Report Date: MAJOR COMPONENT LISTING Sorted By ... 70102-08105-102 M/R SPINDLE NUT F47905529 5610.8 18445 12834.2 D00112206 70102-08111-047 HORN ASSEMBLY G24102240 5610.8 25445 19834.2

Report Date: MAJOR COMPONENT LISTINGSorted By: Serial Number

1/210-May-2016

SERIAL NOPART NO NSNPART NOMENCLATURE

AIRCRAFT

DUE

Major Component Listing for 16 Items

7822971MODEL: UH-60A

CURR

AIRCRAFT SERIAL NO:

REPLACE

HRS TO

14720.2203315610.8UNK34891560-01-081-9244TAIL PYLON FITTING70209-06051-043

4575.2101865610.8D308000111615-01-450-4834HUB, M/R ROTOR ASSY70103-08112-047

4472.2100835610.8A001059051615-01-442-6926MAIN ROTOR SPINDLE ASSY70102-08200-069

4888.2104995610.8B001002901615-01-442-6926MAIN ROTOR SPINDLE ASSY70102-08200-069

5196.2108075610.8D001011021615-01-442-6926MAIN ROTOR SPINDLE ASSY70102-08200-069

6234.2118455610.8D001122061615-01-442-6926MAIN ROTOR SPINDLE ASSY70102-08200-069

8637.2142485610.8C286-003751615-01-074-5151MAIN ROTOR SHAFT EXTENDER70351-08186-043

12475.2180865610.8R327004231615-01-127-7388BIFILAR, M/R ROTOR ASSY70107-08400-046

4627.2102385610.8A009041031615-01-113-8188TAIL ROTOR BLADE ASSY70101-31000-043

7650.2132615610.8A009079831615-01-113-8188TAIL ROTOR BLADE ASSY70101-31000-043

6466.2120775610.8C257000261615-01-083-6812O/B RETENTION PLATE (T/R)70102-11101-042

931.265425610.89E930054SB4141-01-329-3428FAN AXIAL70361-03005-107

8118.2137295610.8B112-072461560-01-129-1256SAS ACTUATOR70410-02500-049

9215.2148265610.8B112-073071560-01-129-1256SAS ACTUATOR70410-02500-049

1635.272465610.8233035751615-01-141-7532TAIL ROTOR PITCH CHANGESHAFT

70400-06100-042

6934.2125455610.8B300015031650-01-305-6954SERVO ASSY, TAIL ROTOR70410-06520-046

15656.2212675610.8B30300913B1650-01-143-1226MAIN ROTOR PRIMARY SERVO70410-02820-054

19140.2247515610.8B303023321650-01-143-1226MAIN ROTOR PRIMARY SERVO70410-02820-054

19695.2253065610.8B303060951650-01-143-1226MAIN ROTOR PRIMARY SERVO70410-02820-054

Report Date: MAJOR COMPONENT LISTINGSorted By: Serial Number

2/210-May-2016

7389.2130005610.8345017291560-01-158-9685AFT BELLCRANK70400-08102-045

15411.2210225610.8E391-021391560-01-164-4161AFT TIE ROD SUPT FITTING70400-08112-045

611.262225610.8M392001211680-01-164-4160AFT TIE ROD ASSY70400-08111-042

3875.294865610.8390-018411560-01-286-8870AFT BELLCRANK SPT ASSY70400-08117-049

9275.2148865610.8A380037953040-01-287-2438LATERAL SWASHPLATE LINK70400-08151-061

19475.2250865610.8F337047971680-01-221-2863LATERAL SERVO BELLCRANK70400-08166-041

13475.2190865610.8344-024011560-01-289-2697LEFT TIE ROD70400-08115-046

1911.275225610.8288-012761560-01-296-9486RIGHT TIE ROD ASSY70400-08114-051

14475.2200865610.818871680-01-158-9652FORWARD BELLCRANK70400-08101-046

5600.2112115610.8B367-044081560-01-221-2619FWD BELLCRANK SPT ASSY70400-08162-042


AIRCRAFT

DUE

Major Component Listing for 76F01

AIRCRAFT SERIAL NO:UH-60AMODEL: 7822971

REPLACE

HRS TO

CURR


AIRCRAFT

DUE

Major Component Listing for 16-1 Items


REPLACE

HRS TO

CURR

-2185021858961242835-01-369-2818AUXILIARY POWER UNIT116305-302


AIRCRAFT

DUE

Major Component Listing for 714 Engines


REPLACE

HRS TO

CURR

Sorted By: Component Serial NumberReportDate:

SUBCOMPONENT LISTING 1/410-May-2016

SUBCOMPONENTPART NUMBER

Sub Component Listing for 16 Items

MAJOR COMPONENTSERIAL NUMBER PART NOMENCLATURE SER NO

AIRCRAFT CURR DUE

UH-60AMODEL: AIRCRAFT SERIAL NO:

HRS TOREPLACE

7822971

70104-08001-045015152-1429 ROTATING SWASHPLATE 7410.25610.8A326-01327 13021

SB1162-10223303575 BRNG T/R PITCH CHG SHAFT 1635.25610.8C84010082 7246

70250-12067-10232937155 PISTON, MAIN L/GEAR STR 5275.25610.8421231 10886

210SFFC39E930054SB BALL BRNG ANN (OILCOOLER FWD)

931.25610.83515 6542

210SFFC39E930054SB BALL BRNG ANN (OILCOOLER FWD)

931.25610.83699 6542

38023-10372-101A00105905 TIE ROD (M/R SPINDLE) 4472.25610.8B50404133 10083

70102-08105-102A00105905 M/R SPINDLE NUT 11072.25610.8C47912369 16683

70102-08111-047A00105905 HORN ASSEMBLY 18072.25610.8A24115450 23683

70358-06612-042A00604489 I/B RETENTION PLATE T/R 11475.25610.8K25911936 17086

70358-06620-102A00604489 GEARSHAFT, BEVEL 4475.25610.8G32000862 10086

70351-08110-045A26501119 HOUSING ASSY MGB 1411.25610.8F21100065 7022

70351-08131-048A26501119 MAIN ROTOR SHAFT 5249.25610.8E25304633 10860

70351-08175-046A26501119 PLANETARY CARRIER ASSY 9189.25610.8A24001235 14800

70351-08227-041A26501119 SWASHPLATE GUIDE 15383.25610.8AER00245 20994

38023-10372-101B00100290 TIE ROD (M/R SPINDLE) 4888.25610.8C504-03992 10499

70102-08105-102B00100290 M/R SPINDLE NUT 11488.25610.8F4790053 17099

70102-08111-047B00100290 HORN ASSEMBLY 18488.25610.8A241-17003 24099



70250-12067-102BEM1635 PISTON, MAIN L/GEAR STR 7767.25610.8BEM1635 13378

38023-10372-101D00101102 TIE ROD (M/R SPINDLE) 5196.25610.8C50405578 10807

70102-08105-102D00101102 M/R SPINDLE NUT 11796.25610.8C47914190 17407

70102-08111-047D00101102 CONTROL HORN ASSY 96.25610.8E24100884 5707

38023-10372-101D00112206 TIE ROD (M/R SPINDLE) 6234.25610.8C50411511 11845

70102-08105-102D00112206 M/R SPINDLE NUT 12834.25610.8F47905529 18445

70102-08111-047D00112206 HORN ASSEMBLY 19834.25610.8G24102240 25445

SER NO AIRCRAFT CURR DUEPART NOMENCLATURE

MAJOR COMPONENTSERIAL NUMBER


HRS TOREPLACE

MODEL: UH-60A 7822971

Sub Component Listing for 76F01

AIRCRAFT SERIAL NO:




HRS TOREPLACE

MODEL: UH-60A 7822971

Sub Component Listing for 16-1 Items

AIRCRAFT SERIAL NO:

4502902896124 WHEEL, COMPRESSOR 109701860V42-C7948 12830

4503991896124 WHEEL, TURBINE 109701860H216 12830

5043T04P02GE-C-007608 TIE ROD, COMPRESSOR 75795759GATHG9DN 13338

5066T79P01GE-C-007608 RING, SPACERCOMPRESSOR

75795759BJWE6140 13338

6032T26G09GE-C-007608 STAGE 1 BLISK 28365759GLHTJMP5 8595

6032T27P08GE-C-007608 STAGE 2 BLISK 28365759GLHTJ7K1 8595



6035T83P01GE-C-007608 COMPRESSOR REAR SHAFT 335759GATSF152 5792

6035T88P03GE-C-007608 GAS GENERATOR TURBINESHAFT

55085759GATW4794 11267

6038T08P04GE-C-007608 STAGE 3 & 4 BLISK 28365759GLHTJT4F 8595

6038T09P04GE-C-007608 STAGE 5 BLISK 28365759GLHTK02F 8595

6055T59P01GE-C-007608 COMPRESSOR IMPELLER 28365759GLHTJD69 8595

5043T04P02GE-C-707432 TIE ROD, COMPRESSOR 66544877GATHJ0WP 11531

5066T79P01GE-C-707432 RING, SPACERCOMPRESSOR

26644877GAT6907N 7541

6032T26G09GE-C-707432 STAGE 1 BLISK 27334877GLHTNJFD 7610

6032T27P08GE-C-707432 STAGE 2 BLISK 27334877GLHTNW3W 7610

6035T83P01GE-C-707432 COMPRESSOR REAR SHAFT 27334877FIAAW67F 7610

6035T88P07GE-C-707432 GAS GENERATOR TURBINESHAFT

87334877GATHWN25 13610

6038T08P04GE-C-707432 STAGE 3 & 4 BLISK 27334877GLHTNW97 7610

6038T09P04GE-C-707432 STAGE 5 BLISK 27334877GLHTP0CW 7610

6055T59P01GE-C-707432 COMPRESSOR IMPELLER 27334877GLHTNNM1 7610

5125T92G01GE-L-006158 POWER TURBINE SHAFT 23214877GATHRGE2 7198

6038T32P01GE-L-006158 STAGE 3 TURBINE DISC -9894877GATKR757 3888

6038T34P05GE-L-006158 STAGE 4 TURBINE DISC -9894877GATNE582 3888

5125T92G01GE-L-006843 POWER TURBINE SHAFT 26415759GATHARE5 8400

6038T32P01GE-L-006843 STAGE 3 TURBINE DISC 11855759GATEF128 6944

6038T34P03GE-L-006843 STAGE 4 TURBINE DISC 11855759GATEB002 6944



6039T50P04MRS08322 STAGE 1 REAR COOLINGPLATE

5204877GATU5433 5397

6039T51P03MRS08322 STAGE 2 REAR COOLINGPLATE

-6054877BIWCK308 4272

6039T52P03MRS08322 STAGE 2 FWD COOLINGPLATE

5204877GATT7755 5397

6039T53P04MRS08322 STAGE 1 FWD COOLINGPLATE

-6244877MA00020 4253

6043T62P02MRS08322 STAGE 1 TURBINE DISK -9804877GATV3827 3897

6043T63P01MRS08322 STAGE 2 TURBINE DISK -9804877GATV5257 3897




HRS TOREPLACE

MODEL: UH-60A 7822971

Sub Component Listing for 714 Engines

AIRCRAFT SERIAL NO:

NUMBERLOCATIONPIDENTRYORGANIZATION

8.7.DATE

6.REMARKS

4. 5.

