DA Form 2408-5 - Equipment Modification Record · mwo:1-1520-237-50-56 c2 prioritymnt level 31-mar-1997 r d tasm-o europe 178 26-may-2000 an/asn-128b doppler/gps navigation system

PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN

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

8323869UH-60AHELICOPTER, UTILITY

3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE

Report Date: Page 1 of 508-Jan-2016

DR21-Jun-2004

0MODIFICATION 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

DR30-Apr-1991

TASM-OEUROPE

17701-MAY-1993

MODIFICATION OF THE HOVERINFERRED SUPPRESSION SYSTEM(UH-60A HELICOPTERS) NATIONALSTOCK NUMBER (NSN) 1520-01-035-0266

1-1520-237-50-63 B-KITMWO:

Mnt LevelPriority

DN01-Jan-1900

L3 COMMBLUEGRASSARMY DEPOT(HA9430)

0.101-Sep-2003

SSG BRODIN,RYAN D

WX-1000 STORMSCOPE WEATHERMAPPING SYSTEM

LEX 1871MWO:

Mnt LevelPriority

DN16-Jun-1994

TASM-OEUROPE

18602-OCT-1995

INST OF ELECTRICALLY HEATEDGLASS CENTER WINDSHIELD

1-520-237-50-70MWO:

Mnt LevelPriority

DN12-Apr-1999

TASM-OEUROPE

12402-OCT-1995

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

1-1520-237-50-66 C1MWO:

Mnt LevelPriority

DN28-Jun-1996

TASM-OEUROPE

43604-DEC-1995

INSTALLATION OF DUAL AN/ARC-186/ARC-201 (V) FM RADIO SYSTEMSAND HARDWIRING OF TSEC KY-58 (UH-60A HELICOPTERS) NATIONALSTOCK NUMBER (NSN) 1520-01-035-0266

1-1520-237-50-69 C1MWO:

Mnt LevelPriority

DN15-Nov-1990

TASM-OEUROPE

507-MAY-1990

INCORPORATION OF IMPROVEDTIEDOWN FITTINGS

1-1520-237-50-52MWO:

Mnt LevelPriority

DN17-Jan-1989

TASM-OEUROPE

209-JUN-1989

MOD OF BEARING RETAINER SPRINGCLIP T/R SERVO

55-1520-237-50-52REAPPLIED

MWO:

Mnt LevelPriority

DN15-Apr-1990

TASM-OEUROPE

3009-JUN-1989

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

55-1520-237-50-44 C3MWO:

Mnt LevelPriority

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

DA FORM 2408-5 E, OCT 91 EQUIPMENT MODIFICATION RECORD

PIDMWODATE HRS






DM15-Nov-1989

TASM-OEUROPE

2209-MAY-1990

MODIFICATION OF DOWEL PINRETENTION MAIN GEARBOX

1-1520-237-50-43MWO:

Mnt LevelPriority

DN04-Mar-1999

TASM-OEUROPE

3509-SEP-1998

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

1-1520-237-50-74 C1MWO:

Mnt LevelPriority

DN01-Sep-1986

TASM-OEUROPE

105412-DEC-1986

INCORP OF ANVIS COMP LIGHTINGSYSTEM

55-1520-237-50-20 CHG 5MWO:

Mnt LevelPriority

DN22-Jun-1999

TASM-OEUROPE

313-AUG-1999

IMPROVED INERTIA REEL1-1520-23-75-79MWO:Mnt LevelPriority

DN01-Oct-1991

TASM-OEUROPE

413-JUL-1990

INCORPORATION OF STABILATORACTUATOR GROUNDING STRAP FORUH-60A/EH-60A HELICOPTERS

1-1520-237-50-54MWO:

Mnt LevelPriority

DR01-Nov-2006

D CO 1-214THAVN

1013-Oct-2009

V, ZMODIFICATION FOR THE DAULINSTALLATION OF ATTITUDEHEADING REFERENCE UNITS (AHRU)

1-1520-237-50-94MWO:

Mnt LevelPriority

DR04-Jan-1986

TASM-OEUROPE

4015-APR-1986

MODIFICATION OF DIRECTIONALCONTROL CABLE ASSEMBLY (UH-60A& EH-60A HELICOPTERS) NATIONALSTOCK NUMBER (NSN) 1520-01-035-0266 & 1520-01-082-0686

55-1520-237-50-34 C1MWO:

Mnt LevelPriority

DN15-Aug-1988

TASM-OEUROPE

6715-DEC-1987

INCORPORATION OF WIRE STRIKEPROTECTION SYSTEM (WSPS) (UH-60A HELICOPTER)

55-1520-237-50-24 C4MWO:

Mnt LevelPriority

DR25-Apr-2006

TASM-OEUROPE

10015-SEP-2008

INSTALLATION OF CRASHWORTHYEXTERNAL FUEL SYSTEM , UH-60SERIES HELICOPTER (SUPERCEDESMWO DTD 14 DEC 2006)

1-1520-237-50-86 DTD 25APR 2006

MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN14-Mar-1990

TASM-OEUROPE

83218-OCT-1992

INCORPORATION OFELECTROMAGNETIC ENVIROMENTPROTECTION

1-1520-237-50-59 CHGS 2MWO:

Mnt LevelPriority

DN15-Aug-1990

TASM-OEUROPE

2420-APR-1990

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

55-1520-237-50-49 C1MWO:

Mnt LevelPriority

DR28-Jun-2002

TASM-OEUROPE

8021-MAY-2002

INSTALLATION OF SEALED LEAD ACIDBATTERY (SLAB) SYSTEM ANDRELOCATION OF UTILITY LIGHTPOWER (UH-60A/L HELICOPTERS) UH-60A NSN 1520-01-035-0266, UH-60LNSN 1520-01-298-4532

1-1520-237-50-77 C1MWO:

Mnt LevelPriority

DR26-Oct-2001

TASM-OEUROPE

30021-MAY-2002

INSTALLATION OF HFCOMMUNICATION SYSTEM AN/ARC-220(V) AND TSEC/KY-100 IN UH-60A/LHELICOPTER NSN 1520-01-035-0266,UH-60A NSN 1520-01-298-4532 UH-60L

1-1520-237-50-76 C1MWO:

Mnt LevelPriority

FN13-Jun-2013

TASM-OEUROPE

521-NOV-2013

INSTRUCTIONS FOR THE REMOVALOF THE #1 (CO-PILOTS) AHRU ANDINSTALLATION OF NAV SYS : CN-1313(VG), TRU-2A/A (RG)

1-1520-237-20-2MWO:

Mnt LevelPriority

DN31-Aug-1992

TASM-OEUROPE

122-APR-1993

IMPROVED CARGO HOOK KEEPERINSTALLATION FOR UH-60AHELICOPTERS

1-1520-237-50-15MWO:

Mnt LevelPriority

DN01-Oct-1990

TASM-OEUROPE

1223-APR-1990

INCORPORATION OF ENGINEQUADRANT SECONDARY STOP TONO. 1 AND NO. 2 ENGINE POWERCONTROL LEVERS (UH-60AHELICOPTERS)

55-1520-237-50-39 C1MWO:

Mnt LevelPriority



PIDMWODATE HRS






FR26-Feb-2008

TASM-OEUROPE

923-DEC-2009

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)

MWO 1-1520-237-20-94MWO:

Mnt LevelPriority

DU01-Apr-1988

TASM-OEUROPE

423-MAR-1987

MODIFICATION OF MAIN ROTORBLADE DE-ICE DISRUPTOR HARNESSAND TAIL ROTOR SLIP RINGHARNESS (UH-60A HELICOPTERS)

55-1520-237-50-36 C1MWO:

Mnt LevelPriority

DU30-Sep-1987

TASM-OEUROPE

623-NOV-1987

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

55-1520-237-50-46 C1MWO:

Mnt LevelPriority

DN15-Aug-1988

TASM-OEUROPE

6724-MAR-1988

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

55-1520-237-50-47 C1MWO:

Mnt LevelPriority

DR06-Sep-2002

TASM-OEUROPE

8026-MAY-2000

MODIFICATION OF THE UH/EH/HH-60HELICOPTER AUXILIARY FUELMANAGEMENT SYSTEM EXTERNALSTORES SUPPORT SYSTEM(INDICATOR KIT NSN 1615-01-451-8200) AND EXTENDED RANGE FUELSYSTEM (PROBE KIT NSN 1615-01-451-8207)

1-1520-237-50-78 C1MWO:

Mnt LevelPriority

DN29-Nov-1999

TASM-OEUROPE

5226-MAY-2000

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

1-1520-237-50-56 C2MWO:

Mnt LevelPriority

DR31-Mar-1997

TASM-OEUROPE

17826-MAY-2000

AN/ASN-128B DOPPLER/GPSNAVIGATION SYSTEM IN UH-60A/LHELICOPTER

1-1520-237-50-75 C1MWO:

Mnt LevelPriority

DN14-Jun-1991

TASM-OEUROPE

630-NOV-1992

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

1-1520-237-50-61 C1MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN30-Apr-1991

TASM-OEUROPE

230-NOV-1992

INSTALLATION OF IMPROVED ENGINECOWLING RELEASE HANDLE ASSY.

55-1520-237-50-64MWO:

Mnt LevelPriority

OU31-Oct-2002

TASM-OEUROPE

230-OCT-2002

UH-60 SERIES AIRCRAFT INSPECTAN/ARC-220 WIRING FOR CHAFING

1-1520-237-20-261MWO:

Mnt LevelPriority

DN28-Oct-1996

TASM-OEUROPE

631-JUL-1998

MODIFICATION OF CHIP DETECTORWIRING FOR UH-60A HELICOPTERS

1-1520-237-50-26MWO:

Mnt LevelPriority

DU15-Jun-1995

TASM-OEUROPE

2431-OCT-1995

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

1-1520-237-50-73 C1MWO:

Mnt LevelPriority



NUMBERLOCATIONPIDENTRYORGANIZATION

8.7.DATE

6.REMARKS

4. 5.

UH-60A 8323869HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL


SIKORSKYAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH S/A DWG. 70400-00003REV. D. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD. A. LATERAL SERVOINPUT ROD P/N 70400-02258-046 HAS BEENSHORTENED 1/8 TURN. B.AFT CONTROLSERVO INPUT ROD P/N 70400-02258-043 HASBEEN LENGTHEDN 1/2 TURN. C. FORWARDCONTROL SERVO INPUT ROD P/N 70400-02258-047 HAS BEEN SHORTENED 1/2 TURN.(UK0000)

21-Nov-1983 1

HARTFORD CONN.

QC000000

SIKORSKYUH-60A-82-16 (TB 55-1520-237-20-34) ONE TIMEINSP. OF FLIGHT CONTROLS MIXER LIMITERCOMPLIED WITH. (UK0000)

10-Dec-1983 1

HARTFORD CONN.

QC000000

SIKORSKYUH-60A-83-04 (TB 55-1520-237-30-01) ONE TIMEINSP. FOR UH-60A INLET DUCT ASSY.P/N70302-10100 & ALIGMENT PIN BRKT. P/N 70203-04301-044 & 045 COMPLIED. (UK0000)

12-Dec-1983 1

HARTFORD CONN.

QC000000

SIKORSKYECP-0178R1 HAS BEEN INCORPORTED IN THISAIRCRAFT. PURSUANT TO MOD. P-0072. THECONTRACTOR HAS INSTALLED ECP-0252WITH THE EXCEPTION OF THE DAMPENINGTO THE NEW AIRSPEED INDICATING WILLSYSTEM AS DESCIRED ON MWO'S 21519 &21541 ATTACHED TO THE AIRCRAFTLOGBOOK. THE CONTRACTOR WILLPROMPTLY RETROFIT THE NEW RESTRICTORTO COMPLY WITH THE ECP REQUIREMENT ATNO DIRECT COST TO THE GOV. (UK0000)

15-Dec-1983 1

HARTFORD CONN.

QC000000

201ST AVN COSOF TWX UH-60A-84-01 COMPLIED WITH201ST AVN. (UK0000)

26-Jan-1984 1

APO S.F. 96271

QC000000

201ST AVN COTB 55-1520-237-20-47 COMPLIED WITH 201STAVN CO APO S.F. 96271. #1 1120E #2 1336E(UK0000)

30-Jan-1984 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME INSP NO 1 & 2 JUNCTION BOXESI/A/W TB 55-1520-237-20-48 & UH-60A-84-02COMPLETED AT 55.O ACFT HRS (UK0000)

21-Mar-1984 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME INSP TAIL ROTOR PYLON COVERHINGE BRACKET DOES NOT APPLY TO THISACFT (UK0000)

18-Apr-1984 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME INSP & REPAIR OF STABILATORAMPLIER C/W BY SIKORSKY ACFT CO I/A/WUH-60-84-04 & TB 55-1520-237-50-2 AT 75.6ACFT HRS. (UK0000)

23-Apr-1984 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME INSP TIAL ROTOR GEARBOX ANDINTERMEDIATE GEARBOX I/A/W UH-60A-84-06COMPLETED AT 26 APR 84 @ 76.6 ACFT HRS.(UK0000)

26-Apr-1984 1

APO S.F. 96271

QC000000

201ST AVN COUH-60A-84-07 AND TB 55-1520-237-20-53 ENGOUTPUT SHAFT INSPECTION P/N 70361-08004-043 BOLTS P/N MS9724-08 AND P/NSS5086-04INSPECTION COMPLETED AT 79.0 21 MAY 84(UK0000)

21-May-1984 1

APO S.F. 96271

QC000000

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 E, OCT 91


8.7.DATE

6.REMARKS

4. 5.



201ST AVN COONE TIME INSP OF CARGO HOOK PRESSURECARTRIDGE I/A/W SOF UH-60A-84-08COMPLETED AT 79.9 ACFT HRS. (UK0000)

05-Jun-1984 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME INSP OF LONGITUDINAL/LATERALLINK ASSY I/A/W SOF MESSAGE UH-60A-84-11AND TB 55-1520-237-20-56 AT 88.6 ACFT HRS.(UK0000)

16-Jul-1984 1

APO S.F. 96271

QC000000

201ST AVN COOCM/ACE INSP PERFORMED ST 89.0 ACFTHRS AT CP HUMPHREYS KOREA BY ACETEAM MEMBER D. GOSSETT AVSCOM OCMSEC. ST. LOUIS, MO. (UK0000)

02-Aug-1984 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME OF MAIN ROTOR SPINDLE ASSYI/A/W SOF MESSAGE UH-60A-84-12 AND TB 55-4520-237-20-55 AT 89.1 ACFT HRS. (UK0000)

02-Aug-1984 2

APO S.F. 96271

QC000000

201ST AVN COONE TIME OF TAIL CONE CANTED HINGEBULKHEAD RADIUS BLOCKS I/A/W SOFMESSAGE UH-60A-84-10 AND TB 55-1520-237-20-54 AT 91.2 ACFT HRS. (UK0000)

24-Aug-1984 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME OF TAIL CONTROL CABLEREQIURED BEFORE NEXT 10HR/14DAY I/A/WSOF MSG UH-60A-84-14 AND TB 55-1520-237-20-58. COMPLETED AT 381.7 ACFT HRS.(UK0000)

13-Dec-1984 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME OF TAIL CONTROL CABLETURNBUCKLE IDENFICATION REQUIRED I/A/WSOF MSG UH-60A-84-13. (UK0000)

10-Jan-1985 1

APO S.F. 96271

QC000000

201ST AVN COUH-60A-84-15 EXTENSION OF TIME TOREPLACE TAIL ROTOR BRASS TURNBUCKLES. (UK0000)

10-Jan-1985 2

APO S.F. 96271

QC000000

201ST AVN COREMOVEAL & REPLACEMENT OF GG ROTORAT CERTAIN LIFE LIMITS. ACFT IS BEINGMONITORD I/A/W SOF UH-60A-84-16 AS PERTB 55-2840-248-20-16. COMPLETED AT 118.3ACFT HRS. (UK0000)

14-Jan-1985 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME RECURRING INSPECTION OF M/G/BDOWEL PIN UH-60A AS PER SOF UH-60A 84-16ONE TIME INSP COMPLETED AT 118.3 ACFTHRS. (UK0000)

14-Jan-1985 2

APO S.F. 96271

QC000000

201ST AVN COONETIME INSP OF STABILATOR AMPLIFIERSFOR LOCKING POTENTIOMETERS I/A/W SOFMSG UH-60A-85-01 COMPLETED AT 151.9ACFT HRS (UK0000)

03-Feb-1985 1

APO SF 96271

QC000000

201ST AVN COONETIME INSP OF PRIMARY SERVOS ANDCONTROL RODS I/A/W SOF MSG UH60A-85-06COMPLETED AT 211.4 ACFT HRS (UK0000)

29-Mar-1985 1

APO SF 96271

QC000000

201ST AVN COIMMEDEDIATE GROUNDING AND INSPECTIONOF FLIGHT CONTROLS I/A/W SOF MSG UH-60A-85-07 COMPLETED AT 226.4 ACFT HRS(UK0000)

07-Apr-1985 1

APO SF 96271

QC000000

201ST AVN COIMMEDEDIATE GROUNDING AND INSPECTIONOF ALL MAJOR SYSTEMS REQUIRED I/A/WSOF MSG UH-60A-85-10 COMPLETED AT 226.4ACFT HRS (UK0000)

26-Apr-1985 1

APO SF 96271

QC000000



8.7.DATE

6.REMARKS

4. 5.



201ST AVN COONETIME INSP OF SPINDLE AND LINER SERILNUMBER CHECK I/A/W SOF MSG UH-60A-85-11COMPLETED AT 226.4 ACFT HRS (UK0000)

02-May-1985 1

APO SF 96271

QC000000

201ST AVN COONETIME INSP AND MODIFIED FLYABLESTORAGE PROCEDURES I/A/W SOF MSG UH-60A-85-13 COMPLETED AT 226.4 ACFT HRS(UK0000)

20-May-1985 1

APO SF 96271

QC000000

201ST AVN COONETIME RECORDS INSP OF M/R SHAFT I/A/WSOF MSG UH60A-85-14 COMPLETED AT 387.7ACFT HRS (UK0000)

04-Jun-1985 1

APO SF 96271

QC000000

201ST AVN COONETIME INSP OF RECORDS ON HUB M/RI/A/W SOF MSG UH60A-85-15 COMPLETED AT226.4 ACFT HRS (UK0000)

04-Jun-1985 2

APO SF 96271

QC000000

201ST AVN COENGINE OUTPUT SHAFT RECURRINGVIBRATION LIMITS I/A/W SOF MSG UH60A-85-17 L/H .50 IPS R/H .70 IPS COMPLETED AT226.4 ACFT HRS (UK0000)

11-Jun-1985 1

APO SF 96271

QC000000

AVSCOM OCM SEC, ST.LOUIS

OCM/ACE PERFORMED AT 226.4 ACFT HRS(UK0000)

02-Jul-1985 1

CP HUMPHREYS,KOREA

QC000000

201ST AVN COONETIME INSP AND MODIFICATIONPROCEDURES FOR UNGROUNDING THEUH60A I/A/W SOF MSG UH60A-85-18COMPLETED AT 226.4 ACFT HRS (UK0000)

09-Jul-1985 1

APO SF 96271

QC000000

201ST AVN COONETIME INSP OF T/R DRIVE SHAFT BEARINGI/A/W SOF MSG UH60A-85-23 COMPLETED AT269.3 ACFT HRS (UK0000)

24-Jul-1985 1

APO SF 96271

QC000000

201ST AVN COSUPPLEMENT TO INSP OF T/R DRIVESHAFTBEARINGS I/A/W SOF MSG UH-60A-85-24COMPLETED AT 269.3 ACFT HRS (UK0000)

02-Aug-1985 1

APO SF 96271

QC000000

201ST AVN COTORQUE STABILIZATION OF M/R PITCH HORNATTACHMENT BOLTS COMP. I/A/W SOF MSGUH-60A-85-25 + UH-60-85-26 COMPLETED AT360.1 ACFT HRS (UK0000)

02-Nov-1985 1

APO SF 96271

QC000000

201ST AVN COREPLACEMENT OF T/R DRIVE SHAFTBEARINGS PN - SB1138-101 I/A/W SOF MSG UH-60A-86-01 COMPLETED (UK0000)

24-Feb-1986 1

APO SF 96271

QC000000

201ST AVN COONETIME TORQUE OF T/R DRIVE SHAFT FLEXCOUPLINGS COMP I/A/W SOF MSG UH-60A-86-02 COMPLETED AT 410.5 ACFT HRS (UK0000)

24-Feb-1986 2

APO SF 96271

QC000000

201ST AVN COIMMEDIATE GROUNDINGING OF UH-60/EH-60SERIES AT 420.6 ACFT HRS (UK0000)

26-Mar-1986 1

APO SF 96271

QC000000

201ST AVN COREQUIREMENTS FOR UNGROUNDING I/A/WSOF UH-60A-86-07 COMPLETED AT 420.6 ACFTHRS (UK0000)

01-May-1986 1

APO SF 96271

QC000000

201ST AVN COREPLACEMENT OF STABLILATORACTUATORS PN - 70400-06641-108/109/110AND INSP OF 2408-16 I/A/W SOF UH-60A-86-08COMPLETED AT 420.6 ACFT HRS (UK0000)

12-May-1986 1

APO SF 96271

QC000000

201ST AVN COOCM/ACE PERFORMED AT 444 A/C HRS AT CPHUMPHREYS BY ACE TEAM AVSCOM SEC, ST.LOUIS (UK0000)

07-Jun-1986 1

APO SF 96271

QC000000



8.7.DATE

6.REMARKS

4. 5.



201ST AVN COSOF MSG UH-60A-86-10 ONETIME INSP OFMAIN CONTROL DEVICE BEARINGS STAKEC/W 14 JUNE 86 AT 427 ACFT HRS THIS SOFWAS NOT LOG BUT DA 2408-13 REFLECTSBEING COMPLY AT ABOVE DATE (UK0000)

14-Jun-1986 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60A-86-12 ONETIME INSP OFYAW AND COLLECTIVE BOOST SERVOS BYSN C/W 6 AUG 86 AT ACFT HRS SOF WAS NOTLONG BEFORE 2408-13 REFLECTS C/W ONABOVE DATE (UK0000)

06-Aug-1986 1

APO SF 96271

QC000000

201ST AVN COREPL OF AN 310-8 NUTS NSN 5310-00-157-1289COMPLETED AT 449 ACFT HRS I/A/W SOF MSGUH-60-86-13 13 AUG 86 (UK0000)

13-Aug-1986 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60A-86-16 REVISION OF SOF UH-60A-86-10 C/W ON 14 JUNE 86 AT 427 ACFTHRS (UK0000)

21-Oct-1986 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60A-86-17 INSP OF XMSN OILCOOLER FAN SPLINES N/A TO THIS ACFT BYSN (UK0000)

31-Oct-1986 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60A-86-19 REINSPECTION OFTHE EYE BOLTS P/N 70209-02136-102 NOTINSTALLED THIS ACFT BY SN (UK0000)

02-Nov-1986 1

APO SF 96271

QC000000

45TH TRANS COINSP OF THE FIRST OF THREE TAIL ROTORDRIVE SHAFT SPLINE COUPLINGS ANDREMOVAL OF MATERIAL FROM UNDER CREWSEATS COMPLIED WITH I/A/W SOF MSG UH-60-86-20 (UK0000)

14-Nov-1986 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60A-86-20 ONETIME INSPECTIONOF THE FIRST 3 T/R CRIVE SHAFT SPLINESC/W 14 NOV 86 AT 493.1 ACFT HRS (UK0000)

14-Nov-1986 2

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60A-86-21 ONETIME INSP OFCREW SEATS FOR LONGITUDINALMOVEMENT OF LOCKPINS ADJUSTMENT C/W10 DEC 86 AT 493.1 ACFT HRS BY OLR(UK0000)

10-Dec-1986 1

APO SF 96271

QC000000

201ST AVN COPE#1 COMPLETED AT 495.9 ACFT HRS 6 FEB87 (UK0000)

06-Feb-1987 1

APO SF 96271

QC000000

201ST AVN COUH-60A-87-03 (TB 1-1520-237-20-89) ONETIMEAND RECURRING COUPLINGS COMPLETED 15MAR 87 AT 525.2 ACFT HRS (UK0000)

15-Mar-1987 1

APO SF 96271

QC000000

201ST AVN COUH-60A-87-04 ONETIME AND RECURRING INSPOF EYEBOLTS PN - 70209-02136-102COMPLETED 27 MAR 87 AT 532.1 ACFT HRS(UK0000)

27-Mar-1987 1

APO SF 96271

QC000000

201ST AVN COSOF UH-60-87-07 ONETIME AND RECURRINGINSP OF LONGITUDINAL/LATERAL LINKS FORCRACKS C/W AT 583.3 HRS (UK0000)

18-May-1987 1

APO SF 96271

QC000000

201ST AVN COSOF UH-60-87-06 ONETIME AND RECURRINGINSP OF OIL COOLER SPLINES C/W BY DEPOTTEAM AT 583.0 ACFT HRS (UK0000)

20-May-1987 1

APO SF 96271

QC000000

201ST AVN COOCM/ACE PERFORMED AT 609 A/C HRS AT CPHUMPHREYS BY ACE TEAM. AVSCOM SEC ST.LOUIS, MO (UK0000)

16-Jun-1987 1

APO SF 96271

QC000000



8.7.DATE

6.REMARKS

4. 5.



201ST AVN COSOF (GEN-87-02) ONETIME INSPECTION OFACFT RECORDS FOR LOCAL PURCHASE OFTIME CHANGE AIRCRAFT COMPONENTS/PARTS C/W AT 615.8 ACFT HRS (UK0000)

06-Jul-1987 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH60A-87-08 ONETIME INSPECTIONOF MID SECTION BELLCRANK ASSEMBILIESC/W AT 615.8 ACFT HRS BY 377TH MED K-16(UK0000)

06-Jul-1987 2

APO SF 96271

QC000000

201ST AVN COSOF UH-60-87-10 ONETIME INSP OF INPUTFLAGE ASSY C/W AT 681.0 ACFT HRS BY377TH MED K-16 (UK0000)

19-Oct-1987 1

APO SF 96271

QC000000

C 6/159 AVN.SOF UH-60A-89-01 C/W 10 FEB 89 AT 875.0ACFT HRS ONETIME INSP OF T-700 ENGINEG/G STATOR SHROUDS (UK0000)

10-Feb-1988 1

APO NY 09025

QC000000

201ST AVN COSOF UH-60-88-01 ONETIME INSP OF T/R BLADESERIAL # COMPLETED AT 732.2 ACFT HRS(UK0000)

19-Feb-1988 1

APO SF 96271

QC000000

201ST AVN COMWO 55-1520-237-20-86 INSTALLATION OFPBA FIXED LINK ASSY C/W AT 732.2 ACFTHRS (UK0000)

24-Feb-1988 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60A 88-02 ONETIME INSP OF T/RGEARBOX OUTPUT SHAFT C/W AT 741.4 ACFTHRS (UK0000)

29-Mar-1988 1

APO SF 96271

QC000000

201ST AVN COAIRCRAFT MAIN ROTOR HEAD RIGGEDLATERAL PRIMARY SERVO CONTROL RODSHORTENED 5/8 TURN (UK0000)

05-Apr-1988 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60A-88-03 ONETIME INSP OFMAIN MODULE CHAPT SERIAL NUMBERS C/WAT 783.0 ACFT HRS (UK0000)

13-May-1988 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60-88-05 ONETIME ANDRECURRING CALCULATION OF APUOPERATING HOURS AND STARTS C/W AT800.9 ACFT HRS (UK0000)

16-Jun-1988 1

APO SF 96271

QC000000

201ST AVN COOCM/ACE PERFORMED AT 812 A/C HRS AT CPHUMPHREYS BY ACE TEAM AVSCOMOCMSEC, ST.LOUIS, MO (UK0000)

29-Jun-1988 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60-88-07 C/W AT 823.2 ACFT HRSREVISION TO SOF MSG UH-60-88-05CONCERNING OPERATING TIME/STARTCALCULATIONS AND FORMS INFO (UK0000)

15-Jul-1988 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60-88-06 C/W AT 828.0 ACFT HRSASSIGN A TBO OF 2000 HOURS TO THE OILCOOLER BLOWER FOR BEARINGREPLACEMENT (UK0000)

19-Jul-1988 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60-88-09 C/W AT 831.2 ACFT HRSONETIME INSPECTION OF ARAMANUFACTURED CREW SEATS FOR LOOSECLEVIS SCREWS (UK0000)

11-Aug-1988 1

APO SF 96271

QC000000

201ST AVN COGEN-XSOF-88-02 C/W AT 843.0 ACFT HRSONETIME INSPECTION OF INSTALLATION OFCORRECT INTERNAL PORTABLE FIREEXTINGUISHERS (UK0000)

26-Sep-1988 1

APO SF 96271

QC000000



8.7.DATE

6.REMARKS

4. 5.



201ST AVN COSOF MSG UH-60-88-11 C/W AT 860.9 ACFT HRSREVISION TO SOF MSG UH-60-86-18IMMEDIATE RESTRICTION OF REPELLINGOPERATIONS (UK0000)

19-Oct-1988 1

APO SF 96271

QC000000

BCO 1/501ST AVN REGTSOF MSG UH-60-88-10 C/W AT 871.1 ACFT HRSONETIME INSPECTION OF THETROOP/GUNNERS SEAT SUPPORT (H-BAR)BRACKETS, RADIS BLOCKS, BOLTS,WASHERS AND NUTS (UK0000)

31-Oct-1988 1

APO SF 96271

QC000000

BCO 1/501ST AVN REGTSOF MSG UH-60-88-12 C/W AT 871.1 ACFT HRSREVISION TO SOF MSG UH-60-88-10 INSP OFTROOP/GUNNERS SEAT H-BAR ASSY(UK0000)

16-Nov-1988 1

APO SF 96271

QC000000

BCO 1/501ST AVN REGTSOF MSG UH-60-88-13 C/W AT 871.1 ACFT HRSONETIME INSP OF MAIN ROTOR BLADEEXPANDABLE RETENTION PINS PN -70103-08107-101 FOR MISSING SEGMENTS ANDCLEVIS (UK0000)

22-Nov-1988 1

APO SF 96271

QC000000

C 6/159 AVN.SOF UH-60A-88-14 TB 55-1500-237-20-103ONETIME INSP OF ALL UH-60A HIGHPERFORMANCE HOIST SYSTEMS NOTAPPLICABLE THIS MODEL, DESIGN ORSERIES AIRCRAFT (MDS) (UK0000)

26-Dec-1988 1

APO NY 09025

QC000000

C 6/159TH AVNSOF MSG UH-60-89-01 C/W 10 FEB 98 AT 875.0ACFT HR ONETIME INSPECTION OF T-700ENGINE G/G STATOR (UK0000)

10-Feb-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60A-89-02 C/W AT 875.0 AC HRSREVISION TO SOF UH-60A-89-01 (UK0000)

13-Feb-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60A-89-04 C/W 04 APR 89 AT 894.2ACFT HRS REVISION TO SOF UH-60A-89-03ONETIME INSP OF ALL M/R SPINDLES(UK0000)

04-Apr-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60A-89-05 C/W 15 JUN 89 AT 949.3ACFT HRS ONETIME INSP OF FWD WIRESTRIKE PROTECTION PITOT CUTTERINDLES(UK0000)

15-Jun-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60A-89-06 C/W 18 JUL 89 AT 954.6ACFT HRS ONETIME INSP OF L/H + R/H RELAYPANEL GROUND MODULES (UK0000)

19-Jul-1989 1

APO NY 09025

QC000000

C 6/159 AVN.OCM/ACE PERFORMED AT 0958 A/C HRS, ATSCHWABISCH HALL, GE BY ACE TEAMAVSCOM OCMSEC, ST. LOUIS, MO (UK0000)

28-Jul-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF MSG UH-60A-89-07 C/W 9 AUG 89CORRECTION TO SOF UH-60A-89-06 (UK0000)

09-Aug-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF MSG UH-60A-89-08 C/W 16 AUG 89 AT964.7 AC HRS ONETIME OPERATIONAL INSPOF THE FUEL BOOST PUMP HOSEINSTALLATION FOR CONNECTION TOSUMERGED BOOST PUMP (UK0000)

16-Aug-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF MSG UH-60A-89-09 C/W 16 AUG 89 AT964.7 AC HRS CORRECTION OF RETIREMENTLIFE SCHEDULE FOR H-60 RETIREMENT LIFECOMPONENTS (UK0000)

16-Aug-1989 2

APO NY 09025

QC000000



8.7.DATE

6.REMARKS

4. 5.



C 6/159 AVN.SOF MSG UH-60A-89-10 C/W AT 973.8 AC HRSONETIME INSP OF T-700 ENG G/G ROTORSAND STATOR (UK0000)

20-Sep-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60A-89-11 C/W 09 NOV 89 AT 991.8ACFT HRS (UK0000)

09-Nov-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60A-89-12 C/W 28 NOV 89 AT 993.7ACFT HRS ONETIME INSPECTION OF OILCOOLER AXIAL FAN BY NEXT 10HR/14DAYINSPECTION (UK0000)

28-Nov-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60A-89-13 C/W 11 DEC 89 AT 994.8ACFT HRS (UK0000)

11-Dec-1989 1

APO NY 09025

QC000000

C 6/159 AVN.PMS 2 COMPLETED 994.6 ACFT HRS (UK0000) 22-Mar-1990 1

APO NY 09025

QC000000

C 6/159 AVN.TB 55-1520-237-20-104 DATED 30 SEP 89 NEWOVERHAUL/RETIREMENT LIFE SCHEDULEFOR H-60 RETIREMENT LIFE COMPONENTSCOMPLETED 23 MAR 90 (UK0000)

23-Mar-1990 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60-90-01 C/W 18 APR 90 AT 998.6 ACFTHRS ONETIME AND RECURRING INSP OF MAINROTOR BLADE EXPANDABLE PINS (UK0000)

18-Apr-1990 1

APO NY 09025

QC000000

C 6/159 AVN.OCM/ACE PERFORMED AT 1012 AC HRS ATSCHWABISCHHALL GERMANY BY ACE TEAMAVSCOM OCMSEC, ST. LOUIS, MO (UK0000)

15-Aug-1990 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60-90-02 C/W 22 AUG 90 AT 1012.4ACFT HRS ONETIME + RECURRING INSP OFT/R PITCH BEAM RETAINING WASHER(UK0000)

17-Aug-1990 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60-90-02 C/W 22 AUG 90 AT 1012.4ACFT HRS ONETIME INSP OF UPPERPRESSURE PLATE AND SPINDLE TO HUBATTACHMENT BOLTS I/A/W TB 55-1520-237-20-111 (UK0000)

22-Aug-1990 1

APO NY 09025

QC000000

DYNCORPTB 1-1500-237-20-28 BLADE EROSIONPROTECTION C/W BY DYNCORP (UK0000)

16-Dec-1990 1

APO NY 09616

QC000000

C CO 6/159TH AVNPROVISION FOR 12 STATION ICS INSTALLED16 JAN 91 AT 1111.5 ACFT HRS DESERTSTORM (UK0000)

18-Jan-1991 1

APO NY 09684

QC000000

C CO 6/159TH AVNUH-60-91-ASAM-05 C/W 28 FEB 91 AT 1160.0ACFT HRS INSPECTION FOR 4UNSERVICEABLE SPINDLE ASSEMBLIES(UK0000)

28-Feb-1991 1

APO NY 09025

QC000000

C CO 6/159TH AVNTB 55-1520-237-20-119 C/W 3 MAR 91 AT 1162.0AC HR ONETIME REPLACEMENT AND 30HRSPECAIL INSPECTION OF TAIL ROTOR PITCHBEAM RETAINING WASHER (UK0000)

03-Mar-1991 1

APO NY 09025

QC000000

C CO 6/159TH AVNTB 55-1520-237-20-121 C/W 6 MAY 91 AT 1275.2AC HR INTALLATION OF GROUNDPOSITIONING SYSTEM (UK0000)

06-May-1991 1

APO NY 09025

QC000000

AVSCOM SECOCM/ACE PERFORMED AT 1324 AC HRS BYACE TEAM (UK0000)

21-Aug-1991 1

NELLIGEN, GERMANY

QC000000



8.7.DATE

6.REMARKS

4. 5.



CCO 6/159 AVNUH-60A-91-ASAM-10 C/W AT 1334 ACFT HRS 70CT 91 ONETIME INSP + REPLACEMENT OFBRAKE ASSY. PISTON INSULATORS (UK0000)

07-Oct-1991 1

APO NY 09025

QC000000

CCO 6/159 AVNUH-60A-91-ASAM-02 C/W AT 1113.5RECURRING EROSION INSP OF MAIN ROTORBLADE TIP CAP IN DESERT OPERATION(UK0000)

16-Jan-1992 1

APO NY 09025

QC000000

CCO 6/159 AVNUH-60A-91-ASAM-03 C/W AT 1113.5 EXTENDEDTBO HOURS UNDER DESERT SHIELDOPERATIONS FOR UH-60A/L OIL COOLERBLOWER + TAIL ROTOR PITCH CHANGESHAFT BEARINGS (UK0000)

16-Jan-1992 2

APO NY 09025

QC000000

CCO 6/159 AVNUH-60A-92-ASAM-01 C/W AT 1352.6 AC HRS 17JAN 92 INSP FOR 3 UNSERVICEABLE SPINDLEASSEMBLIES (UK0000)

17-Jan-1992 1

APO NY 09025

QC000000

CCO 6/159 AVNTHIS ACFT OPERATED IN SWA (DESERTSHIELD/DESERT STORM) FROM 15 DEC 90 TO25 MAY 91 (UK0000)

17-Jan-1992 2

APO NY 09025

QC000000

CCO 6/159 AVNUH-60A-91-ASAM-04 C/W AT 1190.4 ACFT HRSH-60 AIRCRAFT OPERATION IN SWA (DESERTSTORM) TO PROVIDE GUIDANCE FORSITUATIONS REQUIRING EXCEEDING THERETIREMENT (FINITE) LIFE OF CERTAINCOMPONENTS (UK0000)

20-Mar-1992 1

APO NY 09025

QC000000

CCO 6/159 AVNUH-60A-91-ASAM-06 C/W AT 1308.7 ACFT HRSONETIME INSP OF CARGO HOOK INTERNALROUTE OF WIRE BUNDLE COMPLETED(UK0000)

19-Jul-1992 1

APO NY 09025

QC000000

CCO 6/159 AVNUH-60A-91-ASAM-08 C/W AT 1308.7 ACFT HRSONETIME INSP OF FIRE EXTINGUISHINGSYSTEMS (UK0000)

19-Jul-1992 2

APO NY 09025

QC000000

CCO 6/159 AVNOCM/ACE PERFORMED AT 1445 A/C HRS ATHEIDELBERG,GE BY ACE TEAM AVSCOM. ST.LOUIS, MO. (UK0000)

05-Aug-1992 1

APO NY 09025

QC000000

DYNCORPUH-60-92-ASAM-05 C/W AT 1493 ACFT HRSINSPECTION AND REPLACEMENT OF MAINROTOR BLADE EXPANDABLE PINS PN - 70103-08107-101 (UK0000)

23-Mar-1993 1

APO NY 09274

QC000000

DYNCORPUH-60-92-ASAM-06 C/W AT 1493 ACFT HRSONETIME INSPECTION FOR PROPERHARDWARE ON PEDAL ADJUSTERASSEMBLY PN - 70400-01613 (UK0000)

23-Mar-1993 2

APO NY 09274

QC000000

DYNCORPUH-60-93-ASAM-01 C/W AT 1493 ACFT HRSONETIME OPERATION CHECK OF ALL CHIPDETECTORS (UK0000)

23-Mar-1993 3

APO NY 09274

QC000000

DYNCORPUH-60-93-ASAM-03 C/W AT 1493 ACFT HRSREVISIION OF UH-60-92-ASAM-05 INSP ANDREPLACEMENT OF -101 BLADE PINS (UK0000)

23-Mar-1993 4

APO NY 09274

QC000000

DYNCORPUH-60-93-ASAM-04 C/W AT 1493 ACFT HRSREVISIION OF UH-60-92-ASAM-06 ONETIMEINSP FOR PROPER HDWR ON PEDALADJUSTER PN - 70400-01613 (UK0000)

23-Mar-1993 5

APO NY 09274

QC000000



8.7.DATE

6.REMARKS

4. 5.



DYNCORPUH-60-93-ASAM-06 C/W AT 1493 ACFT HRSONETIME INSP TO REMOVE SUSPECT PITCHBEAM ON TAIL ROTOR SYSTEM (UK0000)

23-Mar-1993 6

APO NY 09274

QC000000

DYNCORPUH-60-93-ASAM-08 C/W AT 1493 ACFT HRSALL H-60 SERIES ACFT PRIOR TO 91-26354CHANGE TO 30 BIAS TAIL ROTOR RIG(UK0000)

23-Mar-1993 7

APO NY 09274

QC000000

DYNCORPPMS-II COMPLETED AT 1492.5 ACFT HRS NEXTDUE AT 1992.5 ACFT HRS (UK0000)

23-Mar-1993 8

APO NY 09274

QC000000

DYNCORPTB 1-1520-237-30-2(STIR) CLEANING ANDINSPECTION REQUIREMENTS C/W AT 1492.5ACFT HRS (UK0000)

23-Mar-1993 9

APO NY 09274

QC000000

BCO 70TH TRANS BNUH-60-93-ASAM-09 ONE TIME MWO CHECKC/W @ 1499.3 ACFT HRS (UK0000)

05-Apr-1993 1

APO AE 09028

QC000000

BCO 70TH TRANS BNUH-60-92-ASAM-01 M/R SPINDLE SERIAL #CHECK C/W @ 1499.3 ACFT HRS (UK0000)

05-Apr-1993 2

APO AE 09028

QC000000

BCO 70TH TRANS BNUH-60-93-ASAM-10 RECURRING INSPECTIONOF ESSS SYSTEM N/A THIS ACFT C/W @1499.3 ACFT HRS (UK0000)

05-Apr-1993 3

APO AE 09028

QC000000

SHAPEUH-60-93-ASAM-11 C/W AT 1503.6 ACFT HRS14 APR 93 INSPECTION & REPLACEMENT OFARA CREW RESTRIANT BUCKLE/CROTCHASSY (UK0000)

14-Apr-1993 1

APO AE 09705

QC000000

SHAPEUH-60-93-ASAM-12 C/W AT 1504.6 ACFT HRSONETIME BRIEFING OF PILOTS,MAINTENANCE OFFICERS, TI'S FOR POSSIBLEACFT VIBE DUE TO SPINDLES (UK0000)

04-May-1993 1

APO AE 09705

QC000000

SHAPEUH-60-93-ASAM-13 C/W AT 1510.1 ACFT HRSOPERATIONAL GL OF ALL H-60 ACFT WITHESSS OR ERFS MISSION KITS INSTALLED N/ATHIS ACFT (UK0000)

07-Jun-1993 1

APO AE 09705

QC000000

SHAPEUH-60-93-ASAM-14 C/W AT 1510.1 ACFT HRSINSP OF ERFS EJECTOR RACKS N/A THISACFT (UK0000)

21-Jun-1993 1

APO AE 09705

QC000000

SHAPEUH-60-93-ASAM-15 C/W AT 1510.1 ACFT HRSCONTINUATION OF ERFS INSP N/A THIS ACFT(UK0000)

22-Jun-1993 1

APO AE 09705

QC000000

SHAPEOCM/ACE PERFORMED AT 1516 AC HRS ATCHIEVRES, BE BY ACE TEAM AVSCOMOCMSEC ST. LOUIS, MO (UK0000)

08-Jul-1993 1

APO AE 09705

QC000000

207TH AVN COUH-60-93-ASAM-16 C/W AT 1519.9 ACFT HRSALL H-60 ACFT ONETIME INSP HYD PUMPKNURLED KNOB PIN (UK0000)

02-Aug-1993 1

APO AE 09102

QC000000

DYN CORPMWO VERIFICATION COMPLETED @ 1225.7ACFT HRS (UK0000)

27-Aug-1993 1

APO AE 09266

QC000000

207TH AVN COENTRY FOR COMPLIANCE OF UH-60-92-ASAM-05 INCORRECT 101 BLADE PINS AREINSTALLED ON ACFT ASAM-05 CAN ONLY BEC/W WHEN 102 PINS ARE INSTALLED (UK0000)

23-Nov-1993 1

APO AE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.



207TH AVN COLATE ENTRY - M/R BLADE EROSIONPROTECTION REMOVED BY DYN CORP OLRDATE AND TIME UNKNOWN (UK0000)

23-Nov-1993 2

APO AE 09102

QC000000

207TH AVN COTB 1-1520-237-20-147 INSTALLATION OF GPSCOMPLETED AT 1599.7 ACFT HRS ANDSUCCESSFUL EMC TEST & DAILY INSP(UK0000)

17-Dec-1993 1

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-01 ALL H-60 ACFT NVGCOMPATIBILITY REWORK OF MASTERWARNING PANEL ASSY (UK0000)

07-Jan-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-03 C/W 1605.2 ACFT HRS ALLH-60 ARMY ACFT ONETIME REFURBISHMENTOF MAIN ROTOR SPINDLE AND REPL OFCERTAIN MAIN ROTOR THRUST BEARING(UK0000)

19-Jan-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-04 C/W 1620.0 ACFT HRS ALLH-60 ARMY ACFT REISSUE OF ONETIME INSPTO REMOVE SUSPECT T/R PITCH BEAMS(UK0000)

14-Feb-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-05 C/W 1620.0 ACFT HRS ALLH-60 BLACKHAWK HELICOPTERS, ONETIMEREMOVAL OF T/R G/B WITH TAIL G/B OUTPUTSHAFT PN - 70358-06620-101 FOR REWORK(UK0000)

14-Feb-1994 2

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-06 C/W 1620.0 ACFT HRSCOCKPIT STANDARDIZATION OF PILOT ANDCOPILOT'S RESTRAINT RELEASE SYSTEM INALL H-60 AIRCRAFT (UK0000)

14-Feb-1994 3

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-07 C/W 1620.0 ACFT HRS ALLH-60 ACFT REVISION TO OVERHAUL ANDRETIRMENT TABLE FOR CERTAINCOMPONENTS DUE N/L/T 9 APR 94 (UK0000)

15-Mar-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-08 C/W 1644.2 AC HRS 15 MAR94 REVISION TO UH-60-94-ASAM-07RECALCULATE NEW OVERHAUL/RETIREMENTLIVES FOR CERTAIN COMPONENTS N/L/T 24MAR 94 @ 1654.2 (UK0000)

15-Mar-1994 2

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-09 C/W 1665.5 AC HRS ALL H-60 AIRCRAFT INSP OF SERIAL NUMBERS FORREMOVAL OF CERTAIN PRIMARY SERVOASSEMBLIES (UK0000)

07-Apr-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-10 ARMY AIRCRAFT THIS IS AREVISION TO (UH-60-94-ASAM-03) ONETIMETIME REFURBISHMENT OF M/R SPINDLE ANDREPLACEMENT OF CERTAIN MAIN ROTORTHRUST BEARINGS (UK0000)

19-Apr-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-11 MAIN ROTOR BLADE DE-ICE HEATER MAT RESISTANCEMEASUREMENT TEST METHOD UH-60A ANDEH-60 SERIES AIRCRAFT (UK0000)

19-Apr-1994 2

APO AE 09102

QC000000

207TH AVN COOCM/ACE PERFORMED AT 1691 AC HRS OCMSECTION AT HEIDELBERG, GE BY ACE TEAMST. LOUIS (UK0000)

24-May-1994 1

APO AE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.



207TH AVN COTB 1-1520-237-20-143 ABRUPT CHANGES INM/R TRACK/VIBRATIONS ON H-60 ACFTINFORMATION FOR AIRCREWS REVISION TOTB 1-1520-237-20-143 DTD 15 MAY 93 (UK0000)

06-Sep-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-95-ASAM-01 GUIDENCE FOR HOISTINGAND AERIAL RECOVERY OF H-60 AND EH-60ESSS FIXED PROVISIONED ACFT UNTILPUBLISHED CHANGES ARE MADE C/W AT1782.7 ACFT HRS (UK0000)

17-Oct-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-95-ASAM-02 C/W AT 1799.7 ACFT HRSREQUIREMENT TO OPERATE THE FUEL TANKSUBMERGED BOOST PUMPS ON ALL TIMESWITH ALL FUELS DURING GROUND ANDFLIGHT OPERATIONS CHANGES TO ACFT -10AND CHECKLIST (UK0000)

25-Oct-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-95-ASAM-03 ALL H-60 SERIES ACFTSHALL REQUIRE RE-SHIMMING OF THE T/RBLADE PIVOT BEARINGS OF CERTAIN -043BLADE DUE N/L/T 1952.9 ACFT HRS (UK0000)

31-Oct-1994 1

APO AE 09102

QC000000

207TH AVN COASAM C/W @ 1811.5 ACFT HRS, 18 NOV 94 ALLH-60 ACFT REDUCTION OF TORQUE OFSELFRETAINING PIVOT BOLTS AS PER UH-60-95-ASAM-04 DUE N/L/T 22 DEC 94 OR 1831.5ACFT HRS (UK0000)

07-Dec-1994 1

APO AE 09102

QC000000

207TH AVN COTCTO 1H-60-696, ONETIME INSP OF CLAMPINGPROCEDURES OF PILOTS ICS CORD C/W 10DEC 94 (UK0000)

10-Dec-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-95-SOF-01 ONETIME RECORDS INSP OFTHE T/R G/B C/W 13 DEC 94 @ 1827.0 HRS T/RG/B ULTRASONIC INSP DUE N/L/T 31 MAR 95T/R G/B DUE REPLACEMENT N/L/T 31 DEC 95(UK0000)

13-Dec-1994 1

APO AE 09102

QC000000

BCO 70TH TRANS BNTAIL GEARBOX REPLACEMENT I/A/W UH-60-95-SOF-01 C/W @ 1832.8 ACFT HRS (UK0000)

18-Jan-1995 1

APO AE 09028

QC000000

207TH AVN COUH-60-95-SOF-02 C/W 15 FEB 95 @ 1850.0ACFT HRS CHANGE TO RETIREMENT LIFEFOR CERTAIN M/R BLADE CUFFS (UK0000)

15-Feb-1995 1

APO AE 09102

QC000000

207TH AVN COUH-60-95-ASAM-02 C/W 01 FEB 95 @ 1838.0ACFT HRS CHANGE TO RETIREMENT LIFEFOR SERVO BEAM RAILS (UK0000)

15-Feb-1995 2

APO AE 09102

QC000000

207TH AVN COTB 1-1520-237-20-153 C/W @ 1908.6 ACFT HRSREISSUE OF ONETIME INSP OF T/R PITCHCHANGE SHAFTS (UK0000)

18-May-1995 1

APO AE 09102

QC000000

207TH AVN COUH-60-95-ASAM-06 (TB 1-1520-237-237-20-168)ONETIME INSP FOR CRACKED MAIN XMSNBEAMS UPPER DECK SKIN AND FRAME ANDIMPLEMENTATION OF 100 HR RECURRINGINSP C/W @ 1950.7 ACFT HRS 6 JUL 95(UK0000)

06-Jul-1995 1

APO AE 09102

QC000000

207TH AVN COUH-60-95-ASAM-07 ALL H-60 ACFT TOPROVIDE REVISED CRITERIA FOR SHIMMINGOF TROOP/GUNNER SEATS C/W @ 1977.3ACFT HRS 28 JUL 95 (UK0000)

28-Jul-1995 1

APO AE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.



BCO 70TH TRANSUH-60-95-ASAM-03 RESHIMMING OF CERTAINTAIL ROTOR BLADE PIVOT BEARING C/W @1985.2 ACFT HRS (UK0000)

12-Sep-1995 1

APO AE 09028

QC000000

BCO 70TH TRANSACE/AACE PERFORMED AT 1985 A/C HRS(UK0000)

14-Sep-1995 1

APO AE 09028

QC000000

BCO 70TH TRANSPMS-2 #4 COMPLETED AT 1985.2 ACFT HOURSNEXT PHASE #5 DUE AT 2485.2 ACFT HOURS(UK0000)

30-Oct-1995 1

APO AE 09028

QC000000

BCO 70TH TRANSSOF UH-60-96-01 CHANGE IN RETIREMENTLIFE OF FWD BELLCRANK SPT ASSY. ASSY ISNOT INSTALLED ON ACFT C/W 1985.2 ACFTHRS (UK0000)

07-Nov-1995 1

APO AE 09028

QC000000

DYNCORP OLRSOF UH-60-96-02 ALL H-60 HELICOPTERONETIME INSP OF INBD RETENTION PLATESFOR SN C1324-001 - C1324-150 OR FM00001 -FM00142 N/A THIS A/C AT 1989.2 AC HRS(UK0000)

28-Nov-1995 1

APO AE 09028

QC000000

DYNCORP OLRSOF UH-60-96-03 ALL H-60 A/C CHG OFRETIREMENT LIFE OF M/R CUFF PN - 70150-09109-041 A/C SN'S CHK GOOD SOF C/W 1989A/C HRS (UK0000)

04-Dec-1995 1

APO AE 09028

QC000000

DYNCORP OLRSOF UH-60-96-04 REMOVAL OF SPECIFICSERIAL NUMBERED AFT BELLCRANKSUPPORT ASSEMBLIES C/W @ 1990.2 ACFTHRS (UK0000)

13-Dec-1995 1

APO AE 09028

QC000000

207TH AVN COUH-60-96-ASAM-04 ALL H-60 A/C WITH FASTROPE SYSTEM REDUCTION TO MAX LOAD.N/A THIS A/C C/W @ 2006.8 ACFT HRS(UK0000)

30-Jan-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-96-ASAM-03 REVISION TO ASAM-02,ONETIME INSP TO REMOVE SUSPECT M/RSHAFT NUT BOLTS C/W @ 1998.6 ACFT HRS 18JAN 96 (UK0000)

14-Feb-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-96-ASAM-05 INCREASE IN FATIGUELIFE FOR THE FORWARD SUPPORT ASSY N/ATHIS ACFT C/W @ 2131.4 ACFT HRS (UK0000)

16-Jul-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-96-ASAM-07 CHECK ACFT RECORDSFOR INSTALLED RETENTION RODS WITH PNFROM 33129-3 TO 33129-242 C/W @ 2158.3ACFT HRS (UK0000)

23-Aug-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-96-ASAM-08 INCREASE IN FATIGUELIFE OF T/R INBOARD RETENTION PLATE N/ATHIS ACFT C/W @ 2158.3 ACFT HRS (UK0000)

23-Aug-1996 2

APO AE 09102

QC000000

207TH AVN COUH-60-96-ASAM-09 ONETIME INSP OF STABACTUATTOR CLEVIS LOGGED ON DA FORM2408-18 AT 2174.5 ACFT HRS (UK0000)

13-Sep-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-96-ASAM-10 TB 1-1520-237-20-180ESTABLISH REPLACEMENT TIME FORSPINDLE ELASTOMERIC BEARING LINERCOMP AT 2174.5 ACFT HRS (UK0000)

13-Sep-1996 2

APO AE 09102

QC000000

207TH AVN COUH-60-96-ASAM-11 INCREASE IN FATIGUELIFE OF THE FENN MANUFACTURED M/RBLADE CUFFS. N/A THIS ACFT C/W @ 2179.3ACFT HRS (UK0000)

24-Sep-1996 1

APO AE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.



207TH AVN COOCM/ACE PERFORMED AT 2188 AC HRS ATHEIDELBERG, GE BY ACE TEAM (UK0000)

30-Sep-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-01 ONETIME INSP FORPROPER EDGE BREAKE ON M/R HUBCOMPLETED AT 2212.2 ACFT HRS (UK0000)

16-Oct-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-02 ONETIME INSP TAIL DRIVEFLEXIBLE COUPLING CONNECTIONSCOMPLETED AT 2219.0 ACFT HRS (UK0000)

29-Oct-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-03 ENGINE HISTORICALRECORDS CHECK FOR REPLACEMENT OFUNDAMPED GAS GENERATORROTOR/STATOR ASSY. COMPLETED AT 2224.0ACFT HRS (UK0000)

01-Nov-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-SOF-01 ONETIME INSPECTION OFM/R SWASHPLATE FOR CERTAIN SERIALNUMBER COMPLETED AT 2248.7 ACFT HRS(UK0000)

03-Dec-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-05 ONETIME INSP OF VICOUSDAMPER SUPPORT ASSY COMPLETED AT2268.9 ACFT HRS (UK0000)

09-Jan-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-06 INSP LATERALBELLCRANK ASSY PN - 70400-08150-045COMPLETED AT 2268.9 ACFT HRS (UK0000)

13-Jan-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-08 INSP OF CONNECTINGLINK PN - 70400-08155-056 COMPLETED AT2271.4 ACFT HRS (UK0000)

15-Jan-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-07 INSP OF TAILROTORSERVO FOR SPECIFIC SERIAL NUMBERCOMPLETED AT 2271.4 ACFT HRS (UK0000)

15-Jan-1997 2

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-09 INSP OF MAIN ROTORSHAFT EXTENSIONS COMPLETED AT 2271.7ACFT HRS (UK0000)

27-Jan-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-10 CHANGE TO RETIREMENTLIFE TO MAIN SUPPORT BRIDGE SN - 01201 AITHRU 01686 AI COMPLETED AT 3031.1 ACFTHRS (UK0000)

14-Feb-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-11 CHANGE TO RETIREMENTLIFE FOR CERTAIN MAIN ROTOR BLADECUFFS COMPLETED AT 2298.9 ACFT HRS(UK0000)

06-Mar-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-13 ONETIME INSP OF M/RSPINDLE SPHERICAL ELASTOMERIC BEARINGFOR EXISTENCE OF INNER SLEEVECOMPLETED AT 2337.5 ACFT HRS (UK0000)

09-Jun-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-14 ONETIME INSP AFTBELLCRANK SUPPORT MANUFACTURED BYAMERICAN GENERAL (CAGE 1W160)COMPLETED AT 2376.2 ACFT HRS (UK0000)

22-Aug-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-15 INSP OF MAIN ROTOR P/CLINK ROD END FOR CERTAIN CAGECODE(40137) COMPLETED AT 2376.2 ACFTHRS (UK0000)

22-Aug-1997 2

APO AE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.



207TH AVN COUH-60-97-ASAM-16 INSP OF RECORD ANDCLEVIS CONNECTOR PN - 70400-08151-050COMPLETED AT 2378.2 ACFT HRS (UK0000)

27-Aug-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-17 INSP OF INTERNALRESCUE HOIST BRACKET N/A THIS ACFT ATTHIS TIME COMPLETED AT 2378.2 ACFT HRS(UK0000)

03-Sep-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-18 INSP FOR SPECIFICSUSPECT REWORKED MAIN ROTORSWASHPLATE ASSY. COMPLETED AT 2391.4ACFT HRS (UK0000)

25-Sep-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-19 ANVIS HUD POWERSUPPLY NOTE: MWO NOT INSTALLEDCOMPLETED AT 2393.1 ACFT HRS (UK0000)

03-Oct-1997 1

APO AE 09102

QC000000

207TH AVN COJACE INSPECTION COMPLETED AT 2396.0 A/CHRS AT HEIDELBERG, GER BY TEAMMEMBERS AMCOM OLR/MWO BRANCHHUNTSVILLE, AL (UK0000)

11-Oct-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-98-ASAM-01 CHANGE IN RETIREMENTLIFE OF CERTAIN M/R SHAFT EXTESIONS(UK0000)

17-Oct-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-98-ASAM-02 ONETIME INSPECTION OFPUSHROD MANUFACTURED BY VERSATILEMACHINE COMPLETED AT 2397.8 ACFT HRS(UK0000)

22-Oct-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-98-ASAM-03 INSPECTION OFSWASHPLATE LINK PN - 70400-08110-54COMPLETED AT 2397.8 ACFT HRS (UK0000)

08-Nov-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-98-ASAM-04 ONETIME INSP OFOVERHAULED SERVOS COMPLETED AT2447.2 ACFT HRS (UK0000)

18-Mar-1998 1

APO AE 09102

QC000000

207TH AVN COUH-60-98-ASAM-05 REPLACEMENT OFSPECIFIC CAGE CODE AFT SWASHPLATELINK COMPLETED AT 2482.8 ACFT HRS(UK0000)

17-Jun-1998 1

APO AE 09102

QC000000

207TH AVN COJACE INSPECTION COMPLETED AT 2482.8HOURS AT MANNHEIM, GERMANY (UK0000)

08-Jul-1998 1

APO AE 09102

QC000000

207TH AVN COPMS-2#5 COMPLETED AT 2482.8 ACFT HRSNEXT PMS-2#6 DUE AT 2982.8 ACFT HRS(UK0000)

26-Aug-1998 1

APO AE 09102

QC000000

2-502AVN REGTUH-60-98-ASAM-07 INSPECTION FOR SUSPECTL/H TIE ROD COMPLETED AT 2485.8 ACFT HRS(UK0000)

16-Sep-1998 1

APO AE 09028

QC000000

214TH AVN BNUH-60-99-ASAM 01 ONE TIME INSP RECORDSFOR ALL H-60 ACFT CERTAIN P/NSWASHPLATE LINKS MANUFACTURED BYTEK COMPLIED WITH AT 2537.7 ACFT HRS(JW0000)

05-Nov-1998 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-02 (TB 1-1520-248-20-22)ONETIME INSP OF EXTERNAL HOISTPROVISIONS; N/A THIS ACFT AT 2538.2 ACFTHRS (UK0000)

07-Nov-1998 1

APO AE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.



