFT HRS. (MB1137)

09-Nov-2009 1


DK237781

USAACEH-60-10-AMAM-04 ASN-128B/C DOPPLERGLOBAL POSITIONING SYSTEM GPSNAVIGATION SET COMPLETED AT 5922.7 ACFTHRS. (MB1137)

11-Nov-2009 1


DK237781

USAACEACFT NO LONGER OPERATING UNDER MECF83056 DUE TO L/H CARGO DOOR LOWERTRACK REPLACED AT PHASE # 10 AT 5922.7ACFT HRS (MB1137)

16-Nov-2009 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT5922.7 ACFT HRS. L/H=165, R/H=164, AT 20*C(MB1137)

17-Nov-2009 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 42 of 73

USAACET/R BIAS MEASUREMENTS COMPLETED AT5922.7 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:4.913/4.588, YELLOW:4.914/4.588,BLUE: 4.309/3.984, BLACK: 4.307/3.982(MB1137)

17-Nov-2009 2


DK237781

USAACEH-60-10-ASAM-03 FIRE BOTTLE DISCHARGELINES AND NOZZLES COMPLETED AT 5922.7ACFT HRS. (MB1137)

17-Nov-2009 3


DK237781

USAACEBOTH THE L/H AND R/H CARGO DOOR UPPERTRACKS ARE CRACKED AT THE FWD END.INSPECTION COMPLETED IAW MEC F82295.NEXT DUE IS 6642.7 ACFT HRS. (MB1137)

18-Nov-2009 1


DK237781

USAACEM/R RIG CHECK COMPLETED AT 5922.7 ACFTHRS. FWD=SHORTEN 3 FLATS,AFT=LENGTHENED 3 FLATS, LAT=NOADJUSTMENTS. (MB1137)

19-Nov-2009 1


DK237781

USAACEH-60-10-ASAM-04 STABILITY AUGMENTATIONSYSTEM (SAS) LINKS C/W AT 5922.7 ACFTHRS. (MB1137)

19-Nov-2009 2


DK237781

USAACEPHASE INSPECTION # 10 COMPLETED AT5922.7 ACFT HRS. NEXT PHASE DUE IS # 11 AT6642.7 ACFT HRS. (MB1137)

19-Nov-2009 3


DK237781

USAACEACFT NO LONGER OPERATING UNDER AWR1479 DATED 04 JAN 08. (IMPROVED MAINTRANSMISSION PLANETARY CARRIER ASSY)RECORDED AT 5948.7 ACFT HRS. (MB1137)

04-Jan-2010 1


DK237781

USAACEOPERATE WITIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1505 REV.3DTD 21 OCT 09 (5-MICRON METAL MESH HYDFILTER) @ 15JAN10 @ 5977.7 ACFT HRS(VM4663)

15-Jan-2010 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT6044.1 ACFT HRS. L/H=166, R/H=167 AT 18*C(MB1137)

16-Jan-2010 1


DK237781

USAACEGEN-10-AMAM-02 DISTRIBUTION OF NEWACFT ELECTRONIC LOGBOOK, N/A THISLOCATION, C/W AT 5999.1 ACFT HRS. (MB1137)

26-Jan-2010 1


DK237781

USAACEH-60-10-AMAM-11 OIL SAMPLING CHANGESCOMPLETED AT 6022.4 ACFT. HRS. (MB1137)

01-Feb-2010 1


DK237781

USAACE1-1520-237-23-9 FUEL CELL CORRISIONINSPECTION OF UH-60, EH-60 AND HH-60SERIES HELICOPTERS COMPLETED AT 6041.1ACFT HRS (MB1137)

10-Feb-2010 1


DK237781

USAACE1-1520-237-23-10 INSTALLATIN OF UH-60, EH-60 AND HH-60 SERIES HELICOPTER FORBODY PLUG CORROSION INSPECTIONCOMPLETED AT 6041.1 ACFT HRS. (MB1137)

10-Feb-2010 2


DK237781

USAACEH-60-10-ASAM-06 AUTO-IGNITION ANDTRANSIENT DROOP IMPROVEMENT TDIMODIFICATION COMPLETED AT 6041.1 ACFTHRS. (MB1137)

10-Feb-2010 3


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 43 of 73


11-Feb-2010 1


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT6043.1 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 5.152/4.864=288 YELLOW:5.118/4.823=.295 BLUE:4.370/4.076=.294BLACK: 4.502/4.217=285 (TP1634)

13-Feb-2010 1


DK237781

USAACEH-60-10-AMAM-05 ULLSA IMMC LCF CHANGE60B C/W AT 6042.6 ACFT HRS N/A (TP1634 AFS745)

13-Feb-2010 2


DK237781

USAACECABLE TENSION CHECK COMPLETED AT6044.1 ACFT HRS. L/H=166, R/H=167 AT 18*C(MB1137)

16-Feb-2010 1


DK237781


17-Feb-2010 1


DK237781

USAACEM/R RIG CHECK COMPLETED AT 6044.6 ACFTHRS. NO ADJUSTMENTS MADE. (MB1137)

18-Feb-2010 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT6044.6 ACFT HRS. COMP. ADJ. L/H=165,R/H=95, AT 25*C. NEW READINGS: L/H=105,R/H=105 AT 25*C. (MB1137)

18-Feb-2010 2


DK237781


24-Feb-2010 1


DK237781

USAACEM/R RIG CHECK COMPLETED AT 6044.6 ACFTHRS. FWD=1/2 TURN SHORTEN, AFT= 1/2TURN LENGTHEN, LAT=1/8 TURN SHORTEN(MB1137)

24-Feb-2010 2


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT6044.6 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 5.179/4.839, YELLOW: 5.1845,BLUE: 4.4110/4.0805, BLACK: 4.5185/4.1920(MB1137)

25-Feb-2010 1


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT6044.6 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED:4.605/4.939, YELLOW: 4.480/4.818,BLUE: 3.822/4.512, BLACK: 4.028/4.358(MB1137)

25-Feb-2010 2


DK237781


01-Mar-2010 1


DK237781


01-Mar-2010 2


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 44 of 73

USAACEACFT OPERATING WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN THE ENCLOSEDAWR 1251, DATED 26 FEB 10. REVISION-3(EYEBOLTS) COMPLETED AT 6046.6 ACFT HRS(MB1137)

02-Mar-2010 1


DK237781

USAACEACFT OPERATING I/A/W MEO A6055 DUE TOBLUE M/R LEAD DROOP STOP BUSHINGDEBONDED. REPLACE AT NEXT PMI DUE AT6642.7 ACFT HRS. COMPLETED AT 6050.8ACFT HRS. (MB1137)

05-Mar-2010 1


DK237781


10-Mar-2010 1


DK237781

USAACEAIRCRAFT OPERATING IAW LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1452 REV 1DATED 29 DEC 09. 6056.2 ACFT HRS. (RC1002)

15-Mar-2010 1


DK237781

USAACEACFT NO LONGER OPERATING IAW MEOA6055 DUE TO BLUE M/R DROOP STOPBUSHING REPLACED. COMPLETED AT 6161.4ACFT HRS (MB1137)

13-Apr-2010 1


DK237781

USAACE#2 ENGINE COWLING LATCH CRACKED.AUTHORIZED TO TO REPAIR ENGINE COWLLATCH IAW MEC F108013. COMPLETED AT6193.7 ACFT HRS.(GE-E-207522) (MB1137)

26-Apr-2010 1


DK237781

USAACEH-60-10-AMAM-12, IMPROVED DRAG BEAM.COMPLETED AT 6213.0 ACFT HRS. BOTHGOOD. (MB1137)

03-May-2010 1


DK237781

USAACEACFT NO LONGER OPERATING WITHINLIMITATIONS AND RESTRICTIONS SPECIFIEDIN THE ENCLOSED AWR DATED 06 JUN 03.SUPERCEDED BY AWR 1681 DATED 10 MAY 10AT 6256.0 ACFT HRS (MB1137)

19-May-2010 1


DK237781

USAACEH-60-10-ASAM-07 STABILATOR HINGEFITTINGS C/W AT (MB1137)

20-May-2010 1


DK237781

USAACEACFT OPERATING IAW AWR 1681, DATED 10MAY 2010 (EH-60 DEMOD) ENTERED AT 6256.0ACFT HRS (MB1137)

20-May-2010 2


DK237781

USAACE#2 CROSSFEED BREAKAWAY VALVEREPLACED I/A/W TB1-1520-237-20-213 AT6258.6 ACFT HRS (MB1137)

20-May-2010 3


DK237781

USAACEFRAME FOR THE ENGINE COWL LATCH ISCRACKED, CURRENTLY THESE AREUNAVAILABLE. AUTHORIZED TO REPAIRTHESE IAW MEC F109387 AT 6268.9 ACFT HRS(MB1137)

26-May-2010 1


DK237781

USAACEACFT OPERATED IAW MEO A6055 DUE TODROOP STOP BUSHING DEBONDED.REPLACEMENT OF M/R DROOP STOPBUSHING REQUIRED AT THE NEXT PMI DUE AT6282.7 AIRCRAFT HOURS. (MB1137)

27-May-2010 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 45 of 73

USAACEMAINTAIN AIRCRAFT AS PRESCRIBED IN AWR1220, DATED 28 MAY 10. REVISION 5(ENHANCED SCHEDULED MAINTENANCE)COMPLETED AT 6279.0 ACFT HRS. (MB1137)

02-Jun-2010 1


DK237781

USAACEMAINTAIN AIRCRAFT AS PRESCRIBED IN AWR1220, DATED 22MAY2008. REVISION 4(ENHANCED SCHEDULED MAINTENANCE)SUPERCEDED BY AWR 1220 DTD 28 MAY 10. R-5 (MB1137)

02-Jun-2010 2


DK237781

USAACEH-60-10-ASAM-08 APU AND APU FIREWALLC/W AT 6280.9 ACFT HRS (DW 0950 R/SPEC)

03-Jun-2010 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT6280.9 ACFT HRS. L/H=168 , R/H=168 AT 32*C(DW 0950 R/SPEC)

04-Jun-2010 1


jimmy.s.caylor

USAACET/R BIAS MEASUREMENTS COMPLETED AT6280.9 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 4.657/4.314=0.343 YELLOW:4.759/4.422=.337 BLUE:3.972/3.636=0.336BLACK: 4.121/3.779=0.342 (DW 0950 R/SPEC)

04-Jun-2010 2


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT6280.9 ACFT HRS I/A/W TM1-1520-237-23, PARA11-4-6. RED: 5.014/4.688=0.326 YELLOW:5.211/4.875=0.336 BLUE:4.486/4.155=0.331BLACK: 4.575/4.255=0.320 (DW 0950 R/SPEC)

05-Jun-2010 1


DK237781

CSCOCM/ACE PERFORMED AT 6281.0 ACFT HRSNY TEAM MEMBER DD, AMCOM ,RA57-E (JB9001)

07-Jun-2010 1

FT. CAMPBELL KY

DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT6291.0 ACFT HRS. FAILED IAW WP174700 OUTGAUGE #15 TENSIOMETER MR#87705,L/H=180, R/H=180 AT 30*C. (MB1137)

12-Jun-2010 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT6302.0 ACFT HRS. R/H=149, L/H=150 AT 29*C(MB1137)

17-Jun-2010 1


DK237781

USAACECABLE TENSION CHECK COMPLETED AT6311.0 ACFT HRS. L/H=145, R/H=146 AT 28*C(MB1137)

19-Jun-2010 1


DK237781

USAACEM/R RIG CHECK COMPLETED AT 6311.0 ACFTHRS. FWD=NO CHANGE, AFT=NO CHANGE,LAT=1/4 TURN SHORTEN. (MB1137)

23-Jun-2010 1


DK237781

USAACEH-60-10-SOF-02 SPINDLE LUG NDI ANDRETIREMENT LIFE CHANGES C/W AT 6311.0ACFT HRS. (MB1137)

23-Jun-2010 2


DK237781

USAACEH-60-10-AMAM-16 COMMON MISSILE WARNINGSYSTEM GUARDED DISPENSE SWITCH C/W AT6318.1 ACFT HRS. (MB1137)

25-Jun-2010 1


jimmy.s.caylor


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 46 of 73

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


DK237781

USAACEM/MOD FILTER BUTTON POPPED. REPLACEDFILTER IAW WP#065700-026600 W/P 0626.TTSN: 5266. MOC OK. (A265-00997). (MB1137)

20-Jul-2010 1


DK237781

USAACEH-60-10-ASAM-11 COMMON COMPONENTRETIREMENT CHANGE TIMES UPDATE C/W AT6435.7 (VM4663)

02-Aug-2010 1


DK237781

USAACEOPERATING UNDER LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1514 DTD 3AUG 01 R-1 (DGNS) @ 6434.7 (VM4663)

03-Aug-2010 1


DK237781

USAACEH-60-10-ASAM-12 T700 SERIES ENGINESCOMMON COMPONENT RETIREMENTSCHANGE TIMES C/W AT 6447.5 ACFT HRS.(RC1002 A FS 545)

10-Aug-2010 1


DK237781

USAACEH-60-10-ASAM-15 IMPROVED EXTERNALSTORES SUPPORT SYSTEM ESSS FUELSYSTEM VENT ELBOW @ 6453.3 (VM4663)

11-Aug-2010 1


DK237781

USAACEACFT OPERATED IAW MEO A6055 REV A DUETO BLUE M/R DROOP STOP BUSHINGDEBONDED. REPLACEMENT OF DROOP STOPBUSHING REQUIRED AT NEXT PMI DUE AT6642.7 ACFT HRS. COMPLETED AT 6466.7ACFT HRS (MB1137)

21-Aug-2010 1


DK237781

USAACEACFT OPERATE WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1639DATED 26 MAY 10 (BFT). COMPLETED AT6470.8 ACFT HRS. (MB1137)

30-Aug-2010 1


DK237781

USAACEMAIN ROTOR COMPLETE RIG DUE.COMPLETED AT 6470.8 ACFT HRS. FWD=1/2TURN SHORTEN, AFT=1/2 TURN LENGTHEN,LAT= NO CHANGE. (MB1137)

09-Sep-2010 1


DK237781

USAACEH-60-10-ASAM-16, RESCUE HOIST CABLE CUTHARNESS CONNECTOR. COMPLETED AT6470.8 ACFT HRS. (MB1137)

09-Sep-2010 2


DK237781

USAACET/R BIAS MEASUREMENTS COMPLETED AT6470.8 ACFT HRS. RED: 5.076/4.746, YELLOW:5.105/4.777, BLUE: 4.398/4.064. BLACK:4.441/4.114. (MB1137)

10-Sep-2010 1


DK237781

USAACEM/R RIG CHECK DUE AFTER ADJUSTMENT ONPEDALS. PEDALS IN LINE, NO ADJUSTMENTNEEDED. COMPLETED AT 6470.8 ACFT HRS(MB1137)

10-Sep-2010 2


DK237781

USAACEMAIN ROTOR RIG CHECK COMPLETED AT6470.8 ACFT HRS. FWD=1/2 TURN SHORTEN,AFT=1/2 TURN LENGTHEN, LAT=NO CHANGE(MB1137)

14-Sep-2010 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 47 of 73

USAACET/R BIAS MEASUREMENTS COMPLETED AT6470.8 ACFT HRS. RED=5.160/4.810,YELLOW=5.200/4.850, BLUE=4.400/4.070,BLACK=4.510/4.170. (MB1137)

15-Sep-2010 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT6470.8 ACFT HRS. L/H=135, R/H=135 AT 24*C.(MB1137)

15-Sep-2010 2


DK237781

USAACEACFT NO LONGER OPERATING UNDER MEOA6055 DUE TO BLUE M/R DROOP STOP LEADBUSHING REPLACED. COMPLETED AT 6471.3ACFT HRS (MB1137)

17-Sep-2010 1


DK237781

USAACEACFT OPERATED IAW MEO A6055 REV A DUETO M/R DROOP STOP BUSHINGS DEBONDED.REPLACEMENT OF M/R DROOPSTOPBUSHINGS REQD AT NEXT PMI. DUE AT6642.7 ACFT HRS. (MB1137)

22-Oct-2010 1


DK237781

USAACEH-60-11-AMAM-03 H-60-11-AMAM-03 OILCOOLER FAN AXIAL BEARING C/W AT 6543.2ACFT HRS. (MB1137)

26-Oct-2010 1


DK237781

USAACEH-60-11-AMAM-04 H-60-11-AMAM-04 ULLS-A(E)(IMMC) (LCF CHANGE 61) C/W AT 6543.2 ACFTHRS. (MB1137)

26-Oct-2010 2


DK237781

USAACEAIRCRAFT TRANSFERRED TO HUNTSVILLE,AL FOR PAINT @ 6543.2 ACFT HRS ON THISDATE 03 NOV 2010. (MB1137)

03-Nov-2010 1


DK237781

SES-IAIRCRAFT PAINT STRIPPED BY PLASTICMEDIA BLASTING ON 08 NOV 10. (AG822182)

08-Nov-2010 1

HUNTSVILLE, AL

DK237781

SES-1AIRCRAFT PRIMERED WITH 1 COAT MIL -PRF-23377J, PAINTED WITH 1 COAT MIL -DTL-64159TYPE II (AG822182)

16-Nov-2010 1

HUNTSVILLE, AL

DK237781

USAACEH-60-11-ASAM-03 HAMILTON STANDARDHYDRO-MECHANICAL UNITS (HMU).COMPLETED AT 6547.0 ACFT HRS (MB1137)

29-Nov-2010 1


DK237781

USAACEH-60-11-ASAM-04 AN/ARN-153 TCN-500 TACANRECEIVER BEARING ERROR C/W AT 6558.1ACFT HRS (MB1137)

03-Dec-2010 1


DK237781

USAACET/R BIAS CHECK COMPLETED @ 6577.1 ACFTHRS. BLUE: 4.426/4.096=.330 BLACK:4.5410/4.2155=.3255 RED: 5.121/4.790=.331YELLOW: 5.179/4.841=.338 (JC6208)

11-Dec-2010 1


DK237781

USAACET/R BIAS CHECK COMPLETED @ 6578.3 ACFTHRS. BLUE: 4.423/4.090.333=.330 BLACK:4.489/4.157=.332 RED: 5.144/4.183=..331YELLOW: 5.175/4.841=.334 (TB1027)

15-Dec-2010 1


DK237781

USAACENO LONGER OPERATING WITHIN LIMITATIONSAND RESTRICTIONS SPECIFIED IN AWR 1347 R-12 (EDM, BFT) DTD 27 DEC 10. (VM4663)

27-Dec-2010 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 48 of 73

USAACEACFT NO LONGER OPERATED IAW MEO A6055REV A DUE TO M/R DROOP STOP BUSHINGSDEBONDED. REPLACEMENT OF M/R DROOPSTOP BUSHINGS REQD AT NEXT PMI.SUPERCEDED BY REV B. (TP1634)

19-Jan-2011 1


DK237781

USAACEACFT OPERATED IAW MEO A6055 REV -B DUETO M/R DROOP STOP BUSHING DE-BONDED.REPLACEMENT OF M/R DROOPSTOPBUSHING REQUIRED AT NEXT PMI DUEAT 6642.7 ACFT HRS. COMPLETED AT 6466.7ACFT HRS (TB1027)

20-Jan-2011 1


DK237781

USAACEH-60-11-ASAM-06 CYCLIC STICK STOP BOLTSC/W AT 6616.1 ACFT. HRS. NA ON THIS ACFT.AFS 121 (MQ6211)

25-Jan-2011 1


DK237781

USAACEH-60-11-AMAM-06 MEDICAL CAROUSELREFURBISHMENT C/W AT 6616.1 (VM4663)

07-Feb-2011 1


DK237781

USAACEH-60-11-ASAM-08 LOS / IFF ANTENNA ANDIVHMS ACCELEROMETER CONNECTORSSAFETY WIRE C/W AT 6616.1 ACFT HRS.AFS121 (MQ6211)

10-Feb-2011 1


DK237781

USAACEL/H BEADED PANEL HAS 5 CRACKS MARKEDIN BLUE AND ONE CRACK STOPPED DRILLEDFOUND WITH EDDIE CURRANT. REPLACEDIAW MEC 121320A. COMPLETED AT 6616.1ACFT HRS. (MB1137)

10-Feb-2011 2


DK237781

USAACEH-60-11-ASAM-08 LOS / IFF ANTENNA ANDIVHMS ACCELEROMETER CONNECTORSSAFETY WIRE C/W AT 6610.1 ACFT HRS.AFS121 (MQ6211)

10-Feb-2011 3


DK237781

USAACEMAIN ROTOR RIG CHECK COMPLETED AT6616.1 ACFT HRS. FWD: NO ADJUSTMENTSMADE, AFT: NO ADJUSTMENTS MADE,LAT:LENGHTENED 1/4 FLAT. (MQ6211)

11-Feb-2011 1


DK237781

USAACEPHASE# 11 720 HR INSP COMPLETED AT6616.1 ACFT HRS. NEXT 720 HR INSP PHASE #12 DUE AT 7336.1 ACFT HRS. (MQ6211)

11-Feb-2011 2


DK237781

USAACETAIL ROTOR RIG CHECK COMPLETED AT6616.1 ACFT HRS. BIAS READINGS: RED-3.939/3.616=.323, BLACK-3.252/2.929=.323YELLOW-3.939/3.614=.324 BLUE-3.252/2.931=.321 (MQ6211)

11-Feb-2011 3


DK237781

USAACEMAIN ROTOR CABLE TENSION CHECKCOMPLETED AT 6616.1 ACFT HRS. L/H:165,R/H:165, @ 23*C.

11-Feb-2011 4


DK237781

USSACET/R CABLE TENSION CHECK COMP. TENSIONCHECK FAILED. MEASURED L/H 165, R/H 170@ 9*C. RESET TENSION TP L/H 130, R/H 131 @9*C. COMPLETED AT 6625.7 ACFT HRS.(MB1137)

18-Feb-2011 1


DK237781

USAACET/R CABLE TENSION CHECK COMP. TENSIONCHECK FAILED. MEASURED L/H 133, R/H 133@ 14.8*C. COMPLETED AT 6635.6 ACFT HRS.(DW0950, R/ SPEC)

23-Feb-2011 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 49 of 73

USAACEOPERATE WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN THE ENCLOSEDAWR 1251, DATED 26 FEB 10 REVISIONS 3(EYEBOLTS) (ORIGINAL FAULT DATE: 01 MAR10)

24-Mar-2011 1


DK237781

USAACECOMPLY WITH REQUIREMENTS OF H-60-11-ASAM-09 (INTERNAL AUXILIARY FUELTRANSFER SYSTEM) PRIOR TO 6742.8 A/CHRS BUT NLT 04 APR 11 NA 6732

29-Mar-2011 1


DK237781

USAACEDELAYED ENTRY: ACFT INDUCTED INTO ULLS-A(E) ON 25 MAR 2011 AT 6723.8 ACFT HRS.

06-Apr-2011 1


DK237781

USAACEH-60-11-AMAM-11 AWR STATUS UPDATECOMPLETED @ ACFT HRS 6814.5. N/A BYACFT BY SERIAL NUMBER

06-Apr-2011 2


DK237781

USAACEACFT OPERATE WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1455,DATED 23 OCT 09, R1 (BCAP). ENTERED AT6818.7 ACFT HRS.

29-Apr-2011 1


DK237781

USAACEH-60-11-AMAM-09, 19-3 ENGINE COMPONENTOPERATING HOUR RECORD COMPLETED AT6867.5 ACFT HRS.

18-May-2011 1


DK237781

USAACEH-60-12--ASAM-01, TR OUTPUT BEVEL GEARNDI COMPLETED AT 7326.8 ACFT HRS -PASS

25-May-2011 1


DK237781

USAACEH-60-11-AMAM-13 EXTERNAL RESCUE HOISTMOUNT FITTING COMPLETED AT 6904.3 ACFTHRS. N/A THIS ACFT

08-Jun-2011 1


DK237781

USAACEMAIN MODE FILTER BUTTON POPPED;REPLACED FLITER AND RESET BUTTON IAWTM 1-152-237-23. AC HRS 6925 XMSN TSN 5787(FJ1809).

17-Jun-2011 1


DK237781

USAACEH-60-11SOF-01, DISPREPANT SELF LOCKINGDOUBLE HEXAGON AT 6957 ACFT HRS.

09-Jul-2011 1


DK237781

USAACEH-60-11-ASAM-13, ENGINE AIR INLET ANTI-ICING VALVE AT 6975.0 ACFT HRS.

10-Jul-2011 1


DK237781

USAACEH-60-11-AMAM-15, IVHMS ACCELEROMETERSCOMPLETED AT 6693.2 ACFT HRS.

14-Jul-2011 1


DK237781

USAACEH-60-11-ASAM-14,ENGINE COWLING REPAIRRESTRICTIONS C/W @ 6972.4 AIRCRAFTHOURS (LW2720)

19-Jul-2011 1


DK237781

USAACET/R BIAS READINGS COMPLETED AT 6975.2ACFT HRS. RED 4.333/4.671/.339, YELLOW4.332/4.666/.334, BLUE 3.570/3.912/.342, BLACK3.648/3.985/.337

23-Jul-2011 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 50 of 73

USAACET/R CABLE TENSION CHECK COMPLETED AT6975.2 ACFT HRS. L/H 168; R/H 171 ; TEMP 31.5'C'

23-Jul-2011 2


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT6984.3 ACFT HOURS. L/H=170. R/H=175 AT 33C.

01-Aug-2011 1


DK237781

USAACEDELAYED ENTRY: MEC F99336 IS NO LONGERVALID DUE TO MAIN TRANSMISSION IS NOLONGER INSTALLED ON AIRCRAFT. ENTEREDAT 6990.9 ACFT HRS. A COPY OF THIS MEC ISLOCATED IN THE HISTORICAL RECORDSBOOK.

09-Aug-2011 1


DK237781

USAACEDELAYED ENTRY: MEC F99668 IS NO LONGERVALID DUE TO MAIN TRANSMISSION IS NOLONGER INSTALLED ON ACFT. A COPY OFTHIS MEC IS LOCATED IN THE HISTORICALRECORDS BOOK.

09-Aug-2011 2


DK237781

USAACEDELAYED ENTRY: FITTING ASSY R/H (TAILPYLON) REPLACED SPLIT LINERS WITH ASOLID LINER IAW ENGINEERING STD. 4-01-03.ENTERED AT 6990.9 ACFT HRS. A COPY OFTHIS IS LOCATED IN THE HISTORICALRECORDS BOOK.

09-Aug-2011 3


DK237781

USAACEDELAYED ENTRY: THERE ARE VISIBLECRACKS IN STAGE TWO DUCT (LEFT-HANDSIDE) AND WIGGLE STRIPS; THERE IS ALSO ACRACK IN THE STAGE 3 DUCT STIFFENER OFTHE HIRRS UNIT. REPAIRED IAW MEC F64910.ENTERED AT 6990.9 ACFT HRS. A COPY OFTHIS MEC IS LOCATED IN THE HISTORICALRECORDS BOOK.

09-Aug-2011 4


DK237781

USAACEDELAYED ENTRY: THERE ARE VISIBLECRACKS IN STAGE TWO DUCT (RIGHT-HANDSIDE) AND WIGGLE STRIPS, THERE IS ALSO ACRACK IN THE STAGE 3 DUCT STIFFENER OFTHE HIRRS UNIT. REPAIRED IAW MEC F64912.ENTERED AT 6990.9 ACFT HRS. A COPY OFTHIS MEC IS IN THE HISTORICAL RECORDSBOOK.

09-Aug-2011 5


DK237781

USAACEDELAYED ENTRY: MEC F65266 NO LONGERVALID, APU 846114 REMOVE FROM ACFT.ENTERED AT 6990.9 ACFT HRS. A COPY OFTHIS MEC IS LOCATED IN THE HISTORICALRECORDS BOOK.

09-Aug-2011 6


DK237781

USAACEDELAYED ENTRY: MEC F80845 NO LONGERVALID. M/R HUB S/N: A308-03077 REPLACED.ENTERED AT 6990.9 ACFT HRS. A COPY OFTHIS MEC IS LOCATED IN THE HISTORICALRECORDS BOOK.