UH-60A 7822971HELICOPTER, UTILITY2. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER1. AIRCRAFT MODEL

Report Date: Page 1 of 3905-May-2016

AVIATION OFFICEAIRCRAFT M/R HEAD RIGGED INACCORDANCE WITH SA DWG 70400-0003 REV.B. SYSTEM CONTROLS HAVE BEEN BIASED INACCORD: A. LAT CONTROL SERVO INPUTROD P/N 70400-02258-046 HAS BEENSHORTENED 1/4 TURN. B. AFT CONT SERVOINPUT ROD PART NO. 70400-02258-045 HASBEEN LENGTHENED 1/2 TURN. C. FORWARDCONTROL SERVO INPUT ROD P/N 70400-02258-047 HAS BEEN SHORTENED 1/2 TURN. NOTE:WHEN A/C RIGGING IS BIASED RIGGING PINHOLES ARE TEMPORARILY LOST AT THEABOVE 3 POINTS. S/G. NATTAN

18-Oct-1979 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICEONE-TIME INSPECTION OF UH-60ABLACKHAWK AIRCRAFT TAILROTOR SERVOHYDRAULIC LINES. C/WS/ILLEGIBLE SSG

11-Nov-1979 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICEMSSG. UH-60A-79-1, ONE-TIME INSPECTIONOF UH-60A BLACKHAWK AIRCRAFT LOST THEABOVE 3 POINTS. C/W S/J. LEESON

20-Nov-1979 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETWX P R 061950Z DEC 79 (MSSG NO. UH-60A-79-2), ONE TIME INSPECTION OF INLET ANTI-ICING VALVE. C/W S/ E. SNYDER DAC

11-Dec-1979 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF P R 142015Z DEC 79 (MSSG NO. UH-60A-79-4), ONE TIME INSPECTION OF PEDALADJUSTER BEARING ATTACH BOLTS. C/WS/E. SNYDER DAC

02-Jan-1980 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF P R 142225Z DEC 79 (MSSG NO. UH-60A-79-6), ONE TIME INSPECTION OFSWASHPLATE LINKAGE PUSH ROD. C/WS/E. SNYDER DAC

04-Jan-1980 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF P R 021511, JAN 80 (MSSG NO. UH-60A-79-8), ONE TIME INSPECTION OF TAILROTORSERVO RETURN LINE. C/W S/E.SNYDER DAC

08-Jan-1980 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETWX 052205Z, MAR 80 (UH-60A-80-10), ONE-TIME INSPECTION FOR LIFE LIMITED SPINDLEASSY. C/W S/E. SNYDER DAC

06-Mar-1980 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETWX 241600A, APR 80 (UH-60A-80-18), ONE-TIME INSPECTION FOR SPECIFIC S/N SPINDLEASSEMBLIES. C/W S/E. SNYDER DAC

25-Apr-1980 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETWX 222210Z, APR 80 (UH-60A-80-17), SOFONE-TIME INSP. OF TRANSMISSION HOUSINGFLIGHT CONTROL DOWEL PINS. C/W BYSIKORSKI TEAM S/E. SNYDER DAC

26-Apr-1980 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETWX MSG P 131750Z, MAY 80 (UH-60A-80-22),SOF ONE-INSPECTION OF MAIN ROTOR HEADUPPER PRESSURE PLATE BOLT HOLES. C/WS/E. SNYDER DA

20-May-1980 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETWX MSG P 162045Z MAY 80 (UH-60A-80-24),SOF ONE- INSPECTION OF MAIN LANDINGGEAR DRAG BEAM AND AXEL. C/WS/E. SNYDER DAC

31-May-1980 1

FT. EUSTIS, VA.

AV4588

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.



AVIATION OFFICEUH-60A-80-29, REINSPECTION OFTRANSMISSION HOUSING FLIGHT CONTROLDOWEL PINS BY SIKORSKI ACFT. CO. FIELDTEAM. C/W S/O. KING

09-Jul-1980 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETB 55-1520-237-20-8, UH-60A-80-31, ONE-TIMEINSPECTION OF HIGH PRESSURE REFUELINGRECEPTICAL BOLTS. C/W S/E. SNYDERDAC

06-Aug-1980 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETB 55-1520-237-20-9, ONE-TIME INSPECTIONOF DAMPER INBOARD BOLTS. C/W S/E.SNYDER DAC

15-Oct-1980 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETB 55-1520-237-20-2, ONE-TIME INSPECTIONOF RIGHT HAND RELAY PANNEL. C/WS/E. SNYDER DAC

31-Oct-1980 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETB 55-1520-237-20-10, SOF P 031500Z NOV 80,UH-60A-80-32, ONETIME INSPECTION OF FUELSHUT OFF VALVES. C/W S/E. SNYDERDAC

06-Nov-1980 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETB 55-1520-237-20-11, SOF P 02010Z, NOV 80,UH-60 80-39, ONE-TIME INSPECTION OF INPUTMODULE FREE WHEELING NUT. C/WS/E. SNYDER DAC

18-Dec-1980 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETB 55-1520-237-20-12, ONE-TIME INSP OFTROOP CARGO DOOR. C/WS/ILLEGIBLE

15-Apr-1981 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETB 55-1520-237-20-16, ONE-TIME INSP OF FAN.C/W S/ILLEGIBLE

15-Apr-1981 2

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETB 55-1520-237-20-21, ONE-TIME INSPECTIONOF GEARBOX MAIN MODULE OUTER SHAFT,P/N 60351-08115-102. C/W S/W.WILLIAMSON, TI

03-Jul-1981 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETB 55-1520-237-20-20, ONE-TIME INSP OFSWASHLATE ASSY. C/W S/ILLEGIBLE

08-Jul-1981 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETB 55-1520-237-20-24, ONE-TIME INSPECTIONOF MAIN ROTOR BLADE TIP CAP FOR CRACK.C/WS/W. WILLIAMSON, TI

12-Aug-1981 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETB 55-1520-237-20-25, ONE-TIME INSPECTIONOF ENGINE OUTPUT DRIVE SHAFT. C/WS/ILLEGIBLE

06-Oct-1981 1

FT. EUSTIS, VA.

AV4588

BLACK HAWK MODTEAM

MOD 99-063, UPDATE OF CABIN CELINGPANEL COMPLETE. S/ILLEGIBLE

28-Apr-1982 1

FT. CAMPBELL, KY.

AV4588

BLACK HAWK MODTEAM

MOD 99-120, UPDATE OF OIL COOLER FANASSY COMPLETED. S/ILLEGIBLE

28-Apr-1982 2

FT CAMPBELL, KY.

AV4588

BLACK HAWK MODTEAM

MOD 99-122, UPDATE OF STABILATOR ID PLTCOMPLETED. S/ILLEGIBLE

28-Apr-1982 3

FT CAMPBELL, KY.

AV4588

BLACK HAWK MODTEAM

MOD 99-122-1, UPDATE OF STABILATORWIRING HARNESS COMPETED.S/ILLEGIBLE

28-Apr-1982 4

FT CAMPBELL, KY.

AV4588



8.7.DATE

6.REMARKS

4. 5.



BLACK HAWK MODTEAM

MOD 99-122-2, UPDATE OF CREW DOORRUBBER GROUNDING SEALS COMPLETED.S/ILLEGIBLE

28-Apr-1982 5

FT CAMPBELL, KY.

AV4588

BLACK HAWK MODTEAM

MOD 99-122-3, UPDATE OF CREW DOORMETAL GROUNDING SEALS COMPLETED.S/ILLEGIBLE

28-Apr-1982 6

FT CAMPBELL, KY.

AV4588

BLACK HAWK MODTEAM

MOD 99-125, UPDATE OF THE CARGO DOORSOUND PROOFING COMPLETED.S/ILLEGIBLE

28-Apr-1982 7

FT. CAMPBELL, KY.

AV4588

BLACK HAWK MODTEAM

MOD 99-126, UPDATE OF FUEL SUMP DOORSCOMPLETED. S/ILLEGIBLE

28-Apr-1982 8

FT. CAMPBELL, KY.

AV4588

BLACK HAWK MODTEAM

MOD 99-127, UPDATE OF MAIN ROTOR HEADBOLTS COMPLETED. S/ILLEGIBLE

28-Apr-1982 9

FT. CAMPBELL, KY.

AV4588

BLACK HAWK MODTEAM

MOD 99-127-1, UPDATE OF MAIN ROTORSWASHPLATE BUSHINGS COMPLETED.S/ILLEGIBLE

28-Apr-1982 10

FT. CAMPBELL, KY.

AV4588

BLACK HAWK MODTEAM

MOD 99-127-2, UPDATE OF MAIN ROTOR HEADBUSHINGS COMPLETED. S/ILLEGIBLE

28-Apr-1982 11

FT. CAMPBELL, KY.

AV4588

BLACK HAWK MODTEAM

MOD 99-130-6, INSTALLATION OF THE UPPERDECK RUBBER BOOT COMPLETED.S/ILLEGIBLE

28-Apr-1982 12

FT. CAMPBELL, KY.

AV4588

BLACK HAWK MODTEAM

TWX # UH-60A-82-6, ONE-TIME INSP OFPILOTS/CO-PILOTS SHOULDER HARNESSRUBBING BAR FOR PROPER INSTALLATIONCOMPLETED. S/R.M PAETH, SSG

04-May-1982 1

FT. CAMPBELL, KY.

AV4588

AVIATION OFFICETWX 290830Z, INSPECTION OF CABININTERIOR FOR LOOSE RIVITS. C/WS/E.SYNDER DAC

07-Jul-1982 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETROOP COMMANDERS CONTROL PANEL(C6533), TRANSFORMERS T501 AND T502,REWIRED TO ACCEPT FOUR ACFT. TYPEHEADSETS FOR STUDENT TRAINING. CHANGEON FILE IN Q.C. OFFICE. S/ILLEGIBLE

29-Jul-1982 1

FT. EUSIS, VA.

AV4588

AVIATION OFFICETB 55-2520-237-20-30, ONE-TIME INSPECTIONOF MAIN ROTOR SERVO PRESSURE SWITCHMANIFOLD SCREWS. C/W S/E. SNYDERDAC

10-Aug-1982 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 150025Z, ONE-TIME INSPECTION OFMAIN ROTOR PRIMARY SERVO LINKBEARINGS. C/WS/E. SNYDER DAC

17-Aug-1982 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 091500Z, TB 55-1520-237-20-31),INSPECTION OF TAILROTOR SERVO LINK.C/W S/E.SNYDER DAC

16-Sep-1982 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 222135Z TB 55-1520-237-20-34), ONE-TIME INSPECTION OF CONTROL LIMITERBEARINGS. C/WS/E.SNYDER DAC

27-Sep-1982 1

FT. EUSTIS, VA.

AV4588



8.7.DATE

6.REMARKS

4. 5.



AVIATION OFFICESOF MSG 2214302, TB 55-1520-237-20-35), ONE-TIME INSPECTION OF YAW TRIM AND ROLLTRIM SERVO FOR IMPROVED SEAL. C/WS/D. DOVER SSG

28-Oct-1982 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 101440Z, TB 55-1520-237-20-35), ONE-TIME INSPECTION OF DRAGBEAM AXELASSY. C/W S/D. DOVER SSG

17-Nov-1982 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 211930Z, TB 55-1520-237-20-37), ONE-TIME INSPECTION OF CARGO DOOR TRACK.C/WS/E. SNYDER DAC

22-Dec-1982 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 131430Z, TB 55-1520-237-20-40), ONE-TIME INSPECTION OF FLIGHT CONTROLDIRECTIONAL CONTROL LEVER. C/W S/E.SNYDER DAC

04-Mar-1983 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 081600Z, TB 55-1520-237-30-1), ONE-TIME INSPECTION OF INLET DUCTASSEMBLIES. C/WS/E. SNYDER DAC

27-Apr-1983 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 061530, ONE-TIME INSPECTION OFSTABELATOR ACTUATOR. C/W S/E.SNYDER DAC

13-Oct-1983 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICEOCM/ACE PERFORMED AT 0731.0 AIRCRAFTHRS. S/SCOTT KIK

18-Oct-1983 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 141900, TB 55-1520-237-20-44, ONE-TIME INSPECTION OF COLLECTIVE BIAS TUBEWASHER. C/WS/E. SNYDER

20-Oct-1983 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 042100Z, TB 55-1520-237-20-45, ONE-TIME INSPECTION OF TAILROTOR SERVO.C/WS/E. SNYDER

09-Nov-1983 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 042100Z, TB 55-1520-237-20-46, ONE-TIME INSPECTION OF TAILROTOR SERVO.C/W S/E. SNYDER

06-Dec-1983 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 221600Z, INSP. OF ACCESSORYMODULE OIL RETURN LINE SCREEN. C/WS/E.SNYDER

20-Dec-1983 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 192015Z, TB 55-1520-237-50-1 ONE-TIME INSPECTION OF MAIN ROTOR SHAFT.C/WS/E. SNYDER DAC

24-Jan-1984 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 161430Z, TB 55-1520-237-48, ONE-TIME INSP. OF FEEDER HARNESS BETWEEN#1 & #2 JUNCTION BOXES. C/WS/E. SNYDERDAC

22-Mar-1984 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 042115Z, ONE-TIME INSP. OFTAILROTOR PYLON COVER BRACKET.C/WS/E. SNYDER DAC

11-Apr-1984 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG TWX P 101D930Z, ONE-TIME INSP.OF STABILATOR AMPLIFIER. C/WS/E.SNYDER DAC

12-Apr-1984 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG TWX P 231700Z, ONE-TIME INSP. OFT/R AND INTERIM BEARBOX OIL LEVEL.C/WS/D. DOVER SSG

01-May-1984 1

FT. EUSTIS, VA.

AV4588



8.7.DATE

6.REMARKS

4. 5.