214TH AVN BNUH-60-99-ASAM-03 ONE TIME INSP ENGINERECORDS INSP COMPLIED AT 2540.0 ACFTHRS (JW0000)

10-Nov-1998 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-04 T700-GE-701/701C ENGINEODV RELATED FLAMEOUT N/A THISAIRFRAME (JW0000)

04-Dec-1998 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-05 ONE-TIME INSP OF M/RSPINDLE FOR EXISTENSE OF SLEEVEBEARING COMPLETED AT 2570.2 (UK0000)

15-Dec-1998 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-06 INSPECTION AND REVISEDRETIREMENT LIFE OF MAIN ROTOR PITCHHORNS COMPLETED AT 2520.2 ACFT HRS(UK0000)

16-Dec-1998 1

APO AE 09102

QC000000

214TH AVN BNTB11-1520-237-50 INSTALLATION OF 12 PTSTATION INTERCONNECTING SYSTEM (ICS)APPLIED BY DYN CORP . (JW0000)

12-Mar-1999 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-07 INSP OF M/R HUB (NDI)AND ENRTY ON DA FORM 2408-18 FOR 100HRRECURRING INSP COMPLETED AT 2570.2ACFT HRS (UK0000)

15-Mar-1999 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-08 ALL H-60 ACFT, REVISEDRETIREMENT LIFE OF BELLCRANCKSUPPORT ASSEMBLY PN 70400-08162-042/045/047 MADE BY AIR INDUSTRIES(CAGE8L513). COMPLETED AT 2732.0 ACFTHRS. (BB6264)

14-Jun-1999 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-10 INSP AND PREVENTIVEMAINTENCE ON NUMBER TWO CROSSFEEDBREAKAWAY FUEL VALVE COMPLETE AT2770.0 ACFT HRS (BB6264)

06-Aug-1999 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-09ONE TIME INSP OF M/RBLADE PINS. COMPLETED AT 2777.3 ACFTHRS (BB6264)

12-Aug-1999 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-11 ONE TIME INSP OF T700-GE-701C ENG COMPLETD AT 2777.3 ACFT HRS(BB6264)

16-Aug-1999 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-12 INSP INTERVAL CHANGEON HAMILTON STANDARD H.M.U COMPLETEDAT 2789.4 ACFT HRS (DS1566)

13-Sep-1999 1

APO AE 09102

QC000000

AMCOM-E-OLRHUNTSVILLE, AL

JACE INSP COMPLETED AT 2806 ACFT HRSAT HEIDELBERG GERMANY (UK0000)

08-Oct-1999 1

APO AE 09102

QC000000

E CO 214TH AVN BNUH-60-00-ASAM-01 (TB-1-1520-237-20-15) INSPINTERVAL CHAN OF M/R HUB (NDI) ENTEREDON DA FORM 2408-18 AT 2837.7 ACFTHRS.CFT HRS (SR0259)

12-Nov-1999 1

APO AE 09102

QC000000

214TH AVN BNUH-60-00-ASAM-O2 CYCLIC STICK WIREBUNDLE RELOCATION COMPLETED AT 2837.8(MF2309)

14-Dec-1999 1

APO AE 09102

QC000000

214TH AVN BNUH-60-00-ASAM-O3 ALL H-60 ACFTINSPECTION AND REMOVAL OF SUSPECTPRIMARY SERVO ASSEMBLIES COMPLETEDAT 2870.0 (MF2309)

04-Jan-2000 1

APO AE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.



ECO 214TH AVN BNUH-60-00-ASAM-O4 INSPECT TAIL LANDINGGEAR SHOCK STRUT FOR MISSING BEARINGRETENTION PINS COMPLETED AT 2921.2 ACFTHRS (MF2309)

25-Feb-2000 1

APO AE 09102

QC000000

ECO 214TH AVN BNACE/CPCE PERFORMED AT 2977.1 ACFT HRSAT MANNHEIM, GERMANY BY (MF2309)

12-May-2000 1

APO AE 09102

QC000000

E CO 214TH AVN BNUH-60-00-ASAM-05 INSPECTION OF FIREEXTINGUISHER WIRING COMPLIED WITH ATAVIM (SR0257)

18-May-2000 1

APO AE 09102

QC000000

2-502 AVN REGTUH-60-00-ASAM-06 REVISION TO UH-60-00-ASAM-05 INSP OF FIRE EXTINGUISHERWIRING C/W AT 2977.1 ACFT HRS 20-219COMPLETED AT 2977.1 ACFT HRS (BS9665)

28-Jun-2000 1

APO AE 09028

QC000000

2-502 AVN REGTSOF UH-60-00-01 TECHNICAL, INITIAL ANDRECURRING INSP OF M/R SPINDLE C/W AT2977.1 ACFT HRS (BS9665)

12-Jul-2000 1

APO AE 09028

QC000000

2-502 AVN REGTSOF UH-60-00-02 INSPECTION FOR INPUTMODULE REPAIR AND POTENTIALLYCRACKED BEVEL GEARS C/W AT 2977.1 ACFTHRS (TB6357)

03-Aug-2000 1

APO AE 09028

QC000000

2-502 AVN REGTPMS-2 #6 COMPLETED AT 2977.1 ACFT HRS,NEXT PMS-2 #7 DUE AT 3477.1 ACFT HRSS(TB6357)

14-Aug-2000 1

APO AE 09028

QC000000

E CO 214TH AVN BNUH-60-00-ASAM-07 INSPECT WIRING HARNESSCONNECTING NO 1 AND NO 2 JUNCTIONBOXES IAW UH-60-00-ASAM-07 (TB 1-1520-237-20-24). COMPLETED AT 2987.8 HRS. (CG9711)

05-Sep-2000 1

APO AE 09102

QC000000

1-214TH AVN BNUH-60-01-01 SOF INSPECT MAIN LANDINGGEAR DRAG BEAM ASSEMBLIES FORCRACKS NEAR JACK PAD ASSEMBLYCOMPLIED WITH AT 3044.2 ACFT HRS(CG9711)

01-Dec-2000 1

APO AE 09102

QC000000


06-Jan-2001 1

APO AE 09102

QC000000

1-214TH AVN REGTSOF-UH-60-01-03 (TB 1-1520-237-20-229)INSPECT THE LATERAL SERVO BELLCRANKASSEMBLY COMPLIED WITH AT 3073.0 ACFTHRS (MF2309)

06-Jan-2001 2

APO AE 09102

QC000000

1-214TH AVN REGTSOF-UH-60-01-04 (TB 1-1520-237-20-278)INSPECT FOR INSTALLATION OF FUELMONITORING SYSTEM COMPLIED WITH AT3073.0 ACFT HRS (MF2309)

06-Jan-2001 3

APO AE 09102

QC000000

1-214TH AVN REGTSOF UH-60-01-06 (TB 1-1520-237-23-231)INSPECT SAS ASEMBLIES COMPLETED AT3130.2 ACFT HRS (MF2309)

26-Mar-2001 1

APO AE 09102HEIDELBERG, GE.

QC000000

1-214TH AVN REGTSOF UH-60-01-05 (TB 1-1520-237-20-230)INSPECTION OF M/R SPINDLE (NDI)COMPLETED AT 3133.8 ACFT HRS (JH6726)

25-Apr-2001 1

APO AE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.



1-214TH AVN REGTSOF UH-60-01-07 (TB 1-1520-237-20-232)INSPECT M/R FLT CONTROL SELF LOCKINGBOLTS COMPLETED AT 3178.1 ACFT HRS.(MF2309)

29-May-2001 1

APO AE 09102HEIDELBERG, GE

QC000000

1-214TH AVN REGTSOF UH-60-01-08 (TB 1-1520-237-20-232)INSPECT M/R FLT CONTROL SELF LOCKINGBOLTS COMPLETED AT 3178.1 ACFT HRS(MF2309)

06-Jun-2001 1


QC000000

D CO 1-214TH AVNREGT

SOF UH-60-01-09 INSPECT M/R BLADEEXPANDABLE PINS I/A/W (TB 1-1520-237-20-233) COMPLIED WITH AT 3178.1 ACFT HRS(MF2309)

11-Jun-2001 1

HEIDELBERG GE

QC000000

1-214TH AVN REGTSOF UH-60-01-11 INSPECTION OF M/R HUBASSEMBLY AND REVISION OF 200 HOUR NDIINSPECTION COMPLIED WITH AT 3222.2 ACFTHRS. (BH1263)

27-Aug-2001 1

APO AE 09102

QC000000

1-214TH AVN REGTSOF UH-60-01-12 INSPECTION OF M/REXPANDABLE PINS AND REVISION TO TM 1-1520-237-PMS-1 COMPLIED WITH AT 3222.2ACFT HRS (BH1263)

27-Aug-2001 2

APO AE 09102

QC000000

DYNCORP AMCE OLRACE/CPCE PERFORMED AT 3229.6 ACFT HRSAT HEIDELBERG, GE BY MEMBER CC (IK3963)

26-Sep-2001 1

HEIDELBERG, GE

QC000000

1-214 AVN REGTUH-60-02-ASAM-01 INSPECTION OF FAIRINGASSEMBLY ON T/R BLADES COMPLIED WITHAT 3261.6 ACFT HRS. (MF2309)

19-Nov-2001 1

HEIDELBERG GE

QC000000


SOF UH-60-02-01 INSPECTION OF OIL COOLERFAN SHAFT ASSEMBLY COMPLIED WITH AT3267.3 ACFT HRS. (MF2309)

20-Nov-2001 1

HEIDELBERG GE. APOAE 09102

QC000000


SOF UH-60-02-02 MAIN ROTOR HUBSUBASSEMBLY REWORK COMPLIED WITH AT3267.3 ACFT HRS. (MF2309)

26-Nov-2001 1

HEIDELBERG GE

QC000000


SOF UH-60-02-03 INSP OF PITCH TRIMASSEMBLY COMPLIED WITH AT 3282.2 ACFTHRS (MF2309)

07-Dec-2001 1

HEIDELBERG GE

QC000000

2-502 AVN REGTSOF UH-60-02-04 (TB 1-1520-237-20-242)INSPECTION OF APU FUEL LINE GROMMETC/W AT 3295.6 ACFT HRS (LR0306)

25-Jan-2002 1

APO AE 09028

QC000000

SHAPE FLIGHTDETACHMENT

SOF UH-60-02-05 (TB 1-1520-237-20-243)INSPECTION OF EXPANDABLE PINS C/W AT3306.1 ACFT HRS (LD8792)

06-Feb-2002 1

APO AE 09705

QC000000


UH-60-02-ASAM-02 (TB1-1520-237-20-246)RECURING INSPECTION OF THECONTROLROD JAM NUTS C/W AT 3306.1 ACFTHRS (LD8792)

11-Feb-2002 1

APO AE 09705

QC000000


UH-60-02-ASAM-03 INSP ENG CONTROLQUADRANT POWER CONTROL LEVER (PCL)C/W AT 3306.1 ACFT HRS (LD8792)

13-Feb-2002 1

APO AE 09705

QC000000

1-214 AVN REGTSOF UH-60-02-06,REVISION TO M/R NDIPROCEDURES COMPLETED AT 3306.3 ACFTHRS. (DS1566)

01-Mar-2002 1

HEIDELBERG GE APOAE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.




UH-60-02-ASAM-04 RESTRAINT SYSTEMINSPECTION C/W AT 3341.7 ACFT HRS(LD8792)

28-Mar-2002 1

APO AE 09705

QC000000


UH-60-02-ASAM-05 REMOVAL OF CHICAGORAWHIDE M/R SPINDLE THRUST BEARINGSS/N C325-00001-C325-02407 C/W AT 3341.7ACFT HRS (LD8792)

28-Mar-2002 2

APO AE 09705

QC000000


UH-60-02-ASAM-06 (TB 1-1520-237-20-252)INSPECTION OF SWAGE PINS/COLLERSBOOST ASSEMBLIES COMPLIED WITH AT3345.5 ACFT HRS (MF2309)

19-Apr-2002 1

HEIDELBERG GE

QC000000

1-214TH AVN REGTSOF UH-60-02-07,MAIN MODULE PLANETARYCARRIER ASSY COMPLETED AT 3351.2 ACFTHRS (DS1566)

06-May-2002 1


QC000000

1-214TH AVN REGTSOF UH-60-02-08 (TM 1-1520-237-20-255) MAINMODULE PLANETARY CARRIERASSEMBLY.COMPLETED AT 3351.2 ACFT HRS.(DS1566)

06-May-2002 2


QC000000


INSPECT AIRCRAFT I/A/W SOF UH-60-02-09 (TB1-1520-237-20-258) COMPLIED WITH AT 3351.2ACFT HRS (MF2309)

28-May-2002 1

APO AE 09102

QC000000

1-214TH AVN REGTUH-60-02-ASAM-10, INSPECT AERIAL REFUELPROBE NOZZLES.N/A THIS ACFT (DS1566)

02-Jun-2002 1


QC000000

1-214TH AVN REGTSOF UH-60-02-10, INSPECT MAIN MODULEPLANETARY CARRIERASSEMBLY.COMPLETED AT 3352.9 ACFT HRS.(DS1566)

10-Jun-2002 1


QC000000

1-214TH AVN REGTUH-60-02-ASAM-08, INSPECT AN/ARC-220WIRING FOR CHAFING(TB 1-1520-237-20-256)(DS1566)

19-Jun-2002 1


QC000000

1-214TH AVN REGTUH-60-02-ASAM-09,TAIL ROTOR QUADRANTHARDWARE INSTALLATION (TB 1-1520-237-20-257) (DS1566)

19-Jun-2002 2


QC000000

214THSOF UH-60-02-11 INSPECT MAIN ROTORBLADE CUFF ASSEMBLY COMPLIED WITH AT3372.1 ACFT HRS (JV2740)

12-Aug-2002 1

HEIDELBERG

QC000000

D CO 1/214TH AVNREGT

SOF UH-60-02-12 INSPECTION OF MAINROTOR BLADE CUFFS COMPLIED WITH AT3372.1 ACFT HRS (MF2309)

13-Aug-2002 1

HEIDELBERG, GE APO-AE 09102

QC000000

AMCOM-E OLRACE/CPCE PERFORMED AT 3433.2 ACFT HRSAT COLEMAN BKS BY CC AND KK (RR2743)

23-Oct-2002 1

HUNTSVILLE AL

QC000000

D CO 1/214TH AVNUH-60-02-ASAM-11 AN/ARC 220(V)AMPLIFIER/COUPLER POWER WIRE MODIFIEDIAW UH-60-02-ASAM-08 COMPLETED AT 3433.2ACFT HRS (MF2309)

24-Oct-2002 1

COLEMAN BKS APO-AE09058

QC000000

2-502 AVN REGTSOF UH-60-03-01 MAIN MODULE PLANETARYCARRIER ASSY PASSED ULTRASONIC TEST(UT) INSPECTION AT 3462.7 ACFT HRS AND2683 MAIN MODULE TSN (LR0306)

20-Nov-2002 1

APO AE 09058

QC000000



8.7.DATE

6.REMARKS

4. 5.



2-502 AVN REGTUH-60-03-ASAM-01 FWD BELLCRANKSUPPORT ASSEMBLY RETIREMENT LIFECOMPLETED AT 3462.7 ACFT HRS (LR0306)

09-Dec-2002 1

APO AE 09058

QC000000

2-502 AVN REGTUH-60-03-ASAM-02 ASSIGN TAIL ROTORSERVO ASSEMBLY RETIREMENT LIFECOMPLETED AT 3462.7 ACFT HRS (LR0306)

09-Dec-2002 2

APO AE 09058

QC000000

2-502 AVN REGTGEN-03-ASAM-01 INSPECTION OF THEBATTERY BOX CY-8515 (ARC-201, ARC-220)COMPLIED WITH AT 3462.7 ACFT HRS(LR0306)

30-Dec-2002 1

APO AE 09058

QC000000

2-502 AVN REGTSOF UH-60-03-02 INSPECTION OF MAINROTOR BLADE CUFF ASSEMBLIES, SEALANTREMOVAL AND PRIMER/PAINT APPLICATIONCOMPLETED AT 3462.7 ACFT HRS (LR0306)

14-Jan-2003 1

APO AE 09058

QC000000

2-502 AVN REGTREPAIRED L/H CABIN CAP ANGLE STA 308.0,BL 34.5 IAW MERA NO: LE-EU001-0983 ANDSIKORSKY PROCEDURE AJM-BL34-1B AT3462.7 ACFT HRS (LR0306)

21-Jan-2003 1

APO AE 09058

QC000000

2-502 AVN REGTREWORKED/MODIFIED ENGINE CONTROLQUADRANT POWER CONTROL LEVERS ANDWIRING IAW TB 1-1520-237-20-245 DURINGPMS-2 AT 3462.7 ACFT HRS (LR0306)

23-Jan-2003 1

APO AE 09058

QC000000

2-502 AVN REGTREPLACED TAIL ROTOR QUADRANTHARDWARE INSTALLATION IAW TB 1-1520-237-20-257 DURING PMS-2 AT 3462.7 ACFT HRS(LR0306)

23-Jan-2003 2

APO AE 09058

QC000000

2-502 AVN REGTPMS-2 #7 COMPLETED AT 3462.7 ACFT HRS,NEXT PMS-2 #8 DUE AT 3962.7 ACFT HRS(LR0306)

12-Feb-2003 1

APO AE 09058

QC000000

2-502 AVN REGTSOF UH-60-03-03 MAIN MODULE PLANETARYCARRIER, SUPERSEDES ACFT FLIGHTRESTRICTIONS AND INCREASES CARRIERMAOT FROM 2000 TO 3700 HRS. COMPLETEDAT 3464.2 ACFT HRS (LR0306)

18-Feb-2003 1

APO AE 09058

QC000000

1-214TH AVNAPPLIED AIRWORTHINESS RELEASE FOR THECOMMUNICATION EAR PLUGS. QUALITATIVEEMC COMPLETED ON UH-60A 87-24642(TS1270)

11-Apr-2003 1

COLEMAN BARRACKSAPO AE 09058

QC000000

AMCOM-E OLRACE/CPCE PERFORMED AT 3519.8 ACFT HRSAT COLEMAN BARRACKS BY KK&F (RR2743)

23-Apr-2003 1

HUNTSVILLE,AL.

QC000000

L-3 COMMSTORMSCOPE INSTALLED I/A/W L3COMMUNICATIONS DRAWING #LEX-1871 AT3604.8ACFT HRS (HA9430)

02-Sep-2003 1

BLUEGRASS ARMYDEPOT,KY

QC000000

214TH AVN REGTCOMPLY WITH REQUIREMENTS OF SOF UH-60-04-01 COMPLIED WITH AT 3629.8 ACFTHOURS (JV2740)

01-Oct-2003 1

COLEMAN BKS

QC000000


UH-60-04-ASAM-01 GLARE SHIELD LIGHTINGCIRCUIT BREAKER REPLACEMENT COMPLIEDWITH AT 3679.8 ACFT HRS (JV2740)

27-Jan-2004 1

COLEMAN BKS 09058

QC000000



8.7.DATE

6.REMARKS

4. 5.



D CO 1/214TH AVNUH-60-04-ASAM-02 INSPECT ALL LOW-TIMEACFT (TAIL NUMBER 03-26982 AND PRIORPLUS 03-26992, 3&4 WITH LESS THAN 2000HRS COMPLIED WITH AT 3730.0 ACFT HRS ON01 APR 04 (JV2740)

01-Apr-2004 1

COLEMAN BKS

QC000000

D CO 1/214TH AVNEMC CHECK FOR GR660 PASSIVE RADIATIONSYSTEM COMPLETED ON ACFT 8926165 ON 13MAY 04 AWR 1149 (JV2740)

13-May-2004 1

COLEMAN BKS

QC000000

D CO 1/214TH AVNSOF UH-60-04-02 COMPLIED WITH. NOTAPPLICABLE TO THIS AIRCRAFT. (JV2740)

09-Jun-2004 1

COLEMAN BKS

QC000000


COMPLY WITH REQUIREMENTS OF UH-60-04-ASAM-04 NLT 26 AUG O4 COMPLIED WITH 13AUG 04 3805.8 ACFT HRS AWR 1149 (DS3908)

16-Aug-2004 1

COLEMAN BKS

QC000000

C CO 1-214TH AVNREGT

SOF UH-60-04-04 C/W AT 3817.6 ACFT HRS(RS1033)

26-Aug-2004 1

GRAFENVOHERGERMANY

QC000000


UH-60-04-ASAM-05 C/W AT 11 NOV 04 3870.2ACFT HRS (DH6671)

21-Sep-2004 1

COLEMAN BARRACKS

QC000000

DCO 1-214 AVNLATE ENTRY COMPLY WITH REQUIREMENTSOF UH-60-04-ASAM-03 NO LATER THAN 15APR O6 SUPERCEEDED BY UH-60-05-ASAM-01(DH6671)

10-Jan-2005 1

COLEMAN

QC000000

DYNCORP E OLR APO09058

ACE/CPCE PERFORMED AT 3954.6 ACFT HRSAT COLEMAN BKS MANNHEIM GE BY ACETEAM MEMBER MM (SH0481)

24-Feb-2005 1

COLEMAN BARRACKS

QC000000

D CO 1/214TH AVNUH-60-05-ASAM-02 C/W 20050304 (BLUEFORCE TRACKER) N/A THIS ACFT (JY2740)

04-Mar-2005 1

COLEMAN BARRACKS

QC000000

D CO 1/214TH AVNUH-60-05-SOF-02 COMPLY WITHREQUIREMENTS OF IMPLEMANTATION OFENHANCED MAINTENANCE PROGRAMCOMPLIED WITH 20050418/3964.1 ACFT HRS(JY2740)

22-Mar-2005 1

COLEMAN BARRACKS

QC000000

D CO 1/214TH AVNUH-60-05-ASAM-01 (FUEL SYSTEM TEST) C/WON 04 ARP 05 AT 3954.6 ACFT HRS DURINGPMS2 (DS3908)

05-Apr-2005 1

COLEMAN BARRACKS

QC000000

D CO 1-214 AVN REGTPMS-2 #8 COMPLETED @ 3954.6 ACFT HRS,NEXT PMS DUE #9 @ 4454.6 ACFT HRS(DS3908)

05-Apr-2005 2

CAAF APO AE 09058

QC000000

D CO 1/214TH AVNUH-60-05-ASAM-03 (SEATBELT INSPECTION)COMPLIED WITH AT 3955.4 ACFT HOURS 11APR 05 (JY2740)

05-Apr-2005 3

COLEMAN BKS

QC000000

D CO 1/214TH AVNUH-60-05-ASAM-04 (TAIL YOKE PN-042 INSP)COMPLIED WITH AT 3955.4 ACFT HRS 11 APR05 (JY2740)

06-Apr-2005 1

COLEMAN BKS

QC000000

D CO 1/214TH AVNT/R BIAS DUE FOR COMPLETION OF PHASEON 11 APR 05 YELLOW-.328 BLACK-.328 RED-.328 BLUE-.360 ACFT HRS 3954.6. (DM5656)

11-Apr-2005 1

COLEMAN BKS

QC000000

D CO 1/214TH AVNUH-60-05-ASAM-05 C/W 20050429 AT 3964.1ACFT HRS (R/H TIE ROD ASSY INSP) (DH6671)

29-Apr-2005 1

COLEMAN BARRACKS

QC000000



8.7.DATE

6.REMARKS

4. 5.



D CO 1-214 AVN REGTUH-60-05-ASAM-06 TROOP SEAT RESTRAINTBUCKLE COMPLETED AT 3979.4 ACFT HRS20050531 (DH6671)

26-May-2005 1

CAAF APO AE 09058

QC000000

D CO 1-214 AVN REGTUH-60-O5-ASAM-07 AIR INTRUSION OFHYDRAULIC SYSTEM COMPLETED AT 3970.1ACFT HRS 20050510 (DH6671)

26-May-2005 2

CAAF APO AE 09058

QC000000

D CO 1-214 AVNCOMPLETED UH-60-05-ASAM-10 AT 4029.7ACFT HRS ON 26 AUG 2005 (DH6671)

26-Aug-2005 1

APO AE09058 CAAF

QC000000

D CO 1-214(M/R HUB) COMPLIED WITH REQUIREMENTSOF UH-60-06-SOF-01 AT 4071.2 ACFT HRS ON21 DEC 05 (DH6671)

20-Dec-2005 1

CAAF

QC000000

D 1/214TH AVNEMC CHECK COMPLETED ON ACFT 8724647ON 20060404 FOR AWR 1159, OPERATION OFINFRARED COUNTERMEASURETRANSMITTER, T1360C(V)1/ALQ-144C(V)PN13301520. (JY2740)

04-Apr-2006 1

CAAF GE 09058

QC000000

D CO 1-214AVNUH-60-06-ASAM-03 (SWASHPLATE) C/W AT4166.0 ACFT HRS. N/A THIS ACFT. (JY2740)

12-Jun-2006 1

CAAF, GE 09058

QC000000

D CO 1-214AVNUH-60-06-ASAM-04 (CABS) COMPLIED WITH AT4187.0 ACFT HOURS. N/A THIS ACFT. (JY2740)

22-Jun-2006 1

CAAF, GE 09058

QC000000

D CO 1-214AVNUH-60-06-SOF-02 (CABS) COMPLIED WITH AT4187.0 ACFT HOURS. N/A THIS ACFT. (JY2740)

23-Jun-2006 1

CAAF, GE 09058

QC000000

D CO 1-214AVNUH-60-06-ASAM-05 (BFT) COMPLIED WITH AT4213.1 ACFT HOURS. N/A THIS ACFT. (JV2740)

01-Aug-2006 1

CAAF, GE 09058

QC000000

D 1/214TH AVNUH-60-07-ASAM-01 (WHITE ENG HARNESS)COMPLIED WITH AT 4306.9 AIRCRAFT HOURS.BOTH ENGINES DISCREPANT (JV2740)

05-Dec-2006 1

CAAF GE 09058

QC000000

D.CO 1/214 AVN REGTUH-60-06-ASAM-02 REPLACED ALL CADIUMPLATED STEEL JAMNUTS WITH SILVERPLATED STAINLESS STEEL JAMNUTS,COMPLIED WITH ON 6 DEC 06 DURING PMI#[email protected] ACFT HRS (ST0266)

06-Dec-2006 1

CAAF GE 09058

QC000000

D.CO 1/214TH AVNREGT

UH-60-06-ASAM-01 (REPLACEMENT OF TAILLANDING STRUT ASSY'S 041, 042, 043)COMPLIED WITH @ 4306.9 ACFT HRS ON 15DEC 06. (ST0266)

15-Dec-2006 1

COLEMAN AAF APO09058

QC000000

D CO 1-214 AVN REGTUH-60-07-ASAM-02, REVISION TO UH-60-07-ASAM-01, COMPLIED WITH AT 4306.9 ACFTHRS. (JK6704)

21-Dec-2006 1

COLEMAN BKS, GE09058

QC000000

D CO 1-214 AVN REGTUH-60-07-ASAM-03, YAW AND COLL BOOSTSERVO ROLL PINS, COMLIED AT 4306.9 ACFTHRS. (JK6704)

21-Dec-2006 2


QC000000

D CO 1-214 AVN REGTPMI# 1 COMPLETED @ 4306.9 ACFT HRS, NEXTPMI # 2 DUE @ 4666.9 ACFT HRS (ST0266)

28-Dec-2006 1

COLEMAN AAF 09058

QC000000

D.CO 1-214 AVN REGTUH-60-07-ASAM-04 VERIFICATION OFAUTOROTATION RPM CHARTS COMPLIEDWITH AT 4306.9 ACFT HRS. ON 29 DEC 06.(ST0266)

29-Dec-2006 1

COLEMAN AAF 09058

QC000000



8.7.DATE

6.REMARKS

4. 5.



D.CO 1-214 AVN REGTUH-60-07-ASAM-05, ARC-220 / KY-100 STARTUP PROCEDURES, COMPLIED WITH AT 4308.2ACFT HRS. ON 24 JAN 07. (ST0266)

24-Jan-2007 1

COLEMAN AAF 09058

QC000000

D.CO 1-214 AVN REGTUH-60-07-ASAM-06 C/W @ 4312.1 ACFT HRS.(HOIST CABLE GUARD DEFECTOR) N/A THISACFT. (JV2740)

07-Feb-2007 1

COLEMAN AAF 09058

QC000000

A CO 1/214TH AVNCOMLIED WITH UH-60-07-AMAM-01 AT 4349.0ACFT HRS, (JK4543)

26-Mar-2007 1

GAAF, 09114

QC000000

D.CO 1-214 AVN REGTUH-60-07-ASAM-07, CEFS STATIC BONDINGJUMPER N/A THIS ACFT C/W @ 4400.2 ACFTHRS (JC4882)

10-May-2007 1

COLEMAN AAF 09058

QC000000

G CO 52ND AVN REGTH-60-07-ASAM-10 (MAIN FUEL MANIFOLDCHAFFING) COMPLETED AND COMPLIEDWITH @ 4483.7 ACFT HOURS (AM7315)

12-Oct-2007 1

AVIANO AFB, ITALY09604

QC000000

D.CO 1-214 AVN REGTUH-60-08-AMAM-01 C/W @ 4548.3 ACFT HRS.(MAIN LANDING GEAR SERVICE INSPECTION)(JV2740)

17-Oct-2007 1

COLEMAN AAF 09058

QC000000

G CO 52ND AVN REGTUH-60-08-ASAM-02 (POWER AVAILABLECONTROL CABLE) COMPLETED ANDCOMPLIED WITH AT 4582.6 ACFT HRS(AM7315)

19-Nov-2007 1


QC000000

G CO 52 AVN REGTUH-60-08-AMAM-02 (TAIL ROTOR OUTBOARDRETENTION PLATE SHIMS) INSPECTIONCOMPLETED WITH AND COMPLIED AT 4582.6ACFT HOURS (AM7315)

06-Dec-2007 1


QC000000

G CO 52ND AVN REGTUH-60-08-ASAM-04 (PILOT'S LOWER SEATRAIL CHAFFING ELECTRICAL) COMPLETEDAND COMPLIED WITH AT 4582.6 ACFT HOURS(AM7315)

11-Dec-2007 1


QC000000

G CO 52ND AVN REGTUH-60-08-ASAM-05 COMPLETED ANDCOMPLIED WITH AT 4582.6 ACFT HRS. -18INSPECTION ADDED NEXT DUE 31 JUL 08(AM7315)

12-Dec-2007 1


QC000000

G CO 52ND AVN REGTH-60-08-ASAM-01 (TROOP SEAT UPPERENERGY ATTENUATING WIRES)COMPLETEDAND COMPLIED WITH @ 4582.6 ACFT HOURS(AM7315)

17-Dec-2007 1


QC000000

G CO 52ND AVN REGTUH-60-08-AMAM-03 COMPLETED ANDCOMPLIED WITH @ 4582.6 ACFT HRS.(AB4134)

21-Dec-2007 1


QC000000

G 52 AVN REGTM/R RIG COMPLETED IAW TM 1-1520-237-23FOR MAJOR MAINT-LOW COLL ANGLE=90 8.2180 -1.4 0 -.1 TOTAL -2.2 AVG -.55 -HIGH COLLANGLE= 90 18.3 180 11.7 270 12.6 0 19.1 TOTAL61.7 AVG 15.425 -FWD CYCLIC ANGLE= 90 31.9270 -1.7 TOTAL 33.6 -AFT CYCLIC ANGLE= 9026.3 270 5 TOTAL 21.3 -LEFT CYCLIC ANGLE=180 -7.8 0 7.5 TOTAL 15.3 -RIGHT CYCLICANGLE= 180 7.6 0 -7.1 TOTAL 14.7 -FWD 1/2TURN SHORTER -AFT 1/2 TURN LONGER -LAT3/4 TURN SHORTER.. CHECK WITHINLIMITATIONS (AM7315)

17-Jan-2008 1

AVIANO AB, ITALY09604

QC000000



8.7.DATE

6.REMARKS

4. 5.



G 52 AVN REGTT/R BIAS DUE FOR COMPLETION OF MAJORMAINT. YELLOW-.34 BLACK-.35 RED-.35 BLUE-.35 ACFT HRS 4582.6 (AM7315)

17-Jan-2008 2


QC000000

G CO 52ND AVN REGTUH-60-08-SOF-01 (MAIN ROTOR BLADE PININSP CHANGE) COMPLETED AND COMPLIEDWITH AT 4582.6 ACFT HOURS (AM7315)

29-Jan-2008 1


QC000000

G CO 52ND AVN REGTH-60-08-AMAM-05 GOODRCIH INTERNALRESCUE HOISTS COMPLETED AND COMPLIEDWITH AT 4582.6 ACFT HOURS. (AB4134)

30-Jan-2008 1


QC000000

G CO 52ND AVN REGTH-60-08-ASAM-03 (CHANGES TO FUEL SYSINTEGRITY CHECKS) COMPLETED ANDCOMPLIED WITH @ 4582.6 ACFT HOURS(AM7315)

31-Jan-2008 1


QC000000

G CO 52ND AVN REGTH-60-08-AMAM-06 COMPLIED WITH AT 4585.1ACFT HRS. (AB4134)

06-Feb-2008 1


QC000000

1-214TH AVN REGTCOMPLIED WITH UH-60-08-ASAM-06 MRPYLON SLIDING FAIRING AT 4592.7 ACFT HRS.(AN9260)

05-Mar-2008 1

CAAF,MANNHEIM GE

QC000000

1-214TH AVN REGTCOMPLIED WITH REQUIERMENTS OF H-60-08-AMAM-07, AN/ASN-128/D/B DOPPLER GPSNAVIGATION SET @ 4623 ACFT HRS. LC7577(LC7577)

02-Apr-2008 1

CAAF MANNHEIM, GE09058

QC000000

1-214TH AVN REGTCOMPLIED WITH REQUIERMENTS OF H-60-08-ASAM-08, ACFT SELF RETAINING FLIGHTCONTROL BOLTS @ 4604.5 ACFT HRS. LC7577(LC7577)

08-Apr-2008 1

CAAF, MANNHEIM GE09058

QC000000

1-214 AVN REGTCOMPLYED WITH H-06-08-AMAM-08 FLIGHTCONTROL RIGGING UPDATE AT 4640 ACFT.(ST5526)

27-May-2008 1

CAAF MANNHEIM, GE

QC000000


COMPLY WITH REQUIERMENTS OF H-60-08-ASAM-10, ELECTRICAL WIRE CHAFFING AT4663 ACFT HRS. (LC7577)

10-Jul-2008 1


QC000000

TASM-EACE/CPCE PERFORMED AT 4663.3 ACFT HRSAT COLEMAN BARRACKS GERMANY BY ACETEAM MEMBER MM. (SH0481)

30-Jul-2008 1

CAAF, MANNHEIM GE

QC000000

D CO. 1-214TH AVNREGT

PERMANENT REPAIR COMPLETED IAW MECF69807 DURING PMI PHASE MAINTENANCE AT20080810. (ST5526)

10-Aug-2008 1

CAAF.GERMANY

QC000000

D CO 1-214 AVN REGTCOMPLYED WITH H-60-08-ASAM-11, FLIGHTCONTROL INSP AT 4663.3 ACFT HR (ST5526)

19-Aug-2008 1

CAAF MANNHEIM GE09058

QC000000


UNS-1D WITH APX-118 CONFIGURATION, EMCCHECK PERFORM IAW AWR 1167-R2. UNS-1D,APX-118, CEFS, WX 1000+, 12 POINT ICS, ALQ-144, APR-39, M-130, KY-58 AND 2-AHP MODS.WORKING PROPERLY. (AN9260)

26-Aug-2008 1

CAAF MANNEIM, GE

QC000000



8.7.DATE

6.REMARKS

4. 5.



1-214TH AVN REGTFULL MAIN ROTOR RIG CHECK COMPLETEDON 20080909HIGH COLL ANGLE 15.1FWDCYCLIC ANGLE 33.3AFT CYCLIC ANGLE19LEFT CYCLIC ANGLE 15.6RIGHT CYCLICANGLE 14.2 (LC7577)

09-Sep-2008 1

CAAF, MANNHEIN GE09058

QC000000

1-214TH AVN REGTFULL AIRCRAFT TAIL ROTOR RIGCOMPLETED 20080909RED BLADE BIAS5.16YELLOW BLADE BIAS 5.06BLUE BLADEBIAS 4.47BLACK BLADE BIAS 4.47 (LC7577)

09-Sep-2008 2

CAAF, MANNHEIM GE,09058

QC000000

1-214TH AVN REGTCOMPLETED TAIL ROTOR CABLE TENSIONCHECK 20080909RIGHT HAND 140LEFT HAND140TEMPERATURE 21 DEG C (LC7577)

09-Sep-2008 3


QC000000


COMPLIED WITH REQUIREMENTS OF UH-60-08-ASAM-12, PARKER AEROSPACE AIR TURBINESTARTER AT 4363.3 ACFT HRS. (AN9260)

16-Sep-2008 1

CAAF MANNHEIM, GE

QC000000


COMPLIED WITH H-60-08-ASAM-14 AT 4663.3ACFT HRS ON 20080923 (ENG WIINGHARNESS') (TF6439)

23-Sep-2008 1

COLEMAN AAFGERMANY 09058

QC000000

D CO 1/214 AVN REGTCOMPLIED WITH REQUIREMENTS OF H-60-08-ASAM-13 AT 4663.3 ACFT HOURS ON 20080923(FIRE EXT UNION) (RB3324)

24-Sep-2008 1


QC000000

1-214 AVN REGT.MAIN ROTOR RIG COMPLETED AT 20080909AT 4663 ACFT HOURSCNTRL POS RTFWD LFT AFT TOTAL AVGLOW COLL8.9 -2.7 -10.2 2.1 -1.9 -.475HIGHCOLL 20.2 10.6 9.9 20 60.715.1FWD CYC -2.1 31.233.3AFT CYC 24.9 5.919LFT CYC 8.6 6.815.6RT CYC 7.0 7.214.2PRIMARY SEROVO BIAS: FD +1/2 AFT -1/2LAT 0 (ST5526)

26-Sep-2008 1

CAAF, GERMANY

QC000000

1-214 AVN REGT.T/R RIG COMPLETED AT 20080909 AT 4663ACFT HRT/R CABLE TENSION: RT: 140. LT:140. TEMP: 21CRED BEFOR: 4.84 AFTER:5.16 DIFF: .32YEL BEFOR: 4.72 AFTER: 5.06DIFF: .34BLU BEFOR: 4.13 AFTER: 4.47DIFF: .34BLK BEFOR: 4.13 AFTER: 4.47DIFF: .34 (ST5526)

26-Sep-2008 2

CAAF, GERMANY

QC000000

1-214TH AVN REGTCOMPLY WITH REQUIERMENTS OF H-60-09-SOF-01, HYDRO-MECHANICAL UNIT (HMU) AT4670.3 ACFT HRS. (LC7577)

23-Oct-2008 1


QC000000

1-214TH AVN REGTCOMPLY WITH REQUIERMENTS OF H-60-09-SOF-02, CMWS MWO AT 4684.7 ACFT HRS.(ST5526)

12-Nov-2008 1


QC000000

DCO 1-214 AVN REGTLATE ENTRY COMPLIED WITH H-60-09-SOF-0319 NOV 2008 (POSSIBLE RETIREMENT LIFEOVERFLIGHT)

19-Nov-2008 1

COLEMAN AAF, APO AE09058

QC000000



8.7.DATE

6.REMARKS

4. 5.



D CO 1-214TH AVNUNS-1D WITH APX-118 CONFIGURATION, EMCCHECK PERFORM IAW AWR 1167-R2. UNS-1D,APX-118, CEFS, WX 1000+, 12 POINT ICS, ALQ-144, APR-39, M-130, KY-58 AND 2-AHP MODS.WORKING PROPERLY. COMPLETED ONAIRCRAFT 8323855

21-Jan-2009 1


RB923324

DCO 1/214TH AVN REGTCOMPLIED WITH REQUIRMENTS OF H-60-09-ASAM-04 AT 4723.6 ACFT HOURS AT 27-FEB-2009

27-Feb-2009 1


ST895526

D CO 1-214TH AVN REGCOMPLIED WITH REQUIREMENTS OF H-60-09-ASAM-05

04-Mar-2009 1


D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-09-ASAM-07 @ 4757.0 ACFT HOURS

27-Apr-2009 1


RB923324

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-09-ASAM-08 4783.3 ACFT HOURS (ENG COWLING)

01-Jun-2009 1


RB923324


COMPLIED WITH REQUIREMENTS OF H-60-09-ASAM-09 ON 01 JUN 09 AT 4783.3 ACFT HRS

01-Jun-2009 2


TF546439

1-214TH AVN REGTCOMPLIED WITH REQUIREMENTS OF H-60-09-AMAM-06 @ 4845.8 ACFT HOURS (CARGOHOOK THRUSTER CAD LIFE REDUCTION)

29-Aug-2009 1

CONSTANTA, ROMANIA

JW829277

D CO 1-214TH AVN REGCOMPLIED WITH REQUIREMENTS OF H-60-09-04 A2C2S

17-Sep-2009 1

NOVO SELO, BULGARIA


H-60-10-AMAM-03 (COCKPIT AIRBAG SYSTEMDEACTIVATION) NOT APPLICABLE THISAIRCRAFT, CABS NOT INSTALLED

10-Nov-2009 1


AM787315

D CO 1-214TH AVN REGH-60-10-AMAM-04 ASN-128B/C DGNS. ACFTNOT IN COMPLIANCE.

16-Nov-2009 1


AMCOM TASM-EUROPEACE/CPCE PERFORMED AT 4935.5 ACFT HRSAT COLEMAN BRKS GERMANY BY ACE TEAMMEMBERS "F" & "MM"

16-Nov-2009 3


TA459908

DCO 1-214 AVN REGTH-60-10-ASAM-03 FIRE BOTTLE DISCHARGELINES AND NOZZLES. ACFT NOT INCOMPLIANCE. -1 ENTRY WAS MADE IAW THISASAM TO REFLECT NON-COMPLIANCEREQUIREMENTS.

16-Nov-2009 4


DG106187



8.7.DATE

6.REMARKS

4. 5.




MEC: F101064 PROBLEM; IAW TM1-1520-237-23-7, WP 0640 00, THE ALLOWABLE MAXIMUMDEPTH OF MATERIAL REMOVAL FROM ALLOVER OTHER OUTER CAST SURFACES OFOUTPUT HOUSING IS 0.030 INCH. REQUESTAUTHORIZATION TO BLEND REPAIR AT THE11 O'CLOCK POSITION SUPPORT FIN ANDADJACENT CORNER USING EXISTING TMINSTRUCTIONS. MAXIMUM DEPTHOF DAMAGEIS 0.075INCH DEEP. NO ACTIVE CORROSIONWAS FOUND IN PITS. WORK WILL BEWORKED ORDERED TO TASM-EUROPE,MANNHEIM, GERMANY.ENGINEERINGDISPOSITION; AUTHORIZATION IS GRANTEDFOR TASM-EUROPE, COLEMAN BARRACKS,MANNHEIM GERMANY IN SUPPORT OF D CO1/214TH AVN, TO REPAIR CORROSIONDAMAGE ON INPUT HOUSING MODULEP/N70351-08001-046, S/N A264-03214 USINGPROCEDURES IAW TM 1-1520-237-23-7, WP0640 00, AQS REQUESTED. LOCALLY BLENDALL PITTED AREAS TO REMOVE SHARPEDGES. RETREAT REPAIRED AREAS WITHCHROMATE PICKLE SOLUTION, PRIME ANDREPAINT IAW TM 1-1500-344-23.JEPHREY L.SOUTH, AEROSPACE ENGINEERAED RDECOMLIAISON ENGINEER-EUROPE, COLEMANBARRACKS, SANDHOFEN, GERMANYDSN 382-5244 LOCAL 0621-779-5244 CELL 0162-296-4461

17-Nov-2009 1


TF546439

1-214TH AVN REGTCOMPLIED WITH REQUIREMENTS OF H-60-09-AMAM-07 (HAND HELD FIRE EXTINGUISHERS)

20-Nov-2009 1

CONSTANTA, ROMANIA

JW829277

D CO 1-214 AVN REGT.FULL MAIN ROTOR RIG COMPLETED AT 28NOV 09 AT 4935.5 ACFT HOURS FORREPLACEMENT OF M/R TRANSMISSION ANDHUB.LOW COLL ANGLE 90DEG 7.9 180DEG -1.8 270 DEG -9.3 0 DEG 1.0 TOT -2.2 AVG -5.5HIGH COLL ANGLE 18.2 11.612.0 18.2 60 15FWD CYCLICANGLE -4.3 30.334.6AFT CYCLIC ANGLE 25.65.6 20.0LEFT CYCLICK ANGLE9.4 6.6 16.0RIGHTCLYCLIC ANGLE 7.1 8.215.3PRIMARY SEROVO BIAS: FD -1/2 AFT +1/2LAT 1

28-Nov-2009 1

CAAF, GERMANY APOAE 09058

AM787315

G CO 52ND AVN REGTONE-TIME FCC CHECK COMPLETED FOR AWR1352 (MPS PASSIVE RADIATION DETECTIONSYSTEM) COMPLETED ON 07 DEC 09 AT4937.0 HRS.

07-Dec-2009 1

STUTTGART, GERMANY

WS756726

G CO 52ND AVN REGTAPPLIED AWR 1352 (MPS PASSIVE RADIATIONDETECTION SYSTEM); TEMPORARY ASWEELL AS PERMANENT INSTALLATION ON 07DEC 09 AT 4937.0 HRS

07-Dec-2009 2

STUTTGART, GERMANY

WS756726


COMPLIED WITH REQUIREMENTS OF UH-60-10-AMAM-05 ON 20090121 AT 4984.0 ACFT HRS

21-Jan-2010 1




8.7.DATE

6.REMARKS

4. 5.



DCO 1-214TH AVN REGTCOMPLIED WITH REQUIREMENTS OF H-6--10-AMAM-11(OIL SAMPLING SCHEDULECHANGES) ON 1FEB 2010 AT 5000.0 ACFT HRS

02-Feb-2010 1


WK439480

TASM-EMEC# F104208TASM-E REPAIRED 1 EACRACK IN SHEAR DECK SKIN AT R/H REARCORNER IAW DMWR 1-1520-237 WP 0168 00AND INSTRUCTIONS PER MEC#F104208.AUTHORIZED BY JEPHREY L. SOUTH,AEROSPACE ENGINEER DSN 382-5244

02-Feb-2010 2


MC651750

D CO 1-214 AVN REGTH-60-ASAM-10-06 COMPLIED WITH THIS DATEAT 5000.0 ACFT HRS, T700-GE-700 ENGINESINSTALLED

10-Feb-2010 1


VZ748391


FUEL FEED SYSTEM VACUUM/PRESSURETEST: INITIAL READING-6.000INHGVACUUMTESTNO.1 FUEL SYSTEM: 20 MIN READING-5.988, FIVE MIN READING-5.986, VACUUMLOSS-0.002 VACUUM LOSS SHOULD BE LESSTHAN OR EQUAL TO .100INHG.NO.2 FUELSYSTEM: 20 MIN READING-6.036, FIVE MINREADING-6.036, VACUUM LOSS-.017.PRESSURE TESTINITIAL READING-30.000PSIGNO.1 FUEL SYSTEM: 20MINREADING-29.992, FIVE MIN READING-29.946.PRESSURE LOSS- .046. PRESS LOSS SHOULDBE LESS THAN OR EQUAL TO .300INHG.NO.2FUEL SYSTEM: 20 MIN READING-29.992, 5MINREADING-29.946, PRESSURE LOSS .046DATETESTED 01 MAR 2010, AMBIENT TEMP 20 DEGCELSIUS.

15-Mar-2010 1


TF546439


PROBLEM:MEC: F104208 DTD 02 FEB 10-A CO.1-214TH GS A/C UH-60A 83-23869 A/C, HRS5000.0, TASM-E RECEIVED A WORK ORDER TOREPAIR SHEAR DECK FOUND CRACK DURINGPHASE INSPECTION. APPROX 1 INCH CRACKIN SHEAR DECK SKIN AT R/H REAR CORNER.ONE PREVIOUS REPAIR ON FWD L/H CORNER.TASM-E REQUEST PERMISSION TO REPAIRI/A/W DMWR 1-1520-237 WP 0168 00. TASM-EHAS THE TOOLS, PERSONNEL AND PARTS TOCOMPLETE THIS TASK.ENGINEERINGDISPOSITION:AUTHORIZATION IS GRANTEDFOR TASM-EUROPE, COLEMAN BARRACKS,MANNHEIM GERMANY TO REPAIR SHEARDECK, P/N 70211-05010-041, ON UH-60A 83-23869 IAW DMWR 1-1520-237 WP 0168 00. THESTAINLESS STEAL REPAIR DOUBLER DOESNOT REQUIRE CADMIUM PLATING; APPLY 2COATS OF MIL-P-23377 PRIMER OREQUIVALENT. ALL FASTENERS AND FAYINGSURFACES ARE TO BE INSTALLED WITH SAE-AMS-S-8802 SEALANT OREQUIVALENT.JEPHREY L. SOUTH,AEROSPACE ENGINEERAED RDECOMLIAISON ENGINEER-EUROPE, COLEMANBARRACKS, SANDHOFEN, GERMANYDSN 382-5244 LOCAL 0621-779-5244 CELL CELL 0162-296-4461

15-Mar-2010 2


TF546439



8.7.DATE

6.REMARKS

4. 5.




MEC F105267:PROBLEM:A CO 1-214TH ACFT83-23869 ACFT HRS 5000.0 TASM-E RECEIVEDFITTING ASSY PN 70219-02116-041 FOROVERSIZE BEYOND LIMITS IN BUSHING BORE.BUSHING BORES MEASURE 0.502 INCH. TASM-E IS REQUESTING AUTHORIZATION TOFABRICATE OVERSIZE BUSHINGS 2 EA ANDINSTALL IN THE FITTING. STANDARDBUSHING PN NAS77-6-012. TASM-E HAS THEFACILITIES, EQUIPMENT AND TRAINEDPERSONEL TO PERFORM THISTASK.ENGINEERINGDISPOSITION:AUTHORIZATION IS GRANTEDFOR TASM-EUROPE, IN SUPPORT OF A CO 1-214TH AVN, TO MANUFACTURE AND INSTALLOVERSIZED P/N NAS77 BUSHING INVIBRATION ABSORBER FITTING P/N 70219-02116-041 ON UH-60A 83-23869 AS FOLLOWS:1) MANUFACTURE OVERSIZED BUSHING IAWNAS77-6-012 SPECIFICATION EXCEPT MAKEOUTSIDE DIAMETER .5023 TO .5030.2) 17-4CRES HEAT TREATED TO H1025 IS ANACCEPTABLE ALTERNATIVE MATERIAL.3)INSTALL PRESS FIT BUSHINGS WET WITH MIL-S-8802 SEALANT IF USING CRES BUSHINGSOR MIL-P-23377 PRIMER IF USING CADPLATED STEEL BUSHINGS.JEPHERY L.SOUTH AEROSPACE ENGINEER AED RDECOMLIAISON ENGINEER-EUROPE, COLEMANBARRACKS, SANDHOFEN, GERMANYDSN 382-5244 LOCAL 0621-779-5244 CELL 0162-296-4461.

15-Mar-2010 3


TF546439



8.7.DATE

6.REMARKS

4. 5.




MEC: F105927-FUSELAGE STRUCTUREA CO 1-214TH ACFT 83-23869 ACFT HRS 5000.0DURING PHASE INSPECTION, DAMAGE WASDISCOVERED TO THE P/N 70500-02070-046PHOENIX DRIP PAN SUPPORT RING. AFTERRING REMOVAL, SEVERAL RIVET HOLESWERE FOUND ELONGATED IN THE R/HTRANSMISSION SUPPORT BEAM. THE SIXTHHOLE FORWARD FROM THE AFT EDGE WASDOUBLED DRILLED. REQUEST ENGINEERINGDISPOSITION AND REPAIRINSTRUCTIONS.ENGINEERINGDISPOSITION:AUTHORIZATION IS GRANTEDFOR 1/214TH AVN, COLEMAN BARRACKS,GERMANY TO REPAIR DAMAGE TO THE RHTRANSMISSION SUPPORT BEAM, P/N 70211-02133-046, ON UH-60A 83-23869 IAW TM 1-1520-237-23 AND AS FOLLOWS:1) THE EIGHTHOLES THAT WERE SLIGHTLY ELONGATEDSHALL BE OPENED UP TO ACCEPT 5/32RIVETS.2) THE ONE HOLE HAT WAS SLIGHTLYFIGURE 8 DRILLED SHALL BE OPENED UP TOACCEPT A 3/16 RIVET.3) THE SIXTH HOLEFROM THE AFT EDGE SHALL BE BLENDED TOREMOVE ALL SHARP EDGES. NO FASTENERWILL BE INSTALLED.4) TREAT AND PRIMEALL REPAIRED HOLES IAW TM 1-1500-344-23.5) DURING INSTALLATION OF DRIP PAN,DO NOT INSTALL A FASTENER IN THECLEANED UP SIXTH HOLE. DO NOT FILL HOLEWITH SEALANT. VISUALLY INSPECT TOPSURFACE OF THE BOTTOM BEAM FLANGEFOR CRACKS IN THE AREA OF DAMAGEDDURING EACH SUBSEQUENT PHASEMAINTENANCE. IF A CRACK IS SUSPECTED,PERFORM NDI IAW TM 1-1520-265-23, NOCRACKS ALLOWED.JEPHREY L. SOUTH,AEROSPACE ENGINEERAED RDECOMLIAISON ENGINEER-EUROPE, COLEMANBARRACKS, SANHOFEN, GERMANYDSN 382-5244 LOCAL 0621-779-5244 CELL 0162-296-4461

15-Mar-2010 4


TF546439

DCO 1-214 AVN REGTAWR 1529 DATED 07OCT09, INTERIMSTATEMENT OF AIRWORTHINESSQUALIFICATION FOR THE INSTALLATION OFTHE FIBER OPTIC GYRO SYSTEM AN1716/A,ATTITUDE HEADING REFERENCE UNIT/SET(AHRU/AHRS) IN DUAL CONFIGURATION ONUH/EH/HH-60A/L ON ALL UH-60A/LHELICOPTERS.

31-Mar-2010 1


QC000000

D CO 214THH-60-10-ASAM-07 STABILATOR HINGEFITTINGS COMPLIED WITH AT 5000.00 ACFTHRS.

26-Apr-2010 1


AH967213


LATE ENTRY: PMI-2 WAS COMPLETED AT4663.3 ACFT HRS IN SEPTEMBER 2008, NEXTPMI-1 DUE AT 5023.3 ACFT HRS.

27-Apr-2010 1


VZ748391



8.7.DATE

6.REMARKS

4. 5.




PMI-1 COMPLETED AT 5000.0 ACFT HRS, NEXTPMI-2 DUE AT 5360.0 ACFT HRS

28-Apr-2010 1


VZ748391

D CO 214THCOMPLIED WITH REQUIREMENTS OF H-60-10-AMAM-12, IMPROVED DRAG BEAM, AT 5003.0ACFTS HRS.

10-May-2010 1


AH967213


H-60-10-ASAM-08, APU AND APU FIREWALL,COMPLIED WITH THIS DATE AT 5003.7 ACFTHRS, PASSED

18-May-2010 1


VZ748391

D CO 1-214TH AVNGSAB

H-60-10-ASAM-09 NOT APPLICABLE TO THISAIRFRAME

07-Jun-2010 1


JB456660

G 52ND AVNCOMPLIED WITH THE REQUIREMENTS OF H-60-10-SOF-02 ON 22 JUN 2010, 5035.6 ACFT HRS.

22-Jun-2010 1

GAAF, GERMANY 09114

AB644134

G 52 AVNH-60-10-AMAM-16 DOESN'T APPLY. NO CMWSINSTALLED.

25-Jun-2010 1

GAAF, GERMANY 09114

AB644134


APPLIED NEW REVISION OF AWR 1451 R2 DTD25 JUN10, CRASHWORTHY EXTERNAL FUELTANK SYSTEM (CEFS) ON UH/HH-60A/LHELICOPTERS

30-Jun-2010 1


VZ748391


H-60-10-ASAM-10 DOES NOT APPLY TO THISACFT(FUEL BOOST PUMPS)

09-Jul-2010 1


WK439480

D C0 214THCOMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-04 (SAS LINKS) AT 5055.0 ACFT HRS.

15-Jul-2010 1


AH967213

D CO 1-214TH AVNH-60-10-ASAM-11, ALL H-60 SERIES AIRCRAFTCOMMON COMPONENT RETIREMENT CHANGETIMES UPDATE, COMPLIED WITH THIS DATE

30-Jul-2010 1


VZ748391

D CO 214THCOMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-12 @ 5064.2 ACFT HRS.(T700 RC TIMECHANGE)

04-Aug-2010 1


AH967213

D CO 1-214TH AVNAWR 1167, R3 DTD 13 AUG 10, AIRCRAFTASSIGNED TO 1-214TH AVN, APPLIED THISDATE

13-Aug-2010 1


VZ748391

DCO 1-214TH AVN REGTCOMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-15 (FUEL VENT ELBOW)

25-Aug-2010 1


WK439480


APPLIED CECOM SUGGESTED SAFETY WIRETO DUAL AHRU THROUGH LOCK RING OF P-1CONNECTOR

30-Aug-2010 1


JB456660



8.7.DATE

6.REMARKS

4. 5.



D CO 1-214TH AVNH-60-10-ASAM-16 (RESCUE HOIST CABLE CUTHARNESS CONNECTOR) NOT APPLICABLE TOTHIS AIRFRAME AT THIS TIME.

09-Sep-2010 1


JB456660

D CO 1-214TH AVNAPPLIED NEW REVISION OF AWR 1529 R1 DTD07 OCT 10 FOR OPERATION OF THE FIBEROPTIC GYRO SYSTEM CN-1716/A, ATTITUDEHEADING REFERECE UNIT/SET (AHRU/AHRS)IN DUAL CONFIGURATION ON UH/EH/HH-60A/LAIRCRAFT

12-Oct-2010 1


VZ748391


H-60-11-ASAM-02 T/R SERVO COTTER PINVERIFICATION COMPLIED WITH ON THIS DATE

20-Oct-2010 1


JB456660

D CO 1-214TH AVNCOMPLIED WITH H-60-11-AMAM-03 ON THISDATE (OIL COOLER) NOT APPLICABLE TOTHIS AIRFRAME

03-Nov-2010 1


JB456660

DCO 214THLATE ENTRY: H-60-09-ASAM-11, CARGO DOORWINDOW EMERGENCY JETTISON HANDLEASSEMBLY, COMPLIED WITH ON 25 JUNE 2009

30-Nov-2010 1


QC000000

DCO 1-214 AVN REGTH-60-11-ASAM-04 (TACAN RECEIVER BEARINGERROR) COMPLIED WITH @ 5131.0 ACFT HR.ACFT DOES NOT HAVE THIS EQUIPMENTINSTALLED.

02-Dec-2010 1


DG106187

D CO 1-214TH AVNH-60-11-AMAM-04 UNIT SCP-6 LEVELLOGISTICS SYSTEM-AVIATION (ENHANCED)INTEGRATED MATERIEL MANAGEMENTCENTER LEGITIMATE CODE FILE CHANGE 61REQUIREMENTS, COMPLIED WITH THIS DATE

06-Jan-2011 1


VZ748391

D CO 1-214TH AVNH-60-11-AMAM-06 MEDEVAC CAROUSELREFURBISHMENT, COMPLIED WITH THISDATE AT 5150.9 ACFT HRS, CAROUSEL NOTINSTALLED

10-Feb-2011 1


VZ748391


AMMUNITION INFORMATION NOTICE (AIN 080-11)(MH92), A/C HRS CHANGE ON MH92 SHELLLIFE FROM 216 TO 222 MONTHSCHANGE ONMH92 INSTALL LIFE FROM 108 TO 114MONTHS

02-Mar-2011 1



AMMUNITION INFORMATION NOTICE (AIN 080-11)(MH92),COMPLETED@ 5175.4 A/C HRSCHANGE ON MH92 SHELL LIFE FROM 216 TO222 MONTHSCHANGE ON MH92 INSTALL LIFEFROM 108 TO 114 MONTHS

02-Mar-2011 2



LATE ENTRY: H-60-11-ASAM-08 (IFF SAFETY)COMPLIED WITH ON 04 MAR 11 , A/C HRS5168.1

07-Mar-2011 1


D CO 1-214TH AVNCOMPLIED WITH H-60-11-AMAM-09 (2408-19-3)ON THIS DATE

05-May-2011 3


JB456660

D CO 1-214TH AVNCOMPLIED WITH H-60-11-AMAM-11 (AWRREVIEW) ON THIS DATE

05-May-2011 4


JB456660



8.7.DATE

6.REMARKS

4. 5.



D CO 1-214TH AVNCLASS II AIRCRAFT WEIGHING COMPLETEDON THIS DATE JB456660

07-Jun-2011 1


JB456660


COMPLIED WITH H-60-11-ASAM-06 (CYCLICSTOPS) ON THIS DATE

16-Jun-2011 1


JB456660


COMPLIED WITH REQUIREMENTS OF H-60-11-SOF-01 ( DISCREPANT SELF LOCKINGDOUBLE HEXAGON NUTS )

09-Jul-2011 2


JR016225


COMPLIED WITH REQUIREMENTS OF H-60-11-ASAM-13 ( ENG AIR INLET ANTI-ICING/MODULATING VALVE)

11-Jul-2011 1


JR016225


COMPLIED WITH H-60-11-ASAM-14 (ENGCOWLING) ON THIS DATE

12-Jul-2011 1


JB456660


COMPLIED WITH H-60-11-AMAM-20 ON THISDATE.