09-Aug-2011 7


DK237781

USAACEH-60-11-AMAM-20 (AN/ASN-128D SOFTWAREUPGRADE) COMPLETED AT 7032.5 ACFT HRS.

21-Sep-2011 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT7032.5 ACFT HRS. L/H=156, R/H=154, AT 26.3 C.

28-Sep-2011 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 51 of 73

USAACET/R BIAS COMPLETED AT 7032.5 ACFT HRS.RED: 4.861/5.194, BLUE:4.130/4.467,YELLOW:4.865/5.198, BLACK: 4.160/4.495.

28-Sep-2011 2


DK237781

USAACEM/R RIG CK COMPLETED AT 7032.5 ACFT HRS.FWD=1/2 TURN SHORTEN, AFT=1/2 TURNLENGTHEN, LAT= NEUTRAL.

29-Sep-2011 1


DK237781

USAACECOMPLIED WITH H-60-12-SOF-01 @7034.6ACFT HRS.

08-Oct-2011 1


DK237781

USAACEH-60-12-SOF-02 (TAIL ROTOR INTERMEDIATEGEARBOX) C/W AT 7034.6 ACFT HRS.

11-Oct-2011 1


DK237781

USAACEH-60-12-SOF-03 (TAIL ROTOR INTERMEDIATEGEARBOX) C/W AT 7039.3 ACFT HRS. (AFS472)

15-Oct-2011 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT7041.1 ACFT HRS. R/H=145, L/H=145 AT 20DEGREES C STABILIZED.

17-Oct-2011 1


DK237781

USAACEAWR 1505, REV 3 DTD 21 OCT.09 5-MICRONMETAL MESH HYD FILTER SUPERECEEDED BYAWR 1505 R 4 DTD 21 OCT 11

22-Oct-2011 1


DK237781

USAACEH-60-11-AMAM-19 (IMMC LCF CHG 62REQUIREMENTS) C/W @ 7153.3 ACFT HRS

22-Oct-2011 2


DK237781

USAACEOPERATE WITH LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1639 DTD28 MAY 10 9BFT SUPERCEEDED BY AWR 1639R3 DTD 01 JUN 11 @ 7064.0 ACFT HRS

29-Oct-2011 1


DK237781

USAACECOMPLIED WITDH REQUIREMENTS OF H-60-12-AMAM-03- CMWS NOT COMPLIED WTH @7069.6 ACFT HRS

31-Oct-2011 1


DK237781

USAACEAWR 1455 DTD 23 OCT 09 , R1 BCAPSUPERECEDED BY AWR 1455 DTD 31 OCT 11R,2 @ 7069.6 ACFT HRS

01-Nov-2011 1


DK237781

USAACEAWR 1455 DTD 31 OCT 11 R2 SUPERCEDED BYAWR 1455 R3 DTD 10 NOV 11 AT 7123 ACFTHRS

21-Nov-2011 1


DK237781

USAACEOPERATE WITHIN LIMITATIONS ANDRESTRICTIONS SPECIFIED IN AWR 1153 R6,DATED 18 NOV 11

05-Dec-2011 1


DK237781

USAACECOMPLIED WITH REQ H-60-12-ASAM-02 (DRAGBEAM REPL) NLT 12 DEC 11 REV 6 @ 7150.3ACFT HRS

07-Dec-2011 1


DK237781

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


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 52 of 73

USAACEAWR 1639 R3 DTD -1 JUN 11 SUPERCEDED BYAWR 1800

20-Jan-2012 1


DK237781

USAACEAWR 1452 REV 1 DTD 29 DEC 09 SUPERCEDEDBY AWR 1452 R2 DTD 20 JAN 12

20-Jan-2012 2


DK237781

USAACEAWR 1639 R3 DTD 01 JUN 11 SUPERCEDED BYAWR 1800 DTD 30 NOV 11

21-Jan-2012 1


DK237781

USAACEDELAYED ENTRY - RIGHT HAND BEADEDPANEL HAS SEVEN CRACKED BEADS IN AROW WITH SOME ALREADY PATCH. REPAIRI/A/W MEC F74026B, A COPY OF THIS MEC ISLOCATED IN THE HISTORICAL RECORDS

30-Jan-2012 1


DK237781

USAACEDELAYED ENTRY - L/H CARGO DOOR UPPERTRACKS IS CRACKED AT 72 INCH FOR THEFWD END OF TRACK REPAIR IS AUTHORIZEDIAW MEC FR83961 DTD 04 NOV 08. A COPY OFTHIS MEC IS LOCATED IN THE HISTORICALRECORDS.

30-Jan-2012 2


DK237781

USAACEH-60-12-SOF-04: BREESE EASTERNEXTERNAL HOIST COMPLIED WITH( NO HOIST)INSTALLED @7218.4 ACFT HRS

18-Feb-2012 1


DK237781

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

27-Feb-2012 1


DK237781

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

28-Feb-2012 1


DK237781

USAACECOMPLIED WITH REQ OF H-60-12-ASAM-06(UPPER BULKHEAD FUEL SYSTEMBREAKAWAY VALVE AND FIREEXTINGUSHINGSYS DIRECTIONAL VALVE) AT 7243.2 ACFTHRS- NO FAULTS FOUND

01-Mar-2012 1


DK237781

USAACEOCM / ACE PERFORMED AT 7278.1 ACFT HRSBY TEM MEMBER QQ.

15-Mar-2012 1


DK237781

USAACEM/R RIG COMPLETED AT 7278.1 ACFT HRSMEASUREMENT FWD .25 FLAT CW, AFT.25FLAT, LAT .75 FLAT

17-Mar-2012 1


DK237781

USAACET/R BIAS COMPLETED @ 7278.1 ACFT HRS.READINGS ARE AS FOLLOWS: RED: 5.088-4.783 = .305, YELLOW: 5.119 - 4.815 = .304,BLUE: 4.352 - 4.050 = .305, BLACK: 4.413 -4.110= .303 CALIPER M/R 107020

20-Mar-2012 1


DK237781

USAACET/R CABLE TENSION COMPLETED AT 7278.1ACFT HRS R/H 157, L/H 156 @ 23.2 *C

20-Mar-2012 2


DK237781

USAACEINSP A675 FLIGHT CONTROL RODINSPECTION COMPLETED @ 7276.1 ACFT HRS

20-Mar-2012 3


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 53 of 73

USAACEACFT OPERATING IAW AWR 1648, R2 DTD 09MAR 12, MAGNUS LAPTOPS, SUPERSEDINGR1.

20-Mar-2012 4


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT7284 ACFT HRS L/H 165 R/H 165 TEMP 27 *C

27-Mar-2012 1


DK237781

USAACET/R BIAS COMPLETED @ 7278.1 ACFT HRS.READINGS ARE AS FOLLOWS: BLUE: 4.292-3.990 = .302, RED: 5.050 - 4.741 = .309, BLACK:4.334 - 4.030 = .304, YELLOW: 5.104 - 4.797=.307CALIPER M/R # 107020

28-Mar-2012 1


DK237781

USAACEM/R RIG COMPLETED @ 7278, NOADJUSTMENT

28-Mar-2012 2


DK237781

USAACET/R CABLE TENSION COMPLETED AT 7289.1R/H 157, L/H 156 @ 23.2 *C

29-Mar-2012 1


DK237781

USAACET/R CABLE TENSION COMPLETEDCOMPARISION FAILED (R/H 145, L/H [email protected]*C) @7287.0 ACFT HRS

02-Apr-2012 1


DK237781

USAACET/R CABLE TENSION CHECK - COMPELTEDFAILED) L/H 164, R/H164 @ 7287.0 ACFT HRS.

03-Apr-2012 1


DK237781

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

03-Apr-2012 2


DK237781

USAACET/R CABLE TENSION COMPLETED AT 7295.4ACFT HRS. (PASSED) L/H 159, R/H 159, @ 19.0DEG C

05-Apr-2012 1


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT7304.8 ACFT HRS WITH ADJUSTMENTS OF L/H170, R/H 169 TEMP 24.5 DEG *C STABILIZED

09-Apr-2012 1


DK237781

USAACEMAIN MOD FILTER BUTTON POPPED AT 7319.8ACFT HRS W/TSN 2823- REPLACED STAGE 1FILTER ELEMENT

12-Apr-2012 1


DK237781

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

03-May-2012 1


DK237781

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

08-May-2012 1


DK237781

USAACEINSP A670 CABIN TUB C/W @ 7326.8 ACFT HRS(48 MONTH INSPECTION).

25-May-2012 1


DK237781

USAACECOMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-17 (T/R INBOARD/OUTBOARDRETENTION PLATE SHIMS) @ 7326.8 ACFTHRS.

25-May-2012 2


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 54 of 73

USAACECOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-01 (TAIL ROTOR OUTPUT BEVEL GEARNONDESTRUCTIVE INSPECTION) @ 7326.8ACFT HRS.

25-May-2012 3


DK237781

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

25-May-2012 4


DK237781

USAACER/H DRAG BEAM ASSY SN:B367-2781P/N:70250-22010-042 REMOVED FOR CRACK @7326.8 ACFT HRS. IAW H-60-12-ASAM-02;REPLACED WITH R/H DRAG BEAM SN:C701-05779 PN:70250-222010-042.

29-May-2012 1


DK237781

USAACEMAIN ROTOR RIG CHECK READINGS: FWD: 0,AFT: 0, LAT:1. COMPLETED AT 7326.8 ACFTHRS.

01-Jun-2012 1


DK237781

USAACETAIL ROTOR BIAS READINGS: BLUE:4.386/4.053=.333, YELLOW: 5.209/4.877=.332,BLACK: 4.407/4.076=.331, RED:5.136/4.803=.333. COMPLETED AT 7326.8 ACFTHRS.

01-Jun-2012 2


DK237781

USAACETAIL ROTOR CABLE TENSION READINGS: L/H:176, R/H: 176 @ 30.2 C. COMPLETED AT 7326.8ACFT HRS.

01-Jun-2012 3


DK237781

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-12-AMAM-09 HYDRAULIC LINE CHAFE @7326.8

11-Jun-2012 1


DK237781

USAACEH-60-12-AMAM-09 (HYDRAULIC LINE CHAFE)COMPLIED WITH @ 7326.8 ACFT HRS.

11-Jun-2012 2


DK237781

USAACERECORDS MCDS SCRUB COMPLETED IAWPMO 11-018 DURING 720 HR PHASE INSP #12.COMPLETED AT 7326.8 ACFT HRS.

15-Jun-2012 1


DK237781

USAACET/R CABLE TENSION READINGS: L/H 156,R/H165. 21.8 DEG. COMP PASSED

19-Jun-2012 1


DK237781

USAACEH-60-12-AMAM-12 - MAINTENACE MANDATORY,ALL H-60-A/K/L SERIES AIRCRAFT,RESCINDED COMMON COMPONENT REMOVALDATE COMPLETED AT 7411.6 ACFT HRS

11-Jul-2012 1


DK237781

USAACEDELAYED ENTRY: MEC F139265, YOKE SNU01399 INSTALLED THIS ACFT. 2408-18 INSP881 (40HR) AND 882 (720HR) ADDED TOLOGBOOK. THIS YOKE MUST BE REMOVEDPRIOR TO ACFT TRANSFER. THIS ENTRY ISONLY VALID WHILE THIS SERIALIZED YOKE ISINSTALLED. THIS MEC IS NO LONGERAPPLICABLE TO THIS ACFT WHEN THISSERIALIZED YOKE IS REMOVED.

13-Jul-2012 1


DK237781

USAACEH-60-12-ASAM-08 , CARGO HOOK MANUALRELEASE SPRING ASSY COMPLETED AT7437.1 ACFT HRS

20-Jul-2012 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 55 of 73

USAACEAWR 1514 REV. 1 , DATED 03 AUG 10 (DGHS-P31) SUPERECEDED BY AWR 1514 R-2 DTD 27JUL 12

27-Jul-2012 1


DK237781

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


DK237781

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

01-Aug-2012 1


DK237781

USAACEAWR 1514: ACFT OPERATING IAW AWR 1514,R2 DTD 27JUL12, DGNS-P3I AN/ASN-128D ANDB KIT, SUPERSEDING ALL PRIOR VERSIONSOF THIS AWR.

01-Aug-2012 2


DK237781

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

02-Aug-2012 1


DK237781

USAACEH-60-12-ASAM-09 BREEZE EASTERNEXTERNAL RESCUE HOIST CARTRIDGEACTUATED DEVICE (CAD) ELECTRICALCONNECTOR C/W AS PER 730 FORM @ 7519.5ACFT HRS.

23-Aug-2012 1


DK237781

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

29-Aug-2012 1


DK237781

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

31-Aug-2012 1


DK237781

USAACEOIL FILTER IMPENDING BYPASS BUTTONPOPPED AT 7534.7 ACFT HRS W/TSN 3038

05-Sep-2012 1


DK237781

USAACECOMPLY WITH REQUIREMENTS OF H-60-12-AMAM-15 (TRIM ACTUATORS) C/W @ 7562.3ACFT HRS. (PASSED)

14-Sep-2012 1


DK237781

USAACECOMPLIED WITH THE REQUIRMENTS OF H-60-11-AMAM-17 (TR INBOARD/OUTBOARDRETENTION PLATE SHIMS COMPLETED AT7032.5 ACFT HRS

19-Sep-2012 1


DK237781

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

20-Sep-2012 1


DK237781

USAACECOMPLIED WITH THE REQ OF H-60-12-ASAM-07 (ELCETRICAL WIRE CHAFE) COMP AT7573.0 ACFT HRS

21-Sep-2012 1


DK237781

USAACEAWR 1455: ACFT OPERATING IAW AWR 1455,R4 DTD 18SEP12, BATTELLE CAP,SUPERSEDING ANY PRIOR REVISIONS OFTHIS AWR. THIS AWR ALSO REPLACES ISAQ123 (2 MAR 06)

21-Sep-2012 2


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 56 of 73

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


DK237781

USAACEM/R RIG CHECK COMPLETED AT 7631.6 ACFTHRS WITH FWD SHORTENED 3 FLATS, AFTLENGTHENDED 3 FLATS LAT SHORTENED 3FLATS

21-Oct-2012 1


DK237781

USAAACET/R BIAS ENTERED IN 2408-15 RECORDS RED(5.069-4.737=.332) FINAL DEGREE 3.1 BLACK(4.384-4.070=.314) FINAL DEGREE 3.1 YELLOW(5.047-4.708=.339) FINAL DEGREE 3.1 BLUE(4.364-4.054-.310) FINAL DEGREE 3.1 AT 7634.1ACFT HRS

25-Oct-2012 1


DK237781

USAACEM/R RIG COMPLETED AT 7634.1 ACFT HRSADJUSTMENTS WERE MADE; FWD 1/2 TURNSHORTEN, AFT;1/2 TURN LENGTHEN, LAT;NEUTRAL

01-Nov-2012 1


DK237781

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

01-Nov-2012 2


DK237781

USAACE720 HR PHASE #12 COMPLETED AT 7326.8ACFT HRS. PMI #13 DUE AT 8046.8 ACFT HRS.

01-Nov-2012 3


DK237781

USAACET/R CABLE TENSION CHECK COMPLETED AT7649.1 ACFT HRS L/H 155, R/H 155 @ 14.8 DEGC

07-Nov-2012 1


DK237781

USAACET/R CABLE TENSION COMPLETED, I/A/W TM1-1520-237-23 WP # 1747 00 . L/H=139 LBS.R/H=139 LBS. @ 8.8 DEGRESS CTENSIONMETER MR # 109407 THEROMETERMR # 112081 , PULLED EARLY, SEE OTHER2408-13-1 FOR NEW 9-11 HOUR T/R CABLETENSION CHECK @ 7640.1 ACFT HRS

07-Nov-2012 2


DK237781

USAACEH-60-13-AMAM-02 (AHRS) COMPLETED AT7646.8 ACFT HRS

09-Nov-2012 1


DK237781

USAACECOMPLY WITH THE REQUIREMENTS OF H-60-13-ASAM-01 (ANTI-COLLISON LIGHTS POWERSUPPLY) AT 7670.9 ACFT HRS

29-Nov-2012 1


DK237781

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-13-AMAM-03 (DIGITAL ENG CONTROLUNIT/ELECTRONIC) AT 7670.9 ACFT HRS

29-Nov-2012 2


DK237781

USAACECOMPLY WITH THE REQ OF H-60-13-AMAM-04(CHANGE 63) AT 7710.3 ACFT HRS

08-Jan-2013 1


DK237781

USAACEAWR 1452: ACFT OPERATING IAW AWR 1452,R3 DTD 18JAN13, LC-6 DIGITALCHRONOMETER, SUPERSEDING ANY PRIORVERSIONS OF THIS AWR AND REPLACINGISAQ 113 AND ALL REVISIONS.

18-Jan-2013 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 57 of 73

USAACECOMPLIED WITH THE REQ OF H-60-13-AMAM-05 (MLG BRAKES) AT 7736.2 ACFT HRS

24-Jan-2013 1


DK237781

USAACEMEC F160434, AUTHORIZATION GRANTED TOTEST #1 MAIN FUEL CHECK VALVE BYINCREASING THE PRESSURE IN STEP 28,WP1013, UP TO BUT NOT EXCEEDING 60 PSI.7746.9 ACFT HRS.

31-Jan-2013 1


DK237781

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


DK237781

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-13-AMAM-06 (CEFS) NOT APPLICABLE TOTHIS ACFT @ 7764.2 ACFT HRS

12-Feb-2013 1


DK237781

USAACEMEC F139265 NO LONGER APPLICABLE, TWYOKE U01399 REMOVED THIS DATE.

27-Feb-2013 1


DK237781

USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-03 (MR SPINDLE ANTI-FLAPASSEMBLIES) @ 7813.0 A/C HOURS

01-Mar-2013 1


DK237781

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

01-Mar-2013 2


DK237781

USAACETRANSMISSION S/N A26500946 FILTERBUTTON POPPED AT 7839.3 ACFT HRS W/SN3342, REPLACED THE FILTER IAW WP0657 TM1-1520-237-23 1 ST TIMEIN 200 FLT HRS

13-Mar-2013 1


DK237781

USAACEDELAYED ENTRY: ACFT NO LONGEROPERATING IAW MEO A6055 DUE TO BLUEM/R DROOP STOP BUSHING REPLACED.COMPLETED AT 6616.1 ACFT HRS. (TP011634)

23-Mar-2013 1


DK237781

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-13-ASAM-04 PLASTIC MEDIA BLAST (PMB)OXIDE FLAKE AT 7856.2 ACFT HRS

23-Mar-2013 2


DK237781

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


DK237781

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-13-AMAM-07 (LOAD DEMAND SPINDLE CABLECLEARANCE) AT 7868.5 ACFT HRS

01-Apr-2013 1


DK237781

USAACECOMPLIED WITH THE REQUIREMENTS OF H-60-13-ASAM-05 (ELECTRIC RESCUE HOIST) AT7881.1 ACFT HRS

09-Apr-2013 1


DK237781


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 58 of 73

USAACEACFT BEING OPERATED IAW MEO A6055 REVC FOR M/R DROOP STOP BUSHINGDISBONDED. REPL OF M/R DROOP STOPBUSHING DUE AT NEXT PMI 8046.8 HRS

11-Apr-2013 1


DK237781

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

11-Apr-2013 2


DK237781

USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-06 (PMI CHECKLIST CHANGES) @7932.9 A/C HOURS.

17-Apr-2013 1


DK237781

USAACEAWR 1452: ACFT OPERATING IAW AWR 1452,R4 DTD 12APR13, LC-6 DIGITAL CLOCK,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR AND ISAQ 113.

17-Apr-2013 2


DK237781

USAACEH-60-13-SOF-01 DOES NOT APPLY TO THISACFT. ACFT NON AHRS @ 7972.6 A/C HRS.

31-May-2013 1


jennifer.m.staley

L-3 RASM-EOCM/ACE PERFORMED AT 8013.7 ACFT HRS.BY TEAM MEMBERS P AND QQ.

26-Jun-2013 1


jacob.a.weikart

L-3 RASM-EOCM/ACE PERFORMED AT 8013.7 AIRCRAFTHOURS BY TEAM MEMBERS P AND QQ

26-Jun-2013 2


DK237781

USAACECOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-11 @ 8017.4 ACFT HRS (AFS 594)

03-Jul-2013 1


jennifer.m.staley

USAACEPRIMARY SERVO CONTROL ROD BIAS FWD=0: LAT =3 SHORTENED.

14-Jul-2013 1


jennifer.m.staley

USAACEGEN-13-AMAM-04 AN/APN-209 RADARALTIMETER SET COMPONENT TRACKINGCOMPLETED AT 8025.8 ACFT HRS.

15-Jul-2013 1


jennifer.m.staley

USAACELATE ENTRY: H-60-13-AMAM-01 FLIGHTCONTROL RIGGING PROCEDURES P/C/W 31OCT 12 AT 7632.1 ACFT HRS.

05-Aug-2013 1


tony.barnes

L-3 AFMH-60-13-ASAM-10 WOODWARD HMU P3 TUBECOMPLIED WITH @ 8045.5 ACFT HOURS.

28-Aug-2013 1

SAAF FT.BRAGG

WR849100

L-3 AFMH-60-13-AMAM-10 LCF CHANGE 64 COMPLIEDWITH @ 8045.5 ACFT HOURS

28-Aug-2013 2

SAAF, FT.BRAGG ,NC

WR849100

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

29-Aug-2013 1


dean.a.keirn

L-3 AFMH-60-13-AMAM-15 (CEFS) COMPLIED WITH N/ATHIS ACFT SYSTEM NOT INSTALLED @ 8045.5ACFT HOURS.

26-Sep-2013 1

SAAF, FT. BRAGG, NC

WR849100


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 59 of 73

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

L-3 AFMH-60-14-SOF-01 (BREEZE EASTERN EXTERNALRESCUE HOIST INSTALLATION) COMPLIEDWITH, NOT INSTALLED @ 8045.5 ACFT HOURS.

01-Nov-2013 1

SAAF, FT. BRAGG, NC

WR849100

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

AFM/L3COMPLIED WITH THE REQUIREMENTS OF H-60-14-AMAM-03 AT 8045.5 ACFT HRS(DISCREPANT CONNECTNG LINKS)

23-Dec-2013 1

FT BRAGG, NC 28310-5000

RG000820

L-3 AFMDURING ASER/AIM INSPECTION THE LHOUTBOARD DRAG BEAM FITTING LUG WASFOUND TO BE GROOVED. REPAIRED LUG IAWMEC# 176353 @ 8045.5 ACFT HRS

31-Dec-2013 1

FT. BRAGG, NC

WR849100

L-3 AFMDURING ASER/AIM INSPECTION THE RHCOPILOTS FWD SEAT TRACK FITTING WASFOUND TO HAVE ELONGATED HOLES.REPLACED FITTING IAW MEC# F171834 @8045.5 ACFT HRS

31-Dec-2013 2

FT. BRAGG, NC

WR849100

L-3 AFMDURING ASER/AIM INSPECTION THE LHCOPILOTS FWD SEAT TRACK FITTING WASFOUND TO HAVE ELONGATED HOLES.REPLACED FITTING IAW MEC# F171835 @8045.5 ACFT HRS

31-Dec-2013 3

FT.BRAGG,NC

WR849100

L-3 AFMDURING ASER/AIM INSPECTION THE RHPILOTS FWD SEAT TRACK FITTING WASFOUND TO HAVE ELONGATED HOLES.REPLACED FITTING IAW MEC# F171832 @8045.5 ACFT HRS

31-Dec-2013 4

FT.BRAGG,NC

WR849100

L-3 AFMDURING ASER/AIM INSPECTION THE LHPILOTS FWD SEAT TRACK FITTING WASFOUND TO HAVE ELONGATED HOLES.REPLACED FITTING IAW MEC# F171836 @8045.5 ACFT HRS

31-Dec-2013 5

FT.BRAGG,NC

WR849100

L-3 AFMH-60-14-ASAM-04 MAIN ROTOR HUB ASSYCOMPLIED WITH @ 8045.5 ACFT HOURS.

31-Dec-2013 6

FT.BRAGG,NC

WR849100

L-3 AFMDURING ASER/AIM INSPECTION THE LHUPPER STA 295 FRAME WAS FOUND DO BEDAMAGED BEYOND LIMITS IN WEB AND HADSEVERAL ELONGATED HOLES. REPAIRED LHUPPER STA 295 FRAME IAW MEC # F174131A@ 8045.5 ACFT HOURS.

11-Feb-2014 1

FT.BRAGG,NC

WR849100

L-3 AFMH-60-14-AMAM-05 LCF CHANGE 65 COMPLIEDWITH @ 8045.5 ACFT HOURS

11-Feb-2014 2

FT.BRAGG,NC

WR849100

L-3 AFMDURING ASER/AIM INSPECTION THE AFTXMSN BEAM WAS FOUND TO BE OUT OFALLIGNMENT AND GAP WAS OUT OF LIMITS.AFT XMSN BEAM WAS ADJUSTED ANDREALLIGNED BY CCAD FEILD TEAM IAW MEC#F174819 @ 8045.5 ACFT HOURS.

11-Feb-2014 3

FT.BRAGG,NC

WR849100


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 60 of 73

L-3 AFMDURING ASER/AIM INSPECTION THE FWDXMSN BEAM WAS FOUND TO BE GOUGED ONLH FWD BELLCRANCK SUPPORT MOUNT PADTHAT INTERSECTS INTO BUSHING HOLE. FWDXMSN BEAM WAS REPLACED BY CCAD FEILDTEAM IAW MEC # 174128 @ 8045.5 ACFTHOURS.

11-Feb-2014 4

FT.BRAGG,NC

WR849100

CSCAT 6736.9 ACFT HRS BY TEAM MEMBER R.AFMA RASM-E

18-Feb-2014 1

FT. CAMPBELL, KY42223

DK237781

L-4 AFMH-60-14-AMAM-08 AN/ASC-15ECOMMUNICATION CONSOLE COMPLIED WITH.NOT INSTALLED @ 8045.5 ACFT HOURS.

05-Mar-2014 1

FT.BRAGG,NC

WR849100

AFMAMEC F181057, AUTHORIZATION IS GRANTEDTO REPLACE THE OVERSIZE BUSHING IN THETAIL CONE CANTED BULKHEAD IAW DMWR 1-1520-237, WP 0170 00.

20-Mar-2014 1

FT. BRAGG, NC

tite.mahone

CCADDURING ASER/AIM INSPECTION THE RHLOWER 308 BEAM WAS FOUND TO HAVE AREPAIR ON IT THAT REQUIRED A 90 DAYRECURRING INSPECTION ON IT IAW MEC#F74026B. THE RH LOWER 308 BEAM WASREPLACED BY CCAD FIELD TEAM IAW MEC#F174158B AND IN CONJUNCTION WITHMEC#F178080B @ 8045.5 ACFT HOURS.

02-Apr-2014 1

FT.BRAGG,NC

quality.control

L-3 AFMDURING ASER/AIM INSPECTION THE UPPER308 BEAM WAS FOUND TO HAVE ANUNAUTHORIZED REPAIR ON IT. THEREPLACEMENT OF SERVERAL ITEMS WEREINCORPARATED INTO MEC #F178080B. RHAND LH BEADED PANEL 50-5 KITS, RH ANDLH 34.5 BEAMS WITH 50-7 KITS, FWD ANDAFTXMSN BEAMS, ALL FOUR SERVO BEAMFITTINGS, RH LOWER 308 BEAM AND THEUPPER 308 BEAM WERE ALL REPACEDAND/OR ADJUSTED BY CCAD FEILD TEAM IAWMEC #F178080B. @ 8045.5 ACFT HOURS.