AVIATION OFFICESOF MSG TWX P 101600Z, INSPECTION OFENGINE OUTPUT SHAFT ASSY. C/WS/D.DOVER SSG

15-May-1984 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG TWX P 292000Z, ONE-TIMEINSPECTION OF CARTO HOOK CARTRIDGE.C/WS/ILLEGIBLE

05-Jun-1984 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF TWX 022100Z, INSPECTION OFLONGITUDINAL/LATERAL LINK ASSEMBLIESFOR CRACKED BEARING INNER RACE. C/WS/ILLEGIBLE

09-Jul-1984 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 0817452, INSP., STABILATORAMPLIFIERS FOR LOCKINGPOTENTIOMETERS. C/WS/L.NYREEN

13-Feb-1985 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 221700Z, REMOVAL OF RED TAPEON M/R TACHOMETER INDICATORS.C/WS/L.NYREEN SSG

25-Feb-1985 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 2000282, INSP OF STAB AMPLIFIERSFOR S/N C/W # 1 STAB AMP, SER # P1581 #2STAB AMP SER # 43. C/WS/L. NYREEN, SSG

07-Mar-1985 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 211530Z, INSP OF PRIMARY SERVOS& CONTROL RODS. C/WS/L. NYREEN, SSG

22-Mar-1985 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 051200Z, IMMEDIATE GROUNDINGAND INSP OF FLIGHT CONTROLS.C/WS/ILLEGIBLE

08-Apr-1985 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 222000Z, ONE-TIME INSPECTION OFACFT. C/WS/J. VEGA SSG

25-Apr-1985 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-85-12, ONE-TIMEINSPECTION OF ENGINE TRUBINE CASEINGFOR CRACKS. C/WS/L. NYREEN SSG

06-May-1985 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICEPMS-2 #2 COMPLETED AT 982.9 ACFT HRSNEXT PMS-2 AT 1482.9 ACFT HRS.S/L.NYREEN, SSG

14-May-1985 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-85-13, ONE-TIMEINSPECTION AND MODIFIED FLYABLESTRAGE OF ACFT. C/WS/J. VEGA SSG

15-May-1985 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A 85-14, ONE-TIME RECORDSINSPECTION OF MAIN ROTOR SHAFT.S/L.NYREEN, SSG

03-Jun-1985 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A 85-15, ONE-TIME RECORDSINSPECTION OF MAIN ROTOR HUB. C/WS/F.NYREEN

03-Jun-1985 2

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-85-17, ENGINE OUTPUTSHAFT INSPECTION/VIBRATIONS ANDRECORDINGS. C/WS/J. VEGA SSG

01-Jul-1985 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-85-20, MAIN ROTORSPINDLE AND RETIREMENT LIFE CHANGE.C/WS/J. VEGA SSG

01-Jul-1985 2

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-85-21, MAIN ROTORSPINDLE AND TIE ROD RETIREMENT LIFECHANGE. C/WS/J. VEGA SSG

11-Jul-1985 1

FT. EUSTIS, VA.

AV4588



8.7.DATE

6.REMARKS

4. 5.



AVIATION OFFICESOF MSG UH-60A-85-22, RESTRICTIONS WITHENGINE VALVE ASSEMBLIES RESSURIZINGAND OVERSPEED UNIT ASSEMBLIES. C/WS/J.VEGA, SSG

16-Jul-1985 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A 85-23, ONE-TIMEINSPECTION OF TAIL ROTOR DRIVE SHAFTBEARING. FAFNIR BEARINGS INSTALLED.C/W S/L. NYREEN SSG

26-Jul-1985 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-85-18, REQUIREMENTS FORUNGROUNDING OF ACFT. C/W S/J.VEGA SSG

30-Jul-1985 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-85-24, INSPECTION OF TAILROTOR DRIVESHAFT HANGER BEARINGS.C/WS/J.VEGA, SSG

13-Sep-1985 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICEOCM/ACE PERFORMED AT 0983 AIRCRAFTHRS. S/ILLEGIBLE

23-Sep-1985 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-86-02, ONE-TIMEINSPECTION OF TAIL ROTOR DRIVE SHAFTNUTS. C/WS/M. SHAW MARK SSG

03-Mar-1986 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-86-03, REVISION TO ONE-TIME INSPECTION OF TAILROTOR DRIVESHAFT NUTS. C/WS/M. SHAW MARK SSG

03-Mar-1986 2

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-86-04, REVISION TO ONE-TIME INSPECTION AND DELETION OF -16ENTRIES ON TAIL ROTOR DRIVESHAFTBEARINGS. C/WS/M. SHAW MARK SSG

10-Mar-1986 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-86-06,STATILATOR/AUTOMATIC FLIGHT CONTROLSYSTEM CONTROL PANEL RETROFIT.S/J.VEGA SSG

30-Apr-1986 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-85-18, UNGROUNDINGREQUIREMENTS OF ACFT. C/WS/J.VEGA, SSG

07-May-1986 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-86-10, ONE-TIME STAKINGOF BEARING ON YAW LEVER ASSY.C/WS/J.VEGA, SSG

13-Jun-1986 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-86-12, LOCATION ANDCHANGE OUT OF LISTED S/N YAW ANDCOLLECTIVE BOOST SERVOS. C/WS/J.VEGA, SSG

31-Jul-1986 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-86-13, REMOVAL OF AN310-8 NUTS, NSN 3310-00-167-1289. C/WS/J.VEGA,SSG

31-Jul-1986 2

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-86-17, CONTRACTORINSPECTION OF TRANSMISSION OIL COOLERFAN SPLINES AND TAILROTOR DRIVESHAFT.C/W S/J.VEGA, SSG

22-Oct-1986 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-86-18, IMMEDIATERESTRICTION OF RAPPELLING OPERATORSALL UH-60A SERIES AIRCRAFT.S/J.VEGA, SSG

27-Oct-1986 1

FT. EUSTIS, VA.

AV4588



8.7.DATE

6.REMARKS

4. 5.



AVIATION OFFICESOF MSG UH-60A-85-20, FIELD INSP. OF THEFIRST THREE TAILROTOR DRIVESHAFTSPLINE COUPLINGS AND REMOVAL OFMATERIAL FROM UNDER CREW SEATS. C/WS/J. VEGA SSG

07-Nov-1986 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60A-86-21, ONE-TIME INSP OFCREW SEATS FOR LONGITUDINALMOVEMENT OF LOCKPIN (ARA SEAT)ADJUSTMENT. C/W S/J. VEGA SSG

04-Dec-1986 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETB 55-1520-237-20-82, CONTRACTOR INSP. OFTRANSMISSION OIL COOLER FAN SPLINES &TAILROTOR DRIVESHAFT. SOF UH-60A-86-22NO SHIMS ADDED. S/J. VEGA SSG

10-Dec-1986 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICEOCM/ACE PERFORMED AT 1038 AIRCRAFTHOURS. S/L.NYREEN SSG

12-Jan-1987 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG 1422022 (UH-60-85-05), ENGINE ECULOCKOUT CONDITION OPERATION. C/WS/R.ROGERS

06-Mar-1987 1

FT. EUSTIS, VA.

AV4588

NWASI DIV.SOF (UH-60-87-03), TB 55-1520-237-20-89, ONE-TIME AND RECURRING INSP. OF FIRST THREETAILROTOR DRIVESHAFT COUPLINGS. C/WS/R. ROGERS

14-Mar-1987 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF (UH-60-87-04), REVISION TO INSP. OFEYEBOLT P/N 7020902136-102. C/WS/J. VEGASSG

30-Mar-1987 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF (UH-60-87-05), AT AIRSPEEDS ABOVE 80KIAS ALL UH/EH-60 AIRCRAFT ARERESTRICTED TO A MINIMUM OF 3000 FEETAGL. S/ILLEGIBLE

13-Apr-1987 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF (UH-60-87-06), ONE-TIME ANDRECURRING INSP OF OIL COOLER SPLINE.C/WS/J. ALANIZ

12-May-1987 1

FT. EUSTIS, VA.

AV4588

AVN DIV MAINT.SOF MSG UH-60-87-07, ONE-TIME INSP OFTWO LONGITUDINAL LINK ASSY/ONELATERAL CLEVIS ASY FOR CRACKEDBEARING INNER RACE. C/W S/J. VEGASSG

21-May-1987 1

FT. EUSTIS, VA.

AV4588

AVN DIV MAINT.SOF (GEN 87-02), ONE-TIME INSP OF ALL TIMECHANGE COMPONENT/PART HISTORICALRECORDS TO IDENTIFY NONCONFORMINGPARTS WHICH DO NOT MEET STANDARDSERIALIZATION REQUIREMENTS. C/WS/JVEGA

08-Jul-1987 1

FT. EUSTIS, VA.

AV4588

AVN DIV MAINT.SOF MSG UH-60-37-08, ONE-TIME INSP OFMIDSECTION BELLCRANK ASSY. C/WS/J.VEGA SSG

08-Jul-1987 2

FT. EUSTIS, VA.

AV4588

AVN DIV MAINT.TB 55-1520-237-20-79, INSP ANDREPLACEMENT OF ENGINE DESWIRL DUCTCLAMPS P/N 12372-1568. C/WS/J. VEGA SSG

13-Jul-1987 1

FT. EUSTIS, VA.

AV4588

AVN DIV MAINT.SOF MSG UH-60A-87-09, REQUIREMENTS FORLIFTING OF RESTRICTIONS. C/WS/ILLEGIBLE

11-Aug-1987 1

FT. EUSTIS, VA.

AV4588



8.7.DATE

6.REMARKS

4. 5.



AVN DIV MAINT.SOF MSG UH-60A-87-10, ONE-TIMEINSPECTION OF INPUT FLANGE ASSY.C/WS/ILLEGIBLE

20-Oct-1987 1

FT. EUSTIS, VA.

AV4588

ACE TEAM MEMBEROCM/ACE PERFORMED AT 1128 AIRCRAFTHOURS.S/ILLEGIBLE

26-Oct-1987 1

FT. EUSTIS, VA.

AV4588

AVN DIV. FEVASOF MSG UH-87-12, ONE-TIME INSP FORDEFECTIVE T700 GE-700/701 ENGINE POWERTURBINE MODULE. C/W S/J. VEGA SSG

02-Dec-1987 1

FT. EUSTIS, VA.

AV4588

AVN DIV. FEVASOF MSG UH-60-88-01, TAILROTOR BLADE S/NINSP. C/WS/J. VEGA SSG

17-Feb-1988 1

FT. EUSTIS, VA.

AV4588

AVN DIV. FEVASOF MSG UH-60-88-01, TAILROTOR BLADE S/NINSPECTION C/WS/J. VEGA SSG

21-Feb-1988 1

FT. EUSTIS, VA.

AV4588

AVN DIV. FEVAUH-60-87XSOF-04, T/R BLADE S/NINSPECTION. C/WS/ILLEGIBLE

21-Mar-1988 1

FT. EUSTIS, VA.

AV4588

AVN DIV. FEVASOF MSG UH-60-88-02, ONE-TIME INSP OF T/RGEARBOX AND OUTPUT SHAFT.C/WS/ILLEGIBLE

24-Mar-1988 1

FT. EUSTIS, VA.

AV4588

AVN DIV. FEVASOF MSG UH-60-88-03, LIFE EXTENSION OFTHE UH-60 AIRCRAFT MAIN MODULE SHAFT.C/WS/A. VEGA SSG

17-May-1988 1

FT. EUSTIS, VA.

AV4588

AVN DIV. MAINT.SOF MSG UH-60-88-04, INCREASE OF T/RGEARBOX OUTPUT SHAFT AS PRESCRIBEDIAW SOF UH-60A-88-04. C/WS/ILLEGIBLE

10-Jun-1988 1

FT. EUSTIS, VA.

AV4588

AVN DIV. FEVATB 55-1520-237-20-93, ONE-TIME ANDSUBSEQUENT CONDITIONAL INSP OF ENGINECOWLING LATCH ASSY.S/J. VEGA SSG

13-Jun-1988 1

FT. EUSTIS, VA.

AV4588

AVN DIV. MAINT.SOF MSG UH-60-88-05, TO ESTABLISH ANDMAINTAIN APU OPERATING HOURS ANDTOTAL START. C/WS/ILLEGIBLE

16-Jun-1988 1

FT. EUSTIS, VA.

AV4588

AVN DIV. FEVASOF MSG UH-60-88-06, OVERHAUL LIFE FORTRANSMISSION OIL COOLER BLOWER.C/WS/J. VEGA

12-Jul-1988 1

FT. EUSTIS, VA.