26-Sep-2011 1



COMPLIED WITH REQUIREMENT SOF H-60-11-AMAM-20 ON THIS DATE.

27-Sep-2011 1


D CO214THCOMPLIED WITH THE REQUIREMENTS OF H-60-12-SOF-01 FOR THE ONE TIME INSPECTIONOF THE INTERMEDIATE GEARBOXCOMPLETED AT 5281.3 ACFT HRS.

11-Oct-2011 1


AH967213

D CO 214THCOMPLIED WITH THE REQUIREMENTS OF H-60-12-SOF-02 FOR THE ONE TIME INSPECTIONOF THE INTERMEDIATE GEARBOXCOMPLETED ON THIS DATE.

11-Oct-2011 2


AH967213


AWR 1694 (DUAL STAB AMP), WAS APPLIEDON THIS DATE.

11-Oct-2011 3


D. CO 1-214TH AVNREGT

COMPLY WITH REQUIREMENTS OF H-60-12-SOF-03 (I/G/B) ON THIS DATE

17-Oct-2011 1


JB456660

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-19 (ULLSA UPDATE 62) ON THIS DATE

01-Nov-2011 1


JB456660

D. CO 1-214COMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-03 TRANSPONDER AND COMMONMISSILE WARNING SYSTEM INSTALLATION.EQUIPMENT NOT INSTALLED ON ACFT.

02-Nov-2011 1


RL172902



8.7.DATE

6.REMARKS

4. 5.



AMCOM/TASM-EACE/CPCE EVALUATION COMPLETED @5340.8 ACFT HRS BY ACE TEAM MEMBER "M"

15-Nov-2011 1


SW233009

TASM E, DYNCORPINTL.

COMPLIED WITH MEC FF136761 @5349 ACHOURS. RH PILOT DOOR POST

21-Nov-2011 1


EC579329

TASM-E DYNCORPINTNL

COMPLIED WITH MEC F136756 @ 5340.8 ACHOURS. LH DOOR POST.

21-Nov-2011 2


EC579329

TASM-ECOMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-17 @ 5340.8 ACFT HRS.

22-Nov-2011 1


EW744892

TASM-ECOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-01 TR OUTPUT BEVEL GEAR NDI, @5340.8 ACFT HRS

23-Nov-2011 1


EW744892


COMPLIED WITH MEC F136968 @5340.8 ACHOURS. LH HIRSS BULKHEAD

28-Nov-2011 1


EC579329

TASM-E, DYNCORPINTL.

COMPLIED WITH THE REQUIREMENTS OF H-60-12-ASAM-02

15-Dec-2011 1


EC579329

TASM-ETAIL ROTOR RIG CHECK COMPLETED IAW WP1052 AT 5340.8 ACFT HRS. PC RODDIMENSIONS ARE RED 5.041-4.711=0.330,BLACK 4.471-4.139=0.332, YELLOW 5.077-4.737=0.340, BLUE 4.452-4.114=0.338. T/RSERVO PISTON TRAVEL IS 3.472 OUT AND0.046 IN. T/R RIG CHECK PERFORMED BYTI:BG856814 AMII: DE743795, RH252603,GG733364

21-Dec-2011 1


BG856814


PMI-2 COMPLETED AT 5340.8 AQCFT HRS,NEXT PMI-1 DUE AT 5700.8 ACFT HRS.

27-Dec-2011 1


EC579329

D CO 1-214TH AVNAWR 1479 R2 DTD 13 JAN 12 FOR UH-60A ANDEH-60A HELICOPTERS WITH MAIN MODULEASSEMBLIES(PART NUMBERS 70351-08100-075 AND 70351-08100-076) EQUIPPED WITHTHE IMPROVED PLANETARY CARRIERASSEMBLY, PART NUMBER 70351-08175-046,APPLIED THIS DATE.

23-Jan-2012 1


LD197314

D CO 1-214TH AVNAWR 1452 R2 DTD 20 JAN 12 FOR ALL UH/HH-60A/L HELICOPTERS EQUIPPED WITH THE LC-6 DIGITAL CHRONOMETER, APPLIED THISDATE.

23-Jan-2012 2


LD197314



8.7.DATE

6.REMARKS

4. 5.



TASM-ETAIL ROTOR RIGG CHECK COMPLETEDAFTER 9-11 HR TORQUE CHECKST/R PITCHCONTROL ROD BIAS= RED: INITIAL 4.6 W/BIAS4.919 DIFF 0.319 BLACK: INITIAL 4.047 W/BIAS4.376DIFF 0.329 YELLOW INITIAL 4.656 W.BIAS4.991 DIFF 0.335 BLUE: INITIAL 4.034 W/BIAS4.363 DIFF 0.329

24-Jan-2012 1


MG003384

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; ISAQ110 R-2 DTD 30 MAR 06 FOR UH-60ALHelicopters Equipped with the Material ValueEngineering (MAVEN) Improved HeatingSystem (Option II Kit)

01-Feb-2012 1


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1159 R-3 DTD 29 JUL 11 FOR Operation of theInfrared Countermeasure Transmitter,T1360C(V)1/ALQ-144C(V), Part NumberA3301520 on UH/HH-60A/L/M Aircraft

01-Feb-2012 2


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1309 R6 DTD 22 APR 11 FOR EH-60A andUH/HH-60A/L/M Helicopters Equipped withOregon Aero Seat Cushions

01-Feb-2012 3


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1348 R6 DTD 17 MAR 11 FOR UH-60A/LHelicopters with the 12 Station Wall MountedIntercommunication System (ICS) or 12 StationVIP Intercom I1 ICS, Auxiliary Communications(Aux Com) Panel and the 8-PointIntercommunication System (ICS) Installed

01-Feb-2012 4


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1529 R2 DTD 7 OCT 11 FOR UH/HH-60A/LHelicopters Equipped with the Attitude HeadingReference Set (AHRS), Dual Attitude HeadingReference Unit (AHRU)

01-Feb-2012 5


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1656 R1 DTD 28 DEC 11 FOR UH/HH-60A/LHelicopters Equipped with the PhoenixModified Drip Pan

01-Feb-2012 6


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1694 DTD 25 FEB 11 for UH/HH-60A/LHelicopters Equipped with the Dual StabilatorController.

01-Feb-2012 7


LD197314

D 1-214 AVNCOMPLIED WITH REQUREMENTS OF H-60-12-SOF-04 MSG DTG 170015Z FEB 12

22-Feb-2012 1


LW849130

D CO 1-214 AVN REGTCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-06 MSG ON THIS DATE

22-Feb-2012 2


RT319476

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1466 DTD 31 AUG 11 R4 FOR THE GARMINGPSMAP 696, 695, 496, 495, 396, 296, OR 295ON US ARMY UH/HH-60A/L/M HELICOPTERS

09-Mar-2012 1


LD197314



8.7.DATE

6.REMARKS

4. 5.



D CO 1-214TH AVNAPPLIED NEW REVISION: AWR 1750 R-1 DTD27MAR12 for Operation of the Aviator's NightVision Imaging System (ANVIS) AN/AVS-6Series Night Vision Goggles (NVG) in UH/HH-60A/L/M Aircraft

28-Mar-2012 1


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1348 R-7 DTD 10 FEB 12 for UH-60AILHelicopters with the 12 Station Wall MountedIntercommunication System (ICS) or 12 StationVIP Intercom II ICS, Auxiliary Communications(Aux Com) Panel and the 8-PointIntercommunication System (ICS) Installed

28-Mar-2012 2


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1309 R7 DTD 10 FEB 12 FOR EH-60A andUH/HH-60A/L/M Helicopters Equipped withOregon Aero Seat Cushions

28-Mar-2012 3


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1513 R3 DTD 26 OCT 11 FOR Use of theIntegrated Performance and AircraftConfiguration (IPAC) Software for PerformancePrediction for UH/HH-60A/L/M Helicopters

28-Mar-2012 4


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1694 R3 DTD 5 JAN 12 for UH/HH-60A/LHelicopters Equipped with the Dual StabilatorController.

28-Mar-2012 5


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1738 DTD 1FEB11 FOR UH-60A/LHELICOPTERS EQUIPPED WITH AN/APX-118COMMON TRANSPONDER (CXP)

28-Mar-2012 6


LD197314

D CO 1-214TH AVNAWR 1348 R-8 DTD 4 MAY 12 for UH-60AILHelicopters with the 12 Station Wall MountedIntercommunication System (ICS) or 12 StationVIP Intercom II ICS, Auxiliary Communications(Aux Com) Panel and the 8-PointIntercommunication System (ICS) Installed

04-May-2012 1


LD197314

D 1-214 AVNCOMPLIED WITH H-60-12-AMAM-09 22-May-2012 1


LW849130

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-12. RESCINDED COMMONCOMPONENTS REMOVAL DATES

20-Jul-2012 1


LD197314

D CO 1-214TH AVNNEW REVISION OF AWR 1348 R-9 DTD 22 JUNE12 for UH-60AIL Helicopters with the 12 StationWall Mounted Intercommunication System (ICS)or 12 Station VIP Intercom II ICS, AuxiliaryCommunications (Aux Com) Panel and the 8-Point Intercommunication System (ICS)Installed

20-Jul-2012 2


LD197314

D CO 1-214TH AVNNEW REVISION OF AWR 1451 R3 DTD 20 JULY12 FOR THE CRASHWORTHY EXTERNAL FUELTANK SYSTEM (CEFS) ON UH/HH-60A/LHELICOPTERS

20-Jul-2012 3


LD197314



8.7.DATE

6.REMARKS

4. 5.




COMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-08

23-Jul-2012 1


RT319476

D CO 1-214TH AVNNEW REVISION AWR 1167 R4 DTD 20 MAR 12for Specified UH-60A/L Helicopters with UNS-1DFlight Management System (FMS), AN/ARC-186Antenna Upgrade, 12 Station ICS Modifications,WX-IOOO+ Stormscope, Auxiliary Heater, VIPInterior Kit, APU Exhaust Deflectors, RollVibration Absorbers, and Passenger StepsInstalled

16-Aug-2012 1


LD197314

1-214TH CADCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-09(RESCUE HOIST CARTRIDGE) ONTHIS DATE

25-Aug-2012 1


JF851776

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-07 (ELECTRICAL WIRING CHAFFE)

17-Sep-2012 1


LD197314

D CO 1-214TH AVNNEW REVISION AWR 1513 R4 DTD 2 JUL 12FOR Use of the Integrated Performance andAircraft Configuration (IPAC) Software forPerformance Prediction for UH/HH-60A/L/MHelicopters

17-Sep-2012 2


LD197314

D CO 1-214THNEW REVISION AWR 1466 DTD 22 AUG 12 R5FOR THE GARMIN GPSMAP 696, 695, 496, 495,396, 296, OR 295 ON US ARMY UH/HH-60A/L/MHELICOPTERS

17-Sep-2012 3


LD197314

D 1-214COMPLIED WITH REQUIRMENTS OF H-60-12-AMAM-15 PITCH TRIM SERVOS

26-Sep-2012 1


LW849130

D 1-214UPDATED AWR 1451 R4 15 OCT 2012 (CEFS)AWR 1513 R4 2 JULY 2012 (IPAC)AWR 1479 R2 13 JAN 2012 (IMPROVEDPLANETARY CARRIER)

13-Nov-2012 1


LW849130

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-09 (HYDRAULIC LINE CHAFFING)

15-Nov-2012 1


RL172902

D. CO 1-214 AVN REGTCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-02 (AHRS PASS)

19-Nov-2012 1


RL172902

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-03 (DEC/EDECU TURBINE GASTEMPERATRE (TGT) BIAS)

29-Nov-2012 1


LD197314

D. CO 1-214 AVNCOMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-01 (ANTI COLL LIGHT)

27-Dec-2012 1


RL172902


LATE ENTRY; UPDATED AWR 1513 R4 TO 1513R5 DTD 27 NOV 2012

10-Jan-2013 1


RT319476



8.7.DATE

6.REMARKS

4. 5.



D CO 1-214TH AVNSAQ 1479 Final Statement of AirworthinessQualification (SAQ) for the ImprovedPlanetaryCarrier Assembly, Part Number 70351-08175-046, for UH-60A and EH-60A Helicopters

22-Jan-2013 1


LD197314

D CO 1-214TH AVNNEW REVISION ; AWR 1452 R3 DTD 18 JAN 13FOR ALL UH/HH-60A/L HELICOPTERSEQUIPPED WITH THE LC-6 DIGITALCHRONOMETER

22-Jan-2013 2


LD197314


COMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-05 (M/L/G WHEEL BRAKE ASSY)

24-Jan-2013 1


RL172902

D. CO 1-214 AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1738 R1BDTD 1FEB13 FOR UH-60A/LHELICOPTERS EQUIPPED WITH AN/APX-118COMMON TRANSPONDER (CXP)

11-Feb-2013 1


RL172902

D CO 1-214TH AVNCOMPLIED WITH H-60-13-AMAM-06 ON THISDATE

12-Feb-2013 1


RT319476

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-04 (ULLS-A(E) AMCOM LOGISTICSCENTER (ALC) LCF CHANGE 63REQUIREMENTS)

28-Feb-2013 1


LD197314

TASM-OMain rotor rig completed @ 5606.7 aircrafthours. Primary servos additional bias:Forward:shorten 3 flatsAft: lengthen 3 flatsLateral:shorten 4 flats

28-Feb-2013 2

WIESBADEN, GERMANY

CM567059

TASM-OTail rotor rig completed at 5606.7 aircraft hours.Bias set as follows: Set InitialAdjust Diff FinalRed: -1.6° 4.706"5.034" 0.328" 3.1°Black: -0.1° 4.081"4.381" 0.300" 3.0°Yellow: -0.4° 4.712"5.022" 0.310" 3.1°Blue: -0.9° 4.043"4.345" 0.302" 3.0°

28-Feb-2013 3

WIESBADEN, GERMANY

CM567059

TASM-OComplied with requirements of H-60-13-AMAM-01, Flight Control Rigging, at 5606.7 aircrafthours.

28-Feb-2013 4

WIESBADEN, GERMANY

CM567059

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-02 ( DRAG BEAM REPLACEMENT )

21-Mar-2013 1

WIESBADEN AAF, APOAE 09058

LD197314

D 1-214 AVNCOMPLIED WITH H-60-13-ASAM-04 25-Mar-2013 1


LW849130

D CO 1-214THCOMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-05

09-Apr-2013 1


JR763273


NEW REVISION AWR 1513 R6 DTD 22 MAR 13FOR Use of the Integrated Performance andAircraft Configuration (IPAC) Software forPerformance Prediction for UH/HH-60A/L/MHelicopters

10-Apr-2013 1


RL172902



8.7.DATE

6.REMARKS

4. 5.




APPLIED NEW REVISION: AWR 1750 R-2 DTD29MAR13 for Operation of the Aviator's NightVision Imaging System (ANVIS) AN/AVS-6Series Night Vision Goggles (NVG) in UH/HH-60A/L/M Aircraft

10-Apr-2013 2


RL172902

D 1-214 AVNCOMPLIED WITH H-13-60-AMAM-07 11-Apr-2013 1


LW849130


COMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-06 ( PMI CHECKLIST CHANGES )

08-May-2013 1


RL172902


LATE ENTRY; UPDATED AWR 1452 TO R4 13-May-2013 1


RT319476


COMPLIED WITH REQUIRMENTS OF H-60-13-SOF-01 (AHRS SAFETY)

06-Jun-2013 1


RL172902


COMPLIED WITH REQUIREMENTS OF GEN-13-AMAM-04 (AN/APN 209 COMPONENTTRACKING)

28-Aug-2013 1


JR763273

D CO 1-214TH AVNNEW REVISION AWR 1466 DTD 27 AUG 13 R6FOR THE GARMIN GPSMAP 696, 695, 496, 495,396, 296, OR 295 ON US ARMY UH/HH-60A/L/MHELICOPTERS

18-Sep-2013 1


LD197314

DCO 1-214 AVNCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-10 (LCF CHANGE 64)

18-Sep-2013 2


DR622530

D CO 1-214TH AVNLATE ENTRY: NEW REVISION AWR 1167 R5DTD 13 FEB 13 for Specified UH-60A/LHelicopters with UNS-1D Flight ManagementSystem (FMS), AN/ARC-186 Antenna Upgrade,12 Station ICS Modifications, WX-IOOO+Stormscope, Auxiliary Heater, VIP Interior Kit,APU Exhaust Deflectors, Roll VibrationAbsorbers, and Passenger Steps Installed

19-Sep-2013 1


LD197314

B-412 ASBCOMPLIED WITH TBO ITEM AFT BELLCRANKSUPPORT @ ACFT HRS 5701

25-Sep-2013 1

COLEMAN AAF,GERMANY

TO702414

BCO 412 ASB QCCOMPLYED WITH H-60-13-AMAM-15 DURRINGPMI1. ( CRASHWORTHY EXTERNAL FUELSYSTEM (CEFS) ) AIRCRAFT IS NOT MODEDFOR CEFS

25-Sep-2013 2

COLEMAN AAF,GERMANY

JS756224

D CO 1-214TH AVNCOMPLIED WITH GEN-13-AMAM-04 ( AN/APN209 RADAR ALTIMETER SET COMPONENTTRACKING)

30-Sep-2013 1


JR763273



8.7.DATE

6.REMARKS

4. 5.



B CO 412 ASBMAIN ROTOR RIG COMPLETED @5701 ACFTHR ( L.C ANGLE AVG -.575) (H.C ANGLE AVG15.275) L.C.A AVG 7.65) ( RT CYCLE ANGLEAVG 2) PRIMARY SERVO CONTROL ROD BIAS(FWD -1 FLAT, AFT +1 FLAT, LAT +2.5 FLATS)TAIL ROTOR BIAS (RED .326, BLUE .338,YELLOW .333, BLACK .332) T/R CABLETENSION ( L/H 155, R/H 155 ) TEMP 19 DEG (ACFT T/R PISTON TRAVEL OUT 3.51 , IN 0.0 )COMPLETED

18-Nov-2013 1

KATTERBACH,GERMANY

TO702414

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-02 HUMS ACCLEROMETERS.

05-Dec-2013 1


JR763273

TASM-O/DYNCORPINTERNATIONAL

ACE/CPC EVALUATION COMPLETED AT ACFTHRS. 5700.6 BY TEAM MEMBER W.CRISP "S"

03-Jan-2014 1

KATTERBACH,GERMANY

WC643445

B CO. 412TH ASBALL H-60 SERIES AIRCRAFT, MAIN ROTOR(MR) HUB ASSEMBLY, H-60-14-ASAM-04COMPLIED WITH BUT SUSPECT, AT ACFTHRS. 5702

03-Jan-2014 2

KATTERBACH,GERMANY


COMPLIED WITH REQUIREMENT OF H-60-14-AMAM-03 (CONNECTING LINK)

06-Jan-2014 1


RT319476


COMPLIED WITH REQUIREMENTS H-60-ASAM-03: (EIBF)

21-Feb-2014 1


JR763273

D CO. 1-214TH AV REGTCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-08 BY 4-JUN-14, (AN/ASC-15ECOMMUNICATION CONSOLE CIRCUITBREAKER PROTECTION)

10-Mar-2014 1


AJ815338

TASM-ORIGHT SIDE BEADED PANEL REPAIRED AT5711.7 AIRCRAFT HOURS IAW TM 1-1520-237-23-6 WP 0398. AIRCRAFT SHOREDINTERNALLY IN LIEU OF DEPOPULATION OFMAIN ROTOR PYLON IAW MEC F180830.

17-Mar-2014 1

WIESBADEN, GERMANY

CM567059

TASM-OENTRY #1 DATED 17-MAR-2014 ENTERED INERROR. BEADED PANEL WAS REPAIRED ON83-23875.

17-Mar-2014 2

WIESBADEN, GERMANY

CM560562


COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-09 BY 25 MAY 14 (MAIN TRANSMISSIONFILTER BOWL AND CHIP DETECTORATTACHMENT HARDWARE)

11-Apr-2014 1


AJ815338

D-CO 1-214TH AVNREGT

COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-10 BY 18 APR 14 (HONTEK COATEDMAIN ROTOR (MR) BLADE REMOVAL) "N/A"

14-Apr-2014 1


JM986195


COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-12 (LIFE EXTENTION OF M/R SPINDLENUT) ON THIS DATE.

22-Apr-2014 1


RS630832



8.7.DATE

6.REMARKS

4. 5.



D CO. 1-214 AVNLATE ENTRY: UPDATED AWR 1159R4 DATED31 JUL 13

25-Apr-2014 1


RO215014

D CO. 1-214 AVNLATE ENTRY: UPDATED AWR 1167R5 DATED31 FEB 13

25-Apr-2014 2


RO215014

D CO. 1-214 AVNUPDATED AWR 1309R8 DATED 14 APR 14 25-Apr-2014 3


RO215014

D CO. 1-214 AVNLATE ENTRY: UPDATED AWR 1466R6 DATED27 AUG 13

25-Apr-2014 4


RO215014

D CO 1-214 AVNLATE ENTRY: UPDATED AWR 1656R2 DATED23 JAN 14

25-Apr-2014 5


RO215014

D CO. 1-214LATE ENTRY: UPDATED AWR 1694R4 DATED 6JAN 14

25-Apr-2014 6


RO215014


COMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-06 (FLIGHT CONTROL MIXERASSEMBLY) ON THIS DATE.

25-Apr-2014 7


RS630832



25-Apr-2014 8


RS630832

25-Apr-2014 9



COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-05 (LCF 65) ON THIS DATE.

06-May-2014 1


RS630832


COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-14 (IVHMS CABLING) ON THIS DATE.NOT INSTALLED.

29-May-2014 1


RS630832


COMPLIED WITH REQUIREMENTS OF H-60-14-SOF-03 ON THIS DATE. INSPECTION PASS.

26-Jun-2014 1


RS630832


COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-16(AHRU) ON THIS DATE

21-Jul-2014 1


BJ963354

D-CO 1-214TH AVN LATE ENTRY: ADDED AWR 1348 R 10 30 APR14

31-Jul-2014 1


JM986195



8.7.DATE

6.REMARKS

4. 5.



D CO 1-214TH AVNREMOVED AWR 1348 R9 22 JUN 12 31-Jul-2014 2


JM986195


ADDED AWR 1513 R7 21 MAY 14 31-Jul-2014 3


JM986195

D CO 1-214TH AVNREMOVED AWR 1513 R6 31-Jul-2014 4


JM986195

D CO 1-214TH AVNADDED AWR 1913 25 OCT 13 (ACN ELETRONICLOGBOOK)

31-Jul-2014 5


JM986195

D CO 1-214TH AVNREMOVED AWR 1648 R 3 (LOGBOOK) 31-Jul-2014 6


JM986195


COMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-09(ENGINE INPUT SHAFTS) ON THISDATE

04-Aug-2014 1


BJ963354


COMPLIED WITH REQUIRMENTS OF H-60-14-ASAM-08 (HMU QUICK DISCONNECT ON THISDATE

05-Aug-2014 1


BJ963354

D CO. 1-214 AVNCOMPLIED WITH H-60-14-SOF-04 (CHECKLIST) 29-Aug-2014 1


RO215014


COMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-10(PLANETARY CARRIER) ON THISDATE

08-Sep-2014 1


BJ963354

AMCOM/TASM-OACE/CPCE PERFORMED AT 5840.4 ACFT.HOURS BY ACE TEAM MEMBERS "A & M".

24-Sep-2014 1


LC735556

D CO. 1-214 AVNCOMPLIED WITH H-60-14-AMAM-19 (LCF 66) 14-Oct-2014 1


RO215014

D CO. 1-214 AVNCOMPLIED WITH H-60-15-AMAM-02 (IVHMSWIRING)

21-Oct-2014 1


RO215014

D CO. 1-214TH AVNREGT.

COMPLIED WITH REQUIREMENTS OF H-60-15-SOF-01. (OIL COOLER FAN AXIAL BEARING)ON THIS DATE.

03-Nov-2014 1


AJ815338


COMPLIED WITH H-60-15-ASAM-01 LEDCAUTION ADVISORY PANEL ON THIS DATE

20-Nov-2014 1


BJ963354



8.7.DATE

6.REMARKS

4. 5.




COMPLIED WITH H-60-15-AMAM-05 (AHRSEMERGENCY PROCEDURES) ON THIS DATE.

12-Dec-2014 1


GM118464


ADDED AWR 1513 R8 DTD 1 DEC 14 30-Dec-2014 1


MN681610


COMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-15 (CEFS R/H FUEL CELL COVERPLATE) ON THIS DATE. INSPECTION FAILEDAND REPAIRS COMPLETED IAW THEADDENDUM. PREVIOUS -15 ENTRY DATE 25SEP 2013 #2 WAS ENTERED IN ERROR. ACFTHAS BEEN MODIFIED WITH MWO 1-1520-237-50-86.

29-Jan-2015 1


RS630832


COMPLIED WITH REQUIREMENTS OF H-60-15-AMAM-06 (IDENTIFICATION OF ASE) ON THISDATE

11-Feb-2015 1


JH103297

CORPUS CHRISTI ARMYDEPOT

AFTER AN AIRCRAFT SHIP TRANSPORT AMTF FOR .5 HOURS ON 07-APR-2015 FROM11:00 TO 11:30 WAS CONDUCTED BY CW2HAYNES, COREY CH311314. THE FLIGHT WASUNABLE TO BE RECORDED USING THESTANDARD METHOD (DA FORM 2408-12), DUETO AN ULLS-A(E) ERROR. DUE TO THISERROR, THE AIRCRAFT HOURS HAVE BEENMANUALLY CHANGED FROM 5874.5 TO5875.0.

01-Jun-2015 1

CORPUS CHRISTI,TEXAS

JL664359

FT HOOD AFMA RASMW

ACE COMPLETED AT 5875 AIRCRAFT HOURSAT FT HOOD TX BY TEAM MEMBERS RR & KI

14-Aug-2015 1

FT HOOD, TX 76544

AS425855

SCIENCE ANDENGINEERINGSERVICES LLC

EFFECTIVE THIS DATE, ACFT TRANSFEREDTO SES, INDUCTED INTO B.E.S.T. PROGRAM

04-Jan-2016 1

HUNTSVILLE

JM866540

SCIENCE ANDENGINEERINGSERVICES, LLC

H-60-15-ASAM-03, TROOP/GUNNER SEATENERGY ATTENUATORS NOT COMPLIED

08-Jan-2016 1

HUNTSVILLE

ED046014


H-60-15-AMAM-10, "AV-DEC GASKETINSPECTION" NOT COMPLIED WITH

08-Jan-2016 2

HUNTSVILLE

ED046014


H-60-15-AMAM-14, ULLS-A(E) LCF CHANGE 67NOT COMPLIED WITH

08-Jan-2016 3

HUNTSVILLE

ED046014



8.7.DATE

6.REMARKS

4. 5.




H-60-15-AMAM-11, MODE–S TRANSPONDERADDRESS REVIEW NOT COMPLIED WITH

08-Jan-2016 4

HUNTSVILLE

ED046014


H-60-15-AMAM-18,(MEDEVAC)CAROUSEL NOTCOMPLIED WITH

08-Jan-2016 5

HUNTSVILLE

ED046014


H-60-15-SOF-02,FRIES RELEASE CABLE NOTCOMPLIED WITH

08-Jan-2016 6

HUNTSVILLE

ED046014

SCIENCE ANDENGINEERINGSERVICES,LLC

H-60-16-ASAM-01 INBOARD RETENTIONPLATE TORQUE CHECKS NOT COMPLIEDWITH

08-Jan-2016 7

HUNTSVILLE

ED046014


H-60-16-AMAM-01 ENGINE INLET BARRIERFILTER FRAMES NOT COMPLIED WITH

08-Jan-2016 8

HUNTSVILLE

ED046014


H-60-16-AMAM-03, “PERSONNEL LOCATORSET REMOVAL" NOT COMPLIED WITH

08-Jan-2016 9

HUNTSVILLE

ED046014


H-60-16-AMAM-04, T-CLIP INSTALLATION NOTCOMPLIED WITH

08-Jan-2016 10

HUNTSVILLE

ED046014


H-60-16-ASAM-02, DEFECTIVE FUEL HOSESNOT COMPLIED WITH

08-Jan-2016 11

HUNTSVILLE

ED046014


Report Date: 08-Jan-2016 1/4

8323869HELICOPTER, UTILITY UH-60A

7. FREQUENCY 4.

5. ITEMS TO BE INSPECTED

2. MODEL 3. SERIAL NUMBER 1. NOMENCLATURE

8. NEXTNO DUE 6. REFERENCE 9. COMPLETED AT

INSP

A022 03 Mar 201514TM 1-1520-237-23-914 DAY FLYABLE STORAGEENGINE RUN UP

17 Feb 2015D

A092 14 Mar 201530TM 11-6140-203-23&P30 DAY SLAB BATTERYINSPECTION (D8565/11-1)

12 Feb 2015D

A100 21 Mar 201530DA PAM 738-751#1 ENGINE HISTORY RECORDERREADING DUE

19 Feb 2015D


19 Feb 2015D

A103 15 Mar 201530TM 1-1500-344-23AIRCRAFT WASH DUE 13 Feb 2015D

A110 5896.940TM 1-1520-237-PMSPMS 40 HOUR INSPECTION 5856.9H

A115 15 Mar 201530TM 1-1520-237-23-12LUBE REQUIRMENTS 13 Feb 2015D

A115 591140TM 1-1520-237-23-12LUBE REQUIRMENTS 5871H

A116 6200.4360H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

5840.4H

A116 02 Oct 201512H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

02 Oct 2014M

A117 6200.4360H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 5840.4H

A117 02 Oct 201512H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 02 Oct 2014M

A160 17 May 201590TM 1-1520-237-23-1290 DAY CORROSIONINSPECTION

16 Feb 2015D

A177 16 Mar 201590AR 95-190 DAY REVIEW/UPDATE OF 365-4 ENTRIES

16 Dec 2014D

A210 5936.9120TM 1-1520-237-23-12120 HOUR INSPECTIONREQUIREMENTS

5816.9H

A211 6200.4360H-60-10-AMAM-11APU OIL SAMPLE 5840.4H

A211 02 Oct 201512H-60-10-AMAM-11APU OIL SAMPLE 02 Oct 2014M

A213 5936.9120TM 1-2840-248-23ENGINE COMPRESSORCLEANING

5816.9H

A214 5936.9120TM 1-1520-237-23-12CLEAN TAIL WHEEL ADAPTER 5816.9H

A222 09 Jun 2015360TM 1-1680-377-13&PAMSS SURVIVAL KITINSPECTION

14 Jun 2014D

A227 27 Mar 2015120TM 1-1520-237-23-12INSP/CLEAN EJECTOR RACKSMAU-40A, BRU-22A/A

27 Nov 2014D

A230 12 Mar 2015120MWO 1-1520-237-50-77INSPECT BATTERYCOMPARTMENT FORCORROSION (SLAB)

12 Nov 2014D

A295 6060.6360TM 1-1520-237-23-12STABILATOR ACTUATOR ASSYLUBE

5700.6H

A296 6060.6360TM 1-1520-237-23-12STABILATOR INSPECTION 5700.6H

For use of this form, see DA PAM 738-751; the proponent agency is DCSLOGDA FORM 2408-18, NOV 91, MAY BE USED

DA FORM 2408-18 E, OCT 97 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



7. FREQUENCY 4.




INSP

A298 6215.3360TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 5855.3H

A298 22 Nov 201512TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 22 Nov 2014M

A299 6215.3360TM 1-1520-237-23-12SWASHPLATE LUBE 5855.3H

A299 22 Nov 201512TM 1-1520-237-23-12SWASHPLATE LUBE 22 Nov 2014M

A320 6060.6360TM 1-2840-248-23ENGINE INSPECTION &CLEANING

5700.6H

A400 6420.6720TM 1-1520-237-PMIPMI-1 5700.6H

A401 6060.8720TM 1-1520-237-PMIPMI-2 5340.8H

A408 6060.8720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-2, AREA 5 AND 6)

5340.8H

A410 6420.6720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-1, AREA 1 THRU 4)

5700.6H

A415 6331.8720H-60-10-AMAM-11MAIN GEARBOX OIL SAMPLE-PART # 073, 074, 076

5611.8H

A440 6060.8720TM 1-1520-237-23-12CLEAN TAIL WHEEL LOCKPIN 5340.8H

A450 6060.8720TM 1-1520-237-23-1CLEAN HSS PNEUMATIC CHECKVALVE

5340.8H

A470 6840.81500TM 1-1520-237-23-12REPLACE NUMBER TWOCROSSFEED VALVE

5340.8H

A471 7500.82160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (FWD)

5340.8H

A472 7500.82160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)

5340.8H

A473 7500.82160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (AFT)

5340.8H

A476 100005000TM 1-1520-237-23-12REPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS

5000H

A477 100005000TM 1-1520-237-23-12REPLACEMENT OF STABILATORACTUATOR BOLTS

5000H

A480 100005000TM 1-1520-237-23-12REPLACE PIVOT BOLT 70400-08159-101,102,103,104

5000H

A485 100005000TM 1-1520-237-23-12REPLACE BELLCRANK BOLT70400-08159-105,106,107,108

5000H

A496 04 Aug 20156TM 1-1500-204-23-1CF3BR FIRE EXTINGUISHERWEIGHT TEST & INSPECTION

04 Feb 2015M

A501 11 Jun 20156TM 1-1520-237-23-12MAIN ROTOR BLADE PRESSURECHECK

11 Dec 2014M

A502 07 May 20156TM 1-1520-237-23-12INSPECT AND TEST GROUNDRECEPTACLE IAW TM 1-1500-204-23

07 Nov 2014M

A530 20 Feb 201612DA PAM 738-751AIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)

20 Feb 2015M






7. FREQUENCY 4.




INSP

A532 04 Feb 201612TM 1-1500-204-23-4COMPASS SWING / RMI 04 Feb 2015M

A533 07 Aug 201512TM 1-1520-237-23-12PITOT STATIC SYSTEMINSPECTION

07 Aug 2014M

A534 27 Jun 201624TM 1-1500-204-23-1FIRST AID KIT INSPECTION 27 Jun 2014M

A538 06 Feb 201612TM 1-1520-237-23-12FAT/OAT GAUGEINSPECTION/TEST

06 Feb 2015M

A541 04 Aug 201512TM 1-1520-237-23, C4REPLACE DIGITAL CLOCKBATTERY

04 Aug 2014M

A553 25 Jul 201512AR 95-1AIRCRAFT WEIGHINGINVENTORY (365-1)

25 Jul 2014M

A571 01 Jan 201860TM 1-1520-237-23-1REPLACE EJECTOR RACKCARTRIDGES, DODIC MD66

01 Jan 2013M

A580 11 Dec 201524TM 11-6140-203-23&PRETURN SLAB TO AVIM FORCAPACITY CHECK (VEREY 24MONTH)

11 Dec 2013M

A621 28 Jun 201524AR 95-1AIRCRAFT WEIGHING CLASS 2 28 Jun 2013M

A625 11 Feb 201860TM 11-6140-203-23&PREPLACEMENT OF SLABBATTERY (SLAB)

11 Feb 2013M

A630 01 Feb 2022114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 Aug 2012M

A633 01 Feb 2022114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 Aug 2012M


01 Aug 2012M


01 Aug 2012M

A648 29 Jul 2023180TM 1-1520-237-23REPLACE T/R SPRING CAPSULEASSY

29 Jul 2008M

A660 01 Feb 201972TB 9-1300-385REPLACE THRUSTEREMERGENCY RELEASE CARGOHOOK, MJ20

01 Feb 2013M

A665 22 Apr 201748H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215

22 Apr 2013M

A670 25 Apr 201848TM 1-1520-237-23-1CABIN TUB INSPECTION 25 Apr 2014M

A673 25 Apr 201748TM 1-1520-237-23-12FUEL CELL CORROSIONINSPECTION

25 Apr 2013M

A675 18 Feb 201748TM 1-1520-237-23-12FLIGHT CONTROL ROD INSP 18 Feb 2013M

A695 6060.8720H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

5340.8H

A695 22 Apr 201848H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

22 Apr 2014M

A755 90009000H-60-10-ASAM-11PC LINK TO SWASHPLATEBOLTS REPLACEMENT

0H






7. FREQUENCY 4.




INSP

E004 09 Mar 201514TM 11-5865-200-12AN/ALQ-144 INSPECTION 23 Feb 2015D

E011 19 Mar 201530TM 9-1095-206-12PDISPENSER GENERAL PURPOSEM130

17 Feb 2015D

E015 02 May 2015180MWO 1-1520-237-50-92ASN 128D DOPPLER GPSBATTERY REPLACEMENT

03 Nov 2014D

E041 23 Aug 201430TM 11-5895-294-12TRANSPONDER MODE 4 CHECK 24 Jul 2014D

E088 15 Mar 201530TM 11-5865-200-12AN/ALQ-144 MONTHLYINSPECTION DUE

13 Feb 2015D

E090 21 Mar 201530GEN-MIM-00-001ALQ-144 HOUR METER READING 19 Feb 2015D

E135 28 Aug 20156TM 11-5821-333-12AN/ARC-201(V) SINCGARSRADIO HUB BATT REPL

28 Feb 2015M

E155 02 May 2015180TM 11-5810-262-23KY-58 BATTERY REPLACEMENT 03 Nov 2014D

E351 26 Jun 20156TM 11-5895-1841-13PREPLACE APX-118TRANSPONDER BATTERY

26 Dec 2014M




08-Jan-2016

T700-GE-700ENGINE ASSY, TURBINE

ALT ETFACT TTV°CTIMENUMBERNG %PRESSFATENGINESERIAL 866 +/- 49. TORQUE10.8.7.6.AIRCRAFT REMARKS11. TGTDATE 12.5.4.

GE-E-307338

3. ENGINE SERIAL NUMBER2. ENGINE MODEL1. NOMENCLATUREReport Date: Page 1 of 1

18-May-2010 8323869 MAX POWER FORINSTALLATION

5000 107 106 197.523985 847

03-Jan-2012 8323869 POST PMI 2 MAX PWR4000 111 110 197.313983 845

04-Feb-2014 8323869 POST PMI5000 106 107 0.9998.124640 846

12-Dec-2008 8724642 POST PMI - 2 ENGINEREPLACEMENT

6000 108 105 199.1-63696 846

10-Jun-2009 8724642 RE-ESTABLISHEDBASELINE

5000 105 103 196.983798 847


T700 SERIES TURBINE ENGINE ANALYSIS CHECK RECORDDA FORM 2408-19-2 E, DEC 91

Page of

1. NOMENCLATURE 2. ENGINE MODEL 3. ENGINE SERIAL NUMBER

4. 6. 7. 8. 9.PRESS

ALT

10. 11. 12.5. TORQUEENGINETIME

AIRCRAFTSERIAL NUMBER

FAT TGTDATE REMARKSNG%o. +_C 866 4ACT TTV ETF

DA FORM 2408-19-2, DEC 1991 T700 SERIES TURBINE ENGINE ANALYSIS CHECK RECORDFor use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD LC v1.00

4. 6. 7. 8. 9. 10. 11. 12.5. TORQUEENGINETIME


FAT PRESSALT

TGTDATE REMARKSNG%o. +_C 866 4ACT TTV ETF

APD LC v1.00REVERSE OF DA FORM 2408-19-2, DEC 1991

h

CONDITION ITEMS

kjifdcba g.

RMVL HR

RMVL HRSWUC HRS)COMPO/H

NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE

SINCEPREVSER NO.ANDNOMENCLATURE DUE

REPLACE

INST HRSTIMEINST HRSNO.COMPONENTPNCOMP REP.O/H ORNOMEN6.

3. PART NUMBER ORMODEL

2. NSN 4. SERIAL NUMBER 5. WUC1. NOMENCLATURE

Report Date: 1/1208-Jan-2016

83238691520010350266 00HELICOPTER, UTILITY

156001113021502C12D

00UNK386970219-05001-044TAIL CONE FITTING CCCC COND COND

162001231183103A01 2

51885701C0010188570250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001231183103A01 1

05701IA0122370250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001421089003B01 TAIL

04600G002-0131270250-13101-044SHOCK ABSORBER (TAIL) CCCC COND COND

165001285302405A01Z BLUE

26205000A106-0415170106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z

21625840A1060553870106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z RED

5405000R106-0157270106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z BLACK

10575843R1060346270106-08100-046DAMPER ASSY, M/R CCCC COND COND

531501537465205A02H BLUE LEAD

04663B9410956370103-08108-041SOLID BLADE PIN CCCC COND COND

531501537465205A02H YELLOW LAG


531501537465205A02H YELLOW LEAD


531501537465205A02H RED LEAD


531501537465205A02H BLACK LEAD


531501537465205A02H RED LAG


531501537465205A02H BLUE LAG


531501537465205A02H BLACK LAG


161501199764605A03A M/R

47555000MSU4570104-08000-050SWASHPLATE ASSY CCCC COND COND

161501078571806A11 NO.1

0831A258-0220270351-08080-043ACCESSORY MODULE CCCC COND COND

161501078571806A11 RIGHT


For use of this form, see DA PAM 738-751; the proponet agency is DCSLOGEDITION MAY 67 IS OBSOLETE

DA FORM 2408-16-E, OCT 91 AIRCRAFT COMPONENT HISTORICAL RECORD

h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






161501503311506A XMSN

22484936A2650012670351-08100-076MAIN TRANSMISSIONMODULE

CCCC COND COND

161501230621806E NO.1

0831A264-0242870351-08001-046INPUT MODULE CCCC COND COND

161501353382506E RIGHT


168001074515206F

01493A005-0059270357-06300-042INTERMEDIATE GEARBOX CCCC COND COND

161501376508906G01

28105103A006-0048270358-06600-046TAIL ROTOR GEARBOXASSY

CCCC COND COND

161501524780506H04 NO.1

05000C845-0231770361-08014-041DRIVESHAFT ASSYENGINE

CCCC COND COND

161501524780506H04 NO.2


CCCC COND COND

161501081277506H06 1

39553955A271-0060470361-03001-045SHAFT ASSY, T/R DRV SEC1

CCCC COND COND

161501158951706H08 2

04465WG9991-0003470361-03009-047SHAFT ASSY, T/R DRV SEC2

CCCC COND COND

161501082650006H09

39553955A272-0167870361-05001-045SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501082650006H09


CCCC COND COND

161501082650006H09


CCCC COND COND

161501083295306H11


CCCC COND COND

161501277910606H12


CCCC COND COND

432001136211807A01 NO.1

04214K5002ABR53023-05PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01

13315352208826ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01 NO.2

03696270865A70652-02300-050PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

481001102247307B05A

05748125623213850-3-1VALVE, SOLENIOD CCCC COND COND

481001102247307B05A NO.1

03696P13543213850-3-1VALVE, SOLENIOD CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






165001084309607B11 REAR CABIN

03696B401-0097570651-03201-102ACCUMULATOR CCCC COND COND

168001342049608B20 CO-PILOT

03696330570450-01043-124PANEL INDICATOR (PDU) CCCC COND COND

168001342049608B20 PILOT


611501114969609A01 2

05663114A213228B302-8-DMGENERATOR CCCC COND COND

611501114969609A01 #1

036961120E70550-02031-111GENERATOR CCCC COND COND

161501260074911C21

05379TMD0464374815

70400-02300-046MIXER ASSEMBLY CCCC COND COND

168001261204411D25

28795341B292-0220470400-06641-117STABILATOR ACTUATOR CCCC COND COND

168001261204411D25 LOWER

045830823DL2155M20STABILATOR ACTUATOR CCCC COND COND

599601316274311D26 LEFT

354755473437A70902-02001-048STABILATOR AMPLIFIER CCCC COND COND

599601316274311D26 RIGHT

41955547S1120AB70902-02001-048STABILATOR AMPLIFIER CCCC COND COND

299501496368615A04 ESU

580548806374504587ENGINE SEQUENCINGUNIT

CCCC COND COND

584101245909119E05A 1

057282772KK/NHG7209AC01RECEIVER-TRANSMITTERRADAR

CCCC COND COND

584101245909319E05C

056651895FFA3060591INDICATOR HEIGHT CCCC COND COND

660501503528419E06A 1

057941517765100-20ATTITUDE HEADINGREFERENCE UNIT

CCCC COND COND

661001490516852A

050003404825050-1-001AUTOMAT FLT CONTCOMPUTER

CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






SIGNIFICANT HISTORICAL EVENTS7.




kjigfdcbaRMVL HR RMVL HRS

NOMEN HRS)COMPO/HO/HLOCATIONNSNWUC

he (ACFTLIFESINCEPRESER NO.ANDAND

INST HRSP/N DUEREPLACE

INST HRSTIMENO.COMPONENTNOMENCLATURE

NOMEN REP.O/H OCOMP6.

4. SERIAL NUMBER3. PART NUMBER OR MODEL2. NSN 5. WUC1. NOMENCLATUR

Report Date:

TIME CHANGE COMPONENTS5/1208-Jan-2016

00

156001081924402C15J20000

UNK3869 0070209-06051-043TAIL PYLON FITTING 0020000

161501481695305A01A UH-60A6733

A308-00453 3303493670070-10046-055HUB, M/R ROTOR ASSY 005100

161501442692605A01I RED12055

A001-03313 608466370102-08200-069MAIN ROTOR SPINDLEASSY

008000

161501442692605A01I BLACK12936


008000

161501442692605A01I BLUE13120

D001-11244 0512070102-08200-069MAIN ROTOR SPINDLEASSY

008000

161501442692605A01I YELL13341

D00112447 0534170102-08200-069MAIN ROTOR SPINDLEASSY

008000

161501074515105A01L12117

C286-00095 6819493670351-08186-043MAIN ROTOR SHAFTEXTENDER

0014000

161501127738805A01T13000

015152-0552 5062506270107-08400-046BIFILAR, M/R ROTORASSY

0013000

161501106190305A0213925

A007-13990 795512070150-09100-043MAIN ROTOR BLADEASSY

009600

161501106190305A0213925


009600

161501106190305A029629

A00700708 5312534170150-09100-043MAIN ROTOR BLADEASSY

009600

161501106190305A0211172


009600

161501113818805B0212685

A009-03983 2656534170101-31000-043TAIL ROTOR BLADEASSY

0010000

161501113818805B0211346

A00902802 3865521170101-31000-043TAIL ROTOR BLADEASSY

0010000

161501083681206G01B12718

B25700146 4282500070102-11101-042O/B RETENTION PLATE(T/R)

0012000

414101329342806H236787

C512-00281SB 2994446570361-03005-107FAN AXIAL 19812520

156001129125607A24 YAW14278

B112-05156 3658493670410-02500-049SAS ACTUATOR 0013000

156001129125607A24 ROLL14907

B112-10295 507241470410-02500-049SAS ACTUATOR 0013000

156001129125607A24 PITCH17194

C112-01186 806500070410-02500-049SAS ACTUATOR 0013000

For use of this form, see DA PAM 738-751; The proponet agency isDCSLOG

EDITION MAY 67 IS OBSOLETE

AIRCRAFT COMPONENT HISTORICALRECORD

DA FORM 2408-16-E, OCT 91









Report Date:


00

161501141753211C236823

233-04095 0466370400-06100-042TAIL ROTOR PITCHCHANGE SHAFT

002160

165001305695411C2519989

B300-02142 71257012227000-17TAIL ROTOR SERVOASSY

0015000

165001143122611D01 AFT28159

B30311458B 19425701274000-1031MAIN ROTOR PRIMARYSERVO

0024400

165001143122611D01 LATERAL25695

B30301576B 3368466370410-02820-054MAIN ROTOR PRIMARYSERVO

0024400

165001143122611D01 FWD24735


0024400

156001158968511D0413000

C345-03139 5702570270400-08102-045AFT BELLCRANK 0013000

156001082921311D0517000

A391-00620 0070400-08112-044AFT TIE ROD SUPTFITTING

0017000

168001164416011D066155

A392-00377 0395570400-08111-042AFT TIE ROD ASSY 002200

156001286887011D0710101

39001917 0570170400-08117-049AFT BELLCRANK SPTASSY

004400

304001287243811D0815936

015152-00790 0493670400-08151-061LATERAL SWASHPLATELINK

0011000

168001221286311D0924663

F337-02977 0466370400-08166-041LATERAL SERVOBELLCRANK

0020000

168001158965311D1111000

B346-00735 5062506270400-08104-048AFT WALKING BEAM 0011000

156001158947511D1313820

E344-01303 3937375770400-08115-045LEFT TIE ROD 0014000

156001296948611D148163

33325-61 0466370400-08114-051RIGHT TIE ROD ASSY 003500

168001158965211D1519663

632 0466370400-08101-046FORWARD BELLCRANK 0015000

156001221261911D1610263

B36704490 0466370400-08162-042FWD BELLCRANK SPTASSY

005600













Report Date:


00






ji kgfdcbaRMVL HRSRMVL HRSCOMPO/HNOMENWUC

HRS)O/HLOCATIONNSN

AND he SINCELIFE (ACFT

PREVSER NO. OAND

NOMENCLATURE PN TIMEINST HRS DUEREPLACE

INST HRSNO.COMPONENTNOMEN REP.O/H ORCOMP6.

1520010350266HELICOPTER,UTILITY

UH-60A 8323869 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 8 of 12

08-Jan-2016

COND COND

156001113021502C12D

00TAIL CONE FITTING UNK386970219-05001-044 CCCC

20000 20000

156001081924402C15J

00TAIL PYLON FITTING UNK386970209-06051-043 00

COND COND

1620012311831 203A01

51885701FWD FIXED GEARSHOCK

C0010188570250-12051-045 CCCC

COND COND

1620012311831 103A01


IA0122370250-12051-045 CCCC

COND COND

1620014210890 TAIL03B01

04600SHOCK ABSORBER(TAIL)

G002-0131270250-13101-044 CCCC

5100 6733

1615014816953 UH-60A05A01A

33034936HUB, M/R ROTOR ASSY A308-0045370070-10046-055 00

8000 12055

1615014426926 RED05A01I

6084663MAIN ROTOR SPINDLEASSY

A001-0331370102-08200-069 00

8000 12936

1615014426926 BLACK05A01I


A001-0610870102-08200-069 00

8000 13120

1615014426926 BLUE05A01I


D001-1124470102-08200-069 00

8000 13341

1615014426926 YELL05A01I


D0011244770102-08200-069 00

14000 12117

161501074515105A01L

68194936MAIN ROTOR SHAFTEXTENDER

C286-0009570351-08186-043 00

13000 13000

161501127738805A01T

50625062BIFILAR, M/R ROTORASSY

015152-055270107-08400-046 00

COND COND

1650012853024 BLUE05A01Z

26205000DAMPER ASSY, M/R A106-0415170106-08100-046 CCCC

COND COND

165001285302405A01Z

21625840DAMPER ASSY, M/R A1060553870106-08100-046 CCCC

COND COND

1650012853024 RED05A01Z

5405000DAMPER ASSY, M/R R106-0157270106-08100-046 CCCC

COND COND

1650012853024 BLACK05A01Z

10575843DAMPER ASSY, M/R R1060346270106-08100-046 CCCC

9600 13925

161501106190305A02

7955120MAIN ROTOR BLADEASSY

A007-1399070150-09100-043 00

9600 13925

161501106190305A02


A007-1399170150-09100-043 00

9600 9629

161501106190305A02


A0070070870150-09100-043 00

9600 11172

161501106190305A02


A0070344170150-09100-043 00

COND COND

5315015374652 BLUE LEAD05A02H

04663SOLID BLADE PIN B9410956370103-08108-041 CCCC

EDITION MAY 67 IS OBSOLETE For use of this form, see DA PAM 738-751; the proponet agency is DCSLOG

AIRCRAFT COMPONENT HISTORICAL RECORDDA FORM 2408-16 E, OCT 91


HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 9 of 12

08-Jan-2016

COND COND

5315015374652 YELLOW LAG05A02H


COND COND

5315015374652 YELLOW LEAD05A02H


COND COND

5315015374652 RED LEAD05A02H


COND COND

5315015374652 BLACK LEAD05A02H


COND COND

5315015374652 RED LAG05A02H


COND COND

5315015374652 BLUE LAG05A02H


COND COND

5315015374652 BLACK LAG05A02H


COND COND

1615011997646 M/R05A03A

47555000SWASHPLATE ASSY MSU4570104-08000-050 CCCC

10000 12685

161501113818805B02

26565341TAIL ROTOR BLADEASSY

A009-0398370101-31000-043 00

10000 11346

161501113818805B02


A0090280270101-31000-043 00

COND COND

1615010785718 NO.106A11

0831ACCESSORY MODULE A258-0220270351-08080-043 CCCC

COND COND

1615010785718 RIGHT06A11


COND COND

1615015033115 XMSN06A

22484936MAIN TRANSMISSIONMODULE

A2650012670351-08100-076 CCCC

COND COND

1615012306218 NO.106E

0831INPUT MODULE A264-0242870351-08001-046 CCCC

COND COND

1615013533825 RIGHT06E


COND COND

168001074515206F

01493INTERMEDIATEGEARBOX

A005-0059270357-06300-042 CCCC

COND COND

161501376508906G01

28105103TAIL ROTOR GEARBOXASSY

A006-0048270358-06600-046 CCCC

12000 12718

161501083681206G01B

42825000O/B RETENTION PLATE(T/R)

B2570014670102-11101-042 00

COND COND

1615015247805 NO.106H04

05000DRIVESHAFT ASSYENGINE

C845-0231770361-08014-041 CCCC

COND COND

1615015247805 NO.206H04


C845-0232670361-08014-041 CCCC

COND COND

1615010812775 106H06

39553955SHAFT ASSY, T/R DRVSEC 1

A271-0060470361-03001-045 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 10 of 12

08-Jan-2016

COND COND

1615011589517 206H08


WG9991-0003470361-03009-047 CCCC

COND COND

161501082650006H09

39553955SHAFT ASSY, T/R SEC3,4,5

A272-0167870361-05001-045 CCCC

COND COND

161501082650006H09


A272-0169370361-05001-045 CCCC

COND COND

161501082650006H09


A272-0169470361-05001-045 CCCC

COND COND

161501083295306H11


A273-0056570361-05002-045 CCCC

COND COND

161501277910606H12


A274-0053070361-06002-044 CCCC

2520 6787

414101329342806H23

29944465FAN AXIAL C512-00281SB70361-03005-107 1981

COND COND

4320011362118 NO.107A01

04214PUMP MODULE ASSY,HYDRAUL

K5002ABR53023-05 CCCC

COND COND

432001207722807A01


208826ABR53023-06 CCCC

COND COND

4320012077228 NO.207A01


270865A70652-02300-050 CCCC

13000 14278

1560011291256 YAW07A24

36584936SAS ACTUATOR B112-0515670410-02500-049 00

13000 14907

1560011291256 ROLL07A24

5072414SAS ACTUATOR B112-1029570410-02500-049 00

13000 17194

1560011291256 PITCH07A24

8065000SAS ACTUATOR C112-0118670410-02500-049 00

COND COND

481001102247307B05A

05748VALVE, SOLENIOD 125623213850-3-1 CCCC

COND COND

4810011022473 NO.107B05A

03696VALVE, SOLENIOD P13543213850-3-1 CCCC

COND COND

1650010843096 REAR CABIN07B11

03696ACCUMULATOR B401-0097570651-03201-102 CCCC

COND COND

1680013420496 CO-PILOT08B20

03696PANEL INDICATOR (PDU) 330570450-01043-124 CCCC

COND COND

1680013420496 PILOT08B20


COND COND

6115011149696 209A01

05663GENERATOR 114A213228B302-8-DM CCCC

COND COND

6115011149696 #109A01

03696GENERATOR 1120E70550-02031-111 CCCC

COND COND

161501260074911C21

05379MIXER ASSEMBLY TMD046437481570400-02300-046 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 11 of 12

08-Jan-2016

2160 6823

161501141753211C23

04663TAIL ROTOR PITCHCHANGE SHAFT

233-0409570400-06100-042 00

15000 19989

165001305695411C25

7125701TAIL ROTOR SERVOASSY

B300-021422227000-17 00

24400 28159

1650011431226 AFT11D01

19425701MAIN ROTOR PRIMARYSERVO

B30311458B274000-1031 00

24400 25695

1650011431226 LATERAL11D01


B30301576B70410-02820-054 00

24400 24735

1650011431226 FWD11D01


B30304377B70410-02820-054 00

13000 13000

156001158968511D04

57025702AFT BELLCRANK C345-0313970400-08102-045 00

17000 17000

156001082921311D05

00AFT TIE ROD SUPTFITTING

A391-0062070400-08112-044 00

2200 6155

168001164416011D06

03955AFT TIE ROD ASSY A392-0037770400-08111-042 00

4400 10101

156001286887011D07

05701AFT BELLCRANK SPTASSY

3900191770400-08117-049 00

11000 15936

304001287243811D08

04936LATERAL SWASHPLATELINK

015152-0079070400-08151-061 00

20000 24663

168001221286311D09

04663LATERAL SERVOBELLCRANK

F337-0297770400-08166-041 00

11000 11000

168001158965311D11

50625062AFT WALKING BEAM B346-0073570400-08104-048 00

14000 13820

156001158947511D13

39373757LEFT TIE ROD E344-0130370400-08115-045 00

3500 8163

156001296948611D14

04663RIGHT TIE ROD ASSY 33325-6170400-08114-051 00

15000 19663

168001158965211D15

04663FORWARD BELLCRANK 63270400-08101-046 00

5600 10263

156001221261911D16

04663FWD BELLCRANK SPTASSY

B3670449070400-08162-042 00

COND COND

168001261204411D25

28795341STABILATOR ACTUATOR B292-0220470400-06641-117 CCCC

COND COND

1680012612044 LOWER11D25

04583STABILATOR ACTUATOR 0823DL2155M20 CCCC

COND COND

5996013162743 LEFT11D26

35475547STABILATOR AMPLIFIER 3437A70902-02001-048 CCCC

COND COND

5996013162743 RIGHT11D26

41955547STABILATOR AMPLIFIER S1120AB70902-02001-048 CCCC

COND COND

2995014963686 ESU15A04


06374504587 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 12 of 12

08-Jan-2016

COND COND

5841012459091 119E05A

05728RECEIVER-TRANSMITTER RADAR

2772KK/NHG7209AC01 CCCC

COND COND

584101245909319E05C

05665INDICATOR HEIGHT 1895FFA3060591 CCCC

COND COND

6605015035284 119E06A

05794ATTITUDE HEADINGREFERENCE UNIT

1517765100-20 CCCC

COND COND

661001490516852A

05000AUTOMAT FLT CONTCOMPUTER

3404825050-1-001 CCCC

7. SIGNIFICANT HISTORICAL DATA




HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 C00101885 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

08-Jan-2016

9000 9513

165001125090703A01A

41504150PISTON, MAIN L/GEARSTR

P0211770250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 IA01223 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

08-Jan-2016

9000 14701

165001125090703A01A

00MAIN SHOCK STRUTPISTON

IA0711870250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615014426926MAIN ROTORSPINDLE ASSY

70102-08200-069 A001-03313 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

08-Jan-2016

COND COND

3110011589607 RED05A01I02C

18462222THRUST BEARING B32528199SB7002-048 CCCC

COND COND

1615011614373 RED05A01I02

15891965SPHERICAL BEARINGASSY

B324-20142SB7001-048 CCCC

13000 17055

5310011269444 RED05A01I04

608608M/R SPINDLE NUT C479-0867570102-08105-102 RCRC

8000 12055

5306014606020 RED05A01I06

608608TIE ROD (M/R SPINDLE) B504-0353738023-10372-101 RCRC

20000 24055

1615012149140 RED05A01I07

492492HORN ASSEMBLY A2411365470102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

COND COND

3110011589607 BLACK05A01I02C


COND COND

1615011614373 BLACK05A01I02

608608ELASTOMERIC BEARING B324-26099SB7001-048 CCCC

13000 17936

5310011269444 BLACK05A01I04

00M/R SPINDLE NUT C4791208070102-08105-102 RCRC

8000 12936

5306014606020 BLACK05A01I06

00TIE ROD (M/R SPINDLE) C5040278438023-10372-101 RCRC

20000 24936

1615012149140 BLACK05A01I07

00HORN ASSEMBLY E241-0016470102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-069 D001-11244 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

08-Jan-2016

COND COND

3110011589607 BLUE05A01I02C


COND COND

1615011614373 BLUE05A01I02


C324-07855SB7001-048 CCCC

13000 18120

5310011269444 YELLOW05A01I04

00M/R SPINDLE NUT F479-0364670102-08105-102 RCRC

8000 13120

5306014606020 YELLOW05A01I06

00TIE ROD (M/R SPINDLE) C504-0983238023-10372-101 RCRC

20000 25120

1615012149140 BLUE05A01I07

00HORN ASSEMBLY G2410127870102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-069 D00112447 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

08-Jan-2016

COND COND

3110011589607 YELL05A01I02C


COND COND

1615011614373 YELLOW05A01I02


B324-18819SB7001-048 CCCC

13000 18341

531001126944405A01I04

00M/R SPINDLE NUT F4790530270102-08105-102 RCRC

8000 13341

530601460602005A01I06


20000 25341

161501214914005A01I07






HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70150-09100-043 A007-13990 05A024. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

08-Jan-2016

COND COND

1560014479774 BLUE05A02E

00M/R BLADE TIP CAP B849-0528070150-09207-041 CCCC

5000 9325

161501099234105A02I

00M/R BLADE CUFF G237-0042670150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

COND COND

1560014479774 YELLOW05A02E


5000 9325

1615010992341 YELLOW05A02I

00M/R BLADE CUFF E237-0039970150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70150-09100-043 A00700708 05A024. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

08-Jan-2016

COND COND

156001447977405A02E

12625312M/R BLADE TIP CAP A8490830270150-09207-041 CCCC

5000 6139

161501099234105A02I

42025312M/R BLADE CUFF A2370658070150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

COND COND

156001447977405A02E


5000 9632

161501099234105A02I






HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615011997646SWASHPLATE ASSY 70104-08000-050 MSU45 05A03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

08-Jan-2016

COND COND

161501087160205A03A01

55954755STATIONARYSWASHPLATE

D2220005070104-08010-044 CCCC

11000 16000

161501357508905A03A02

04755ROTATINGSWASHPLATE

151520150670104-08001-045 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

17000 21936

1615010785711 TRANS06A08

02248SWASHPLATE GUIDE F4250050370351-08227-041 RCRC

3000 6794

161501110149106A13

11422248MAIN GEARBOXHOUSING ASSY

F2110007470351-08110-045 RCRC

7600 12536

3040014158388 XMSN06A18

02248MAIN ROTOR SHAFT E2530461470351-08131-048 RCRC

12000 16751

1615014977257 TRANS06A19

1852248PLANETARY CARRIERASSY

A2400192270351-08175-046 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615013765089TAIL ROTORGEARBOX ASSY

70358-06600-046 A006-00482 06G014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

08-Jan-2016

12000 17341

161501074515306G01C

03048I/B RETENTION PLATET/R

FM270070358-06612-042 RCRC

5000 10103

304001292161706G01D

02810GEARSHAFT, BEVEL A320-0416170358-06620-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



4141013293428FAN AXIAL 70361-03005-107 C512-00281SB 06H234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

08-Jan-2016

2520 7183

311001127300506H23A

03192BALL BRNG ANN (OILCOOLER FWD)

UNK1SB210SFFC RCRC

2520 7183

311001127300506H23A


UNK2SB210SFFC RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




Report Date:

Page 2 of 2

08-Jan-2016




DATE AC HRS SHAFT VERTICAL REASON FOR VIB CHECKLONGITUDINALLATERAL

IPS READINGS4.