02-Apr-2014 2

FT.BRAGG,NC

WR849100

L-3 AFMH-60-14-ASAM-06 (MIXER ASSY) COMPLIEDWITH @ 8045.5 ACFT HOURS

15-Apr-2014 1

FT.BRAGG,NC

WR849100

L-3 AFMH-60-14-AMAM-12 SPINDLE NUT RETIREMENTLIFE EXTENTION COMPLIED WITH @ 8045.5ACFT HOURS

23-Apr-2014 1

FT.BRAGG,NC

WR849100

L-3 AFMH-60-14-AMAM-14 IVHMS CABLING COMPLIEDWITH IVHMS NOT INSTALLED @ 8045.5 ACFTHOURS

30-May-2014 1

FT.BRAGG,NC

WR849100

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

L-3 AFMH-60-14-SOF-03 DISCREPANT SELF LOCKINGDOUBLE HEXAGON NUTS COMPLIED WITH @8045.5 ACFT HOURS

30-Jun-2014 1

FT.BRAGG,NC

WR849100


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 61 of 73

L-3 AFMAIRCRAFT BEING OPERATED WITHINLIMITATION AND RESTRICTIONS SPECIFIED INAWR 1800 R2, DATED 22 MAR 13. (BFT/EDM)@8045.5 ACFT HOURS

07-Jul-2014 1

FT.BRAGG,NC

WR849100

L-3 AFMAIRCRAFT BEING OPERATED WITHINLIMITATION AND RESTRICTIONS SPECIFIED INAWR 1514 R2, DATED 27 JUL 12. (DGNS)@8045.5 ACFT HOURS

07-Jul-2014 2

FT.BRAGG,NC

WR849100

L-3 AFMAIRCRAFT BEING OPERATED WITHINLIMITATION AND RESTRICTIONS SPECIFIED INAWR 1681 R4, DATED 30 APR 14. (EH 60ADEMOD)@ 8045.5 ACFT HOURS

07-Jul-2014 3

FT.BRAGG,NC

WR849100

L-3 AFMAIRCRAFT BEING OPERATED WITHINLIMITATION AND RESTRICTIONS SPECIFIED INAWR 1455 R4, DATED 18 SEP 12. (BATTELLECAUTION ADVISORY PANEL) @ 8045.5 ACFTHOURS

07-Jul-2014 4

FT.BRAGG,NC

WR849100

L-3 AFMAIRCRAFT BEING OPERATED WITHINLIMITATION AND RESTRICTIONS SPECIFIED INAWR 1452 R4, DATED 12 APR 13. (L-6DIGITALCHRONOMETER) @ 8045.5 ACFTHOURS

07-Jul-2014 5

FT.BRAGG,NC

WR849100

L-3 AFMAIRCRAFT BEING OPERATED WITHINLIMITATION AND RESTRICTIONS SPECIFIED INAWR 1750 R2, DATED 29 MAR 13.WHENFLYINGWITH ANIS AN/AVS-6 SERIES NVGS.@ 8045.5ACFT HOURS

07-Jul-2014 6

FT.BRAGG,NC

WR849100

L-3 AFMAIRCRAFT BEING OPERATED WITHIN L-3/AFMLIMITATION AND RESTRICTIONSSPECIFIED IN AWR 1505 R5, DATED 18 OCT 13(5 MICRONMETAL MESH HYDRAULIC FILTERAND THE HYDRAULIC SYSTEM SAMPLINGVALVE INSTALLED) @ 8045.5 ACFT HOURS

07-Jul-2014 7

FT.BRAGG,NC

WR849100

L-3 AFMAIRCRAFT BEING OPERATED WITHINLIMITATION AND RESTRICTIONS SPECIFIED INAWR 1444 R6, DATED 11 JUL 13.(SINGLEAHRU) @ 8045.5 ACFT HRS

07-Jul-2014 8

FT.BRAGG,NC

WR849100

L-3 AFM48 MONTH FUEL CELL INSPECTIONCOMPLETED @ 8045.5 ACFT HOURS. BOTHFUEL CELLS, LINERS AND FOAMWEREREMOVED AND REPLACED

07-Jul-2014 9

FT.BRAGG,NC

WR849100

L-3 AFM48 MONTH CABIN TUB INSPECTIONCOMPLETED @ 8045.5 ACFT HOURS.

07-Jul-2014 10

FT.BRAGG,NC

WR849100

L-3 AFMTAIL ROTOR RIGGED IAW ADDENDUM 1 TO H-60-13-AMAM-01.COMPLETED @ 8045.5 ACFTHOURS. TAIL ROTOR CABLE TENSION SET@TEMP 30 C LEFT CABLE 173, AND RIGHTCABLE 175. BLADE AGLES:BLADE SETDIM ADIM B DIFF FINAL ANGLE RED-0.6 4.703 5.0020.299 2.9 DEG BLACK -0.3 4.024 4.342 0.318 3.0DEG YELLOW -0.3 4.785 5.080 0.295 2.9 DEGBLUE 0.1 4.047 4.350 0.303 2.9 DEG

07-Jul-2014 11

FT.BRAGG,NC

WR849100


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 62 of 73

L-3 AFMMAIN ROTOR RIGGED IAW ADDENDUM 1 TO H-L-3/AFM60-13-AMAM-1. BLADE ANGLES: LOWCOLLECTIVE = -0.650, HIGH COLLECTIVE=15.125, FWD CYCLIC = 33.6, AFT CYCLIC =20.9, LEFT CYCLIC = 15.4, RIGHT CYCLIC =14.7.THE PRIMARY SERVO CONTROL RODSWERE ADJUSTED AS FOLLOWS: NOADUSTMENTSMADE ON FWD AND AFTPRIMARY SERVO CONTROL RODS AFT BIAS.LATERAL PRIMARY SERVO CONTROL RODWAS LENGTHENED 2 FLATS. MAIN ROTOR RIGWAS COMPLETED @ 8045.5 ACFT HOURS.

07-Jul-2014 12

FT.BRAGG,NC

WR849100

L-3 AFM48 MONTH FLIGHT CONTROL RODINSPECTION COMPLETED @ 8045.5 ACFTHOURS

07-Jul-2014 13

FT.BRAGG,NC

WR849100

L-3 AFMH-60-14-AMAM-16 (AHRU TRACKING)COMPLIED WITH @ 8045.5 ACFT HOURS.

15-Jul-2014 1

FT.BRAGG,NC

WR849100

L-3 AFMTAIL ROTOR RIG CHECK COMPLETED IAWADDENDUM 1 TO H-60-13-AMAM-01.COMPLETED @ 8045.5 ACFTHOURS.BLADEAGLES: DIM A DIM B DIFFFINAL ANGLE RED 4.683 5.003 0.3203.0 DEGBLACK 4.064 4.369 0.305 3.0 DEG YELLOW4.716 5.051 0.335 3.0 DEG BLUE 4.029 4.3460.317 3.1 DEG

22-Jul-2014 1

FT.BRAGG,NC

WR849100

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

L-3 AMCOM, RASM-EACE COMPLETED @ 8045.5 ACFT HRS BY ACETEAM MEMBERS D AND L L-3 AMCOM, RASM-E

28-Jul-2014 1

FT.BRAGG,NC

SD928779

L-3 AFMTB 1-1520-237-ASER COMPLETED @ 8045.5ACFT HOURS. PMI #1 AND PMI #2 WERECOMPLETED INCONJUNCTION WITH TB 1-1520-237-ASER. NEXT PMI DUE @ 8405.5 ACFTHOURS

28-Jul-2014 2

FT.BRAGG,NC

WR849100

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

31-Jul-2014 1


dean.a.keirn

L-3 AFMH-60-14-ASAM-09 ENGINE OUTPUT SHAFTCOMPLIED WITH @ 8048.5 ACFT HOURS

04-Aug-2014 1

FT.BRAGG,NC

WR849100

L-3 AFMTAIL ROTOR RIG CHECK COMPLETED IAWADDENDUM 1 TO H-60-13-AMAM-01.COMPLETED @ 8048.5 ACFT HOURS.BLADE ANGLES: NO BIAS ADJUSTMENTSWERE MADE. BLADE ANGLES FELL WITHINRANGE OF RIGCHECK. PREVIOUS BLADEANGLES SET AS FOLLOWS: DIM A DIM B DIFFFINAL ANGLE RED 4.683 5.003 0.320 3.0 DEGBLACK 4.064 4.369 0.305 3.0 DEG YELLOW4.716 5.051 0.335 3.0 DEG BLUE 4.029 4.3460.317 3.1 DEG

13-Aug-2014 1

FT.BRAGG,NC

WR849100


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 63 of 73

L-3 AFMAIRCRAFT BEING OPERATED WITHINLIMITATION AND RESTRICTIONS SPECIFIED INAWR 1514 R3 DATED 31 JUL 14. (DGNS) @8048.5 ACFT HOURS

14-Aug-2014 1

FT.BRAGG,NC

WR849100

L-3 AFMAS PART OF TB 1-1520-237-ASER, AIRCRAFTWAS PAINTED IAW TM 55-1500-345-23 @ 8048.5ACFT HOURS

20-Aug-2014 1

FT.BRAGG,NC

WR849100

USAACEACFT TRANSFERRED TO THIS LOCATION.UPON RECEIPT, THE ACFT IS/WILL BEOPERATING IAW THE FOLLOWING AWRS: 1153R7 24AUG12 JP8-100, 1220 R8 01NOV12 ESM,1251 R9 06JUN14 EYEBOLTS, 1444 R7 14APR14SINGLE AHRS, 1452 R412APR13 DIG CLOCK,1455 R4 18SEP12 BATTELLE CAP, 1505 R603JUN14 5M HYD FILTERS, 1514 R3 31JUL14DGNS, 1648 R3 28MAR14 MAGNUS LAPTOP,1681 R4 30APR14 EH DEMOD, 1738 R101FEB13 AN/APX118, 1750 R2 29MAR13AN/AVS-6 NVG, 1800 R3 16JUL14 EDM/BFT.

04-Sep-2014 1


dean.a.keirn

USAACEH-60-14-SOF-04 (OPERATORS ANDCREWMEMBERS CHECKLIST) C/W 08 SEP 14AT 8052.2 ACFRT. HRS

08-Sep-2014 1


anthony.s.speigner

USAACEH-60-14-ASAM-10 (MAIN TRANSMISSIONPLANETARY CARRIER ASSEMBLY) C/W AT8052.2 ACFT HRS.

10-Sep-2014 1


jimmy.s.caylor

USAACET/R BIAS WORKSHEET BLADE ANGLEMEASUREMENTS: RED: 1ST DEG 3.2, 2ND DEG3.2, FINAL DEG 3.2 BLACK: 1ST DEG 2.9, 2NDDEG 2.9, FINAL DEG 2.9 YELLOW: 1ST DEG 3.2,2ND DEG 3.2, FINAL DEG 3.2 BLUE: 1ST DEG2.9, 2ND DEG 2.9 FINAL DEG 2.9

14-Sep-2014 1


jimmy.s.caylor

USAACET/R CABLE TENSION CHECK COMPLETED AT8057.6 ACFT HRS. R/H 153 LBS, L/H 155 LBS @26.8 DEGREES C.

14-Sep-2014 2


jimmy.s.caylor

USAACET/R CABLE TENSION CHECK COMPLETED AT8067.4 ACFT HRS. R/H 140, L/H 138 AT 22.6DEGREES CELSIUS.

20-Sep-2014 1


jimmy.s.caylor

USAACET/R CABLE TENSION CHECK COMPLETED AT8077.3 ACFT HRS. L/H 135 R/H 135 AT 20.9DEGREES C.

27-Sep-2014 1


jimmy.s.caylor

USAACEMEC F190476, YOKE SN U4266:AUTHORIZATION GRANTED TO RESEAT LOCKPIN BUSHING PER INSTRUCTIONS CONTAINEDIN MEC. 8081.5 ACFT HRS.

03-Oct-2014 1


dean.a.keirn

USAACET/R CABLE TENSION CHECK COMPLETED AT8086.4 ACFT HRS. L/H 140, R/H 140 AT 21.3DEGREES C.

08-Oct-2014 1


jimmy.s.caylor

USAACEMEC F191393, YOKE SN U2853:AUTHORIZATION GRANTED TO RESEAT LOCKPIN BUSHING PER INSTRUCTIONS CONTAINEDIN MEC. 8107.8 ACFT HRS

23-Oct-2014 1


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 64 of 73

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) @ 8119.2 ACFT HRS

29-Oct-2014 1


carolyn.m.bailey

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

03-Nov-2014 1


dean.a.keirn

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

03-Nov-2014 2


dean.a.keirn

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

07-Nov-2014 1


dean.a.keirn

USAACECOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-19 (ULLS-A (E), LCF CHANGE 66)COMPLIED WITH AT 8149.6 ACFT HRS.

07-Nov-2014 2


carolyn.m.bailey

USAACECOMPLIED WITH H-60-15-ASAM-01, LEDCAUTION ADVISORY PANEL @ 8163.0 ACFTHRS

22-Nov-2014 1


carolyn.m.bailey

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

25-Nov-2014 1


anthony.s.speigner

USAACEH-60-15-AMAM-05 AHR EMERGENCEYPROCEDURES REQUIREMENTS COMPLETEDAT 8169.4

16-Dec-2014 1


OW0950

USAACEDELAYED ENTRY: ACFT OPERATING UNDERMEO A6116 INSTALLATION OF FUEL FLAG FORE/UH-60 FLEET @ FT RUCKER, AL ACFTCURRENT HRS 8220.7

27-Jan-2015 1


carolyn.m.bailey

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

USAACEH-60-15-AMAM-06(IDENTIFICATION OFAVIATION SURVIVABILITY EQUIPMENT) C/W AT8270.8 ACFT HRS.

23-Feb-2015 1


kenneth.e.griffin


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 65 of 73

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

04-Mar-2015 1


dean.a.keirn

USAACEMEC F191393A, BUSHING IN THE TLG YOKEWAS FOUND DISBONDED AT 8282.0 ACHOURS. THE BUSHING WAS REMOVED, THEBORE WAS MEASURED, AND IT WAS WITHINTM LIMITS. AUTHORIZATION GRANTED TOREINSTALL BUSHING WITH 9309.3NA IF/WHENTHE BORE IS WITHIN TM LIMITS.

12-Mar-2015 1


dean.a.keirn

USAACEMAIN MOD S/N A265-00946 WITH TSN: 3788IMPENDING BYPASS BUTTON POPPED.REPLACED M/MOD OIL FILTERS & INSPECTEDCHIP DETECTOR & SCREEN. NO CHIPSPRESENT AT ACFT HRS 8285.

25-Mar-2015 1


kenneth.e.griffin

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

USAACEH-60-15-ASAM-03(TROOP/GUNNER SEATENERGY ATTENUATORS) C/W AT 8328.2 ACFTHRS.

15-Apr-2015 1


kenneth.e.griffin

USAACEGEN-12-AMAM-07(AIRCRAFT FIRST AID KITMODERNIZATION) C/W AT 8338.4 ACFT HRS.

21-Apr-2015 1


kenneth.e.griffin

USAACEACFT OPERATING IAW AWR 1452, R5 DTD10APR15, DIGITAL CLOCK, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR AND ISAQ 113.

22-Apr-2015 1


dean.a.keirn

USAACEMEC F194446, YOKE SN U4120 REPAIREDUNDER THIS MEC INSTALLED THIS ACFT AT8341 ACFT HRS. THIS YOKE MUST BEREMOVED PRIOR TO ACFT TRANSFER. THISENTRY IS ONLY VALID WHILE THISSERIALIZED YOKE IS INSTALLED. THIS MEC ISNO LONGER APPLICABLE TO THIS ACFTWHEN THIS SERIALIZED YOKE IS REMOVED.

23-Apr-2015 1


dean.a.keirn

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

13-May-2015 1


dean.a.keirn

USAACEH-60-15-AMAM-10(AV-DEC GASKETINSPECTION) C/W AT 8370.6 ACFT HRS.

22-May-2015 1


kenneth.e.griffin

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

28-May-2015 1


dean.a.keirn

USAACEH-60-15-AMAM-11(MODE-S TRANSPONDERADDRESS REVIEW) C/W AT 8370.7 ACFT HRS.

29-May-2015 1


kenneth.e.griffin


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 66 of 73

USAACEACFT OPERATING IAW AWR 1681, R5 DTD22JUN15, EH DE-MOD, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR AND AWRS927 AND 890.

24-Jun-2015 1


dean.a.keirn

USAACEMEO A6055 IS NO LONGER APPLICABLE DUETO REPLACEMENT OF BLUE M/R BLADEDROOP STOP BUSHINGS AT 8410.4 ACFT HRS.

11-Jul-2015 1


kenneth.e.griffin

USAACET/R BIAS WORKSHEET C/W AT 8410.4 ACFTHRS. BLADE BLADE SET (DEG) 1ST (DEG) 2ND(DEG) FINAL (DEG) DIM A DIM B DIFFERENCEPID RED .2 3.0 3.0 3.0 4.692 5.015 .323RH014623 BLACK .3 3.0 3.0 3.0 4.03 4.36 .33RH014623 YELLOW .1 3.0 3.0 3.0 4.7 5.03 .33RH014623BLUE.23.03.03.04.0144.344.33RH014623

13-Jul-2015 1


kenneth.e.griffin

USAACET/R CABLE TENSION CHECK: L/H 150, R/H 150@ 29 DEG C C/W AT 8410.4 ACFT HRS.

13-Jul-2015 2


kenneth.e.griffin

DCR RASM-COCM/ACE PERFORMED AT 8410.4 AIRCRAFTHOURS BY TEAM MEMBERS P AND UU

14-Jul-2015 1


jacob.a.weikart

USAACEH-60-15-AMAM-14 LEGITIMATE CODE FILE(LCF) CHANGE 67 REQUIREMENTS C/W AT8422.7

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

USAACET/R CABLE TENSION CHECK READINGS: L/H140, R/H 140 AT 28.8 DEGREES C AT 8430.2ACFT HRS.

29-Jul-2015 1


kenneth.e.griffin

USAACEACFT FLOWN OVER SALTWATER. FRESHWATER RINSE COMPLETED AT 8457.2 ACFTHRS.

15-Sep-2015 1


kenneth.e.griffin

USAACEH-60-15-SOF-02(FAST ROPEINSERTION/EXTRACTION SYSTEM(FRIES)RELEASE CABLE) C/W AT 8462.7 ACFT HRS.

24-Sep-2015 1


kenneth.e.griffin

USAACEACFT OPERATING IAW AWR 1965 R1, DTD 16SEP 15, APPLE IPAD DEVICES, SUPERSEDINGALL PRIOR VERSIONS OF THIS AWR.

14-Oct-2015 1


kenneth.e.griffin

USAACEH-60-15-AMAM-18(MEDICAL EVACUATION(MEDEVAC) CAROUSEL) C/W AT 8481.3 ACFTHRS.

15-Oct-2015 1


kenneth.e.griffin

USAACEH-60-16-AMAM-01(ENGINE INLET BARRIERFILTER (EIBF) FRAMES) C/W AT 8494.6 ACFTHRS.

27-Oct-2015 1


kenneth.e.griffin

USAACEH-60-16-ASAM-01(INBOARD RETENTION PLATETORQUE CHECKS) C/W AT 8510.5 ACFT HRS.

10-Nov-2015 1


kenneth.e.griffin


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 67 of 73

USAACEACFT BEING OPERATED IAW MEO A6055 REVC FOR M/R DROOP STOP BUSHINGDISBONDED. REPLACEMENT OF BUSHINGDUE AT NEXT PMI AT 8765.5 ACFT HRS.

19-Nov-2015 1


kenneth.e.griffin

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

01-Dec-2015 1


dean.a.keirn

USAACEACFT NO LONGER OPERATING IAW AWR 1649R3 (MAGNUS LAPTOP)

22-Dec-2015 1


chelsey.p.phillips

USAACEACFT OPERATING IAW AWR 1913 R1 DATED06NOV15 (ACN ELECTRONIC LAPTOP)

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

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

USAACEH-60-16-ASAM-02(DEFECTIVE FUEL HOSES)C/W AT 8536.9 ACFT HRS.

08-Jan-2016 2


kenneth.e.griffin

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

USAACEM/MOD S/N: A265-00946 WITH TSN: 4094FILTER IMPENDING BYPASS BUTTON POPPED.SERVICEABILITY INSPECTION COMPLETEDON ACFT 8724660 AT 8591.4 ACFT HRS.

29-Feb-2016 1


kenneth.e.griffin

USAACEACFT OPERATING IAW AWR 1681, R6 DTD13APR16, EH60A DEMOD, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR AND AWRS927 AND 890.

13-Apr-2016 1


dean.a.keirn

USAACEM/R RIG CHECK C/W AT 8656.4 ACFT HRS.CONTROL POSITION 90DEG RT 180DEG FWD270DEG LEFT 0DEG AFT TOTAL AVG COLL.RANGE (HI-LO) LOW COLL ANGLE 8.1 -2.5 -10.4-0.3 -5.1 -1.275 HIGH COLL ANGLE 18.5 12.813.6 17.6 62.5 15.625 16.9 FWD CYCLIC ANGLE -3.2 30.1 33.3 AFT CYCLIC ANGLE 26.3 7.3 19LEFT CYCLIC ANGLE -9.1 6.9 16 RT CYCLICANGLE 6.8 -8.1 14.9

06-May-2016 1


kenneth.e.griffin

USAACEACFT OPERATING IAW AWR 1800, R5 DTD27APR16, SINGLE EDM AND/OR BFT,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR AND AWR'S 1284, 1347, 1414 AND 1639.

13-May-2016 1


kenneth.e.griffin


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 68 of 73

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(TRANSPONDER BATTERYREPLACEMENT) C/W AT 8674.8 ACFT HRS.

04-Jun-2016 1


kenneth.e.griffin

USAACEH-60-16-SOF-01(UPPER CABIN STATION (STA)379 FRAME CRACKING) C/W AT 8685.9 ACFTHRS.

21-Jun-2016 1


kenneth.e.griffin

USAACEH-60-16-AMAM-09(ULLS-A(E) COMPONENTPN/SN DUPLICATIONS) C/W AT 8685.9 ACFTHRS.

21-Jun-2016 2


kenneth.e.griffin

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 HOIST OPERATIONALRESTRICTIONS) C/W AT 8742.7 ACFT HRS.

15-Aug-2016 1


kenneth.e.griffin

USAACEH-60-16-ASAM-06(IMPROVED TAIL ROTORQUADRANT SUPPORT) C/W AT 8747.8 ACFTHRS.

25-Aug-2016 1


kenneth.e.griffin

USAACEH-60-16-AMAM-10(ULLS-A(E) PHASE LCFUPDATES) C/W AT 8752.3 ACFT HRS.

02-Sep-2016 1


kenneth.e.griffin

USAACEACFT NO LONGER OPERATING IAW MEOA6055 DUE TO M/R DROOP STOP BUSHINGREPLACED AT 8752.3 ACFT HRS.

08-Sep-2016 1


kenneth.e.griffin

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

URS RASM-COCM/ACE PERFORMED AT 8752.3 AIRCRAFTHOURS BY TEAM MEMBERS P AND WW

26-Sep-2016 1


jacob.a.weikart

USAACEH-60-17-ASAM-01(ULLS-A(E) CADS MODULE)C/W AT 8753.3 ACFT HRS.

06-Oct-2016 1


kenneth.e.griffin

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


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 69 of 73

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

26-Oct-2016 2


joanna.n.lucier

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

27-Oct-2016 1


dean.a.keirn

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

01-Nov-2016 1


dean.a.keirn

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

12-Dec-2016 1


dean.a.keirn

USAACEH-60-17-SOF-01(RESCUE HOIST EMERGENCYPROCEDURES CHANGES) C/W AT 8753.3 ACFTHRS.

21-Dec-2016 1


KG4191

USAACEH-60-17-AMAM-01(ULLS-A(E) LCF CHANGE 68)C/W AT 8753.3 ACFT HRS.

21-Dec-2016 2


KG4191

USAACEH-60-17-ASAM-04(AIRFRAME STRUCTURALPARTS) C/W AT 8753.7 ACFT HRS.

06-Jan-2017 1


KG4191

USAACEMEC F321441, 8754.7 ACFT HRS,AUTHORIZATION GRANTED TO BLEND ANDREPAIR CP CYCLIC STICK YOKE HOUSING IAWDMWR 1-1680-323 DTD 30DEC11 PG 3-13, PARA3-12. REMOVING MINIMAL MATERIAL NOT TOEXCEED DEPTH. MEC NUMBER WILL BESTENCILED ON HOUSING.

20-Jan-2017 1


dean.a.keirn

USAACEMEC F321444, 8754.7 ACFT HRS,AUTHORIZATION GRANTED TO BLEND ANDREPAIR PI CYCLIC STICK YOKE HOUSING IAWDMWR 1-1680-323 DTD 30DEC11 PG 3-13, PARA3-12. REMOVING MINIMAL MATERIAL NOT TOEXCEED DEPTH. MEC NUMBER WILL BESTENCILED ON HOUSING.

20-Jan-2017 2


dean.a.keirn

USAACEMEC F194446 NO LONGER APPLIES TO THISAIRCRAFT DUE TO TAIL LANIDING GEARYOKE ASSY REPLACEMENT. NEW YOKENUMBER IS U5271 WITH NO APPLICABLEMEC'S TOWARD IT.

23-Jan-2017 1


tammy.k.murphy

USAACEMEC F321513, 8754.7 ACFT HRS,AUTHORIZATION GRANTED TO DEVIATE FROMTHE PERMISSIBLE 2" DIAMETER REPAIRLIMITS IAW EM0013 WP 0387 TO REPAIR A 5.5X 3.25" VOID IN THE RH CATWALK.

24-Jan-2017 1


dean.a.keirn

USAACEMEC F321622, 8754.7 ACFT HRS,AUTHORIZATION GRANTED TO DEVIATE FROMTHE PERMISSIBLE 2" DIAMETER REPAIRLIMITS IAW EM0013 WP 0387 TO REPAIR A 3 X2" VOID IN THE LH CATWALK.

25-Jan-2017 1


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 70 of 73

USAACEH-60-16-ASAM-06- IMPROVED TAIL ROTORQUADRANT SUPPORT, COMPLETED AT 8754.7ACFT HRS.

08-Feb-2017 1


christina.l.negron

USAACET/R BIAS CHECK COMPLETED AT 8754.7 ACFTHRS. COLOR SET BIAS QAVERIFICATION COLLECTIVE FULL UP,PEDAL FULL LEFTRED 3.0AFS166 19.7BLACK3.0 AFS16619.8YELLOW 3.0 AFS16619.8BLUE 3.0 ASF16620.0

14-Feb-2017 1


christina.l.negron

USAACEMAIN ROTOR RIGGING COMPLETED AT 8754.7ACFT HRS. BLADES ON.PRIMARY SERVOCONTROL ROD BIAS: FWD AND LAT : NOADJUSTMENTS, LAT: LENGTHENED 3FLATS.LOW COLLECTIVE ANGLEBLADE90 DEG R 180DEG FWD 270 DEG L 0DEG AFT TOTAL DEG AVG DEGRED #19.0 -0.1 -10.0 0.1-1.9 -0.475BLACK #2 9.0 -0.1 -10.0 0.1 -1.9 -0.475YELLOW#3 9.0 -0.1 -10.0 0.1 -1.9 -0.475BLUE#4 9.0 -0.1 -10.0 0.6 -1.9 -0.475HIGH COLLECTIVE ANGLENEUTRAL CYCLIC90 DEG R 180DEG FWD270 DEG L 0 DEG AFT TOTAL DEG AVGDEG 19.5 11.7 10.618.2 60.0 15.0FWD CYCLICANGLE NEUTRAL LAT90 DEG R 180DEGFWD 270 DEG L 0 DEG AFT TOTAL DEGAVG DEG -2.1 31.233.3AFT CYCLE ANGLE NEUTRAL LAT90DEG R 180DEG FWD 270 DEG L 0 DEGAFT TOTAL DEG AVG DEG 25.94.4 21.5LEFT CYCLEANGLE LEFT LAT90 DEG R 180DEG FWD270 DEG L 0 DEG AFT TOTAL DEG AVGDEG -8.46.8 15.2RIGHT CYCLIC ANGLERIGHT LAT90 DEG R 180DEG FWD 270DEG L 0 DEG AFT TOTAL DEG AVGDEG 7.0-7.6 14.6

14-Feb-2017 2


christina.l.negron

USAACETAIL ROTOR TENSION CHECK COMPLETED @8754.7 HRS; L/H 166 LB, R/H 167 LB W/MR#126115 @ 23.8 DEGREES CELCIUS MR# 107156

16-Feb-2017 1


tammy.k.murphy

USAACEVERIFICATION OF INSTALLED CADS,COMPLETED IAW H-60-17-ASAM-01 AT 8754.7.