AV4588

AVN DIV. FEVA.SOF MSG UH-60-88-07, REVISION TO SOF MSGUH-60-88-05 CONCERNING OPERATINGTIME/START CALCULATIONS & FORMSINFORMATION. C/W S/J. VEGA SSG

19-Jul-1988 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60-88-08, REVISION TOOVERHAUL LIFE FOR THE TRANS. OILCOOLER BLOWER. C/WS/J. VEGA SSG

01-Aug-1988 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60-88-09, ONE-TIME INSP OF ARACREW SEATS FOR LOOSE CLEVISSCREWS.S/J. VEGA SSG

10-Aug-1988 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF MSG UH-60-88-02, ONE-TIME INSP OFPORTABLE FIRE EXTINGUISHERS. C/WS/J.VEGA SSG

22-Sep-1988 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF GEN UH-60-88-03, REVISION OF SOF GEN-88-02, INSP. OF CORRECT INTERNALPORTABLE FIRE EXTINGUISHER. C/WS/ILLEGIBLE

05-Oct-1988 1

FT. EUSTIS, VA.

AV4588



8.7.DATE

6.REMARKS

4. 5.



AVIATION DIV. FEVASOF GEN UH-60-88-10, ONE-TIME INSPECTIONOF TROOP/GUNNER SEAT AND THREE MANMEDEVAC SEAT UPPER SUPPORTINSTALLATION ASSEMBLIES.C/WS/ILLEGIBLE

02-Nov-1988 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF GEN UH-60-88-11, OPERATIONALREVISION TO UH-60-86-18, IMMEDIATERESTRICTION OF RAPPELLING OPERATION.C/W S/ILLEGIBLE

10-Nov-1988 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-88-12, REVISION TO UH-60-88-10,ONE-TIME INSPECTION OF TROOP/GUNNERSEAT AND THREE MAN MEDEVAC SEATUPPER SUPPORT INSTALLATIONASSEMBLIES. C/W S/ILLEGIBLE

15-Nov-1988 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-88-13, ONE-TIME INSPECTION OFTHE MAIN ROTOR BLADE EXPANDABLE PINP/N 70103-08107-101 FOR MISSINGSEGMENTS. C/W S/ILLEGIBLE

23-Nov-1988 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-88-14, ONE-TIME INSPECTION OFALL UH-60A HIGH PERFORMANCE HOISTSYSTEM, NOT INSTALLED IN ACFT. C/WS/ILLEGIBLE

08-Dec-1988 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVAOCM/ACE PERFORMED AT 1228 ACFT HRS.S/ILLEGIBLE

18-Jan-1989 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-89-01, ONE-TIME INSPECTION OFT700 ENGINE GAS GENERATOR STATORSHROUDS, SUSPECTED ENGINE INSTALLEDFURTHER INSP, REQUIRE AT 1229 ACFT HRS.C/W S/ILLEGIBLE

22-Feb-1989 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-89-02, CORRECTION OF SOFUH-60-89-91, ONE TIME INSP OF T700-GE-700 GASGENERATION STATOR. C/WS/ILLEGIBLE

22-Feb-1989 2

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-89-03, ONE-TIME INSPECTION OFALL MAIN ROTOR SPINDLES. ALL PARTNUMBERS C/W AT 1234 ACFT HRS.S/ILLEGIBLE

05-Apr-1989 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-89-04, REVISION ONE-TIMEINSPECTION OF ALL MAIN ROTOR SPINDLES.ALL PART NUMBERS C/W AT 1234 ACFT HRS.S/ILLEGIBLE

05-Apr-1989 2

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-89-05, ONE-TIME INSPECTION OFWIRE STRIKE PROTECTION SYSTEMCOMPLIED WITH AT 1242.1 ACFT HRS.S/ILLEGIBLE

22-Jun-1989 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-89-06, ONE-TIME INSPECTION OFRIGHT HAND RELAY PANEL ASSEMBLIES P/N70550-02102-050, -051, -054 FOR SUSPECTGROUNDING MODULES COMPLIED WITH AT1242.1 ACFT HRS. S/ILLEGIBLE

19-Jul-1989 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-89-07, REVISION TO RIGHT ANDLEFT HAND RELAY PANEL. C/WS/ILLEGIBLE

08-Aug-1989 1

FT. EUSTIS, VA.

AV4588



8.7.DATE

6.REMARKS

4. 5.



AVIATION DIV. FEVASOF UH-60-89-09, CORRECTION OFRETIREMENT LIFE SCHEDULE FOR UH-60ARETIREMENT LIFE COMPONENTS COMPLIEDWITH AT 1242.1 ACFT HRS.S/ILLEGIBLE

17-Aug-1989 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-89-10, ONE-TIME INSPECTION OFT700-GE-700 ENGINE GAS GENERATOR (GG)ROTOR AND STATOR. C/W AT 1242.1 ACFTHRS. S/ILLEGIBLE

22-Sep-1989 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-89-11, ONE-TIME INSPECTION OFOIL COOLER AXIAL FAN COMPLIED WITH AT1242.1 ACFT HRS.S/ILLEGIBLE

23-Oct-1989 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-89-08, ONE-TIME INSPECTION OFFUEL BOOST PUMP HOSE ATTACHMENTCOMPLIED WITH AT 1242.1 ACFT HRS. C/WS/ILLEGIBLE

25-Oct-1989 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVAOCM/ACE PERFORMED AT 1482.0 A/C HRS.S/ILLEGIBLE

26-Nov-1989 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-89-12, ONE-TIME INSPECTION OFOIL COOLER AXIAL FAN COMPLIED WITH AT1244.5 ACFT HRS.S/ILLEGIBLE

28-Nov-1989 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-89-13, ALL UH-60 SERIESAIRCRAFT, RESTRICTIONS AGAINST USINGFITTING ASSY P/N 70700-20433-045 FORRAPPELLING, PARACHUTING ANDTRANSPORTATIBILITY TIEDOWNOPERATIONS C/W AT 1244.5 ACFT HRS.S/ILLEGIBLE

05-Dec-1989 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-90-1, ONE-TIME AND RECURRINGINSPECTION OF MAIN ROTOR EXPANDABLEPINS COMPLIED WITH AT 1294.4 ACFT HRS.S/ILLEGIBLE

24-Apr-1990 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVATB 55-1520-237-20-113, ONE-TIME INSPECTIONFOR DEFECTIVE ROSEMOUNT JOEINDICATORS ON ALL H-60 AIRCRAFT. C/WS/J. PEREZ

05-Jul-1990 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVATB 55-1520-237-20-111, ONE-TIME INSPECTIONFOR UPPER PRESSURE PLATE AND SPINDLETO HUB ATTACHMENT BOLTS. C/WS/J. PEREZ

05-Jul-1990 2

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVASOF UH-60-92-02, ONE-TIME INSPECTION OFTAILROTOR PITCH BEAM RETAINING WASHERAND PITCH BEAM RETAINING NUT COMPLIEDWITH AT 1361.8 ACFT HRS. S/J. PEREZ

10-Aug-1990 1

FT. EUSTIS, VA.

AV4588

LSSI/OLRMWO 55-1520-237-50-39, INCORPORATION OFENGINE QUARANT SECONDARY STOP TO # 1AND # 2 ENGINE POWER CONTROL LEVERS.C/W S/F.G. BERNAL

06-Sep-1990 1

FT. EUSTUS, VA.

AV4588

ACD TEAM MEMBER (F)OCM/ACE PERFORMED AT 1403.0 AIRCRAFTHRS. S/ILLEGIBLE

12-Dec-1990 1

FT. EUSTIS, VA.

AV4588



8.7.DATE

6.REMARKS

4. 5.



AVM DIV FEVATB 55-1520-237-20-119, ONE-TIMEREPLACEMENT AND 30 HOUR SPECIALINSPECTION OF THE TAILROTOR PITCH BEAMRETAINING WASHER NO LATER THAN 12 MAR91 COMPLETED. S/J. PEREZ

17-Dec-1990 1

FT. EUSTIS, VA.

AV4588

AVM DIV FEVATB 55-1520-237-20-120, ALL UH-60 SERIESAIRCRAFT INVOLVED IN OPERATION DESERTSHIELD RECURRING INSPECTION OF MAINROTOR BLADE TIP. S/J. PEREZ

17-Dec-1990 2

FT. EUSTIS, VA.

AV4588

LSSI/OLR FEVAMWO 55-1520-237-50-54, INCORPORATION OFSTABILATOR ACTUATOR GROUNDING STRAPC/W AT 1412.6 ACFT HRS. S/F. BERNAL

08-Jan-1991 1

FT. EUSTIS, VA.

AV4588

AVN DIV FEVATB 1-1500-200-20-28, MAIN ROTOR BLADEEROSION TIP CAP BOOTS INSTALLED 20 DEC90 AT 1409.9 ACFT HRS. S/ J. PEREZ

09-Jan-1991 1

FT. EUSTIS, VA.

AV4588

AVN DIV FEVATB 1-1500-200-20-122, UH-60A SERIESAIRCRAFT, INSPECTION FORUNSERVICEABLE SPINDLE ASSEMBLIES. C/WS/ J. PEREZ

10-Feb-1991 1

FT. EUSTIS, VA.

AV4588

AVN DIV FEVATB 1-1500-200-20-124, ALL UH-60 SERIESAIRCRAFT, DUE TIME INSPECTION OF CARGOHOOK INTERNAL WIPE CUNDLE ROUTING IAWUH-60-91-ASAM-06. S/J. PEREZ

14-Mar-1991 1

FT. EUSTIS, VA.

AV4588

AVN DIV FEVATB 1-1500-200-20-125, ALL UH-60 SERIESAIRCRAFT, ONE TIME INSPECTION OF FIREEXTINGUISHING SYSTEM IAW UH-60-91-ASAM-08. C/W S/R. RIVERA JR. SGT

25-Mar-1991 1

FT. EUSTIS, VA.

AV4588

AVN DIV FEVATB 1-1500-200-20-126, ALL UH-60 SERIESAIRCRAFT, CHANGES TO INSPECTIONPROCEDURES FOR MAIN ROTORELASTOMERIC BEARING IAW UH-60-91-ASAM-09. C/W S/J. PEREZ

06-Jun-1991 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICETB 1-1520-237-20-127, ALL UH-60 SERIES, ONETIME INSPECTION OF MAIN LANDING GEARBRAKE ASSEMBLY PISTON INSULATOR, C/WAT 1482.8 ACFT HRS IAW UH-60 91-ASAM-10.S/ILLEGIBLE

12-Jul-1991 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVAPMS 2 THIRD PHASE COMPLETED AT 1482.8ACFT HRS, NEXT PMS-2 DUE AT 1982.8 ACFTHRS.S/J. PEREZ SSG

15-Aug-1991 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVAOCM/ACE PERFORMED AT 1524 ACFT HRSS/ILLEGIBLE

02-Dec-1991 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVATB 1-1520-231-20-129, UH-60 SERIESINSPECTION OF MAIN FOR THREEUNSERVICEABLE SPINDLE ASSEMBLY. C/WIAW UH-60-92-ASAM-01 AT 1428.9. S/J.PEREZ SSG

08-Jan-1992 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVATB 1-1520-231-20-132, ALL EVEN NUMBERED H-60 A/L SERIES ACFT ENGINE OUTPUT SHAFTBOLT TORQUE AND VIB CHECK N/A THISAIRCRAFT IAW UH-60-92-ASAM-02 AT 1599.7ACFT HRS. S/J. PEREZ SSG

15-May-1992 1

FT. EUSTIS, VA.

AV4588



8.7.DATE

6.REMARKS

4. 5.



AVIATION DIV. FEVATB 1-1520-231-20-130, ALL H-60 SERIESAIRCRAFT, INSPECTION AND REPLACEMENTOF MAIN ROTOR BLADE PINS C/W AT 1664.4ACFT HRS. IAW UH-60-92-ASAM-05. S/J.PEREZ SSG

21-Sep-1992 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVATB 1-1520-231-20-135, ALL H-60 SERIESAIRCRAFT, ONE-TIME OPERATIONAL CHECKOF THE TRANSMISSION AND GEARBOX CHIPDETECTOR SYSTEM, C/W AT 1682.0 ACFTHRS. IAW UH-60-63-ASAM-01. S/ILLEGIBLE

27-Oct-1992 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVATB 1-1520-231-20-135, ALL H-60 SERIESAIRCRAFT, REVISION TO UH-60-92-ASAM-06,C/W AT 1722.8 ACFT HRS. S/ILLEGIBLE

02-Dec-1992 1

FT. EUSTIS, VA.

AV4588

AVIATION DIV. FEVATB 1-1520-231-20-136, ALL H-60 SERIESAIRCRAFT, ONE-TIME INSPECTION TOREMOVE SUSPECT TAILROTOR PITCHBEAMS, C/W, AT 1736.6 ACFT HR.S/ILLEGIBLE

21-Dec-1992 1

FT. EUSTIS, VA.