8323869HELICOPTER, UTILITYUH-60A3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL


PMI-202-Oct-2008 TAIL ROTOR 000.094663.3

100HR26-Sep-1996 #1 ENG 0.09002185.6

100HR26-Sep-1996 #2 ENG 0.47002185.6

100HR26-Sep-1996 OIL COOLER 0.1500.342185.6

100HR24-Feb-1997 #1 ENG 0.19002286

100HR24-Feb-1997 #2 ENG 0.3002286

100HR24-Feb-1997 OIL COOLER 0.3200.252286

100HR04-Sep-1997 #1 ENG 0.3002383.1

100HR04-Sep-1997 #2 ENG 0.41002383.1

100HR04-Sep-1997 OIL COOLER 0.1700.442383.1

PMS 226-Aug-1998 #1 ENG 0.02002482.5

PMS 226-Aug-1998 #2 ENG 0.22002482.5

PMS 226-Aug-1998 OIL COOLER 0.1900.492482.5

100HR28-Dec-1998 #1 ENG 0.45002581.9

100HR28-Dec-1998 #2 ENG 0.25002581.9

100HR28-Dec-1998 OIL COOLER 0.2700.152581.9

100HR27-Aug-1999 #1 ENG 0.45002778.1

100HR27-Aug-1999 #2 ENG 0.33002778.1

100HR27-Aug-1999 OIL COOLER 0.1400.152778.1

100HR13-Jan-2000 #1 ENG 0.47002880

100HR13-Jan-2000 #2 ENG 0.3002880

100HR13-Jan-2000 OIL COOLER 0.4700.372880

POST PHASE08-Aug-2000 #1 ENG 0.22002977.1


POST PHASE08-Aug-2000 OIL COOLER 0.1900.572977.1

POST PHASE08-Aug-2000 TAIL ROTOR 0.04002977.1

100 HR05-Jan-2001 TAIL ROTOR 0.11003073

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

DA FORM 2408-15-2 E, OCT 91 AIRCRAFT VIBRATION RECORD


IPS READINGS4.



100 HR05-Jan-2001 OIL COOLER 0.6100.23073

100 HR05-Jan-2001 #2 ENG 0.33003073

100 HR05-Jan-2001 #1 ENG 0.18003073

REPLACE #1 ENGINE22-Aug-2001 #1 ENG HSS 0.23003220.5

ENGINE REPLACE30-Jan-2002 NO.1 ENG 0.31003295.6

ENG CHANGE21-Mar-2002 #2 ENG 0.23003337.8

PMS-2 #711-Feb-2003 NO.1 ENG 0.43003462.7

PMS-2 #711-Feb-2003 NO.2 ENG 0.16003462.7

PMS-2 #711-Feb-2003 AXIAL FAN 0.3200.513462.7

PMS-2 #711-Feb-2003 TAIL ROTOR 0.03003462.7

100HR17-Nov-2003 #1 ENG 0.3003655.6

100HR17-Nov-2003 #2 ENG 0.43003655.6

100HR17-Nov-2003 OIL COOLER 0.0900.283655.6

100HR10-Sep-2004 #1 ENG 0.1003834.6

100HR10-Sep-2004 #2 ENG 0.29003834.6

100HR10-Sep-2004 OIL COOLER 0.1200.363834.6

100HR10-Sep-2004 TAIL ROTOR 0.13003834.6

100HR24-Jan-2005 #1 ENG 0.14003933.1

100HR24-Jan-2005 #2 ENG 0.4003933.1

100HR24-Jan-2005 OIL COOLER 0.0800.133933.1

100HR24-Jan-2005 TAIL ROTOR 0.06003933.1

120 HR04-Jan-2006 TAIL ROTOR 0.09004071.2

120 HR04-Jan-2006 #1 ENGINE 0.21004071.2

120 HR04-Jan-2006 #2 ENGINE 0.36004071.2

120 HR04-Jan-2006 OIL COOLER 0.090.1704071.2

120 HR06-Jul-2006 #1 ENG 0.28003189

120 HR06-Jul-2006 #2 ENG 0.3004189




IPS READINGS4.



120 HR06-Jul-2006 OIL COOLER 0.0700.164189

120 HR06-Jul-2006 TAIL ROTOR 0.12004189

DE-ICE BRACKET REPL29-Sep-2006 TAIL ROTOR 000.084255.1

PMI-1 POST PHASE01-Feb-2007 TAIL ROTOR 000.034311

PMI-1 POST PHASE01-Feb-2007 OIL COOLER 0.0600.124311

PMI-1 POST PHASE01-Feb-2007 #1 ENGINE 0.21004311






120 HR23-May-2007 #1 ENG 0.11004422

120 HR23-May-2007 #2 ENG 0.37004422

120 HR23-May-2007 OIL COOLER 00.6204422

120 HR23-May-2007 TAIL ROTOR 0.06004422

ENG REPLACEMENT22-Feb-2008 #2 ENG 0.31004588.2

UNFOLD22-May-2008 TAIL ROTOR 00.0304640.6

PMI-201-Oct-2008 OIL COOLER 0.010.3104663.3

120 HOUR01-Jun-2009 TAIL ROTOR 0.07004783.3

# 1 ENG REPLACEMENT01-Jun-2009 #1 ENG 0.08004783.3

120 HOUR01-Jun-2009 #2 ENG 0.4004783.3

120 HOUR01-Jun-2009 OIL COOLER 0.62004783.3

T/R VERIFICATION (RIG)26-Jun-2009 TAIL ROTOR 0.05004788.8

120HR01-Oct-2009 #1 ENG 0.32004902.8

120HR01-Oct-2009 #2 ENG 0.39004902.8

120HR01-Oct-2009 OIL COOLER 0.55004902.8

120HR01-Oct-2009 TAIL ROTOR 0.06004902.8




IPS READINGS4.



POST PHASE TD803826-Apr-2010 #1 ENG 0.36005000


POST PHASE TD803826-Apr-2010 OIL COOLER 0.58005000

RE-TORQUE26-Apr-2010 T/R 0.07005009.2

ENG REPLACEMENT12-May-2010 #2 ENG 0.37005003

T/R GEARBOX REPLACED29-Sep-2010 T/R 00.1205103.8

INBOARD RETENTION PLATE CHKS19-Oct-2010 T/R 00.105112.3

120 HR27-Oct-2010 T/R 0.11005120

120HR27-Oct-2010 #1 HSS 0.23005120

120HR27-Oct-2010 #2 HSS 0.23005120

120HR27-Oct-2010 OIL COOLER 0005120

VERIFICATION OF 27-OCT-2010 0.0 IPS09-Nov-2010 OIL COOLER 0.67005120

POST PHASE PMI-203-Jan-2012 #2 ENG 0.27005342.3

POST PHASE PMI203-Jan-2012 T/R 00.0705342.2

POST PHASE PMI 203-Jan-2012 #1 ENG 0.15005342.3

POST PHASE PMI204-Jan-2012 OIL OOLER 0.41005342.3

INBOARD RETENTION PLATE RETOURQE25-Jan-2012 T/R 0.16005351.8

120 HR19-Jun-2012 #2 ENG 0.37005460.8

120 HR19-Jun-2012 #1 ENG 0.19005460.8

120 HR19-Jun-2012 OIL COOLER 0.03005460.8

120 HR19-Jun-2012 T/R 00.0205460.8

POST MAIN/TAIL ROTOR RIG08-Aug-2012 T/R 0.03005489.9

# 2 INPUT MOD REPLACEMENT19-Jun-2013 #2 ENG 0.4005623.2

POST PMI04-Feb-2014 TAIL ROTOR 0.03005704.9

POST PMI04-Feb-2014 #1 HSS 0.18005704.9

POST PMI04-Feb-2014 #2 HSS 0.19005704.9

POST PMI04-Feb-2014 OIL COOLER 00.1505704.9




IPS READINGS4.



#1 ENG REPLACEMENT05-Feb-2015 #1 HSS 0.1005869.9

6. Remarks

QC000000

CW3 FORBES02-Oct-2008

(NO LOCATION)(NO ORGANIZATION)




HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70400-06100-042 233-04095 11C234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

08-Jan-2016

2160 6823

311001113828811C23A

00BRNG T/R PITCH CHGSHAFT

11404SB1162-102 RCRC

COND COND

534001094578911C23C

399399CLEVIS, ROD END 233-040952307201070400-06702-041 CCCC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016




PIDMWODATE HRS



ANTI-ICE VALVE 8323869AEX105841. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


22-Jun-2011 OM

JR01622507-Jul-2011

0.2D CO 1-214THAVN REGT

ALL H-60 SERIES ACFT,ANTI-ICE/START BLEED VALVEACTUATOR SHAFTS

H-60-11-ASAM-11MWO:

Priority Mnt Level

05-Sep-2012 OM

LD19731413-Sep-2012

1D CO 1-214THAVN

ENGINE ANTI-ICE/START BLEEDVALVE

H-60-12-ASAM-10MWO:

Priority Mnt Level


EQUIPMENT MODIFICATION RECORD (COMPONENT)DA FORM 2408-5-1-E, OCT 91


8323869116305-302AUXILIARY POWER UNIT876276

598

1313

3866

6881

0

5

3

3

5=

TOTAL COMPONENT COUNTS

COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-

READING AT INSTALLATION OF

MODULE/RECORDER3

READING AT REMOVAL OF

7. HISTORY RECORDER S/N

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE

OPERATING HOURSTEMP/TEMP INDEXLCF - 2LCF - 1

HISTORICAL COUNTS ON COMPONENT/MODULE

7. HISTORY RECORDER S/N6.

5. NHA - Serial Number4. P/N3. NOMENCLATURE2. Serial Number1. MODEL

**Note - APU Information LCF1 = NUMBER OF OVERHAULS LCF2 = STARTS SINCEOVERHAUL TTI = STARTS SINCE NEW OPH = ONLY FOR APU's WITH HOUR METERINSTALLED - ENTER TIME ON METER

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

HISTORY RECORDER, COMPONENT, MODULE RECORDDA FORM 2408-16-1-E, OCT91

OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-

12.HISTORY COUNTS AT LAST DEPOTREPL

11.

O/H OR

10.

SERIAL NUMBER9.PART NUMBERNOMENCLATURE

8.

ReportDate:

Major Nomenclature Major Part NumberMajor Wuc Major Serial Number

08-Jan-2016 2/2

15B 116305-302 AUXILIARY POWER UNIT 876276

764472200

163000SIF13714502902WHEEL,COMPRESSOR

7707

6000

1312687603

0000K7094503991WHEEL, TURBINE

9861

6000


11/17/201112:00:00 AM

1 TRANSCRIBED FROM 22 APR 2011) APU OVERHAULED AND REPAIREDIAW DMWR 55-2835-209. REPLACED THE FOLLOWING PARTS: TURBINEROTOR ASSY, CARRIER ASSY, FUEL MANIFOLD, STARTER GEAR, MAGPICK UP, OIL PUMP AND ALL FUEL AND OIL FILTERS TBO TIME FOR THISAPU IS 12876 SSN @ 9861 METER EVENTS, ENTERED BY TOM SULLIVANCIV TI ESRA FTCKY DSN 635-6201.

EW744892 TASM-E CAAF

REVERSE OF DA FORM 2408-16-1 E, OCT 91

365

360

5343

8323869 0 0

e. ACFT HRS INSTALLEDc. TIME SINCE NEW OR OVERHAULc. SERIAL NUMBER

UH-60A 876276 Days

b. MAKE OR TYPE d. ACFT HRS LAST OIL CHANGEb. SERIAL NUMBER

HELICOPTER, UTILITY AUXILIARY POWER UNIT Hrs

a. NOMENCLATURE AND TYPEa. NOMENCLATUREFREQUENCY

COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b

SAMPLE DATE PIDSAMPLELAST OILEND ITEM

RESULTSDATE RESULTS RECEIVED7. 8.6. REASON FORHOURS5.4.

COMPONENTCHANGE

04-Jan-2012NORMALBASELINE5343.012224534304-Jan-2012

LD19731417-Jan-2013NORMALROUTINE239.01313558214-Jan-2013

JR76327309-Oct-2013NORMALROUTINE358.01313570118-Sep-2013

CG11223326-Nov-2014NORMALROUTINE497.414755840.402-Oct-2014

PRE PHASE

9. REMARKS:

For use of this form, see DA PAMs 738-751; the proponent agency is DCSLOGDA FORM 2408-20, DEC 91, MAY BE USED

OIL ANALYSIS LOGDA FORM 2408-20, OCT 1997


CAO01654

83238696035T00G01ENGINE ASSY, TURBINEGE-E-307910

4103

3276

16695

19695

9044

7544

2051

2059

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE





T700-GE-700




OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 2/12

04A 6035T00G01 ENGINE ASSY, TURBINE GE-E-307910

32741962575382057

33171667956861694GEC0376556035T02G01COLD SECTIONMODULE

COND

COND

32741962575382057

4496000GGMP55816039T58G02COMBUSTION LINER

COND

COND

32741962575382057

30841892975171602MRSG38796055T20G05MTCHDROTOR/STATOR ASSY

COND

COND

32741962575382057

3591000AMDA27965043T24G14STAGE 1 NOZZLEASSY

COND

COND

32741962575382057

40302415695612766GEL0372356064T98G01POWER TURBINEMODULE

COND

COND

32741962575382057

2957000GED0373796035T01G01ACCESSORY MODULE

COND

COND

32741962575382057

490000K06726034T62P18PARTICLESEPARATOR BLOWER

COND

COND

32761962575382057

3866000UDAJ04275074T79G07FUEL CONTROL

COND

COND

32741962575382057

2476000APM011RU4076T64G01POU ASSY-O/S DRAINVALVE

COND

COND

32761962575382057

1055000EMDE06974046T29G13ELECTRICALCONTROL UNIT

COND

COND

32741962575382057

41011662590382049CAO016544046T26G03HISTORY RECORDER

COND

COND


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 3/12


32741962575382057

918000UDDK01224046T25G06COOLER, OIL

COND

COND

32741962575382057

412000COMH64094046T28G14ANTI-ICE VALVE

COND

COND




CAO01654

GE-E-3079106035T02G01COLD SECTION MODULEGEC037655

4101

3317

16625

16679

9038

5686

2049

1694

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 5/12

04A01 6035T02G01 COLD SECTION MODULE GEC037655

33171667956861694

4402823592692559SAP011855044T27G02POWER TAKEOFFDRIVE

COND

COND

33171667956861694

33171667956861694GLH230536035T77G19COMPRESSORROTOR ASSEMBLY

COND

COND

33171667956861694

37718741230206NCE141CC6035T88P07GAS GENERATORTURBINE SHAFT

14724

11000

33171667956861694

0000WESP20265036T95P01INNER BALANCEPISTON SE

COND

COND

33171667956861694

0000BIWYBENH6035T79P04COMPRESSORDISCHARGE SEAL

COND

COND

33171667956861694

34271430780042131FIA8C6316035T83P01COMPRESSOR REARSHAFT

5674

5000

33171667956861694

0000VAECK2475044T07P01NO 3 LABYRINTHSEAL

COND

COND

33171667956861694

3201838752391752WIN949CD5035T57P02VORTEX SPOILER

COND

COND

33171667956861694

6274149GATHPMD45043T04P02TIE ROD,COMPRESSOR

14095

10000

33171667956861694

204351973351873GATV46034045T08P01RING, SPACERCOMPRESSOR

12058

10000

33171667956861694

0000GLHTMTM36055T59P01COMPRESSORIMPELLER

9101

5000


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 6/12


33171667956861694

44241271572162182GGA077586039T56G04OUTPUT SHAFT ASSY

COND

COND

33171667956861694

0000GLHTM5WA6032T26G09STAGE 1 BLISK

9101

5000

33171667956861694

0000GLHTMWJG6032T27P08STAGE 2 BLISK

11101

7000

33171667956861694

0000GLHTN0466038T08P04STAGE 3 & 4 BLISK

11101

7000

33171667956861694

0000GLHTMP3E6038T09P04STAGE 5 BLISK

11101

7000

33171667956861694

0000TMKAGE936064T35P01NO 3 BALL BEARING

COND

COND

33171667956861694

724621117007605MDA344LW6064T14P01NO 4 ROLLERBEARING

COND

COND




CAO01654

GEC0376556039T56G04OUTPUT SHAFT ASSYGGA07758

4101

4424

16625

12715

9038

7216

2049

2182

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 8/12

04A01G 6039T56G04 OUTPUT SHAFT ASSY GGA07758

44241271572612182

0000FCAR32666064T34P02NO 1 BALL BEARING

COND

COND

44241271572612182

61378597138502901MABA13415035T69P01NO 2 ROLLERBEARING

COND

COND




CAO01654

GE-E-3079106055T20G05MTCHD ROTOR/STATORASSY

MRSG3879

4101

3084

16625

18929

9038

7517

2049

1602

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 10/12

04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRSG3879

30841892975171602

2313798860391219GAT2861T6064T85P01STAGE 1 TURBINEDISK

6788

5000

30841892975171602

30841892975171602GGAC7468A6039T57G18G/G STATOR ASSY

COND

COND

30841892975171602

260306282113GATHGKPH6064T86P02STAGE 2 TURBINEDISK

8841

5000

30841892975171602

431323901205PAMEU3096064T81P01STAGE 1 FWDCOOLING PLATE

8670

5000

30841892975171602

4681578802229GFF5D6E46064T82P01STAGE 1 REARCOOLING PLATE

8633

5000

30841892975171602

189071154138870PAMBG5606039T52P03STAGE 2 FWDCOOLING PLATE

6211

4000

30841892975171602

18203451415710866GFF5A0TT6064T84P02STAGE 2 REARCOOLING PLATE

7281

5000

30841892975171602

30841892975171602GGAG38796039T54G13G/G ROTORASSEMBLY

COND

COND




CAO01654

GE-E-3079106064T98G01POWER TURBINE MODULEGEL037235

4101

4030

16625

24156

9038

9561

2049

2766

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 12/12

04A03 6064T98G01 POWER TURBINE MODULE GEL037235

40302415695612766

40302415695612766GGA108225043T75G07POWER TURBINEROTOR

COND

COND

40302415695612766

97282281496748GATHG5G86038T32P02STAGE 3 TURBINEDISK

8129

5000

40302415695612766

3322024627GATHELCK6038T34P05STAGE 4 TURBINEDISK

9068

5000

40302415695612766

64956082278397GATHKRG15125T92G01POWER TURBINESHAFT

8452

5000

40302415695612766

29611632160831678MABK25155034T27P01NO 5 ROLLERBEARING

COND

COND

40302415695612766

2800323832781274FAFF27135034T28P01NO 6 BALL BEARING

COND

COND




ECD01118


3983

3983

42052

42052

9100

9100

3495

3495

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE





T700-GE-700




OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 2/12


36873859387543292

2922849362791347GE-C-0373396035T02G01COLD SECTIONMODULE

COND

COND

0000

0000GGMAP3816039T58G02COMBUSTION LINER

COND

COND

28572812873642744

4026307070301513MRS076146055T20G05MTCHDROTOR/STATOR ASSY

COND

COND

2857000


COND

COND

36893869187633298

25971103972461975GE-L-0372566064T98G01POWER TURBINEMODULE

COND

COND

0000

0000GE-D-0373386035T01G01ACCESSORY MODULE

COND

COND

0000

0000SUSJ48516034T62P13PARTICLESEPARATOR BLOWER

COND

COND

3983000


COND

COND

3218000


COND

COND

3983000


COND

COND

0000

0000ECD011184046T26G03HISTORY RECORDER

COND

COND


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 3/12


0000

0000SUS1275C4046T25G03COOLER, OIL

COND

COND

1656000

755000AEX105845066T38G04ANTI-ICE VALVE

COND

COND




ECD01118

GE-E-3073386035T02G01COLD SECTION MODULEGE-C-037339

3687

2922

38593

8493

8754

6279

3292

1347

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 5/12

04A01 6035T02G01 COLD SECTION MODULE GE-C-037339

2920839362711344


COND

COND

2920839362711344


COND

COND

2920839362711344

9076301409378GATCV6K06035T88P04GAS GENERATORTURBINE SHAFT

13778

11000

2920839362711344

000039648465036T95P01INNER BALANCEPISTON SE

COND

COND

2920839362711344

0000MMTF55096035T79P04COMPRESSORDISCHARGE SEAL

COND

COND

2920839362711344

22791397777322023GAT9936F6035T83P01COMPRESSOR REARSHAFT

6406

5000

2920839362711344

0000VAEA88855044T07P01NO 3 LABYRINTHSEAL

COND

COND

2920839362711344

25981580579622212BIWBN1355035T57P02VORTEX SPOILER

COND

COND

2920839362711344

117219011156430GATMF7475043T04P02TIE ROD,COMPRESSOR

12513

10000

2920839362711344

30241461840861476GATAJ2894045T08P01RING, SPACERCOMPRESSOR

10661

10000

2920839362711344

0000GLHTKC6A6055T59P01COMPRESSORIMPELLER

8685

5000


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 6/12


2920839362711344


COND

COND

2920839362711344

0000GLHTKJNJ6032T26G09STAGE 1 BLISK

8685

5000

2920839362711344

0000GATHGMRM6032T27P08STAGE 2 BLISK

10685

7000

2920839362711344

0000GLHTJWE46038T08P04STAGE 3 & 4 BLISK

10685

7000

2920839362711344

0000GLHTK2F06038T09P04STAGE 5 BLISK

10685

7000

2920839362711344

9311565116043338388966064T35P02NO 3 BALL BEARING

COND

COND

2920839332711344

29551203092352093MAB565196064T15P01NO 4 ROLLERBEARING

COND

COND




ECD01118

GE-C-0373396039T56G04OUTPUT SHAFT ASSYGGA06194

3687

4926

38593

10647

8754

11253

3292

2573

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 8/12


4924000

2525000BARA71195034T07P03NO 1 BALL BEARING

COND

COND

4924000

18000MDAL72075035T71P01NO 2 ROLLERBEARING

COND

COND




ECD01118


MRS07614

2857

4026

28128

3070

7364

7030

2744

1513

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 10/12

04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRS07614

4026307070301513

0000GATH89T96064T85P01STAGE 1 TURBINEDISK

7857

5000

4026307070301513

4026307070301513GGA160446039T57G24G/G STATOR ASSY

COND

COND

4026307070301513

119589343236746GAT8262U6064T86P01STAGE 2 TURBINEDISK

6662

5000

4026307070301513

0000GFF5A91F6064T81P01STAGE 1 FWDCOOLING PLATE

7857

5000

4026307070301513

0000GFF5A92W6064T82P01STAGE 1 REARCOOLING PLATE

7857

5000

4026307070301513

0000GFF5ADCC6064T83P01STG 2 FWD COOLINGPLATE

7857

5000

4026307070301513

0000GFF5A0JP6064T84P02STAGE 2 REARCOOLING PLATE

7857

5000

4026307070301513

4026307070301513GGA076146039T54G13G/G ROTORASSEMBLY

COND

COND




ECD01118

GE-E-3073386064T98G01POWER TURBINE MODULEGE-L-037256

3689

2597

38691

11039

8763

7246

3298

1975

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 12/12

04A03 6064T98G01 POWER TURBINE MODULE GE-L-037256

25961102672421973


COND

COND

0000

0000GATJV4216038T32P01STAGE 3 TURBINEDISK

6092

5000

0000

0000GATJJ8546038T34P05STAGE 4 TURBINEDISK

6092

5000

25961102672421973

27041082767801711GATLY4375125T92G01REPOWER TURBINESHAFT

5984

5000

25961102672421973

160027192761615FCAB74225034T27P02NO 5 ROLLERBEARING

COND

COND

25961102672421973

153623522115759MABF82216064T36P01NO 6 BALL BEARING

COND

COND



PIDMWODATE HRS



ENGINE ASSY, TURBINE 8323869GE-E-3073381. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


30-Jun-1994 OR

29-May-19964D-CO 2-1 APO

AE 09250(LR0306)

ONE TIME INSPECTION ANDCONVERSION OF FORMS ANDRECORDS FOR T700-GE-700, -701AND -701C SERIES GAS TURBINEENGINES

1-2840-248-20-2MWO:

Priority Mnt Level

30-Oct-1996 OU

08-Apr-19981DYNCORP-

GSMP APO AE09028 (LR0306)

REPLACEMENT OF UNDAMPED GASGENERATOR ROTOR/STATORASSEMBLIES FOR ALL UH-60A ANDEH-60A AIRCRAFT WITH T700-GE-700ENGINES

1-2840-248-20-19MWO:

Priority Mnt Level

15-Dec-1998 OU

17-Feb-200012-502 AVN REGT

AE 09028(LR0306)

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

1-2840-248-20-22MWO:

Priority Mnt Level

02-Aug-1999 FM

17-Feb-200012-502 AVN REGT

AE 09058(LR0306)

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

UH-60-99-ASAM-11MWO:

Priority Mnt Level

16-Aug-1999 OM

17-Feb-20000.52-502 AVN REGT

AE 09058(LR0306)

ALL UH-60A, EH-60A AND UH-60QAIRCRAFT, SUBJECT: INSPECTIONINTERVAL CHANGE FOR HAMILTONSTANDARD HYDRO MECHANICALUNITS (HMU) P/NS 4046T52G01,4046T52G04, 4046T52G06,4046T52G09 AND 4046T52G11 USEDON THE T700-GE-700 ENGINE


Priority Mnt Level

16-Jul-2007 OM

18-Jul-20070.11-214TH AVN

REGT (ST0922)ALL H-60A SERIES AIRCRAFT,HAMILTON-SUNDSTRAND HYDRO-MECHANICAL UNITS (HMU'S)


Priority Mnt Level

23-Jul-2007 OM

25-Jul-20070.51-214TH AVN

REGT (ST0922)ALL UH/HH-60L AIRCRAFT,DEFECTIVE DIGITAL ENGINECONTROL UNITS (DECU)


Priority Mnt Level

13-Aug-2007 OM

14-Aug-20070.51-214TH AVN

REGT (AN9260)ALL H-60 SERIES AIRCRAFT, MAINFUEL MANIFOLD CHAFING


Priority Mnt Level

28-Dec-20070.11-214TH AVN

REGT (ST0922)ALL H-60 AND ALL AH-64 SERIESAIRCRAFT, MIL-PRF-23699 HIGHTEMPERATURE STABILITY (HTS) OIL

H-60-08-AMAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS





20-Dec-2007 OM

22-Sep-2008 OM

20-Oct-20081TASM-E APO AE

09058 (LR0306)SUSPECT ENGINE HARNESSESH-60-08-ASAM-14MWO:

Priority Mnt Level

12-Jan-2009 OM

13-Jan-20091D CO 1-214TH

AVN REGCOLEMAN BKS,GE

T701C GAS GENERATOR (GG)ROTOR ASSEMBLIES

H-60-09-ASAM-01MWO:

Priority Mnt Level

01-Oct-2009 OM

SD65391215-Oct-2009

11-214TH AVNREGT

ALL H-60A SERIES AIRCRAFT,HAMILTON-SUNDSTRAND HYDRO-MECHANICAL UNITS

H-60-10-ASAM-01MWO:

Priority Mnt Level



T/T I HIST RCDR SNSERIAL 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

16015 SESI

2. Organization

CSGLD-1052

REQUIREMENT CONTROL SYMBOL(Julian)1. PERIOD ENDING DATE


1GEE307320 ECD-011984198222739836263862627923289

2GEE307936 CAO0222758161989114460401862627923289

1GEE307539 CAO008363337110495859172257328123603

2GE-E-307912 ECD03263314596425013164557328123603

1GE-E-307910 CAO016544109166959049205358758323869

2GE-E-307338 ECD0111848154558810326391258758323869


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

Eddie.Denney

Highlight

PIDMWODATE HRS



FUEL CONTROL 8323869UDAJ07101. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


16-Jul-2007 OM

JB45666007-Dec-2010

0.2D CO 214TH AVNALL H-60A SERIES AIRCRAFT,HAMILTON-SUNDSTRAND HYDRO-MECHANICAL UNITS (HMU'S)


Priority Mnt Level

01-Oct-2009 ON

JB45666007-Dec-2010

0.2D CO 1-214THHMU SUSPECTED PART NUMBERH-60-10-ASAM-01MWO:

Priority Mnt Level

23-Nov-2010 OM

JB45666007-Dec-2010

0.2D CO 1-214THAVN

ALL H-60 SERIES AIRCRAFT,HAMILTON STANDARD HYDRO-MECHANICAL UNITS PN 5074T79GO2, 5074T79GO3, AND 5074T79GO5REMOVE FROM SERVICE. REMOVEPN 5074T79GO7 IF LAST DEPOTREPAIR PRIOR TO 01 JAN 2003.

H-60-11-ASAM-03MWO:

Priority Mnt Level

05-Sep-2012 OM

LD19731417-Sep-2012

1D CO 1-214THAVN

ALL H-60A SERIES AIRCRAFT,HYDRO-MECHANICAL UNIT(HMU).

H-60-12-ASAM-11 (CORREMWO:

Priority Mnt Level

19-Aug-2013 FM

DR62253028-Aug-2013

1DCO 1-214THAVN BN

WOODWARD HYDR-MECHANICALUNIT (HMU) P3 TUBE

H-60-13-ASAM-10MWO:

Priority Mnt Level

13-Aug-2014 FM

BJ96335431-Jul-2014

0.1D CO. 1-214THAVN REGT

COMPLY WITH REQUIRENENTS OF H-60-14-ASAM-08

H-60-14-ASAM-08MWO:

Priority Mnt Level



PIDMWODATE HRS






DR21-Jun-2004

0MODIFICATION 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

DR30-Apr-1991

TASM-OEUROPE

17701-MAY-1993

MODIFICATION OF THE HOVERINFERRED SUPPRESSION SYSTEM(UH-60A HELICOPTERS) NATIONALSTOCK NUMBER (NSN) 1520-01-035-0266

1-1520-237-50-63 B-KITMWO:

Mnt LevelPriority

DN01-Jan-1900

L3 COMMBLUEGRASSARMY DEPOT(HA9430)

0.101-Sep-2003

SSG BRODIN,RYAN D

WX-1000 STORMSCOPE WEATHERMAPPING SYSTEM

LEX 1871MWO:

Mnt LevelPriority

DN16-Jun-1994

TASM-OEUROPE

18602-OCT-1995

INST OF ELECTRICALLY HEATEDGLASS CENTER WINDSHIELD

1-520-237-50-70MWO:

Mnt LevelPriority

DN12-Apr-1999

TASM-OEUROPE

12402-OCT-1995

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

1-1520-237-50-66 C1MWO:

Mnt LevelPriority

DN28-Jun-1996

TASM-OEUROPE

43604-DEC-1995

INSTALLATION OF DUAL AN/ARC-186/ARC-201 (V) FM RADIO SYSTEMSAND HARDWIRING OF TSEC KY-58 (UH-60A HELICOPTERS) NATIONALSTOCK NUMBER (NSN) 1520-01-035-0266

1-1520-237-50-69 C1MWO:

Mnt LevelPriority

DN15-Nov-1990

TASM-OEUROPE

507-MAY-1990

INCORPORATION OF IMPROVEDTIEDOWN FITTINGS

1-1520-237-50-52MWO:

Mnt LevelPriority

DN17-Jan-1989

TASM-OEUROPE

209-JUN-1989

MOD OF BEARING RETAINER SPRINGCLIP T/R SERVO

55-1520-237-50-52REAPPLIED

MWO:

Mnt LevelPriority

DN15-Apr-1990

TASM-OEUROPE

3009-JUN-1989

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

55-1520-237-50-44 C3MWO:

Mnt LevelPriority



PIDMWODATE HRS






DM15-Nov-1989

TASM-OEUROPE

2209-MAY-1990

MODIFICATION OF DOWEL PINRETENTION MAIN GEARBOX

1-1520-237-50-43MWO:

Mnt LevelPriority

DN04-Mar-1999

TASM-OEUROPE

3509-SEP-1998

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

1-1520-237-50-74 C1MWO:

Mnt LevelPriority

DN01-Sep-1986

TASM-OEUROPE

105412-DEC-1986

INCORP OF ANVIS COMP LIGHTINGSYSTEM

55-1520-237-50-20 CHG 5MWO:

Mnt LevelPriority

DN22-Jun-1999

TASM-OEUROPE

313-AUG-1999

IMPROVED INERTIA REEL1-1520-23-75-79MWO:Mnt LevelPriority

DN01-Oct-1991

TASM-OEUROPE

413-JUL-1990

INCORPORATION OF STABILATORACTUATOR GROUNDING STRAP FORUH-60A/EH-60A HELICOPTERS

1-1520-237-50-54MWO:

Mnt LevelPriority

DR01-Nov-2006

D CO 1-214THAVN

1013-Oct-2009

V, ZMODIFICATION FOR THE DAULINSTALLATION OF ATTITUDEHEADING REFERENCE UNITS (AHRU)

1-1520-237-50-94MWO:

Mnt LevelPriority

DR04-Jan-1986

TASM-OEUROPE

4015-APR-1986

MODIFICATION OF DIRECTIONALCONTROL CABLE ASSEMBLY (UH-60A& EH-60A HELICOPTERS) NATIONALSTOCK NUMBER (NSN) 1520-01-035-0266 & 1520-01-082-0686

55-1520-237-50-34 C1MWO:

Mnt LevelPriority

DN15-Aug-1988

TASM-OEUROPE

6715-DEC-1987

INCORPORATION OF WIRE STRIKEPROTECTION SYSTEM (WSPS) (UH-60A HELICOPTER)

55-1520-237-50-24 C4MWO:

Mnt LevelPriority

DR25-Apr-2006

TASM-OEUROPE

10015-SEP-2008

INSTALLATION OF CRASHWORTHYEXTERNAL FUEL SYSTEM , UH-60SERIES HELICOPTER (SUPERCEDESMWO DTD 14 DEC 2006)

1-1520-237-50-86 DTD 25APR 2006

MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN14-Mar-1990

TASM-OEUROPE

83218-OCT-1992

INCORPORATION OFELECTROMAGNETIC ENVIROMENTPROTECTION

1-1520-237-50-59 CHGS 2MWO:

Mnt LevelPriority

DN15-Aug-1990

TASM-OEUROPE

2420-APR-1990

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

55-1520-237-50-49 C1MWO:

Mnt LevelPriority

DR28-Jun-2002

TASM-OEUROPE

8021-MAY-2002

INSTALLATION OF SEALED LEAD ACIDBATTERY (SLAB) SYSTEM ANDRELOCATION OF UTILITY LIGHTPOWER (UH-60A/L HELICOPTERS) UH-60A NSN 1520-01-035-0266, UH-60LNSN 1520-01-298-4532

1-1520-237-50-77 C1MWO:

Mnt LevelPriority

DR26-Oct-2001

TASM-OEUROPE

30021-MAY-2002

INSTALLATION OF HFCOMMUNICATION SYSTEM AN/ARC-220(V) AND TSEC/KY-100 IN UH-60A/LHELICOPTER NSN 1520-01-035-0266,UH-60A NSN 1520-01-298-4532 UH-60L

1-1520-237-50-76 C1MWO:

Mnt LevelPriority

FN13-Jun-2013

TASM-OEUROPE

521-NOV-2013

INSTRUCTIONS FOR THE REMOVALOF THE #1 (CO-PILOTS) AHRU ANDINSTALLATION OF NAV SYS : CN-1313(VG), TRU-2A/A (RG)

1-1520-237-20-2MWO:

Mnt LevelPriority

DN31-Aug-1992

TASM-OEUROPE

122-APR-1993

IMPROVED CARGO HOOK KEEPERINSTALLATION FOR UH-60AHELICOPTERS

1-1520-237-50-15MWO:

Mnt LevelPriority

DN01-Oct-1990

TASM-OEUROPE

1223-APR-1990

INCORPORATION OF ENGINEQUADRANT SECONDARY STOP TONO. 1 AND NO. 2 ENGINE POWERCONTROL LEVERS (UH-60AHELICOPTERS)

55-1520-237-50-39 C1MWO:

Mnt LevelPriority



PIDMWODATE HRS






FR26-Feb-2008

TASM-OEUROPE

923-DEC-2009

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)

MWO 1-1520-237-20-94MWO:

Mnt LevelPriority

DU01-Apr-1988

TASM-OEUROPE

423-MAR-1987

MODIFICATION OF MAIN ROTORBLADE DE-ICE DISRUPTOR HARNESSAND TAIL ROTOR SLIP RINGHARNESS (UH-60A HELICOPTERS)

55-1520-237-50-36 C1MWO:

Mnt LevelPriority

DU30-Sep-1987

TASM-OEUROPE

623-NOV-1987

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

55-1520-237-50-46 C1MWO:

Mnt LevelPriority

DN15-Aug-1988

TASM-OEUROPE

6724-MAR-1988

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

55-1520-237-50-47 C1MWO:

Mnt LevelPriority

DR06-Sep-2002

TASM-OEUROPE

8026-MAY-2000

MODIFICATION OF THE UH/EH/HH-60HELICOPTER AUXILIARY FUELMANAGEMENT SYSTEM EXTERNALSTORES SUPPORT SYSTEM(INDICATOR KIT NSN 1615-01-451-8200) AND EXTENDED RANGE FUELSYSTEM (PROBE KIT NSN 1615-01-451-8207)

1-1520-237-50-78 C1MWO:

Mnt LevelPriority

DN29-Nov-1999

TASM-OEUROPE

5226-MAY-2000

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

1-1520-237-50-56 C2MWO:

Mnt LevelPriority

DR31-Mar-1997

TASM-OEUROPE

17826-MAY-2000

AN/ASN-128B DOPPLER/GPSNAVIGATION SYSTEM IN UH-60A/LHELICOPTER

1-1520-237-50-75 C1MWO:

Mnt LevelPriority

DN14-Jun-1991

TASM-OEUROPE

630-NOV-1992

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

1-1520-237-50-61 C1MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN30-Apr-1991

TASM-OEUROPE

230-NOV-1992

INSTALLATION OF IMPROVED ENGINECOWLING RELEASE HANDLE ASSY.

55-1520-237-50-64MWO:

Mnt LevelPriority

OU31-Oct-2002

TASM-OEUROPE

230-OCT-2002

UH-60 SERIES AIRCRAFT INSPECTAN/ARC-220 WIRING FOR CHAFING

1-1520-237-20-261MWO:

Mnt LevelPriority

DN28-Oct-1996

TASM-OEUROPE

631-JUL-1998

MODIFICATION OF CHIP DETECTORWIRING FOR UH-60A HELICOPTERS

1-1520-237-50-26MWO:

Mnt LevelPriority

DU15-Jun-1995

TASM-OEUROPE

2431-OCT-1995

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

1-1520-237-50-73 C1MWO:

Mnt LevelPriority




8.7.DATE

6.REMARKS

4. 5.



SIKORSKYAIRCRAFT MAIN ROTOR HEAD RIGGED INACCORDANCE WITH S/A DWG. 70400-00003REV. D. SYSTEM CONTROLS HAVE BEENBIASED IN ACCORD. A. LATERAL SERVOINPUT ROD P/N 70400-02258-046 HAS BEENSHORTENED 1/8 TURN. B.AFT CONTROLSERVO INPUT ROD P/N 70400-02258-043 HASBEEN LENGTHEDN 1/2 TURN. C. FORWARDCONTROL SERVO INPUT ROD P/N 70400-02258-047 HAS BEEN SHORTENED 1/2 TURN.(UK0000)

21-Nov-1983 1

HARTFORD CONN.

QC000000

SIKORSKYUH-60A-82-16 (TB 55-1520-237-20-34) ONE TIMEINSP. OF FLIGHT CONTROLS MIXER LIMITERCOMPLIED WITH. (UK0000)

10-Dec-1983 1

HARTFORD CONN.

QC000000

SIKORSKYUH-60A-83-04 (TB 55-1520-237-30-01) ONE TIMEINSP. FOR UH-60A INLET DUCT ASSY.P/N70302-10100 & ALIGMENT PIN BRKT. P/N 70203-04301-044 & 045 COMPLIED. (UK0000)

12-Dec-1983 1

HARTFORD CONN.

QC000000

SIKORSKYECP-0178R1 HAS BEEN INCORPORTED IN THISAIRCRAFT. PURSUANT TO MOD. P-0072. THECONTRACTOR HAS INSTALLED ECP-0252WITH THE EXCEPTION OF THE DAMPENINGTO THE NEW AIRSPEED INDICATING WILLSYSTEM AS DESCIRED ON MWO'S 21519 &21541 ATTACHED TO THE AIRCRAFTLOGBOOK. THE CONTRACTOR WILLPROMPTLY RETROFIT THE NEW RESTRICTORTO COMPLY WITH THE ECP REQUIREMENT ATNO DIRECT COST TO THE GOV. (UK0000)

15-Dec-1983 1

HARTFORD CONN.

QC000000

201ST AVN COSOF TWX UH-60A-84-01 COMPLIED WITH201ST AVN. (UK0000)

26-Jan-1984 1

APO S.F. 96271

QC000000

201ST AVN COTB 55-1520-237-20-47 COMPLIED WITH 201STAVN CO APO S.F. 96271. #1 1120E #2 1336E(UK0000)

30-Jan-1984 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME INSP NO 1 & 2 JUNCTION BOXESI/A/W TB 55-1520-237-20-48 & UH-60A-84-02COMPLETED AT 55.O ACFT HRS (UK0000)

21-Mar-1984 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME INSP TAIL ROTOR PYLON COVERHINGE BRACKET DOES NOT APPLY TO THISACFT (UK0000)

18-Apr-1984 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME INSP & REPAIR OF STABILATORAMPLIER C/W BY SIKORSKY ACFT CO I/A/WUH-60-84-04 & TB 55-1520-237-50-2 AT 75.6ACFT HRS. (UK0000)

23-Apr-1984 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME INSP TIAL ROTOR GEARBOX ANDINTERMEDIATE GEARBOX I/A/W UH-60A-84-06COMPLETED AT 26 APR 84 @ 76.6 ACFT HRS.(UK0000)

26-Apr-1984 1

APO S.F. 96271

QC000000

201ST AVN COUH-60A-84-07 AND TB 55-1520-237-20-53 ENGOUTPUT SHAFT INSPECTION P/N 70361-08004-043 BOLTS P/N MS9724-08 AND P/NSS5086-04INSPECTION COMPLETED AT 79.0 21 MAY 84(UK0000)

21-May-1984 1

APO S.F. 96271

QC000000



8.7.DATE

6.REMARKS

4. 5.



201ST AVN COONE TIME INSP OF CARGO HOOK PRESSURECARTRIDGE I/A/W SOF UH-60A-84-08COMPLETED AT 79.9 ACFT HRS. (UK0000)

05-Jun-1984 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME INSP OF LONGITUDINAL/LATERALLINK ASSY I/A/W SOF MESSAGE UH-60A-84-11AND TB 55-1520-237-20-56 AT 88.6 ACFT HRS.(UK0000)

16-Jul-1984 1

APO S.F. 96271

QC000000

201ST AVN COOCM/ACE INSP PERFORMED ST 89.0 ACFTHRS AT CP HUMPHREYS KOREA BY ACETEAM MEMBER D. GOSSETT AVSCOM OCMSEC. ST. LOUIS, MO. (UK0000)

02-Aug-1984 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME OF MAIN ROTOR SPINDLE ASSYI/A/W SOF MESSAGE UH-60A-84-12 AND TB 55-4520-237-20-55 AT 89.1 ACFT HRS. (UK0000)

02-Aug-1984 2

APO S.F. 96271

QC000000

201ST AVN COONE TIME OF TAIL CONE CANTED HINGEBULKHEAD RADIUS BLOCKS I/A/W SOFMESSAGE UH-60A-84-10 AND TB 55-1520-237-20-54 AT 91.2 ACFT HRS. (UK0000)

24-Aug-1984 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME OF TAIL CONTROL CABLEREQIURED BEFORE NEXT 10HR/14DAY I/A/WSOF MSG UH-60A-84-14 AND TB 55-1520-237-20-58. COMPLETED AT 381.7 ACFT HRS.(UK0000)

13-Dec-1984 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME OF TAIL CONTROL CABLETURNBUCKLE IDENFICATION REQUIRED I/A/WSOF MSG UH-60A-84-13. (UK0000)

10-Jan-1985 1

APO S.F. 96271

QC000000

201ST AVN COUH-60A-84-15 EXTENSION OF TIME TOREPLACE TAIL ROTOR BRASS TURNBUCKLES. (UK0000)

10-Jan-1985 2

APO S.F. 96271

QC000000

201ST AVN COREMOVEAL & REPLACEMENT OF GG ROTORAT CERTAIN LIFE LIMITS. ACFT IS BEINGMONITORD I/A/W SOF UH-60A-84-16 AS PERTB 55-2840-248-20-16. COMPLETED AT 118.3ACFT HRS. (UK0000)

14-Jan-1985 1

APO S.F. 96271

QC000000

201ST AVN COONE TIME RECURRING INSPECTION OF M/G/BDOWEL PIN UH-60A AS PER SOF UH-60A 84-16ONE TIME INSP COMPLETED AT 118.3 ACFTHRS. (UK0000)

14-Jan-1985 2

APO S.F. 96271

QC000000

201ST AVN COONETIME INSP OF STABILATOR AMPLIFIERSFOR LOCKING POTENTIOMETERS I/A/W SOFMSG UH-60A-85-01 COMPLETED AT 151.9ACFT HRS (UK0000)

03-Feb-1985 1

APO SF 96271

QC000000

201ST AVN COONETIME INSP OF PRIMARY SERVOS ANDCONTROL RODS I/A/W SOF MSG UH60A-85-06COMPLETED AT 211.4 ACFT HRS (UK0000)

29-Mar-1985 1

APO SF 96271

QC000000

201ST AVN COIMMEDEDIATE GROUNDING AND INSPECTIONOF FLIGHT CONTROLS I/A/W SOF MSG UH-60A-85-07 COMPLETED AT 226.4 ACFT HRS(UK0000)

07-Apr-1985 1

APO SF 96271

QC000000

201ST AVN COIMMEDEDIATE GROUNDING AND INSPECTIONOF ALL MAJOR SYSTEMS REQUIRED I/A/WSOF MSG UH-60A-85-10 COMPLETED AT 226.4ACFT HRS (UK0000)

26-Apr-1985 1

APO SF 96271

QC000000



8.7.DATE

6.REMARKS

4. 5.



201ST AVN COONETIME INSP OF SPINDLE AND LINER SERILNUMBER CHECK I/A/W SOF MSG UH-60A-85-11COMPLETED AT 226.4 ACFT HRS (UK0000)

02-May-1985 1

APO SF 96271

QC000000

201ST AVN COONETIME INSP AND MODIFIED FLYABLESTORAGE PROCEDURES I/A/W SOF MSG UH-60A-85-13 COMPLETED AT 226.4 ACFT HRS(UK0000)

20-May-1985 1

APO SF 96271

QC000000

201ST AVN COONETIME RECORDS INSP OF M/R SHAFT I/A/WSOF MSG UH60A-85-14 COMPLETED AT 387.7ACFT HRS (UK0000)

04-Jun-1985 1

APO SF 96271

QC000000

201ST AVN COONETIME INSP OF RECORDS ON HUB M/RI/A/W SOF MSG UH60A-85-15 COMPLETED AT226.4 ACFT HRS (UK0000)

04-Jun-1985 2

APO SF 96271

QC000000

201ST AVN COENGINE OUTPUT SHAFT RECURRINGVIBRATION LIMITS I/A/W SOF MSG UH60A-85-17 L/H .50 IPS R/H .70 IPS COMPLETED AT226.4 ACFT HRS (UK0000)

11-Jun-1985 1

APO SF 96271

QC000000

AVSCOM OCM SEC, ST.LOUIS

OCM/ACE PERFORMED AT 226.4 ACFT HRS(UK0000)

02-Jul-1985 1

CP HUMPHREYS,KOREA

QC000000

201ST AVN COONETIME INSP AND MODIFICATIONPROCEDURES FOR UNGROUNDING THEUH60A I/A/W SOF MSG UH60A-85-18COMPLETED AT 226.4 ACFT HRS (UK0000)

09-Jul-1985 1

APO SF 96271

QC000000

201ST AVN COONETIME INSP OF T/R DRIVE SHAFT BEARINGI/A/W SOF MSG UH60A-85-23 COMPLETED AT269.3 ACFT HRS (UK0000)

24-Jul-1985 1

APO SF 96271

QC000000

201ST AVN COSUPPLEMENT TO INSP OF T/R DRIVESHAFTBEARINGS I/A/W SOF MSG UH-60A-85-24COMPLETED AT 269.3 ACFT HRS (UK0000)

02-Aug-1985 1

APO SF 96271

QC000000

201ST AVN COTORQUE STABILIZATION OF M/R PITCH HORNATTACHMENT BOLTS COMP. I/A/W SOF MSGUH-60A-85-25 + UH-60-85-26 COMPLETED AT360.1 ACFT HRS (UK0000)

02-Nov-1985 1

APO SF 96271

QC000000

201ST AVN COREPLACEMENT OF T/R DRIVE SHAFTBEARINGS PN - SB1138-101 I/A/W SOF MSG UH-60A-86-01 COMPLETED (UK0000)

24-Feb-1986 1

APO SF 96271

QC000000

201ST AVN COONETIME TORQUE OF T/R DRIVE SHAFT FLEXCOUPLINGS COMP I/A/W SOF MSG UH-60A-86-02 COMPLETED AT 410.5 ACFT HRS (UK0000)

24-Feb-1986 2

APO SF 96271

QC000000

201ST AVN COIMMEDIATE GROUNDINGING OF UH-60/EH-60SERIES AT 420.6 ACFT HRS (UK0000)

26-Mar-1986 1

APO SF 96271

QC000000

201ST AVN COREQUIREMENTS FOR UNGROUNDING I/A/WSOF UH-60A-86-07 COMPLETED AT 420.6 ACFTHRS (UK0000)

01-May-1986 1

APO SF 96271

QC000000

201ST AVN COREPLACEMENT OF STABLILATORACTUATORS PN - 70400-06641-108/109/110AND INSP OF 2408-16 I/A/W SOF UH-60A-86-08COMPLETED AT 420.6 ACFT HRS (UK0000)

12-May-1986 1

APO SF 96271

QC000000

201ST AVN COOCM/ACE PERFORMED AT 444 A/C HRS AT CPHUMPHREYS BY ACE TEAM AVSCOM SEC, ST.LOUIS (UK0000)

07-Jun-1986 1

APO SF 96271

QC000000



8.7.DATE

6.REMARKS

4. 5.



201ST AVN COSOF MSG UH-60A-86-10 ONETIME INSP OFMAIN CONTROL DEVICE BEARINGS STAKEC/W 14 JUNE 86 AT 427 ACFT HRS THIS SOFWAS NOT LOG BUT DA 2408-13 REFLECTSBEING COMPLY AT ABOVE DATE (UK0000)

14-Jun-1986 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60A-86-12 ONETIME INSP OFYAW AND COLLECTIVE BOOST SERVOS BYSN C/W 6 AUG 86 AT ACFT HRS SOF WAS NOTLONG BEFORE 2408-13 REFLECTS C/W ONABOVE DATE (UK0000)

06-Aug-1986 1

APO SF 96271

QC000000

201ST AVN COREPL OF AN 310-8 NUTS NSN 5310-00-157-1289COMPLETED AT 449 ACFT HRS I/A/W SOF MSGUH-60-86-13 13 AUG 86 (UK0000)

13-Aug-1986 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60A-86-16 REVISION OF SOF UH-60A-86-10 C/W ON 14 JUNE 86 AT 427 ACFTHRS (UK0000)

21-Oct-1986 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60A-86-17 INSP OF XMSN OILCOOLER FAN SPLINES N/A TO THIS ACFT BYSN (UK0000)

31-Oct-1986 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60A-86-19 REINSPECTION OFTHE EYE BOLTS P/N 70209-02136-102 NOTINSTALLED THIS ACFT BY SN (UK0000)

02-Nov-1986 1

APO SF 96271

QC000000

45TH TRANS COINSP OF THE FIRST OF THREE TAIL ROTORDRIVE SHAFT SPLINE COUPLINGS ANDREMOVAL OF MATERIAL FROM UNDER CREWSEATS COMPLIED WITH I/A/W SOF MSG UH-60-86-20 (UK0000)

14-Nov-1986 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60A-86-20 ONETIME INSPECTIONOF THE FIRST 3 T/R CRIVE SHAFT SPLINESC/W 14 NOV 86 AT 493.1 ACFT HRS (UK0000)

14-Nov-1986 2

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60A-86-21 ONETIME INSP OFCREW SEATS FOR LONGITUDINALMOVEMENT OF LOCKPINS ADJUSTMENT C/W10 DEC 86 AT 493.1 ACFT HRS BY OLR(UK0000)

10-Dec-1986 1

APO SF 96271

QC000000

201ST AVN COPE#1 COMPLETED AT 495.9 ACFT HRS 6 FEB87 (UK0000)

06-Feb-1987 1

APO SF 96271

QC000000

201ST AVN COUH-60A-87-03 (TB 1-1520-237-20-89) ONETIMEAND RECURRING COUPLINGS COMPLETED 15MAR 87 AT 525.2 ACFT HRS (UK0000)

15-Mar-1987 1

APO SF 96271

QC000000

201ST AVN COUH-60A-87-04 ONETIME AND RECURRING INSPOF EYEBOLTS PN - 70209-02136-102COMPLETED 27 MAR 87 AT 532.1 ACFT HRS(UK0000)

27-Mar-1987 1

APO SF 96271

QC000000

201ST AVN COSOF UH-60-87-07 ONETIME AND RECURRINGINSP OF LONGITUDINAL/LATERAL LINKS FORCRACKS C/W AT 583.3 HRS (UK0000)

18-May-1987 1

APO SF 96271

QC000000

201ST AVN COSOF UH-60-87-06 ONETIME AND RECURRINGINSP OF OIL COOLER SPLINES C/W BY DEPOTTEAM AT 583.0 ACFT HRS (UK0000)

20-May-1987 1

APO SF 96271

QC000000

201ST AVN COOCM/ACE PERFORMED AT 609 A/C HRS AT CPHUMPHREYS BY ACE TEAM. AVSCOM SEC ST.LOUIS, MO (UK0000)

16-Jun-1987 1

APO SF 96271

QC000000



8.7.DATE

6.REMARKS

4. 5.



201ST AVN COSOF (GEN-87-02) ONETIME INSPECTION OFACFT RECORDS FOR LOCAL PURCHASE OFTIME CHANGE AIRCRAFT COMPONENTS/PARTS C/W AT 615.8 ACFT HRS (UK0000)

06-Jul-1987 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH60A-87-08 ONETIME INSPECTIONOF MID SECTION BELLCRANK ASSEMBILIESC/W AT 615.8 ACFT HRS BY 377TH MED K-16(UK0000)

06-Jul-1987 2

APO SF 96271

QC000000

201ST AVN COSOF UH-60-87-10 ONETIME INSP OF INPUTFLAGE ASSY C/W AT 681.0 ACFT HRS BY377TH MED K-16 (UK0000)

19-Oct-1987 1

APO SF 96271

QC000000

C 6/159 AVN.SOF UH-60A-89-01 C/W 10 FEB 89 AT 875.0ACFT HRS ONETIME INSP OF T-700 ENGINEG/G STATOR SHROUDS (UK0000)

10-Feb-1988 1

APO NY 09025

QC000000

201ST AVN COSOF UH-60-88-01 ONETIME INSP OF T/R BLADESERIAL # COMPLETED AT 732.2 ACFT HRS(UK0000)

19-Feb-1988 1

APO SF 96271

QC000000

201ST AVN COMWO 55-1520-237-20-86 INSTALLATION OFPBA FIXED LINK ASSY C/W AT 732.2 ACFTHRS (UK0000)

24-Feb-1988 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60A 88-02 ONETIME INSP OF T/RGEARBOX OUTPUT SHAFT C/W AT 741.4 ACFTHRS (UK0000)

29-Mar-1988 1

APO SF 96271

QC000000

201ST AVN COAIRCRAFT MAIN ROTOR HEAD RIGGEDLATERAL PRIMARY SERVO CONTROL RODSHORTENED 5/8 TURN (UK0000)

05-Apr-1988 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60A-88-03 ONETIME INSP OFMAIN MODULE CHAPT SERIAL NUMBERS C/WAT 783.0 ACFT HRS (UK0000)

13-May-1988 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60-88-05 ONETIME ANDRECURRING CALCULATION OF APUOPERATING HOURS AND STARTS C/W AT800.9 ACFT HRS (UK0000)

16-Jun-1988 1

APO SF 96271

QC000000

201ST AVN COOCM/ACE PERFORMED AT 812 A/C HRS AT CPHUMPHREYS BY ACE TEAM AVSCOMOCMSEC, ST.LOUIS, MO (UK0000)

29-Jun-1988 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60-88-07 C/W AT 823.2 ACFT HRSREVISION TO SOF MSG UH-60-88-05CONCERNING OPERATING TIME/STARTCALCULATIONS AND FORMS INFO (UK0000)

15-Jul-1988 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60-88-06 C/W AT 828.0 ACFT HRSASSIGN A TBO OF 2000 HOURS TO THE OILCOOLER BLOWER FOR BEARINGREPLACEMENT (UK0000)

19-Jul-1988 1

APO SF 96271

QC000000

201ST AVN COSOF MSG UH-60-88-09 C/W AT 831.2 ACFT HRSONETIME INSPECTION OF ARAMANUFACTURED CREW SEATS FOR LOOSECLEVIS SCREWS (UK0000)

11-Aug-1988 1

APO SF 96271

QC000000

201ST AVN COGEN-XSOF-88-02 C/W AT 843.0 ACFT HRSONETIME INSPECTION OF INSTALLATION OFCORRECT INTERNAL PORTABLE FIREEXTINGUISHERS (UK0000)

26-Sep-1988 1

APO SF 96271

QC000000



8.7.DATE

6.REMARKS

4. 5.