17-Feb-2017 1


christina.l.negron

USAACE720 HOUR PHASE INSPECTION #13COMPLETED @ 8754.7 HOURS.NEXT PHASE,#14 DUE @ 9474.7 HOURS

17-Feb-2017 2


tammy.k.murphy


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 71 of 73

USAACECOMPLIED WITH H -60-17-ASAM-05,INSTALLED M/R BLADE S/N'S NOTAPPLICABLE TO THIS ASAM

23-Feb-2017 1


tammy.k.murphy

USAACEMAIN TRANSMISSION, SN: A265-00946, FILTERBUTTON POPPED AT 8756.9 ACFT HRS.REPLACED FIRST AND SECOND STAGEFILTERS, RESET BUTTON. LEAK CHECK ANDSERVICEABILITY CHECK COMPLETED,

24-Feb-2017 1


christina.l.negron

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

08-Mar-2017 1


dean.a.keirn

USAACET/R CABLE TENSION CHECK FAILED AT 8764.3ACFT HRS. SET TENSION TO L/H: 105, R/H:105 @ 4 DEGREES C.

16-Mar-2017 1


KG4191

USAACET/R CABLE TENSION CHECK NOT STABILIZEDAT 8774.2 ACFT HRS. ADJUSTED TENSION TOL/H: 142, R/H: 142 @ 25.3 DEGREES C.

21-Mar-2017 1


KG4191

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

22-Mar-2017 1


dean.a.keirn

USAACET/R CABLE TENSION CHECK COMPLETED ASFOLLOWS: L/H 155 R/H 155 @ 27 DEGREES C.

26-Mar-2017 1


jimmy.s.caylor

USAACEH-60-17-AMAM-07 EXTERNAL MOUNTEDRESCUE HOIST (EMRH) ARM ADAPTORCORROSION CONTROL C/W AT 8783.8 ACFTHRS.

28-Mar-2017 1


jimmy.s.caylor

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

03-Apr-2017 1


dean.a.keirn

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

04-Apr-2017 1


thomas.e.mitchell

USAACET/R CABLE TENSION FAILED AT 8794.3 ACFTHRS. READINGS WERE L/H: 133, R/H: 133 @13.3 DEGREES C.

08-Apr-2017 1


KG4191

USAACET/R CABLE TENSION CHECK C/W AT 8804.3ACFT HRS WITH READINGS OF L/H: 152, R/H:150 @ 20.3 DEGREES C.

15-Apr-2017 1


KG4191

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

24-Apr-2017 1


dean.a.keirn

USAACEACFT OPERATING IAW AWR 1452, R6 DTD19APR17, LC-6 DIGITAL CLOCK,SUPERSEDING ALL PRIOR VERSIONS OF THISAWR AND REPLACES ISAQ 113 AND ALLREVISIONS.

28-Apr-2017 1


dean.a.keirn


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 72 of 73

USAACEH-60-17-ASAM-10(IMMSS HINGE PINS) C/W AT8893.3 ACFT HRS.

21-Jun-2017 1


KG4191

USAACEH-60-17-ASAM-12(IMMSS RETROFIT KIT) C/WAT 8950.4 ACFT HRS.

31-Jul-2017 1


KG4191

USAACEH-60-17-AMAM-12(AIRWORTHINESS RELEASE(AWR) UPDATE) C/W AT 8990.9 ACFT HRS.

21-Aug-2017 1


KG4191

URS RASM-COCM/ACE PERFORMED AT 8992.4 AIRCRAFTHOURS BY TEAM MEMBER P

30-Aug-2017 1


jacob.a.weikart

USAACEH-60-17-AMAM-13(CYCLIC BOOT HARDWARE)C/W AT 9030.9 ACFT HRS.

28-Sep-2017 1


KG4191

USAACEH-60-17-AMAM-11(ESM-2 PROGRAMIMPLEMENTATION) C/W AT 9038.2 ACFT HRS.

07-Oct-2017 1


KG4191

USAACEACFT NO LONGER OPERATING IAW AWR 1220,ALL VERSIONS, ESM, DUE TO COMPLIANCEWITH H-60-17-AMAM-11, ESM-2.

11-Oct-2017 1


dean.a.keirn

USAACEH-60-18-ASAM-02(RESCUE HOIST PENDANT)C/W AT 9048.5 ACFT HRS.

16-Nov-2017 1


KG4191

USAACEACFT BEING OPERATED IAW MEO A6055 DUETO M/R DROOP STOP BUSHING DE-BOND.REPLACEMENT OF M/R DROOP STOPBUSHING REQUIRED AT THE NEXT PMI DUE AT9234.7 ACFT HRS.

18-Nov-2017 1


KG4191

USAACEH-60-18-ASAM-03(LEGACY FUEL HOSE) C/W AT9066.7 ACFT HRS.

13-Dec-2017 1


KG4191

USAACEH-60-18-AMAM-01, DUAL AN/ARC-231 GROUNDWIRE INSTALLATION COMPLETED AT 9073.3ACFT HRS.

18-Dec-2017 1


olivia.d.williams

USAACEACFT OPERATING IAW AWR 1913, R3 DTD26JAN2018, ACFT LAPTOP, SUPERSEDING ALLPRIOR VERSIONS OF THIS AWR.

26-Jan-2018 1


dean.a.keirn

USAACEACFT TRANSFERRED TO BEST PROGRAMFOR ARMY/BEST PROGRAM AT 9117.3 ACFTHRS. DATA PLATE REMAINED INSTALLED.

23-Feb-2018 1


kenneth.e.griffin

SCIENCE ANDENGINEERINGSERVICES, LLC

ACFT TRANSFERED TO BEST PROGRAM ON23 FEB 2018 @ 9119.5 ACFT HOURS FROMUSAACE FORT RUCKER, AL. DATA PLATEINSTALLED

23-Feb-2018 2

HUNTSVILLE

michael.t.wood


NUMBER PIDENTRY


DATE6.

REMARKS4. 5.


Page 73 of 73

SCIENCE ANDENGINEERINGSERVICES, LLC

H-60-17-ASAM-11, FUEL HOSE BORESCOPEINSPECTION, NOT C/W

06-Mar-2018 1

HUNTSVILLE

michael.t.wood


DATE AC HRS SHAFT VERTICAL REASON FOR VIBRATION CHECKLONGITUDINALLATERALIPS READINGS4.

8724660HELICOPTER, UTILITYEH-60A

3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL

Page 1 of 6

a b c d e f g

120 HR14-Apr-2007 #1 ENG 0.050.000.004,336.7

120HR14-Apr-2007 #2 0.170.000.004,336.7

120HR14-Apr-2007 OIL COOLER 0.000.350.004,336.7

120HR23-May-2007 #1 ENG 0.120.000.004,457.3

120HR23-May-2007 #2 ENG 0.180.000.004,457.3

120HR23-May-2007 OIL COOLER 0.000.080.004,457.3

720 HR PHASE14-Aug-2007 #1 ENG 0.110.000.004,518.0

720HR PHASE14-Aug-2007 #2 ENG 0.050.000.004,518.0

720HR PHASE14-Aug-2007 OIL COOLER 0.000.610.004,518.0

OUTPUT SHAFT BAL.08-Sep-2007 #2 ENG 0.240.000.004,551.0

120HR24-May-2008 OIL COOLER 0.000.370.005,002.6

120HR24-May-2008 #2 ENG 0.340.000.005,002.6

120HR24-May-2008 #1 ENG 0.250.000.005,002.6

120HR INSP09-Jul-2008 OIL COOLER 0.000.400.005,125.8

120HR INSP09-Jul-2008 #2 ENG 0.380.000.005,125.8

120HR INSP09-Jul-2008 #1 ENG 0.220.000.005,125.8

720HR26-Oct-2008 #1 ENG 0.240.000.005,235.5

720HR PHASE26-Oct-2008 #2 ENG 0.260.000.005,235.5

720 HR PHASE26-Oct-2008 OIL COOLER 0.000.330.005,235.5

120HR11-Jan-2009 #1 ENG 0.140.000.005,358.3

120HR11-Jan-2009 #2 ENG 0.250.000.005,358.3

120HR11-Jan-2009 OIL COOLER 0.000.330.005,358.3

120HR02-Feb-2009 OIL COOLER 0.000.030.005,476.0

120HR25-Feb-2009 #1 ENG 0.060.000.005,476.0

120HR25-Feb-2009 #2 ENG 0.130.000.005,476.0

120HR25-Feb-2009 T/R 0.040.000.005,476.0


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




Page 2 of 6

a b c d e f g

360HR11-May-2009 #1 ENG 0.050.000.005,595.2

360HR11-May-2009 #2 ENG 0.370.000.005,595.2

360HR11-May-2009 OIL COOLER 0.000.050.005,595.2

D/S BAL TQ=38%16-Jun-2009 #1 ENG 0.290.000.005,672.4

120HR29-Jun-2009 #1 ENG 0.230.000.005,710.5

120HR29-Jun-2009 #2 ENG 0.430.000.005,710.5

120HR29-Jun-2009 OIL COOLER 0.000.020.005,710.5

120HR03-Sep-2009 #1 ENG 0.300.000.005,835.3

120HR03-Sep-2009 #2 ENG 0.450.000.005,835.3

120HR03-Sep-2009 OIL COOLER 0.000.020.005,835.3

720HR17-Nov-2009 #1 ENG 0.080.000.005,922.7

720HR17-Nov-2009 #2 ENG 0.140.000.005,922.7

720HR17-Nov-2009 OIL COOLER 0.000.020.005,922.7

120HR11-Feb-2010 #1 ENG 0.130.000.006,041.1

120HR11-Feb-2010 #2 ENG 0.230.000.006,041.1

120HR13-Apr-2010 #1 ENG 0.180.000.006,161.4

120HR13-Apr-2010 #2 ENG 0.270.000.006,161.4

120HR13-Apr-2010 OIL COOLER 0.000.060.006,161.4

120HR06-Jun-2010 #1 ENG 0.220.000.006,280.9

120HR06-Jun-2010 #2 ENG 0.240.000.006,280.9

120HR06-Jun-2010 OIL COOLER 0.000.020.006,280.9

120HR18-Jul-2010 #1 ENG 0.270.000.006,401.1

120HR18-Jul-2010 #2 ENG 0.270.000.006,401.1

120HR18-Jul-2010 OIL COOLER 0.000.120.006,401.1

120HR17-Oct-2010 OIL COOLER 0.000.200.006,523.5

120HR17-Oct-2010 #2 ENG 0.280.000.006,523.5






Page 3 of 6

a b c d e f g

120HR17-Oct-2010 #1 ENG 0.140.000.006,523.5

120HR NO TQ12-Feb-2011 OIL COOLER 0.000.810.006,616.1

120HR12-Feb-2011 #2 ENG 0.810.000.006,616.1

120HR12-Feb-2011 #1 ENG 0.380.000.006,616.1

BAL FOR BOOT REPL.28-Feb-2011 T/R 0.070.000.006,564.2

120HR MTP MOC31-Mar-2011 #1 ENG 0.280.000.006,736.9

120HR MOC31-Mar-2011 #2 ENG 0.180.000.006,736.9

120 HR MOC31-Mar-2011 OIL COOLER 0.000.450.006,736.9

120HR MOC31-Mar-2011 T/R 0.120.000.006,736.9

MTP BAL CK05-May-2011 T/R 0.000.030.006,790.8

120HR INSP15-May-2011 #1 ENG 0.180.000.006,856.7

120HR INSP15-May-2011 #2 ENG 0.200.000.006,856.7

120 HR INSP15-May-2011 OIL COOLER 0.000.130.006,856.7

120HR INSP24-Jul-2011 T/R 0.000.050.006,975.2

120HR INSP24-Jul-2011 #1 ENG 0.330.000.006,975.2

120HR INSP24-Jul-2011 #2 ENG 0.300.000.006,975.2

120HR INSP24-Jul-2011 OIL COOLER 0.000.120.006,975.2

D/S BAL31-Jul-2011 #2 ENG 0.370.000.006,983.1

D/S BAL11-Aug-2011 #1 ENG 0.130.000.006,991.2

VIBE CK01-Oct-2011 OIL COOLER 0.000.370.007,032.5

BAL CK01-Oct-2011 T/R 0.000.080.007,032.5

HSS BAL01-Oct-2011 1 ENG 0.250.000.007,032.5

HSS BAL01-Oct-2011 #2 ENG 0.300.000.007,032.5

120HR INSP12-Nov-2011 #1 ENG 0.450.000.007,099.7

120HR INSP12-Nov-2011 #2 ENG 0.250.000.007,099.7

120HR INSP12-Nov-2011 OIL COOLER 0.000.420.007,099.7






Page 4 of 6

a b c d e f g

120HR INSP12-Nov-2011 T/R 0.000.070.007,099.7

BAL CHECK, NO TORQUE PROVIDED27-Nov-2011 #1 ENG 0.370.000.007,131.0

MOC 120HR18-Feb-2012 #1 ENG 0.170.000.007,218.4

MOC 120HR INSP18-Feb-2012 #2 ENG 0.210.000.007,218.4

MOC 120HR18-Feb-2012 OIL COOLER 0.000.670.007,218.4

MOC 120HR18-Feb-2012 T/R 0.000.120.007,218.4

POST PHASE MTP MOC12-Jun-2012 OIL COOLER 0.000.580.007,326.8

POST PHASE MTP MOC12-Jun-2012 T/R 0.000.030.007,326.8

POST PHASE MTP MOC12-Jun-2012 #1 ENG 0.320.000.007,326.8

POST PHASE MTP MOC12-Jun-2012 #2 ENG 0.290.000.007,326.8

VIB CHECK14-Dec-2012 #1 ENG 0.400.000.007,686.7

VIB CHECK14-Dec-2012 #2 ENG 0.430.000.007,686.7

T/R BAL CHECK14-Dec-2012 T/R 0.000.060.007,686.7

VIB CHECK14-Dec-2012 OIL COOLER 0.000.270.007,686.7

120HR INSP02-Mar-2013 T/R 0.000.050.007,815.2

120HR INSP02-Mar-2013 OIL COOLER 0.000.220.007,815.2

120HR INSP02-Mar-2013 #1 ENG 0.450.000.007,815.2

120HR INSP02-Mar-2013 #2 ENG 0.480.000.007,815.2

120HR INSP11-May-2013 #1 ENG 0.370.000.007,932.9

120HR INSP11-May-2013 #2 ENG 0.490.000.007,932.9

120HR INSP11-May-2013 OIL COOLER 0.000.240.007,932.9

120HR INSP11-May-2013 T/R 0.000.130.007,932.9

HSS SHAFT BAL DUE28-Jun-2013 #2 ENG 0.180.000.008,013.7

T/R BALANCE CK15-Sep-2014 T/R 0.000.100.008,057.6

120 HR MTF VIB CHECK13-Dec-2014 #1 ENG 0.380.000.008,169.4

120 HR MTF VIB CHECK13-Dec-2014 #2 ENG 0.240.000.008,169.4






Page 5 of 6

a b c d e f g

120 HR MTF VIB CHECK13-Dec-2014 OIL COOLER 0.000.170.008,169.4

120 HR MTF VIB CHECK13-Dec-2014 T/R 0.000.070.008,169.4

120 HR VIB29-Mar-2015 #1 ENG 0.380.000.008,288.0

120 HR VIB29-Mar-2015 #2 ENG 0.240.000.008,288.0

120 HR VIB29-Mar-2015 OIL COOLER 0.000.230.008,288.0

120 HR VIB29-Mar-2015 T/R 0.000.110.008,288.0

EROSION STRIP REPAIR25-Apr-2015 T/R 0.000.070.008,340.5

120 HR VIB14-Jul-2015 #1 ENG 0.400.000.008,410.4

120 HR VIB14-Jul-2015 #2 ENG 0.260.000.008,410.4

120 HR VIB14-Jul-2015 T/R 0.000.050.008,410.4

120 HR VIB14-Jul-2015 OIL COOLER 0.000.220.008,410.4

T/R BALANCE CHECK22-Jul-2015 T/R 0.000.080.008,419.7

OUTPUT SHAFT BALANCE26-Aug-2015 #1 ENG 0.340.000.008,451.2

REMOVAL/REINSTALLATION18-Sep-2015 #2 ENG 0.200.000.008,457.2

RESHIMMING OF OUTBOARD RETENTION PLATE19-Sep-2015 T/R 0.000.130.008,457.2

APPLICATION OF EPOXY PRIMER25-Sep-2015 #1 ENG 0.360.000.008,462.7

APPLICATION OF EPOXY PRIMER25-Sep-2015 #2 ENG 0.150.000.008,462.7

120 HR VIB05-Dec-2015 #1 ENG 0.490.000.008,532.4

120 HR VIB05-Dec-2015 #2 ENG 0.120.000.008,532.4

120 HR VIB05-Dec-2015 OIL COOLER 0.000.160.008,532.4

120 HR VIB05-Dec-2015 T/R 0.000.140.008,532.4

T/R BLADE REPLACEMENT20-Jan-2016 T/R 0.000.100.008,544.4

120 HR VIBE01-May-2016 #2 ENG 0.130.000.008,656.4

120 HR VIBE01-May-2016 OIL COOLER 0.000.170.008,656.4

120 HR VIBE01-May-2016 T/R 0.000.030.008,656.4

120 HR VIBE02-May-2016 #1 ENG 0.370.000.008,656.4






Page 6 of 6

a b c d e f g

REPLACEMENT OF #1 ENG 06 AUG 1609-Aug-2016 #1 ENG 0.350.000.008,742.0

ABRASION STRIP REPLACEMENT12-Aug-2016 T/R 0.000.060.008,742.0

POST 720 HR PHASE27-Feb-2017 #1 ENG 0.270.000.008,757.9

POST 720 HOUR PHASE27-Feb-2017 #2 ENG 0.140.000.008,757.9

POST 720 HOUR PHASE27-Feb-2017 OIL COOLER 0.180.000.008,757.9

POST 720 HOUR PHASE27-Feb-2017 T/R D/S 0.000.130.008,757.9

120 HR VIB09-Jun-2017 #1 ENG 0.320.000.008,876.2

120 HR VIB09-Jun-2017 #2 ENG 0.300.000.008,876.2

120 HR VIB09-Jun-2017 OIL COOLER 0.000.090.008,876.2

120 HR VIB09-Jun-2017 T/R 0.000.150.008,876.2

REM. & REINSTALLATION OF #2 ENGINE16-Jul-2017 #2 ENG 0.190.000.008,938.5

120 HR VIB27-Aug-2017 #1 ENG 0.350.000.008,991.4

120 HR VIB27-Aug-2017 #2 ENG 0.390.000.008,991.4

120 HR VIB27-Aug-2017 OIL COOLER 0.000.100.008,991.4

120 HR VIB27-Aug-2017 T/R 0.000.050.008,991.4

REPLACEMENT OF BLUE T/R BOOT22-Oct-2017 T/R 0.000.060.009,041.9

120 HR VIB04-Feb-2018 #1 ENG 0.370.000.009,114.3

120 HR VIB04-Feb-2018 #2 ENG 0.410.000.009,114.3

120 HR VIB04-Feb-2018 OIL COOLER 0.000.040.009,114.3

120 HR VIB04-Feb-2018 T/R 0.000.080.009,114.3

5. REMARKS



(ACFT HRS)

ji kgfdcba

RMVL HRSRMVL HRSCOMPO/HNOMENWUC O/HLOCATIONNSN

AND he SINCELIFE

PREVSER NO.ANDNOMENCLATURE P/N TIMEINST HRS MENT DUEREPLACINST HRSNO.COMPONENT

NOMEN REPLACE -O/H ORCOMP6.

1520010820686HELICOPTER, UTILITY EH-60A 8724660 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Condition Change Components Page 1 of 7

COND COND

156001113021502C12D

00TAIL CONE FITTING A330-0034070219-05001-044 CCCC

COND COND

162001231183103A01

10698755FWD FIXED GEAR SHOCK BEM218570250-12051-045 CCCC

COND COND

162001231183103A01

08046FWD FIXED GEAR SHOCK BEM249770250-12051-045 CCCC

COND COND

162001421089003B01

26888046SHOCK ABSORBER (TAIL) C0020065670250-13101-044 CCCC

COND COND

165001285302405A01Z

49978046DAMPER ASSY, M/R A1060326970106-08100-046 CCCC

COND COND

165001285302405A01Z

22678046DAMPER ASSY, M/R A1060379070106-08100-046 CCCC

COND COND

165001285302405A01Z

43098046DAMPER ASSY, M/R R1060130470106-08100-046 CCCC

COND COND

165001285302405A01Z

7438046DAMPER ASSY, M/R R1060150770106-08100-046 CCCC

COND COND

531501537465205A02H

5097632BLADE PIN, SOLID B941-0469470103-08108-041 CCCC

COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H

26978647BLADE PIN, SOLID B9411544770103-08108-041 CCCC

COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

531501537465205A02H


COND COND

161501199764605A03A

75468046SWASHPLATE ASSY U370104-08000-050 CCCC

COND COND

161501503311506A

25367033MAIN TRANSMISSION MODUL A265-0094670351-08100-076 CCCC

COND COND

161501078571806A11

00ACCESSORY MODULE A258-0292070351-08080-043 CCCC

COND COND

161501078571806A11

00ACCESSORY MODULE A258-0292170351-08080-043 CCCC

COND COND

161501230621806E

14281640INPUT MODULE A264-0018770351-08001-046 CCCC

APD LC v2.00EDITION MAY 1967 IS OBSOLETE For use of this form, see DA PAM 738-751; the proponet agency is DCSLOG

AIRCRAFT COMPONENT HISTORICAL RECORDDA FORM 2408-16, OCT 1991

(ACFT HRS)

ji kgfdcba


AND he SINCELIFE





COND COND

161501230621806E

00INPUT MODULE A264-0286370351-08001-046 CCCC

COND COND

168001074515206F

8298046INTERMEDIATE GEARBOX A005-0192670357-06300-042 CCCC

COND COND

161501376508906G01

29818046TAIL ROTOR GEARBOX ASSY A006-0245370358-06600-046 CCCC

COND COND

161501524780506H04

07327DRIVESHAFT ASSY ENGINE C845-0847970361-08014-041 CCCC

COND COND

161501524780506H04

08451DRIVESHAFT ASSY ENGINE C8450975370361-08014-041 CCCC

COND COND

161501081277506H06

00SHAFT ASSY, T/R DRV SEC 1 A2710115370361-03001-045 CCCC

COND COND

161501158951706H08

21208755SHAFT ASSY, T/R DRV SEC 2 C270-0014570361-03009-047 CCCC

COND COND

161501158952206H09

19411941SHAFT ASSY, T/R SEC 3,4,5 A272-0374470361-05001-051 CCCC

COND COND

161501158952206H09

19411941SHAFT ASSY, T/R SEC 3,4,5 A2720363970361-05001-051 CCCC

COND COND

161501158952206H09

19411941SHAFT ASSY, T/R SEC 3,4,5 A2720373870361-05001-051 CCCC

COND COND

161501083295306H11

55028046SHAFT ASSY, T/R DRV SEC 6 A273-0074170361-05002-045 CCCC

COND COND

161501158578806H12

17788046SHAFT ASSY, T/R DRV SEC 7 WG300450004370361-06002-047 CCCC

COND COND

432001207722807A01

14268845PUMP MODULE ASSY, HYDR K3399ABR53023-06 CCCC

COND COND

432001207722807A01

16397631PUMP MODULE ASSY, HYDR K4169ABR53023-06 CCCC

COND COND

432001207722807A01

23548536PUMP MODULE ASSY, HYDR 7600326ABR70652-02300-050 CCCC

COND COND

481001102247307B05A

08656VALVE, SOLENIOD 198153213850-3-1 CCCC

COND COND

481001102247307B05A

09082VALVE, SOLENIOD 254093213850-3-1 CCCC

COND COND

165001222431607B11

28427033ACCUMULATOR 3851A3197170-5 CCCC

COND COND

168001342049608B20

02407PANEL INDICATOR (PDU) 1874100-601561-000 CCCC

COND COND

168001342049608B20

31286481PANEL INDICATOR (PDU) 3056100-601561-000 CCCC

COND COND

611501114969609A01

9006868GENERATOR 1131A130270550-02031-111 CCCC



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE





COND COND

611501114969609A01

20147039GENERATOR 40409770550-02031-111 CCCC

COND COND

161501260074911C21

08046MIXER ASSEMBLY 8L5130058870400-02300-046 CCCC

COND COND

156001411515111D17

08046SERVO BEAM FITTING J3380129370209-22103-065 CCCC

COND COND

156001411515611D17


COND COND

156001411515011D17


COND COND

156001411514811D17


COND COND

168001261204411D25

3527327STABILATOR ACTUATOR C2920825370400-06641-117 CCCC

COND COND

168001261204411D25

3527327STABILATOR ACTUATOR C2920828370400-06641-117 CCCC

COND COND

599601316274311D26

11267327STABILATOR AMPLIFIER 1037A70902-02001-048 CCCC

COND COND

599601316274311D26

05236STABILATOR AMPLIFIER A9300384070902-02001-048 CCCC

COND COND

299501496368615A04

5567887ENGINE SEQUENCING UNIT 30214504587 CCCC

COND COND

584101245909019E05A

13298917RECEIVER-TRANSMITTER, R 60GGSM-C-967292 CCCC

COND COND

584101245909319E05C

08046INDICATOR,HEIGHT 1551FFA3060591 CCCC

COND COND

660501503528419E06A

08046ATTITUDE HEADING REFERE 1395765100-20 CCCC

COND COND

661001490516852A

08131AUTOMAT FLT CONT COMPU 3452235825050-1-001 CCCC



COMPO/H OR REPLACE -

NOMENCOMPONENT NO. INST HRS

REPLAC MENT DUEINST HRS TIMEP/NNOMENCLATURE

AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND

NSN LOCATION O/HWUC NOMEN O/H COMPRMVL HRS RMVL HRS

a b c d f g ki j

Page 4 of 7Condition Change Components

7. SIGNIFICANT HISTORICAL DATA

APD LC v2.00REVERSE OF DA FORM 2408-16, OCT 1991

(ACFT HRS)

ji kgfdcba


AND he SINCELIFE




Time Change Components Page 5 of 7

20000 20000

156001081924402C15J

87558755TAIL PYLON FITTING A496-0108170209-06051-043 RCRC

5100 13146

161501450483405A01A

08046HUB, M/R ROTOR ASSY D3080008870103-08112-047 RCRC

6400 9141

161501442692605A01I

60148755MAIN ROTOR SPINDLE ASSY A001-0422370102-08200-069 RCRC

6400 11617

161501442692605A01I

35388755MAIN ROTOR SPINDLE ASSY D001-1150270102-08200-069 RCRC

6400 11617

161501442692605A01I


6400 11617

161501442692605A01I


14000 22046

161501074515105A01L

08046MAIN ROTOR SHAFT EXTEND 151520183270351-08186-043 RCRC

13000 21046

161501127738805A01T

08046BIFILAR, M/R ROTOR ASSY R46270107-08400-046 RCRC

9600 13504

161501106190305A02

48518755MAIN ROTOR BLADE ASSY A007-0610970150-09100-043 RCRC

9600 17017

161501106190305A02


9600 15332

161501106190305A02


9600 16888

161501106190305A02

14678755MAIN ROTOR BLADE ASSY A0071468070150-09100-043 RCRC

10000 15406

161501113818805B02

26408046TAIL ROTOR BLADE ASSY A009-0361770101-31000-043 RCRC

10000 18544

161501113818805B02

08544TAIL ROTOR BLADE ASSY A0090821870101-31000-043 RCRC

12000 10461

161501083681206G01B

30091470O/B RETENTION PLATE (T/R) A257-0123970102-11101-042 RCRC

2520 11275

414001329342806H23

29468755FAN AXIAL D5120154970361-03005-107 02

13000 19441

156001129125607A24

16058046SAS ACTUATOR C1120490870410-02500-049 RCRC

13000 20427

156001129125607A24


13000 19326

156001129125607A24


2160 10206

161501141753211C23

21468046T/R PITCH CHANGE SHAFT 2330291270400-06100-042 01

11000 11628

165001305695411C25

74188046SERVO ASSY, TAIL ROTOR B3000304070410-06520-046 RCRC



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE




Time Change Components Page 6 of 7

24400 30593

165001143122611D01

18538046SERVO, PRIMARY MAIN ROT B30310770274000-1031 RCRC

24400 27214

165001143122611D01

52328046SERVO, PRIMARY MAIN ROT B30300169B70410-02820-054 RCRC

24400 29598

165001143122611D01

28488046SERVO, PRIMARY MAIN ROT B30306946B70410-02820-054 RCRC

13000 16670

156001158968511D04

49868656AFT BELLCRANK 345-0261470400-08102-045 RCRC

17000 17000

156001164416111D05

00AFT TIE ROD SUPT FITTING A3910112870400-08112-045 RCRC

2200 10955

168001164416011D06

08755AFT TIE ROD ASSY M392-1055470400-08111-042 RCRC

4400 12446

156001286887011D07

08046AFT BELLCRANK SPT ASSY 3900194670400-08117-049 RCRC

11000 18195

304001287243811D08

2367431LATERAL SWASHPLATE LINK 151520338870400-08151-061 RCRC

11000 19046

168001221286311D09

08046LATERAL SERVO BELLCRAN F3370496670400-08166-041 RCRC

11000 14616

168001158965311D11

44308046AFT WALKING BEAM C3460035170400-08104-048 RCRC

4600 12646

156001289269711D13

08046LEFT TIE ROD ASSY F3440153570400-08115-046 RCRC

3500 10475

156001296948611D14

06975RIGHT TIE ROD ASSY 2880132570400-08114-051 RCRC

15000 23046

168001158965211D15

08046FORWARD BELLCRANK 200070400-08101-046 RCRC

5600 13626

156001221261911D16

08026FWD BELLCRANK SPT ASSY B3670687470400-08162-042 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 7 of 7Time Change Components