AV4588

AVN DIV. FEVATB 1-1520-237-20-134, ALL H-60 SERIESAIRCRAFT, ONE-TIMEINSPECTION/REPLACEMENT FOR PROPERHARDWARE ON THE TAIL ROTOR PEDALADJUSTER ASSY, C/W AT 1736.0 ACFT HRS.S/ILLEGIBLE

06-Jan-1993 1

FT. EUSTIS, VA.

AV4588

AVN DIV. FEVATB 1-1520-237-20-138, ALL H-60 SERIESAIRCRAFT, BIAS OF TAIL ROTOR RIGGINGTHREE DEGREES, C/W AT 1736.6 ACFT HRS.S/ILLEGIBLE

06-Jan-1993 2

ST. LOUIS MO.

AV4588

AVN DIV. (HW POST)FEVA 23604

TB 1-1520-237-20-148, OPERATIONAL ALL H-60WITH ESSS AND ERFS MISSION KITSINSTALLED N/R, C/W AT 1794.0 IAW UH-60-93-ASAM-13. S/ILLEGIBLE

03-Apr-1993 1

FT. EUSTI VA.

AV4588


TB 1-1520-237-20-141, ONE TIME ANDRECURRING INSP. CLEANING OF ESSSVALVES AND PNEUMATIC LINES, NA AT 1776.1UH-60-93-ASAM-10. S/ILLEGIBLE

06-Apr-1993 1

FT. EUSTI VA.

AV4588


TB 1-1520-237-20-142, ONE TIME INSPECTIONOF CREW RESTRAINT SYSTEM, C/W AT 1776.1ACFT HRS, UH-60-ASAM-11.S/ILLEGIBLE

12-Apr-1993 1

FT. EUSTI VA.

AV4588


TB 1-1520-237-20-143, OPERATIONALMESSAGE FOR MAIN ROTOR TRACKVIBRATIONS C/W AT 1776.1 ACFT HRS IAW UH-60-93-ASAM-12. S/ILLEGIBLE

28-Apr-1993 1

FT. EUSTI VA.

AV4588


TB 1-1520-237-20-145, ACFT WITH ESSS &ERFS EJECTOR RACK INSP. N/R AT 1804.1ACFT HRS IAW PARA 8 UH-60-93-ASAM-14.S/ILLEGIBLE

17-Jun-1993 1

FT. EUSTI VA.

AV4588


TB 1-1520-237-20-146, ONE-TIME INSP OF THEHYD PUMP MOD KNURLED BLEED/RELIEFKNOB SECURING PIN, C/W AT 1842.7 ACFTHRS IAW UH-60-93-ASAM-16.S/ILLEGIBLE

29-Jul-1993 1

FT. EUSTI VA.

AV4588



8.7.DATE

6.REMARKS

4. 5.




TB 1-1520-237-20-139, NVG COMPATIBILITYREWORK OF MASTER WARNING PANE C/W AT1867.8 ACFT HRS IAW UH-60-94-ASAM-01.S/ILLEGIBLE

07-Dec-1993 1

FT. EUSTI VA.

AV4588


ACE/AACE PARFORMED 1887.0 AIRCRAFTHOURS. S/ILLEGIBLE

28-Dec-1993 1

FT. EUSTI VA.

AV4588

AVIATION OFFICESOF MSG 02171615Z, INSP. OF MAINGEARBOX DOWELL PINS. C/WS/L.NYREENSSG

04-Jan-1994 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF TWX 301515Z, INSPECTION OFTAILROTOR CABLES & CABLE TENSION CK.C/WS/D. F. NYREEN SSG

05-Jan-1994 1

FT. EUSTIS, VA.

AV4588


TB 1-1520-237-20-149, ONE-TIME INSP. OFBUCKLE/CROTCH STRAP ASSY C/W AT 1887.4ACFT HRS IAW UH-60-94-ASAM-02.S/ILLEGIBLE

12-Jan-1994 1

FT. EUSTI VA.

AV4588


ALL HISTORICAL ENTRIES AND TIMES FORREPLACEMENT OF MAIN ROTOR SPINDLESHAVE BEEN CHANGED TO REFLECT NEXTPMS-2 IAW TB 1-1520-237-20-15, UH60-94-ASAM-03 AT 1887.4 ACFT HRS.S/ILLEGIBLE

02-Feb-1994 1

FT. EUSTI VA.

AV4588


TB-1520-237-20-136, ONE-TIME INSP TOREMOVE SUSPECT TAILROTOR PITCH BEAMSC/W AT 1877.4 ACFT HRS S/ILLEGIBLE

03-Feb-1994 1

FT. EUSTI VA.

AV4588


TB-1520-237-20-154, CHANGE TO OVERHAULAND RETIREMENT TABLE C/WAT 1907.8 ACFTHRS IAW UH60-94-ASAM-07.S/ILLEGIBLE

07-Feb-1994 1

FT. EUSTI VA.

AV4588


TB-1520-237-20-152, ONE-TIME INSP TOREMOVE SUSPECT TAILROTOR GEARBOXOUTPUT SHAFTS C/W AT 1877.4 ACFT HRSIAW UH-60-94-ASAM-05. S/ILLEGIBLE

09-Feb-1994 1

FT. EUSTI VA.

AV4588


TB-1520-237-20-150, ONE-TIME INSP FORSTANDARDIZATION OF PILOTS AND CO-PILOTS SEAT RESTRAINT SYSTEM C/W AT1888.4ACFT HRS IAW UH-60-94-ASAM-06.S/ILLEGIBLE

09-Feb-1994 2

FT. EUSTI VA.

AV4588


TB 1-1520-237-20-155, REMOVAL OF CERTAINPRIMARYS SERVO ASSY C/W IAW UH-60-94-ASAM-07 AT 1920.2 ACFT HRS.S/ILLEGIBLE

05-Apr-1994 1

FT. EUSTI VA.

AV4588

AVIATION OFFICESOF TWX 301420, INSPECTION OF MAINROTOR SPINDLE ASSY PITCH CONTROL ARMATTACHING BOLTS. C/W S/D. DOVER SSG

01-Aug-1994 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICESOF TWX 0231620Z, INSPECTION OFTAILCONE HINGE BULKHEAD ROADIUSBLOCKS. C/WS/D. LEWIS SSG

29-Aug-1994 1

FT. EUSTIS, VA.

AV4588

AVIATION OFFICEOCM/ACE PERFORMED AT 895 AIRCRAFT.S/D. LEWIS SSG

26-Sep-1994 1

FT. EUSTIS, VA.

AV4588



8.7.DATE

6.REMARKS

4. 5.



USAAVNCMAIN ROTOR SPINDLE THRUST BEARINGSINSPECTION COMPLETED AT PMS 2INSPECTION, 1976.1 ACFT HRS, PER UH-60-94-ASAM-03. S/ILLEGIBLE

17-Oct-1994 1

FT. RUCKER, AL.

AV4588

AVIATION OFFICESOF TWX 0301500Z, INSPECTION OFTAILROTOR CONTROL CABLETURNBUCKLES. C/WS/D. LEWIS SSG

05-Nov-1994 1

FT. EUSTIS, VA.

AV4588

USAAVNCTB 1-1520-20-158, UH-60-95-ASAM-03, INSPFOR RESHIMMING OF T/R PIVOTS, COMPLIEDWITH.S/ILLEGIBLE

14-Nov-1994 1

FT. RUCKER, AL.

AV4588

USAAVNCTB 1-1520-237-20-160, UH-60-95-ASAM-04,REDUCTION OF TORQUE OF SELF RETAININGBOLT. C/WS/ILLEGIBLE

06-Jan-1995 1

FT. RUCKER, AL.

AV4588

USAAVNCUH-60A 500 HOUR PERIODIC INSPECTION PMS-2 COMPLIED WITH AT 1975.1 ACFT HOURS.S/ILLEGIBLE

13-Jan-1995 1

FT. RUCKER, AL.

AV4588

USAAVNCMAIN ROTOR SPINDLE THRUST BEARINGSINSPECTION COMPLETED AT PMS 2INSPECTION, 1976.1 ACFT HOUR PER UH-60-94-ASAM-03. S/ILLEGIBLE

13-Jan-1995 2

FT. RUCKER, AL.

AV4588

OCM SECTIONOCM/ACE PERFORMED AT 1976.0 AIRCRAFTHOURS. S/ILLEGIBLE

31-Jan-1995 1

ST. LOUIS, MO

AV4588

USAAVNCTB 1-1520-237-20-159, (UH-60-95-ASAM-02),REQUIREMENT TO OPERATE THE FUEL TANKSUBMERGED BOOST PUMPS, C/W.S/ILLEGIBLE

02-Feb-1995 1

FT. RUCKER, AL.

AV4588

USAAVNCTB 1-1520-237-20-163, UH-60-95-ASAM-05,INSPECTION AND CHANGE OF RETIREMENTLIFE OF SERVO BEAMS RAILS P/N 70209SERIES. C/W S/ILLEGIBLE

09-Feb-1995 1

FT. RUCKER, AL.

AV4588

USAAVNCTB 1-1520-237-20-161, UH-60-95-ASAM-05, INSPAND CHANGE TO RETIREMENT LIFE FORCERTAIN MAIN ROTOR BLADE CUFFS. C/WS/ILLEGIBLE

27-Feb-1995 1

FT. RUCKER, AL.

AV4588

USAAVNCTB 1-1520-237-20-153, REISSUE OF ONE-TIMEINSP. TO REMOVE SUSPECT TAILROTORPITCH CHANGE SHAFTS. C/WS/ILLEGIBLE

25-Mar-1995 1

FT. RUCKER, AL.

AV4588

USAAVNCTB 1-1520-237-20-168, ONE-TIME INSPECTIONFOR CRACKED MAIN XMSN BEAMS, UPPERDECK SKIN CRACKS, FRAME CRACKS ANDIMPLEMENTATION OF A 100 HOURRECURRING INSPECTION. C/WS/ILLEGIBLE

22-Jun-1995 1

FT. RUCKER, AL.

AV4588

USAAVNCTB 1-1520-237-20-166, ONE-TIME INSP. TOREMOVE SUSPECT TAILROTOR CHANGESHAFTS. C/WS/ILLEGIBLE

12-Jul-1995 1

FT. RUCKER, AL.

AV4588

USAAVNCTB 1-1520-237-20-169, NOTIFICATION TOSCHED. APPLICATION OF MWO 50-73.C/WS/ILLEGIBLE

12-Sep-1995 1

FT. RUCKER, AL.

AV4588

USAAVNCUH-60-95-ASAM-08, GAS GENERATORTURBINE ROTOR BLADE INFORMATION.C/WS/ILLEGIBLE

21-Sep-1995 1

FT. RUCKER, AL.

AV4588



8.7.DATE

6.REMARKS

4. 5.



USAAVNCTB 1-1520-237-20-164, (UH-60-95-ASAM-07),ONE-TIME INSP. OF TROOP/GUNNER SEATATTENUATION WIRE AND ROLLERS. C/WS/ILLEGIBLE

18-Oct-1995 1

FT. RUCKER, AL.

AV4588

USAAVNCACFT EQUIPPED WITH RT-158C/ARC-154 HAVEQUICK II USF/AM RADIO, AN AWR DTD 20 SEP95 RECEIVED AND PLACED IN LOGBOOKACFT HOURS 2085.6. S/ILLEGIBLE

31-Oct-1995 1

FT. RUCKER, AL.

AV4588

USAAVNCTB 1-1520-237-20-172, (UH-60-96-01), CHANGEIN RETIREMENT LIFE OF FWD BELLCRANKSUPPORT ASSY. C/W S/ILLEGIBLE

06-Nov-1995 1

FT. RUCKER, AL.

AV4588

USAAVNCTB 1-1520-237-20-171, (UH-60-95-ASAM-02),ONE-TIME INSP. FOR SUSPECT MAIN ROTORSHAFT NUT BOLTS, SUPERSEDED BY UH-60-96-ASAM-03. S/ILLEGIBLE

05-Jan-1996 1

FT. RUCKER, AL.

AV4588

USAAVNCOCM/ACE PERFORMED AT 2134.0 ACFTHOURS.S/ILLEGIBLE

05-Mar-1996 1

FT. RUCKER, AL.

AV4588

USAAVNCTB 1-1520-237-20-17, (UH-60-96-ASAM-03),REVISION TO ONE-TIME INSPECTION FORSUSPECT M/R SHAFT NUT BOLTS REQUIREDBY UH-60-96-ASAM-02. C/WS/ILLEGIBLE

20-May-1996 1

FT. RUCKER, AL.