201ST AVN COSOF MSG UH-60-88-11 C/W AT 860.9 ACFT HRSREVISION TO SOF MSG UH-60-86-18IMMEDIATE RESTRICTION OF REPELLINGOPERATIONS (UK0000)

19-Oct-1988 1

APO SF 96271

QC000000

BCO 1/501ST AVN REGTSOF MSG UH-60-88-10 C/W AT 871.1 ACFT HRSONETIME INSPECTION OF THETROOP/GUNNERS SEAT SUPPORT (H-BAR)BRACKETS, RADIS BLOCKS, BOLTS,WASHERS AND NUTS (UK0000)

31-Oct-1988 1

APO SF 96271

QC000000

BCO 1/501ST AVN REGTSOF MSG UH-60-88-12 C/W AT 871.1 ACFT HRSREVISION TO SOF MSG UH-60-88-10 INSP OFTROOP/GUNNERS SEAT H-BAR ASSY(UK0000)

16-Nov-1988 1

APO SF 96271

QC000000

BCO 1/501ST AVN REGTSOF MSG UH-60-88-13 C/W AT 871.1 ACFT HRSONETIME INSP OF MAIN ROTOR BLADEEXPANDABLE RETENTION PINS PN -70103-08107-101 FOR MISSING SEGMENTS ANDCLEVIS (UK0000)

22-Nov-1988 1

APO SF 96271

QC000000

C 6/159 AVN.SOF UH-60A-88-14 TB 55-1500-237-20-103ONETIME INSP OF ALL UH-60A HIGHPERFORMANCE HOIST SYSTEMS NOTAPPLICABLE THIS MODEL, DESIGN ORSERIES AIRCRAFT (MDS) (UK0000)

26-Dec-1988 1

APO NY 09025

QC000000

C 6/159TH AVNSOF MSG UH-60-89-01 C/W 10 FEB 98 AT 875.0ACFT HR ONETIME INSPECTION OF T-700ENGINE G/G STATOR (UK0000)

10-Feb-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60A-89-02 C/W AT 875.0 AC HRSREVISION TO SOF UH-60A-89-01 (UK0000)

13-Feb-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60A-89-04 C/W 04 APR 89 AT 894.2ACFT HRS REVISION TO SOF UH-60A-89-03ONETIME INSP OF ALL M/R SPINDLES(UK0000)

04-Apr-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60A-89-05 C/W 15 JUN 89 AT 949.3ACFT HRS ONETIME INSP OF FWD WIRESTRIKE PROTECTION PITOT CUTTERINDLES(UK0000)

15-Jun-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60A-89-06 C/W 18 JUL 89 AT 954.6ACFT HRS ONETIME INSP OF L/H + R/H RELAYPANEL GROUND MODULES (UK0000)

19-Jul-1989 1

APO NY 09025

QC000000

C 6/159 AVN.OCM/ACE PERFORMED AT 0958 A/C HRS, ATSCHWABISCH HALL, GE BY ACE TEAMAVSCOM OCMSEC, ST. LOUIS, MO (UK0000)

28-Jul-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF MSG UH-60A-89-07 C/W 9 AUG 89CORRECTION TO SOF UH-60A-89-06 (UK0000)

09-Aug-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF MSG UH-60A-89-08 C/W 16 AUG 89 AT964.7 AC HRS ONETIME OPERATIONAL INSPOF THE FUEL BOOST PUMP HOSEINSTALLATION FOR CONNECTION TOSUMERGED BOOST PUMP (UK0000)

16-Aug-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF MSG UH-60A-89-09 C/W 16 AUG 89 AT964.7 AC HRS CORRECTION OF RETIREMENTLIFE SCHEDULE FOR H-60 RETIREMENT LIFECOMPONENTS (UK0000)

16-Aug-1989 2

APO NY 09025

QC000000



8.7.DATE

6.REMARKS

4. 5.



C 6/159 AVN.SOF MSG UH-60A-89-10 C/W AT 973.8 AC HRSONETIME INSP OF T-700 ENG G/G ROTORSAND STATOR (UK0000)

20-Sep-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60A-89-11 C/W 09 NOV 89 AT 991.8ACFT HRS (UK0000)

09-Nov-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60A-89-12 C/W 28 NOV 89 AT 993.7ACFT HRS ONETIME INSPECTION OF OILCOOLER AXIAL FAN BY NEXT 10HR/14DAYINSPECTION (UK0000)

28-Nov-1989 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60A-89-13 C/W 11 DEC 89 AT 994.8ACFT HRS (UK0000)

11-Dec-1989 1

APO NY 09025

QC000000

C 6/159 AVN.PMS 2 COMPLETED 994.6 ACFT HRS (UK0000) 22-Mar-1990 1

APO NY 09025

QC000000

C 6/159 AVN.TB 55-1520-237-20-104 DATED 30 SEP 89 NEWOVERHAUL/RETIREMENT LIFE SCHEDULEFOR H-60 RETIREMENT LIFE COMPONENTSCOMPLETED 23 MAR 90 (UK0000)

23-Mar-1990 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60-90-01 C/W 18 APR 90 AT 998.6 ACFTHRS ONETIME AND RECURRING INSP OF MAINROTOR BLADE EXPANDABLE PINS (UK0000)

18-Apr-1990 1

APO NY 09025

QC000000

C 6/159 AVN.OCM/ACE PERFORMED AT 1012 AC HRS ATSCHWABISCHHALL GERMANY BY ACE TEAMAVSCOM OCMSEC, ST. LOUIS, MO (UK0000)

15-Aug-1990 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60-90-02 C/W 22 AUG 90 AT 1012.4ACFT HRS ONETIME + RECURRING INSP OFT/R PITCH BEAM RETAINING WASHER(UK0000)

17-Aug-1990 1

APO NY 09025

QC000000

C 6/159 AVN.SOF UH-60-90-02 C/W 22 AUG 90 AT 1012.4ACFT HRS ONETIME INSP OF UPPERPRESSURE PLATE AND SPINDLE TO HUBATTACHMENT BOLTS I/A/W TB 55-1520-237-20-111 (UK0000)

22-Aug-1990 1

APO NY 09025

QC000000

DYNCORPTB 1-1500-237-20-28 BLADE EROSIONPROTECTION C/W BY DYNCORP (UK0000)

16-Dec-1990 1

APO NY 09616

QC000000

C CO 6/159TH AVNPROVISION FOR 12 STATION ICS INSTALLED16 JAN 91 AT 1111.5 ACFT HRS DESERTSTORM (UK0000)

18-Jan-1991 1

APO NY 09684

QC000000

C CO 6/159TH AVNUH-60-91-ASAM-05 C/W 28 FEB 91 AT 1160.0ACFT HRS INSPECTION FOR 4UNSERVICEABLE SPINDLE ASSEMBLIES(UK0000)

28-Feb-1991 1

APO NY 09025

QC000000

C CO 6/159TH AVNTB 55-1520-237-20-119 C/W 3 MAR 91 AT 1162.0AC HR ONETIME REPLACEMENT AND 30HRSPECAIL INSPECTION OF TAIL ROTOR PITCHBEAM RETAINING WASHER (UK0000)

03-Mar-1991 1

APO NY 09025

QC000000

C CO 6/159TH AVNTB 55-1520-237-20-121 C/W 6 MAY 91 AT 1275.2AC HR INTALLATION OF GROUNDPOSITIONING SYSTEM (UK0000)

06-May-1991 1

APO NY 09025

QC000000

AVSCOM SECOCM/ACE PERFORMED AT 1324 AC HRS BYACE TEAM (UK0000)

21-Aug-1991 1

NELLIGEN, GERMANY

QC000000



8.7.DATE

6.REMARKS

4. 5.



CCO 6/159 AVNUH-60A-91-ASAM-10 C/W AT 1334 ACFT HRS 70CT 91 ONETIME INSP + REPLACEMENT OFBRAKE ASSY. PISTON INSULATORS (UK0000)

07-Oct-1991 1

APO NY 09025

QC000000

CCO 6/159 AVNUH-60A-91-ASAM-02 C/W AT 1113.5RECURRING EROSION INSP OF MAIN ROTORBLADE TIP CAP IN DESERT OPERATION(UK0000)

16-Jan-1992 1

APO NY 09025

QC000000

CCO 6/159 AVNUH-60A-91-ASAM-03 C/W AT 1113.5 EXTENDEDTBO HOURS UNDER DESERT SHIELDOPERATIONS FOR UH-60A/L OIL COOLERBLOWER + TAIL ROTOR PITCH CHANGESHAFT BEARINGS (UK0000)

16-Jan-1992 2

APO NY 09025

QC000000

CCO 6/159 AVNUH-60A-92-ASAM-01 C/W AT 1352.6 AC HRS 17JAN 92 INSP FOR 3 UNSERVICEABLE SPINDLEASSEMBLIES (UK0000)

17-Jan-1992 1

APO NY 09025

QC000000

CCO 6/159 AVNTHIS ACFT OPERATED IN SWA (DESERTSHIELD/DESERT STORM) FROM 15 DEC 90 TO25 MAY 91 (UK0000)

17-Jan-1992 2

APO NY 09025

QC000000

CCO 6/159 AVNUH-60A-91-ASAM-04 C/W AT 1190.4 ACFT HRSH-60 AIRCRAFT OPERATION IN SWA (DESERTSTORM) TO PROVIDE GUIDANCE FORSITUATIONS REQUIRING EXCEEDING THERETIREMENT (FINITE) LIFE OF CERTAINCOMPONENTS (UK0000)

20-Mar-1992 1

APO NY 09025

QC000000

CCO 6/159 AVNUH-60A-91-ASAM-06 C/W AT 1308.7 ACFT HRSONETIME INSP OF CARGO HOOK INTERNALROUTE OF WIRE BUNDLE COMPLETED(UK0000)

19-Jul-1992 1

APO NY 09025

QC000000

CCO 6/159 AVNUH-60A-91-ASAM-08 C/W AT 1308.7 ACFT HRSONETIME INSP OF FIRE EXTINGUISHINGSYSTEMS (UK0000)

19-Jul-1992 2

APO NY 09025

QC000000

CCO 6/159 AVNOCM/ACE PERFORMED AT 1445 A/C HRS ATHEIDELBERG,GE BY ACE TEAM AVSCOM. ST.LOUIS, MO. (UK0000)

05-Aug-1992 1

APO NY 09025

QC000000

DYNCORPUH-60-92-ASAM-05 C/W AT 1493 ACFT HRSINSPECTION AND REPLACEMENT OF MAINROTOR BLADE EXPANDABLE PINS PN - 70103-08107-101 (UK0000)

23-Mar-1993 1

APO NY 09274

QC000000

DYNCORPUH-60-92-ASAM-06 C/W AT 1493 ACFT HRSONETIME INSPECTION FOR PROPERHARDWARE ON PEDAL ADJUSTERASSEMBLY PN - 70400-01613 (UK0000)

23-Mar-1993 2

APO NY 09274

QC000000

DYNCORPUH-60-93-ASAM-01 C/W AT 1493 ACFT HRSONETIME OPERATION CHECK OF ALL CHIPDETECTORS (UK0000)

23-Mar-1993 3

APO NY 09274

QC000000

DYNCORPUH-60-93-ASAM-03 C/W AT 1493 ACFT HRSREVISIION OF UH-60-92-ASAM-05 INSP ANDREPLACEMENT OF -101 BLADE PINS (UK0000)

23-Mar-1993 4

APO NY 09274

QC000000

DYNCORPUH-60-93-ASAM-04 C/W AT 1493 ACFT HRSREVISIION OF UH-60-92-ASAM-06 ONETIMEINSP FOR PROPER HDWR ON PEDALADJUSTER PN - 70400-01613 (UK0000)

23-Mar-1993 5

APO NY 09274

QC000000



8.7.DATE

6.REMARKS

4. 5.



DYNCORPUH-60-93-ASAM-06 C/W AT 1493 ACFT HRSONETIME INSP TO REMOVE SUSPECT PITCHBEAM ON TAIL ROTOR SYSTEM (UK0000)

23-Mar-1993 6

APO NY 09274

QC000000

DYNCORPUH-60-93-ASAM-08 C/W AT 1493 ACFT HRSALL H-60 SERIES ACFT PRIOR TO 91-26354CHANGE TO 30 BIAS TAIL ROTOR RIG(UK0000)

23-Mar-1993 7

APO NY 09274

QC000000

DYNCORPPMS-II COMPLETED AT 1492.5 ACFT HRS NEXTDUE AT 1992.5 ACFT HRS (UK0000)

23-Mar-1993 8

APO NY 09274

QC000000

DYNCORPTB 1-1520-237-30-2(STIR) CLEANING ANDINSPECTION REQUIREMENTS C/W AT 1492.5ACFT HRS (UK0000)

23-Mar-1993 9

APO NY 09274

QC000000

BCO 70TH TRANS BNUH-60-93-ASAM-09 ONE TIME MWO CHECKC/W @ 1499.3 ACFT HRS (UK0000)

05-Apr-1993 1

APO AE 09028

QC000000

BCO 70TH TRANS BNUH-60-92-ASAM-01 M/R SPINDLE SERIAL #CHECK C/W @ 1499.3 ACFT HRS (UK0000)

05-Apr-1993 2

APO AE 09028

QC000000

BCO 70TH TRANS BNUH-60-93-ASAM-10 RECURRING INSPECTIONOF ESSS SYSTEM N/A THIS ACFT C/W @1499.3 ACFT HRS (UK0000)

05-Apr-1993 3

APO AE 09028

QC000000

SHAPEUH-60-93-ASAM-11 C/W AT 1503.6 ACFT HRS14 APR 93 INSPECTION & REPLACEMENT OFARA CREW RESTRIANT BUCKLE/CROTCHASSY (UK0000)

14-Apr-1993 1

APO AE 09705

QC000000

SHAPEUH-60-93-ASAM-12 C/W AT 1504.6 ACFT HRSONETIME BRIEFING OF PILOTS,MAINTENANCE OFFICERS, TI'S FOR POSSIBLEACFT VIBE DUE TO SPINDLES (UK0000)

04-May-1993 1

APO AE 09705

QC000000

SHAPEUH-60-93-ASAM-13 C/W AT 1510.1 ACFT HRSOPERATIONAL GL OF ALL H-60 ACFT WITHESSS OR ERFS MISSION KITS INSTALLED N/ATHIS ACFT (UK0000)

07-Jun-1993 1

APO AE 09705

QC000000

SHAPEUH-60-93-ASAM-14 C/W AT 1510.1 ACFT HRSINSP OF ERFS EJECTOR RACKS N/A THISACFT (UK0000)

21-Jun-1993 1

APO AE 09705

QC000000

SHAPEUH-60-93-ASAM-15 C/W AT 1510.1 ACFT HRSCONTINUATION OF ERFS INSP N/A THIS ACFT(UK0000)

22-Jun-1993 1

APO AE 09705

QC000000

SHAPEOCM/ACE PERFORMED AT 1516 AC HRS ATCHIEVRES, BE BY ACE TEAM AVSCOMOCMSEC ST. LOUIS, MO (UK0000)

08-Jul-1993 1

APO AE 09705

QC000000

207TH AVN COUH-60-93-ASAM-16 C/W AT 1519.9 ACFT HRSALL H-60 ACFT ONETIME INSP HYD PUMPKNURLED KNOB PIN (UK0000)

02-Aug-1993 1

APO AE 09102

QC000000

DYN CORPMWO VERIFICATION COMPLETED @ 1225.7ACFT HRS (UK0000)

27-Aug-1993 1

APO AE 09266

QC000000

207TH AVN COENTRY FOR COMPLIANCE OF UH-60-92-ASAM-05 INCORRECT 101 BLADE PINS AREINSTALLED ON ACFT ASAM-05 CAN ONLY BEC/W WHEN 102 PINS ARE INSTALLED (UK0000)

23-Nov-1993 1

APO AE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.



207TH AVN COLATE ENTRY - M/R BLADE EROSIONPROTECTION REMOVED BY DYN CORP OLRDATE AND TIME UNKNOWN (UK0000)

23-Nov-1993 2

APO AE 09102

QC000000

207TH AVN COTB 1-1520-237-20-147 INSTALLATION OF GPSCOMPLETED AT 1599.7 ACFT HRS ANDSUCCESSFUL EMC TEST & DAILY INSP(UK0000)

17-Dec-1993 1

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-01 ALL H-60 ACFT NVGCOMPATIBILITY REWORK OF MASTERWARNING PANEL ASSY (UK0000)

07-Jan-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-03 C/W 1605.2 ACFT HRS ALLH-60 ARMY ACFT ONETIME REFURBISHMENTOF MAIN ROTOR SPINDLE AND REPL OFCERTAIN MAIN ROTOR THRUST BEARING(UK0000)

19-Jan-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-04 C/W 1620.0 ACFT HRS ALLH-60 ARMY ACFT REISSUE OF ONETIME INSPTO REMOVE SUSPECT T/R PITCH BEAMS(UK0000)

14-Feb-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-05 C/W 1620.0 ACFT HRS ALLH-60 BLACKHAWK HELICOPTERS, ONETIMEREMOVAL OF T/R G/B WITH TAIL G/B OUTPUTSHAFT PN - 70358-06620-101 FOR REWORK(UK0000)

14-Feb-1994 2

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-06 C/W 1620.0 ACFT HRSCOCKPIT STANDARDIZATION OF PILOT ANDCOPILOT'S RESTRAINT RELEASE SYSTEM INALL H-60 AIRCRAFT (UK0000)

14-Feb-1994 3

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-07 C/W 1620.0 ACFT HRS ALLH-60 ACFT REVISION TO OVERHAUL ANDRETIRMENT TABLE FOR CERTAINCOMPONENTS DUE N/L/T 9 APR 94 (UK0000)

15-Mar-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-08 C/W 1644.2 AC HRS 15 MAR94 REVISION TO UH-60-94-ASAM-07RECALCULATE NEW OVERHAUL/RETIREMENTLIVES FOR CERTAIN COMPONENTS N/L/T 24MAR 94 @ 1654.2 (UK0000)

15-Mar-1994 2

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-09 C/W 1665.5 AC HRS ALL H-60 AIRCRAFT INSP OF SERIAL NUMBERS FORREMOVAL OF CERTAIN PRIMARY SERVOASSEMBLIES (UK0000)

07-Apr-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-10 ARMY AIRCRAFT THIS IS AREVISION TO (UH-60-94-ASAM-03) ONETIMETIME REFURBISHMENT OF M/R SPINDLE ANDREPLACEMENT OF CERTAIN MAIN ROTORTHRUST BEARINGS (UK0000)

19-Apr-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-94-ASAM-11 MAIN ROTOR BLADE DE-ICE HEATER MAT RESISTANCEMEASUREMENT TEST METHOD UH-60A ANDEH-60 SERIES AIRCRAFT (UK0000)

19-Apr-1994 2

APO AE 09102

QC000000

207TH AVN COOCM/ACE PERFORMED AT 1691 AC HRS OCMSECTION AT HEIDELBERG, GE BY ACE TEAMST. LOUIS (UK0000)

24-May-1994 1

APO AE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.



207TH AVN COTB 1-1520-237-20-143 ABRUPT CHANGES INM/R TRACK/VIBRATIONS ON H-60 ACFTINFORMATION FOR AIRCREWS REVISION TOTB 1-1520-237-20-143 DTD 15 MAY 93 (UK0000)

06-Sep-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-95-ASAM-01 GUIDENCE FOR HOISTINGAND AERIAL RECOVERY OF H-60 AND EH-60ESSS FIXED PROVISIONED ACFT UNTILPUBLISHED CHANGES ARE MADE C/W AT1782.7 ACFT HRS (UK0000)

17-Oct-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-95-ASAM-02 C/W AT 1799.7 ACFT HRSREQUIREMENT TO OPERATE THE FUEL TANKSUBMERGED BOOST PUMPS ON ALL TIMESWITH ALL FUELS DURING GROUND ANDFLIGHT OPERATIONS CHANGES TO ACFT -10AND CHECKLIST (UK0000)

25-Oct-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-95-ASAM-03 ALL H-60 SERIES ACFTSHALL REQUIRE RE-SHIMMING OF THE T/RBLADE PIVOT BEARINGS OF CERTAIN -043BLADE DUE N/L/T 1952.9 ACFT HRS (UK0000)

31-Oct-1994 1

APO AE 09102

QC000000

207TH AVN COASAM C/W @ 1811.5 ACFT HRS, 18 NOV 94 ALLH-60 ACFT REDUCTION OF TORQUE OFSELFRETAINING PIVOT BOLTS AS PER UH-60-95-ASAM-04 DUE N/L/T 22 DEC 94 OR 1831.5ACFT HRS (UK0000)

07-Dec-1994 1

APO AE 09102

QC000000

207TH AVN COTCTO 1H-60-696, ONETIME INSP OF CLAMPINGPROCEDURES OF PILOTS ICS CORD C/W 10DEC 94 (UK0000)

10-Dec-1994 1

APO AE 09102

QC000000

207TH AVN COUH-60-95-SOF-01 ONETIME RECORDS INSP OFTHE T/R G/B C/W 13 DEC 94 @ 1827.0 HRS T/RG/B ULTRASONIC INSP DUE N/L/T 31 MAR 95T/R G/B DUE REPLACEMENT N/L/T 31 DEC 95(UK0000)

13-Dec-1994 1

APO AE 09102

QC000000

BCO 70TH TRANS BNTAIL GEARBOX REPLACEMENT I/A/W UH-60-95-SOF-01 C/W @ 1832.8 ACFT HRS (UK0000)

18-Jan-1995 1

APO AE 09028

QC000000

207TH AVN COUH-60-95-SOF-02 C/W 15 FEB 95 @ 1850.0ACFT HRS CHANGE TO RETIREMENT LIFEFOR CERTAIN M/R BLADE CUFFS (UK0000)

15-Feb-1995 1

APO AE 09102

QC000000

207TH AVN COUH-60-95-ASAM-02 C/W 01 FEB 95 @ 1838.0ACFT HRS CHANGE TO RETIREMENT LIFEFOR SERVO BEAM RAILS (UK0000)

15-Feb-1995 2

APO AE 09102

QC000000

207TH AVN COTB 1-1520-237-20-153 C/W @ 1908.6 ACFT HRSREISSUE OF ONETIME INSP OF T/R PITCHCHANGE SHAFTS (UK0000)

18-May-1995 1

APO AE 09102

QC000000

207TH AVN COUH-60-95-ASAM-06 (TB 1-1520-237-237-20-168)ONETIME INSP FOR CRACKED MAIN XMSNBEAMS UPPER DECK SKIN AND FRAME ANDIMPLEMENTATION OF 100 HR RECURRINGINSP C/W @ 1950.7 ACFT HRS 6 JUL 95(UK0000)

06-Jul-1995 1

APO AE 09102

QC000000

207TH AVN COUH-60-95-ASAM-07 ALL H-60 ACFT TOPROVIDE REVISED CRITERIA FOR SHIMMINGOF TROOP/GUNNER SEATS C/W @ 1977.3ACFT HRS 28 JUL 95 (UK0000)

28-Jul-1995 1

APO AE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.



BCO 70TH TRANSUH-60-95-ASAM-03 RESHIMMING OF CERTAINTAIL ROTOR BLADE PIVOT BEARING C/W @1985.2 ACFT HRS (UK0000)

12-Sep-1995 1

APO AE 09028

QC000000

BCO 70TH TRANSACE/AACE PERFORMED AT 1985 A/C HRS(UK0000)

14-Sep-1995 1

APO AE 09028

QC000000

BCO 70TH TRANSPMS-2 #4 COMPLETED AT 1985.2 ACFT HOURSNEXT PHASE #5 DUE AT 2485.2 ACFT HOURS(UK0000)

30-Oct-1995 1

APO AE 09028

QC000000

BCO 70TH TRANSSOF UH-60-96-01 CHANGE IN RETIREMENTLIFE OF FWD BELLCRANK SPT ASSY. ASSY ISNOT INSTALLED ON ACFT C/W 1985.2 ACFTHRS (UK0000)

07-Nov-1995 1

APO AE 09028

QC000000

DYNCORP OLRSOF UH-60-96-02 ALL H-60 HELICOPTERONETIME INSP OF INBD RETENTION PLATESFOR SN C1324-001 - C1324-150 OR FM00001 -FM00142 N/A THIS A/C AT 1989.2 AC HRS(UK0000)

28-Nov-1995 1

APO AE 09028

QC000000

DYNCORP OLRSOF UH-60-96-03 ALL H-60 A/C CHG OFRETIREMENT LIFE OF M/R CUFF PN - 70150-09109-041 A/C SN'S CHK GOOD SOF C/W 1989A/C HRS (UK0000)

04-Dec-1995 1

APO AE 09028

QC000000

DYNCORP OLRSOF UH-60-96-04 REMOVAL OF SPECIFICSERIAL NUMBERED AFT BELLCRANKSUPPORT ASSEMBLIES C/W @ 1990.2 ACFTHRS (UK0000)

13-Dec-1995 1

APO AE 09028

QC000000

207TH AVN COUH-60-96-ASAM-04 ALL H-60 A/C WITH FASTROPE SYSTEM REDUCTION TO MAX LOAD.N/A THIS A/C C/W @ 2006.8 ACFT HRS(UK0000)

30-Jan-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-96-ASAM-03 REVISION TO ASAM-02,ONETIME INSP TO REMOVE SUSPECT M/RSHAFT NUT BOLTS C/W @ 1998.6 ACFT HRS 18JAN 96 (UK0000)

14-Feb-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-96-ASAM-05 INCREASE IN FATIGUELIFE FOR THE FORWARD SUPPORT ASSY N/ATHIS ACFT C/W @ 2131.4 ACFT HRS (UK0000)

16-Jul-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-96-ASAM-07 CHECK ACFT RECORDSFOR INSTALLED RETENTION RODS WITH PNFROM 33129-3 TO 33129-242 C/W @ 2158.3ACFT HRS (UK0000)

23-Aug-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-96-ASAM-08 INCREASE IN FATIGUELIFE OF T/R INBOARD RETENTION PLATE N/ATHIS ACFT C/W @ 2158.3 ACFT HRS (UK0000)

23-Aug-1996 2

APO AE 09102

QC000000

207TH AVN COUH-60-96-ASAM-09 ONETIME INSP OF STABACTUATTOR CLEVIS LOGGED ON DA FORM2408-18 AT 2174.5 ACFT HRS (UK0000)

13-Sep-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-96-ASAM-10 TB 1-1520-237-20-180ESTABLISH REPLACEMENT TIME FORSPINDLE ELASTOMERIC BEARING LINERCOMP AT 2174.5 ACFT HRS (UK0000)

13-Sep-1996 2

APO AE 09102

QC000000

207TH AVN COUH-60-96-ASAM-11 INCREASE IN FATIGUELIFE OF THE FENN MANUFACTURED M/RBLADE CUFFS. N/A THIS ACFT C/W @ 2179.3ACFT HRS (UK0000)

24-Sep-1996 1

APO AE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.



207TH AVN COOCM/ACE PERFORMED AT 2188 AC HRS ATHEIDELBERG, GE BY ACE TEAM (UK0000)

30-Sep-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-01 ONETIME INSP FORPROPER EDGE BREAKE ON M/R HUBCOMPLETED AT 2212.2 ACFT HRS (UK0000)

16-Oct-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-02 ONETIME INSP TAIL DRIVEFLEXIBLE COUPLING CONNECTIONSCOMPLETED AT 2219.0 ACFT HRS (UK0000)

29-Oct-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-03 ENGINE HISTORICALRECORDS CHECK FOR REPLACEMENT OFUNDAMPED GAS GENERATORROTOR/STATOR ASSY. COMPLETED AT 2224.0ACFT HRS (UK0000)

01-Nov-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-SOF-01 ONETIME INSPECTION OFM/R SWASHPLATE FOR CERTAIN SERIALNUMBER COMPLETED AT 2248.7 ACFT HRS(UK0000)

03-Dec-1996 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-05 ONETIME INSP OF VICOUSDAMPER SUPPORT ASSY COMPLETED AT2268.9 ACFT HRS (UK0000)

09-Jan-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-06 INSP LATERALBELLCRANK ASSY PN - 70400-08150-045COMPLETED AT 2268.9 ACFT HRS (UK0000)

13-Jan-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-08 INSP OF CONNECTINGLINK PN - 70400-08155-056 COMPLETED AT2271.4 ACFT HRS (UK0000)

15-Jan-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-07 INSP OF TAILROTORSERVO FOR SPECIFIC SERIAL NUMBERCOMPLETED AT 2271.4 ACFT HRS (UK0000)

15-Jan-1997 2

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-09 INSP OF MAIN ROTORSHAFT EXTENSIONS COMPLETED AT 2271.7ACFT HRS (UK0000)

27-Jan-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-10 CHANGE TO RETIREMENTLIFE TO MAIN SUPPORT BRIDGE SN - 01201 AITHRU 01686 AI COMPLETED AT 3031.1 ACFTHRS (UK0000)

14-Feb-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-11 CHANGE TO RETIREMENTLIFE FOR CERTAIN MAIN ROTOR BLADECUFFS COMPLETED AT 2298.9 ACFT HRS(UK0000)

06-Mar-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-13 ONETIME INSP OF M/RSPINDLE SPHERICAL ELASTOMERIC BEARINGFOR EXISTENCE OF INNER SLEEVECOMPLETED AT 2337.5 ACFT HRS (UK0000)

09-Jun-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-14 ONETIME INSP AFTBELLCRANK SUPPORT MANUFACTURED BYAMERICAN GENERAL (CAGE 1W160)COMPLETED AT 2376.2 ACFT HRS (UK0000)

22-Aug-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-15 INSP OF MAIN ROTOR P/CLINK ROD END FOR CERTAIN CAGECODE(40137) COMPLETED AT 2376.2 ACFTHRS (UK0000)

22-Aug-1997 2

APO AE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.



207TH AVN COUH-60-97-ASAM-16 INSP OF RECORD ANDCLEVIS CONNECTOR PN - 70400-08151-050COMPLETED AT 2378.2 ACFT HRS (UK0000)

27-Aug-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-17 INSP OF INTERNALRESCUE HOIST BRACKET N/A THIS ACFT ATTHIS TIME COMPLETED AT 2378.2 ACFT HRS(UK0000)

03-Sep-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-18 INSP FOR SPECIFICSUSPECT REWORKED MAIN ROTORSWASHPLATE ASSY. COMPLETED AT 2391.4ACFT HRS (UK0000)

25-Sep-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-97-ASAM-19 ANVIS HUD POWERSUPPLY NOTE: MWO NOT INSTALLEDCOMPLETED AT 2393.1 ACFT HRS (UK0000)

03-Oct-1997 1

APO AE 09102

QC000000

207TH AVN COJACE INSPECTION COMPLETED AT 2396.0 A/CHRS AT HEIDELBERG, GER BY TEAMMEMBERS AMCOM OLR/MWO BRANCHHUNTSVILLE, AL (UK0000)

11-Oct-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-98-ASAM-01 CHANGE IN RETIREMENTLIFE OF CERTAIN M/R SHAFT EXTESIONS(UK0000)

17-Oct-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-98-ASAM-02 ONETIME INSPECTION OFPUSHROD MANUFACTURED BY VERSATILEMACHINE COMPLETED AT 2397.8 ACFT HRS(UK0000)

22-Oct-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-98-ASAM-03 INSPECTION OFSWASHPLATE LINK PN - 70400-08110-54COMPLETED AT 2397.8 ACFT HRS (UK0000)

08-Nov-1997 1

APO AE 09102

QC000000

207TH AVN COUH-60-98-ASAM-04 ONETIME INSP OFOVERHAULED SERVOS COMPLETED AT2447.2 ACFT HRS (UK0000)

18-Mar-1998 1

APO AE 09102

QC000000

207TH AVN COUH-60-98-ASAM-05 REPLACEMENT OFSPECIFIC CAGE CODE AFT SWASHPLATELINK COMPLETED AT 2482.8 ACFT HRS(UK0000)

17-Jun-1998 1

APO AE 09102

QC000000

207TH AVN COJACE INSPECTION COMPLETED AT 2482.8HOURS AT MANNHEIM, GERMANY (UK0000)

08-Jul-1998 1

APO AE 09102

QC000000

207TH AVN COPMS-2#5 COMPLETED AT 2482.8 ACFT HRSNEXT PMS-2#6 DUE AT 2982.8 ACFT HRS(UK0000)

26-Aug-1998 1

APO AE 09102

QC000000

2-502AVN REGTUH-60-98-ASAM-07 INSPECTION FOR SUSPECTL/H TIE ROD COMPLETED AT 2485.8 ACFT HRS(UK0000)

16-Sep-1998 1

APO AE 09028

QC000000

214TH AVN BNUH-60-99-ASAM 01 ONE TIME INSP RECORDSFOR ALL H-60 ACFT CERTAIN P/NSWASHPLATE LINKS MANUFACTURED BYTEK COMPLIED WITH AT 2537.7 ACFT HRS(JW0000)

05-Nov-1998 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-02 (TB 1-1520-248-20-22)ONETIME INSP OF EXTERNAL HOISTPROVISIONS; N/A THIS ACFT AT 2538.2 ACFTHRS (UK0000)

07-Nov-1998 1

APO AE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.



214TH AVN BNUH-60-99-ASAM-03 ONE TIME INSP ENGINERECORDS INSP COMPLIED AT 2540.0 ACFTHRS (JW0000)

10-Nov-1998 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-04 T700-GE-701/701C ENGINEODV RELATED FLAMEOUT N/A THISAIRFRAME (JW0000)

04-Dec-1998 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-05 ONE-TIME INSP OF M/RSPINDLE FOR EXISTENSE OF SLEEVEBEARING COMPLETED AT 2570.2 (UK0000)

15-Dec-1998 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-06 INSPECTION AND REVISEDRETIREMENT LIFE OF MAIN ROTOR PITCHHORNS COMPLETED AT 2520.2 ACFT HRS(UK0000)

16-Dec-1998 1

APO AE 09102

QC000000

214TH AVN BNTB11-1520-237-50 INSTALLATION OF 12 PTSTATION INTERCONNECTING SYSTEM (ICS)APPLIED BY DYN CORP . (JW0000)

12-Mar-1999 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-07 INSP OF M/R HUB (NDI)AND ENRTY ON DA FORM 2408-18 FOR 100HRRECURRING INSP COMPLETED AT 2570.2ACFT HRS (UK0000)

15-Mar-1999 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-08 ALL H-60 ACFT, REVISEDRETIREMENT LIFE OF BELLCRANCKSUPPORT ASSEMBLY PN 70400-08162-042/045/047 MADE BY AIR INDUSTRIES(CAGE8L513). COMPLETED AT 2732.0 ACFTHRS. (BB6264)

14-Jun-1999 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-10 INSP AND PREVENTIVEMAINTENCE ON NUMBER TWO CROSSFEEDBREAKAWAY FUEL VALVE COMPLETE AT2770.0 ACFT HRS (BB6264)

06-Aug-1999 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-09ONE TIME INSP OF M/RBLADE PINS. COMPLETED AT 2777.3 ACFTHRS (BB6264)

12-Aug-1999 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-11 ONE TIME INSP OF T700-GE-701C ENG COMPLETD AT 2777.3 ACFT HRS(BB6264)

16-Aug-1999 1

APO AE 09102

QC000000

214TH AVN BNUH-60-99-ASAM-12 INSP INTERVAL CHANGEON HAMILTON STANDARD H.M.U COMPLETEDAT 2789.4 ACFT HRS (DS1566)

13-Sep-1999 1

APO AE 09102

QC000000

AMCOM-E-OLRHUNTSVILLE, AL

JACE INSP COMPLETED AT 2806 ACFT HRSAT HEIDELBERG GERMANY (UK0000)

08-Oct-1999 1

APO AE 09102

QC000000

E CO 214TH AVN BNUH-60-00-ASAM-01 (TB-1-1520-237-20-15) INSPINTERVAL CHAN OF M/R HUB (NDI) ENTEREDON DA FORM 2408-18 AT 2837.7 ACFTHRS.CFT HRS (SR0259)

12-Nov-1999 1

APO AE 09102

QC000000

214TH AVN BNUH-60-00-ASAM-O2 CYCLIC STICK WIREBUNDLE RELOCATION COMPLETED AT 2837.8(MF2309)

14-Dec-1999 1

APO AE 09102

QC000000

214TH AVN BNUH-60-00-ASAM-O3 ALL H-60 ACFTINSPECTION AND REMOVAL OF SUSPECTPRIMARY SERVO ASSEMBLIES COMPLETEDAT 2870.0 (MF2309)

04-Jan-2000 1

APO AE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.



ECO 214TH AVN BNUH-60-00-ASAM-O4 INSPECT TAIL LANDINGGEAR SHOCK STRUT FOR MISSING BEARINGRETENTION PINS COMPLETED AT 2921.2 ACFTHRS (MF2309)

25-Feb-2000 1

APO AE 09102

QC000000

ECO 214TH AVN BNACE/CPCE PERFORMED AT 2977.1 ACFT HRSAT MANNHEIM, GERMANY BY (MF2309)

12-May-2000 1

APO AE 09102

QC000000

E CO 214TH AVN BNUH-60-00-ASAM-05 INSPECTION OF FIREEXTINGUISHER WIRING COMPLIED WITH ATAVIM (SR0257)

18-May-2000 1

APO AE 09102

QC000000

2-502 AVN REGTUH-60-00-ASAM-06 REVISION TO UH-60-00-ASAM-05 INSP OF FIRE EXTINGUISHERWIRING C/W AT 2977.1 ACFT HRS 20-219COMPLETED AT 2977.1 ACFT HRS (BS9665)

28-Jun-2000 1

APO AE 09028

QC000000

2-502 AVN REGTSOF UH-60-00-01 TECHNICAL, INITIAL ANDRECURRING INSP OF M/R SPINDLE C/W AT2977.1 ACFT HRS (BS9665)

12-Jul-2000 1

APO AE 09028

QC000000

2-502 AVN REGTSOF UH-60-00-02 INSPECTION FOR INPUTMODULE REPAIR AND POTENTIALLYCRACKED BEVEL GEARS C/W AT 2977.1 ACFTHRS (TB6357)

03-Aug-2000 1

APO AE 09028

QC000000

2-502 AVN REGTPMS-2 #6 COMPLETED AT 2977.1 ACFT HRS,NEXT PMS-2 #7 DUE AT 3477.1 ACFT HRSS(TB6357)

14-Aug-2000 1

APO AE 09028

QC000000

E CO 214TH AVN BNUH-60-00-ASAM-07 INSPECT WIRING HARNESSCONNECTING NO 1 AND NO 2 JUNCTIONBOXES IAW UH-60-00-ASAM-07 (TB 1-1520-237-20-24). COMPLETED AT 2987.8 HRS. (CG9711)

05-Sep-2000 1

APO AE 09102

QC000000


01-Dec-2000 1

APO AE 09102

QC000000


06-Jan-2001 1

APO AE 09102

QC000000

1-214TH AVN REGTSOF-UH-60-01-03 (TB 1-1520-237-20-229)INSPECT THE LATERAL SERVO BELLCRANKASSEMBLY COMPLIED WITH AT 3073.0 ACFTHRS (MF2309)

06-Jan-2001 2

APO AE 09102

QC000000

1-214TH AVN REGTSOF-UH-60-01-04 (TB 1-1520-237-20-278)INSPECT FOR INSTALLATION OF FUELMONITORING SYSTEM COMPLIED WITH AT3073.0 ACFT HRS (MF2309)

06-Jan-2001 3

APO AE 09102

QC000000

1-214TH AVN REGTSOF UH-60-01-06 (TB 1-1520-237-23-231)INSPECT SAS ASEMBLIES COMPLETED AT3130.2 ACFT HRS (MF2309)

26-Mar-2001 1

APO AE 09102HEIDELBERG, GE.

QC000000

1-214TH AVN REGTSOF UH-60-01-05 (TB 1-1520-237-20-230)INSPECTION OF M/R SPINDLE (NDI)COMPLETED AT 3133.8 ACFT HRS (JH6726)

25-Apr-2001 1

APO AE 09102

QC000000



8.7.DATE

6.REMARKS

4. 5.



1-214TH AVN REGTSOF UH-60-01-07 (TB 1-1520-237-20-232)INSPECT M/R FLT CONTROL SELF LOCKINGBOLTS COMPLETED AT 3178.1 ACFT HRS.(MF2309)

29-May-2001 1


QC000000

1-214TH AVN REGTSOF UH-60-01-08 (TB 1-1520-237-20-232)INSPECT M/R FLT CONTROL SELF LOCKINGBOLTS COMPLETED AT 3178.1 ACFT HRS(MF2309)

06-Jun-2001 1


QC000000


SOF UH-60-01-09 INSPECT M/R BLADEEXPANDABLE PINS I/A/W (TB 1-1520-237-20-233) COMPLIED WITH AT 3178.1 ACFT HRS(MF2309)

11-Jun-2001 1

HEIDELBERG GE

QC000000

1-214TH AVN REGTSOF UH-60-01-11 INSPECTION OF M/R HUBASSEMBLY AND REVISION OF 200 HOUR NDIINSPECTION COMPLIED WITH AT 3222.2 ACFTHRS. (BH1263)

27-Aug-2001 1

APO AE 09102

QC000000

1-214TH AVN REGTSOF UH-60-01-12 INSPECTION OF M/REXPANDABLE PINS AND REVISION TO TM 1-1520-237-PMS-1 COMPLIED WITH AT 3222.2ACFT HRS (BH1263)

27-Aug-2001 2

APO AE 09102

QC000000

DYNCORP AMCE OLRACE/CPCE PERFORMED AT 3229.6 ACFT HRSAT HEIDELBERG, GE BY MEMBER CC (IK3963)

26-Sep-2001 1

HEIDELBERG, GE

QC000000

1-214 AVN REGTUH-60-02-ASAM-01 INSPECTION OF FAIRINGASSEMBLY ON T/R BLADES COMPLIED WITHAT 3261.6 ACFT HRS. (MF2309)

19-Nov-2001 1

HEIDELBERG GE

QC000000


SOF UH-60-02-01 INSPECTION OF OIL COOLERFAN SHAFT ASSEMBLY COMPLIED WITH AT3267.3 ACFT HRS. (MF2309)

20-Nov-2001 1

HEIDELBERG GE. APOAE 09102

QC000000


SOF UH-60-02-02 MAIN ROTOR HUBSUBASSEMBLY REWORK COMPLIED WITH AT3267.3 ACFT HRS. (MF2309)

26-Nov-2001 1

HEIDELBERG GE

QC000000


SOF UH-60-02-03 INSP OF PITCH TRIMASSEMBLY COMPLIED WITH AT 3282.2 ACFTHRS (MF2309)

07-Dec-2001 1

HEIDELBERG GE

QC000000

2-502 AVN REGTSOF UH-60-02-04 (TB 1-1520-237-20-242)INSPECTION OF APU FUEL LINE GROMMETC/W AT 3295.6 ACFT HRS (LR0306)

25-Jan-2002 1

APO AE 09028

QC000000


SOF UH-60-02-05 (TB 1-1520-237-20-243)INSPECTION OF EXPANDABLE PINS C/W AT3306.1 ACFT HRS (LD8792)

06-Feb-2002 1

APO AE 09705

QC000000


UH-60-02-ASAM-02 (TB1-1520-237-20-246)RECURING INSPECTION OF THECONTROLROD JAM NUTS C/W AT 3306.1 ACFTHRS (LD8792)

11-Feb-2002 1

APO AE 09705

QC000000


UH-60-02-ASAM-03 INSP ENG CONTROLQUADRANT POWER CONTROL LEVER (PCL)C/W AT 3306.1 ACFT HRS (LD8792)

13-Feb-2002 1

APO AE 09705

QC000000

1-214 AVN REGTSOF UH-60-02-06,REVISION TO M/R NDIPROCEDURES COMPLETED AT 3306.3 ACFTHRS. (DS1566)

01-Mar-2002 1


QC000000



8.7.DATE

6.REMARKS

4. 5.




UH-60-02-ASAM-04 RESTRAINT SYSTEMINSPECTION C/W AT 3341.7 ACFT HRS(LD8792)

28-Mar-2002 1

APO AE 09705

QC000000


UH-60-02-ASAM-05 REMOVAL OF CHICAGORAWHIDE M/R SPINDLE THRUST BEARINGSS/N C325-00001-C325-02407 C/W AT 3341.7ACFT HRS (LD8792)

28-Mar-2002 2

APO AE 09705

QC000000


UH-60-02-ASAM-06 (TB 1-1520-237-20-252)INSPECTION OF SWAGE PINS/COLLERSBOOST ASSEMBLIES COMPLIED WITH AT3345.5 ACFT HRS (MF2309)

19-Apr-2002 1

HEIDELBERG GE

QC000000

1-214TH AVN REGTSOF UH-60-02-07,MAIN MODULE PLANETARYCARRIER ASSY COMPLETED AT 3351.2 ACFTHRS (DS1566)

06-May-2002 1


QC000000

1-214TH AVN REGTSOF UH-60-02-08 (TM 1-1520-237-20-255) MAINMODULE PLANETARY CARRIERASSEMBLY.COMPLETED AT 3351.2 ACFT HRS.(DS1566)

06-May-2002 2


QC000000


INSPECT AIRCRAFT I/A/W SOF UH-60-02-09 (TB1-1520-237-20-258) COMPLIED WITH AT 3351.2ACFT HRS (MF2309)

28-May-2002 1

APO AE 09102

QC000000

1-214TH AVN REGTUH-60-02-ASAM-10, INSPECT AERIAL REFUELPROBE NOZZLES.N/A THIS ACFT (DS1566)

02-Jun-2002 1


QC000000

1-214TH AVN REGTSOF UH-60-02-10, INSPECT MAIN MODULEPLANETARY CARRIERASSEMBLY.COMPLETED AT 3352.9 ACFT HRS.(DS1566)

10-Jun-2002 1


QC000000

1-214TH AVN REGTUH-60-02-ASAM-08, INSPECT AN/ARC-220WIRING FOR CHAFING(TB 1-1520-237-20-256)(DS1566)

19-Jun-2002 1


QC000000

1-214TH AVN REGTUH-60-02-ASAM-09,TAIL ROTOR QUADRANTHARDWARE INSTALLATION (TB 1-1520-237-20-257) (DS1566)

19-Jun-2002 2


QC000000

214THSOF UH-60-02-11 INSPECT MAIN ROTORBLADE CUFF ASSEMBLY COMPLIED WITH AT3372.1 ACFT HRS (JV2740)

12-Aug-2002 1

HEIDELBERG

QC000000


SOF UH-60-02-12 INSPECTION OF MAINROTOR BLADE CUFFS COMPLIED WITH AT3372.1 ACFT HRS (MF2309)

13-Aug-2002 1

HEIDELBERG, GE APO-AE 09102

QC000000

AMCOM-E OLRACE/CPCE PERFORMED AT 3433.2 ACFT HRSAT COLEMAN BKS BY CC AND KK (RR2743)

23-Oct-2002 1

HUNTSVILLE AL

QC000000

D CO 1/214TH AVNUH-60-02-ASAM-11 AN/ARC 220(V)AMPLIFIER/COUPLER POWER WIRE MODIFIEDIAW UH-60-02-ASAM-08 COMPLETED AT 3433.2ACFT HRS (MF2309)

24-Oct-2002 1

COLEMAN BKS APO-AE09058

QC000000

2-502 AVN REGTSOF UH-60-03-01 MAIN MODULE PLANETARYCARRIER ASSY PASSED ULTRASONIC TEST(UT) INSPECTION AT 3462.7 ACFT HRS AND2683 MAIN MODULE TSN (LR0306)

20-Nov-2002 1

APO AE 09058

QC000000



8.7.DATE

6.REMARKS

4. 5.



2-502 AVN REGTUH-60-03-ASAM-01 FWD BELLCRANKSUPPORT ASSEMBLY RETIREMENT LIFECOMPLETED AT 3462.7 ACFT HRS (LR0306)

09-Dec-2002 1

APO AE 09058

QC000000

2-502 AVN REGTUH-60-03-ASAM-02 ASSIGN TAIL ROTORSERVO ASSEMBLY RETIREMENT LIFECOMPLETED AT 3462.7 ACFT HRS (LR0306)

09-Dec-2002 2

APO AE 09058

QC000000

2-502 AVN REGTGEN-03-ASAM-01 INSPECTION OF THEBATTERY BOX CY-8515 (ARC-201, ARC-220)COMPLIED WITH AT 3462.7 ACFT HRS(LR0306)

30-Dec-2002 1

APO AE 09058

QC000000

2-502 AVN REGTSOF UH-60-03-02 INSPECTION OF MAINROTOR BLADE CUFF ASSEMBLIES, SEALANTREMOVAL AND PRIMER/PAINT APPLICATIONCOMPLETED AT 3462.7 ACFT HRS (LR0306)

14-Jan-2003 1

APO AE 09058

QC000000

2-502 AVN REGTREPAIRED L/H CABIN CAP ANGLE STA 308.0,BL 34.5 IAW MERA NO: LE-EU001-0983 ANDSIKORSKY PROCEDURE AJM-BL34-1B AT3462.7 ACFT HRS (LR0306)

21-Jan-2003 1

APO AE 09058

QC000000

2-502 AVN REGTREWORKED/MODIFIED ENGINE CONTROLQUADRANT POWER CONTROL LEVERS ANDWIRING IAW TB 1-1520-237-20-245 DURINGPMS-2 AT 3462.7 ACFT HRS (LR0306)

23-Jan-2003 1

APO AE 09058

QC000000

2-502 AVN REGTREPLACED TAIL ROTOR QUADRANTHARDWARE INSTALLATION IAW TB 1-1520-237-20-257 DURING PMS-2 AT 3462.7 ACFT HRS(LR0306)

23-Jan-2003 2

APO AE 09058

QC000000

2-502 AVN REGTPMS-2 #7 COMPLETED AT 3462.7 ACFT HRS,NEXT PMS-2 #8 DUE AT 3962.7 ACFT HRS(LR0306)

12-Feb-2003 1

APO AE 09058

QC000000

2-502 AVN REGTSOF UH-60-03-03 MAIN MODULE PLANETARYCARRIER, SUPERSEDES ACFT FLIGHTRESTRICTIONS AND INCREASES CARRIERMAOT FROM 2000 TO 3700 HRS. COMPLETEDAT 3464.2 ACFT HRS (LR0306)

18-Feb-2003 1

APO AE 09058

QC000000

1-214TH AVNAPPLIED AIRWORTHINESS RELEASE FOR THECOMMUNICATION EAR PLUGS. QUALITATIVEEMC COMPLETED ON UH-60A 87-24642(TS1270)

11-Apr-2003 1

COLEMAN BARRACKSAPO AE 09058

QC000000

AMCOM-E OLRACE/CPCE PERFORMED AT 3519.8 ACFT HRSAT COLEMAN BARRACKS BY KK&F (RR2743)

23-Apr-2003 1

HUNTSVILLE,AL.

QC000000

L-3 COMMSTORMSCOPE INSTALLED I/A/W L3COMMUNICATIONS DRAWING #LEX-1871 AT3604.8ACFT HRS (HA9430)

02-Sep-2003 1

BLUEGRASS ARMYDEPOT,KY

QC000000

214TH AVN REGTCOMPLY WITH REQUIREMENTS OF SOF UH-60-04-01 COMPLIED WITH AT 3629.8 ACFTHOURS (JV2740)

01-Oct-2003 1

COLEMAN BKS

QC000000


UH-60-04-ASAM-01 GLARE SHIELD LIGHTINGCIRCUIT BREAKER REPLACEMENT COMPLIEDWITH AT 3679.8 ACFT HRS (JV2740)

27-Jan-2004 1

COLEMAN BKS 09058

QC000000



8.7.DATE

6.REMARKS

4. 5.



D CO 1/214TH AVNUH-60-04-ASAM-02 INSPECT ALL LOW-TIMEACFT (TAIL NUMBER 03-26982 AND PRIORPLUS 03-26992, 3&4 WITH LESS THAN 2000HRS COMPLIED WITH AT 3730.0 ACFT HRS ON01 APR 04 (JV2740)

01-Apr-2004 1

COLEMAN BKS

QC000000

D CO 1/214TH AVNEMC CHECK FOR GR660 PASSIVE RADIATIONSYSTEM COMPLETED ON ACFT 8926165 ON 13MAY 04 AWR 1149 (JV2740)

13-May-2004 1

COLEMAN BKS

QC000000

D CO 1/214TH AVNSOF UH-60-04-02 COMPLIED WITH. NOTAPPLICABLE TO THIS AIRCRAFT. (JV2740)

09-Jun-2004 1

COLEMAN BKS

QC000000


COMPLY WITH REQUIREMENTS OF UH-60-04-ASAM-04 NLT 26 AUG O4 COMPLIED WITH 13AUG 04 3805.8 ACFT HRS AWR 1149 (DS3908)

16-Aug-2004 1

COLEMAN BKS

QC000000

C CO 1-214TH AVNREGT

SOF UH-60-04-04 C/W AT 3817.6 ACFT HRS(RS1033)

26-Aug-2004 1

GRAFENVOHERGERMANY

QC000000


UH-60-04-ASAM-05 C/W AT 11 NOV 04 3870.2ACFT HRS (DH6671)

21-Sep-2004 1

COLEMAN BARRACKS

QC000000

DCO 1-214 AVNLATE ENTRY COMPLY WITH REQUIREMENTSOF UH-60-04-ASAM-03 NO LATER THAN 15APR O6 SUPERCEEDED BY UH-60-05-ASAM-01(DH6671)

10-Jan-2005 1

COLEMAN

QC000000

DYNCORP E OLR APO09058

ACE/CPCE PERFORMED AT 3954.6 ACFT HRSAT COLEMAN BKS MANNHEIM GE BY ACETEAM MEMBER MM (SH0481)

24-Feb-2005 1

COLEMAN BARRACKS

QC000000

D CO 1/214TH AVNUH-60-05-ASAM-02 C/W 20050304 (BLUEFORCE TRACKER) N/A THIS ACFT (JY2740)

04-Mar-2005 1

COLEMAN BARRACKS

QC000000

D CO 1/214TH AVNUH-60-05-SOF-02 COMPLY WITHREQUIREMENTS OF IMPLEMANTATION OFENHANCED MAINTENANCE PROGRAMCOMPLIED WITH 20050418/3964.1 ACFT HRS(JY2740)

22-Mar-2005 1

COLEMAN BARRACKS

QC000000

D CO 1/214TH AVNUH-60-05-ASAM-01 (FUEL SYSTEM TEST) C/WON 04 ARP 05 AT 3954.6 ACFT HRS DURINGPMS2 (DS3908)

05-Apr-2005 1

COLEMAN BARRACKS

QC000000

D CO 1-214 AVN REGTPMS-2 #8 COMPLETED @ 3954.6 ACFT HRS,NEXT PMS DUE #9 @ 4454.6 ACFT HRS(DS3908)

05-Apr-2005 2

CAAF APO AE 09058

QC000000

D CO 1/214TH AVNUH-60-05-ASAM-03 (SEATBELT INSPECTION)COMPLIED WITH AT 3955.4 ACFT HOURS 11APR 05 (JY2740)

05-Apr-2005 3

COLEMAN BKS

QC000000

D CO 1/214TH AVNUH-60-05-ASAM-04 (TAIL YOKE PN-042 INSP)COMPLIED WITH AT 3955.4 ACFT HRS 11 APR05 (JY2740)

06-Apr-2005 1

COLEMAN BKS

QC000000

D CO 1/214TH AVNT/R BIAS DUE FOR COMPLETION OF PHASEON 11 APR 05 YELLOW-.328 BLACK-.328 RED-.328 BLUE-.360 ACFT HRS 3954.6. (DM5656)

11-Apr-2005 1

COLEMAN BKS

QC000000

D CO 1/214TH AVNUH-60-05-ASAM-05 C/W 20050429 AT 3964.1ACFT HRS (R/H TIE ROD ASSY INSP) (DH6671)

29-Apr-2005 1

COLEMAN BARRACKS

QC000000



8.7.DATE

6.REMARKS

4. 5.



D CO 1-214 AVN REGTUH-60-05-ASAM-06 TROOP SEAT RESTRAINTBUCKLE COMPLETED AT 3979.4 ACFT HRS20050531 (DH6671)

26-May-2005 1

CAAF APO AE 09058

QC000000

D CO 1-214 AVN REGTUH-60-O5-ASAM-07 AIR INTRUSION OFHYDRAULIC SYSTEM COMPLETED AT 3970.1ACFT HRS 20050510 (DH6671)

26-May-2005 2

CAAF APO AE 09058

QC000000

D CO 1-214 AVNCOMPLETED UH-60-05-ASAM-10 AT 4029.7ACFT HRS ON 26 AUG 2005 (DH6671)

26-Aug-2005 1

APO AE09058 CAAF

QC000000

D CO 1-214(M/R HUB) COMPLIED WITH REQUIREMENTSOF UH-60-06-SOF-01 AT 4071.2 ACFT HRS ON21 DEC 05 (DH6671)

20-Dec-2005 1

CAAF

QC000000

D 1/214TH AVNEMC CHECK COMPLETED ON ACFT 8724647ON 20060404 FOR AWR 1159, OPERATION OFINFRARED COUNTERMEASURETRANSMITTER, T1360C(V)1/ALQ-144C(V)PN13301520. (JY2740)

04-Apr-2006 1

CAAF GE 09058

QC000000

D CO 1-214AVNUH-60-06-ASAM-03 (SWASHPLATE) C/W AT4166.0 ACFT HRS. N/A THIS ACFT. (JY2740)

12-Jun-2006 1

CAAF, GE 09058

QC000000

D CO 1-214AVNUH-60-06-ASAM-04 (CABS) COMPLIED WITH AT4187.0 ACFT HOURS. N/A THIS ACFT. (JY2740)

22-Jun-2006 1

CAAF, GE 09058

QC000000

D CO 1-214AVNUH-60-06-SOF-02 (CABS) COMPLIED WITH AT4187.0 ACFT HOURS. N/A THIS ACFT. (JY2740)

23-Jun-2006 1

CAAF, GE 09058

QC000000

D CO 1-214AVNUH-60-06-ASAM-05 (BFT) COMPLIED WITH AT4213.1 ACFT HOURS. N/A THIS ACFT. (JV2740)

01-Aug-2006 1

CAAF, GE 09058

QC000000

D 1/214TH AVNUH-60-07-ASAM-01 (WHITE ENG HARNESS)COMPLIED WITH AT 4306.9 AIRCRAFT HOURS.BOTH ENGINES DISCREPANT (JV2740)

05-Dec-2006 1

CAAF GE 09058

QC000000

D.CO 1/214 AVN REGTUH-60-06-ASAM-02 REPLACED ALL CADIUMPLATED STEEL JAMNUTS WITH SILVERPLATED STAINLESS STEEL JAMNUTS,COMPLIED WITH ON 6 DEC 06 DURING PMI#[email protected] ACFT HRS (ST0266)

06-Dec-2006 1

CAAF GE 09058

QC000000

D.CO 1/214TH AVNREGT

UH-60-06-ASAM-01 (REPLACEMENT OF TAILLANDING STRUT ASSY'S 041, 042, 043)COMPLIED WITH @ 4306.9 ACFT HRS ON 15DEC 06. (ST0266)

15-Dec-2006 1

COLEMAN AAF APO09058

QC000000

D CO 1-214 AVN REGTUH-60-07-ASAM-02, REVISION TO UH-60-07-ASAM-01, COMPLIED WITH AT 4306.9 ACFTHRS. (JK6704)

21-Dec-2006 1


QC000000

D CO 1-214 AVN REGTUH-60-07-ASAM-03, YAW AND COLL BOOSTSERVO ROLL PINS, COMLIED AT 4306.9 ACFTHRS. (JK6704)

21-Dec-2006 2


QC000000

D CO 1-214 AVN REGTPMI# 1 COMPLETED @ 4306.9 ACFT HRS, NEXTPMI # 2 DUE @ 4666.9 ACFT HRS (ST0266)

28-Dec-2006 1

COLEMAN AAF 09058

QC000000

D.CO 1-214 AVN REGTUH-60-07-ASAM-04 VERIFICATION OFAUTOROTATION RPM CHARTS COMPLIEDWITH AT 4306.9 ACFT HRS. ON 29 DEC 06.(ST0266)

29-Dec-2006 1

COLEMAN AAF 09058

QC000000



8.7.DATE

6.REMARKS

4. 5.



D.CO 1-214 AVN REGTUH-60-07-ASAM-05, ARC-220 / KY-100 STARTUP PROCEDURES, COMPLIED WITH AT 4308.2ACFT HRS. ON 24 JAN 07. (ST0266)

24-Jan-2007 1

COLEMAN AAF 09058

QC000000

D.CO 1-214 AVN REGTUH-60-07-ASAM-06 C/W @ 4312.1 ACFT HRS.(HOIST CABLE GUARD DEFECTOR) N/A THISACFT. (JV2740)

07-Feb-2007 1

COLEMAN AAF 09058

QC000000

A CO 1/214TH AVNCOMLIED WITH UH-60-07-AMAM-01 AT 4349.0ACFT HRS, (JK4543)

26-Mar-2007 1

GAAF, 09114

QC000000

D.CO 1-214 AVN REGTUH-60-07-ASAM-07, CEFS STATIC BONDINGJUMPER N/A THIS ACFT C/W @ 4400.2 ACFTHRS (JC4882)

10-May-2007 1

COLEMAN AAF 09058

QC000000

G CO 52ND AVN REGTH-60-07-ASAM-10 (MAIN FUEL MANIFOLDCHAFFING) COMPLETED AND COMPLIEDWITH @ 4483.7 ACFT HOURS (AM7315)

12-Oct-2007 1


QC000000

D.CO 1-214 AVN REGTUH-60-08-AMAM-01 C/W @ 4548.3 ACFT HRS.(MAIN LANDING GEAR SERVICE INSPECTION)(JV2740)

17-Oct-2007 1

COLEMAN AAF 09058

QC000000

G CO 52ND AVN REGTUH-60-08-ASAM-02 (POWER AVAILABLECONTROL CABLE) COMPLETED ANDCOMPLIED WITH AT 4582.6 ACFT HRS(AM7315)

19-Nov-2007 1


QC000000

G CO 52 AVN REGTUH-60-08-AMAM-02 (TAIL ROTOR OUTBOARDRETENTION PLATE SHIMS) INSPECTIONCOMPLETED WITH AND COMPLIED AT 4582.6ACFT HOURS (AM7315)

06-Dec-2007 1


QC000000

G CO 52ND AVN REGTUH-60-08-ASAM-04 (PILOT'S LOWER SEATRAIL CHAFFING ELECTRICAL) COMPLETEDAND COMPLIED WITH AT 4582.6 ACFT HOURS(AM7315)

11-Dec-2007 1


QC000000

G CO 52ND AVN REGTUH-60-08-ASAM-05 COMPLETED ANDCOMPLIED WITH AT 4582.6 ACFT HRS. -18INSPECTION ADDED NEXT DUE 31 JUL 08(AM7315)

12-Dec-2007 1


QC000000

G CO 52ND AVN REGTH-60-08-ASAM-01 (TROOP SEAT UPPERENERGY ATTENUATING WIRES)COMPLETEDAND COMPLIED WITH @ 4582.6 ACFT HOURS(AM7315)

17-Dec-2007 1


QC000000

G CO 52ND AVN REGTUH-60-08-AMAM-03 COMPLETED ANDCOMPLIED WITH @ 4582.6 ACFT HRS.(AB4134)

21-Dec-2007 1


QC000000

G 52 AVN REGTM/R RIG COMPLETED IAW TM 1-1520-237-23FOR MAJOR MAINT-LOW COLL ANGLE=90 8.2180 -1.4 0 -.1 TOTAL -2.2 AVG -.55 -HIGH COLLANGLE= 90 18.3 180 11.7 270 12.6 0 19.1 TOTAL61.7 AVG 15.425 -FWD CYCLIC ANGLE= 90 31.9270 -1.7 TOTAL 33.6 -AFT CYCLIC ANGLE= 9026.3 270 5 TOTAL 21.3 -LEFT CYCLIC ANGLE=180 -7.8 0 7.5 TOTAL 15.3 -RIGHT CYCLICANGLE= 180 7.6 0 -7.1 TOTAL 14.7 -FWD 1/2TURN SHORTER -AFT 1/2 TURN LONGER -LAT3/4 TURN SHORTER.. CHECK WITHINLIMITATIONS (AM7315)

17-Jan-2008 1


QC000000



8.7.DATE

6.REMARKS

4. 5.