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1620012311831FWD FIXED GEAR SHOCK 70250-12051-045 BEM2185 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

9000 16686

165001125090703A01A

00PISTON, MAIN L/GEAR STR BEM218570250-12067-102 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


21-Jun-2016 1 REMOVED FWD FIXED GEAR SHOCK S/N BEM2185, FROM ACFT 8724595 @ ACFT HRS 8269.3 DUE TOLEAKING, TSN, 1069.

lashana.r.sasser USAACE FT. RUCKER, AL

31-Jan-2017 1 INSTALLED FWD FIXED GEAR SHOCK STRUT S/N BEM2185 W/TSN 1069 HRS ON ACFT 8724660 @ 8755ACFT HRS

tammy.k.murphy USAACE FT RUCKER, AL


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1620012311831FWD FIXED GEAR SHOCK 70250-12051-045 BEM2497 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

9000 17046

165001125090703A01A

00PISTON, MAIN L/GEAR STR BEM300770250-12067-102 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615014426926MAIN ROTOR SPINDLE ASSY 70102-08200-069 A001-04223 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

COND COND

161501161437305A01I02

06014ELASTOMERIC BEARING B32441869SB7001-048 CCCC

COND COND

311001158960705A01I02C

06014THRUST BEARING C32505830SB7002-048 CCCC

13000 15741

531001126944405A01I04

00M/R SPINDLE NUT C479-1025270102-08105-102 RCRC

6400 9141

530601460602005A01I06

00TIE ROD (M/R SPINDLE) C504-0095338023-10372-101 RCRC

10000 12741

161501214914005A01I07

00CONTROL HORN ASSY A241-1448170102-08111-047 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


01-Jan-1900 1 RETAINING NUT TORQUE: 130 FT. LBS SIKORSKY AIRCRAFT.

thomas.m.lilly SIKORSKY AIRCRAFT (NO LOCATION)

17-Jul-2004 1 17 JULY 04-INSTALLED M/R SPINDLE ASSY SN: A001-04223 W/TSN: 0 ON ACFT 8424028 @ 3397 ACFTHRS. C. ANDERSON, 3091, USAAVNC, FT. RUCKER, AL.

mae.p.belford USAAVNC FT. RUCKER, AL

10-Sep-2004 1 10 SEP 04 - TBO CHANGED FROM 2500 TO 3100 HRS. I/A/W UH-60-MIM-04-014 DTD 9SEP04. CA3091R/SPEC; USAAVNC, FT. RUCKER, AL.

mae.p.belford USAAVNC FT. RUCKER, AL

14-Mar-2011 1 RETAINING NUT TORQUE: 130 FT. LBS SIKORSKY AIRCRAFT.

mae.p.belford SIKORSKY AIRCRAFT (NO LOCATION)

17-Sep-2012 1 INSTALLED ELASTOMERIC BEARING SN: B324-22866 ON M/R SPINDLE SN: A001-04223 17SEP12 @ 7738.8ACFT HRS

jessica.l.wendel USAACE FT. RUCKER, AL

17-Sep-2012 2 INSTALLED THRUST BEARING SN: B325-34717, WITH TSN: 2183, ON SPINDLE SN: A001-04223, ATSPINDLE TSN: 4342, IAW H-60-12-AMAM-16.

christina.l.negron USAACE FT RUCKER,AL

16-Mar-2016 1 REMOVED M/R SPINDLE ASSY S/N: A001-04223 W/TSN: 5686 FROM ACFT 8424028 @ 9083 ACFT HRS(TM014571 R/SPEC) USAACE FT RUCKER, AL


25-Mar-2016 1 720 HOUR INSPECTION COMPLETED WITH TTSN: 5686. (MEC F305943) RETURN TO SERVICE.

cynthia.w.moore USAACE (AMSS) FT. RUCKER, AL.

04-Apr-2016 1 INSTALLED SPINDLE ASSY SN: A001-04223, ON ACFT 8424028, AT 9083 ACFT HRS, WITH TSN: 5686.

christina.l.negron USAACE FT. RUCKER, AL

10-Nov-2016 1 REMOVED M/R SPINDLE ASSY SN: A001-04223 W/TTSN: 6014 FROM ACFT 8424028 @ 9411.1 ACFT HRSDUE TO SEPARATION IN BEARING.

mary.b.hodge USAACE FT. RUCKER, AL

16-Dec-2016 1 PERFORMED 720 HOUR INSPECTION (MEC F305943B) REPLACED THRUST BEARING S/N:B325-34717WITH S/N: C32505830 AND REPLACED ELASTOMERIC BEARING S/N:B324-22866 WITH S/N: B32441869WITH TTSN: 6014. RETURNED TO SERVICE. WORK ORDER NO. 609085

cynthia.w.moore USAACE (AMSS) FT. RUCKER, AL.

30-Jan-2017 1 INSTALLED M/R SPINDLE ASSY S/N A001-04223 W/TSN 6014 HRS ON ACFT 8724660 @ 8755 ACFT HRS



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615014426926MAIN ROTOR SPINDLE ASSY 70102-08200-069 D001-11502 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

COND COND

161501161437305A01I02

671671ELASTOMERIC BEARING B324-27924SB7001-048 CCCC

COND COND

311001158960705A01I02C

28232823THRUST BEARING B32541291SB7002-048 CCCC

13000 18217

531001126944405A01I04

28232823M/R SPINDLE NUT F479-0389870102-08105-102 RCRC

6400 11617

530601460602005A01I06


10000 15217

161501214914005A01I07

28232823CONTROL HORN ASSY H241-0010470102-08111-047 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


22-Sep-2010 1 RETAINING ROD NUT TORQUE: 140 FT. LBS. E.HERDAN

debra.r.chancellor SIKORSKY AIRCRAFT STRATFORD, CT.

07-Oct-2016 0 REMOVED SPINDLE FROM ACFT AT 2127 ACFT HRS DUE 720 HOUR INSP W/TSN 3538

theresa.d.pollard USAACE FT RUCKER AL

19-Oct-2016 1 COMPLETED 720 HR. INSPECTION I/A/W MEC: F305945B & F317778 AND RETURNED TO SERVICE ATTTSN: 3538 HRS.

gerald.d.arrington USAACE(AMSS) FT. RUCKER, AL

30-Jan-2017 1 INSTALLED M/R SPINDLE ASSY S/N D001-11502 W/TSN 3538 HRS ON ACFT 8724660 @ 8755 ACFT HRS



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE




Page 1 of 2

COND COND

161501161437305A01I02


COND COND

311001158960705A01I02C

671671THRUST BEARING B325-40965SB7002-048 CCCC

13000 18217

531001126944405A01I04


6400 11617

530601460602005A01I06


10000 15217

161501214914005A01I07

28232823CONTROL HORN ASSY H241-0009670102-08111-047 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


21-Sep-2010 1 RETAINING ROD NUT TORQUE: 115 FT. LBS. E. HERDAN



theresa.d.pollard USAACE FT. RUCKER,AL


gerald.d.arrington USAACE(AMSS) FT. RUCKER, AL.




(ACFT HRS)

ji kgfdcba


AND he SINCELIFE




Page 1 of 2

COND COND

161501161437305A01I02


COND COND

311001158960705A01I02C

671671THRUST BEARING B325-41195SB7002-048 CCCC

13000 18217

531001126944405A01I04


6400 11617

530601460602005A01I06


10000 15217

161501214914005A01I07

28232823CONTROL HORN ASSY G241-0140570102-08111-047 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


21-Sep-2010 1 RETAINING ROD NUT TORQUE: 150 FT. LBS. (E. HERDAN)



theresa.d.pollard USAACE FT. RUCKER,AL


GA235751 USAACE(AMSS) FT. RUCKER, AL.




(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011061903MAIN ROTOR BLADE ASSY 70150-09100-043 A007-06109 05A024. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

COND COND

156001447977405A02E

7214837M/R BLADE TIP CAP B849-1182070150-09207-041 CCCC

5000 11720

161501099234105A02I

20214837M/R BLADE CUFF E237-0069570150-09109-041 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


23-Jun-2016 1 RECAPPED IAW DMWR 1-1615-281, TSN: 4837, FINAL TRIM TAB SETTINGS: STA.1.338, STA.2.340,STA.3.342, STA.4.341, STA.5.340, STA.6.342, SPAR #B302-05207.

AM5219 CCAD CORPUS CHRISTI, TX

07-Aug-2016 1 INSTALLED ON ACFT 8724660 AT ACFT HRS 8741 WITH TSN: 4837.

kenneth.e.griffin USAACE FT. RUCKER, AL

18-Jan-2017 1 REMOVED M/R BLADE ASSY S/N A007-06109 W/TSN 4851 HRS FROM ACFT 8724660 @ 8755 ACFT HRSFOR 720 HR PHASE INSPECTION


01-Feb-2017 1 720 HOUR INSPECTION COMPLETED, IAW TM1-1520-237-23&P, WP 055300.

christina.l.negron USAACE FT. RUCKER, AL.

17-Feb-2017 1 INSTALLED BLADE SN: A007-06109, ON ACFT 8724660, AT 8755 ACFT HRS, WITH TSN: 4851.



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE




Page 1 of 2

COND COND

156001447977405A02E


5000 13546

161501099234105A02I

01129M/R BLADE CUFF G237-0446570150-09109-041 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


12-Sep-2014 1 OVERHAULED IAW CONT# W58RGZ-12-D-0212 DO#0004 SO# B713232-01 TT:1129. OUTGOING BIMINDICATOR SN: 100160, LEAK CHECKED 9/10/14, PAINTED AND STENCILED DATA, STATIC AND DYNAMICBALANCE, COMPLETE FLUOROSCOPE, COMPLIED WITH: NEW CUFF INSTALLED SN: G237-04465,REPLACED TIP BLOCK & SCREWS, ELECTRICAL CHECK PER ATP 21.186, SHIM WEIGHTS-INSPECTIONFOR INTERFERENCE, DISASSEMBLED/REPROCESSED SPAR SN: C302-12169/REBUILT BLADE, TIP CAPP/N 70150-09207-041, SN: B849-14994, TT: NEW, FINAL TRIM TAB SETTINGS: STA 1-317, STA 2-318, STA 3-317, STA 4-318, STA 5-318, STA 6-318, PRE-TRACK +21.

QC000000 SISKORSKY AIRCRAFT BPT.,CT

12-Sep-2014 2 OVERHAULED IAW CONT# W58RGZ-12-D-0212 DO#0004 SO# B713232-01 TT:1129. OUTGOING BIMINDICATOR SN: 100160, LEAK CHECKED 9/10/14, PAINTED AND STENCILED DATA, STATIC AND DYNAMICBALANCE, COMPLETE FLUOROSCOPE, COMPLIED WITH: NEW CUFF INSTALLED SN: G237-04465,REPLACED TIP BLOCK & SCREWS, ELECTRICAL CHECK PER ATP 21.186, SHIM WEIGHTS-INSPECTIONFOR INTERFERENCE, DISASSEMBLED/REPROCESSED SPAR SN: C302-12169/REBUILT BLADE, TIP CAPP/N 70150-09207-041, SN: B849-14994, TT: NEW, FINAL TRIM TAB SETTINGS: STA 1-317, STA 2-318, STA 3-317, STA 4-318, STA 5-318, STA 6-318, PRE-TRACK +21.

QC000000 SISKORSKY AIRCRAFT BPT.,CT

22-Nov-2014 1 M/R BLADE S/N A007-13232 INSTL. ON ACFT. 8524404 AT 14598 ACFT. HRS. WITH 1129 TSN. AFSINSPECTOR 151

brian.k.dow USAACE FT. RUCKER, AL.

04-Dec-2015 1 M/R BLADE REMOVED FROM ACFT 8524404 AT 14603 WITH TTSN 1134 DUE TO TURNED IN TO SUPPLY.

OW01095 USAACE FT RUCKER,AL

16-Dec-2015 1 720 HR INSP REPAIRS & PAINT C/W. SPAR PRESSSURE CHECK @ 1025PSI @ 70*F IAW WP05500 & 16770.BALANCE BLADE @ 35,398 IN LN IAW H-60AL UNCOATED SOFTWARE BALANCE BLADE FIXTURECALIBRATION CK C/W "PASSED". DW1476 @334-503-3765

chelsey.p.phillips USAACE FORT RUCKER, AL

26-Jan-2016 1 INSTALLED M/R BLADE SN A007-13232 WITH TSN OF 1134 ON ACFT 8724660 AT 8551 ACFT HOURS.

chelsey.p.phillips USAACE FORT RUCKER, AL

18-Jan-2017 1 REMOVED M/R BLADE ASSY S/N A007-13232 W/TSN 1338 FROM ACFT 8724660 @ 8755 ACFT HRS FOR 720HR PHASE INSPECTION


31-Jan-2017 1 720 HOUR INSPECTION COMPLETED, IAW TM1-1520-237-23&P, WP 055300.


17-Feb-2017 1 INSTALLED BLADE SN: A007-13232, ON ACFT 8724660, AT 8755 ACFT HRS, WITH TSN: 1338.



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE




Page 1 of 2

COND COND

156001447977405A02E


5000 10732

161501099234105A02I

00M/R BLADE CUFF G237-0064270150-09109-041 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


18-Jul-2009 1 18 JUL 09 - SPAR PRESSURE CHECK; 11.00 @ 29.9°C. MECH. EV6360 (JT0967 R/SPEC) USAACE, FT.RUCKER, AL

thomas.m.lilly USAACE (JT0967) FT. RUCKER, AL

23-Apr-2010 1 23APR10 - 720 HR PHASE INSP; REPAIRS & PAINT C/W; SPAR PRESSURE CK @ 10.50 PSI @ 75* F;BALANCE CK @ 35.413 IN. LB. WORK COMPLETED BY D. WHITE 1476 T (334) 503 - 2702.

thomas.m.lilly USAACE (D.WHITE) (NO LOCATION)

22-Nov-2010 1 (NO DATE) BLADE TRIM TAB SETTINGSLOCATION: 1 - .287 2 - .286 3 - .287 4 - .287 5 - .288 6 - .286SPAR PRESSURE CHECK DATE: 00000SIKORSKY AIRCRAFT

thomas.m.lilly SIKORSKY AIRCRAFT (NO PID) (NO LOCATION)

13-Sep-2011 1 REMOVED FROM ACFT SN:8624570 @ TSN:1070 @ 5674 ACFT HRS DUE TO 720 HR INSPECTION.

stacie.d.darlymple USAACE FT. RUCKER, AL

05-Oct-2011 1 INSTALLED M/R BLADE SN: A007-14749 W/TSN: 1070 ON ACFT 8524467 @7049.6 ACFT HRS. SPARPRESSURECK @ 10.00 PSI @ 67 DEGREES F. BALANCE CK @ 35.424 IN. LB. 720 HR INSP REPAIRS &PAINT C/W.

mary.b.hodge USAACE FT. RUCKER, AL

21-Nov-2012 1 REMOVED M/R BLADE S/N: A007-14749 W/TTSN: 1779 FROM ACFT 8524467 AT 7759 ACFT HRS DUE TO 720HR PMI.

rhonda.e.jackson USAACE FT. RUCKER, AL

21-Nov-2012 2 REPAIRED @ 720 HR INSP REPAIR AND POIN CW. SPAR PRESSURE IS @ 10.25 PSI @ 70 DEG F. BALANCEIS @ 35,398 IN LB IAW H-60-A/L UNCOATED SOFTWARE

DW1476 USAACE FT RUCKER, AL

13-Dec-2012 1 INSTALLED M/R BLADE ASSY A007-14749 WITH TSN-1779 ON 8524469 @ 6914 ACFT HRS. PRE-TRACK +10

vickie.l.meadows USAACE FT RUCKER, AL

09-Jul-2016 1 REMOVED MAIN ROTOR BLADE ASSY S/N A007-14749 FROM ACFT 8524469 DUE TO CONTROLEXCHANGE TO ACFT 8624565, TSN: 2922 @ ACFT HRS 8056.7


10-Jul-2016 1 INSTALLED MAIN ROTOR BLADE ASSY S/N A007-14749 WITH TSN 2922 ACFT HRS 7983.6


18-Jan-2017 1 REMOVED M/R BLADE ASSY S/N A007-14749 W/TSN 3025 HRS FROM ACFT 8624565 @ 8087 ACFT HRSFOR 720 HR PHASE INSPECTION


24-Feb-2017 1 INSTALLED M/R BLADE ASSY S/N A007-14749 W/TSN 3025 HRS ON ACFT 8724660 @ 8757 ACFT HRS



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011061903MAIN ROTOR BLADE ASSY 70150-09100-043 A00714680 05A024. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

COND COND

156001447977405A02E

22971376M/R BLADE TIP CAP A8490757170150-09207-041 CCCC

5000 11677

161501099234105A02I

1270659M/R BLADE CUFF A2371560770150-09109-041 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


10-May-2016 1 REMOVED M/R BLADE SN: A00714680, FROM ACFT 8724666, AT 7383 ACFT HRS, WITH TTSN: 1376.REMOVAL IS DUE TO FAILING H-60-15-ASAM-07, AND 720 HOUR PHASE INSP DUE.


17-May-2016 1 REMOVED MAIN ROTOR TIP CAP S/N A84908346 DUE TO FRAYED, TSN: 717, HOURS OF MAIN ROTORBLADE 1376


18-May-2016 1 INSTALLED MAIN ROTOR TIP CAP S/N:A84907571, TSN: 2297, 1376 MAIN ROTOR BLADE HOURS


24-May-2016 1 24 MAY 2016 - D. WHITE 1476. 503-3765, UIC W0U911. 43 MAN HOURS. 720 HR INSP. REPAIRS TOBLADE. PAINT C/W. SPAR PRESSURE CK @ 10.00 PSI @ 65 DEGREES F. IAW WP 055000 AND 167900.M/R # 85746. BALANCE CK @ 35,398 IN LB IAW H-60-A/L UNCOATED SOFTWARE. M/R # 1005168.BALANCE FIXTURE CALIBRATION CK C/W "PASSED". H-60-15-ASAM-07 INSPECTION C/W "PASSED".

thomas.e.mitchell USAACE LOWE FLD, FT. RUCKER, AL.

26-May-2016 1 INSTALLED M/R BLADE SN: A00714680 WITH TSN OF 1376 ON ACFT SN: 8724660 @ 8663.9 ACFT HOURS.

thomas.e.mitchell USAACE LOWE FLD, FT. RUCKER, AL.

18-Jan-2017 1 REMOVED M/R BLADE S/N A00714680 W/TSN 1467 HRS FROM ACFT 8724660 @ 8755 ACFT HRS FOR 720HOUR PHASE INSPECTION


31-Jan-2017 1 720 HOUR INSPECTION COMPLETED, IAW TM1-1520-237-23&P, WP055300.


17-Feb-2017 1 INSTALLED BLADE SN: A00714680, ON ACFT 8724660, AT 8755 ACFT HRS, WITH TSN: 1467.



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011997646SWASHPLATE ASSY 70104-08000-050 U3 05A03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

COND COND

161501087160205A03A01

75467546STATIONARY SWASHPLATE U1170104-08010-044 CCCC

11000 11500

161501357508905A03A02

00ROTATING SWASHPLATE U2970104-08001-045 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE

PREVSER NO.ANDNOMENCLATURE P/N TIMEINST HRS

MENT DUEREPLACINST HRSNO.COMPONENT

NOMENREPLACE -

O/H ORCOMP6.

1615015033115MAIN TRANSMISSIONMODULE

70351-08100-076 A265-00946 06A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

17000 24033

161501078571106A08

02536SWASHPLATE GUIDE F4250034670351-08227-041 RCRC

3000 10033

161501110149106A13

02536HOUSING ASSY MGB F2110022070351-08110-045 RCRC

7600 14633

304001415838806A18

02536MAIN ROTOR SHAFT E2530472870351-08131-048 RCRC

12000 18458

161501497725706A19

5752536PLANETARY CARRIER ASSY A2400175570351-08175-046 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


25-Mar-2015 1 MAIN MOD IMPENDING BYPASS BUTTON POPPED. REPLACED OIL FILTERS AND INSPECTED M/MODCHIP DETECTOR & SCREEN. NO CHIPS PRESENT WITH TSN: 3788 ON ACFT 8724660 AT 8285 ACFT HRS.


29-Feb-2016 1 M/MOD S/N: A265-00946 WITH TSN: 4094 FILTER IMPENDING BYPASS BUTTON POPPED.SERVICEABILITY INSPECTION COMPLETED ON ACFT 8724660 AT 8591.4 ACFT HRS.


24-Feb-2017 1 MAIN TRANSMISSION, SN: A265-00946, FILTER BUTTON POPPED, AT TSN: 4260, ON ACFT 8724660, AT8757 ACFT HRS. REPLACED FIRST AND SECOND STAGE FILTERS, RESET BUTTON.


20-Sep-2017 1 MAIN MOD FILTER BUTTON POPPED WITH TSN: 4522. SERVICEABILITY INSPECTION COMPLETED ONACFT 8724660 AT 9019.1 ACFT HRS.

KG4191 USAACE FT. RUCKER, AL


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615013765089TAIL ROTOR GEARBOX ASSY 70358-06600-046 A006-02453 06G014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

12000 20046

161501074515306G01C

02981I/B RETENTION PLATE T/R K2591024270358-06612-042 RCRC

5000 13046

304001292161706G01D

02981GEARSHAFT, BEVEL G3200104770358-06620-102 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


15-Jan-2010 1 OVERHAULED/RECAPPED IAW DWMR1-1615-279. TSN:2981, TSO: 0,

RO7306 CCAD CORPUS CHRISTI TX.

13-Aug-2013 1 RECAPPED/OVERHAULED IAW DMWR 1-1615-279. TSN: 2981, TSO:0.

JC1688 CCAD CORPUS CHRISTI TX.


(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



4140013293428FAN AXIAL 70361-03005-107 D51201549 06H234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

2520 11275

311001127300506H23A

02946BEARING, AXIAL FAN 10662210SFFC3 RCRC

2520 11275

311001127300506H23A

02946BEARING, AXIAL FAN 10673210SFFC3 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2


09-Feb-2017 1 INSTALLED AXIAL FAN S/N C270-00145 W/TSN 2120 HRS ON ACFT 8724660 @ 8755 ACFT HRS



(ACFT HRS)

ji kgfdcba


AND he SINCELIFE



1615011417532T/R PITCH CHANGE SHAFT 70400-06100-042 23302912 11C234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Page 1 of 2

2160 10206

311001113828811C23A

02146BRNG T/R PITCH CHG SHFT C84012201SB1162-102 RCRC






AND SER NO. PREV

(AFCT HRS)LIFE

SINCEe hAND


a b c d f g ki j

Page 2 of 2



ACFT 87-24660

The following Components were unable to have the S/N’s verified during the BEST Induction and S/N

check process. Either Data Plates were not installed, not legible, painted over or access was not able to

be gained to the Data Plate because of the way the component was stowed for transport. All of these

components have been S/N matched against MCDS and if the records do not match between ULLS-A

and MCDS, then the 2410 Hotline will provide follow on guidance.