AV4588

USAAVNCTB 1-1520-237-20-172, (UH-60-95-ASAM-05),CHANGE IN RETIREMENT LIFE OF FWDBELLCRANK ASSY TO 1800 HOURS. C/WS/ILLEGIBLE

12-Jul-1996 1

FT. RUCKER, AL.

AV4588

USAAVNCACFT TRANSFERRED TO CCAD, CORPUSCHRISTI, TXS/ILLEGIBLE

09-Sep-1996 1

FT. RUCKER, AL.

AV4588

CCAD NASUH-60-97-ASAM-14, TB 1-1520-237-20-195,INSPECTION BELLCRANK SUPPORT P/N 70400-08158-101, REPLACE ALL BELLCRANKS MFGBY AMERICAN GENERAL (1W160). C/WA. VACCA, ACFT RECDS CLK

26-Jan-1997 1

CORPC, TX.

AV4588

CCAD NASUH-60-97-ASAM-15, TB 1-1520-237-20-196,INSP. BRNG ROD END P/N: 70101-08202-101,REPLAE ALL BEARING MFB. BY ISLANDENGINEERING (40137). C/W A. VACCA,ACFT RECDS CLK

26-Jan-1997 2

CORPUS CHRISTI, TX

AV4588

CCAD NASUH-60-97-ASAM17, TB 1-1520-237-20-199INSPECTION OF ALL ACFT WITH INTERNALRESCUE HOIST BRACKET P/N 70800-02508-046FOR CRACKS IN ALUMINUM STRUCT. PLT70800-02508-108. C/W NOT INST ON A/CA.VACCA, ACFT RECDS CLK

26-Jan-1997 3

CORPUS CHRISTI, TX

AV4588

CCAD NASUH-60-98-ASAM-03, TB 1-1520-237-20-203,SWASHPLATE LINK, P/N 70400-08110-054,MANUFACTURED BY TEK CAGE CODE 65780.C/W A. VACCA, ACFT RECDS CLK

19-Oct-1997 1

CORPUS CHRISTI,TEXAS

AV4588

CCAD NASUH-60-98-ASAM-02, TB 1-1520-237-20-197,REMOVE AND DISPOSE ALL PUSHRODS P/N70400-08155-050/-051 MANUFACTURE BYVESGATILE MACHINING INC. (CODE 6S522).C/W A. VACCA ACFT REC CLK

19-Oct-1997 2

CORPUS CHRISTI, TX

AV4588



8.7.DATE

6.REMARKS

4. 5.



CCAD NASACFT COMPLETEDREFURBISHMENT/STANDARDIZATIONPROGRAM 22 DEC 97 BY CCAD AT 2368.1ACFT HRS IAW ATCOM SOW DTD 05 AUG 93AND PMS-2. A. VACCA, ACFT RECDSCLK

22-Dec-1997 1


AV4588

CCAD NASACFT COMPLETED PMS AT 2368.1 ACFT HRS,NEXT PMS-2 DUE AT 2868.1 ACFT HRS.A.VACCA, ACFT RECDS CLK

22-Dec-1997 2

CORPUS CHRISTI, TX.

AV4588

CCADACFT EXTERIOR PAINTED WITH LOWREFLECTIVE POLYURETHANE ACFT GREEN,MIL-C-46168 IAW TM 55-1500-345-23 DTD 12JUN 86, AND ECP # 0245. A. VACCA,ACFT RECDS CLK

22-Dec-1997 3


AV4588

CCAD NASACFT SIX-MONTHS FILE WILL BE RETAINEDAT CCAD, IAW TDS NO. AGEN-X0363, CH 1,DTD 13 JAN 84.A. VACCA, ACFT RECDS CLK

22-Dec-1997 4


AV4588

CCAD NASUH-60-96-ASAM-09, TB 1-1520-250-20-179,INSPECTION OF AIRCRAFT STABILATORACTUATOR CLEVISIS. C/W A. VACCA,ACFT RECS CLK

22-Dec-1997 5


AV4588

CCAD NASUH-60-97-ASAM-02, TB 1-1520-250-20-184, ONE-TIME INSPECTION OF TAIL DRIVE FLEXIBLECOUPLING CONNECTIONS. A. VACCA,ACFT RECS CLK

22-Dec-1997 6


AV4588

CCAD NASTB 1-1520-237-20-193, INCORPORATION OFCORROSION RESISTANCE ENHANCEMENTMODIFICATIONS IN CORROSION PRONEAREAS. C/W A. VACCA, ACFT RECDSCLK

22-Dec-1997 7

CORPC, TX.

AV4588

CCADUH-60-98-ASAM-01, TB 1-1520-237-20-202, M/RSHAFT EXTENSION ASSY P/N 70351-08186-043MFG BY FENN MFG CO. (CAGE CODE 82001)OR THE PURDY CORP (CAGE CODE 15152).C/W

22-Dec-1997 8

CORPUS CHRISTI, TX

AV4588

CCAD NASUH-60-97-ASAM-19, TB 1-1520-237-20-204, ONE-TIME INSP OF ANVIS/HUD POWER SUPPLY.C/WA. VACCA, ACFT RECDS CLK

14-Jan-1998 1

CORPUS CHRISTI, TX

AV4588

AASF#1UH-60-98-ASAM-05, TB 1-1520-237-20-203, ALLACFT WITH SWASHPLATE LINK P/N 70400-08110-054/061 MFG BY TEK (65780) C/W AT2379.0 ACFT HRS.

30-Apr-1998 1

TOPEKA, KS.

XT4634

AASF #1UH-60-98-ASAM-06, N/A THIS ACFT, C/W AT2379.0 ACFT HRS

15-May-1998 1

TOPEKA, KS

XT4634

AASF #1UH-60-98-ASAM-04, TB 1-1520-237-20-205,HUCK BOLTS INSP C/W AT 2379.0 ACFT HRS

17-Jun-1998 1

TOPEKA, KS

XT4634

24TH MED CO(A/A)/TFME, EAGLEBASE/TUZLA

UH-60-99-ASAM-10, #2 FUEL CROSSFEEDBREAKAWAY VALVE INSPECTION COMPLIEDWITH AT 2536.2 ACFT HRS

02-Aug-1998 1

APO AE 09789

DK5939

AASF #1UH-60-98-ASAM-07, TB 1-1520-237-20-206, INSPL/H TIE ROD FOR CERTAIN CAGE CODE C/WAT 2379.0 ACFT HRS

16-Sep-1998 1

TOPEKA, KS

XT4634



8.7.DATE

6.REMARKS

4. 5.



AASF #1UH-60-99-ASAM-01, TB 1-1520-237-20-208, INSPREQ FOR SWASHPLATE LINK C/WRS AT2388.4 ACFT HRS

03-Nov-1998 1

TOPEKA, KS

XT4634

AASF #1UH-60-99-ASAM-02, TB 1-1520-237-20-207, INSPACFT WITH EXTERNAL HOIST PROVISIONSC/W AT 2388.4 ACFT HRS

18-Nov-1998 1

TOPEKA, KS

XT4634

AASF #1UH-60-99-ASAM-03, TB 1-2840-248-20-22, INSPENG RECORDS FOR LCF1 AND ENG OP HRSC/W AT 2388.4 ACFT HRS

18-Nov-1998 2

TOPEKA, KS

XT4634

AASF #1UH-60-99-ASAM-04, N/A THIS ACFT-20-210 ONETIME INSP REQ FOR CERTAIN M/R PITCHHORNS BY SN# C/W AT 2388.4 ACFT HRS

03-Dec-1998 1

TOPEKA, KS

XT4634

AASF #1UH-60-99-ASAM-05, TB 1-1520-237-20-209, ONETIME INSP REQ OF THE SPINDLE BEARINGASSY FOR EXISTENCE OF THE SLEEVEBEARING C/W AT 2389.7 ACFT HRS

14-Dec-1998 1

TOPEKA, KS

XT4634

AASF #1UH-60-99-ASAM-06, TB 1-1520-237-20-210, ONETIME INSP REQ FOR CERTAIN M/R PITCHHORNS BY SN# C/W EXISTENCE OF THESLEEVE BEARING C/W AT 2389.7 ACFTHRS

15-Dec-1998 1

TOPEKA, KS

XT4634

DET 1 24TH MEDICALCOMPANY

AIRCRAFT TRANSFERRED TO PARENT UNIT24TH MEDICAL COMPANY WXFVAA, FOROCONUS DEPLOYMENT 10FEB99 2416.6 ACFTHOURS, CW4 JOHN ALEXANDER DET1 24THMED CO

10-Feb-1999 1

FOE

JA4282

DYNCORPUH-60-99-ASAM-07, INSPECTIONOF M/R HUBCOMPLIED WITH ON 20 MAR 99 C/W AT 2444.1ACFT HRS

20-Mar-1999 1

BOSNIA, APO AE 09789

EW2953

24TH MED CO(A/A)/TFME

UH-60-99-ASAM-08, VISUALLY INSPECT FWDBELLCRANK SUPPORT, PN: 70400-08162-XXX,COMPLIED WITH ON 15 JUN 99. C/W AT 2501.0ACFT HRS

15-Jun-1999 1

EAGLE BASE/TUZLAAPO AE 09789

MT9058

24TH MED CO.UH-60-99-ASAM-09, M/R BLADE EXPANDABLEPIN INSPECTION. C/W AT 2536.2 ACFT HRS

02-Aug-1999 1

TUZLA, BOSNIA

DK5939

24TH MED COUH-60-99-ASAM-09. M/R BLADE EXPANDABLEPIN INSPECTION. C/W AT 2536.2 ACFT HRS

02-Aug-1999 2

TUZLA, BOSNIA

DK5939

24TH MED COUH-60-99-ASAM-11, ONE TIME INSPECTION OFT700 ENGINE HISTORICAL RECORDS FROCERTAIN COMPONENTS, CHANGE FROMCONDITION ITEM TO TIME CHANGE ITEM.COMPLIED WITH AT 2537.5 ACFT HRSGEE207728, GEE306325

06-Aug-1999 1

EAGLE BASE, BOSNIA

DK5939

24TH MEDUH-60-99-ASAM-12, ONE TIME INSP OFHISTORICAL RECORDS TO INITIALIZE 250 HRINSP OF CERTAIN P/N HMU'S C/W AT 2539.8ACFT HRS

18-Aug-1999 1

BOSNIA

BS6483

AASF #1ACFT RETURNED FROM OCONUS OPERATIONIN BOSNIA REASSIGNED TO AASF #1 AS 24THMED DET C/W AT 2557.9 ACFT HRS

14-Oct-1999 1

TOPEKA, KS

XT4634

AASF #1UH-60-00-ASAM-01, TB 1-1520-237-20-215,INCREASE HUB NDI INSP TO 200 HRS C/W AT2565.8 ACFT HRS

18-Nov-1999 1

TOPEKA, KS

XT4634



8.7.DATE

6.REMARKS

4. 5.