G 52 AVN REGTT/R BIAS DUE FOR COMPLETION OF MAJORMAINT. YELLOW-.34 BLACK-.35 RED-.35 BLUE-.35 ACFT HRS 4582.6 (AM7315)

17-Jan-2008 2


QC000000

G CO 52ND AVN REGTUH-60-08-SOF-01 (MAIN ROTOR BLADE PININSP CHANGE) COMPLETED AND COMPLIEDWITH AT 4582.6 ACFT HOURS (AM7315)

29-Jan-2008 1


QC000000

G CO 52ND AVN REGTH-60-08-AMAM-05 GOODRCIH INTERNALRESCUE HOISTS COMPLETED AND COMPLIEDWITH AT 4582.6 ACFT HOURS. (AB4134)

30-Jan-2008 1


QC000000

G CO 52ND AVN REGTH-60-08-ASAM-03 (CHANGES TO FUEL SYSINTEGRITY CHECKS) COMPLETED ANDCOMPLIED WITH @ 4582.6 ACFT HOURS(AM7315)

31-Jan-2008 1


QC000000

G CO 52ND AVN REGTH-60-08-AMAM-06 COMPLIED WITH AT 4585.1ACFT HRS. (AB4134)

06-Feb-2008 1


QC000000

1-214TH AVN REGTCOMPLIED WITH UH-60-08-ASAM-06 MRPYLON SLIDING FAIRING AT 4592.7 ACFT HRS.(AN9260)

05-Mar-2008 1

CAAF,MANNHEIM GE

QC000000

1-214TH AVN REGTCOMPLIED WITH REQUIERMENTS OF H-60-08-AMAM-07, AN/ASN-128/D/B DOPPLER GPSNAVIGATION SET @ 4623 ACFT HRS. LC7577(LC7577)

02-Apr-2008 1


QC000000

1-214TH AVN REGTCOMPLIED WITH REQUIERMENTS OF H-60-08-ASAM-08, ACFT SELF RETAINING FLIGHTCONTROL BOLTS @ 4604.5 ACFT HRS. LC7577(LC7577)

08-Apr-2008 1


QC000000

1-214 AVN REGTCOMPLYED WITH H-06-08-AMAM-08 FLIGHTCONTROL RIGGING UPDATE AT 4640 ACFT.(ST5526)

27-May-2008 1

CAAF MANNHEIM, GE

QC000000


COMPLY WITH REQUIERMENTS OF H-60-08-ASAM-10, ELECTRICAL WIRE CHAFFING AT4663 ACFT HRS. (LC7577)

10-Jul-2008 1


QC000000

TASM-EACE/CPCE PERFORMED AT 4663.3 ACFT HRSAT COLEMAN BARRACKS GERMANY BY ACETEAM MEMBER MM. (SH0481)

30-Jul-2008 1

CAAF, MANNHEIM GE

QC000000


PERMANENT REPAIR COMPLETED IAW MECF69807 DURING PMI PHASE MAINTENANCE AT20080810. (ST5526)

10-Aug-2008 1

CAAF.GERMANY

QC000000

D CO 1-214 AVN REGTCOMPLYED WITH H-60-08-ASAM-11, FLIGHTCONTROL INSP AT 4663.3 ACFT HR (ST5526)

19-Aug-2008 1

CAAF MANNHEIM GE09058

QC000000


UNS-1D WITH APX-118 CONFIGURATION, EMCCHECK PERFORM IAW AWR 1167-R2. UNS-1D,APX-118, CEFS, WX 1000+, 12 POINT ICS, ALQ-144, APR-39, M-130, KY-58 AND 2-AHP MODS.WORKING PROPERLY. (AN9260)

26-Aug-2008 1

CAAF MANNEIM, GE

QC000000



8.7.DATE

6.REMARKS

4. 5.



1-214TH AVN REGTFULL MAIN ROTOR RIG CHECK COMPLETEDON 20080909HIGH COLL ANGLE 15.1FWDCYCLIC ANGLE 33.3AFT CYCLIC ANGLE19LEFT CYCLIC ANGLE 15.6RIGHT CYCLICANGLE 14.2 (LC7577)

09-Sep-2008 1

CAAF, MANNHEIN GE09058

QC000000

1-214TH AVN REGTFULL AIRCRAFT TAIL ROTOR RIGCOMPLETED 20080909RED BLADE BIAS5.16YELLOW BLADE BIAS 5.06BLUE BLADEBIAS 4.47BLACK BLADE BIAS 4.47 (LC7577)

09-Sep-2008 2

CAAF, MANNHEIM GE,09058

QC000000

1-214TH AVN REGTCOMPLETED TAIL ROTOR CABLE TENSIONCHECK 20080909RIGHT HAND 140LEFT HAND140TEMPERATURE 21 DEG C (LC7577)

09-Sep-2008 3


QC000000


COMPLIED WITH REQUIREMENTS OF UH-60-08-ASAM-12, PARKER AEROSPACE AIR TURBINESTARTER AT 4363.3 ACFT HRS. (AN9260)

16-Sep-2008 1

CAAF MANNHEIM, GE

QC000000


COMPLIED WITH H-60-08-ASAM-14 AT 4663.3ACFT HRS ON 20080923 (ENG WIINGHARNESS') (TF6439)

23-Sep-2008 1


QC000000

D CO 1/214 AVN REGTCOMPLIED WITH REQUIREMENTS OF H-60-08-ASAM-13 AT 4663.3 ACFT HOURS ON 20080923(FIRE EXT UNION) (RB3324)

24-Sep-2008 1


QC000000

1-214 AVN REGT.MAIN ROTOR RIG COMPLETED AT 20080909AT 4663 ACFT HOURSCNTRL POS RTFWD LFT AFT TOTAL AVGLOW COLL8.9 -2.7 -10.2 2.1 -1.9 -.475HIGHCOLL 20.2 10.6 9.9 20 60.715.1FWD CYC -2.1 31.233.3AFT CYC 24.9 5.919LFT CYC 8.6 6.815.6RT CYC 7.0 7.214.2PRIMARY SEROVO BIAS: FD +1/2 AFT -1/2LAT 0 (ST5526)

26-Sep-2008 1

CAAF, GERMANY

QC000000

1-214 AVN REGT.T/R RIG COMPLETED AT 20080909 AT 4663ACFT HRT/R CABLE TENSION: RT: 140. LT:140. TEMP: 21CRED BEFOR: 4.84 AFTER:5.16 DIFF: .32YEL BEFOR: 4.72 AFTER: 5.06DIFF: .34BLU BEFOR: 4.13 AFTER: 4.47DIFF: .34BLK BEFOR: 4.13 AFTER: 4.47DIFF: .34 (ST5526)

26-Sep-2008 2

CAAF, GERMANY

QC000000

1-214TH AVN REGTCOMPLY WITH REQUIERMENTS OF H-60-09-SOF-01, HYDRO-MECHANICAL UNIT (HMU) AT4670.3 ACFT HRS. (LC7577)

23-Oct-2008 1


QC000000

1-214TH AVN REGTCOMPLY WITH REQUIERMENTS OF H-60-09-SOF-02, CMWS MWO AT 4684.7 ACFT HRS.(ST5526)

12-Nov-2008 1


QC000000

DCO 1-214 AVN REGTLATE ENTRY COMPLIED WITH H-60-09-SOF-0319 NOV 2008 (POSSIBLE RETIREMENT LIFEOVERFLIGHT)

19-Nov-2008 1


QC000000



8.7.DATE

6.REMARKS

4. 5.



D CO 1-214TH AVNUNS-1D WITH APX-118 CONFIGURATION, EMCCHECK PERFORM IAW AWR 1167-R2. UNS-1D,APX-118, CEFS, WX 1000+, 12 POINT ICS, ALQ-144, APR-39, M-130, KY-58 AND 2-AHP MODS.WORKING PROPERLY. COMPLETED ONAIRCRAFT 8323855

21-Jan-2009 1


RB923324

DCO 1/214TH AVN REGTCOMPLIED WITH REQUIRMENTS OF H-60-09-ASAM-04 AT 4723.6 ACFT HOURS AT 27-FEB-2009

27-Feb-2009 1


ST895526

D CO 1-214TH AVN REGCOMPLIED WITH REQUIREMENTS OF H-60-09-ASAM-05

04-Mar-2009 1


D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-09-ASAM-07 @ 4757.0 ACFT HOURS

27-Apr-2009 1


RB923324

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-09-ASAM-08 4783.3 ACFT HOURS (ENG COWLING)

01-Jun-2009 1


RB923324


COMPLIED WITH REQUIREMENTS OF H-60-09-ASAM-09 ON 01 JUN 09 AT 4783.3 ACFT HRS

01-Jun-2009 2


TF546439

1-214TH AVN REGTCOMPLIED WITH REQUIREMENTS OF H-60-09-AMAM-06 @ 4845.8 ACFT HOURS (CARGOHOOK THRUSTER CAD LIFE REDUCTION)

29-Aug-2009 1

CONSTANTA, ROMANIA

JW829277

D CO 1-214TH AVN REGCOMPLIED WITH REQUIREMENTS OF H-60-09-04 A2C2S

17-Sep-2009 1

NOVO SELO, BULGARIA


H-60-10-AMAM-03 (COCKPIT AIRBAG SYSTEMDEACTIVATION) NOT APPLICABLE THISAIRCRAFT, CABS NOT INSTALLED

10-Nov-2009 1


AM787315

D CO 1-214TH AVN REGH-60-10-AMAM-04 ASN-128B/C DGNS. ACFTNOT IN COMPLIANCE.

16-Nov-2009 1


AMCOM TASM-EUROPEACE/CPCE PERFORMED AT 4935.5 ACFT HRSAT COLEMAN BRKS GERMANY BY ACE TEAMMEMBERS "F" & "MM"

16-Nov-2009 3


TA459908

DCO 1-214 AVN REGTH-60-10-ASAM-03 FIRE BOTTLE DISCHARGELINES AND NOZZLES. ACFT NOT INCOMPLIANCE. -1 ENTRY WAS MADE IAW THISASAM TO REFLECT NON-COMPLIANCEREQUIREMENTS.

16-Nov-2009 4


DG106187



8.7.DATE

6.REMARKS

4. 5.




MEC: F101064 PROBLEM; IAW TM1-1520-237-23-7, WP 0640 00, THE ALLOWABLE MAXIMUMDEPTH OF MATERIAL REMOVAL FROM ALLOVER OTHER OUTER CAST SURFACES OFOUTPUT HOUSING IS 0.030 INCH. REQUESTAUTHORIZATION TO BLEND REPAIR AT THE11 O'CLOCK POSITION SUPPORT FIN ANDADJACENT CORNER USING EXISTING TMINSTRUCTIONS. MAXIMUM DEPTHOF DAMAGEIS 0.075INCH DEEP. NO ACTIVE CORROSIONWAS FOUND IN PITS. WORK WILL BEWORKED ORDERED TO TASM-EUROPE,MANNHEIM, GERMANY.ENGINEERINGDISPOSITION; AUTHORIZATION IS GRANTEDFOR TASM-EUROPE, COLEMAN BARRACKS,MANNHEIM GERMANY IN SUPPORT OF D CO1/214TH AVN, TO REPAIR CORROSIONDAMAGE ON INPUT HOUSING MODULEP/N70351-08001-046, S/N A264-03214 USINGPROCEDURES IAW TM 1-1520-237-23-7, WP0640 00, AQS REQUESTED. LOCALLY BLENDALL PITTED AREAS TO REMOVE SHARPEDGES. RETREAT REPAIRED AREAS WITHCHROMATE PICKLE SOLUTION, PRIME ANDREPAINT IAW TM 1-1500-344-23.JEPHREY L.SOUTH, AEROSPACE ENGINEERAED RDECOMLIAISON ENGINEER-EUROPE, COLEMANBARRACKS, SANDHOFEN, GERMANYDSN 382-5244 LOCAL 0621-779-5244 CELL 0162-296-4461

17-Nov-2009 1


TF546439

1-214TH AVN REGTCOMPLIED WITH REQUIREMENTS OF H-60-09-AMAM-07 (HAND HELD FIRE EXTINGUISHERS)

20-Nov-2009 1

CONSTANTA, ROMANIA

JW829277

D CO 1-214 AVN REGT.FULL MAIN ROTOR RIG COMPLETED AT 28NOV 09 AT 4935.5 ACFT HOURS FORREPLACEMENT OF M/R TRANSMISSION ANDHUB.LOW COLL ANGLE 90DEG 7.9 180DEG -1.8 270 DEG -9.3 0 DEG 1.0 TOT -2.2 AVG -5.5HIGH COLL ANGLE 18.2 11.612.0 18.2 60 15FWD CYCLICANGLE -4.3 30.334.6AFT CYCLIC ANGLE 25.65.6 20.0LEFT CYCLICK ANGLE9.4 6.6 16.0RIGHTCLYCLIC ANGLE 7.1 8.215.3PRIMARY SEROVO BIAS: FD -1/2 AFT +1/2LAT 1

28-Nov-2009 1

CAAF, GERMANY APOAE 09058

AM787315

G CO 52ND AVN REGTONE-TIME FCC CHECK COMPLETED FOR AWR1352 (MPS PASSIVE RADIATION DETECTIONSYSTEM) COMPLETED ON 07 DEC 09 AT4937.0 HRS.

07-Dec-2009 1

STUTTGART, GERMANY

WS756726

G CO 52ND AVN REGTAPPLIED AWR 1352 (MPS PASSIVE RADIATIONDETECTION SYSTEM); TEMPORARY ASWEELL AS PERMANENT INSTALLATION ON 07DEC 09 AT 4937.0 HRS

07-Dec-2009 2

STUTTGART, GERMANY

WS756726


COMPLIED WITH REQUIREMENTS OF UH-60-10-AMAM-05 ON 20090121 AT 4984.0 ACFT HRS

21-Jan-2010 1




8.7.DATE

6.REMARKS

4. 5.



DCO 1-214TH AVN REGTCOMPLIED WITH REQUIREMENTS OF H-6--10-AMAM-11(OIL SAMPLING SCHEDULECHANGES) ON 1FEB 2010 AT 5000.0 ACFT HRS

02-Feb-2010 1


WK439480

TASM-EMEC# F104208TASM-E REPAIRED 1 EACRACK IN SHEAR DECK SKIN AT R/H REARCORNER IAW DMWR 1-1520-237 WP 0168 00AND INSTRUCTIONS PER MEC#F104208.AUTHORIZED BY JEPHREY L. SOUTH,AEROSPACE ENGINEER DSN 382-5244

02-Feb-2010 2


MC651750

D CO 1-214 AVN REGTH-60-ASAM-10-06 COMPLIED WITH THIS DATEAT 5000.0 ACFT HRS, T700-GE-700 ENGINESINSTALLED

10-Feb-2010 1


VZ748391


FUEL FEED SYSTEM VACUUM/PRESSURETEST: INITIAL READING-6.000INHGVACUUMTESTNO.1 FUEL SYSTEM: 20 MIN READING-5.988, FIVE MIN READING-5.986, VACUUMLOSS-0.002 VACUUM LOSS SHOULD BE LESSTHAN OR EQUAL TO .100INHG.NO.2 FUELSYSTEM: 20 MIN READING-6.036, FIVE MINREADING-6.036, VACUUM LOSS-.017.PRESSURE TESTINITIAL READING-30.000PSIGNO.1 FUEL SYSTEM: 20MINREADING-29.992, FIVE MIN READING-29.946.PRESSURE LOSS- .046. PRESS LOSS SHOULDBE LESS THAN OR EQUAL TO .300INHG.NO.2FUEL SYSTEM: 20 MIN READING-29.992, 5MINREADING-29.946, PRESSURE LOSS .046DATETESTED 01 MAR 2010, AMBIENT TEMP 20 DEGCELSIUS.

15-Mar-2010 1


TF546439


PROBLEM:MEC: F104208 DTD 02 FEB 10-A CO.1-214TH GS A/C UH-60A 83-23869 A/C, HRS5000.0, TASM-E RECEIVED A WORK ORDER TOREPAIR SHEAR DECK FOUND CRACK DURINGPHASE INSPECTION. APPROX 1 INCH CRACKIN SHEAR DECK SKIN AT R/H REAR CORNER.ONE PREVIOUS REPAIR ON FWD L/H CORNER.TASM-E REQUEST PERMISSION TO REPAIRI/A/W DMWR 1-1520-237 WP 0168 00. TASM-EHAS THE TOOLS, PERSONNEL AND PARTS TOCOMPLETE THIS TASK.ENGINEERINGDISPOSITION:AUTHORIZATION IS GRANTEDFOR TASM-EUROPE, COLEMAN BARRACKS,MANNHEIM GERMANY TO REPAIR SHEARDECK, P/N 70211-05010-041, ON UH-60A 83-23869 IAW DMWR 1-1520-237 WP 0168 00. THESTAINLESS STEAL REPAIR DOUBLER DOESNOT REQUIRE CADMIUM PLATING; APPLY 2COATS OF MIL-P-23377 PRIMER OREQUIVALENT. ALL FASTENERS AND FAYINGSURFACES ARE TO BE INSTALLED WITH SAE-AMS-S-8802 SEALANT OREQUIVALENT.JEPHREY L. SOUTH,AEROSPACE ENGINEERAED RDECOMLIAISON ENGINEER-EUROPE, COLEMANBARRACKS, SANDHOFEN, GERMANYDSN 382-5244 LOCAL 0621-779-5244 CELL CELL 0162-296-4461

15-Mar-2010 2


TF546439



8.7.DATE

6.REMARKS

4. 5.




MEC F105267:PROBLEM:A CO 1-214TH ACFT83-23869 ACFT HRS 5000.0 TASM-E RECEIVEDFITTING ASSY PN 70219-02116-041 FOROVERSIZE BEYOND LIMITS IN BUSHING BORE.BUSHING BORES MEASURE 0.502 INCH. TASM-E IS REQUESTING AUTHORIZATION TOFABRICATE OVERSIZE BUSHINGS 2 EA ANDINSTALL IN THE FITTING. STANDARDBUSHING PN NAS77-6-012. TASM-E HAS THEFACILITIES, EQUIPMENT AND TRAINEDPERSONEL TO PERFORM THISTASK.ENGINEERINGDISPOSITION:AUTHORIZATION IS GRANTEDFOR TASM-EUROPE, IN SUPPORT OF A CO 1-214TH AVN, TO MANUFACTURE AND INSTALLOVERSIZED P/N NAS77 BUSHING INVIBRATION ABSORBER FITTING P/N 70219-02116-041 ON UH-60A 83-23869 AS FOLLOWS:1) MANUFACTURE OVERSIZED BUSHING IAWNAS77-6-012 SPECIFICATION EXCEPT MAKEOUTSIDE DIAMETER .5023 TO .5030.2) 17-4CRES HEAT TREATED TO H1025 IS ANACCEPTABLE ALTERNATIVE MATERIAL.3)INSTALL PRESS FIT BUSHINGS WET WITH MIL-S-8802 SEALANT IF USING CRES BUSHINGSOR MIL-P-23377 PRIMER IF USING CADPLATED STEEL BUSHINGS.JEPHERY L.SOUTH AEROSPACE ENGINEER AED RDECOMLIAISON ENGINEER-EUROPE, COLEMANBARRACKS, SANDHOFEN, GERMANYDSN 382-5244 LOCAL 0621-779-5244 CELL 0162-296-4461.

15-Mar-2010 3


TF546439



8.7.DATE

6.REMARKS

4. 5.




MEC: F105927-FUSELAGE STRUCTUREA CO 1-214TH ACFT 83-23869 ACFT HRS 5000.0DURING PHASE INSPECTION, DAMAGE WASDISCOVERED TO THE P/N 70500-02070-046PHOENIX DRIP PAN SUPPORT RING. AFTERRING REMOVAL, SEVERAL RIVET HOLESWERE FOUND ELONGATED IN THE R/HTRANSMISSION SUPPORT BEAM. THE SIXTHHOLE FORWARD FROM THE AFT EDGE WASDOUBLED DRILLED. REQUEST ENGINEERINGDISPOSITION AND REPAIRINSTRUCTIONS.ENGINEERINGDISPOSITION:AUTHORIZATION IS GRANTEDFOR 1/214TH AVN, COLEMAN BARRACKS,GERMANY TO REPAIR DAMAGE TO THE RHTRANSMISSION SUPPORT BEAM, P/N 70211-02133-046, ON UH-60A 83-23869 IAW TM 1-1520-237-23 AND AS FOLLOWS:1) THE EIGHTHOLES THAT WERE SLIGHTLY ELONGATEDSHALL BE OPENED UP TO ACCEPT 5/32RIVETS.2) THE ONE HOLE HAT WAS SLIGHTLYFIGURE 8 DRILLED SHALL BE OPENED UP TOACCEPT A 3/16 RIVET.3) THE SIXTH HOLEFROM THE AFT EDGE SHALL BE BLENDED TOREMOVE ALL SHARP EDGES. NO FASTENERWILL BE INSTALLED.4) TREAT AND PRIMEALL REPAIRED HOLES IAW TM 1-1500-344-23.5) DURING INSTALLATION OF DRIP PAN,DO NOT INSTALL A FASTENER IN THECLEANED UP SIXTH HOLE. DO NOT FILL HOLEWITH SEALANT. VISUALLY INSPECT TOPSURFACE OF THE BOTTOM BEAM FLANGEFOR CRACKS IN THE AREA OF DAMAGEDDURING EACH SUBSEQUENT PHASEMAINTENANCE. IF A CRACK IS SUSPECTED,PERFORM NDI IAW TM 1-1520-265-23, NOCRACKS ALLOWED.JEPHREY L. SOUTH,AEROSPACE ENGINEERAED RDECOMLIAISON ENGINEER-EUROPE, COLEMANBARRACKS, SANHOFEN, GERMANYDSN 382-5244 LOCAL 0621-779-5244 CELL 0162-296-4461

15-Mar-2010 4


TF546439

DCO 1-214 AVN REGTAWR 1529 DATED 07OCT09, INTERIMSTATEMENT OF AIRWORTHINESSQUALIFICATION FOR THE INSTALLATION OFTHE FIBER OPTIC GYRO SYSTEM AN1716/A,ATTITUDE HEADING REFERENCE UNIT/SET(AHRU/AHRS) IN DUAL CONFIGURATION ONUH/EH/HH-60A/L ON ALL UH-60A/LHELICOPTERS.

31-Mar-2010 1


QC000000

D CO 214THH-60-10-ASAM-07 STABILATOR HINGEFITTINGS COMPLIED WITH AT 5000.00 ACFTHRS.

26-Apr-2010 1


AH967213


LATE ENTRY: PMI-2 WAS COMPLETED AT4663.3 ACFT HRS IN SEPTEMBER 2008, NEXTPMI-1 DUE AT 5023.3 ACFT HRS.

27-Apr-2010 1


VZ748391



8.7.DATE

6.REMARKS

4. 5.




PMI-1 COMPLETED AT 5000.0 ACFT HRS, NEXTPMI-2 DUE AT 5360.0 ACFT HRS

28-Apr-2010 1


VZ748391

D CO 214THCOMPLIED WITH REQUIREMENTS OF H-60-10-AMAM-12, IMPROVED DRAG BEAM, AT 5003.0ACFTS HRS.

10-May-2010 1


AH967213


H-60-10-ASAM-08, APU AND APU FIREWALL,COMPLIED WITH THIS DATE AT 5003.7 ACFTHRS, PASSED

18-May-2010 1


VZ748391

D CO 1-214TH AVNGSAB

H-60-10-ASAM-09 NOT APPLICABLE TO THISAIRFRAME

07-Jun-2010 1


JB456660

G 52ND AVNCOMPLIED WITH THE REQUIREMENTS OF H-60-10-SOF-02 ON 22 JUN 2010, 5035.6 ACFT HRS.

22-Jun-2010 1

GAAF, GERMANY 09114

AB644134

G 52 AVNH-60-10-AMAM-16 DOESN'T APPLY. NO CMWSINSTALLED.

25-Jun-2010 1

GAAF, GERMANY 09114

AB644134


APPLIED NEW REVISION OF AWR 1451 R2 DTD25 JUN10, CRASHWORTHY EXTERNAL FUELTANK SYSTEM (CEFS) ON UH/HH-60A/LHELICOPTERS

30-Jun-2010 1


VZ748391


H-60-10-ASAM-10 DOES NOT APPLY TO THISACFT(FUEL BOOST PUMPS)

09-Jul-2010 1


WK439480

D C0 214THCOMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-04 (SAS LINKS) AT 5055.0 ACFT HRS.

15-Jul-2010 1


AH967213

D CO 1-214TH AVNH-60-10-ASAM-11, ALL H-60 SERIES AIRCRAFTCOMMON COMPONENT RETIREMENT CHANGETIMES UPDATE, COMPLIED WITH THIS DATE

30-Jul-2010 1


VZ748391

D CO 214THCOMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-12 @ 5064.2 ACFT HRS.(T700 RC TIMECHANGE)

04-Aug-2010 1


AH967213

D CO 1-214TH AVNAWR 1167, R3 DTD 13 AUG 10, AIRCRAFTASSIGNED TO 1-214TH AVN, APPLIED THISDATE

13-Aug-2010 1


VZ748391

DCO 1-214TH AVN REGTCOMPLIED WITH REQUIREMENTS OF H-60-10-ASAM-15 (FUEL VENT ELBOW)

25-Aug-2010 1


WK439480


APPLIED CECOM SUGGESTED SAFETY WIRETO DUAL AHRU THROUGH LOCK RING OF P-1CONNECTOR

30-Aug-2010 1


JB456660



8.7.DATE

6.REMARKS

4. 5.



D CO 1-214TH AVNH-60-10-ASAM-16 (RESCUE HOIST CABLE CUTHARNESS CONNECTOR) NOT APPLICABLE TOTHIS AIRFRAME AT THIS TIME.

09-Sep-2010 1


JB456660

D CO 1-214TH AVNAPPLIED NEW REVISION OF AWR 1529 R1 DTD07 OCT 10 FOR OPERATION OF THE FIBEROPTIC GYRO SYSTEM CN-1716/A, ATTITUDEHEADING REFERECE UNIT/SET (AHRU/AHRS)IN DUAL CONFIGURATION ON UH/EH/HH-60A/LAIRCRAFT

12-Oct-2010 1


VZ748391


H-60-11-ASAM-02 T/R SERVO COTTER PINVERIFICATION COMPLIED WITH ON THIS DATE

20-Oct-2010 1


JB456660

D CO 1-214TH AVNCOMPLIED WITH H-60-11-AMAM-03 ON THISDATE (OIL COOLER) NOT APPLICABLE TOTHIS AIRFRAME

03-Nov-2010 1


JB456660

DCO 214THLATE ENTRY: H-60-09-ASAM-11, CARGO DOORWINDOW EMERGENCY JETTISON HANDLEASSEMBLY, COMPLIED WITH ON 25 JUNE 2009

30-Nov-2010 1


QC000000

DCO 1-214 AVN REGTH-60-11-ASAM-04 (TACAN RECEIVER BEARINGERROR) COMPLIED WITH @ 5131.0 ACFT HR.ACFT DOES NOT HAVE THIS EQUIPMENTINSTALLED.

02-Dec-2010 1


DG106187

D CO 1-214TH AVNH-60-11-AMAM-04 UNIT SCP-6 LEVELLOGISTICS SYSTEM-AVIATION (ENHANCED)INTEGRATED MATERIEL MANAGEMENTCENTER LEGITIMATE CODE FILE CHANGE 61REQUIREMENTS, COMPLIED WITH THIS DATE

06-Jan-2011 1


VZ748391

D CO 1-214TH AVNH-60-11-AMAM-06 MEDEVAC CAROUSELREFURBISHMENT, COMPLIED WITH THISDATE AT 5150.9 ACFT HRS, CAROUSEL NOTINSTALLED

10-Feb-2011 1


VZ748391


AMMUNITION INFORMATION NOTICE (AIN 080-11)(MH92), A/C HRS CHANGE ON MH92 SHELLLIFE FROM 216 TO 222 MONTHSCHANGE ONMH92 INSTALL LIFE FROM 108 TO 114MONTHS

02-Mar-2011 1



AMMUNITION INFORMATION NOTICE (AIN 080-11)(MH92),COMPLETED@ 5175.4 A/C HRSCHANGE ON MH92 SHELL LIFE FROM 216 TO222 MONTHSCHANGE ON MH92 INSTALL LIFEFROM 108 TO 114 MONTHS

02-Mar-2011 2



LATE ENTRY: H-60-11-ASAM-08 (IFF SAFETY)COMPLIED WITH ON 04 MAR 11 , A/C HRS5168.1

07-Mar-2011 1


D CO 1-214TH AVNCOMPLIED WITH H-60-11-AMAM-09 (2408-19-3)ON THIS DATE

05-May-2011 3


JB456660

D CO 1-214TH AVNCOMPLIED WITH H-60-11-AMAM-11 (AWRREVIEW) ON THIS DATE

05-May-2011 4


JB456660



8.7.DATE

6.REMARKS

4. 5.



D CO 1-214TH AVNCLASS II AIRCRAFT WEIGHING COMPLETEDON THIS DATE JB456660

07-Jun-2011 1


JB456660


COMPLIED WITH H-60-11-ASAM-06 (CYCLICSTOPS) ON THIS DATE

16-Jun-2011 1


JB456660


COMPLIED WITH REQUIREMENTS OF H-60-11-SOF-01 ( DISCREPANT SELF LOCKINGDOUBLE HEXAGON NUTS )

09-Jul-2011 2


JR016225


COMPLIED WITH REQUIREMENTS OF H-60-11-ASAM-13 ( ENG AIR INLET ANTI-ICING/MODULATING VALVE)

11-Jul-2011 1


JR016225


COMPLIED WITH H-60-11-ASAM-14 (ENGCOWLING) ON THIS DATE

12-Jul-2011 1


JB456660


COMPLIED WITH H-60-11-AMAM-20 ON THISDATE.

26-Sep-2011 1



COMPLIED WITH REQUIREMENT SOF H-60-11-AMAM-20 ON THIS DATE.

27-Sep-2011 1


D CO214THCOMPLIED WITH THE REQUIREMENTS OF H-60-12-SOF-01 FOR THE ONE TIME INSPECTIONOF THE INTERMEDIATE GEARBOXCOMPLETED AT 5281.3 ACFT HRS.

11-Oct-2011 1


AH967213

D CO 214THCOMPLIED WITH THE REQUIREMENTS OF H-60-12-SOF-02 FOR THE ONE TIME INSPECTIONOF THE INTERMEDIATE GEARBOXCOMPLETED ON THIS DATE.

11-Oct-2011 2


AH967213


AWR 1694 (DUAL STAB AMP), WAS APPLIEDON THIS DATE.

11-Oct-2011 3



COMPLY WITH REQUIREMENTS OF H-60-12-SOF-03 (I/G/B) ON THIS DATE

17-Oct-2011 1


JB456660

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-19 (ULLSA UPDATE 62) ON THIS DATE

01-Nov-2011 1


JB456660

D. CO 1-214COMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-03 TRANSPONDER AND COMMONMISSILE WARNING SYSTEM INSTALLATION.EQUIPMENT NOT INSTALLED ON ACFT.

02-Nov-2011 1


RL172902



8.7.DATE

6.REMARKS

4. 5.



AMCOM/TASM-EACE/CPCE EVALUATION COMPLETED @5340.8 ACFT HRS BY ACE TEAM MEMBER "M"

15-Nov-2011 1


SW233009


COMPLIED WITH MEC FF136761 @5349 ACHOURS. RH PILOT DOOR POST

21-Nov-2011 1


EC579329

TASM-E DYNCORPINTNL

COMPLIED WITH MEC F136756 @ 5340.8 ACHOURS. LH DOOR POST.

21-Nov-2011 2


EC579329

TASM-ECOMPLIED WITH REQUIREMENTS OF H-60-11-AMAM-17 @ 5340.8 ACFT HRS.

22-Nov-2011 1


EW744892

TASM-ECOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-01 TR OUTPUT BEVEL GEAR NDI, @5340.8 ACFT HRS

23-Nov-2011 1


EW744892


COMPLIED WITH MEC F136968 @5340.8 ACHOURS. LH HIRSS BULKHEAD

28-Nov-2011 1


EC579329


COMPLIED WITH THE REQUIREMENTS OF H-60-12-ASAM-02

15-Dec-2011 1


EC579329

TASM-ETAIL ROTOR RIG CHECK COMPLETED IAW WP1052 AT 5340.8 ACFT HRS. PC RODDIMENSIONS ARE RED 5.041-4.711=0.330,BLACK 4.471-4.139=0.332, YELLOW 5.077-4.737=0.340, BLUE 4.452-4.114=0.338. T/RSERVO PISTON TRAVEL IS 3.472 OUT AND0.046 IN. T/R RIG CHECK PERFORMED BYTI:BG856814 AMII: DE743795, RH252603,GG733364

21-Dec-2011 1


BG856814


PMI-2 COMPLETED AT 5340.8 AQCFT HRS,NEXT PMI-1 DUE AT 5700.8 ACFT HRS.

27-Dec-2011 1


EC579329

D CO 1-214TH AVNAWR 1479 R2 DTD 13 JAN 12 FOR UH-60A ANDEH-60A HELICOPTERS WITH MAIN MODULEASSEMBLIES(PART NUMBERS 70351-08100-075 AND 70351-08100-076) EQUIPPED WITHTHE IMPROVED PLANETARY CARRIERASSEMBLY, PART NUMBER 70351-08175-046,APPLIED THIS DATE.

23-Jan-2012 1


LD197314

D CO 1-214TH AVNAWR 1452 R2 DTD 20 JAN 12 FOR ALL UH/HH-60A/L HELICOPTERS EQUIPPED WITH THE LC-6 DIGITAL CHRONOMETER, APPLIED THISDATE.

23-Jan-2012 2


LD197314



8.7.DATE

6.REMARKS

4. 5.



TASM-ETAIL ROTOR RIGG CHECK COMPLETEDAFTER 9-11 HR TORQUE CHECKST/R PITCHCONTROL ROD BIAS= RED: INITIAL 4.6 W/BIAS4.919 DIFF 0.319 BLACK: INITIAL 4.047 W/BIAS4.376DIFF 0.329 YELLOW INITIAL 4.656 W.BIAS4.991 DIFF 0.335 BLUE: INITIAL 4.034 W/BIAS4.363 DIFF 0.329

24-Jan-2012 1


MG003384

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; ISAQ110 R-2 DTD 30 MAR 06 FOR UH-60ALHelicopters Equipped with the Material ValueEngineering (MAVEN) Improved HeatingSystem (Option II Kit)

01-Feb-2012 1


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1159 R-3 DTD 29 JUL 11 FOR Operation of theInfrared Countermeasure Transmitter,T1360C(V)1/ALQ-144C(V), Part NumberA3301520 on UH/HH-60A/L/M Aircraft

01-Feb-2012 2


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1309 R6 DTD 22 APR 11 FOR EH-60A andUH/HH-60A/L/M Helicopters Equipped withOregon Aero Seat Cushions

01-Feb-2012 3


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1348 R6 DTD 17 MAR 11 FOR UH-60A/LHelicopters with the 12 Station Wall MountedIntercommunication System (ICS) or 12 StationVIP Intercom I1 ICS, Auxiliary Communications(Aux Com) Panel and the 8-PointIntercommunication System (ICS) Installed

01-Feb-2012 4


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1529 R2 DTD 7 OCT 11 FOR UH/HH-60A/LHelicopters Equipped with the Attitude HeadingReference Set (AHRS), Dual Attitude HeadingReference Unit (AHRU)

01-Feb-2012 5


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1656 R1 DTD 28 DEC 11 FOR UH/HH-60A/LHelicopters Equipped with the PhoenixModified Drip Pan

01-Feb-2012 6


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1694 DTD 25 FEB 11 for UH/HH-60A/LHelicopters Equipped with the Dual StabilatorController.

01-Feb-2012 7


LD197314

D 1-214 AVNCOMPLIED WITH REQUREMENTS OF H-60-12-SOF-04 MSG DTG 170015Z FEB 12

22-Feb-2012 1


LW849130

D CO 1-214 AVN REGTCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-06 MSG ON THIS DATE

22-Feb-2012 2


RT319476

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1466 DTD 31 AUG 11 R4 FOR THE GARMINGPSMAP 696, 695, 496, 495, 396, 296, OR 295ON US ARMY UH/HH-60A/L/M HELICOPTERS

09-Mar-2012 1


LD197314



8.7.DATE

6.REMARKS

4. 5.



D CO 1-214TH AVNAPPLIED NEW REVISION: AWR 1750 R-1 DTD27MAR12 for Operation of the Aviator's NightVision Imaging System (ANVIS) AN/AVS-6Series Night Vision Goggles (NVG) in UH/HH-60A/L/M Aircraft

28-Mar-2012 1


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1348 R-7 DTD 10 FEB 12 for UH-60AILHelicopters with the 12 Station Wall MountedIntercommunication System (ICS) or 12 StationVIP Intercom II ICS, Auxiliary Communications(Aux Com) Panel and the 8-PointIntercommunication System (ICS) Installed

28-Mar-2012 2


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1309 R7 DTD 10 FEB 12 FOR EH-60A andUH/HH-60A/L/M Helicopters Equipped withOregon Aero Seat Cushions

28-Mar-2012 3


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1513 R3 DTD 26 OCT 11 FOR Use of theIntegrated Performance and AircraftConfiguration (IPAC) Software for PerformancePrediction for UH/HH-60A/L/M Helicopters

28-Mar-2012 4


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1694 R3 DTD 5 JAN 12 for UH/HH-60A/LHelicopters Equipped with the Dual StabilatorController.

28-Mar-2012 5


LD197314

D CO 1-214TH AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1738 DTD 1FEB11 FOR UH-60A/LHELICOPTERS EQUIPPED WITH AN/APX-118COMMON TRANSPONDER (CXP)

28-Mar-2012 6


LD197314

D CO 1-214TH AVNAWR 1348 R-8 DTD 4 MAY 12 for UH-60AILHelicopters with the 12 Station Wall MountedIntercommunication System (ICS) or 12 StationVIP Intercom II ICS, Auxiliary Communications(Aux Com) Panel and the 8-PointIntercommunication System (ICS) Installed

04-May-2012 1


LD197314

D 1-214 AVNCOMPLIED WITH H-60-12-AMAM-09 22-May-2012 1


LW849130

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-12. RESCINDED COMMONCOMPONENTS REMOVAL DATES

20-Jul-2012 1


LD197314

D CO 1-214TH AVNNEW REVISION OF AWR 1348 R-9 DTD 22 JUNE12 for UH-60AIL Helicopters with the 12 StationWall Mounted Intercommunication System (ICS)or 12 Station VIP Intercom II ICS, AuxiliaryCommunications (Aux Com) Panel and the 8-Point Intercommunication System (ICS)Installed

20-Jul-2012 2


LD197314

D CO 1-214TH AVNNEW REVISION OF AWR 1451 R3 DTD 20 JULY12 FOR THE CRASHWORTHY EXTERNAL FUELTANK SYSTEM (CEFS) ON UH/HH-60A/LHELICOPTERS

20-Jul-2012 3


LD197314



8.7.DATE

6.REMARKS

4. 5.




COMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-08

23-Jul-2012 1


RT319476

D CO 1-214TH AVNNEW REVISION AWR 1167 R4 DTD 20 MAR 12for Specified UH-60A/L Helicopters with UNS-1DFlight Management System (FMS), AN/ARC-186Antenna Upgrade, 12 Station ICS Modifications,WX-IOOO+ Stormscope, Auxiliary Heater, VIPInterior Kit, APU Exhaust Deflectors, RollVibration Absorbers, and Passenger StepsInstalled

16-Aug-2012 1


LD197314

1-214TH CADCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-09(RESCUE HOIST CARTRIDGE) ONTHIS DATE

25-Aug-2012 1


JF851776

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-07 (ELECTRICAL WIRING CHAFFE)

17-Sep-2012 1


LD197314

D CO 1-214TH AVNNEW REVISION AWR 1513 R4 DTD 2 JUL 12FOR Use of the Integrated Performance andAircraft Configuration (IPAC) Software forPerformance Prediction for UH/HH-60A/L/MHelicopters

17-Sep-2012 2


LD197314

D CO 1-214THNEW REVISION AWR 1466 DTD 22 AUG 12 R5FOR THE GARMIN GPSMAP 696, 695, 496, 495,396, 296, OR 295 ON US ARMY UH/HH-60A/L/MHELICOPTERS

17-Sep-2012 3


LD197314

D 1-214COMPLIED WITH REQUIRMENTS OF H-60-12-AMAM-15 PITCH TRIM SERVOS

26-Sep-2012 1


LW849130

D 1-214UPDATED AWR 1451 R4 15 OCT 2012 (CEFS)AWR 1513 R4 2 JULY 2012 (IPAC)AWR 1479 R2 13 JAN 2012 (IMPROVEDPLANETARY CARRIER)

13-Nov-2012 1


LW849130

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-12-AMAM-09 (HYDRAULIC LINE CHAFFING)

15-Nov-2012 1


RL172902

D. CO 1-214 AVN REGTCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-02 (AHRS PASS)

19-Nov-2012 1


RL172902

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-03 (DEC/EDECU TURBINE GASTEMPERATRE (TGT) BIAS)

29-Nov-2012 1


LD197314

D. CO 1-214 AVNCOMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-01 (ANTI COLL LIGHT)

27-Dec-2012 1


RL172902


LATE ENTRY; UPDATED AWR 1513 R4 TO 1513R5 DTD 27 NOV 2012

10-Jan-2013 1


RT319476



8.7.DATE

6.REMARKS

4. 5.



D CO 1-214TH AVNSAQ 1479 Final Statement of AirworthinessQualification (SAQ) for the ImprovedPlanetaryCarrier Assembly, Part Number 70351-08175-046, for UH-60A and EH-60A Helicopters

22-Jan-2013 1


LD197314

D CO 1-214TH AVNNEW REVISION ; AWR 1452 R3 DTD 18 JAN 13FOR ALL UH/HH-60A/L HELICOPTERSEQUIPPED WITH THE LC-6 DIGITALCHRONOMETER

22-Jan-2013 2


LD197314


COMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-05 (M/L/G WHEEL BRAKE ASSY)

24-Jan-2013 1


RL172902

D. CO 1-214 AVNLATE ENTRY; PREVIOUSLY APPLIED; AWR1738 R1BDTD 1FEB13 FOR UH-60A/LHELICOPTERS EQUIPPED WITH AN/APX-118COMMON TRANSPONDER (CXP)

11-Feb-2013 1


RL172902

D CO 1-214TH AVNCOMPLIED WITH H-60-13-AMAM-06 ON THISDATE

12-Feb-2013 1


RT319476

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-04 (ULLS-A(E) AMCOM LOGISTICSCENTER (ALC) LCF CHANGE 63REQUIREMENTS)

28-Feb-2013 1


LD197314

TASM-OMain rotor rig completed @ 5606.7 aircrafthours. Primary servos additional bias:Forward:shorten 3 flatsAft: lengthen 3 flatsLateral:shorten 4 flats

28-Feb-2013 2

WIESBADEN, GERMANY

CM567059

TASM-OTail rotor rig completed at 5606.7 aircraft hours.Bias set as follows: Set InitialAdjust Diff FinalRed: -1.6° 4.706"5.034" 0.328" 3.1°Black: -0.1° 4.081"4.381" 0.300" 3.0°Yellow: -0.4° 4.712"5.022" 0.310" 3.1°Blue: -0.9° 4.043"4.345" 0.302" 3.0°

28-Feb-2013 3

WIESBADEN, GERMANY

CM567059

TASM-OComplied with requirements of H-60-13-AMAM-01, Flight Control Rigging, at 5606.7 aircrafthours.

28-Feb-2013 4

WIESBADEN, GERMANY

CM567059

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-12-ASAM-02 ( DRAG BEAM REPLACEMENT )

21-Mar-2013 1


LD197314

D 1-214 AVNCOMPLIED WITH H-60-13-ASAM-04 25-Mar-2013 1


LW849130

D CO 1-214THCOMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-05

09-Apr-2013 1


JR763273


NEW REVISION AWR 1513 R6 DTD 22 MAR 13FOR Use of the Integrated Performance andAircraft Configuration (IPAC) Software forPerformance Prediction for UH/HH-60A/L/MHelicopters

10-Apr-2013 1


RL172902



8.7.DATE

6.REMARKS

4. 5.




APPLIED NEW REVISION: AWR 1750 R-2 DTD29MAR13 for Operation of the Aviator's NightVision Imaging System (ANVIS) AN/AVS-6Series Night Vision Goggles (NVG) in UH/HH-60A/L/M Aircraft

10-Apr-2013 2


RL172902

D 1-214 AVNCOMPLIED WITH H-13-60-AMAM-07 11-Apr-2013 1


LW849130


COMPLIED WITH REQUIREMENTS OF H-60-13-ASAM-06 ( PMI CHECKLIST CHANGES )

08-May-2013 1


RL172902


LATE ENTRY; UPDATED AWR 1452 TO R4 13-May-2013 1


RT319476


COMPLIED WITH REQUIRMENTS OF H-60-13-SOF-01 (AHRS SAFETY)

06-Jun-2013 1


RL172902


COMPLIED WITH REQUIREMENTS OF GEN-13-AMAM-04 (AN/APN 209 COMPONENTTRACKING)

28-Aug-2013 1


JR763273

D CO 1-214TH AVNNEW REVISION AWR 1466 DTD 27 AUG 13 R6FOR THE GARMIN GPSMAP 696, 695, 496, 495,396, 296, OR 295 ON US ARMY UH/HH-60A/L/MHELICOPTERS

18-Sep-2013 1


LD197314

DCO 1-214 AVNCOMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-10 (LCF CHANGE 64)

18-Sep-2013 2


DR622530

D CO 1-214TH AVNLATE ENTRY: NEW REVISION AWR 1167 R5DTD 13 FEB 13 for Specified UH-60A/LHelicopters with UNS-1D Flight ManagementSystem (FMS), AN/ARC-186 Antenna Upgrade,12 Station ICS Modifications, WX-IOOO+Stormscope, Auxiliary Heater, VIP Interior Kit,APU Exhaust Deflectors, Roll VibrationAbsorbers, and Passenger Steps Installed

19-Sep-2013 1


LD197314

B-412 ASBCOMPLIED WITH TBO ITEM AFT BELLCRANKSUPPORT @ ACFT HRS 5701

25-Sep-2013 1

COLEMAN AAF,GERMANY

TO702414

BCO 412 ASB QCCOMPLYED WITH H-60-13-AMAM-15 DURRINGPMI1. ( CRASHWORTHY EXTERNAL FUELSYSTEM (CEFS) ) AIRCRAFT IS NOT MODEDFOR CEFS

25-Sep-2013 2

COLEMAN AAF,GERMANY

JS756224

D CO 1-214TH AVNCOMPLIED WITH GEN-13-AMAM-04 ( AN/APN209 RADAR ALTIMETER SET COMPONENTTRACKING)

30-Sep-2013 1


JR763273



8.7.DATE

6.REMARKS

4. 5.



B CO 412 ASBMAIN ROTOR RIG COMPLETED @5701 ACFTHR ( L.C ANGLE AVG -.575) (H.C ANGLE AVG15.275) L.C.A AVG 7.65) ( RT CYCLE ANGLEAVG 2) PRIMARY SERVO CONTROL ROD BIAS(FWD -1 FLAT, AFT +1 FLAT, LAT +2.5 FLATS)TAIL ROTOR BIAS (RED .326, BLUE .338,YELLOW .333, BLACK .332) T/R CABLETENSION ( L/H 155, R/H 155 ) TEMP 19 DEG (ACFT T/R PISTON TRAVEL OUT 3.51 , IN 0.0 )COMPLETED

18-Nov-2013 1

KATTERBACH,GERMANY

TO702414

D CO 1-214TH AVNCOMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-02 HUMS ACCLEROMETERS.

05-Dec-2013 1


JR763273

TASM-O/DYNCORPINTERNATIONAL

ACE/CPC EVALUATION COMPLETED AT ACFTHRS. 5700.6 BY TEAM MEMBER W.CRISP "S"

03-Jan-2014 1

KATTERBACH,GERMANY

WC643445

B CO. 412TH ASBALL H-60 SERIES AIRCRAFT, MAIN ROTOR(MR) HUB ASSEMBLY, H-60-14-ASAM-04COMPLIED WITH BUT SUSPECT, AT ACFTHRS. 5702

03-Jan-2014 2

KATTERBACH,GERMANY


COMPLIED WITH REQUIREMENT OF H-60-14-AMAM-03 (CONNECTING LINK)

06-Jan-2014 1


RT319476


COMPLIED WITH REQUIREMENTS H-60-ASAM-03: (EIBF)

21-Feb-2014 1


JR763273

D CO. 1-214TH AV REGTCOMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-08 BY 4-JUN-14, (AN/ASC-15ECOMMUNICATION CONSOLE CIRCUITBREAKER PROTECTION)

10-Mar-2014 1


AJ815338

TASM-ORIGHT SIDE BEADED PANEL REPAIRED AT5711.7 AIRCRAFT HOURS IAW TM 1-1520-237-23-6 WP 0398. AIRCRAFT SHOREDINTERNALLY IN LIEU OF DEPOPULATION OFMAIN ROTOR PYLON IAW MEC F180830.

17-Mar-2014 1

WIESBADEN, GERMANY

CM567059

TASM-OENTRY #1 DATED 17-MAR-2014 ENTERED INERROR. BEADED PANEL WAS REPAIRED ON83-23875.

17-Mar-2014 2

WIESBADEN, GERMANY

CM560562


COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-09 BY 25 MAY 14 (MAIN TRANSMISSIONFILTER BOWL AND CHIP DETECTORATTACHMENT HARDWARE)

11-Apr-2014 1


AJ815338

D-CO 1-214TH AVNREGT

COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-10 BY 18 APR 14 (HONTEK COATEDMAIN ROTOR (MR) BLADE REMOVAL) "N/A"

14-Apr-2014 1


JM986195


COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-12 (LIFE EXTENTION OF M/R SPINDLENUT) ON THIS DATE.

22-Apr-2014 1


RS630832



8.7.DATE

6.REMARKS

4. 5.



D CO. 1-214 AVNLATE ENTRY: UPDATED AWR 1159R4 DATED31 JUL 13

25-Apr-2014 1


RO215014

D CO. 1-214 AVNLATE ENTRY: UPDATED AWR 1167R5 DATED31 FEB 13

25-Apr-2014 2


RO215014

D CO. 1-214 AVNUPDATED AWR 1309R8 DATED 14 APR 14 25-Apr-2014 3


RO215014

D CO. 1-214 AVNLATE ENTRY: UPDATED AWR 1466R6 DATED27 AUG 13

25-Apr-2014 4


RO215014

D CO 1-214 AVNLATE ENTRY: UPDATED AWR 1656R2 DATED23 JAN 14

25-Apr-2014 5


RO215014

D CO. 1-214LATE ENTRY: UPDATED AWR 1694R4 DATED 6JAN 14

25-Apr-2014 6


RO215014



25-Apr-2014 7


RS630832



25-Apr-2014 8


RS630832

25-Apr-2014 9



COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-05 (LCF 65) ON THIS DATE.

06-May-2014 1


RS630832


COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-14 (IVHMS CABLING) ON THIS DATE.NOT INSTALLED.

29-May-2014 1


RS630832


COMPLIED WITH REQUIREMENTS OF H-60-14-SOF-03 ON THIS DATE. INSPECTION PASS.

26-Jun-2014 1


RS630832


COMPLIED WITH REQUIREMENTS OF H-60-14-AMAM-16(AHRU) ON THIS DATE

21-Jul-2014 1


BJ963354

D-CO 1-214TH AVN LATE ENTRY: ADDED AWR 1348 R 10 30 APR14

31-Jul-2014 1


JM986195



8.7.DATE

6.REMARKS

4. 5.



D CO 1-214TH AVNREMOVED AWR 1348 R9 22 JUN 12 31-Jul-2014 2


JM986195


ADDED AWR 1513 R7 21 MAY 14 31-Jul-2014 3


JM986195

D CO 1-214TH AVNREMOVED AWR 1513 R6 31-Jul-2014 4


JM986195

D CO 1-214TH AVNADDED AWR 1913 25 OCT 13 (ACN ELETRONICLOGBOOK)

31-Jul-2014 5


JM986195

D CO 1-214TH AVNREMOVED AWR 1648 R 3 (LOGBOOK) 31-Jul-2014 6


JM986195


COMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-09(ENGINE INPUT SHAFTS) ON THISDATE

04-Aug-2014 1


BJ963354


COMPLIED WITH REQUIRMENTS OF H-60-14-ASAM-08 (HMU QUICK DISCONNECT ON THISDATE

05-Aug-2014 1


BJ963354

D CO. 1-214 AVNCOMPLIED WITH H-60-14-SOF-04 (CHECKLIST) 29-Aug-2014 1


RO215014


COMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-10(PLANETARY CARRIER) ON THISDATE

08-Sep-2014 1


BJ963354

AMCOM/TASM-OACE/CPCE PERFORMED AT 5840.4 ACFT.HOURS BY ACE TEAM MEMBERS "A & M".

24-Sep-2014 1


LC735556

D CO. 1-214 AVNCOMPLIED WITH H-60-14-AMAM-19 (LCF 66) 14-Oct-2014 1


RO215014

D CO. 1-214 AVNCOMPLIED WITH H-60-15-AMAM-02 (IVHMSWIRING)

21-Oct-2014 1


RO215014

D CO. 1-214TH AVNREGT.

COMPLIED WITH REQUIREMENTS OF H-60-15-SOF-01. (OIL COOLER FAN AXIAL BEARING)ON THIS DATE.

03-Nov-2014 1


AJ815338


COMPLIED WITH H-60-15-ASAM-01 LEDCAUTION ADVISORY PANEL ON THIS DATE

20-Nov-2014 1


BJ963354



8.7.DATE

6.REMARKS

4. 5.




COMPLIED WITH H-60-15-AMAM-05 (AHRSEMERGENCY PROCEDURES) ON THIS DATE.

12-Dec-2014 1


GM118464


ADDED AWR 1513 R8 DTD 1 DEC 14 30-Dec-2014 1


MN681610


COMPLIED WITH REQUIREMENTS OF H-60-13-AMAM-15 (CEFS R/H FUEL CELL COVERPLATE) ON THIS DATE. INSPECTION FAILEDAND REPAIRS COMPLETED IAW THEADDENDUM. PREVIOUS -15 ENTRY DATE 25SEP 2013 #2 WAS ENTERED IN ERROR. ACFTHAS BEEN MODIFIED WITH MWO 1-1520-237-50-86.

29-Jan-2015 1


RS630832


COMPLIED WITH REQUIREMENTS OF H-60-15-AMAM-06 (IDENTIFICATION OF ASE) ON THISDATE

11-Feb-2015 1


JH103297

CORPUS CHRISTI ARMYDEPOT

AFTER AN AIRCRAFT SHIP TRANSPORT AMTF FOR .5 HOURS ON 07-APR-2015 FROM11:00 TO 11:30 WAS CONDUCTED BY CW2HAYNES, COREY CH311314. THE FLIGHT WASUNABLE TO BE RECORDED USING THESTANDARD METHOD (DA FORM 2408-12), DUETO AN ULLS-A(E) ERROR. DUE TO THISERROR, THE AIRCRAFT HOURS HAVE BEENMANUALLY CHANGED FROM 5874.5 TO5875.0.

01-Jun-2015 1

CORPUS CHRISTI,TEXAS

JL664359

FT HOOD AFMA RASMW

ACE COMPLETED AT 5875 AIRCRAFT HOURSAT FT HOOD TX BY TEAM MEMBERS RR & KI

14-Aug-2015 1

FT HOOD, TX 76544

AS425855

SCIENCE ANDENGINEERINGSERVICES LLC

EFFECTIVE THIS DATE, ACFT TRANSFEREDTO SES, INDUCTED INTO B.E.S.T. PROGRAM

04-Jan-2016 1

HUNTSVILLE

JM866540


H-60-15-ASAM-03, TROOP/GUNNER SEATENERGY ATTENUATORS NOT COMPLIED

08-Jan-2016 1

HUNTSVILLE

ED046014


H-60-15-AMAM-10, "AV-DEC GASKETINSPECTION" NOT COMPLIED WITH

08-Jan-2016 2

HUNTSVILLE

ED046014


H-60-15-AMAM-14, ULLS-A(E) LCF CHANGE 67NOT COMPLIED WITH

08-Jan-2016 3

HUNTSVILLE

ED046014



8.7.DATE

6.REMARKS

4. 5.