COMPONENT ULLS-A P/N ULLS-A S/N

SHAFT ASSY, T/R DRV SEC 2 70361-03009-047 C270-00145

SHAFT ASSY, T/R DRV SEC 3,4,5 70361-05001-051 A272-03639

ACCUMULATOR 3197170-5 3851A

STABILATOR ACTUATOR 70400-06641-117 C292-08253

STABILATOR ACTUATOR 70400-06641-117 C292-08283

T/R PITCH CHANGE SHAFT 70400-06100-042 233-02912

AFT TIE ROD SUPT FITTING 70400-08112-045 A391-01128

AFT WALKING BEAM 70400-08104-048 C346-00351

PISTON, MAIN L/GEAR STR 70250-12067-102 BEM3007

of 12

ECD01013

87246606035T00G01T700-GE-700 ENGINE ASSYGE-E-207849

4679

3250

43935

5686

10271

9153

2456

1955

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-207849

hr)

50726745139592811

500715919115742719GE-C-0068186035T02G01COLD SECTIONMODULE

COND

COND

3250

1129GGM8WRE46064T55G01COMBUSTION LINER

COND

COND

3250568691531955

33911681073091818MRS097446055T20G05MTCHDROTOR/STATOR ASSY

COND

COND

3250

3226AMDA76295043T24G14STAGE 1 NOZZLE

COND

COND

3250568691531955

3826969160742259GEL0073396064T98G01POWER TURBINEMODULE

COND

COND

3250

5979GED0374476035T01G01ACCESSORY MODULE

COND

COND

3250

0SUPK65066034T62P18PARTICLESEPARATOR BLOWER

COND

COND

3418

107154640974046T52G39FUEL CONTROL

COND

COND

3250

90731TU4076T64G01POU ASSY-O/S DRAINVALVE

COND

COND

3250

289EMDE02464046T29G13ELECTRICALCONTROL UNIT

COND

COND

3250568691531955

467943935102712456ECD010134046T26G03HISTORY RECORDER

COND

COND

REVERSE OF DA FORM 2408-16-1, OCT 1991

OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 3 of 12


hr)

3250

3418UDC046584046T25G01COOLER, OIL

COND

COND

3250

757COMH54454046T28G14ANTI-ICE VALVE

COND

COND


9/26/201112:00:00 AM

1 REPAIRED ENGINE 25 FEB 2011 I/A/W DMWR 1-2840-248 AND CHANGESAND RECAPPED DATED 03 DEC 01.

J.DALLY CCAD CCAD

1/24/201712:00:00 AM

1 REMOVED COLD SECTION S/N GE-C-007849 FROM ENGINE GE-E-207849 W/HISTORY RECORDER READINGS OF: LCF1: 3312, LCF2: 15077, TTI: 15077,OPH: 6501 AND ENG CC; LCF1: 2811, LCF2: 13959, TTI: 6745, OPH: 5072


1/26/201712:00:00 AM

1 REPLACED COLD SECTION WITH S/N GE-C-006818 . HR READINGS LCF1:3312, LCF2: 15077, TTI: 44994, OPH: 6501; ENGINE CC: LCF1: 2811, LCF2:13959, TTI: 6745, OPH: 5072; COLD SECTION CC: LCF1: 2719, LCF2: 11574, TTI:15919, OPH: 5007. ON ENGINE S/N GE-E-207849



of 12

ECD01013

GE-E-2078496035T02G01COLD SECTION MODULEGE-C-006818

6501

5007

44994

15919

15077

11574

3312

2719

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-006818

hr)

500515832115692717

425333354353071621SAP052805056T66G02POWER TAKEOFFDRIVE

COND

COND

500515832115692717

500515832115692717GLB207816035T77G14COMPRESSORROTOR ASSY

COND

COND

500515832115692717

592018621153343048FIAID3726035T88P04GAS GEN TURBINESHAFT

11579

11000

500515832115692717

0000WEST48285036T95P01INNER BALANCEPISTON SE

COND

COND

500515832115692717

0000MMTF02396035T79P04COMPRESSORDISCHARGE SE

COND

COND

500515832115692717

36648491168331FIAAPE596035T83P01COMPRESSOR REARSHAFT

11133

5000

500515832115692717

0000VAEFP3675044T07P01NO 3 LABYRINTH

COND

COND

500515832115692717

372513465102252014FMC032165035T57P02VORTEX SPOILER

COND

COND

500515832115692717

1231104371920962GATHAD8N5043T04P02TIE ROD,COMPRESSOR

15268

10000

500515832115692717

158062472549787GATH89NR5066T79P01RING, SPACERCOMPRESSOR

14919

10000

500515832115692717

0000GLHTP50R6055T59P01COMPRESSORIMPELLER

11499

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


hr)

500515832115692717

5754869884445GGAY81113065T21G01OUTPUT SHAFT ASSY

COND

COND

500515832115692717

0000GLHTNAA26032T26G09STAGE 1 BLISK

11499

5000

500515832115692717

0000GLHTP9G06032T27P08STAGE 2 BLISK

13499

7000

500515832115692717

0000GLHTP7GK6038T08P04STAGE 3 & 4 BLISK

13499

7000

500515832115692717

0000GLHTP21A6038T09P04STAGE 5 BLISK

13499

7000

500515832115692717

3602297866341703BARB28216043T45P01NO 3 BALL BEARING

COND

COND

500515832115692717

95681491477735FCAM15886064T15P03NO 4 ROLLER

COND

COND


1/26/201712:00:00 AM

1 INSTALLED COLD SECTION S/N GE-C-006818 ON ENGINE GE-E-207849 W/HR READINGS LCF1: 3312, LCF2: 15077, TTI: 44994, OPH: 6501. ENGINE CC:LCF1: 2811, LCF2: 13959, TTI: 5072. COLD SECTION LCF1: 2719, LCF2: 11574,TTI: 15919, OPH: 5007.



of 12

ECD01013

GE-C-0068183065T21G01OUTPUT SHAFT ASSYGGAY8111

6501

577

44994

4956

15077

889

3312

447

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 GGAY8111

hr)

5754869884445

66714271672392TMKAD0MT6064T34P01NO 1 BALL BEARING

COND

COND

5754869884445

16379941374FCAH66425121T46P02NO 2 ROLLER

COND

COND



of 12

ECD01013

GE-E-2078496055T20G05MTCHD ROTOR/STATORMRS09744

4679

3391

43935

16810

10271

7309

2456

1818

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 MRS09744

hr)

33911681073091818

70859432045414GATHGA8N6064T85P01STAGE 1 TURBINE

8971

5000

33911681073091818

35171476672023012GGAAM0346039T57G18STATOR GASGENERATOR

COND

COND

33911681073091818

2215255172635846GATCTGRA6064T86P01STAGE 2 TURBINE

7464

5000

33911681073091818

1707414539711112MA005326039T53P04STG 1 FWD COOLINGPLATE

6972

4000

33911681073091818

82714232059477BFFS01256039T50P04STG 1 AFT COOLINGPLATE

7852

4000

33911681073091818

22721841949141225GFFN82206064T83P01STG 2 FWD COOLINGPLATE

7407

5000

33911681073091818

53319061359362GFF5A4176064T84P02STG 2 AFT COOLINGPLATE

9146

5000

33911681073091818

33911681073091818GGA097446039T54G13ROTOR GASGENERATOR

COND

COND


2/26/201112:00:00 AM

1 REPAIRED MATCHED GG ROTOR/STATOR 25 FEB 11 I/A/W DMWR 1-2840-248AND CHANGES AND RECAPPED DTD 03 DEC 01.

J.DALLY CCAD CCAD


of 12

ECD01013

GE-E-2078496064T98G01POWER TURBINE MODULEGEL007339

4679

3826

43935

9691

10271

6074

2456

2259

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 GEL007339

hr)

3826969160742259

3826969160742259GGA070385043T75G07POWER TURBINEROTOR

COND

COND

3826969160742259

0000GATHRRGM6038T32P02STAGE 3 TURBINE

9679

5000

3826969160742259

436229486172GATHLMTD6038T34P06STAGE 4 TURBINE

9243

5000

3826969160742259

1387139172331597GATHK3LE5125T92G01POWER TURBINESHAFT

8292

5000

3826969160742259

94220631402491FCAH71245034T27P02NO 5 ROLLER

COND

COND

3826969160742259

236520566866993FCAE42016064T36P02NO 6 BALL BEARING

COND

COND


9/16/200812:00:00 AM

1 POWER TURBINE REPAIRED 16 SEP 08 I/A/W DMWR 1-2840-248 ANDCHANGES AND RECAPPED AED P3430B DTD 03 DEC 01.

QC000000 CCAD CCAD

2/26/201112:00:00 AM

1 REPAIRED POWER TURBINE 25 FEB 11 I/A/W DMWR 1-2840-248 ANDCHANGES AND RECAPPED DTD 03 DEC 01.

J.DALLY CCAD CCAD


of 14

ECD03451

87246606035T00G01T700-GE-700 ENGINE ASSYGE-E-307511

3075

5288

24269

52601

4961

12336

1706

3885

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 14


hr)

393136006105543045

36521390895722340GE-C-0078326035T02G01COLD SECTIONMODULE

COND

COND

3931

1695GG-M-FK8266064T55G01COMBUSTION LINER

COND

COND

528852601123363885

2499937059771544MRS096196055T20G05MTCHDROTOR/STATOR ASSY

COND

COND

3931

4916AMDA-10865043T24G14STAGE 1 NOZZLE

COND

COND

52885260123363885

375113321122082747GEL0067466064T98G01POWER TURBINEMODULE

COND

COND

3931

5289GE-D-0067926035T01G01ACCESSORY MODULE

COND

COND

4187

0K30736034T62P18PARTICLESEPARATOR BLOWER

COND

COND

5275

3678UDAJ40085074T79G07FUEL CONTROL

COND

COND

3931

149144-TU4076T64G01POU ASSY-O/S DRAINVALVE

COND

COND

5276

3697ECD002334046T29G11ELECTRICALCONTROL UNIT

COND

COND

393136006105543045

171876763179866ECD034514046T26G03HISTORY 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 14


hr)

3931

418UDC-028894046T25G06COOLER, OIL

COND

COND

3931

0COMH-103134046T28G14ANTI-ICE VALVE

COND

COND


3/3/200912:00:00 AM

1 24NOV08 CCAD ENGINE REPAIRED IAW DMWR 1-2840-248&CHANGES ANDRECAPPED AED P3430B DTD 03DEC01./S/S. DAVIS, ACFT DATA TECH

QC D CO 1-214TH CAAF

7/2/201312:00:00 AM

1 ENGINE REMOVED FROM UH-60A 8724589 @ 6054.1 ACFT HRS. CUM.COUNTS: LCF1 3665, LCF2 11740, TTI 51332, HRS 4934, H/R READINGS: LCF11486, LCF2 4365, TTI 23002, HRS 2721.

QC TASM-O WIESBADEN, GER

5/20/201512:00:00 AM

1 REMOVED HMU S/N: UDAJ6378 WITH TSN: 4118 FROM ENGINE GEE307511ENG CUM CTS: LCF1 4390, LCF2 13166, TTI 67731, HRS 6163. H/R S/N:ECD03451 READINGS: LCF1 1593, LCF2 4611, TTI 24158, HRS 2949 FOR TIMECHANGE. INSTALLED HMU S/N: UDA96522 WITH TSN: 3602, O/H'S: 1,

QC USAACE FT. RUCKER, AL

8/5/201512:00:00 AM

1 ENGINE S/N: GEE307511 WAS INSTALLED ON ACFT 8223756 ON 09SEP2014 @4919 ACFT HRS. ENG CTS AT INST: 3736/11879/52408/5096 AS CORRECTEDAND UPDATED BY MIKE MCSWAIN, SR, AMCOM. HISTORY RECORDERREADINGS AT INSTALL ON ACFT 8223756: 1557/4504/24076/2883. PERAMCOM CALL ENGINE HAD TO BE REMOVED AND RE-INSTALLED ONACFT 8223756 IN LOCAL ULLS-A(E) FOR CORRECTED READINGS AND HRS.SAME DATE HMU UDA6378 THAT WAS REPLACED ON 20MAY2015 WASREMOVED AND REINSTALLED TO REFLECT THE CORRECT HRS.


1/27/201612:00:00 AM

1 REMOVED ECU S/N: EMDE0570 FROM ENGINE S/N: GEE307511 W/TSN: 921HRS (INTERMITTEN TQ SPLIT). H/R S/N: ECD03451 READINGS:1699/4938/24256/3062. ENGINE S/N : GEE307511 CUMM. CTS.:3878/12313/52588/5275. INSTALLED ECU S/N: EMDE0825 W/TSN: 1512 HRS.


1/28/201612:00:00 AM

1 REMOVED FUEL CTRL S/N: UDA96522 W/TSN: 3715 HRS FROM ENG S/N:GEE307511 W/TSN: 5275 HRS. (TORQUE SPLIT GREATER THAN 5% FPG).ACFT 8223756 @ 5088.2 ACFT HRS. H/R S/N: ECD03451 READINGS:1699/4938/24256/3062. ENG CUMM. CTS: 3878/12313/52588/5275. INSTALLEDFUEL CTRL S/N: UDAJ4008 W/TSN: 3678 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 4 of 14


hr)


2/1/201612:00:00 AM

1 REMOVED ECU S/N: EMDE0825, FROM ENG SN: GE-E-307511, H/R S/N:ECD03451, AT H.R. READINGS: LCF1: 1700, LCF2: 4939, TTI: 24246, HRS: 3063.ENG CUM. COUNTS: LCF1 3879, LCF2 12314, TTI 52588, HRS 5276. REMOVEDIN SERVICEABLE CONDITION. INSTALLED ECU S/N: ECD00233 WITH TSN:


2/6/201612:00:00 AM

1 REMOVED ENG ASSY S/N: GEE307511 W/TSN: 5285 HRS (TQ STICTION). H/RS/N: ECD03541 READINGS: 1705/4960/24269/3072. ENG. CUM. CTS:3884/12335/52601/5285. ACFT 8223756 @ 5848.7 ACFT HRS.


4/14/201612:00:00 AM

1 REMOVED POWER TURBINE AT 5288 ENG HRS DUE TO BINDING. LCF1 3068,LCF2 10376, TTI 36752, HRS 6194, H/R ECD03451, LCF1 1706, LCF2 4961, TTI24269, HRS 3075, ENG CUM CTS: LCF1 3855, LCF2 12336, TTI 52601, HRS 5288.

theresa.d.pollard USAACE FT. RUCKER, AL

4/15/201612:00:00 AM

1 INSTALLED POWER TURBINE AT 5288 ENG HRS LCF1 2747, LCF2 12208, TTI13321, HRS 3751, H/R (ECD03451) LCF1 1706, LCF2 4961, TTI 24269, HRS 3075,ENG CUM CTS: LCF1 3855, LCF2 12336, TTI 52601, HRS 5288.

BD012379 USAACE FT. RUCKER, AL

4/16/201612:00:00 AM

1 REMOVED GG ROTOR S/N MRS 09264 AT 5288 ENG HRS DUE TO WORN.LCF1 2542, LCF2 8746, TTI 25475, HRS 4300, H/R (ECD03451) LCF1 1706, LCF24961, TTI 24269, HRS 3075, ENG CUM. CTS: LCF1 3855, LCF2 12336, TTI 52601,

brian.k.dow USAACE FT. RUCKER, AL

4/17/201612:00:00 AM

1 INSTALLED GG ROTOR S/N MRS09619 AT 5288 ENG HRS LCF1 1544, LCF25977, TTI 9370, HRS 2499, H/R (ECD03451) LCF1 1706, LCF2 4961, TTI 24269,HRS 3075, ENG CUM CTS: LCF1 3855, LCF2 12336, TTI 52601, HRS 5288.

brian.k.dow USAACE FT. RUCKER, AL

4/19/201612:00:00 AM

1 ON THIS DATE H/R S/N ECD03451 READINGS WERE VERIFIED BY ENGINESHOP MARK JERREL (TI) AS BEING: LCF1 1706, LCF2 4961, TTI 24269, HRS3075, ENG CUM CTS: LCF1 3885, LCF2 12336, TTI 52601, HRS 5288.

TP01634 USAACE FT. RUCKER, AL

8/6/201612:00:00 AM

1 ENGINE INSTALLED ON ACFT 8724660 AT 8741 ACFT HRS WITH LCF1 3885LCF2 12336 TTI 52601 OP HRS 5288, H/R S/N ECD03451 READINGS = LCF11706 LCF2 4961 TTI 24269 OP HRS 3075.

olivia.d.williams USAACE FT RUCKER,AL


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 5 of 14


hr)


of 14

ECD03451

GE-E-3075116035T02G01COLD SECTION MODULEGE-C-007832

1718

3652

7676

13908

3179

9572

866

2340

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 7 of 14


hr)

36521390895722340

663110047172022878SAP006475044T27G02POWER TAKEOFFDRIVE

COND

COND

36521390895722340

35954548277332124GLB008756035T77G10COMPRESSORROTOR ASSY

COND

COND

36521390895722340

29941642749951911GATN50636035T88P03GAS GEN TURBINESHAFT

9724

11000

36521390895722340

5405801369283BJWF21295036T95P01INNER BALANCEPISTON SE

COND

COND

36521390695722340

0000BIW039N66035T79P04COMPRESSORDISCHARGE SE

COND

COND

36521390895722340

2830596262741486GATDU5286035T83P01COMPRESSOR REARSHAFT

3888

5000

36521390895722340

2536785249821652GATALG055044T07P01NO 3 LABYRINTH

COND

COND

36521390895722340

3444953237721307BIWCH2975035T57P02VORTEX SPOILER

COND

COND

36521390895722340

109141941353373GATHAD8M5043T04P02TIE ROD,COMPRESSOR

10627

10000

36521390895722340

122739803905697GATCYFHP5066T79P01RING, SPACERCOMPRESSOR

10491

10000

36521390895722340

0000GLHTLAJF6055T59P01COMPRESSORIMPELLER

6718

5000


OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 8 of 14


hr)

36521390895722340

2185798452941563GG-A-077996039T56G04OUTPUT SHAFT ASSY

COND

COND

36521390895722340

0000GLHTL07J6032T26G09STAGE 1 BLISK

6718

5000

36521390895722340

0000GLHTJ6F26032T27P08STAGE 2 BLISK

8718

7000

36521390895722340

0000GLHTLDJD6038T08P04STAGE 3 & 4 BLISK

8718

7000

36521390895722340

0000GLHTL5GW6038T09P04STAGE 5 BLISK

8718

7000

36521390895722340

335227650100282500MDAM30206038T48P02NO 3 BALL BEARING

COND

COND

36521390895722340

11109931108663387671536064T15P03NO 4 ROLLER

COND

COND


3/3/200912:00:00 AM

1 24NOV08 CCAD C/S MOD REPAIRED 20NOVE 08 IAW DMWR 1-2840 &CHANGES AND RECAPPED AED P34308B DTD 03 DEC01. FUEL INJECTORSCLEANED AND FLOWED REP DMWR AT C/S TSN 3652 ON 20NOV08. /S/S S.DAVIS, AIRCRAFT DATA TECHNICIAN.

D CO1-214TH AVN CAAF


of 14

ECD03451

GE-C-0078326039T56G04OUTPUT SHAFT ASSYGG-A-07799

1718

2185

7676

7984

3179

5294

866

1563

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 10 of 14

04A01G 6039T56G04 OUTPUT SHAFT ASSY GG-A-07799

hr)

2185798452941563

28662258443941157MDAL63605043T18P01NO 1 BALL BEARING

COND

COND

2185798452941563

29602432093892601MABL48905035T69P01NO 2 ROLLER

COND

COND


3/3/200912:00:00 AM

1 24NOV08 CCAD OUTPUT SHAFT REPAIRED 20NOV08 IAW 9DMWR 1-2840-248 CHANGES AND RECAPPED AED P3430B DTDE 03DEC01. /S/ S.DAVIS,AIRCRAFT DATA TECHNICIAN

D CO 1-214TH AVN CAAF


of 14

ECD03451

GE-E-3075116055T20G05MTCHD ROTOR/STATORMRS09619

3075

2499

24271

9370

4961

5977

1706

1544

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 12 of 14

04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRS09619

hr)

2499937059771544

1776364527GATHH44N6064T85P02STAGE 1 TURBINE

7898

5000

2499937059771544

35601261689222377GGA077716039T57G18STATOR GASGENERATOR

COND

COND

2499937059771544

53331631240334GATTY8636043T63P01STAGE 2 TURBINE

5042

2500

2499937059771544

2530970784281304BCM243376064T81P01STG 1 FWD COOLINGPLATE

5545

5000

2499937059771544

70859432045414PAMEN8106064T82P01STG 1 AFT COOLINGPLATE

7367

5000

2499937059771544

2901282402135GFF5C67J6064T83P01STG 2 FWD COOLINGPLATE

7785

5000

2499937059771544

136891641102998R65476064T84P02STG 2 AFT COOLINGPLATE

6707

5000

2499937059771544

2499937059771544GGA096196039T54G13ROTOR GASGENERATOR

COND

COND


11/23/201012:00:00 AM

1 TB1-2840-248-20-2 dtd 30 jun 94 c/w at ccad and life limits c/w i/a/w tm1-2840-248-23, table 1-10 1jun99, "stage one and two gg blade sets contain new or used blades thathave always been run with dampers," ccad-c/w uh-60-95-asam-08 and -97-asam-03,s/f. ortiz records clerk.


4/15/201612:00:00 AM

1 INSTALLED GG ROTOR S/N MRS09619 AT 5288 ENG HRS . LCF1; 1544, LCF2;5977, TTI; 9370, OP HRS 2499, HR ( ECD03451) LCF1; 1706, LCF2; 4961, TTI;24269 , OP HRS 3075, ENG CUM CTS: LCF1; 3855, LCF2; 12336, TTI; 52601, OP



of 14

ECD03451

GE-E-3075116064T98G01POWER TURBINE MODULEGEL006746

3075

3751

7676

44067

4961

12208

1706

2747

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2

MODULE/RECORDER2-


MODULE/RECORDER3




COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=LINE 3 MINUS 2







T700-GE-700



OP HRS

d

T/T I

c

LCF-2

ba

LCF-1 (Hist rcdr

13.

REPLACE-MENT DUE

MENT LIFE

REPLACE-


11.

O/H OR

10.


8.


Page 14 of 14

04A03 6064T98G01 POWER TURBINE MODULE GEL006746

hr)

375013285122042745

375013285122042745GGA090645043T75G07POWER TURBINEROTOR

COND

COND

375013285122042745

97980393882732GATH7GL56038T32P01STAGE 3 TURBINE

7095

5000

375013285122042745

60017841246331GATHCAAJ6038T34P05STAGE 4 TURBINE

7474

5000

375013285122042745

27001133055431640GATE71605125T92G01REPOWER TURBINESHAFT

5374

5000

375013285122042745

2437701244011178MDAA05895034T06P01NO 5 ROLLER

COND

COND

375013285122042745

16551061439171028FCAE42156064T36P02NO 6 BALL BEARING

COND

COND


1/24/201112:00:00 AM

1 power turbine 20jan11 iaw dmwr 1-2840-248 & changes and recapped dtd 03dec01

SJDALLY CCAD CORPUS CHRSTI, TX

4/15/201612:00:00 AM

1 INSTALLED POWER TURBINE AT 5288 ENG HRS . LCF1; 2747, LCF2;12208,TTI;13321 OP HRS 3751, HR ( ECD03451) LCF1; 1706, LCF2;4961, TTI;7676 , OPHRS 3075, ENG CUM CTS: LCF1; 3855, LCF2; 12336, TTI;5260, OP HRS 5288

theresa.d.pollard 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=

0

0

0

2

0

1

SPE-122576

APU

116305-302 8724660

0 0116305-302 SPE-122576AUXILIARY POWER UNIT 0

15B 2835013692818

60026000

starts

RC RC4502902 SIF3594WHEEL, COMPRESSOR 0 0

15B02B 2835014596002

60026000

starts

RC RC4503991 R221WHEEL, TURBINE 0 0

15B03 2835013638089

60026000

starts


15-May-2012 1 INSTALLED APU S/N: SPE-122576 W/TTSN: 2, # OH'S:0, TTSO: 0 ON ACFT 8724660 @ 7326.8 ACFT HRS.

jessica.n.kennedy USAACE FT. RUCKER, AL.

For use of this form, see DA PAM 738-751; the proponent agency is DCS G-4

APD LC v1.00AUXILIARY POWER UNIT AND COMPONENT RECORDDA FORM 2408-16-2, MAR 2014

of 3

8724660HELICOPTER, 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 08 Mar 201814.0TM 1-1520-237-23&P14 DAY FLYABLE STORAGEENGINE RUN UP

22 Feb 2018D

A092 24 Feb 201830.0TM 11-6140-203-23 P30 DAY SLAB BATTERYINSPECTION (D8565/11-1)

25 Jan 2018D

A103 06 Mar 201830.0TM 1-1500-344-23AIRCRAFT WASH DUE 04 Feb 2018D

A110 9140.440.0TM 1-1520-237-PMSPMS 40 HOUR INSPECTION (ESMONLY)

9100.4H

A115 24 Mar 201830.0TM 1-1520-237-23&PLUBE REQUIRMENTS (ESMONLY)

22 Feb 2018D

A115 9157.340.0TM 1-1520-237-23&PLUBE REQUIRMENTS (ESMONLY)

9117.3H

A116 9234.7480.0H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

8754.7H

A116 23 Feb 201812.0H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

23 Feb 2017M

A117 9234.7480.0H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 8754.7H

A117 23 Feb 201812.0H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 23 Feb 2017M

A118 9234.7480.0H-60-10-AMAM-11MAIN GEARBOX OIL SAMPLE -ALL EXCEPT 073,074,076

8754.7H

A160 21 Mar 201890.0TM 1-1520-237-23&PESM 90 DAY CORROSIONINSPECTION

21 Dec 2017D

A210 9236.2120.0TM 1-1520-237-23&P120 HOUR INSPECTIONREQUIREMENTS (ESM ONLY)

9116.2H

A211 9234.7480.0H-60-10-AMAM-11APU OIL SAMPLE 8754.7H

A211 23 Feb 201812.0H-60-10-AMAM-11APU OIL SAMPLE 23 Feb 2017M

A213 9234.7120.0TB 1-1520-237-20-266ENGINE COMPRESSORCLEANING (ESM ONLY)

9114.7H

A295 9474.7360.0TM 1-1520-237-23&PSTABILATOR ACTUATOR ASSYLUBE (ESM ONLY)

9114.7H

A296 9474.7360.0TM 1-1520-237-23_PINSPECT STABILATOR ATTACHFITTINGS

9114.7H

A298 9594.3480.0TM 1-1520-237-23&PLUBRICATE TAIL WHEELBEARINGS

9114.3H

A298 12 Jan 201912.0TM 1-1520-237-23&PLUBRICATE TAIL WHEELBEARINGS

12 Jan 2018M

A299 9594.3480.0TM 1-1520-237-23&PLUBRICATE SWASHPLATE 9114.3H

A299 23 Jan 201912.0TM 1-1520-237-23&PLUBRICATE SWASHPLATE 23 Jan 2018M

A301 9234.7480.0TM 1-1520-237-23&PTORQUE INNER AND OUTERSWASHPLATE DUPLEX BEARINGRETAIN

8754.7H

A302 9594.3480.0TM 1-1520-237-23&PLUBRICATE MAIN LANDINGGEAR WHEEL BEARINGS

9114.3H

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


A302 12 Jan 201912.0TM 1-1520-237-23&PLUBRICATE MAIN LANDINGGEAR WHEEL BEARINGS

12 Jan 2018M

A303 9234.7480.0TM 1-1520-237-23&PINSPECT LEFT AND RIGHTRELAY PANELS

8754.7H

A304 9234.7480.0TM 1-1520-237-23&PLUBRICATE MIXERBELLCRANKS

8754.7H

A304 10 Feb 202148.0TM 1-1520-237-23&PLUBRICATE MIXERBELLCRANKS

10 Feb 2017M

A305 9234.7480.0TM 1-1520-237-23&PLUBRICATE ROTARY INPUTS 8754.7H

A306 9234.7480.0TM 1-1520-237-23&PLUBRICATE TAIL WHEELLOCKPIN

8754.7H

A400 9234.7960.0TM 1-1520-237-PMIPMI-1 8274.7H

A401 9714.7960.0TM 1-1520-237-PMIPMI-2 8754.7H

A408 9714.7960.0TM 1-1520-237-PMI960 HOUR LUBE REQUIRMENTS(PMI-2, AREA 5 AND 6)

8754.7H

A410 9234.7960.0TM 1-1520-237-PMI960 HOUR LUBE REQUIRMENTS(PMI-1, AREA 1 THRU 4)

8274.7H

A412 9714.7960.0TM 1-1520-237-23_PLUBRICATE WINDSHIELD WIPERCONVERTER

8754.7H

A413 9714.7960.0TM 1-1520-237-23&PLUBRICATE DOOR LOCKS 8754.7H

A440 9234.7480.0TM 1-1520-237-23&PCLEAN TAIL WHEEL LOCKPIN 8754.7H

A470 9545.51500.0TM 1-1520-237-23&PREPLACE NUMBER TWOCROSSFEED VALVE

8045.5H

A471 10205.52160.0TM 1-1520-237-23&PREPLACE T/R SHAFT SUPPORTBEARINGS (FWD)

8045.5H

A472 10205.52160.0TM 1-1520-237-23&PREPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)

8045.5H

A473 10205.52160.0TM 1-1520-237-23&PREPLACE T/R SHAFT SUPPORTBEARINGS (AFT)

8045.5H

A476 13045.55000.0TM 1-1520-237-23&PREPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS

8045.5H

A477 13045.55000.0TM 1-1520-237-23&PREPLACEMENT OF STABILATORACTUATOR BOLTS

8045.5H

A480 13045.55000.0TM 1-1520-237-23&PREPLACE PIVOT BOLT 70400-08159-101,102,103,104

8045.5H

A485 13045.55000.0TM 1-1520-237-23&PREPLACE BELLCRANK BOLT70400-08159-105,106,107,108

8045.5H

A495 23 Jan 201912.0TM 1-1520-237-23&PLUBRICATE WINDSHIELD WIPERCONVERTER (P/N 70209-01012-1

23 Jan 2018M

A496 13 Jun 2018180.0TM 1-1520-237-23&PCF3BR FIRE EXTINGUISHERWEIGHT TEST INSPECTION

15 Dec 2017D

A501 16 Feb 20186.0TM 1-1520-237-23&PMAIN ROTOR BLADE SPARPRESSURE CHECK

16 Aug 2017M




of 3




8.DUE


A502 10 Aug 2018180.0TM 1-1520-237-23&PINSPECT AND TEST GROUNDRECEPTACLE IAW TM 1-1500-204-23

11 Feb 2018D

A530 14 Jul 201812.0DA PAM 738-751AIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)

14 Jul 2017M

A532 23 Aug 201812.0TM 1-1500-204-23-4COMPASS SWING / RMI SWING 23 Aug 2017M

A533 14 Jul 201812.0TM 1-1520-237-23&PPITOT STATIC SYSTEMINSPECTION

14 Jul 2017M

A534 19 Jul 201812.0TM 1-1500-204-23-1FIRST AID KIT INSPECTION 19 Jul 2017M

A538 14 Jul 201812.0TM 1-1520-237-23&PFAT/OAT GAUGEINSPECTION/TEST

14 Jul 2017M

A553 01 Aug 201812.0AR 95-1ANNUAL WEIGHT AND BALANCEINVENTORY (365-1)