AASF #1UH-60-00-ASAM-02 (TB1-1520-237-20-215), ONETIME INSP REQUIRED OF THE CYCLIC STICKFOR WIRE BUNDLE INTERFERENCE WITHSTICK MOVEMENT C/W AT 2573.2 ACFT HRS

08-Jan-2000 1

TOPEKA, KS

KJ1803

AASF #1UH-60-00-ASAM-03 (TB1-1520-237-20-217),INSPECTION ANS REMOVAL OF SUSPECT PRISERVO ASSYS BUNDLE INTERFERENCE C/WAT 2573.2 ACFT HRS

09-Jan-2000 1

TOPEKA, KS

XT4634

AASF #1AWR DTD 05FEB99 FOR ALL ELT C/W AT2575.5 ACFT HRS

20-Jan-2000 1

TOPEKA, KS

XT4634

AASF #1UH-60-00-ASAM-04, TB 1-1520-237-20-218,INSPECT TAIL LANDING GEAR SHOCK STRUTASSY FOR MISSING BEARING RETENTION PINC/W AT 2610.5 ACFT HRS

24-Feb-2000 1

TOPEKA, KS

AK7274

AASF #1UH-60-00-ASAM-05, TB 1-1520-237-20-219,INSPECTION OF FIRE EXTINGUISHER WIRINGC/W AT 2654.6 ACFT HRS

19-May-2000 1

TOPEKA, KS

JM4376

AASF #1UH-60-00-SOF-01, TB1-1520-237-20-221, ONETIME AND REOCCURRING INSP OF M/RSPINDLE LUGS C/W AT 2693.2 ACFT HRS

12-Jul-2000 1

TOPEKA, KS

XT4634

AASF #1UH-60-00-SOF-02, TB1-1520-237-20-222, INSPINPUT MODULE FOR SUSPECT BEVEL GEARC/W AT 2706.7 ACFT HRS

03-Aug-2000 1

TOPEKA, KS

XM4376

AASF #1UH-60-00-ASAM-06, CHANGE TO TB 1-1520-237-20-219, ACCOMPLISHED ON ASAM 05 N/ATHIS ACFT

02-Sep-2000 1

TOPEKA, KS

XM4376

AASF #1UH-60-00-ASAM-06 CHANGE TO TB1-1520-237-20-219, ACCOMPLISHED ON ASAM 05 N/A THISACFT

21-Sep-2000 1

TOPEKA, KS

XM4376

AASF #1UH60-SOF-01-03 TB1-1520-237-20-229, INSPLATERAL SERVO BELLCRANK FRO CERTAINCAGE CODE 2846.6 ACFT HRS

06-Jan-2001 1

TOPEKA, KS

JM4376

AASF #1UH-60-SOF-01-04 (TB1-1520-237-20-228)INSPECT FOR INSTALLATION OF THE FUELMONITORING SYSTEM ACFT HRS 2846.6 N/ATHIS ACFT

06-Jan-2001 2

TOPEKA, KS

JM4376

AASF #1UH-60-SOF-01-01 TB 1-1520-237-20-225 MAINLANDING GEAR DRAG BEAM INSPCOMPLETED AT 2840.9 ACFT HRS (SEE SOF-01-02)01-02)

28-Feb-2001 1

TOPEKA, KS

XT4634

AASF #1UH-60-SOF-01-06 TB1-1520-237-20-231 INSPSAS ASSY FOR SAFETY CABLE COMP ATACFT HRS 2868.1

11-Apr-2001 1

TOPEKA, KS

XM4376

AASF #1UH-60-SOF-01-05 TB1-1520-237-20-237 INSPM/R SPINDLE LUGS COMP. AT 2868.1 ACFTHRS

04-May-2001 1

TOPEKA, KS

XM4376

AASF #1PMS-2 #6 COMPLETED AT 2868.1 ACFT HRSNEXT PMS-2 DUE AT 3368.1 ACFT HRS

05-Jun-2001 1

TOPEKA, KS

XJ1803



8.7.DATE

6.REMARKS

4. 5.



AASF #1L LIFEPACK 10-59PMI NSN 6515-01-480-8614,AND LIFEPAK 10-62PMI, NSN 651501-481-0245,DEFIBRILLATOR/MONITOR, THE DNI-NEVADAPATIENT SIMULATOR, THEALARISMEDSYSTEM III INFUSION PUMP 2863BOR 2865B, THE B CI 3303 PULSE OXIMETER,THE IMPACT 754 VENTILATOR,IMPACTPORTABLE ASPIRATOR MODEL 325M, IMPACTPORTABLE SUCTION SYSTEM MODEL326/326M, UNITRON PORTABLE POWERSYSTEM, 60 HER

17-Jul-2001 1

TOPEKA, KS

XM4376

AASF #1ACFT RIGGING TOTALS LOW COLL. -2.5 AVG -.625 HIGH COLL 60.6 AVG 1513 FWRD CYCLIC34.1 AFT CYCLIC 19.8 LEFT CYCLIC 15.7 RIGHTCYCLIC 15.6 BIAS FWD FLATS AFT 4 FLATSLAT 2 FLATS

03-Aug-2001 1

TOPEKA, KS

XM4376

AASF #1UH-60-S0F-01-12 TB1-1520-237-20-236 ONETIME INSP TO DETERMINE AND ADJUST ASNECESSARY MAIN ROTOR BLADE PINTENSION COMP AT 2873.3 ACFT HRS

24-Aug-2001 1

TOPEKA, KS

XM4376

AASF #1TEMPORARY INSTALLATION OF APU INLETBARRIER FILTERS IAW AIRWORTHINESSRELEASE (AWR) FOR UH-60A/L HELICOPTERSEQUIPPED WITH AUXILIARY POWER UNIT(APU) INLET BARRIER FILTERS (AWR911)

07-Sep-2001 1

TOPEKA, KS

XM4376

24TH MED CO AASUCCESFUL COMPLETION AND EMC TESTIAW AIRWORTHINESS RELEASE (AWR) FORMEDEVAC UH-60A HELICOPTERS EQUIPPEDWITH THE PHYSIO CONTROL LIFEPACK 10-59MI NSN 6515-01-480-8614, AND LIFEPACK 10-62PMI, NSN 651501-481-0245,DEFIRILLATOR/MONITOR, THE DNI-NEVADAPATIENT SIMULATOR, THEALARISMEDSYSTEM III INFUSION PUMP 2863BOR2865B, THE BCI 3303 PULSE OXIMETER,THE IMPACT 754 VENTILATOR, IMPACTPORTABLE ASPIRATOR MODEL 325M, IMPACTPORTABLE SUCTION SYSTEM MODEL326/326M, UNITRON PORTABLE POWERSYSTEM, 60 HER

07-Sep-2001 2

CARIO WEST EGYPT

RH2906

AASF #1UH-60-02-SOF-03 ONE TIME INSP. OF PITCHTRIM ASSY. COMPLIED WITH

12-Dec-2001 1

TOPEKA, KS

XM4376

AASF #1GEN-02-ASAM-01 ALL AIRCRAFT ANDAVIATION HYDRAULIC GROUND UNITS,HYDRAULIC FLUID CONTAMINATIONCONTROL

02-Jan-2002 1

TOPEKA, KS

XM4376

AASF #1UH-60-S0F-02-04 TB1-1520-237-20-242INSPECTION OF APU FUEL LINE GROMMETCOMPLETED AT 2960.0 ACFT HRS

24-Jan-2002 1

TOPEKA, KS

XM4376

AASF #1UH-60-02-ASAM-02 TB1-1520-237-20-246INSPECTION OFTHE CONTROL ROD JAMNUTSC/W AT 2964.8 ACFT HRS

08-Feb-2002 1

TOPEKA, KS

MT4634



8.7.DATE

6.REMARKS

4. 5.



AASF #1UH-60-02-ASAM-03 TB1-1520-237-20-245INSPECT ENGINE CONTROL QUADRANTPOWER CONTROL (PCL WIRING IAW UH-60-02-ASAM-03 BEFORE COMPLETION OF NEXT PMS-2 NLT 15 FEB 2005 COMP AT ACFT HRS

12-Feb-2002 1

TOPEKA, KS

XM4376

AASF #1UH-60-02-ASAM-04TB1-1520-237-20-244INSPECT ALL RESTRAINT SYSTEMS COMP. AT2978.0 ACFT HRS

15-Mar-2002 1

TOPEKA, KS

XM4376

AASF #1UH-60-02-ASAM-06 (TB 1-1520-237-20-2520INSPECT SWAGE PIN/COLLARS ON BOOSTSERVO ASSEMBLIES COMPLETED AT ACFTXX01.5 ACFT HRS

26-Apr-2002 1

TOPEKA, KS

XJ1803

AASF #1UH-60-02-ASAM-07 . TORQUE FACTOR CHARTDISCREPANCY COMPLETED. COPY INSERTEDIN -10

29-Apr-2002 1

TOPEKA, KS

XM4376

AASF #1UH-60-02-SOF-08 TB1-1520-237-20-255 MAINMODULE PLANETARY CARRIER ASSEMBLYDETERMINE TSN OF MAIN G/B. ACFTRESTRICTED TO MEDEVAC AND COMBATMISSIONS ONLY. COMP. AT 3006.9 ACFT HRS

04-May-2002 1

TOPEKA, KS

XM4376

AASF #1UH-60-02-ASAM-08 (TB 1-1520-237-20-256)INSPECT AN/ARC-220 HF RADIO WIRING C/WAT 3039 ACFT HRS

13-Jun-2002 1

TOPEKA, KS

XJ1803

AASF #1UH-60-02-ASAM-09 (TB 1-1520-237-20-257)INSPECT TAIL ROTOR QUADRANTHARDWARE C/W AT 3058 ACFT HRS

13-Jun-2002 2

TOPEKA, KS

XJ1803

DYNCORP, KILLEEN, TX,AASF #1

ACE/CPCE PERFORMED AT 3072 ACFT HRSBY TEAM MEMBER K & W. AMCOM PROJECTOLR. KILLEEN, TX

06-Sep-2002 1

TOPEKA, KS 66619

JP2527

AASF #1REVISION TO UH-60-02-ASAM-08 TB1-1520-237-20-256 INSPECT AN/ARC-220 WIRING FROCHAFFING UH-60-02-ASAM-11 TB1-1520-237-20-261 COMP AT 3081.2 ACFT HRS

26-Sep-2002 1

TOPEKA, KS

XM4376

PROJECT OLRINSTALLATION OF THE 90 DEGREEBACKSHELL I/A/W UH-60-02-ASAM-11COMPLETED

06-Nov-2002 1

KILLEEN, TX

JC1523

AASF #1UH-60-03-ASAM-01 ONR TIME INSP OF FWDSUPPORT BRIDGES MANUFACTURED BY SACW/ SN A367-00001 THRU A367-00035 C/W AT2944 ACFT HRS

09-Dec-2002 1

TOPEKA, KS

XJ1803

AASF #1GEN-03-ASAM-01 ONE TIME INSP OF CY-8515BATTERY BOXES C/W AT 3132 ACFT HRS

03-Jan-2003 1

TOPEKA, KS

XJ1803

DYNCORP, KILLEEN, TX,AASF #1

ACE/CPCE PERFORMED AT 3072 ACFT HRSBY TEAM MEMBER K & I. AMCOM PROJECTOLR. KILLEEN, TX

04-Sep-2003 1

TOPEKA, KS 66619

JM4376

AASF #1SOF MSG UH-60-04-01 COMPLIED WITH20031008@ 3266.3 ACFT HRS

09-Oct-2003 1

TOPEKA, KS

XJ1803

AASF #1UH-60-04-ASAM-02 (TAIL ROTOR DRIVE SHAFTFLANGE NUT TQ CHECK) COMPLIED WITH AT3325.3 ACFT HRS

06-Apr-2004 1

TOPEKA, KS

JM4376



8.7.DATE

6.REMARKS

4. 5.



AASF #1UH-60-04-ASAM-03 (FUEL SYSTEM CHECKS)COMPLIED WITH 20040506 AT 3325 ACFT HRS.(PRESSURE CHECK PERFORMED)

06-May-2004 1

TOPEKA, KS. 66619

XJ1803

AASF #120040601-PMS-2 COMPLETED AT 3325.3 ACFTHRS. NEXT DUE 3825.3 HRS

01-Jun-2004 1

TOPEKA, KS

XJ1803

AASF #1UH-60-04-02 DISABLING OF COCKPIT AIRBAGSYSTEM N/A THIS ACFT. MWO NOT APPLIED

30-Jun-2004 1

TOPEKA, KS

XJ1803

AASF #1UH-60-04-03 H-60 SERIES AIRCRAFTCRASHWORTHY EXTERNAL FUEL SYSTEMFLIGHT OPERATIONS N/A THIS ACFT DOESNOT HAVE ESSS

30-Jun-2004 2

TOPEKA, KS

XJ1803

DYNCORP, KILLEEN, TX,AASF#1

ACE/CPCE PERFORMED AT 3072 ACFT HRSBY TEAM MEMBER K & W. AMCOM PROJECTOLR. KILLEEN, TX

13-Jul-2004 1

TOPEKA, KS

JP2527

AASF #1UH-60-04-04 MAIN ROTOR HUBSUBASSEMBLY REWORK C/W 12 AUG 04 AT3326 ACFT HRS

13-Aug-2004 1

TOPEKA, KS

XJ1803

AASF TOPEKA, KSUH-60-04-ASAM-05 RESTRAINT SYSTEMINSPECTION INPS NO DEFECTIVERESTRAINTS

21-Sep-2004 1

TOPEKA, KS

XJ1803

AASF #1UH-60-04-ASAM-05 ONE TIME INSPECTION OFSEAT BELTS COMPLETED AT 3339 ACFT HRS

28-Sep-2004 1

TOPEKA, KS. 66609

XJ1803

AASF TOPEKA, KANSASISAQ 110 DATED 06 FEB 04 INTERIMSTATEMENT OF AWR FOR UH-60A/LHELICOPTERS EQUIPPED WITH THEMATERIAL VALUE ENGINEERING (MAVEN)IMPORVED HEATING SYSTEM (OPTION II KIT)(ISAQ 110) INSTALLED ON ACFT AT 3344.7ACFT HRS

10-Oct-2004 1

TOPEKA, KANSAS

DC4707

C-CO TF SHADOWUH-60-ASAM-05-01 REVISION OF FUELSYSTEM INTEGRITY CHECKS

04-Jan-2005 1

CAMP BONDSTEEL,KOSOVO

DC4707

C-CO TF SHADOWUH-60-ASAM-05-03 H60 AIRCRAFT RESTRAINTSYSTEM COMPATIBILITY

05-Mar-2005 1


DC4707

C-CO TF SHADOWUH-60-05-ASAM-02 (FLUE FORCE TRACKER-BFT)

08-Mar-2005 1


DC4707

C-CO TF SHADOWUH-60-05-SOF-01 REACTIVATION OF COCKPITAIRBAG SYSTEM (CASS)

22-Mar-2005 1


DC4707

C-CO TF SHADOWUH-60-05-04 ALL H-60 SERIES HELICOPTERS,TAIL LANDING GEAR YOKE ASSEMBLY

06-Apr-2005 1


DC4707

C-CO TF SHADOWUH-60-05-ASAM-03 (H-60 AIRCRAFT, AIRCREWRESTRAINT SYSTEM COMPATIBILITY (INSPOK)

07-Apr-2005 1


DC4707



8.7.DATE

6.REMARKS

4. 5.