H-60-15-AMAM-11, MODE–S TRANSPONDERADDRESS REVIEW NOT COMPLIED WITH

08-Jan-2016 4

HUNTSVILLE

ED046014


H-60-15-AMAM-18,(MEDEVAC)CAROUSEL NOTCOMPLIED WITH

08-Jan-2016 5

HUNTSVILLE

ED046014


H-60-15-SOF-02,FRIES RELEASE CABLE NOTCOMPLIED WITH

08-Jan-2016 6

HUNTSVILLE

ED046014

SCIENCE ANDENGINEERINGSERVICES,LLC

H-60-16-ASAM-01 INBOARD RETENTIONPLATE TORQUE CHECKS NOT COMPLIEDWITH

08-Jan-2016 7

HUNTSVILLE

ED046014


H-60-16-AMAM-01 ENGINE INLET BARRIERFILTER FRAMES NOT COMPLIED WITH

08-Jan-2016 8

HUNTSVILLE

ED046014


H-60-16-AMAM-03, “PERSONNEL LOCATORSET REMOVAL" NOT COMPLIED WITH

08-Jan-2016 9

HUNTSVILLE

ED046014


H-60-16-AMAM-04, T-CLIP INSTALLATION NOTCOMPLIED WITH

08-Jan-2016 10

HUNTSVILLE

ED046014


H-60-16-ASAM-02, DEFECTIVE FUEL HOSESNOT COMPLIED WITH

08-Jan-2016 11

HUNTSVILLE

ED046014




7. FREQUENCY 4.




INSP

A022 03 Mar 201514TM 1-1520-237-23-914 DAY FLYABLE STORAGEENGINE RUN UP

17 Feb 2015D

A092 14 Mar 201530TM 11-6140-203-23&P30 DAY SLAB BATTERYINSPECTION (D8565/11-1)

12 Feb 2015D


19 Feb 2015D


19 Feb 2015D

A103 15 Mar 201530TM 1-1500-344-23AIRCRAFT WASH DUE 13 Feb 2015D

A110 5896.940TM 1-1520-237-PMSPMS 40 HOUR INSPECTION 5856.9H

A115 15 Mar 201530TM 1-1520-237-23-12LUBE REQUIRMENTS 13 Feb 2015D

A115 591140TM 1-1520-237-23-12LUBE REQUIRMENTS 5871H

A116 6200.4360H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

5840.4H

A116 02 Oct 201512H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

02 Oct 2014M

A117 6200.4360H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 5840.4H

A117 02 Oct 201512H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 02 Oct 2014M

A160 17 May 201590TM 1-1520-237-23-1290 DAY CORROSIONINSPECTION

16 Feb 2015D

A177 16 Mar 201590AR 95-190 DAY REVIEW/UPDATE OF 365-4 ENTRIES

16 Dec 2014D

A210 5936.9120TM 1-1520-237-23-12120 HOUR INSPECTIONREQUIREMENTS

5816.9H

A211 6200.4360H-60-10-AMAM-11APU OIL SAMPLE 5840.4H

A211 02 Oct 201512H-60-10-AMAM-11APU OIL SAMPLE 02 Oct 2014M

A213 5936.9120TM 1-2840-248-23ENGINE COMPRESSORCLEANING

5816.9H

A214 5936.9120TM 1-1520-237-23-12CLEAN TAIL WHEEL ADAPTER 5816.9H

A222 09 Jun 2015360TM 1-1680-377-13&PAMSS SURVIVAL KITINSPECTION

14 Jun 2014D

A227 27 Mar 2015120TM 1-1520-237-23-12INSP/CLEAN EJECTOR RACKSMAU-40A, BRU-22A/A

27 Nov 2014D

A230 12 Mar 2015120MWO 1-1520-237-50-77INSPECT BATTERYCOMPARTMENT FORCORROSION (SLAB)

12 Nov 2014D

A295 6060.6360TM 1-1520-237-23-12STABILATOR ACTUATOR ASSYLUBE

5700.6H

A296 6060.6360TM 1-1520-237-23-12STABILATOR INSPECTION 5700.6H






7. FREQUENCY 4.




INSP

A298 6215.3360TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 5855.3H

A298 22 Nov 201512TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 22 Nov 2014M

A299 6215.3360TM 1-1520-237-23-12SWASHPLATE LUBE 5855.3H

A299 22 Nov 201512TM 1-1520-237-23-12SWASHPLATE LUBE 22 Nov 2014M

A320 6060.6360TM 1-2840-248-23ENGINE INSPECTION &CLEANING

5700.6H

A400 6420.6720TM 1-1520-237-PMIPMI-1 5700.6H

A401 6060.8720TM 1-1520-237-PMIPMI-2 5340.8H

A408 6060.8720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-2, AREA 5 AND 6)

5340.8H

A410 6420.6720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-1, AREA 1 THRU 4)

5700.6H

A415 6331.8720H-60-10-AMAM-11MAIN GEARBOX OIL SAMPLE-PART # 073, 074, 076

5611.8H

A440 6060.8720TM 1-1520-237-23-12CLEAN TAIL WHEEL LOCKPIN 5340.8H

A450 6060.8720TM 1-1520-237-23-1CLEAN HSS PNEUMATIC CHECKVALVE

5340.8H

A470 6840.81500TM 1-1520-237-23-12REPLACE NUMBER TWOCROSSFEED VALVE

5340.8H

A471 7500.82160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (FWD)

5340.8H

A472 7500.82160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)

5340.8H

A473 7500.82160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (AFT)

5340.8H

A476 100005000TM 1-1520-237-23-12REPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS

5000H

A477 100005000TM 1-1520-237-23-12REPLACEMENT OF STABILATORACTUATOR BOLTS

5000H

A480 100005000TM 1-1520-237-23-12REPLACE PIVOT BOLT 70400-08159-101,102,103,104

5000H

A485 100005000TM 1-1520-237-23-12REPLACE BELLCRANK BOLT70400-08159-105,106,107,108

5000H

A496 04 Aug 20156TM 1-1500-204-23-1CF3BR FIRE EXTINGUISHERWEIGHT TEST & INSPECTION

04 Feb 2015M

A501 11 Jun 20156TM 1-1520-237-23-12MAIN ROTOR BLADE PRESSURECHECK

11 Dec 2014M

A502 07 May 20156TM 1-1520-237-23-12INSPECT AND TEST GROUNDRECEPTACLE IAW TM 1-1500-204-23

07 Nov 2014M

A530 20 Feb 201612DA PAM 738-751AIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)

20 Feb 2015M






7. FREQUENCY 4.




INSP

A532 04 Feb 201612TM 1-1500-204-23-4COMPASS SWING / RMI 04 Feb 2015M

A533 07 Aug 201512TM 1-1520-237-23-12PITOT STATIC SYSTEMINSPECTION

07 Aug 2014M

A534 27 Jun 201624TM 1-1500-204-23-1FIRST AID KIT INSPECTION 27 Jun 2014M

A538 06 Feb 201612TM 1-1520-237-23-12FAT/OAT GAUGEINSPECTION/TEST

06 Feb 2015M

A541 04 Aug 201512TM 1-1520-237-23, C4REPLACE DIGITAL CLOCKBATTERY

04 Aug 2014M

A553 25 Jul 201512AR 95-1AIRCRAFT WEIGHINGINVENTORY (365-1)

25 Jul 2014M

A571 01 Jan 201860TM 1-1520-237-23-1REPLACE EJECTOR RACKCARTRIDGES, DODIC MD66

01 Jan 2013M

A580 11 Dec 201524TM 11-6140-203-23&PRETURN SLAB TO AVIM FORCAPACITY CHECK (VEREY 24MONTH)

11 Dec 2013M

A621 28 Jun 201524AR 95-1AIRCRAFT WEIGHING CLASS 2 28 Jun 2013M

A625 11 Feb 201860TM 11-6140-203-23&PREPLACEMENT OF SLABBATTERY (SLAB)

11 Feb 2013M


01 Aug 2012M


01 Aug 2012M


01 Aug 2012M


01 Aug 2012M

A648 29 Jul 2023180TM 1-1520-237-23REPLACE T/R SPRING CAPSULEASSY

29 Jul 2008M

A660 01 Feb 201972TB 9-1300-385REPLACE THRUSTEREMERGENCY RELEASE CARGOHOOK, MJ20

01 Feb 2013M

A665 22 Apr 201748H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215

22 Apr 2013M

A670 25 Apr 201848TM 1-1520-237-23-1CABIN TUB INSPECTION 25 Apr 2014M

A673 25 Apr 201748TM 1-1520-237-23-12FUEL CELL CORROSIONINSPECTION

25 Apr 2013M

A675 18 Feb 201748TM 1-1520-237-23-12FLIGHT CONTROL ROD INSP 18 Feb 2013M

A695 6060.8720H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

5340.8H

A695 22 Apr 201848H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

22 Apr 2014M

A755 90009000H-60-10-ASAM-11PC LINK TO SWASHPLATEBOLTS REPLACEMENT

0H






7. FREQUENCY 4.




INSP

E004 09 Mar 201514TM 11-5865-200-12AN/ALQ-144 INSPECTION 23 Feb 2015D

E011 19 Mar 201530TM 9-1095-206-12PDISPENSER GENERAL PURPOSEM130

17 Feb 2015D

E015 02 May 2015180MWO 1-1520-237-50-92ASN 128D DOPPLER GPSBATTERY REPLACEMENT

03 Nov 2014D

E041 23 Aug 201430TM 11-5895-294-12TRANSPONDER MODE 4 CHECK 24 Jul 2014D

E088 15 Mar 201530TM 11-5865-200-12AN/ALQ-144 MONTHLYINSPECTION DUE

13 Feb 2015D

E090 21 Mar 201530GEN-MIM-00-001ALQ-144 HOUR METER READING 19 Feb 2015D

E135 28 Aug 20156TM 11-5821-333-12AN/ARC-201(V) SINCGARSRADIO HUB BATT REPL

28 Feb 2015M

E155 02 May 2015180TM 11-5810-262-23KY-58 BATTERY REPLACEMENT 03 Nov 2014D

E351 26 Jun 20156TM 11-5895-1841-13PREPLACE APX-118TRANSPONDER BATTERY

26 Dec 2014M




08-Jan-2016

T700-GE-700ENGINE ASSY, TURBINE

ALT ETFACT TTV°CTIMENUMBERNG %PRESSFATENGINESERIAL 866 +/- 49. TORQUE10.8.7.6.AIRCRAFT REMARKS11. TGTDATE 12.5.4.

GE-E-307338

3. ENGINE SERIAL NUMBER2. ENGINE MODEL1. NOMENCLATUREReport Date: Page 1 of 1

18-May-2010 8323869 MAX POWER FORINSTALLATION

5000 107 106 197.523985 847

03-Jan-2012 8323869 POST PMI 2 MAX PWR4000 111 110 197.313983 845

04-Feb-2014 8323869 POST PMI5000 106 107 0.9998.124640 846

12-Dec-2008 8724642 POST PMI - 2 ENGINEREPLACEMENT

6000 108 105 199.1-63696 846

10-Jun-2009 8724642 RE-ESTABLISHEDBASELINE

5000 105 103 196.983798 847


T700 SERIES TURBINE ENGINE ANALYSIS CHECK RECORDDA FORM 2408-19-2 E, DEC 91

Page of

1. NOMENCLATURE 2. ENGINE MODEL 3. ENGINE SERIAL NUMBER

4. 6. 7. 8. 9.PRESS

ALT

10. 11. 12.5. TORQUEENGINETIME


FAT TGTDATE REMARKSNG%o. +_C 866 4ACT TTV ETF

DA FORM 2408-19-2, DEC 1991 T700 SERIES TURBINE ENGINE ANALYSIS CHECK RECORDFor use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD LC v1.00

4. 6. 7. 8. 9. 10. 11. 12.5. TORQUEENGINETIME


FAT PRESSALT

TGTDATE REMARKSNG%o. +_C 866 4ACT TTV ETF

APD LC v1.00REVERSE OF DA FORM 2408-19-2, DEC 1991

h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






156001113021502C12D

00UNK386970219-05001-044TAIL CONE FITTING CCCC COND COND

162001231183103A01 2

51885701C0010188570250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001231183103A01 1

05701IA0122370250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001421089003B01 TAIL

04600G002-0131270250-13101-044SHOCK ABSORBER (TAIL) CCCC COND COND

165001285302405A01Z BLUE

26205000A106-0415170106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z

21625840A1060553870106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z RED

5405000R106-0157270106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z BLACK

10575843R1060346270106-08100-046DAMPER ASSY, M/R CCCC COND COND

531501537465205A02H BLUE LEAD


531501537465205A02H YELLOW LAG


531501537465205A02H YELLOW LEAD


531501537465205A02H RED LEAD


531501537465205A02H BLACK LEAD


531501537465205A02H RED LAG


531501537465205A02H BLUE LAG


531501537465205A02H BLACK LAG


161501199764605A03A M/R

47555000MSU4570104-08000-050SWASHPLATE ASSY CCCC COND COND

161501078571806A11 NO.1


161501078571806A11 RIGHT




h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






161501503311506A XMSN

22484936A2650012670351-08100-076MAIN TRANSMISSIONMODULE

CCCC COND COND

161501230621806E NO.1


161501353382506E RIGHT


168001074515206F

01493A005-0059270357-06300-042INTERMEDIATE GEARBOX CCCC COND COND

161501376508906G01

28105103A006-0048270358-06600-046TAIL ROTOR GEARBOXASSY

CCCC COND COND

161501524780506H04 NO.1


CCCC COND COND

161501524780506H04 NO.2


CCCC COND COND

161501081277506H06 1


CCCC COND COND

161501158951706H08 2

04465WG9991-0003470361-03009-047SHAFT ASSY, T/R DRV SEC2

CCCC COND COND

161501082650006H09


CCCC COND COND

161501082650006H09


CCCC COND COND

161501082650006H09


CCCC COND COND

161501083295306H11


CCCC COND COND

161501277910606H12


CCCC COND COND

432001136211807A01 NO.1

04214K5002ABR53023-05PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01

13315352208826ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01 NO.2

03696270865A70652-02300-050PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

481001102247307B05A

05748125623213850-3-1VALVE, SOLENIOD CCCC COND COND

481001102247307B05A NO.1

03696P13543213850-3-1VALVE, SOLENIOD CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






165001084309607B11 REAR CABIN

03696B401-0097570651-03201-102ACCUMULATOR CCCC COND COND

168001342049608B20 CO-PILOT


168001342049608B20 PILOT


611501114969609A01 2

05663114A213228B302-8-DMGENERATOR CCCC COND COND

611501114969609A01 #1

036961120E70550-02031-111GENERATOR CCCC COND COND

161501260074911C21

05379TMD0464374815

70400-02300-046MIXER ASSEMBLY CCCC COND COND

168001261204411D25

28795341B292-0220470400-06641-117STABILATOR ACTUATOR CCCC COND COND

168001261204411D25 LOWER

045830823DL2155M20STABILATOR ACTUATOR CCCC COND COND

599601316274311D26 LEFT

354755473437A70902-02001-048STABILATOR AMPLIFIER CCCC COND COND

599601316274311D26 RIGHT

41955547S1120AB70902-02001-048STABILATOR AMPLIFIER CCCC COND COND

299501496368615A04 ESU


CCCC COND COND

584101245909119E05A 1

057282772KK/NHG7209AC01RECEIVER-TRANSMITTERRADAR

CCCC COND COND

584101245909319E05C

056651895FFA3060591INDICATOR HEIGHT CCCC COND COND

660501503528419E06A 1

057941517765100-20ATTITUDE HEADINGREFERENCE UNIT

CCCC COND COND

661001490516852A

050003404825050-1-001AUTOMAT FLT CONTCOMPUTER

CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE

















Report Date:


00

156001081924402C15J20000

UNK3869 0070209-06051-043TAIL PYLON FITTING 0020000

161501481695305A01A UH-60A6733

A308-00453 3303493670070-10046-055HUB, M/R ROTOR ASSY 005100

161501442692605A01I RED12055


008000

161501442692605A01I BLACK12936


008000

161501442692605A01I BLUE13120

D001-11244 0512070102-08200-069MAIN ROTOR SPINDLEASSY

008000

161501442692605A01I YELL13341

D00112447 0534170102-08200-069MAIN ROTOR SPINDLEASSY

008000

161501074515105A01L12117

C286-00095 6819493670351-08186-043MAIN ROTOR SHAFTEXTENDER

0014000

161501127738805A01T13000

015152-0552 5062506270107-08400-046BIFILAR, M/R ROTORASSY

0013000

161501106190305A0213925


009600

161501106190305A0213925


009600

161501106190305A029629


009600

161501106190305A0211172


009600

161501113818805B0212685

A009-03983 2656534170101-31000-043TAIL ROTOR BLADEASSY

0010000

161501113818805B0211346

A00902802 3865521170101-31000-043TAIL ROTOR BLADEASSY

0010000

161501083681206G01B12718

B25700146 4282500070102-11101-042O/B RETENTION PLATE(T/R)

0012000

414101329342806H236787

C512-00281SB 2994446570361-03005-107FAN AXIAL 19812520

156001129125607A24 YAW14278

B112-05156 3658493670410-02500-049SAS ACTUATOR 0013000

156001129125607A24 ROLL14907

B112-10295 507241470410-02500-049SAS ACTUATOR 0013000

156001129125607A24 PITCH17194

C112-01186 806500070410-02500-049SAS ACTUATOR 0013000













Report Date:


00

161501141753211C236823

233-04095 0466370400-06100-042TAIL ROTOR PITCHCHANGE SHAFT

002160

165001305695411C2519989

B300-02142 71257012227000-17TAIL ROTOR SERVOASSY

0015000

165001143122611D01 AFT28159

B30311458B 19425701274000-1031MAIN ROTOR PRIMARYSERVO

0024400

165001143122611D01 LATERAL25695


0024400

165001143122611D01 FWD24735


0024400

156001158968511D0413000

C345-03139 5702570270400-08102-045AFT BELLCRANK 0013000

156001082921311D0517000

A391-00620 0070400-08112-044AFT TIE ROD SUPTFITTING

0017000

168001164416011D066155

A392-00377 0395570400-08111-042AFT TIE ROD ASSY 002200

156001286887011D0710101

39001917 0570170400-08117-049AFT BELLCRANK SPTASSY

004400

304001287243811D0815936

015152-00790 0493670400-08151-061LATERAL SWASHPLATELINK

0011000

168001221286311D0924663

F337-02977 0466370400-08166-041LATERAL SERVOBELLCRANK

0020000

168001158965311D1111000

B346-00735 5062506270400-08104-048AFT WALKING BEAM 0011000

156001158947511D1313820

E344-01303 3937375770400-08115-045LEFT TIE ROD 0014000

156001296948611D148163

33325-61 0466370400-08114-051RIGHT TIE ROD ASSY 003500

168001158965211D1519663

632 0466370400-08101-046FORWARD BELLCRANK 0015000

156001221261911D1610263

B36704490 0466370400-08162-042FWD BELLCRANK SPTASSY

005600













Report Date:


00







HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 8 of 12

08-Jan-2016

COND COND

156001113021502C12D

00TAIL CONE FITTING UNK386970219-05001-044 CCCC

20000 20000

156001081924402C15J

00TAIL PYLON FITTING UNK386970209-06051-043 00

COND COND

1620012311831 203A01


C0010188570250-12051-045 CCCC

COND COND

1620012311831 103A01


IA0122370250-12051-045 CCCC

COND COND

1620014210890 TAIL03B01

04600SHOCK ABSORBER(TAIL)

G002-0131270250-13101-044 CCCC

5100 6733

1615014816953 UH-60A05A01A

33034936HUB, M/R ROTOR ASSY A308-0045370070-10046-055 00

8000 12055

1615014426926 RED05A01I


A001-0331370102-08200-069 00

8000 12936

1615014426926 BLACK05A01I


A001-0610870102-08200-069 00

8000 13120

1615014426926 BLUE05A01I


D001-1124470102-08200-069 00

8000 13341

1615014426926 YELL05A01I


D0011244770102-08200-069 00

14000 12117

161501074515105A01L

68194936MAIN ROTOR SHAFTEXTENDER

C286-0009570351-08186-043 00

13000 13000

161501127738805A01T

50625062BIFILAR, M/R ROTORASSY

015152-055270107-08400-046 00

COND COND

1650012853024 BLUE05A01Z

26205000DAMPER ASSY, M/R A106-0415170106-08100-046 CCCC

COND COND

165001285302405A01Z

21625840DAMPER ASSY, M/R A1060553870106-08100-046 CCCC

COND COND

1650012853024 RED05A01Z

5405000DAMPER ASSY, M/R R106-0157270106-08100-046 CCCC

COND COND

1650012853024 BLACK05A01Z

10575843DAMPER ASSY, M/R R1060346270106-08100-046 CCCC

9600 13925

161501106190305A02


A007-1399070150-09100-043 00

9600 13925

161501106190305A02


A007-1399170150-09100-043 00

9600 9629

161501106190305A02


A0070070870150-09100-043 00

9600 11172

161501106190305A02


A0070344170150-09100-043 00

COND COND

5315015374652 BLUE LEAD05A02H





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 9 of 12

08-Jan-2016

COND COND

5315015374652 YELLOW LAG05A02H


COND COND

5315015374652 YELLOW LEAD05A02H


COND COND

5315015374652 RED LEAD05A02H


COND COND

5315015374652 BLACK LEAD05A02H


COND COND

5315015374652 RED LAG05A02H


COND COND

5315015374652 BLUE LAG05A02H


COND COND

5315015374652 BLACK LAG05A02H


COND COND

1615011997646 M/R05A03A

47555000SWASHPLATE ASSY MSU4570104-08000-050 CCCC

10000 12685

161501113818805B02


A009-0398370101-31000-043 00

10000 11346

161501113818805B02


A0090280270101-31000-043 00

COND COND

1615010785718 NO.106A11


COND COND

1615010785718 RIGHT06A11


COND COND

1615015033115 XMSN06A


A2650012670351-08100-076 CCCC

COND COND

1615012306218 NO.106E


COND COND

1615013533825 RIGHT06E


COND COND

168001074515206F

01493INTERMEDIATEGEARBOX

A005-0059270357-06300-042 CCCC

COND COND

161501376508906G01

28105103TAIL ROTOR GEARBOXASSY

A006-0048270358-06600-046 CCCC

12000 12718

161501083681206G01B

42825000O/B RETENTION PLATE(T/R)

B2570014670102-11101-042 00

COND COND

1615015247805 NO.106H04


C845-0231770361-08014-041 CCCC

COND COND

1615015247805 NO.206H04


C845-0232670361-08014-041 CCCC

COND COND

1615010812775 106H06


A271-0060470361-03001-045 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 10 of 12

08-Jan-2016

COND COND

1615011589517 206H08


WG9991-0003470361-03009-047 CCCC

COND COND

161501082650006H09


A272-0167870361-05001-045 CCCC

COND COND

161501082650006H09


A272-0169370361-05001-045 CCCC

COND COND

161501082650006H09


A272-0169470361-05001-045 CCCC

COND COND

161501083295306H11


A273-0056570361-05002-045 CCCC

COND COND

161501277910606H12


A274-0053070361-06002-044 CCCC

2520 6787

414101329342806H23

29944465FAN AXIAL C512-00281SB70361-03005-107 1981

COND COND

4320011362118 NO.107A01


K5002ABR53023-05 CCCC

COND COND

432001207722807A01


208826ABR53023-06 CCCC

COND COND

4320012077228 NO.207A01


270865A70652-02300-050 CCCC

13000 14278

1560011291256 YAW07A24

36584936SAS ACTUATOR B112-0515670410-02500-049 00

13000 14907

1560011291256 ROLL07A24

5072414SAS ACTUATOR B112-1029570410-02500-049 00

13000 17194

1560011291256 PITCH07A24

8065000SAS ACTUATOR C112-0118670410-02500-049 00

COND COND

481001102247307B05A

05748VALVE, SOLENIOD 125623213850-3-1 CCCC

COND COND

4810011022473 NO.107B05A

03696VALVE, SOLENIOD P13543213850-3-1 CCCC

COND COND

1650010843096 REAR CABIN07B11

03696ACCUMULATOR B401-0097570651-03201-102 CCCC

COND COND

1680013420496 CO-PILOT08B20


COND COND

1680013420496 PILOT08B20


COND COND

6115011149696 209A01

05663GENERATOR 114A213228B302-8-DM CCCC

COND COND

6115011149696 #109A01

03696GENERATOR 1120E70550-02031-111 CCCC

COND COND

161501260074911C21

05379MIXER ASSEMBLY TMD046437481570400-02300-046 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 11 of 12

08-Jan-2016

2160 6823

161501141753211C23


233-0409570400-06100-042 00

15000 19989

165001305695411C25

7125701TAIL ROTOR SERVOASSY

B300-021422227000-17 00

24400 28159

1650011431226 AFT11D01


B30311458B274000-1031 00

24400 25695

1650011431226 LATERAL11D01


B30301576B70410-02820-054 00

24400 24735

1650011431226 FWD11D01


B30304377B70410-02820-054 00

13000 13000

156001158968511D04

57025702AFT BELLCRANK C345-0313970400-08102-045 00

17000 17000

156001082921311D05

00AFT TIE ROD SUPTFITTING

A391-0062070400-08112-044 00

2200 6155

168001164416011D06

03955AFT TIE ROD ASSY A392-0037770400-08111-042 00

4400 10101

156001286887011D07

05701AFT BELLCRANK SPTASSY

3900191770400-08117-049 00

11000 15936

304001287243811D08

04936LATERAL SWASHPLATELINK

015152-0079070400-08151-061 00

20000 24663

168001221286311D09

04663LATERAL SERVOBELLCRANK

F337-0297770400-08166-041 00

11000 11000

168001158965311D11

50625062AFT WALKING BEAM B346-0073570400-08104-048 00

14000 13820

156001158947511D13

39373757LEFT TIE ROD E344-0130370400-08115-045 00

3500 8163

156001296948611D14

04663RIGHT TIE ROD ASSY 33325-6170400-08114-051 00

15000 19663

168001158965211D15

04663FORWARD BELLCRANK 63270400-08101-046 00

5600 10263

156001221261911D16

04663FWD BELLCRANK SPTASSY

B3670449070400-08162-042 00

COND COND

168001261204411D25

28795341STABILATOR ACTUATOR B292-0220470400-06641-117 CCCC

COND COND

1680012612044 LOWER11D25

04583STABILATOR ACTUATOR 0823DL2155M20 CCCC

COND COND

5996013162743 LEFT11D26

35475547STABILATOR AMPLIFIER 3437A70902-02001-048 CCCC

COND COND

5996013162743 RIGHT11D26

41955547STABILATOR AMPLIFIER S1120AB70902-02001-048 CCCC

COND COND

2995014963686 ESU15A04


06374504587 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 12 of 12

08-Jan-2016

COND COND

5841012459091 119E05A

05728RECEIVER-TRANSMITTER RADAR

2772KK/NHG7209AC01 CCCC

COND COND

584101245909319E05C

05665INDICATOR HEIGHT 1895FFA3060591 CCCC

COND COND

6605015035284 119E06A

05794ATTITUDE HEADINGREFERENCE UNIT

1517765100-20 CCCC

COND COND

661001490516852A

05000AUTOMAT FLT CONTCOMPUTER

3404825050-1-001 CCCC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

9000 9513

165001125090703A01A

41504150PISTON, MAIN L/GEARSTR

P0211770250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

9000 14701

165001125090703A01A

00MAIN SHOCK STRUTPISTON

IA0711870250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

COND COND

3110011589607 RED05A01I02C


COND COND

1615011614373 RED05A01I02


B324-20142SB7001-048 CCCC

13000 17055

5310011269444 RED05A01I04

608608M/R SPINDLE NUT C479-0867570102-08105-102 RCRC

8000 12055

5306014606020 RED05A01I06

608608TIE ROD (M/R SPINDLE) B504-0353738023-10372-101 RCRC

20000 24055

1615012149140 RED05A01I07

492492HORN ASSEMBLY A2411365470102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

COND COND

3110011589607 BLACK05A01I02C


COND COND

1615011614373 BLACK05A01I02

608608ELASTOMERIC BEARING B324-26099SB7001-048 CCCC

13000 17936

5310011269444 BLACK05A01I04

00M/R SPINDLE NUT C4791208070102-08105-102 RCRC

8000 12936

5306014606020 BLACK05A01I06


20000 24936

1615012149140 BLACK05A01I07

00HORN ASSEMBLY E241-0016470102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

COND COND

3110011589607 BLUE05A01I02C


COND COND

1615011614373 BLUE05A01I02


C324-07855SB7001-048 CCCC

13000 18120

5310011269444 YELLOW05A01I04

00M/R SPINDLE NUT F479-0364670102-08105-102 RCRC

8000 13120

5306014606020 YELLOW05A01I06

00TIE ROD (M/R SPINDLE) C504-0983238023-10372-101 RCRC

20000 25120

1615012149140 BLUE05A01I07






HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

COND COND

3110011589607 YELL05A01I02C


COND COND

1615011614373 YELLOW05A01I02


B324-18819SB7001-048 CCCC

13000 18341

531001126944405A01I04

00M/R SPINDLE NUT F4790530270102-08105-102 RCRC

8000 13341

530601460602005A01I06


20000 25341

161501214914005A01I07






HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

COND COND

1560014479774 BLUE05A02E


5000 9325

161501099234105A02I

00M/R BLADE CUFF G237-0042670150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

COND COND

1560014479774 YELLOW05A02E


5000 9325

1615010992341 YELLOW05A02I

00M/R BLADE CUFF E237-0039970150-09109-041 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

COND COND

156001447977405A02E


5000 6139

161501099234105A02I






HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

COND COND

156001447977405A02E


5000 9632

161501099234105A02I






HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




Report Date:

Page 1 of 2

08-Jan-2016

COND COND

161501087160205A03A01

55954755STATIONARYSWASHPLATE

D2220005070104-08010-044 CCCC

11000 16000

161501357508905A03A02

04755ROTATINGSWASHPLATE

151520150670104-08001-045 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

17000 21936

1615010785711 TRANS06A08

02248SWASHPLATE GUIDE F4250050370351-08227-041 RCRC

3000 6794

161501110149106A13

11422248MAIN GEARBOXHOUSING ASSY

F2110007470351-08110-045 RCRC

7600 12536

3040014158388 XMSN06A18

02248MAIN ROTOR SHAFT E2530461470351-08131-048 RCRC

12000 16751

1615014977257 TRANS06A19

1852248PLANETARY CARRIERASSY

A2400192270351-08175-046 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

12000 17341

161501074515306G01C

03048I/B RETENTION PLATET/R

FM270070358-06612-042 RCRC

5000 10103

304001292161706G01D

02810GEARSHAFT, BEVEL A320-0416170358-06620-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




Report Date:

Page 1 of 2

08-Jan-2016

2520 7183

311001127300506H23A


UNK1SB210SFFC RCRC

2520 7183

311001127300506H23A


UNK2SB210SFFC RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




Report Date:

Page 2 of 2

08-Jan-2016





IPS READINGS4.



PMI-202-Oct-2008 TAIL ROTOR 000.094663.3

100HR26-Sep-1996 #1 ENG 0.09002185.6

100HR26-Sep-1996 #2 ENG 0.47002185.6

100HR26-Sep-1996 OIL COOLER 0.1500.342185.6

100HR24-Feb-1997 #1 ENG 0.19002286

100HR24-Feb-1997 #2 ENG 0.3002286

100HR24-Feb-1997 OIL COOLER 0.3200.252286

100HR04-Sep-1997 #1 ENG 0.3002383.1

100HR04-Sep-1997 #2 ENG 0.41002383.1

100HR04-Sep-1997 OIL COOLER 0.1700.442383.1

PMS 226-Aug-1998 #1 ENG 0.02002482.5

PMS 226-Aug-1998 #2 ENG 0.22002482.5

PMS 226-Aug-1998 OIL COOLER 0.1900.492482.5

100HR28-Dec-1998 #1 ENG 0.45002581.9

100HR28-Dec-1998 #2 ENG 0.25002581.9

100HR28-Dec-1998 OIL COOLER 0.2700.152581.9

100HR27-Aug-1999 #1 ENG 0.45002778.1

100HR27-Aug-1999 #2 ENG 0.33002778.1

100HR27-Aug-1999 OIL COOLER 0.1400.152778.1

100HR13-Jan-2000 #1 ENG 0.47002880

100HR13-Jan-2000 #2 ENG 0.3002880

100HR13-Jan-2000 OIL COOLER 0.4700.372880



POST PHASE08-Aug-2000 OIL COOLER 0.1900.572977.1

POST PHASE08-Aug-2000 TAIL ROTOR 0.04002977.1

100 HR05-Jan-2001 TAIL ROTOR 0.11003073




IPS READINGS4.



100 HR05-Jan-2001 OIL COOLER 0.6100.23073

100 HR05-Jan-2001 #2 ENG 0.33003073

100 HR05-Jan-2001 #1 ENG 0.18003073

REPLACE #1 ENGINE22-Aug-2001 #1 ENG HSS 0.23003220.5

ENGINE REPLACE30-Jan-2002 NO.1 ENG 0.31003295.6

ENG CHANGE21-Mar-2002 #2 ENG 0.23003337.8

PMS-2 #711-Feb-2003 NO.1 ENG 0.43003462.7

PMS-2 #711-Feb-2003 NO.2 ENG 0.16003462.7

PMS-2 #711-Feb-2003 AXIAL FAN 0.3200.513462.7

PMS-2 #711-Feb-2003 TAIL ROTOR 0.03003462.7

100HR17-Nov-2003 #1 ENG 0.3003655.6

100HR17-Nov-2003 #2 ENG 0.43003655.6

100HR17-Nov-2003 OIL COOLER 0.0900.283655.6

100HR10-Sep-2004 #1 ENG 0.1003834.6

100HR10-Sep-2004 #2 ENG 0.29003834.6

100HR10-Sep-2004 OIL COOLER 0.1200.363834.6

100HR10-Sep-2004 TAIL ROTOR 0.13003834.6

100HR24-Jan-2005 #1 ENG 0.14003933.1

100HR24-Jan-2005 #2 ENG 0.4003933.1

100HR24-Jan-2005 OIL COOLER 0.0800.133933.1

100HR24-Jan-2005 TAIL ROTOR 0.06003933.1

120 HR04-Jan-2006 TAIL ROTOR 0.09004071.2

120 HR04-Jan-2006 #1 ENGINE 0.21004071.2

120 HR04-Jan-2006 #2 ENGINE 0.36004071.2

120 HR04-Jan-2006 OIL COOLER 0.090.1704071.2

120 HR06-Jul-2006 #1 ENG 0.28003189

120 HR06-Jul-2006 #2 ENG 0.3004189




IPS READINGS4.



120 HR06-Jul-2006 OIL COOLER 0.0700.164189

120 HR06-Jul-2006 TAIL ROTOR 0.12004189

DE-ICE BRACKET REPL29-Sep-2006 TAIL ROTOR 000.084255.1









120 HR23-May-2007 #1 ENG 0.11004422

120 HR23-May-2007 #2 ENG 0.37004422

120 HR23-May-2007 OIL COOLER 00.6204422

120 HR23-May-2007 TAIL ROTOR 0.06004422

ENG REPLACEMENT22-Feb-2008 #2 ENG 0.31004588.2

UNFOLD22-May-2008 TAIL ROTOR 00.0304640.6

PMI-201-Oct-2008 OIL COOLER 0.010.3104663.3

120 HOUR01-Jun-2009 TAIL ROTOR 0.07004783.3

# 1 ENG REPLACEMENT01-Jun-2009 #1 ENG 0.08004783.3

120 HOUR01-Jun-2009 #2 ENG 0.4004783.3

120 HOUR01-Jun-2009 OIL COOLER 0.62004783.3

T/R VERIFICATION (RIG)26-Jun-2009 TAIL ROTOR 0.05004788.8

120HR01-Oct-2009 #1 ENG 0.32004902.8

120HR01-Oct-2009 #2 ENG 0.39004902.8

120HR01-Oct-2009 OIL COOLER 0.55004902.8

120HR01-Oct-2009 TAIL ROTOR 0.06004902.8




IPS READINGS4.





POST PHASE TD803826-Apr-2010 OIL COOLER 0.58005000

RE-TORQUE26-Apr-2010 T/R 0.07005009.2

ENG REPLACEMENT12-May-2010 #2 ENG 0.37005003

T/R GEARBOX REPLACED29-Sep-2010 T/R 00.1205103.8

INBOARD RETENTION PLATE CHKS19-Oct-2010 T/R 00.105112.3

120 HR27-Oct-2010 T/R 0.11005120

120HR27-Oct-2010 #1 HSS 0.23005120

120HR27-Oct-2010 #2 HSS 0.23005120

120HR27-Oct-2010 OIL COOLER 0005120

VERIFICATION OF 27-OCT-2010 0.0 IPS09-Nov-2010 OIL COOLER 0.67005120

POST PHASE PMI-203-Jan-2012 #2 ENG 0.27005342.3

POST PHASE PMI203-Jan-2012 T/R 00.0705342.2

POST PHASE PMI 203-Jan-2012 #1 ENG 0.15005342.3

POST PHASE PMI204-Jan-2012 OIL OOLER 0.41005342.3

INBOARD RETENTION PLATE RETOURQE25-Jan-2012 T/R 0.16005351.8

120 HR19-Jun-2012 #2 ENG 0.37005460.8

120 HR19-Jun-2012 #1 ENG 0.19005460.8

120 HR19-Jun-2012 OIL COOLER 0.03005460.8

120 HR19-Jun-2012 T/R 00.0205460.8

POST MAIN/TAIL ROTOR RIG08-Aug-2012 T/R 0.03005489.9

# 2 INPUT MOD REPLACEMENT19-Jun-2013 #2 ENG 0.4005623.2

POST PMI04-Feb-2014 TAIL ROTOR 0.03005704.9

POST PMI04-Feb-2014 #1 HSS 0.18005704.9

POST PMI04-Feb-2014 #2 HSS 0.19005704.9

POST PMI04-Feb-2014 OIL COOLER 00.1505704.9




IPS READINGS4.



#1 ENG REPLACEMENT05-Feb-2015 #1 HSS 0.1005869.9

6. Remarks

QC000000

CW3 FORBES02-Oct-2008

(NO LOCATION)(NO ORGANIZATION)




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

08-Jan-2016

2160 6823

311001113828811C23A

00BRNG T/R PITCH CHGSHAFT

11404SB1162-102 RCRC

COND COND

534001094578911C23C

399399CLEVIS, ROD END 233-040952307201070400-06702-041 CCCC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

08-Jan-2016




PIDMWODATE HRS



ANTI-ICE VALVE 8323869AEX105841. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


22-Jun-2011 OM

JR01622507-Jul-2011

0.2D CO 1-214THAVN REGT

ALL H-60 SERIES ACFT,ANTI-ICE/START BLEED VALVEACTUATOR SHAFTS

H-60-11-ASAM-11MWO:

Priority Mnt Level

05-Sep-2012 OM

LD19731413-Sep-2012

1D CO 1-214THAVN

ENGINE ANTI-ICE/START BLEEDVALVE

H-60-12-ASAM-10MWO:

Priority Mnt Level




8323869116305-302AUXILIARY POWER UNIT876276

598

1313

3866

6881

0

5

3

3

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 2/2

15B 116305-302 AUXILIARY POWER UNIT 876276

764472200

163000SIF13714502902WHEEL,COMPRESSOR

7707

6000

1312687603

0000K7094503991WHEEL, TURBINE

9861

6000


11/17/201112:00:00 AM

1 TRANSCRIBED FROM 22 APR 2011) APU OVERHAULED AND REPAIREDIAW DMWR 55-2835-209. REPLACED THE FOLLOWING PARTS: TURBINEROTOR ASSY, CARRIER ASSY, FUEL MANIFOLD, STARTER GEAR, MAGPICK UP, OIL PUMP AND ALL FUEL AND OIL FILTERS TBO TIME FOR THISAPU IS 12876 SSN @ 9861 METER EVENTS, ENTERED BY TOM SULLIVANCIV TI ESRA FTCKY DSN 635-6201.

EW744892 TASM-E CAAF


365

360

5343

8323869 0 0


UH-60A 876276 Days


HELICOPTER, UTILITY AUXILIARY POWER UNIT Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

04-Jan-2012NORMALBASELINE5343.012224534304-Jan-2012



CG11223326-Nov-2014NORMALROUTINE497.414755840.402-Oct-2014

PRE PHASE

9. REMARKS:




CAO01654


4103

3276

16695

19695

9044

7544

2051

2059

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE





T700-GE-700




OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 2/12


32741962575382057

33171667956861694GEC0376556035T02G01COLD SECTIONMODULE

COND

COND

32741962575382057

4496000GGMP55816039T58G02COMBUSTION LINER

COND

COND

32741962575382057

30841892975171602MRSG38796055T20G05MTCHDROTOR/STATOR ASSY

COND

COND

32741962575382057


COND

COND

32741962575382057

40302415695612766GEL0372356064T98G01POWER TURBINEMODULE

COND

COND

32741962575382057

2957000GED0373796035T01G01ACCESSORY MODULE

COND

COND

32741962575382057

490000K06726034T62P18PARTICLESEPARATOR BLOWER

COND

COND

32761962575382057


COND

COND

32741962575382057


COND

COND

32761962575382057


COND

COND

32741962575382057

41011662590382049CAO016544046T26G03HISTORY RECORDER

COND

COND


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 3/12


32741962575382057

918000UDDK01224046T25G06COOLER, OIL

COND

COND

32741962575382057

412000COMH64094046T28G14ANTI-ICE VALVE

COND

COND




CAO01654

GE-E-3079106035T02G01COLD SECTION MODULEGEC037655

4101

3317

16625

16679

9038

5686

2049

1694

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 5/12


33171667956861694


COND

COND

33171667956861694


COND

COND

33171667956861694

37718741230206NCE141CC6035T88P07GAS GENERATORTURBINE SHAFT

14724

11000

33171667956861694

0000WESP20265036T95P01INNER BALANCEPISTON SE

COND

COND

33171667956861694

0000BIWYBENH6035T79P04COMPRESSORDISCHARGE SEAL

COND

COND

33171667956861694

34271430780042131FIA8C6316035T83P01COMPRESSOR REARSHAFT

5674

5000

33171667956861694

0000VAECK2475044T07P01NO 3 LABYRINTHSEAL

COND

COND

33171667956861694

3201838752391752WIN949CD5035T57P02VORTEX SPOILER

COND

COND

33171667956861694

6274149GATHPMD45043T04P02TIE ROD,COMPRESSOR

14095

10000

33171667956861694

204351973351873GATV46034045T08P01RING, SPACERCOMPRESSOR

12058

10000

33171667956861694

0000GLHTMTM36055T59P01COMPRESSORIMPELLER

9101

5000


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 6/12


33171667956861694


COND

COND

33171667956861694

0000GLHTM5WA6032T26G09STAGE 1 BLISK

9101

5000

33171667956861694

0000GLHTMWJG6032T27P08STAGE 2 BLISK

11101

7000

33171667956861694

0000GLHTN0466038T08P04STAGE 3 & 4 BLISK

11101

7000

33171667956861694

0000GLHTMP3E6038T09P04STAGE 5 BLISK

11101

7000

33171667956861694

0000TMKAGE936064T35P01NO 3 BALL BEARING

COND

COND

33171667956861694

724621117007605MDA344LW6064T14P01NO 4 ROLLERBEARING

COND

COND




CAO01654

GEC0376556039T56G04OUTPUT SHAFT ASSYGGA07758

4101

4424

16625

12715

9038

7216

2049

2182

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 8/12


44241271572612182

0000FCAR32666064T34P02NO 1 BALL BEARING

COND

COND

44241271572612182

61378597138502901MABA13415035T69P01NO 2 ROLLERBEARING

COND

COND




CAO01654


MRSG3879

4101

3084

16625

18929

9038

7517

2049

1602

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 10/12

04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRSG3879

30841892975171602

2313798860391219GAT2861T6064T85P01STAGE 1 TURBINEDISK

6788

5000

30841892975171602

30841892975171602GGAC7468A6039T57G18G/G STATOR ASSY

COND

COND

30841892975171602

260306282113GATHGKPH6064T86P02STAGE 2 TURBINEDISK

8841

5000

30841892975171602

431323901205PAMEU3096064T81P01STAGE 1 FWDCOOLING PLATE

8670

5000

30841892975171602

4681578802229GFF5D6E46064T82P01STAGE 1 REARCOOLING PLATE

8633

5000

30841892975171602

189071154138870PAMBG5606039T52P03STAGE 2 FWDCOOLING PLATE

6211

4000

30841892975171602

18203451415710866GFF5A0TT6064T84P02STAGE 2 REARCOOLING PLATE

7281

5000

30841892975171602

30841892975171602GGAG38796039T54G13G/G ROTORASSEMBLY

COND

COND




CAO01654

GE-E-3079106064T98G01POWER TURBINE MODULEGEL037235

4101

4030

16625

24156

9038

9561

2049

2766

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 12/12

04A03 6064T98G01 POWER TURBINE MODULE GEL037235

40302415695612766


COND

COND

40302415695612766

97282281496748GATHG5G86038T32P02STAGE 3 TURBINEDISK

8129

5000

40302415695612766

3322024627GATHELCK6038T34P05STAGE 4 TURBINEDISK

9068

5000

40302415695612766

64956082278397GATHKRG15125T92G01POWER TURBINESHAFT

8452

5000

40302415695612766

29611632160831678MABK25155034T27P01NO 5 ROLLERBEARING

COND

COND

40302415695612766

2800323832781274FAFF27135034T28P01NO 6 BALL BEARING

COND

COND




ECD01118


3983

3983

42052

42052

9100

9100

3495

3495

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE





T700-GE-700




OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 2/12


36873859387543292

2922849362791347GE-C-0373396035T02G01COLD SECTIONMODULE

COND

COND

0000

0000GGMAP3816039T58G02COMBUSTION LINER

COND

COND

28572812873642744

4026307070301513MRS076146055T20G05MTCHDROTOR/STATOR ASSY

COND

COND

2857000


COND

COND

36893869187633298

25971103972461975GE-L-0372566064T98G01POWER TURBINEMODULE

COND

COND

0000

0000GE-D-0373386035T01G01ACCESSORY MODULE

COND

COND

0000

0000SUSJ48516034T62P13PARTICLESEPARATOR BLOWER

COND

COND

3983000


COND

COND

3218000


COND

COND

3983000


COND

COND

0000

0000ECD011184046T26G03HISTORY RECORDER

COND

COND


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 3/12


0000

0000SUS1275C4046T25G03COOLER, OIL

COND

COND

1656000

755000AEX105845066T38G04ANTI-ICE VALVE

COND

COND




ECD01118

GE-E-3073386035T02G01COLD SECTION MODULEGE-C-037339

3687

2922

38593

8493

8754

6279

3292

1347

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 5/12


2920839362711344


COND

COND

2920839362711344


COND

COND

2920839362711344

9076301409378GATCV6K06035T88P04GAS GENERATORTURBINE SHAFT

13778

11000

2920839362711344

000039648465036T95P01INNER BALANCEPISTON SE

COND

COND

2920839362711344

0000MMTF55096035T79P04COMPRESSORDISCHARGE SEAL

COND

COND

2920839362711344

22791397777322023GAT9936F6035T83P01COMPRESSOR REARSHAFT

6406

5000

2920839362711344

0000VAEA88855044T07P01NO 3 LABYRINTHSEAL

COND

COND

2920839362711344

25981580579622212BIWBN1355035T57P02VORTEX SPOILER

COND

COND

2920839362711344

117219011156430GATMF7475043T04P02TIE ROD,COMPRESSOR

12513

10000

2920839362711344

30241461840861476GATAJ2894045T08P01RING, SPACERCOMPRESSOR

10661

10000

2920839362711344

0000GLHTKC6A6055T59P01COMPRESSORIMPELLER

8685

5000


OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 6/12


2920839362711344


COND

COND

2920839362711344

0000GLHTKJNJ6032T26G09STAGE 1 BLISK

8685

5000

2920839362711344

0000GATHGMRM6032T27P08STAGE 2 BLISK

10685

7000

2920839362711344

0000GLHTJWE46038T08P04STAGE 3 & 4 BLISK

10685

7000

2920839362711344

0000GLHTK2F06038T09P04STAGE 5 BLISK

10685

7000

2920839362711344

9311565116043338388966064T35P02NO 3 BALL BEARING

COND

COND

2920839332711344

29551203092352093MAB565196064T15P01NO 4 ROLLERBEARING

COND

COND




ECD01118

GE-C-0373396039T56G04OUTPUT SHAFT ASSYGGA06194

3687

4926

38593

10647

8754

11253

3292

2573

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 8/12


4924000

2525000BARA71195034T07P03NO 1 BALL BEARING

COND

COND

4924000

18000MDAL72075035T71P01NO 2 ROLLERBEARING

COND

COND




ECD01118


MRS07614

2857

4026

28128

3070

7364

7030

2744

1513

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 10/12

04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRS07614

4026307070301513

0000GATH89T96064T85P01STAGE 1 TURBINEDISK

7857

5000

4026307070301513

4026307070301513GGA160446039T57G24G/G STATOR ASSY

COND

COND

4026307070301513

119589343236746GAT8262U6064T86P01STAGE 2 TURBINEDISK

6662

5000

4026307070301513

0000GFF5A91F6064T81P01STAGE 1 FWDCOOLING PLATE

7857

5000

4026307070301513

0000GFF5A92W6064T82P01STAGE 1 REARCOOLING PLATE

7857

5000

4026307070301513

0000GFF5ADCC6064T83P01STG 2 FWD COOLINGPLATE

7857

5000

4026307070301513

0000GFF5A0JP6064T84P02STAGE 2 REARCOOLING PLATE

7857

5000

4026307070301513

4026307070301513GGA076146039T54G13G/G ROTORASSEMBLY

COND

COND




ECD01118

GE-E-3073386064T98G01POWER TURBINE MODULEGE-L-037256

3689

2597

38691

11039

8763

7246

3298

1975

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3



5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

LINE 3 MINUS LINE 2

MODULE/RECORDER2-


MODULE/RECORDER3


dcbaLINE








OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


08-Jan-2016 12/12

04A03 6064T98G01 POWER TURBINE MODULE GE-L-037256

25961102672421973


COND

COND

0000

0000GATJV4216038T32P01STAGE 3 TURBINEDISK

6092

5000

0000

0000GATJJ8546038T34P05STAGE 4 TURBINEDISK

6092

5000

25961102672421973

27041082767801711GATLY4375125T92G01REPOWER TURBINESHAFT

5984

5000

25961102672421973

160027192761615FCAB74225034T27P02NO 5 ROLLERBEARING

COND

COND

25961102672421973

153623522115759MABF82216064T36P01NO 6 BALL BEARING

COND

COND



PIDMWODATE HRS





30-Jun-1994 OR

29-May-19964D-CO 2-1 APO

AE 09250(LR0306)

ONE TIME INSPECTION ANDCONVERSION OF FORMS ANDRECORDS FOR T700-GE-700, -701AND -701C SERIES GAS TURBINEENGINES

1-2840-248-20-2MWO:

Priority Mnt Level

30-Oct-1996 OU

08-Apr-19981DYNCORP-

GSMP APO AE09028 (LR0306)

REPLACEMENT OF UNDAMPED GASGENERATOR ROTOR/STATORASSEMBLIES FOR ALL UH-60A ANDEH-60A AIRCRAFT WITH T700-GE-700ENGINES

1-2840-248-20-19MWO:

Priority Mnt Level

15-Dec-1998 OU

17-Feb-200012-502 AVN REGT

AE 09028(LR0306)

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

1-2840-248-20-22MWO:

Priority Mnt Level

02-Aug-1999 FM

17-Feb-200012-502 AVN REGT

AE 09058(LR0306)

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


Priority Mnt Level

16-Aug-1999 OM

17-Feb-20000.52-502 AVN REGT

AE 09058(LR0306)

ALL UH-60A, EH-60A AND UH-60QAIRCRAFT, SUBJECT: INSPECTIONINTERVAL CHANGE FOR HAMILTONSTANDARD HYDRO MECHANICALUNITS (HMU) P/NS 4046T52G01,4046T52G04, 4046T52G06,4046T52G09 AND 4046T52G11 USEDON THE T700-GE-700 ENGINE


Priority Mnt Level

16-Jul-2007 OM

18-Jul-20070.11-214TH AVN

REGT (ST0922)ALL H-60A SERIES AIRCRAFT,HAMILTON-SUNDSTRAND HYDRO-MECHANICAL UNITS (HMU'S)


Priority Mnt Level

23-Jul-2007 OM

25-Jul-20070.51-214TH AVN

REGT (ST0922)ALL UH/HH-60L AIRCRAFT,DEFECTIVE DIGITAL ENGINECONTROL UNITS (DECU)


Priority Mnt Level

13-Aug-2007 OM

14-Aug-20070.51-214TH AVN

REGT (AN9260)ALL H-60 SERIES AIRCRAFT, MAINFUEL MANIFOLD CHAFING


Priority Mnt Level

28-Dec-20070.11-214TH AVN

REGT (ST0922)ALL H-60 AND ALL AH-64 SERIESAIRCRAFT, MIL-PRF-23699 HIGHTEMPERATURE STABILITY (HTS) OIL

H-60-08-AMAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS





20-Dec-2007 OM

22-Sep-2008 OM

20-Oct-20081TASM-E APO AE

09058 (LR0306)SUSPECT ENGINE HARNESSESH-60-08-ASAM-14MWO:

Priority Mnt Level

12-Jan-2009 OM

13-Jan-20091D CO 1-214TH

AVN REGCOLEMAN BKS,GE

T701C GAS GENERATOR (GG)ROTOR ASSEMBLIES

H-60-09-ASAM-01MWO:

Priority Mnt Level

01-Oct-2009 OM

SD65391215-Oct-2009

11-214TH AVNREGT

ALL H-60A SERIES AIRCRAFT,HAMILTON-SUNDSTRAND HYDRO-MECHANICAL UNITS

H-60-10-ASAM-01MWO:

Priority Mnt Level



T/T I HIST RCDR SNSERIAL 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

16015 SESI

2. Organization

CSGLD-1052

REQUIREMENT CONTROL SYMBOL(Julian)1. PERIOD ENDING DATE


1GEE307320 ECD-011984198222739836263862627923289

2GEE307936 CAO0222758161989114460401862627923289

1GEE307539 CAO008363337110495859172257328123603

2GE-E-307912 ECD03263314596425013164557328123603

1GE-E-307910 CAO016544109166959049205358758323869

2GE-E-307338 ECD0111848154558810326391258758323869


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

Eddie.Denney

Highlight

PIDMWODATE HRS



FUEL CONTROL 8323869UDAJ07101. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


16-Jul-2007 OM

JB45666007-Dec-2010

0.2D CO 214TH AVNALL H-60A SERIES AIRCRAFT,HAMILTON-SUNDSTRAND HYDRO-MECHANICAL UNITS (HMU'S)


Priority Mnt Level

01-Oct-2009 ON

JB45666007-Dec-2010

0.2D CO 1-214THHMU SUSPECTED PART NUMBERH-60-10-ASAM-01MWO:

Priority Mnt Level

23-Nov-2010 OM

JB45666007-Dec-2010

0.2D CO 1-214THAVN

ALL H-60 SERIES AIRCRAFT,HAMILTON STANDARD HYDRO-MECHANICAL UNITS PN 5074T79GO2, 5074T79GO3, AND 5074T79GO5REMOVE FROM SERVICE. REMOVEPN 5074T79GO7 IF LAST DEPOTREPAIR PRIOR TO 01 JAN 2003.

H-60-11-ASAM-03MWO:

Priority Mnt Level

05-Sep-2012 OM

LD19731417-Sep-2012

1D CO 1-214THAVN

ALL H-60A SERIES AIRCRAFT,HYDRO-MECHANICAL UNIT(HMU).

H-60-12-ASAM-11 (CORREMWO:

Priority Mnt Level

19-Aug-2013 FM

DR62253028-Aug-2013

1DCO 1-214THAVN BN

WOODWARD HYDR-MECHANICALUNIT (HMU) P3 TUBE

H-60-13-ASAM-10MWO:

Priority Mnt Level

13-Aug-2014 FM

BJ96335431-Jul-2014

0.1D CO. 1-214THAVN REGT

COMPLY WITH REQUIRENENTS OF H-60-14-ASAM-08

H-60-14-ASAM-08MWO:

Priority Mnt Level



PIDMWODATE HRS



HUB, M/R ROTOR ASSY 8323869A308-004531. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


30-Dec-2013 FM

RS63083226-Jun-2014

1D CO 1-214THAVN REGT

ALL H-60 SERIES AIRCRAFT, ONETIME EDDY CURRENT INSPECTIONOF SUSPECTED REWORKED M/RHUB ASSY FOR CRACKS.

H-60-14-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



INPUT MODULE 8323869A264-024281. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


02-Aug-2000 OT

03-Aug-20000.52-502 AVN REGT

APO 09028(TB6357)

ALL H-60 SERIES AIRCRAFT,REMOVAL OF INPUT MODULE GEARBOX ASSEMBLIESWITHPOTENTIALLY CRACKED BEVELGEARS

UH-60-00-02MWO:

Priority Mnt Level



360

360

1493

8323869 4382 1493


UH-60A A005-00592 Days


HELICOPTER, UTILITY INTERMEDIATE GEARBOX Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

BS57423509-Jul-2008NORMALROUTINE4663.03170466308-Jul-2008

BS57423516-Dec-2008NORMALROUTINE4703.03210470309-Dec-2008

VZ74839127-Mar-2009NORMALROUTINE4743.03250474320-Mar-2009

TF54643922-May-2009NORMALROUTINE3290.03290478311-May-2009

JW82927726-Aug-2009NORMAL40 HOUR3329.03329482205-Aug-2009

22-Sep-2009NORMAL40 HOUR3368.03368486108-Sep-2009

DG10618708-Dec-2009NO RESULTS40 HOUR3410.03410490301-Oct-2009

VZ74839108-Dec-2009NORMAL40 HOUR3446.03446493908-Dec-2009

VZ74839122-Feb-2010NORMAL40 HOUR3481.03481497416-Jan-2010

VZ74839105-Feb-2010NORMALPRE-PHASE3507.03507500029-Jan-2010

15-Feb-2011NORMALROUTINE3657.03657515015-Feb-2011

15-Nov-2011ABNORMALPRE PHASE3848.03848534109-Nov-2011

RT31947612-Mar-2012NORMALSPECIAL3887.03887538012-Mar-2012

RT31947629-Apr-2013NORMALROUTINE4123.04123561627-Apr-2013


CG11223326-Nov-2014NORMALROUTINE4347.44347.45840.402-Oct-2014

PRE PHASE

9. REMARKS:



PIDMWODATE HRS



MAIN ROTOR BLADE ASSY 8323869A007-139901. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


15-Apr-2010 OT

21-Apr-20102D CO 1-214TH

AVN REGTALL H-60A/K/L SERIES AIRCRAFT,DEPOT REPAIRED LEGACY MAINROTOR BLADES

H-60-10-SOF-01MWO:

Priority Mnt Level

09-Apr-2012 OT

LD19731411-Apr-2012

1D CO 1-214THAVN

CHANGE TO DEPOT REPAIREDLEGACY MAIN ROTOR BLADESCOMPLIANCE DATE

H-60-12-SOF-05MWO:

Priority Mnt Level



PIDMWODATE HRS





15-Apr-2010 OT

21-Apr-20102D CO 1-214TH


H-60-10-SOF-01MWO:

Priority Mnt Level

09-Apr-2012 OT

LD19731411-Apr-2012

1D CO 1-214THAVN


H-60-12-SOF-05MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR BLADE ASSY 8323869A007007081. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


28-Feb-1998 DU

EL995229-May-2009

1CCADINCREASE IN FATIGUE LIFE FORTHE M/R CUFF ASSY, PN 70150-09109-041 AND 70150-09109-043

1-1520-237-20-16MWO:

Priority Mnt Level

28-Feb-1998 DU

LM674926-Jul-2011

1CCADINCREASE IN FATIGUE LIFE FORTHE MAIN ROTOR BLADE CUFFS,P/N 70150-09109-041 AND 70150-09109-043

UH-60-97-ASAM-11/TB 1-1MWO:

Priority Mnt Level

12-Aug-2002 OT

LM674926-Jul-2011

1CCADALL H-60 SERIES AIRCRAFT,REVISION TO UH-60-02-11, ONE-TIMEINSPECTION OF MAIN ROTORBLADE CUFF ASSEMBLY

UH-60-02-12MWO:

Priority Mnt Level

07-Jan-2003 DM

LM674926-Jul-2011

1CCADONE TIME INSP OF M/R CUFF ASSYSOF UH-60-03-02MWO:

Priority Mnt Level

07-Jan-2003 OT

EL995229-May-2009

1CCADINITIAL AND RECURRINGINSPECTION OF MAIN ROTORBLADE CUFF ASSEMBLY, ALL H-60AIRCRAFT

UH-60-03-SOF-02MWO:

Priority Mnt Level

15-Sep-2005 DU

LM674926-Jul-2011

130CCADRECAPITALIZATION REQUIRED FORH-60 MAIN ROTOR BLADE P/N 70150-09100-043 NSN 1615-01-106-1903

DMWR 1-1615-281, C1MWO:

Priority Mnt Level

15-Sep-2005 DU

EL995229-May-2009

130CCADRECAP REQUIREMENTS COMPLIEDWITH.

DMWR 1-1615-281,C1,U,DMWO:

Priority Mnt Level

15-Apr-2010 OT

LM674926-Jul-2011

3CCADALL H-60A/K/L SERIES AIRCRAFT,DEPOT REPAIRED LEGACY MAINROTOR BLADES

H-60-10-SOF-01MWO:

Priority Mnt Level

09-Apr-2012 OT

LD19731411-Apr-2012

1D CO 1-214THAVN


H-60-12-SOF-05MWO:

Priority Mnt Level



PIDMWODATE HRS





15-Apr-2010 OT

LD19731406-Jul-2012

1D CO 1-214THAVN

ALL H-60A/K/L SERIES AIRCRAFT,DEPOT REPAIRED LEGACY MAINROTOR BLADES

H-60-10-SOF-01MWO:

Priority Mnt Level

09-Apr-2012 OT

LD19731411-Apr-2012

1D CO 1-214THAVN


H-60-12-SOF-05MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 8323869A001-033131. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


19-Mar-2001 FU

14-Jan-20030.52-502 AVN REGT

AE 09058(LR0306)

ALL H-60 AIRCRAFT, INSPECTION OFMAIN ROTOR SPINDLE

1-1520-237-20-230MWO:

Priority Mnt Level

09-Apr-2002 FU

14-Jan-20030.52-502 AVN REGT

AE 09058(LR0306)

ALL UH-60, SERIES AIRCRAFT,REMOVAL OF CHICAGO RAW HIDEM/R SPINDLE THRUST BEARINGSWITH SERIAL NUMBERS C325-00001THROUGH C325-02407

1-1520-237-20-251MWO:

Priority Mnt Level

05-Sep-2012 FM

LD19731404-Oct-2012

1D CO 1-214THAVN

ALL H-60 SERIES AIRCRAFT, MAINROTOR SPINDLE SUB-COMPONENTTRACKING REQUIREMENTS

H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

LD19731401-Mar-2013

1D CO 10214THAVN

PERFORM ONE-TIME INSPECTIONFOR SUSPECT MAIN ROTORSPINDLE ANTI-FLAP BRACKETASSEMBLIES

H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS





05-Sep-2012 FM

LD19731404-Oct-2012

1D CO 1-214THAVN


H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

LD19731401-Mar-2013

1D CO 1-214THAVN


H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 8323869D001-112441. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Sep-2012 FM

LD19731404-Oct-2012

1D CO 1-214THAVN


H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

LD19731401-Mar-2013

1D CO 1-214THAVN


H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 8323869D001124471. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Sep-2012 FM

LD19731404-Oct-2012

1D CO 1-214THAVN


H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

LD19731401-Mar-2013

1D CO 1-214THAVN


H-60-13-ASAM-03MWO:

Priority Mnt Level



0

720

5701

8323869 3187 4936


UH-60A A26500126 Days


HELICOPTER, UTILITY MAIN TRANSMISSION MODULE Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

VZ74839108-Dec-2009NORMALBASELINE1.02249493708-Dec-2009



15-Nov-2011NORMALPRE PHASE405.02653534109-Nov-2011

JR01622530-Aug-2012NORMALSPECIAL572.02820550830-Aug-2012

LW84913019-Sep-2012NORMALSPECIAL590.02838552618-Sep-2012

RT31947611-Apr-2013NORMALSPECIAL676.02924561204-Apr-2013

RT31947602-May-2013NORMALSPECIAL680.02928561601-May-2013

RL17290214-May-2013NORMALSPECIAL680.02928561614-May-2013

RT31947616-Jul-2013NORMALSPECIAL699.02947563508-Jul-2013


BJ96335409-Oct-2014NORMALROUTINE170.03183587109-Oct-2014

PRE PHASE

9. REMARKS:



PIDMWODATE HRS



MAIN TRANSMISSION MODULE 8323869A265001261. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


26-Mar-2014 FM

RT31947611-Apr-2014


MAIN TRANSMISSION FILTER BOWLAND CHIP DETECTOR ATTACHMENTHARDWARE REPLACEMENT.