01 Aug 2017M

A580 20 Jun 201824.0TM 11-6140-203-23 PRETURN SLAB TO AVIM FORCAPACITY CHECK (EVERY 24MONTH)

20 Jun 2016M

A621 01 Aug 201824.0AR 95-1AIRCRAFT WEIGHING CLASS 1 01 Aug 2016M

A625 06 Jun 201960.0TM 11-6140-203-23 PREPLACEMENT OF SLABBATTERY (SLAB)

06 Jun 2014M

A630 01 Mar 2022114.0TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 Sep 2012M

A633 01 May 2021114.0TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #1,CARTRIDGE DODIC MH92

01 Nov 2011M

A638 01 May 2021114.0TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #2,CARTRIDGE DODIC MH92

01 Nov 2011M

A640 01 Mar 2022114.0TB 9-1300-385 CHG 22MAIN FIRE BOTTLE CARTRIDGE,31512AS105, 30903824-1

01 Sep 2012M

A648 14 Jul 2029180.0TM 1-1520-237-23_PREPLACE T/R SPRING CAPSULEASSY

14 Jul 2014M

A665 14 Jul 201848.0H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215

14 Jul 2014M

A670 14 Jul 201848.0TM 1-1520-237-23&PCABIN TUB INSPECTION 14 Jul 2014M

A675 14 Jul 201848.0TM 1-1520-237-23&PFLIGHT CONTROL RODSINSPECTION

14 Jul 2014M

A755 17045.59000.0H-60-10-ASAM-11PC LINK TO SWASHPLATEBOLTS REPLACEMENT

8045.5H




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-207849

3. ENGINE SERIAL NUMBER2. ENGINE MODEL1. NOMENCLATURE

Page 1 of 1

15-Sep-2014 8724660 CCAD BASELINE4000 104.0 101.0 1.0099.2204352.0 845.0

19-Sep-2015 8724660 ENGINE REINSTALLED7000 92.0 91.0 1.0097.6174762.0 841.0

24-Feb-2017 8724660 POST PHASE 7204500 103.0 101.0 1.0097.5195071.0 846.0


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-307511

3. ENGINE SERIAL NUMBER2. ENGINE MODEL1. NOMENCLATURE

Page 1 of 1

12-Aug-2016 8724660 NEW INSTALL2500 105.0 103.0 1.0098.8255291.0 846.0

12-Aug-2016 8724660 POST PHASE 7204500 101.0 101.0 1.0097.5155303.0 846.0

27-Feb-2017 8724660 POST 720 HOUR PHASE.4500 101.0 101.0 1.0097.5155303.0 846.0


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

18074 SESI

2. ORGANIZATION

CSGLD-1052

REQUIREMENT CONTROL SYMBOL(Julian)1. PERIOD ENDING DATE

Page 1 of 1

1GE-E-306926 CAO0128869321193312925274089858524478

2GE-E-306842 CAO0056636852161119418380689858524478

1GE-E-306167 ECD00086267443774601113187568624578

2GE-E-306898 ECD003103071190699330285587568624578

1GE-E-307511 ECD034513469243496996191491178724660

1GE-E-307511 ECD034513471243496998191591208724660

2GE-E-207849 ECD0101368744506316002347391178724660

2GE-E-207849 ECD0101368764507816002347391208724660

1GE-E306028 CAO005495039150588420254385318724668

2GE-E-306634 CAO0161663913814817421346085318724668

1GE-E-306074 ECDH0372120912196216866486428724672

2GE-E-207316 CAO010959819587122751416786428724672

1GE-E-306040C LMDH74926833904290739724770326988

2GE-E-761897 ECDH624165183889320273309824770326988

1GE-E-762049 ECDH8368210765424330112956468123606

2GE-E-762228 ECDH5446190983113247104356468123606


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

ULLSADMIN

Highlight

ULLSADMIN

Highlight

0

480.0

8754.7

8724660 1902.5 8046

e. ACFT HRS INSTALLEDc. TIME SINCE NEW OR OVERHAULc. SERIAL NUMBER

EH-60A A005-01926 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

kenneth.e.griffin15-Jul-2015NORMALROUTINE0.01193.48410.414-Jul-2015

kenneth.e.griffin01-Aug-2016NORMALROUTINE310.71504.18721.128-Jul-2016

KG419107-Mar-2017NORMALBASELINE0.01537.78754.723-Feb-2017

23 FEB 17 BASELINE POST PHASE OIL SAMPLE TM014571

9. REMARKS:

For use of this form, see DA PAM 738-751; the proponent agency is DCSLOGDA FORM 2408-20, DEC 91, MAY BE USED

OIL ANALYSIS LOGDA FORM 2408-20, OCT 1997

0

480.0

8721.1

8724660 4622.5 7033


EH-60A A265-00946 Days


HELICOPTER, UTILITY MAIN TRANSMISSION MODULE Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 1 of 1

a b

SUBMITTED

c a b



COMPONENTCHANGE

shelia.d.cook02-Oct-2011NORMALBASELINE7033.02536703302-Oct-2011

TP0163415-Jun-2012NORMALROUTINE295.02830732713-Jun-2012

theresa.d.pollard10-Sep-2012NORMALOTHER503.03038753505-Sep-2012

kathleen.m.jungell14-Mar-2013ABNORMALOTHER806.03342783913-Mar-2013

TP0163421-Mar-2013NORMALLAB REQUEST820.03355785219-Mar-2013



michael.t.wood07-Mar-2017NORMALROUTINE33.64257.78754.723-Feb-2017

23 FEB 17- ROUTINE POST PHASE TM01457114 MAR 13 - ABNORMAL RESULTS: EXCESSIVE SPALLING/FATIGUE WEAR, DO NOT CHANGE OIL. SUBMIT HOT RESAMPLE.(KG 4191,R/SPEC.)USAACE, FT.RUCKER, AL 36362.

9. REMARKS:



0

480.0

8754.7

8724660 4054.5 8046


EH-60A A006-02453 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

kenneth.e.griffin15-Jul-2015ABNORMALROUTINE0.03345.48410.414-Jul-2015

kenneth.e.griffin21-Jul-2015NORMALLAB REQUEST5.23350.68415.617-Jul-2015


KG419107-Mar-2017NORMALBASELINE0.03687.78754.723-Feb-2017

23 FEB 17-BASELINE POST PHASE OIL SAMPLE TM01457115JUL15 CODE J : DRAIN AND FLUSH SYSTEM RESAMPLE AFTER FIRST FLIGHT CYCLE DUE TO CU USAACE FT RUCKER OIL LAB SH027621

9. REMARKS:



0

480.0

8754.7

8724660 2835.0 0


EH-60A SPE-122576 Days


HELICOPTER, UTILITY AUXILIARY POWER UNIT Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.

Page 1 of 1

a b

SUBMITTED

c a b



COMPONENTCHANGE

TP0163415-Jun-2012NORMALBASELINE0.0732713-Jun-2012

TP0163415-Dec-2012NORMALROUTINE360.0360768714-Dec-2012



michael.t.wood07-Mar-2017NORMALBASELINE0.04658754.723-Feb-2017

23 FEB 17- BASELINE POST PHASE TM014571

9. REMARKS:



PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN -


ACCESSORY MODULE 8724660A258-029201. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

21-Mar-2013 FM

theresa.d.pollard23-Mar-2013

5.0USAACE, FT.RUCKER, AL.

COMPLY WITH THE REQUIREMENTSOF H-60-13-ASAM-04(PMB) PLASTICMEDIA BLAST AND OXIDE FLAKERESIDUE

H-60-13-ASAM-04MWO:

Priority Mnt Level


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

PIDMWODATE HRS



ACCESSORY MODULE 8724660A258-029211. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

21-Mar-2013 FM



COMPLY WITH THE REQUIREMENTSOF H-60-13-ASAM-04(PMB) PLASTICMEDIA BLAST AND OXIDE FLAKERESIDUE

H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



ACCUMULATOR 87246603851A1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

08-Dec-2003 DM

RR522829-Jun-2011

25.0CCAD/WOMUAAACCUMULATOR OVERHAUL1-1650-376MWO:

Priority Mnt Level

08-Dec-2003 DM

RR522829-Jun-2011

25.0CCAD/WOMUAAACCUMULATOR OVERHAUL1-1650-376MWO:

Priority Mnt Level



PIDMWODATE HRS



ANTI-ICE VALVE 8724660COMH54451. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

05-Sep-2012 OM

theresa.d.pollard05-Sep-2012

0.1USAACE FT.RUCKER, AL.

ALL UH-60A SERIES AIRCRAFTENGINE ANTI-ICE (AISBV)

H-60-12-ASAM-10MWO:

Priority Mnt Level



PIDMWODATE HRS



ANTI-ICE VALVE 8724660COMH-103131. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

22-Jun-2011 OM

08-Jul-20110.2D CO 1-214TH

AVN REGTANTI-ICE / START BLEED VALVEACTUATOR SHAFTS

H-60-11-ASAM-11MWO:

Priority Mnt Level

05-Sep-2012 OM

17-Sep-20121.0D CO 1-214TH

AVNALL UH-60A SERIES AIRCRAFTENGINE ANTI-ICE (AISBV)

H-60-12-ASAM-10MWO:

Priority Mnt Level



Inspection #

9119.58724660EH-60A

Till DueShelf LifeSerial NumberMFG DateLot #NarrativePart NumberDODIC

PROJECTEDDAYS: CURRENT HRS: Ser No.MDS:

Sorted By: Days to InspectionAUTOMATED CADS & PADS PROJECTIONSReport Date: Page 1 of 107-Mar-2018

999,999,999

MA630 22829701-Jan-2010MSB10A001-007MAIN FIRE EXT. #11512AS105MH-92 1455

MA633 22892901-Nov-2010MSB10E002-002RES. FIRE BOTTLE #11512AS105MH-92 1151

MA638 22891301-Mar-2010MSB10C002-002RES. FIRE BOTTLE #21512AS105MH92 1151

MA640 22826901-Jan-2010MSB10A001-007MAIN FIRE BOTTLE, #21512AS105MH92 1455

PIDMWODATE HRS



CONTROL HORN ASSY 8724660A241-144811. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

10-Dec-1998 OM

mae.p.belford17-Jul-2004

0.3USAAVNC, FT.RUCKER, AL(CA3091)

ALL H-60 SERIES AIRCRAFT,INSPECTION AND REVISEDRETIREMENT LIFE OF MAIN ROTORPITCH HORNS, P/N 70102-08111-047

UH-60-99-ASAM-06MWO:

Priority Mnt Level

10-Dec-1998 OM



ALL H-60 SERIES AIRCRAFT,INSPECTION AND REVISEDRETIREMENT LIFE OF MAIN ROTORPITCH HORNS, P/N 70102-08111-047


Priority Mnt Level



PIDMWODATE HRS



FUEL CONTROL 8724660154640971. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

05-Sep-2012 OM

theresa.d.pollard08-Sep-2012

2.0USAACE FT.RUCKER, AL.

ALL H-60A SERIES AIRCRAFT,HYDRO-MECHANICAL UNIT (HMU)

H-60-12-ASAM-11MWO:

Priority Mnt Level

27-Sep-2017 FM

KG419128-Sep-2017

0.5USAACEREMOVAL OF HYDRO-MECHANICALUNIT (HMU), PN 5074T79G07

H-60-17-ASAM-15MWO:

Priority Mnt Level



PIDMWODATE HRS



FUEL CONTROL 8724660UDAJ40081. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

27-Sep-2017 FM

KG419128-Sep-2017

0.5USAACEREMOVAL OF HYDRO-MECHANICALUNIT (HMU), PN 5074T79G07

H-60-17-ASAM-15MWO:

Priority Mnt Level



PIDMWODATE HRS



INPUT MODULE 8724660A264-001871. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

02-Aug-2000 OT

thomas.m.lilly08-Mar-2000

0.3D CO 2/501 AVAPO (ST5114)

ALL H-60 SERIES AIRCRAFT,REMOVAL OF INPUT MODULE GEARBOX ASSEMBLIESWITHPOTENTIALLY CRACKED BEVELGEARS

UH-60-00-02MWO:

Priority Mnt Level

21-Mar-2013 FM



PLASTIC MEDIA BLAST (PMB) ANDOXIDE FLAKE RESIDUE

H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



INPUT MODULE 8724660A264-028631. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

02-Aug-2000 OT

thomas.m.lilly08-Mar-2000

0.0D CO 2/501 AVAPO AE 09165(ST5114)

ALL H-60 SERIES AIRCRAFT,REMOVAL OF INPUT MODULE GEARBOX ASSEMBLIESWITHPOTENTIALLY CRACKED BEVELGEARS

UH-60-00-02MWO:

Priority Mnt Level

21-Mar-2013 FM




H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR BLADE ASSEMBLY 8724660A007-061091. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 2

10-Feb-2012 DM

AM521923-Jun-2016

130.0CCADRECAP REQUIREMENTS FOR THEUH-60 MAIN ROTOR BLADE P/N:70150-09100-043, NSN: 1615-01-106-1903

DMWR 1-1615-281MWO:

Priority Mnt Level

10-Feb-2012 DM

AM521923-Jun-2016

130.0CCADRECAP REQUIREMENTS FOR THEUH-60 MAIN ROTOR BLADE P/N:70150-09100-043, NSN: 1615-01-106-1903

DMWR 1-1615-281MWO:

Priority Mnt Level

09-Apr-2012 DM

AM521923-Jun-2016

1.0CCADCHANGE TO DEPOT REPAIREDLEGACY MAIN ROTOR BLADESCOMPLIANCE DATE.

H-60-12-SOF-05MWO:

Priority Mnt Level

09-Apr-2012 DM

AM521923-Jun-2016

1.0CCADCHANGE TO DEPOT REPAIREDLEGACY MAIN ROTOR BLADESCOMPLIANCE DATE.

H-60-12-SOF-05MWO:

Priority Mnt Level

06-May-2015 FM

christina.l.negron27-Jan-2017


H-60-15-ASAM-04 MAIN ROTORBLADE DEBONDING

H-60-15-ASAM-04MWO:

Priority Mnt Level

06-May-2015 FM




H-60-15-ASAM-04MWO:

Priority Mnt Level

11-Aug-2015 FM



MAIN ROTOR BLADE DEBONDINGAND TIP RIB CRACKING.

H-60-15-ASAM-07MWO:

Priority Mnt Level

11-Aug-2015 FM




H-60-15-ASAM-07MWO:

Priority Mnt Level

17-May-2016 FM



H-60-16-ASAM-05(MAIN ROTORBLADE DEBONDING)

H-60-16-ASAM-05MWO:

Priority Mnt Level

17-May-2016 FM




H-60-16-ASAM-05MWO:

Priority Mnt Level

27-Dec-2016 DM

KG419128-Dec-2016

0.5USAACEH-60-17-ASAM-03 M/R BLADEDEBONDING

H-60-17-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS




Page 2 of 2

27-Dec-2016 DM

KG419128-Dec-2016


H-60-17-ASAM-03MWO:

Priority Mnt Level

21-Feb-2017 FM

KG419123-Feb-2017

1.0USAACEMAIN ROTOR BLADE QUALITYESCAPEMENT

H-60-17-ASAM-05MWO:

Priority Mnt Level

21-Feb-2017 FM

KG419123-Feb-2017


H-60-17-ASAM-05MWO:

Priority Mnt Level

30-Oct-2017 FM

KG419101-Nov-2017

0.5USAACEMAIN ROTOR BLADE (MRB) PEELTEST

H-60-18-ASAM-01MWO:

Priority Mnt Level

30-Oct-2017 FM

KG419101-Nov-2017


H-60-18-ASAM-01MWO:

Priority Mnt Level



PIDMWODATE HRS




Page 1 of 1

06-May-2015 FM

theresa.d.pollard07-May-2015

2.0USAACE, FT.RUCKER, AL


H-60-15-ASAM-04MWO:

Priority Mnt Level

06-May-2015 FM




H-60-15-ASAM-04MWO:

Priority Mnt Level

11-Aug-2015 FM

kenneth.e.griffin10-Feb-2016

1.0USAACEMAIN ROTOR BLADE DEBONDINGAND TIP RIB CRACKING.

H-60-15-ASAM-07MWO:

Priority Mnt Level

11-Aug-2015 FM

kenneth.e.griffin10-Feb-2016

1.0USAACEMAIN ROTOR BLADE DEBONDINGAND TIP RIB CRACKING.

H-60-15-ASAM-07MWO:

Priority Mnt Level

17-May-2016 FM

kenneth.e.griffin19-May-2016

0.5USAACEH-60-16-ASAM-05(MAIN ROTORBLADE DEBONDING)

H-60-16-ASAM-05MWO:

Priority Mnt Level

17-May-2016 FM

kenneth.e.griffin19-May-2016


H-60-16-ASAM-05MWO:

Priority Mnt Level

27-Dec-2016 DM

KG419128-Dec-2016


H-60-17-ASAM-03MWO:

Priority Mnt Level

27-Dec-2016 DM

KG419128-Dec-2016


H-60-17-ASAM-03MWO:

Priority Mnt Level

21-Feb-2017 FM

KG419123-Feb-2017


H-60-17-ASAM-05MWO:

Priority Mnt Level

21-Feb-2017 FM

KG419123-Feb-2017


H-60-17-ASAM-05MWO:

Priority Mnt Level

30-Oct-2017 FM

KG419101-Nov-2017


H-60-18-ASAM-01MWO:

Priority Mnt Level

30-Oct-2017 FM

KG419101-Nov-2017


H-60-18-ASAM-01MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR BLADE ASSEMBLY 8724660A007146801. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 2

DR

RS100522-Aug-2013

130.0CCADMAIN ROTOR BLADE ASSEMBLY P/N:70150-09100-041 (NSN 1615-01-074-5150) AND P/N 70150-09100-043 (NSN1615-01-106-1903)

1-1615-281 C1MWO:

Priority Mnt Level

DR

RS100522-Aug-2013

130.0CCADMAIN ROTOR BLADE ASSEMBLY P/N:70150-09100-041 (NSN 1615-01-074-5150) AND P/N 70150-09100-043 (NSN1615-01-106-1903)

1-1615-281 C1MWO:

Priority Mnt Level

08-Sep-2002 OT

MG861305-Nov-2013

0.1AFM/RASM-CONE TIME INSP OF ALL M/R BLADECUFF ASSY.

SOF UH-60-02-11MWO:

Priority Mnt Level

08-Sep-2002 OT

MG861305-Nov-2013

0.1AFM/RASM-CONE TIME INSP OF ALL M/R BLADECUFF ASSY.

SOF UH-60-02-11MWO:

Priority Mnt Level

07-Jan-2003 DU

MG861305-Nov-2013

0.1AFM/RASM-CONE TIME INSPECTION OF M/RBLADE CUFF ASSY

SOF UH-60-03--2MWO:

Priority Mnt Level

07-Jan-2003 DU

MG861305-Nov-2013

0.1AFM/RASM-CONE TIME INSPECTION OF M/RBLADE CUFF ASSY

SOF UH-60-03--2MWO:

Priority Mnt Level

01-Jul-2003 DU

MG861305-Nov-2013

0.1AFM/RASM-CONE TIME INSPECTION OF M/RBLADE CUFF ASSY.

SOF UH-60-02-12MWO:

Priority Mnt Level

01-Jul-2003 DU

MG861305-Nov-2013

0.1AFM/RASM-CONE TIME INSPECTION OF M/RBLADE CUFF ASSY.

SOF UH-60-02-12MWO:

Priority Mnt Level

09-Apr-2012 DM

MG861305-Nov-2013

1.0AFM/RASM-CCHANGE TO DEPOT REPAIREDLEGACY MAIN ROTOR BLADESCOMPLIANCE DATE.

H-60-12-SOF-05MWO:

Priority Mnt Level

09-Apr-2012 DM

MG861305-Nov-2013

1.0AFM/RASM-CCHANGE TO DEPOT REPAIREDLEGACY MAIN ROTOR BLADESCOMPLIANCE DATE.

H-60-12-SOF-05MWO:

Priority Mnt Level

06-May-2015 FM

mae.p.belford07-May-2015



H-60-15-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR BLADE ASSEMBLY 8724660A007146801. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 2 of 2

06-May-2015 FM

mae.p.belford07-May-2015



H-60-15-ASAM-04MWO:

Priority Mnt Level

11-Aug-2015 FM

christina.l.negron10-May-2016



H-60-15-ASAM-07MWO:

Priority Mnt Level

11-Aug-2015 FM

christina.l.negron10-May-2016



H-60-15-ASAM-07MWO:

Priority Mnt Level

17-May-2016 FM




H-60-16-ASAM-05MWO:

Priority Mnt Level

17-May-2016 FM




H-60-16-ASAM-05MWO:

Priority Mnt Level

27-Dec-2016 DM

KG419128-Dec-2016


H-60-17-ASAM-03MWO:

Priority Mnt Level

27-Dec-2016 DM

KG419128-Dec-2016


H-60-17-ASAM-03MWO:

Priority Mnt Level

21-Feb-2017 FM

KG419123-Feb-2017


H-60-17-ASAM-05MWO:

Priority Mnt Level

21-Feb-2017 FM

KG419123-Feb-2017


H-60-17-ASAM-05MWO:

Priority Mnt Level

30-Oct-2017 FM

KG419101-Nov-2017


H-60-18-ASAM-01MWO:

Priority Mnt Level

30-Oct-2017 FM

KG419101-Nov-2017


H-60-18-ASAM-01MWO:

Priority Mnt Level



PIDMWODATE HRS




Page 1 of 2

OT

thomas.m.lilly30-Apr-2010

1.0USAACE, FT.RUCKER, AL(JT0967)

ALL H-60A/K/L SERIES AIRCRAFT,DEPOT REPAIRED LEGACY MAINROTOR BLADES

H-60-10-SOF-01MWO:

Priority Mnt Level

OT



ALL H-60A/K/L SERIES AIRCRAFT,DEPOT REPAIRED LEGACY MAINROTOR BLADES

H-60-10-SOF-01MWO:

Priority Mnt Level

08-Sep-2002 OT

thomas.m.lilly18-Jul-2009


ALL H-60 SERIES AIRCRAFT, ONE-TIME INSPECTION OF MAIN ROTORBLADE CUFF ASSEMBLY

UH-60-02-11MWO:

Priority Mnt Level

08-Sep-2002 OT



ALL H-60 SERIES AIRCRAFT, ONE-TIME INSPECTION OF MAIN ROTORBLADE CUFF ASSEMBLY

UH-60-02-11MWO:

Priority Mnt Level

08-Dec-2002 OT



ALL H-60 SERIES AIRCRAFT,REVISION TO UH-60-02-11, ONE-TIMEINSPECTION OF MAIN ROTOR BLADECUFF ASSEMBLY

UH-60-02-12MWO:

Priority Mnt Level

08-Dec-2002 OT



ALL H-60 SERIES AIRCRAFT,REVISION TO UH-60-02-11, ONE-TIMEINSPECTION OF MAIN ROTOR BLADECUFF ASSEMBLY

UH-60-02-12MWO:

Priority Mnt Level

09-Apr-2012 DM

thomas.e.mitchell17-Apr-2012


CHANGE TO DEPOT REPAIREDLEGACY MAIN ROTOR BLADESCOMPLIANCE DATE.

H-60-12-SOF-05MWO:

Priority Mnt Level

09-Apr-2012 DM



CHANGE TO DEPOT REPAIREDLEGACY MAIN ROTOR BLADESCOMPLIANCE DATE.

H-60-12-SOF-05MWO:

Priority Mnt Level

06-May-2015 FM




H-60-15-ASAM-04MWO:

Priority Mnt Level

06-May-2015 FM




H-60-15-ASAM-04MWO:

Priority Mnt Level

thomas.e.mitchell



PIDMWODATE HRS




Page 2 of 2

11-Aug-2015 FM




H-60-15-ASAM-07MWO:

Priority Mnt Level

11-Aug-2015 FM




H-60-15-ASAM-07MWO:

Priority Mnt Level

17-May-2016 FM

thomas.e.mitchell18-May-2016


H-60-16-ASAM-05MWO:

Priority Mnt Level

17-May-2016 FM

thomas.e.mitchell18-May-2016


H-60-16-ASAM-05MWO:

Priority Mnt Level

27-Dec-2016 DM

mary.b.hodge28-Dec-2016


H-60-17-ASAM-03 M/R BLADEDEBONDING

H-60-17-ASAM-03MWO:

Priority Mnt Level

27-Dec-2016 DM

mary.b.hodge28-Dec-2016


H-60-17-ASAM-03 M/R BLADEDEBONDING

H-60-17-ASAM-03MWO:

Priority Mnt Level

21-Feb-2017 FM

KG419123-Feb-2017


H-60-17-ASAM-05MWO:

Priority Mnt Level

21-Feb-2017 FM

KG419123-Feb-2017


H-60-17-ASAM-05MWO:

Priority Mnt Level

30-Oct-2017 FM

KG419101-Nov-2017


H-60-18-ASAM-01MWO:

Priority Mnt Level

30-Oct-2017 FM

KG419101-Nov-2017


H-60-18-ASAM-01MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSEMBLY 8724660A001-042231. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 3

20-Aug-1996 OM



ALL H-60 AIRCRAFT, REPLACEMENTOF ALL SPINDLE ASSEMBLIES WITHTHE SPINDLE RETAINING ROD P/N70102-08102-102/103MANUFACTURED BY THE PURDYCORPORATION INSTALLED


Priority Mnt Level

20-Aug-1996 OM





Priority Mnt Level

13-Jul-2000 DU



INSPECTION OF SPINDLE LUGS FORCRACKS

UH-60-00-01MWO:

Priority Mnt Level

13-Jul-2000 DU



INSPECTION OF SPINDLE LUGS FORCRACKS

UH-60-00-01MWO:

Priority Mnt Level

05-Mar-2001 FT



ALL H-60 AIRCRAFT, REVISION TO UH-60-00-01 INSPECTION OF MAINROTOR SPINDLE

UH-60-01-05MWO:

Priority Mnt Level

05-Mar-2001 FT




UH-60-01-05MWO:

Priority Mnt Level

26-Mar-2002 OM



ALL H-60 SERIES AIRCRAFT,REMOVAL OF CHICAGO RAWHIDEM/R SPINDLE THRUST BEARINGSWITH SERIAL NUMBERS C325-00001THROUGH C325-02407


Priority Mnt Level

26-Mar-2002 OM





Priority Mnt Level

tammy.k.murphy17-Nov-2010

0.5USAACE FTRUCKER, AL

SPINDLE LUG UNTRASONIC INSPUH-60-08-ASAM-09MWO:

Priority Mnt Level



PIDMWODATE HRS




Page 2 of 3

30-Jun-2008 FM

30-Jun-2008 FM




Priority Mnt Level

17-Sep-2012 OM

janice.m.bruce29-Sep-2012

1.0USAACE (TITB1027)

MAIN ROTOR SPINDLE SUB-COMPONENT TRACKINGREQUIREMENTS

H-60-12-AMAM-16MWO:

Priority Mnt Level

17-Sep-2012 OM

janice.m.bruce29-Sep-2012

1.0USAACE (TITB1027)


H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

loletia.v.williams02-Mar-2013

0.8USAACE. FT.RUCKER, AL

MAIN ROTOR SPINDLE ANTI-FLAPASSY (CORRECTION)

H-60-13-ASAM-03MWO:

Priority Mnt Level

26-Feb-2013 FM

loletia.v.williams02-Mar-2013

0.8USAACE. FT.RUCKER, AL


H-60-13-ASAM-03MWO:

Priority Mnt Level

17-Nov-2015 FM

tammy.k.murphy05-Jun-2016


AUTHORIZATION TO USE LOCALLYFABRICATED TOOL TO REMOVE ANDINSTALL BUSHINGS.

F305945BMWO:

Priority Mnt Level

17-Nov-2015 FM

tammy.k.murphy05-Jun-2016



F305945BMWO:

Priority Mnt Level

22-Jan-2016 FM

cynthia.w.moore25-Mar-2016

1.0USAACE, FTRUCKER, AL

AUTHORIZATION TO USE MACHINESHOP DESIGNED PULLER.