H-60-14-AMAM-09MWO:

Priority Mnt Level



9032149075875B112-102951560011291256SAS ACTUATOR70410-02500-04907A24

Report Date: MAJOR COMPONENT LISTINGSorted By: Work Unit Code

1/308-Jan-2016

DUE

AIRCRAFT HRS TO

REPLACESERIAL NONSNPART NOMENCLATUREPART NO

UH-60AMODEL:

WUC

8323869

CURR

AIRCRAFT SERIAL NO:

Major Component Listing for 16 Items

14125200005875UNK38691560010819244TAIL PYLON FITTING70209-06051-04302C15J

85867335875A308-004531615014816953HUB, M/R ROTOR ASSY70070-10046-05505A01A

6180120555875A001-033131615014426926MAIN ROTOR SPINDLE ASSY70102-08200-06905A01I


7245131205875D001-112441615014426926MAIN ROTOR SPINDLE ASSY70102-08200-06905A01I

7466133415875D001124471615014426926MAIN ROTOR SPINDLE ASSY70102-08200-06905A01I

6242121175875C286-000951615010745151MAIN ROTOR SHAFT EXTENDER70351-08186-04305A01L

7125130005875015152-05521615011277388BIFILAR, M/R ROTOR ASSY70107-08400-04605A01T

8050139255875A007-139901615011061903MAIN ROTOR BLADE ASSY70150-09100-04305A02


375496295875A007007081615011061903MAIN ROTOR BLADE ASSY70150-09100-04305A02


6810126855875A009-039831615011138188TAIL ROTOR BLADE ASSY70101-31000-04305B02

5471113465875A009028021615011138188TAIL ROTOR BLADE ASSY70101-31000-04305B02

6843127185875B257001461615010836812O/B RETENTION PLATE (T/R)70102-11101-04206G01B

91267875875C512-00281SB4141013293428FAN AXIAL70361-03005-10706H23

8403142785875B112-051561560011291256SAS ACTUATOR70410-02500-04907A24


2/308-Jan-2016

9032149075875B112-102951560011291256SAS ACTUATOR70410-02500-04907A24

11319171945875C112-011861560011291256SAS ACTUATOR70410-02500-04907A24

94868235875233-040951615011417532TAIL ROTOR PITCH CHANGE SHAFT70400-06100-04211C23

14114199895875B300-021421650013056954TAIL ROTOR SERVO ASSY2227000-1711C25

22284281595875B30311458B1650011431226MAIN ROTOR PRIMARY SERVO274000-103111D01

19820256955875B30301576B1650011431226MAIN ROTOR PRIMARY SERVO70410-02820-05411D01


7125130005875C345-031391560011589685AFT BELLCRANK70400-08102-04511D04

11125170005875A391-006201560010829213AFT TIE ROD SUPT FITTING70400-08112-04411D05

28061555875A392-003771680011644160AFT TIE ROD ASSY70400-08111-04211D06

4226101015875390019171560012868870AFT BELLCRANK SPT ASSY70400-08117-04911D07

10061159365875015152-007903040012872438LATERAL SWASHPLATE LINK70400-08151-06111D08

18788246635875F337-029771680012212863LATERAL SERVO BELLCRANK70400-08166-04111D09

5125110005875B346-007351680011589653AFT WALKING BEAM70400-08104-04811D11

7945138205875E344-013031560011589475LEFT TIE ROD70400-08115-04511D13

22888163587533325-611560012969486RIGHT TIE ROD ASSY70400-08114-05111D14

137881966358756321680011589652FORWARD BELLCRANK70400-08101-04611D15

4388102635875B367044901560012212619FWD BELLCRANK SPT ASSY70400-08162-04211D16

NSN SERIAL NOPART NO PART NOMENCLATURE

AIRCRAFT

DUE REPLACE

HRS TO

CURR

Major Component Listing for 76F01

AIRCRAFT SERIAL NO:MODEL: UH-60A 8323869

WUC


3/308-Jan-2016


AIRCRAFT

DUE REPLACE

HRS TO

CURR

Major Component Listing for 16-1 Items


WUC

-48024802 08762762835013692818AUXILIARY POWER UNIT116305-30215B


AIRCRAFT

DUE REPLACE

HRS TO

CURR

Major Component Listing for 714 Engines


WUC

PIDMWODATE HRS



MTCHD ROTOR/STATOR ASSY 8323869MRS076141. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


31-Jul-1989 OM

18-Sep-200333CCAD

(FO0000)MODIFICATION OF GG ROTORASSEMBLY T700/701 REWORK T700ENGINES

55-2840-248-50-32MWO:

Priority Mnt Level

30-Jun-1994 OR

18-Sep-20034CCAD

(FO0000)ONE TIME INSPECTION ANDCONVERSION OF FORMS ANDRECORDS FOR T700-GE-700, -701AND -701C SERIES GAS TURBINEENGINES

1-2840-248-20-2MWO:

Priority Mnt Level

19-Sep-1995 OI

18-Sep-20030.1CCAD

(FO0000)ALL UH-60A, EH-60A, AND AH-64AAIRCRAFT WITH T700-GE-700 ANDT700-GE-701 ENGINES, SUBJECT:GAS GENERATOR TURBINE ROTORBLADE INFORMATION


Priority Mnt Level

25-Oct-1996 OM

18-Sep-20030.5CCAD

(FO0000)ALL UH-60A, EH-60A AIRCRAFT WITHT700-GE-700 ENGINES SUBJECT:REPLACEMENT OF UNDAMPED GASGENERATOR ROTOR/STATORASSEMBLIES


Priority Mnt Level



PIDMWODATE HRS



SAS ACTUATOR 8323869B112-102951. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


23-Mar-2001 FT

26-Mar-20010.5D C0, 1-214TH

AVN REGT(DB4697)

ALL H-60 SERIES AIRCRAFT,INSPECTION OF ALL SASACTUATORS

UH-60-01-06MWO:

Priority Mnt Level



SECTION I COCKPITSES BEST

4. EQUIPMENT CHECKLIST

8323869 UH-60A

3. AREA NAME 2. MODEL 1. SERIAL NUMBER


1RECEIVER RADIO - R-1496A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER

QTY REQ:NOMENCLATURITEM NO

1DISPLACEMENT GYRO - CN-1314/A (9000C)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un0

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING FOR KIT-1A/1C/TSEC - MT-3949A/U

Unt

UUUUUUnt

Unt

Un

Unt

Un0

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMMAND INSTR SYS PROCESSOR - 70600-01038-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING RACK - 70600-01038-102

Unt

UUUUUUnt

Unt

Un

Unt

Un1

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT FOR TSEC/KY-58 - 5290279-502

Unt

UUUUUUnt

Unt

Un

Unt

Un1

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#2 VHF-FM ANTENNA - AS-4171/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un1

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SAS AMPLIFIER - 70901-02908-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO ASSEMBLY - 70600-01047-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2RATE GYRO - TRU-2A/A

Unt

UUUUUUnt

Unt

Un

Unt

Un1

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

16

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 E, NOV 91



8323869 UH-60A



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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un2

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER RADAR - RT-1193/ASN-128

Unt

UUUUUUnt

Unt

Un

Unt

Un1

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un2

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GLIDE SLOPE ANTENNA - 70600-01043-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un2

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRE EXTINGUISHER - FR23-4-11848

Unt

UUUUUUnt

Unt

Un

Unt

Un1

25

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BAROMETERIC ALTIMETER - AAU-31/A-1

Unt

UUUUUUnt

Unt

Un

Unt

Un1

26

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BAROMETERIC ALTIMETER - AAU-32/A

Unt

UUUUUUnt

Unt

Un

Unt

Un1

27

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2CREW SEAT - D3801-2

Unt

UUUUUUnt

Unt

Un

Unt

Un2

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF-AM RADIO SET - RT-1518/ARC-164(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

31

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2INTERPHONE CONTROL - C6533/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un2

32

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER/TRANSMITTER - RT-1115D/APN-209

Unt

UUUUUUnt

Unt

Un

Unt

Un1

33

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

34

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8323869 UH-60A



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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

35

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2CONTROL - C-10604(V)6/ARN-184

Unt

UUUUUUnt

Unt

Un

Unt

Un2

36

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPARATOR SIGNAL DATA - CM482/ARC-186(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

38

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2MOUNTREVERSIBLE ARC-186/ARC-201 - 4290268-501

Unt

UUUUUUnt

Unt

Un

Unt

Un2

40

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPUTER DISPLAY UNIT - CP-1252C/ASN-128B

Unt

UUUUUUnt

Unt

Un

Unt

Un1

42

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

43

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un0

44

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RADIO RETRANSMISSION PANEL -70550-01008-042

Unt

UUUUUUnt

Unt

Un

Unt

Un1

45

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MAGNETIC COMPASS - MS17983-4

Unt

UUUUUUnt

Unt

Un

Unt

Un1

46

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2OUTSIDE AIR TEMP INDICATOR - MS28028-1

Unt

UUUUUUnt

Unt

Un

Unt

Un2

47

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ARMOR WING PANEL - 70500-01152-093

Unt

UUUUUUnt

Unt

Un

Unt

Un1

48

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER



Unt

UUUUUUnt

Unt

Un

Unt

Un1

49

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MISC. SWITCH PANEL - 70450-01090-044

Unt

UUUUUUnt

Unt

Un

Unt

Un1

50

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1STABILATOR/FLT CONT PANEL - 70902-01070-048

Unt

UUUUUUnt

Unt

Un

Unt

Un1

51

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2AHRU MOUNTING PLATE FOGS

Unt

UUUUUUnt

Unt

Un

Unt

Un1

60

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8323869 UH-60A



1MOUNTING BASE APX-118

Unt

UUUUUUnt

Unt

Un

Unt

Un1

61

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1765200-20 FOGS CONTROL UNIT (AHRU)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

62

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2ATTITUDE & HEADING REFERENCE UNIT, CN-1716/A (FOGS)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

63

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO ASSEMBLY 70600-01213-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

64

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER




5/5Report Date: 08-Jan-2016AREA NAMEMODELSERIAL NUMBER

SECTION I COCKPITSES BEST8323869 UH-60A

NAME OR PIDNUMBER DATE

db c

DATE NUMBER RANKRANK NAME OR PID

CHECK CHECK

ba ad

5. VERIFICATION

c

TM7295391 CIV 05-Jan-2016

b. LOCATION/REMARKSCHECK NO.

6. LOCATION OR REMARKS

a. ITEM NUMBER

Nomenclature

GYRO, DIRECTIONAL - CN-998/ASN-43

1 ACFT has FOGS Configuration3

MOUNTING FOR KIT-1A/1C/TSEC - MT-3949A/U

1 ACFT Configured for KY585

RATE GYRO - TRU-2A/A1 ACFT Configured for FOGS14

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

1 ACFT Configured for FOGS44

AHRU MOUNTING PLATEFOGS

1 ACFT Configured for single FOGS60

ATTITUDE & HEADINGREFERENCE UNIT, CN-1716/A(FOGS)


REVERSE OF DA FORM 2408-17 E, NOV 91

SECTION II CABINSES BEST


8323869 UH-60A



1CARGO HOOK, FE-7590-145 70800-02503-111

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MARKER BEACON ANTENNA - 70600-02011-103

Unt

UUUUUUnt

Unt

Un

Unt

Un1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM HOMING ANTENNA ASSY - 70600-02017-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER



Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRST AID KIT - 6545-00919-6650

Unt

UUUUUUnt

Unt

Un

Unt

Un1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER



Unt

UUUUUUnt

Unt

Un

Unt

Un2

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CRASH AXE - 56D6221

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HAND SET - H-250/U

Unt

UUUUUUnt

Unt

Un

Unt

Un1

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SLAB BATTERY -D8565/11-1

Unt

UUUUUUnt

Unt

Un

Unt

Un1

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER



Unt

UUUUUUnt

Unt

Un

Unt

Un3

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ADAPTER FUEL DRAIN - 70307-03018-102

Unt

UUUUUUnt

Unt

Un

Unt

Un0

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


4LOCK ASSY BLADE TIEDOWN - 70700-20369-041

Unt

UUUUUUnt

Unt

Un

Unt

Un4

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2PLUG ASSY INTAKE - HIRSS SUPP - 70700-20515-041/042

Unt

UUUUUUnt

Unt

Un

Unt

Un2

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un0

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PLUG ASSY APU EXHAUST - 70700-20509-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

15

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8323869 UH-60A



1COVER ASSY OIL COOLER - 70700-20511-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BLADE FOLD SET - 70700-20412-011

Unt

UUUUUUnt

Unt

Un

Unt

Un1

17

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER PITOT TUBE - 70700-20460-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


7TROOP SEATS - 70500-02151-045

Unt

UUUUUUnt

Unt

Un

Unt

Un7

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3TROOP SEATS - 70500-02151-047

Unt

UUUUUUnt

Unt

Un

Unt

Un4

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


10RESTRAINT SYSTEM - 70500-02153-103

Unt

UUUUUUnt

Unt

Un

Unt

Un11

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GUNNER SEAT - 70500-02152-047

Unt

UUUUUUnt

Unt

Un

Unt

Un1

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GUNNER SEAT - 70500-02152-048

Unt

UUUUUUnt

Unt

Un

Unt

Un1

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER



Unt

UUUUUUnt

Unt

Un

Unt

Un2

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ICS WALK-AROUND CORD - 70602-02016-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

29

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HYD. PUMP HANDLE - 15400-50126

Unt

UUUUUUnt

Unt

Un

Unt

Un1

30

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRING KEY - 70550-03101-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

31

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2EQUIPMENT LOGBOOK - MIL-D-43064

Unt

UUUUUUnt

Unt

Un

Unt

Un1

32

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1WEIGHT AND BALANCE HANDBOOK - TM 55-1500-342-23

Unt

UUUUUUnt

Unt

Un

Unt

Un1

34

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8323869 UH-60A



1ELECTRONIC SEQUENCE UNIT - 163290-100-E

Unt

UUUUUUnt

Unt

Un

Unt

Un1

52

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION II CABINSES BEST8323869 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

TM7295391 CIV 05-Jan-2016



a. ITEM NUMBER

Nomenclature

ADAPTER FUEL DRAIN - 70307-03018-102

1 ACFT delivered in this configuration11

PLUG ASSY EXHAUST - HIRSS- 70700-20515-043

1 ACFT Delivered in this configuration14

PLUG ASSY APU EXHAUST -70700-20509-041


COVER PITOT TUBE - 70700-20460-041

1 ACFT dellivered in this configuration18

TROOP SEATS - 70500-02151-047

1 ACFT in proper configuration20

RESTRAINT SYSTEM - 70500-02153-103


ICS WALK-AROUND CORD -70602-02016-041


EQUIPMENT LOGBOOK - MIL-D-43064


WEIGHT AND BALANCEHANDBOOK - TM 55-1500-342-23



SECTION III TRANSITION SECTIONSES BEST


8323869 UH-60A



1ANTENNA LOOP - AS-2108A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2IFF ANTENNA - 70600-02010-103

Unt

UUUUUUnt

Unt

Un

Unt

Un2

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF/AM ANTENNA - 70600-03002-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PUMP FUEL SAMPLER - 82829/4P156-3

Unt

UUUUUUnt

Unt

Un

Unt

Un0

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPENSATOR MAGNETIC FLUX - CN-405/ASN

Unt

UUUUUUnt

Unt

Un

Unt

Un1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS TRANSMITTER - T-611/ASN-43

Unt

UUUUUUnt

Unt

Un

Unt

Un1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GPS ANTENNA - 22433-40

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF AMPLIFIER - AM-7531/URC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA. GPS (BFT) S67-1575-863

Unt

UUUUUUnt

Unt

Un

Unt

Un0

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA, L-BAND (BFT) S65-8282-301

Unt

UUUUUUnt

Unt

Un

Unt

Un0

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT, IFM AMPLIFIER-MT-6592/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

42

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3933/ARN-149(V)1, ANTENNA, LOOP

Unt

UUUUUUnt

Unt

Un

Unt

Un1

49

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1TROOP COMMANDER ANTENNA (CMWS ONLY)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

50

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IVHMU (CBM MONITOR SYSTEM)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

55

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION III TRANSITION SECTIONSES BEST8323869 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

TM7295391 CIV 05-Jan-2016



a. ITEM NUMBER

Nomenclature

PUMP FUEL SAMPLER -82829/4P156-3


HF AMPLIFIER - AM-7531/URC1 ACFT delivered in this configuration8

ANTENNA. GPS (BFT) S67-1575-863


ANTENNA, L-BAND (BFT) S65-8282-301


MOUNT, IFM AMPLIFIER-MT-6592/ARC


TROOP COMMANDERANTENNA (CMWS ONLY)

1 ACFT delivered in this configuration. No CMWS Mod50


SECTION IV TAIL CONESES BEST


8323869 UH-60A



2VOR/LOC ANTENNA - 70600-05002-101

Unt

UUUUUUnt

Unt

Un

Unt

Un2

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IFM AMPLIFIER - AM-7189A/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF ANTENNA - 4700516-30

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION IV TAIL CONESES BEST8323869 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

TM7295391 CIV 05-Jan-2016



a. ITEM NUMBER

Nomenclature

IFM AMPLIFIER - AM-7189A/ARC



SECTION V TAIL ROTOR PYLONSES BEST


8323869 UH-60A



1CU-2457/ARC(405-11-1), VHF-FM #1 COUPLER ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM10-267, VHF-FM #2 (LEADING EDGE) ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM10-3230, VHF-FM TROOP COMMANDER ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION V TAIL ROTOR PYLONSES BEST8323869 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

TM7295391 CIV 05-Jan-2016



a. ITEM NUMBER

Nomenclature


ReportDate:

SUBCOMPONENT LISTING Sorted By: Work Unit Code 1/408-Jan-2016

PART NOMENCLATURE SER NO

AIRCRAFTCURR DUEWUC

MAJORCOMPONENTSERIAL NUMBER

SUBCOMPONENT PART NUMBER

HRS TOREPLACE

8323869MODEL: UH-60A

Sub Component Listing for 16 Items

AIRCRAFT SERIAL NO:

03A01A PISTON, MAIN L/GEAR STR70250-12067-102C00101885 P02117 9513 36385875

03A01A MAIN SHOCK STRUTPISTON

70250-12067-102IA01223 IA07118 14701 88265875

05A01I04 M/R SPINDLE NUT70102-08105-102A001-03313 C479-08675 17055 111805875

05A01I04 M/R SPINDLE NUT70102-08105-102A001-06108 C47912080 17936 120615875

05A01I04 M/R SPINDLE NUT70102-08105-102D001-11244 F479-03646 18120 122455875

05A01I04 M/R SPINDLE NUT70102-08105-102D00112447 F47905302 18341 124665875

05A01I06 TIE ROD (M/R SPINDLE)38023-10372-101A001-03313 B504-03537 12055 61805875

05A01I06 TIE ROD (M/R SPINDLE)38023-10372-101A001-06108 C50402784 12936 70615875

05A01I06 TIE ROD (M/R SPINDLE)38023-10372-101D001-11244 C504-09832 13120 72455875

05A01I06 TIE ROD (M/R SPINDLE)38023-10372-101D00112447 C50409318 13341 74665875

05A01I07 HORN ASSEMBLY70102-08111-047A001-03313 A24113654 24055 181805875

05A01I07 HORN ASSEMBLY70102-08111-047A001-06108 E241-00164 24936 190615875

05A01I07 HORN ASSEMBLY70102-08111-047D001-11244 G24101278 25120 192455875

05A01I07 HORN ASSEMBLY70102-08111-047D00112447 G24102477 25341 194665875

05A02I M/R BLADE CUFF70150-09109-041A00700708 A23706580 6139 2645875


05A02I M/R BLADE CUFF70150-09109-041A007-13990 G237-00426 9325 34505875

ReportDate:


05A02I M/R BLADE CUFF70150-09109-041A007-13991 E237-00399 9325 34505875

05A03A02 ROTATING SWASHPLATE70104-08001-045MSU45 1515201506 16000 101255875

06A08 SWASHPLATE GUIDE70351-08227-041A26500126 F42500503 21936 160615875

06A13 MAIN GEARBOX HOUSINGASSY

70351-08110-045A26500126 F21100074 6794 9195875

06A18 MAIN ROTOR SHAFT70351-08131-048A26500126 E25304614 12536 66615875

06A19 PLANETARY CARRIER ASSY70351-08175-046A26500126 A24001922 16751 108765875

06G01C I/B RETENTION PLATE T/R70358-06612-042A006-00482 FM2700 17341 114665875

06G01D GEARSHAFT, BEVEL70358-06620-102A006-00482 A320-04161 10103 42285875

06H23A BALL BRNG ANN (OILCOOLER FWD)

210SFFCC512-00281SB UNK1SB 7183 13085875


210SFFCC512-00281SB UNK2SB 7183 13085875

11C23A BRNG T/R PITCH CHGSHAFT

SB1162-102233-04095 11404 6823 9485875

WUC PART NOMENCLATURE

HRS TOREPLACE

SUBCOMPONENTPART NUMBER


AIRCRAFTCURR DUE

AIRCRAFT SERIAL NO:UH-60AMODEL:

SER NO

Sub Component Listing for 76F01

8323869


HRS TOREPLACE

SUBCOMPONENTPART NUMBER PART NOMENCLATUREWUC SER NO


AIRCRAFTCURR DUE

Sub Component Listing for 16-1 Items

AIRCRAFT SERIAL NO:

6035T88P04GE-C-03733904A01C01 GAS GENERATOR TURBINESHAFT

89634815GATCV6K0 13778

6035T88P07GEC03765504A01C01 GAS GENERATOR TURBINESHAFT

106154109NCE141CC 14724

ReportDate:


6035T83P01GE-C-03733904A01C04 COMPRESSOR REAR SHAFT 15914815GAT9936F 6406

6035T83P01GEC03765504A01C04 COMPRESSOR REAR SHAFT 15654109FIA8C631 5674

5043T04P02GE-C-03733904A01C07 TIE ROD, COMPRESSOR 76984815GATMF747 12513

5043T04P02GEC03765504A01C07 TIE ROD, COMPRESSOR 99864109GATHPMD4 14095

4045T08P01GE-C-03733904A01C08 RING, SPACERCOMPRESSOR

58464815GATAJ289 10661

4045T08P01GEC03765504A01C08 RING, SPACERCOMPRESSOR

79494109GATV4603 12058

6055T59P01GE-C-03733904A01D COMPRESSOR IMPELLER 38704815GLHTKC6A 8685

6055T59P01GEC03765504A01D COMPRESSOR IMPELLER 49924109GLHTMTM3 9101

6032T26G09GE-C-03733904A01H STAGE 1 BLISK 38704815GLHTKJNJ 8685

6032T26G09GEC03765504A01H STAGE 1 BLISK 49924109GLHTM5WA 9101

6032T27P08GE-C-03733904A01J STAGE 2 BLISK 58704815GATHGMRM 10685

6032T27P08GEC03765504A01J STAGE 2 BLISK 69924109GLHTMWJG 11101

6038T08P04GE-C-03733904A01K STAGE 3 & 4 BLISK 58704815GLHTJWE4 10685

6038T08P04GEC03765504A01K STAGE 3 & 4 BLISK 69924109GLHTN046 11101

6038T09P04GE-C-03733904A01L STAGE 5 BLISK 58704815GLHTK2F0 10685

6038T09P04GEC03765504A01L STAGE 5 BLISK 69924109GLHTMP3E 11101

6064T85P01MRS0761404A02B01 STAGE 1 TURBINE DISK 30424815GATH89T9 7857

6064T85P01MRSG387904A02B01 STAGE 1 TURBINE DISK 26794109GAT2861T 6788

6064T86P01MRS0761404A02B04 STAGE 2 TURBINE DISK 18474815GAT8262U 6662

6064T86P02MRSG387904A02B04 STAGE 2 TURBINE DISK 47324109GATHGKPH 8841

ReportDate:


6064T81P01MRS0761404A02B05 STAGE 1 FWD COOLINGPLATE

30424815GFF5A91F 7857

6064T81P01MRSG387904A02B05 STAGE 1 FWD COOLINGPLATE

45614109PAMEU309 8670

6064T82P01MRS0761404A02B06 STAGE 1 REAR COOLINGPLATE

30424815GFF5A92W 7857

6064T82P01MRSG387904A02B06 STAGE 1 REAR COOLINGPLATE

45244109GFF5D6E4 8633

6064T83P01MRS0761404A02B08 STG 2 FWD COOLING PLATE 30424815GFF5ADCC 7857


21024109PAMBG560 6211


30424815GFF5A0JP 7857


31724109GFF5A0TT 7281

6038T32P02GEL03723504A03E01 STAGE 3 TURBINE DISK 40204109GATHG5G8 8129

6038T32P01GE-L-03725604A03E01 STAGE 3 TURBINE DISK 12774815GATJV421 6092

6038T34P05GEL03723504A03E02 STAGE 4 TURBINE DISK 49594109GATHELCK 9068

6038T34P05GE-L-03725604A03E02 STAGE 4 TURBINE DISK 12774815GATJJ854 6092

5125T92G01GEL03723504A03F POWER TURBINE SHAFT 43434109GATHKRG1 8452

5125T92G01REGE-L-03725604A03F POWER TURBINE SHAFT 11694815GATLY437 5984

450290287627615B02B WHEEL, COMPRESSOR 29054802SIF1371 7707

450399187627615B03 WHEEL, TURBINE 50594802K709 9861


HRS TOREPLACE



AIRCRAFTCURR DUE

Sub Component Listing for 714 Engines

AIRCRAFT SERIAL NO:

PIDMWODATE HRS



SWASHPLATE ASSY 8323869MSU451. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


14-Oct-1997 OU

DS232111-Jun-2007

0.5CCAD C.C.TEXAS 78419-5260

ALL UH-60A/L, EH-60A AND MH-60KHELICOPTERS, REMOVAL OFSPECIFIC SUSPECT REWORKEDMAIN ROTOR SWASHPLATEASSEMBLIES

1-1520-237-20-201MWO:

Priority Mnt Level



360

360

5103

8323869 3582 5103


UH-60A A006-00482 Days


HELICOPTER, UTILITY TAIL ROTOR GEARBOX ASSY Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

VZ74839130-Sep-2010NORMALBASELINE0.02810510329-Sep-2010

29-Sep-2011NORMALROUTINE177.02987528022-Sep-2011



LD19731429-Apr-2013NORMALROUTINE520.03330562329-Apr-2013

JR76327318-Sep-2013ABNORMALROUTINE598.03408570118-Sep-2013

g02-Apr-2014BASELINE599.93409.95702.906-Jan-2014

AJ81533814-Mar-2014NORMALROUTINE620.93430.95723.926-Feb-2014


INSUFFICIENT AMT OF OIL. RESAMPLE AT THE END OF THE NEXT FLIGHT DAY CYCLE.

9. REMARKS:



PIDMWODATE HRS



TAIL ROTOR GEARBOX ASSY 8323869A006-004821. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


22-Dec-2004 DR

KK845630-May-2008

1CCADRECAPITALIZATION REQUIREMENTSDMWR 1-1615-279MWO:

Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR PITCH CHANGE SHAFT 8323869233-040951. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


24-Jan-2014 FT

RT31947629-Jan-2014


ALL UH-60 SERIES AIRCRAFT,PERFORM ONE TIME INSPECTIONOF THE TAIL ROTOR PITCH CHANGESHAFT ASSEMBLY (SERVOCOUPLING ASSEMBLY)

H-60-14-SOF-02MWO:

Priority Mnt Level



UNIT UNIQUE INVENTORY ITEMSSES BEST


8323869 UH-60A



1BFT PALLET ASSEMBLY (040537-001)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

66

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





UNIT UNIQUE INVENTORY ITEMSSES BEST8323869 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

TM7295391 CIV 05-Jan-2016



a. ITEM NUMBER

Nomenclature

BFT PALLET ASSEMBLY(040537-001)



PIDMWODATE HRS



HUB, M/R ROTOR ASSY 8323869A308-004531. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


30-Dec-2013 FM

RS63083226-Jun-2014


ALL H-60 SERIES AIRCRAFT, ONETIME EDDY CURRENT INSPECTIONOF SUSPECTED REWORKED M/RHUB ASSY FOR CRACKS.

H-60-14-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



INPUT MODULE 8323869A264-024281. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


02-Aug-2000 OT

03-Aug-20000.52-502 AVN REGT

APO 09028(TB6357)

ALL H-60 SERIES AIRCRAFT,REMOVAL OF INPUT MODULE GEARBOX ASSEMBLIESWITHPOTENTIALLY CRACKED BEVELGEARS

UH-60-00-02MWO:

Priority Mnt Level



360

360

1493

8323869 4382 1493


UH-60A A005-00592 Days


HELICOPTER, UTILITY INTERMEDIATE GEARBOX Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

BS57423509-Jul-2008NORMALROUTINE4663.03170466308-Jul-2008

BS57423516-Dec-2008NORMALROUTINE4703.03210470309-Dec-2008

VZ74839127-Mar-2009NORMALROUTINE4743.03250474320-Mar-2009

TF54643922-May-2009NORMALROUTINE3290.03290478311-May-2009

JW82927726-Aug-2009NORMAL40 HOUR3329.03329482205-Aug-2009

22-Sep-2009NORMAL40 HOUR3368.03368486108-Sep-2009

DG10618708-Dec-2009NO RESULTS40 HOUR3410.03410490301-Oct-2009

VZ74839108-Dec-2009NORMAL40 HOUR3446.03446493908-Dec-2009

VZ74839122-Feb-2010NORMAL40 HOUR3481.03481497416-Jan-2010



15-Nov-2011ABNORMALPRE PHASE3848.03848534109-Nov-2011

RT31947612-Mar-2012NORMALSPECIAL3887.03887538012-Mar-2012

RT31947629-Apr-2013NORMALROUTINE4123.04123561627-Apr-2013



PRE PHASE

9. REMARKS:



PIDMWODATE HRS





15-Apr-2010 OT

21-Apr-20102D CO 1-214TH


H-60-10-SOF-01MWO:

Priority Mnt Level

09-Apr-2012 OT

LD19731411-Apr-2012

1D CO 1-214THAVN


H-60-12-SOF-05MWO:

Priority Mnt Level



PIDMWODATE HRS





15-Apr-2010 OT

21-Apr-20102D CO 1-214TH


H-60-10-SOF-01MWO:

Priority Mnt Level

09-Apr-2012 OT

LD19731411-Apr-2012

1D CO 1-214THAVN


H-60-12-SOF-05MWO:

Priority Mnt Level



PIDMWODATE HRS





28-Feb-1998 DU

EL995229-May-2009

1CCADINCREASE IN FATIGUE LIFE FORTHE M/R CUFF ASSY, PN 70150-09109-041 AND 70150-09109-043

1-1520-237-20-16MWO:

Priority Mnt Level

28-Feb-1998 DU

LM674926-Jul-2011

1CCADINCREASE IN FATIGUE LIFE FORTHE MAIN ROTOR BLADE CUFFS,P/N 70150-09109-041 AND 70150-09109-043

UH-60-97-ASAM-11/TB 1-1MWO:

Priority Mnt Level

12-Aug-2002 OT

LM674926-Jul-2011

1CCADALL H-60 SERIES AIRCRAFT,REVISION TO UH-60-02-11, ONE-TIMEINSPECTION OF MAIN ROTORBLADE CUFF ASSEMBLY

UH-60-02-12MWO:

Priority Mnt Level

07-Jan-2003 DM

LM674926-Jul-2011

1CCADONE TIME INSP OF M/R CUFF ASSYSOF UH-60-03-02MWO:

Priority Mnt Level

07-Jan-2003 OT

EL995229-May-2009

1CCADINITIAL AND RECURRINGINSPECTION OF MAIN ROTORBLADE CUFF ASSEMBLY, ALL H-60AIRCRAFT

UH-60-03-SOF-02MWO:

Priority Mnt Level

15-Sep-2005 DU

LM674926-Jul-2011

130CCADRECAPITALIZATION REQUIRED FORH-60 MAIN ROTOR BLADE P/N 70150-09100-043 NSN 1615-01-106-1903

DMWR 1-1615-281, C1MWO:

Priority Mnt Level

15-Sep-2005 DU

EL995229-May-2009

130CCADRECAP REQUIREMENTS COMPLIEDWITH.

DMWR 1-1615-281,C1,U,DMWO:

Priority Mnt Level

15-Apr-2010 OT

LM674926-Jul-2011

3CCADALL H-60A/K/L SERIES AIRCRAFT,DEPOT REPAIRED LEGACY MAINROTOR BLADES

H-60-10-SOF-01MWO:

Priority Mnt Level

09-Apr-2012 OT

LD19731411-Apr-2012

1D CO 1-214THAVN


H-60-12-SOF-05MWO:

Priority Mnt Level



PIDMWODATE HRS





15-Apr-2010 OT

LD19731406-Jul-2012

1D CO 1-214THAVN

ALL H-60A/K/L SERIES AIRCRAFT,DEPOT REPAIRED LEGACY MAINROTOR BLADES

H-60-10-SOF-01MWO:

Priority Mnt Level

09-Apr-2012 OT

LD19731411-Apr-2012

1D CO 1-214THAVN


H-60-12-SOF-05MWO:

Priority Mnt Level



PIDMWODATE HRS





19-Mar-2001 FU

14-Jan-20030.52-502 AVN REGT

AE 09058(LR0306)

ALL H-60 AIRCRAFT, INSPECTION OFMAIN ROTOR SPINDLE

1-1520-237-20-230MWO:

Priority Mnt Level

09-Apr-2002 FU

14-Jan-20030.52-502 AVN REGT

AE 09058(LR0306)

ALL UH-60, SERIES AIRCRAFT,REMOVAL OF CHICAGO RAW HIDEM/R SPINDLE THRUST BEARINGSWITH SERIAL NUMBERS C325-00001THROUGH C325-02407

1-1520-237-20-251MWO:

Priority Mnt Level

05-Sep-2012 FM

LD19731404-Oct-2012

1D CO 1-214THAVN


H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

LD19731401-Mar-2013

1D CO 10214THAVN


H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS





05-Sep-2012 FM

LD19731404-Oct-2012

1D CO 1-214THAVN


H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

LD19731401-Mar-2013

1D CO 1-214THAVN


H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 8323869D001-112441. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Sep-2012 FM

LD19731404-Oct-2012

1D CO 1-214THAVN


H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

LD19731401-Mar-2013

1D CO 1-214THAVN


H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 8323869D001124471. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Sep-2012 FM

LD19731404-Oct-2012

1D CO 1-214THAVN


H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

LD19731401-Mar-2013

1D CO 1-214THAVN


H-60-13-ASAM-03MWO:

Priority Mnt Level



0

720

5701

8323869 3187 4936


UH-60A A26500126 Days


HELICOPTER, UTILITY MAIN TRANSMISSION MODULE Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

VZ74839108-Dec-2009NORMALBASELINE1.02249493708-Dec-2009




JR01622530-Aug-2012NORMALSPECIAL572.02820550830-Aug-2012

LW84913019-Sep-2012NORMALSPECIAL590.02838552618-Sep-2012

RT31947611-Apr-2013NORMALSPECIAL676.02924561204-Apr-2013

RT31947602-May-2013NORMALSPECIAL680.02928561601-May-2013

RL17290214-May-2013NORMALSPECIAL680.02928561614-May-2013

RT31947616-Jul-2013NORMALSPECIAL699.02947563508-Jul-2013


BJ96335409-Oct-2014NORMALROUTINE170.03183587109-Oct-2014

PRE PHASE

9. REMARKS:



PIDMWODATE HRS



MAIN TRANSMISSION MODULE 8323869A265001261. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


26-Mar-2014 FM

RT31947611-Apr-2014


MAIN TRANSMISSION FILTER BOWLAND CHIP DETECTOR ATTACHMENTHARDWARE REPLACEMENT.

H-60-14-AMAM-09MWO:

Priority Mnt Level



9032149075875B112-102951560011291256SAS ACTUATOR70410-02500-04907A24


1/308-Jan-2016

DUE

AIRCRAFT HRS TO

REPLACESERIAL NONSNPART NOMENCLATUREPART NO

UH-60AMODEL:

WUC

8323869

CURR

AIRCRAFT SERIAL NO:

Major Component Listing for 16 Items

14125200005875UNK38691560010819244TAIL PYLON FITTING70209-06051-04302C15J

85867335875A308-004531615014816953HUB, M/R ROTOR ASSY70070-10046-05505A01A



7245131205875D001-112441615014426926MAIN ROTOR SPINDLE ASSY70102-08200-06905A01I

7466133415875D001124471615014426926MAIN ROTOR SPINDLE ASSY70102-08200-06905A01I

6242121175875C286-000951615010745151MAIN ROTOR SHAFT EXTENDER70351-08186-04305A01L

7125130005875015152-05521615011277388BIFILAR, M/R ROTOR ASSY70107-08400-04605A01T





6810126855875A009-039831615011138188TAIL ROTOR BLADE ASSY70101-31000-04305B02

5471113465875A009028021615011138188TAIL ROTOR BLADE ASSY70101-31000-04305B02

6843127185875B257001461615010836812O/B RETENTION PLATE (T/R)70102-11101-04206G01B

91267875875C512-00281SB4141013293428FAN AXIAL70361-03005-10706H23

8403142785875B112-051561560011291256SAS ACTUATOR70410-02500-04907A24


2/308-Jan-2016

9032149075875B112-102951560011291256SAS ACTUATOR70410-02500-04907A24

11319171945875C112-011861560011291256SAS ACTUATOR70410-02500-04907A24

94868235875233-040951615011417532TAIL ROTOR PITCH CHANGE SHAFT70400-06100-04211C23

14114199895875B300-021421650013056954TAIL ROTOR SERVO ASSY2227000-1711C25

22284281595875B30311458B1650011431226MAIN ROTOR PRIMARY SERVO274000-103111D01



7125130005875C345-031391560011589685AFT BELLCRANK70400-08102-04511D04

11125170005875A391-006201560010829213AFT TIE ROD SUPT FITTING70400-08112-04411D05

28061555875A392-003771680011644160AFT TIE ROD ASSY70400-08111-04211D06

4226101015875390019171560012868870AFT BELLCRANK SPT ASSY70400-08117-04911D07

10061159365875015152-007903040012872438LATERAL SWASHPLATE LINK70400-08151-06111D08

18788246635875F337-029771680012212863LATERAL SERVO BELLCRANK70400-08166-04111D09

5125110005875B346-007351680011589653AFT WALKING BEAM70400-08104-04811D11

7945138205875E344-013031560011589475LEFT TIE ROD70400-08115-04511D13

22888163587533325-611560012969486RIGHT TIE ROD ASSY70400-08114-05111D14

137881966358756321680011589652FORWARD BELLCRANK70400-08101-04611D15

4388102635875B367044901560012212619FWD BELLCRANK SPT ASSY70400-08162-04211D16


AIRCRAFT

DUE REPLACE

HRS TO

CURR

Major Component Listing for 76F01


WUC


3/308-Jan-2016


AIRCRAFT

DUE REPLACE

HRS TO

CURR

Major Component Listing for 16-1 Items


WUC

-48024802 08762762835013692818AUXILIARY POWER UNIT116305-30215B


AIRCRAFT

DUE REPLACE

HRS TO

CURR

Major Component Listing for 714 Engines


WUC

PIDMWODATE HRS



MTCHD ROTOR/STATOR ASSY 8323869MRS076141. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


31-Jul-1989 OM

18-Sep-200333CCAD

(FO0000)MODIFICATION OF GG ROTORASSEMBLY T700/701 REWORK T700ENGINES

55-2840-248-50-32MWO:

Priority Mnt Level

30-Jun-1994 OR

18-Sep-20034CCAD

(FO0000)ONE TIME INSPECTION ANDCONVERSION OF FORMS ANDRECORDS FOR T700-GE-700, -701AND -701C SERIES GAS TURBINEENGINES

1-2840-248-20-2MWO:

Priority Mnt Level

19-Sep-1995 OI

18-Sep-20030.1CCAD

(FO0000)ALL UH-60A, EH-60A, AND AH-64AAIRCRAFT WITH T700-GE-700 ANDT700-GE-701 ENGINES, SUBJECT:GAS GENERATOR TURBINE ROTORBLADE INFORMATION


Priority Mnt Level

25-Oct-1996 OM

18-Sep-20030.5CCAD

(FO0000)ALL UH-60A, EH-60A AIRCRAFT WITHT700-GE-700 ENGINES SUBJECT:REPLACEMENT OF UNDAMPED GASGENERATOR ROTOR/STATORASSEMBLIES


Priority Mnt Level



PIDMWODATE HRS



SAS ACTUATOR 8323869B112-102951. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


23-Mar-2001 FT

26-Mar-20010.5D C0, 1-214TH

AVN REGT(DB4697)

ALL H-60 SERIES AIRCRAFT,INSPECTION OF ALL SASACTUATORS

UH-60-01-06MWO:

Priority Mnt Level





8323869 UH-60A



1RECEIVER RADIO - R-1496A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1DISPLACEMENT GYRO - CN-1314/A (9000C)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un0

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING FOR KIT-1A/1C/TSEC - MT-3949A/U

Unt

UUUUUUnt

Unt

Un

Unt

Un0

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMMAND INSTR SYS PROCESSOR - 70600-01038-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNTING RACK - 70600-01038-102

Unt

UUUUUUnt

Unt

Un

Unt

Un1

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT FOR TSEC/KY-58 - 5290279-502

Unt

UUUUUUnt

Unt

Un

Unt

Un1

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1#2 VHF-FM ANTENNA - AS-4171/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un1

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SAS AMPLIFIER - 70901-02908-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO ASSEMBLY - 70600-01047-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2RATE GYRO - TRU-2A/A

Unt

UUUUUUnt

Unt

Un

Unt

Un1

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8323869 UH-60A



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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un2

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER RADAR - RT-1193/ASN-128

Unt

UUUUUUnt

Unt

Un

Unt

Un1

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un2

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GLIDE SLOPE ANTENNA - 70600-01043-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un2

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER



Unt

UUUUUUnt

Unt

Un

Unt

Un1

25

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BAROMETERIC ALTIMETER - AAU-31/A-1

Unt

UUUUUUnt

Unt

Un

Unt

Un1

26

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BAROMETERIC ALTIMETER - AAU-32/A

Unt

UUUUUUnt

Unt

Un

Unt

Un1

27

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2CREW SEAT - D3801-2

Unt

UUUUUUnt

Unt

Un

Unt

Un2

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF-AM RADIO SET - RT-1518/ARC-164(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

31

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER



Unt

UUUUUUnt

Unt

Un

Unt

Un2

32

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RECEIVER/TRANSMITTER - RT-1115D/APN-209

Unt

UUUUUUnt

Unt

Un

Unt

Un1

33

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

34

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8323869 UH-60A



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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

35

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2CONTROL - C-10604(V)6/ARN-184

Unt

UUUUUUnt

Unt

Un

Unt

Un2

36

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPARATOR SIGNAL DATA - CM482/ARC-186(V)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

38

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2MOUNTREVERSIBLE ARC-186/ARC-201 - 4290268-501

Unt

UUUUUUnt

Unt

Un

Unt

Un2

40

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPUTER DISPLAY UNIT - CP-1252C/ASN-128B

Unt

UUUUUUnt

Unt

Un

Unt

Un1

42

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

43

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un0

44

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RADIO RETRANSMISSION PANEL -70550-01008-042

Unt

UUUUUUnt

Unt

Un

Unt

Un1

45

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MAGNETIC COMPASS - MS17983-4

Unt

UUUUUUnt

Unt

Un

Unt

Un1

46

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2OUTSIDE AIR TEMP INDICATOR - MS28028-1

Unt

UUUUUUnt

Unt

Un

Unt

Un2

47

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER



Unt

UUUUUUnt

Unt

Un

Unt

Un1

48

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER



Unt

UUUUUUnt

Unt

Un

Unt

Un1

49

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MISC. SWITCH PANEL - 70450-01090-044

Unt

UUUUUUnt

Unt

Un

Unt

Un1

50

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1STABILATOR/FLT CONT PANEL - 70902-01070-048

Unt

UUUUUUnt

Unt

Un

Unt

Un1

51

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2AHRU MOUNTING PLATE FOGS

Unt

UUUUUUnt

Unt

Un

Unt

Un1

60

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8323869 UH-60A



1MOUNTING BASE APX-118

Unt

UUUUUUnt

Unt

Un

Unt

Un1

61

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1765200-20 FOGS CONTROL UNIT (AHRU)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

62

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2ATTITUDE & HEADING REFERENCE UNIT, CN-1716/A (FOGS)

Unt

UUUUUUnt

Unt

Un

Unt

Un1

63

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1RATE GYRO ASSEMBLY 70600-01213-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

64

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION I COCKPITSES BEST8323869 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

TM7295391 CIV 05-Jan-2016



a. ITEM NUMBER

Nomenclature

GYRO, DIRECTIONAL - CN-998/ASN-43

1 ACFT has FOGS Configuration3

MOUNTING FOR KIT-1A/1C/TSEC - MT-3949A/U

1 ACFT Configured for KY585

RATE GYRO - TRU-2A/A1 ACFT Configured for FOGS14

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

1 ACFT Configured for FOGS44

AHRU MOUNTING PLATEFOGS


ATTITUDE & HEADINGREFERENCE UNIT, CN-1716/A(FOGS)





8323869 UH-60A



1CARGO HOOK, FE-7590-145 70800-02503-111

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MARKER BEACON ANTENNA - 70600-02011-103

Unt

UUUUUUnt

Unt

Un

Unt

Un1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER



Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER



Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRST AID KIT - 6545-00919-6650

Unt

UUUUUUnt

Unt

Un

Unt

Un1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER



Unt

UUUUUUnt

Unt

Un

Unt

Un2

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1CRASH AXE - 56D6221

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HAND SET - H-250/U

Unt

UUUUUUnt

Unt

Un

Unt

Un1

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1SLAB BATTERY -D8565/11-1

Unt

UUUUUUnt

Unt

Un

Unt

Un1

9

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER



Unt

UUUUUUnt

Unt

Un

Unt

Un3

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ADAPTER FUEL DRAIN - 70307-03018-102

Unt

UUUUUUnt

Unt

Un

Unt

Un0

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


4LOCK ASSY BLADE TIEDOWN - 70700-20369-041

Unt

UUUUUUnt

Unt

Un

Unt

Un4

12

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2PLUG ASSY INTAKE - HIRSS SUPP - 70700-20515-041/042

Unt

UUUUUUnt

Unt

Un

Unt

Un2

13

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un0

14

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PLUG ASSY APU EXHAUST - 70700-20509-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

15

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8323869 UH-60A



1COVER ASSY OIL COOLER - 70700-20511-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

16

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1BLADE FOLD SET - 70700-20412-011

Unt

UUUUUUnt

Unt

Un

Unt

Un1

17

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2COVER PITOT TUBE - 70700-20460-041

Unt

UUUUUUnt

Unt

Un

Unt

Un1

18

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


7TROOP SEATS - 70500-02151-045

Unt

UUUUUUnt

Unt

Un

Unt

Un7

19

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


3TROOP SEATS - 70500-02151-047

Unt

UUUUUUnt

Unt

Un

Unt

Un4

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER



Unt

UUUUUUnt

Unt

Un

Unt

Un11

21

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GUNNER SEAT - 70500-02152-047

Unt

UUUUUUnt

Unt

Un

Unt

Un1

22

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GUNNER SEAT - 70500-02152-048

Unt

UUUUUUnt

Unt

Un

Unt

Un1

23

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER



Unt

UUUUUUnt

Unt

Un

Unt

Un2

24

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ICS WALK-AROUND CORD - 70602-02016-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

28

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


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

Unt

UUUUUUnt

Unt

Un

Unt

Un1

29

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HYD. PUMP HANDLE - 15400-50126

Unt

UUUUUUnt

Unt

Un

Unt

Un1

30

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FIRING KEY - 70550-03101-101

Unt

UUUUUUnt

Unt

Un

Unt

Un1

31

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2EQUIPMENT LOGBOOK - MIL-D-43064

Unt

UUUUUUnt

Unt

Un

Unt

Un1

32

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1WEIGHT AND BALANCE HANDBOOK - TM 55-1500-342-23

Unt

UUUUUUnt

Unt

Un

Unt

Un1

34

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






8323869 UH-60A



1ELECTRONIC SEQUENCE UNIT - 163290-100-E

Unt

UUUUUUnt

Unt

Un

Unt

Un1

52

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION II CABINSES BEST8323869 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

TM7295391 CIV 05-Jan-2016



a. ITEM NUMBER

Nomenclature

ADAPTER FUEL DRAIN - 70307-03018-102


PLUG ASSY EXHAUST - HIRSS- 70700-20515-043


PLUG ASSY APU EXHAUST -70700-20509-041


COVER PITOT TUBE - 70700-20460-041

1 ACFT dellivered in this configuration18

TROOP SEATS - 70500-02151-047


RESTRAINT SYSTEM - 70500-02153-103


ICS WALK-AROUND CORD -70602-02016-041


EQUIPMENT LOGBOOK - MIL-D-43064


WEIGHT AND BALANCEHANDBOOK - TM 55-1500-342-23



SECTION III TRANSITION SECTIONSES BEST


8323869 UH-60A



1ANTENNA LOOP - AS-2108A/ARN-89

Unt

UUUUUUnt

Unt

Un

Unt

Un1

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2IFF ANTENNA - 70600-02010-103

Unt

UUUUUUnt

Unt

Un

Unt

Un2

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1UHF/AM ANTENNA - 70600-03002-104

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1PUMP FUEL SAMPLER - 82829/4P156-3

Unt

UUUUUUnt

Unt

Un

Unt

Un0

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPENSATOR MAGNETIC FLUX - CN-405/ASN

Unt

UUUUUUnt

Unt

Un

Unt

Un1

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1COMPASS TRANSMITTER - T-611/ASN-43

Unt

UUUUUUnt

Unt

Un

Unt

Un1

6

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1GPS ANTENNA - 22433-40

Unt

UUUUUUnt

Unt

Un

Unt

Un1

7

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF AMPLIFIER - AM-7531/URC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

8

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA. GPS (BFT) S67-1575-863

Unt

UUUUUUnt

Unt

Un

Unt

Un0

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA, L-BAND (BFT) S65-8282-301

Unt

UUUUUUnt

Unt

Un

Unt

Un0

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1MOUNT, IFM AMPLIFIER-MT-6592/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

42

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1AS-3933/ARN-149(V)1, ANTENNA, LOOP

Unt

UUUUUUnt

Unt

Un

Unt

Un1

49

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1TROOP COMMANDER ANTENNA (CMWS ONLY)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

50

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IVHMU (CBM MONITOR SYSTEM)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

55

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION III TRANSITION SECTIONSES BEST8323869 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

TM7295391 CIV 05-Jan-2016



a. ITEM NUMBER

Nomenclature

PUMP FUEL SAMPLER -82829/4P156-3


HF AMPLIFIER - AM-7531/URC1 ACFT delivered in this configuration8

ANTENNA. GPS (BFT) S67-1575-863


ANTENNA, L-BAND (BFT) S65-8282-301


MOUNT, IFM AMPLIFIER-MT-6592/ARC


TROOP COMMANDERANTENNA (CMWS ONLY)

1 ACFT delivered in this configuration. No CMWS Mod50


SECTION IV TAIL CONESES BEST


8323869 UH-60A



2VOR/LOC ANTENNA - 70600-05002-101

Unt

UUUUUUnt

Unt

Un

Unt

Un2

1

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1IFM AMPLIFIER - AM-7189A/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1HF ANTENNA - 4700516-30

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION IV TAIL CONESES BEST8323869 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

TM7295391 CIV 05-Jan-2016



a. ITEM NUMBER

Nomenclature

IFM AMPLIFIER - AM-7189A/ARC



SECTION V TAIL ROTOR PYLONSES BEST


8323869 UH-60A



1CU-2457/ARC(405-11-1), VHF-FM #1 COUPLER ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un1

2

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM10-267, VHF-FM #2 (LEADING EDGE) ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un1

3

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1FM10-3230, VHF-FM TROOP COMMANDER ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un1

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION V TAIL ROTOR PYLONSES BEST8323869 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

TM7295391 CIV 05-Jan-2016



a. ITEM NUMBER

Nomenclature


ReportDate:


PART NOMENCLATURE SER NO

AIRCRAFTCURR DUEWUC


SUBCOMPONENT PART NUMBER

HRS TOREPLACE


Sub Component Listing for 16 Items

AIRCRAFT SERIAL NO:

03A01A PISTON, MAIN L/GEAR STR70250-12067-102C00101885 P02117 9513 36385875

03A01A MAIN SHOCK STRUTPISTON

70250-12067-102IA01223 IA07118 14701 88265875

05A01I04 M/R SPINDLE NUT70102-08105-102A001-03313 C479-08675 17055 111805875

05A01I04 M/R SPINDLE NUT70102-08105-102A001-06108 C47912080 17936 120615875

05A01I04 M/R SPINDLE NUT70102-08105-102D001-11244 F479-03646 18120 122455875

05A01I04 M/R SPINDLE NUT70102-08105-102D00112447 F47905302 18341 124665875

05A01I06 TIE ROD (M/R SPINDLE)38023-10372-101A001-03313 B504-03537 12055 61805875

05A01I06 TIE ROD (M/R SPINDLE)38023-10372-101A001-06108 C50402784 12936 70615875

05A01I06 TIE ROD (M/R SPINDLE)38023-10372-101D001-11244 C504-09832 13120 72455875

05A01I06 TIE ROD (M/R SPINDLE)38023-10372-101D00112447 C50409318 13341 74665875

05A01I07 HORN ASSEMBLY70102-08111-047A001-03313 A24113654 24055 181805875

05A01I07 HORN ASSEMBLY70102-08111-047A001-06108 E241-00164 24936 190615875

05A01I07 HORN ASSEMBLY70102-08111-047D001-11244 G24101278 25120 192455875

05A01I07 HORN ASSEMBLY70102-08111-047D00112447 G24102477 25341 194665875



05A02I M/R BLADE CUFF70150-09109-041A007-13990 G237-00426 9325 34505875

ReportDate:


05A02I M/R BLADE CUFF70150-09109-041A007-13991 E237-00399 9325 34505875

05A03A02 ROTATING SWASHPLATE70104-08001-045MSU45 1515201506 16000 101255875

06A08 SWASHPLATE GUIDE70351-08227-041A26500126 F42500503 21936 160615875

06A13 MAIN GEARBOX HOUSINGASSY

70351-08110-045A26500126 F21100074 6794 9195875

06A18 MAIN ROTOR SHAFT70351-08131-048A26500126 E25304614 12536 66615875

06A19 PLANETARY CARRIER ASSY70351-08175-046A26500126 A24001922 16751 108765875

06G01C I/B RETENTION PLATE T/R70358-06612-042A006-00482 FM2700 17341 114665875

06G01D GEARSHAFT, BEVEL70358-06620-102A006-00482 A320-04161 10103 42285875


210SFFCC512-00281SB UNK1SB 7183 13085875


210SFFCC512-00281SB UNK2SB 7183 13085875

11C23A BRNG T/R PITCH CHGSHAFT

SB1162-102233-04095 11404 6823 9485875

WUC PART NOMENCLATURE

HRS TOREPLACE

SUBCOMPONENTPART NUMBER


AIRCRAFTCURR DUE

AIRCRAFT SERIAL NO:UH-60AMODEL:

SER NO

Sub Component Listing for 76F01

8323869


HRS TOREPLACE



AIRCRAFTCURR DUE

Sub Component Listing for 16-1 Items

AIRCRAFT SERIAL NO:

6035T88P04GE-C-03733904A01C01 GAS GENERATOR TURBINESHAFT

89634815GATCV6K0 13778

6035T88P07GEC03765504A01C01 GAS GENERATOR TURBINESHAFT

106154109NCE141CC 14724

ReportDate:


6035T83P01GE-C-03733904A01C04 COMPRESSOR REAR SHAFT 15914815GAT9936F 6406

6035T83P01GEC03765504A01C04 COMPRESSOR REAR SHAFT 15654109FIA8C631 5674

5043T04P02GE-C-03733904A01C07 TIE ROD, COMPRESSOR 76984815GATMF747 12513

5043T04P02GEC03765504A01C07 TIE ROD, COMPRESSOR 99864109GATHPMD4 14095

4045T08P01GE-C-03733904A01C08 RING, SPACERCOMPRESSOR

58464815GATAJ289 10661

4045T08P01GEC03765504A01C08 RING, SPACERCOMPRESSOR

79494109GATV4603 12058

6055T59P01GE-C-03733904A01D COMPRESSOR IMPELLER 38704815GLHTKC6A 8685

6055T59P01GEC03765504A01D COMPRESSOR IMPELLER 49924109GLHTMTM3 9101

6032T26G09GE-C-03733904A01H STAGE 1 BLISK 38704815GLHTKJNJ 8685

6032T26G09GEC03765504A01H STAGE 1 BLISK 49924109GLHTM5WA 9101

6032T27P08GE-C-03733904A01J STAGE 2 BLISK 58704815GATHGMRM 10685

6032T27P08GEC03765504A01J STAGE 2 BLISK 69924109GLHTMWJG 11101

6038T08P04GE-C-03733904A01K STAGE 3 & 4 BLISK 58704815GLHTJWE4 10685

6038T08P04GEC03765504A01K STAGE 3 & 4 BLISK 69924109GLHTN046 11101

6038T09P04GE-C-03733904A01L STAGE 5 BLISK 58704815GLHTK2F0 10685

6038T09P04GEC03765504A01L STAGE 5 BLISK 69924109GLHTMP3E 11101

6064T85P01MRS0761404A02B01 STAGE 1 TURBINE DISK 30424815GATH89T9 7857

6064T85P01MRSG387904A02B01 STAGE 1 TURBINE DISK 26794109GAT2861T 6788

6064T86P01MRS0761404A02B04 STAGE 2 TURBINE DISK 18474815GAT8262U 6662

6064T86P02MRSG387904A02B04 STAGE 2 TURBINE DISK 47324109GATHGKPH 8841

ReportDate:


6064T81P01MRS0761404A02B05 STAGE 1 FWD COOLINGPLATE

30424815GFF5A91F 7857


45614109PAMEU309 8670


30424815GFF5A92W 7857


45244109GFF5D6E4 8633

6064T83P01MRS0761404A02B08 STG 2 FWD COOLING PLATE 30424815GFF5ADCC 7857


21024109PAMBG560 6211


30424815GFF5A0JP 7857


31724109GFF5A0TT 7281

6038T32P02GEL03723504A03E01 STAGE 3 TURBINE DISK 40204109GATHG5G8 8129

6038T32P01GE-L-03725604A03E01 STAGE 3 TURBINE DISK 12774815GATJV421 6092

6038T34P05GEL03723504A03E02 STAGE 4 TURBINE DISK 49594109GATHELCK 9068

6038T34P05GE-L-03725604A03E02 STAGE 4 TURBINE DISK 12774815GATJJ854 6092

5125T92G01GEL03723504A03F POWER TURBINE SHAFT 43434109GATHKRG1 8452

5125T92G01REGE-L-03725604A03F POWER TURBINE SHAFT 11694815GATLY437 5984

450290287627615B02B WHEEL, COMPRESSOR 29054802SIF1371 7707

450399187627615B03 WHEEL, TURBINE 50594802K709 9861


HRS TOREPLACE



AIRCRAFTCURR DUE

Sub Component Listing for 714 Engines

AIRCRAFT SERIAL NO:

PIDMWODATE HRS



SWASHPLATE ASSY 8323869MSU451. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


14-Oct-1997 OU

DS232111-Jun-2007

0.5CCAD C.C.TEXAS 78419-5260

ALL UH-60A/L, EH-60A AND MH-60KHELICOPTERS, REMOVAL OFSPECIFIC SUSPECT REWORKEDMAIN ROTOR SWASHPLATEASSEMBLIES

1-1520-237-20-201MWO:

Priority Mnt Level



360

360

5103

8323869 3582 5103


UH-60A A006-00482 Days


HELICOPTER, UTILITY TAIL ROTOR GEARBOX ASSY Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

VZ74839130-Sep-2010NORMALBASELINE0.02810510329-Sep-2010

29-Sep-2011NORMALROUTINE177.02987528022-Sep-2011



LD19731429-Apr-2013NORMALROUTINE520.03330562329-Apr-2013

JR76327318-Sep-2013ABNORMALROUTINE598.03408570118-Sep-2013

g02-Apr-2014BASELINE599.93409.95702.906-Jan-2014

AJ81533814-Mar-2014NORMALROUTINE620.93430.95723.926-Feb-2014


INSUFFICIENT AMT OF OIL. RESAMPLE AT THE END OF THE NEXT FLIGHT DAY CYCLE.

9. REMARKS:



PIDMWODATE HRS



TAIL ROTOR GEARBOX ASSY 8323869A006-004821. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


22-Dec-2004 DR

KK845630-May-2008

1CCADRECAPITALIZATION REQUIREMENTSDMWR 1-1615-279MWO:

Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR PITCH CHANGE SHAFT 8323869233-040951. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


24-Jan-2014 FT

RT31947629-Jan-2014


ALL UH-60 SERIES AIRCRAFT,PERFORM ONE TIME INSPECTIONOF THE TAIL ROTOR PITCH CHANGESHAFT ASSEMBLY (SERVOCOUPLING ASSEMBLY)

H-60-14-SOF-02MWO:

Priority Mnt Level



UNIT UNIQUE INVENTORY ITEMSSES BEST


8323869 UH-60A



1BFT PALLET ASSEMBLY (040537-001)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

66

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





UNIT UNIQUE INVENTORY ITEMSSES BEST8323869 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c

TM7295391 CIV 05-Jan-2016



a. ITEM NUMBER

Nomenclature

BFT PALLET ASSEMBLY(040537-001)



DA Form 2408-5 - Equipment Modification Record · mwo:1-1520-237-50-56 c2 prioritymnt level 31-mar-1997 r d tasm-o europe 178 26-may-2000 an/asn-128b doppler/gps navigation system

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