F305943MWO:

Priority Mnt Level

22-Jan-2016 FM

cynthia.w.moore25-Mar-2016

1.0USAACE, FTRUCKER, AL

AUTHORIZATION TO USE MACHINESHOP DESIGNED PULLER.

F305943MWO:

Priority Mnt Level

27-Sep-2016 FM

tammy.k.murphy27-Sep-2016


AUTHORIZATION TO SUB SHEARBOLD NAS 1954-6 WHENASSEMBLING THRUST BEARING TOELASTOMERIC SPHERICAL BEARING

F317778MWO:

Priority Mnt Level



AUTHORIZATION TO SUB SHEARBOLD NAS 1954-6 WHENASSEMBLING THRUST BEARING TO

F317778MWO:



PIDMWODATE HRS




Page 3 of 3

27-Sep-2016 FM

ELASTOMERIC SPHERICAL BEARING

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSEMBLY 8724660D001-115021. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

30-Jun-2008 FM




Priority Mnt Level

30-Jun-2008 FM




Priority Mnt Level

17-Sep-2012 OM




H-60-12-AMAM-16MWO:

Priority Mnt Level

17-Sep-2012 OM




H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

tammy.k.murphy27-Feb-2013



H-60-13-ASAM-03MWO:

Priority Mnt Level

26-Feb-2013 FM




H-60-13-ASAM-03MWO:

Priority Mnt Level

17-Nov-2015 FM




F305945BMWO:

Priority Mnt Level

17-Nov-2015 FM




F305945BMWO:

Priority Mnt Level

27-Sep-2016 FM




F317778MWO:

Priority Mnt Level

27-Sep-2016 FM




F317778MWO:

Priority Mnt Level



PIDMWODATE HRS




Page 1 of 1

20-Aug-1996 OM

tammy.k.murphy17-Jul-2004




Priority Mnt Level

20-Aug-1996 OM





Priority Mnt Level

11-Jul-2000 OM



ALL H-60 ACFT INITIAL ANDRECURRING INSP OF M/R SPINDLELUGS

SOF UH-60-00-01MWO:

Priority Mnt Level

11-Jul-2000 OM



ALL H-60 ACFT INITIAL ANDRECURRING INSP OF M/R SPINDLELUGS

SOF UH-60-00-01MWO:

Priority Mnt Level

05-Mar-2001 FT




SOF UH-60-01-05MWO:

Priority Mnt Level

05-Mar-2001 FT




SOF UH-60-01-05MWO:

Priority Mnt Level

26-Mar-2002 OM





Priority Mnt Level

26-Mar-2002 OM





Priority Mnt Level



PIDMWODATE HRS




Page 1 of 1

30-Jun-2008 FM




Priority Mnt Level

30-Jun-2008 FM




Priority Mnt Level

17-Sep-2012 OM




H-60-12-AMAM-16MWO:

Priority Mnt Level

17-Sep-2012 OM




H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM




H-60-13-ASAM-03MWO:

Priority Mnt Level

26-Feb-2013 FM




H-60-13-ASAM-03MWO:

Priority Mnt Level

17-Nov-2015 FM

tammy.k.murphy16-May-2016



F305945BMWO:

Priority Mnt Level

17-Nov-2015 FM

tammy.k.murphy16-May-2016



F305945BMWO:

Priority Mnt Level

27-Sep-2016 FM

tammy.k.murphy13-Oct-2016



F317778MWO:

Priority Mnt Level

27-Sep-2016 FM

tammy.k.murphy13-Oct-2016



F317778MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN TRANSMISSION MODULE 8724660A265-009461. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

21-Mar-2013 FM




H-60-13-ASAM-04MWO:

Priority Mnt Level

25-Sep-2017 FM

KG419102-Oct-2017

1.0USAACEH-60-17-ASAM-14 PLANETARYCARRIER RETIREMENT LIFEREDUCTION

H-60-17-ASAM-14MWO:

Priority Mnt Level



PIDMWODATE HRS



M/R BLADE CUFF 8724660G237-006421. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

OM



ALL EH-60A/L, UH-60A/L, MH-60L ANDMH-60K AIRCRAFT, INCREASE INFATIGUE LIFE FOR THE MAIN ROTORBLADE CUFFS, P/N 70150-09109-041AND 70150-09109-043


Priority Mnt Level

OM



ALL EH-60A/L, UH-60A/L, MH-60L ANDMH-60K AIRCRAFT, INCREASE INFATIGUE LIFE FOR THE MAIN ROTORBLADE CUFFS, P/N 70150-09109-041AND 70150-09109-043


Priority Mnt Level

03-Jul-1997 OU

mary.b.hodge05-Oct-2011


INCREASE IN FATIGUE LIFE FOR THEMAIN ROTOR BLADE CUFFS, P/N70150-09109-041 AND 70150-09109-043 ALL EH-60A /L, UH-60A/L, MH-60LAND MH-60K AIRCRAFT

1-1520-237-20-192MWO:

Priority Mnt Level

03-Jul-1997 OU

mary.b.hodge05-Oct-2011


INCREASE IN FATIGUE LIFE FOR THEMAIN ROTOR BLADE CUFFS, P/N70150-09109-041 AND 70150-09109-043 ALL EH-60A /L, UH-60A/L, MH-60LAND MH-60K AIRCRAFT

1-1520-237-20-192MWO:

Priority Mnt Level

01-Jul-2003 OT



ALL H-60 SERIES AIRCRAFT,INSPECTION OF MAIN ROTOR BLADECUFF ASSEMBLY

UH-60-03-02MWO:

Priority Mnt Level

01-Jul-2003 OT



ALL H-60 SERIES AIRCRAFT,INSPECTION OF MAIN ROTOR BLADECUFF ASSEMBLY

UH-60-03-02MWO:

Priority Mnt Level



PIDMWODATE HRS



MTCHD ROTOR/STATOR ASSY 8724660MRS096191. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

02-Jan-2018 FM

kenneth.e.griffin03-Jan-2018

0.5USAACEH-60-18-ASAM-04 REMOVAL OFTURBINE ROTOR ASSEMBLIES

H-60-18-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



MTCHD ROTOR/STATOR ASSY 8724660MRS097441. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

02-Jan-2018 FM

kenneth.e.griffin03-Jan-2018

0.5USAACEH-60-18-ASAM-04 REMOVAL OFTURBINE ROTOR ASSEMBLIES

H-60-18-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



PUMP MODULE ASSY, HYDRAULIC 8724660K3399ABR1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

29-Jul-2005 DR

MU855130-May-2015

54.0CCADRECAPPEDDMWR 1-4320-271MWO:

Priority Mnt Level



PIDMWODATE HRS



PUMP MODULE ASSY, HYDRAULIC 8724660K4169ABR1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

29-Jul-2005 DM

MU855123-Jun-2012

54.0CCADUTILITY PUMP MODULE ASSEMBLY -PART NUMBER (NATIONAL STOCKNUMBER) - 70652-02300-048 (4320-01-092-6724), 70652-02300-049 (4320-01-136-2118), 70652-02300-050 (4320-01-207-7228)

1-4320-271MWO:

Priority Mnt Level



SECTION I COCKPITEH-60A_BASELINE

4. EQUIPMENT CHECKLIST

8724660 EH-60A

3. AREA NAME 2. MODEL 1. SERIAL NUMBER

Page 1 of 10

1RECEIVER RADIO - R-1496A/ARN-89

U UUUUUUUU UU 11

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER

QTY REQNOMENCLATURE:ITEM NO

2DISPLACEMENT GYRO - CN-1314/A (9000C)

U UUUUUUUU UU 11

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 00

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 01

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING FOR KIT-1A/1C/TSEC - MT-3949A/U

U UUUUUUUU UU 11

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 11

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 11

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMMAND INSTR SYS PROCESSOR - 70600-01038-101

U UUUUUUUU UU 11

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING RACK - 70600-01038-102

U UUUUUUUU UU 11

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SAS AMPLIFIER - 70901-02908-104

U UUUUUUUU UU 11

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO ASSEMBLY - 70600-01047-041

U UUUUUUUU UU 11

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2RATE GYRO - TRU-2A/A

U UUUUUUUU UU 11

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 33

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3BATTERY FOR KY 58 - BA-1372/U

U UUUUUUUU UU 00

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 00

15

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

AIRCRAFT INVENTORY RECORDDA FORM 2408-17, NOV 1991



8724660 EH-60A


Page 2 of 10

3REMOTE CONTROL UNIT (KY-58) - Z-AHP/YSEC

U UUUUUUUU UU 00

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 01

17

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#2 VHF-FM ANTENNA COUPLER - 70600-01010-104

U UUUUUUUU UU 00

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 11

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 22

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 22

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GLIDE SLOPE ANTENNA - 70600-01043-101

U UUUUUUUU UU 11

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 11

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 22

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRE EXTINGUISHER - FR23-4-11848

U UUUUUUUU UU 11

25

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2BAROMETERIC ALTIMETER - AAU-32/A

U UUUUUUUU UU 22

26

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2CREW SEAT - D3801-2

U UUUUUUUU UU 33

27

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2AIRCRAFT CLOCK - ABU-11A

U UUUUUUUU UU 22

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 00

29

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2INTERPHONE CONTROL - C6533/ARC

U UUUUUUUU UU 22

30

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8724660 EH-60A


Page 3 of 10

1RECEIVER/TRANSMITTER - RT-1115D/APN-209

U UUUUUUUU UU 11

31

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 11

32

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 11

33

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 01

34

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL - C-11466A/ARC-201

U UUUUUUUU UU 00

35

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPARATOR SIGNAL DATA - CM482/ARC186(V)

U UUUUUUUU UU 11

36

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3MOUNT - MT-6051/ARC-186

U UUUUUUUU UU 33

37

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 01

38

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 11

39

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 00

40

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RADIO RETRANSMISSION PANEL -70550-01008-042

U UUUUUUUU UU 11

41

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MAGNETIC COMPASS - MS17983-4

U UUUUUUUU UU 11

42

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2OUTSIDE AIR TEMP INDICATOR - MS28028-1

U UUUUUUUU UU 22

43

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOUR WING PANEL - 70500-01152-093

U UUUUUUUU UU 11

44

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOUR WING PANEL - 70500-01152-094

U UUUUUUUU UU 11

45

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8724660 EH-60A


Page 4 of 10

1STABILATOR/FLT CONT PNL - 70902-01070-048

U UUUUUUUU UU 11

46

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 00

47

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 00

48

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT FOR ASN-132 MT-4915/A

U UUUUUUUU UU 00

49

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 00

50

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1TACAN RECEIVER/TRANSMITTER RT-1159/A

U UUUUUUUU UU 00

51

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ELECTRONIC SEQUENCE UNIT, 163290-100-E

U UUUUUUUU UU 00

52

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RADAR DETECTION SET SIGNAL AN/APR39

U UUUUUUUU UU 00

53

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 00

54

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1DISPENSER GENERAL PURPOSE AIRCRAFT M130

U UUUUUUUU UU 00

55

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3SECURE SPEECH UNIT TSEC/KY-58

U UUUUUUUU UU 00

56

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 00

57

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1KY-100 AIRTERM 0N616736-1

U UUUUUUUU UU 00

58

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CONTROL DISPLAY UNIT C-12346/URC

U UUUUUUUU UU 00

59

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPUTER DISPLAY UNIT CP-1252C/ASN 128B/128D

U UUUUUUUU UU 01

60

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER




of 10SERIAL NUMBER MODEL AREA NAME

8724660 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

james.m.aldri1 CIV 06-Mar-2018

michael.t.woo2 CIV 26-Mar-2018

b. LOCATION/REMARKSCHECK NO.

6. LOCATION OR REMARKS

a. ITEM NUMBER

Nomenclature

DISPLACEMENT GYRO - CN-1314/A (9000C)

1 ACFT ARRIVED IN THIS CONFIGURATION2

DISPLACEMENT GYRO - CN-1314/A (9000C)


GYRO, DIRECTIONAL - CN-998/ASN-43


GYRO, DIRECTIONAL - CN-998/ASN-43


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

2 COMPONENT REMOVED PER GOVERNMENT DIRECTIVE4

RATE GYRO - TRU-2A/A1 ACFT ARRIVED IN THIS CONFIGURATION12

RATE GYRO - TRU-2A/A2 ACFT ARRIVED IN THIS CONFIGURATION12

BATTERY FOR KY 58 - BA-1372/U


BATTERY FOR KY 58 - BA-1372/U


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


REVERSE OF DA FORM 2408-17, NOV 1991




db c


CHECK CHECK

ba ad

5. VERIFICATION

c



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


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

1 16

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


AMPLIFIER IMPEDANCE - AM-4859A/ARN-89


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


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


CREW SEAT - D3801-21 ACFT ARRIVED IN THIS CONFIGURATION27

CREW SEAT - D3801-22 ACFT ARRIVED IN THIS CONFIGURATION27

RECEIVER/TRANSMITTER - RT-1477/ARC-201


RECEIVER/TRANSMITTER - RT-1477/ARC-201


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






db c


CHECK CHECK

ba ad

5. VERIFICATION

c



CONTROL - C-11466A/ARC-2011 ACFT ARRIVED IN THIS CONFIGURATION35

CONTROL - C-11466A/ARC-2012 ACFT ARRIVED IN THIS CONFIGURATION35

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


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


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


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


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


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


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


MOUNT FOR ASN-132 MT-4915/A






db c


CHECK CHECK

ba ad

5. VERIFICATION

c



MOUNT FOR ASN-132 MT-4915/A


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


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


TACANRECEIVER/TRANSMITTER RT-1159/A


TACANRECEIVER/TRANSMITTER RT-1159/A


ELECTRONIC SEQUENCEUNIT, 163290-100-E


ELECTRONIC SEQUENCEUNIT, 163290-100-E


RADAR DETECTION SETSIGNAL AN/APR39


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


SECURE SPEECH UNITTSEC/KY-58


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


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


KY-100 AIRTERM 0N616736-11 ACFT ARRIVED IN THIS CONFIGURATION58

KY-100 AIRTERM 0N616736-12 ACFT ARRIVED IN THIS CONFIGURATION58

CONTROL DISPLAY UNIT C-12346/URC


CONTROL DISPLAY UNIT C-12346/URC






db c


CHECK CHECK

ba ad

5. VERIFICATION

c



COMPUTER DISPLAY UNIT CP-1252C/ASN 128B/128D



SECTION II CABINEH-60A_BASELINE


8724660 EH-60A


Page 1 of 7

1INERTIAL NAVIGATION SET - AN/ASN-141

U UUUUUUUU UU 00

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BEARING, DISTANCE, HEADING INDICATOR - ID2301/U

U UUUUUUUU UU 00

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MARKER BEACON ANTENNA - 70600-02011-103

U UUUUUUUU UU 11

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-104

U UUUUUUUU UU 11

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-105

U UUUUUUUU UU 11

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRST AID KIT - 6545-00919-6650

U UUUUUUUU UU 11

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRE EXTINGUISHER - FR23-4-11848

U UUUUUUUU UU 11

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CRASH AXE - 56D6221

U UUUUUUUU UU 11

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HAND SET - H-250/U

U UUUUUUUU UU 11

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SLAB BATTERY - D8565/11-1

U UUUUUUUU UU 11

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3INTERPHONE CONTROL - C6533/ARC

U UUUUUUUU UU 33

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ADAPTER FUEL DRAIN - 70307-03018-102

U UUUUUUUU UU 00

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


4LOCK ASSY BLADE TIEDOWN - 70700-20369-041

U UUUUUUUU UU 44

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2PLUG ASSY INTAKE - HIRSS SUPP - 70700-20515-041/042

U UUUUUUUU UU 00

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 00

15

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8724660 EH-60A


Page 2 of 7

1PLUG ASSY APU EXHAUST - 70700-20509-041

U UUUUUUUU UU 00

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COVER ASSY OIL COOLER - 70700-20511-041

U UUUUUUUU UU 00

17

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BLADE FOLD SET - 70700-20412-011

U UUUUUUUU UU 00

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER PITOT TUBE - 70700-20460-041

U UUUUUUUU UU 22

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1TROOP SEATS - 70500-02151-045

U UUUUUUUU UU 00

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER ENGINE INLET - 83DSCC-D006

U UUUUUUUU UU 00

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 00

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 00

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ICS WALK-AROUND CORD - 70602-02016-041

U UUUUUUUU UU 00

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 00

25

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HYD. PUMP HANDLE - 15400-50126

U UUUUUUUU UU 11

26

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2EQUIPMENT LOGBOOK - MIL-D-43064

U UUUUUUUU UU 22

27

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPUTER LOGBOOK

U UUUUUUUU UU 00

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1WEIGHT AND BALANCE HANDBOOK - TM 55-1500-342-23

U UUUUUUUU UU 11

29

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


4TIEDOWN ASSEMBLY, TOW - 70700-20433-045

U UUUUUUUU UU 00

30

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8724660 EH-60A


Page 3 of 7

1ELECTRONIC SEQUENCE UNIT, 163290-100-E

U UUUUUUUU UU 11

52

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8724660 EH-60A_BASELIN SECTION II CABINEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c





a. ITEM NUMBER

Nomenclature

INERTIAL NAVIGATION SET -AN/ASN-141


INERTIAL NAVIGATION SET -AN/ASN-141


BEARING, DISTANCE,HEADING INDICATOR -ID2301/U


BEARING, DISTANCE,HEADING INDICATOR -ID2301/U


ADAPTER FUEL DRAIN - 70307-03018-102


ADAPTER FUEL DRAIN - 70307-03018-102


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


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


PLUG ASSY EXHAUST - HIRSS- 70700-20515-043


PLUG ASSY EXHAUST - HIRSS- 70700-20515-043






db c


CHECK CHECK

ba ad

5. VERIFICATION

c



PLUG ASSY APU EXHAUST -70700-20509-041


PLUG ASSY APU EXHAUST -70700-20509-041


COVER ASSY OIL COOLER -70700-20511-041


COVER ASSY OIL COOLER -70700-20511-041


BLADE FOLD SET - 70700-20412-011


BLADE FOLD SET - 70700-20412-011


TROOP SEATS - 70500-02151-045


TROOP SEATS - 70500-02151-045


COVER ENGINE INLET -83DSCC-D006


COVER ENGINE INLET -83DSCC-D006


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






db c


CHECK CHECK

ba ad

5. VERIFICATION

c


michael.t.woo2 CIV 26-Mar-201870751-02023-043

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


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


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


ICS WALK-AROUND CORD -70602-02016-041


ICS WALK-AROUND CORD -70602-02016-041


PORTABLE INSP. FLOODLIGHT - 15-0366-1


PORTABLE INSP. FLOODLIGHT - 15-0366-1


COMPUTER LOGBOOK1 ACFT ARRIVED IN THIS CONFIGURATION28

COMPUTER LOGBOOK2 REMOVED PER GOVERNMENT DIRECTIVE28

TIEDOWN ASSEMBLY, TOW -70700-20433-045






db c


CHECK CHECK

ba ad

5. VERIFICATION

c



TIEDOWN ASSEMBLY, TOW -70700-20433-045



SECTION III TRANSITION SECTIONEH-60A_BASELINE


8724660 EH-60A


Page 1 of 2

1ANTENNA, LOOP - AS-2108A/ARN-89

U UUUUUUUU UU 11

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2IFF ANTENNA - 70600-02010-103

U UUUUUUUU UU 22

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF/AM ANTENNA 70600-03002-104

U UUUUUUUU UU 11

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PUMP FUEL SAMPLER - 82829/4P156-3

U UUUUUUUU UU 00

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPENSATOR MAGNETIC FLUX - CN-405/ASN

U UUUUUUUU UU 11

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS TRANSMITTER - T-611/ASN-43

U UUUUUUUU UU 11

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GPS ANTENNA 22433-40

U UUUUUUUU UU 11

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF AMPLIFIER COUPLER AM-7531/URC

U UUUUUUUU UU 00

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER/TRANSMITTER RT-1749/URC

U UUUUUUUU UU 00

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 00

54

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8724660 EH-60A_BASELIN SECTION III TRANSITION SECTIONEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c





a. ITEM NUMBER

Nomenclature

PUMP FUEL SAMPLER -82829/4P156-3


PUMP FUEL SAMPLER -82829/4P156-3


HF AMPLIFIER COUPLER AM-7531/URC


HF AMPLIFIER COUPLER AM-7531/URC


RECEIVER/TRANSMITTER RT-1749/URC


RECEIVER/TRANSMITTER RT-1749/URC







SECTION IV TAIL CONEEH-60A_BASELINE


8724660 EH-60A


Page 1 of 2

2VOR/LOC ANTENNA - 70600-05002-101

U UUUUUUUU UU 22

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF ANTENNA 4700516-30

U UUUUUUUU UU 00

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1DISPENSER GENERAL PURPOSE AIRCRAFT M130

U UUUUUUUU UU 00

55

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8724660 EH-60A_BASELIN SECTION IV TAIL CONEEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c





a. ITEM NUMBER

Nomenclature

HF ANTENNA 4700516-301 ACFT ARRIVED IN THIS CONFIGURATION2

HF ANTENNA 4700516-302 ACFT ARRIVED IN THIS CONFIGURATION2






SECTION V TAIL ROTOR PYLONEH-60A_BASELINE


8724660 EH-60A


Page 1 of 2

1TROOP COMMANDER ANTENNA - 70600-06001-104

U UUUUUUUU UU 11

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

U UUUUUUUU UU 11

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8724660 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 8724660B300030401. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

16-May-2016 FM

tammy.k.murphy23-Jan-2017

0.5USAACETAIL ROTOR SAFETY CABLE.H-60-16-AMAM-07MWO:

Priority Mnt Level

16-May-2016 FM

tammy.k.murphy23-Jan-2017

0.5USAACETAIL ROTOR SAFETY CABLE.H-60-16-AMAM-07MWO:

Priority Mnt Level

21-Nov-2016 FM

kenneth.e.griffin24-Nov-2016

1.0USAACETAIL ROTOR SERVO PILOT INPUTARM ASSEMBLY

H-60-17-ASAM-02MWO:

Priority Mnt Level

21-Nov-2016 FM

kenneth.e.griffin24-Nov-2016

1.0USAACETAIL ROTOR SERVO PILOT INPUTARM ASSEMBLY

H-60-17-ASAM-02MWO:

Priority Mnt Level



PIDMWODATE HRS



SWASHPLATE ASSEMBLY 8724660U31. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

02-Dec-1996 OT

thomas.m.lilly04-Dec-1996

1.0D CO 2/501 AVREG APO AE09165(RC3061)

REMOVAL OF CERTAIN REWORKEDMAIN ROTOR SWASHPLATEASSEMBLIES, ALL UH-60A, UH-60L,EM-60A, AND MH-60K HELICOPTERS

UH-60-97-01MWO:

Priority Mnt Level

02-Dec-1996 OT

thomas.m.lilly04-Dec-1996

1.0D CO 2/501 AVREG APO AE09165(RC3061)

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


0.1D 2/501 AVN(DA666)

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


Priority Mnt Level

08-Sep-1997 OM


0.1D 2/501 AVN(DA666)

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


Priority Mnt Level

02-Nov-1998 OM

thomas.m.lilly10-Oct-1998

0.0A CO 127 ASBAPO AE 09165(JI7391)

ALL H-60 AIRCRAFT, RESTORATIONOF FULL SERVICE LIFE ON THESWASHPLATE LINK ASSEMBLY, P/N70400-08110-054/-061,MANUFACTURED BY TEK (CAGECODE 65780)


Priority Mnt Level

02-Nov-1998 OM

thomas.m.lilly10-Oct-1998

0.0A CO 127 ASBAPO AE 09165(JI7391)

ALL H-60 AIRCRAFT, RESTORATIONOF FULL SERVICE LIFE ON THESWASHPLATE LINK ASSEMBLY, P/N70400-08110-054/-061,MANUFACTURED BY TEK (CAGECODE 65780)


Priority Mnt Level

12-Jun-2006 OM

thomas.m.lilly12-Jun-2006

2.0USAAWC, FT.RUCKER, AL(MB4039)

ALL H-60 SERIES AIRCRAFT,SWASHPLATE DUPLEX BEARING


Priority Mnt Level

12-Jun-2006 OM

thomas.m.lilly12-Jun-2006

2.0USAAWC, FT.RUCKER, AL(MB4039)

ALL H-60 SERIES AIRCRAFT,SWASHPLATE DUPLEX BEARING


Priority Mnt Level



PIDMWODATE HRS



T700-GE-700 ENGINE ASSY 8724660GE-E-2078491. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

30-Mar-1990 OM

JD813922-Feb-2011

0.0WOMUAASELF SEAL ADAPTER ASSEMBLY1-2840-248-50-28MWO:

Priority Mnt Level

31-Mar-1993 DR

JD813922-Feb-2011

0.0WOMUAAINSTALLATION OF PTO DRIVEASSEMBLY P/NS 5044T27G02 OR5056T66G02 (T700-GE-700 AND 701ENGINES)

1-2840-248-50-29MWO:

Priority Mnt Level

30-Jun-1994 OR

JD813922-Feb-2011

1.0WOMUAAONE TIME INSPECTION ANDCONVERSION OF FORMS ANDRECORDS FOR T700-GE-700, -701AND -701C SERIES GAS TURBINEENGINES

1-2840-248-20-2MWO:

Priority Mnt Level

22-Sep-2008 OM

JD813920-Feb-2011

0.0JD8139ALL H-60 AND H-64 SERIESAIRCRAFT, SUSPECT ENGINEHARNESSES

H-60-08-ASAM-14MWO:

Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR BLADE ASSEMBLY 8724660A009-036171. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

17-May-2017 FM

KG419125-May-2017

1.0USAACEH-60-17-SOF-04 TAIL ROTORTORQUE TUBE

H-60-17-SOF-04MWO:

Priority Mnt Level

17-May-2017 FM

KG419125-May-2017


H-60-17-SOF-04MWO:

Priority Mnt Level

06-Jul-2017 FT

KG419110-Jul-2017

1.0USAACEH-60-17-SOF-05 UPDATED TAILROTOR (TR) TORQUE TUBEINSPECTION

H-60-17-SOF-05MWO:

Priority Mnt Level

06-Jul-2017 FT

KG419110-Jul-2017


H-60-17-SOF-05MWO:

Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR BLADE ASSEMBLY 8724660A009082181. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER

Page 1 of 1

17-May-2017 FM

KG419125-May-2017


H-60-17-SOF-04MWO:

Priority Mnt Level

17-May-2017 FM

KG419125-May-2017


H-60-17-SOF-04MWO:

Priority Mnt Level

06-Jul-2017 FT

KG419110-Jul-2017


H-60-17-SOF-05MWO:

Priority Mnt Level

06-Jul-2017 FT

KG419110-Jul-2017


H-60-17-SOF-05MWO:

Priority Mnt Level



UNIT UNIQUE INVENTORYEH-60A_BASELINE


8724660 EH-60A


Page 1 of 2

1ATTITUDE AND HEADING REFERENCE UNIT (CN1716/A)

U UUUUUUUU UU 11

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IFM AMPLIFIER AM-7189A/ARC

U UUUUUUUU UU 01

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT IFM AMP PN: MT-6592/ARC

U UUUUUUUU UU 11

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BFT ANTENNA GPS PN: S671575-863

U UUUUUUUU UU 11

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BFT ANTENNA L-BAND PN: S65-8282-301

U UUUUUUUU UU 11

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BFT PALLET ASSY PN: 080094-1

U UUUUUUUU UU 01

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2IGNITION KEYS

U UUUUUUUU UU 00

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1AHRU CONTROL HEAD (CN1716/A)

U UUUUUUUU UU 11

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





8724660 EH-60A_BASELIN UNIT UNIQUE INVENTORYEH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c





a. ITEM NUMBER

Nomenclature

IFM AMPLIFIER AM-7189A/ARC2 COMPONENT REMOVED PER GOVERNMENT DIRECTIVE2

BFT PALLET ASSY PN: 080094-1


IGNITION KEYS1 ACFT ARRIVED IN THIS CONFIGURATION7

IGNITION KEYS2 ACFT ARRIVED IN THIS CONFIGURATION7


1. nomenclature 2. model 3. aircraft serial …€¦ · date mwo pid hrs and mwo title applying or...

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