C-COMPANY TFSHADOW

UH-60-05-ASAM-04 ALL H-60 SERIESHELICOPTERS TAIL LANDING GEAR YOKEASSEMBLY COMPLTED INSP OK

07-Apr-2005 2


DC4707

C-CO TF SHADOWUH-60-05-ASAM-05 H-60 SERIESHELICOPTERS, TIE ROD ASSEMBLIES

20-Apr-2005 1


DC4707

C-CO TF SHADOWUH-60-05-ASAM-06, TROOP SEAT RESTRAINTBUCKLE

27-Apr-2005 1


DC4707

C-CO TF SHADOWUH-60-05-ASAM-07, ALL H-60 SERIESHELICOPTERS, AIR INTRUSION OFHYDRAULIC SYSTEM

27-Apr-2005 2


DC4707

C-CO TF SHADOWUH-60-05-SOF-02 AIRCRAFT PLACED ONILLEGIBLE 05/06/05 3452.1 ACFT HRS. PMI #1DUE X718.1 ACFT HRS

30-Apr-2005 1


DC4707

C-CO TF SHADOWEMC COMPLETED FOR ANVIS-6, CEP ONHGU56, LIFEPAK10 PROPAQ, & PORTABLESUCTION @ 3477.1 ACFT HRS

15-Jun-2005 1


SP5857

C-CO TF SHADOWUH-60-05-ASAM-09 COMPLIED WITH AT 3496.3ACFT HRS MWO NOT APPLIED

02-Aug-2005 1


PH1277

C-CO TF SHADOWUH-60-05-ASAM-10 ENGINE OUTPUT SHAFTINITIAL INSP COMPLIED WITH AT 3500 ACFTHOURS

09-Aug-2005 1


PH1277

D CO TASK FORCE,TALON

UH-60-06-SOF-01 MAIN ROTOR HUB ASSYC/W

07-Jan-2006 1


KJ7539

D CO TASK FORCETALON

UH-60-06-ASAM-01 TAIL SHOCK STRUT ASSYC/W

27-Mar-2006 1


BH7448

CO D, T F TALONUH-60-06-ASAM-02 INSPECTION COMPLIEDWITH. NO CORROSION FOUND. ACFT HASCAD PLATED STEEL NUTS ON P/C ASSYS.

02-May-2006 1

CAMP BONDSTEEL,APO AE 09340

SP1244

CO D, TASK FORCETALON

UH-60-06-ASAM-04, COCKPIT AIRBAG SYSTEM(CABS) ELECTRONIC CRASH SENSOR UNIT(ECSU) DRAIN PLUGS. MWO NOT INSTALLEDTHIS AIRCRAFT

24-Jun-2006 1


SP1244

TASK FORCE TALON,KFOR-7

UH-60-06-ASAM-05, BLUE FORCE TRACKERHARDWARE INSTALLATION. MWO NOTAPPLIED TO THIS AIRCRAFT/

22-Jul-2006 1


SP1244

D CO., TASK FORCETALON

PMI-1 COMPLETED AT 3727.8 ACFT HRS. PMI-2 DUE AT 4087.8 ACFT HRS.

26-Jul-2006 1


BH7448



8.7.DATE

6.REMARKS

4. 5.



D CO, TASK FORCETALON

UH-60-06-SOF-02, DISABLE COCKPIT AIRBAGSYSTEM N/A THIS ACFT. CABS MWO NOTAPPLIED.

06-Aug-2006 1

CAMP BONDSTEEL.APO AE 09340

SP1244

TASK FORCE TALONACFT PREPED FOR SHIPMENT TO CONUSTHIS DATE

02-Dec-2006 1

COLEMAN ARMYAIRFIELD

JB0151

AASF #1, FORBESFIELD

UH-60-07-ASAM-05 COMPLIED WITH. INTERIMCHANGES POSTED FOR ARC220/KY-100

23-Jan-2007 1

TOPEKA, KS

LF921636

AASF #1, FORBESFIELD

UH-60-07-ASAM-03 ONE TIME INSPECTION OFCOLLECTIVE/YAW BOOST SERVOS FORLOOSE OR MISSING ROLL PINS

23-Jan-2007 2

TOPEKA, KS

LF921636

AASF #1UH-60-07-ASAM-01 REROUTING OF WHITEENGINE/AIRFRAME HARNESS ASSEMBLYCOMPLIED WITH AT 3882.2 ACFT HRS

06-Mar-2007 1

TOPEKA, KS

LF921636

CCADAIRCRAFT RECEIVED & INDUCTED INTO THEUH-60 A TO A RECAPITALIZATION/REBUILD(RECAP) PROGRAM AT 4021.7 ACFT HRS,S.O.W. DTD 01 OCT 03 WITH CHANGE 8, & TM 1-1500-328-23, COMBAT OPERATIONS. ALLINSPECTION REQUIREMENTS SPECIFIED INTHE TM 1-1520-237-23, PMI-1, PMI-2, & PMDSHALL BE COMPLETED.

29-Feb-2008 1


OB967082

CCADAIRWORTHINESS RELEASE (AWR) FOR FMIMMUNE AN/ARN-147 VOR/ILS RECEIVERS P/N622-6376-020 IN THE STANDARDCONFIGURATION & FM IMMUNE AN/ARN-147VOR/ILS RECEIVERS P/N 622-6376-020 WITHTHE VIM-123 ADAPTER TRAY MOUNT INAN/ARN-123 CONFIGURED UH-60A/L, EH-60A,& CINC HAWK HELICOPTERS (AWR 917), DTD21 DEC 01 (R3).

29-Feb-2008 2


OB967082

CCADINTERIM STATEMENT OF AIRWORTHINESSQUALIFICATION (ISAQ) FOR ALL H-60 SERIESHELICOPTERS EQUIPPED WITH THEIMPROVED DRAG BEAM (ISAQ 120) DTD 15DEC 06 (R1).

29-Feb-2008 3


OB967082

CCADAIRWORTHINESS RELEASE (AWR) FOR UH-60A & EH-60A HELICOPTERS WITH MAINMODULE ASSEMBLIES (PART NUMBERS 70351-08100-075 & 70351-08100-076) EQUIPPEDWITH THE IMPROVED PLANETARY CARRIERASSEMBLY, PART NUMBER 70351-08175-046(AWR 1479), DTD 04 JAN 08.

29-Feb-2008 4


OB967082

CCADAIRWORTHINESS RELEASE (AWR) FOR UH-HH-60A/L HELICOPTERS EQUIPPED WITH THETECHNOLOGY RESEARCH CONSULTANTS,INC. (TRC) CN-1552B/A & CN-1564C/A MICRO-ELECTRO MECHANICAL SYSTEM (MEMS)RATE GYROSCOPES (AWR 1515), DTD 10 JUN08.

29-Feb-2008 5


OB967082



8.7.DATE

6.REMARKS

4. 5.



CCADUH-60-97-ASAM-15/TB 1-1520-237-20-196,INSPECTION FOR BEARING ROD END, P/N70101-08202-101, MANUFACTURED BY ISLANDENGINEERING, CAGE 40137.

11-Mar-2008 1


ZW1864

CCADUH-60-02-ASAM-03/TB 1-1520-237-20-245,INSPECTION OF ENGINE CONTROLQUADRANT POWER CONTROL LEVER (PCL)WIRING.

12-Jun-2008 1


KV4314

CCADTB 1-1520-237-20-218, ALL H-60 AIRCRAFT,INSPECT TAIL LANDING GEAR SHOCK STRUTASSEMBLY FOR MISSING BEARINGRETENTION PIN.

30-Jun-2008 1


MJ2066

CCADUH-60-05-ASAM-04, TAIL LANDING GEARYOKE ASSEMBLY.

30-Jun-2008 3


MJ2066

CCADUH-60-02-ASAM-06/TB 1-1520-237-20-252,COLLECTIVE & YAW BOOST SERVOASSEMBLIES SWAGE PIN COLLARS.

19-Jul-2008 1


RL0519

CCADUH-60-00-ASAM-07/TB 1-1520-237-20-224, ONETIME INSPECTION OF WIRE HARNESSESCONNECTING THE NO. 1 & NO. 2 JUNCTIONBOXES THAT HAVE BEEN REFURBISHED, ALLUH-60A AIRCRAFT, S/N: 77-22720 THRU 82-23746..

29-Jul-2008 2


OB967082

CCADTB 1-1520-237-20-231 (UH-60-02-SOF-03), ONETIME INSPECTION OF THE FLIGHT CONTROLSYSTEM, PITCH TRIM ASSEMBLY.

27-Aug-2008 1


RL0519

CCADUH-60-97-ASAM-05/TB 1-1520-237-23-3, ONETIME INSPECTION FOR REMOVAL & REWORKOF CERTAIN VISCOUS DAMPER BEARINGSUPPORT ASSEMBLIES.

29-Aug-2008 2


CR5847

CCADUH-60-04-ASAM-02, INSPECT TAIL ROTORDRIVESHAFT FLANGE NUTS.

29-Aug-2008 3


CR5847

CCADUH-60-02-SOF-04/TB 1-1520-237-20-242,INSPECTION OF APU FUEL LINE GROMMET.

08-Sep-2008 1


MJ2066

CCADH-60-08-AMAM-02, TAIL ROTOR OUTBOARDRETENTION PLATE SHIMS.

10-Sep-2008 1


CM6275

CCADH-60-08-ASAM-05, ALL H-60 SERIES, TAILROTOR QUADRANT SPRING CAPSULEASSEMBLY. C/W @ 4021.7 ACFT HRS.

10-Sep-2008 2


OB967082

CCADUH-60-06-ASAM-01, TAIL LANDING GEARSHOCK STRUT.

15-Sep-2008 1


MJ2066

CCADUH-60-96-ASAM-03/TB 1-1520-237-20-171, ONETIME INSPECTION OF M/R SHAFT NUT BOLTS.

18-Sep-2008 1


WH0217



8.7.DATE

6.REMARKS

4. 5.



CCADUH-60-97-ASAM-14/TB 1-1520-237-20-195,INSPECTION FOR BELLCRANK SUPPORT, P/N70400-08158-101, MANUFACTURE BYAMERICAN GENERAL, CAGE 1W160.

25-Sep-2008 1


AS1216

CCADUH-60-01-SOF-07, INSPECTION OF M/R FLIGHTCONTROL SELF-LOCKING BOLTS.

25-Sep-2008 2


AS1216

CCADUH-60-01-SOF-08/TB 1-1520-237-20-232,INSPECTION OF M/R FLIGHT CONTROL SELF-LOCKING BOLTS.

25-Sep-2008 3


AS1216

CCADH-60-08-ASAM-11, ALL H-60A SERIESAIRCRAFT, FLIGHT CONTROL INSPECTION.

25-Sep-2008 4


AS1216

CCADUH-60-06-ASAM-02, M/R RIGID CONNECTINGLINK/PITCH CONTROL ASSEMBLIES, ALL H-60SERIES AIRCRAFT.

29-Sep-2008 1


ZW1864

CCADH-60-08-ASAM-13, FIRE EXTINGUISHING TUBEUNION RING, ALL H-60 SERIES AIRCRAFT.

04-Oct-2008 1


OB967082

CCADUH-60-07-ASAM-03, YAW & COLLECTIVEBOOST SERVOS ROLL PIN.

07-Oct-2008 1


RL0519

CCADH-60-08-AMAM-04, ALL H-60 SERIESAIRCRAFT, COCKPIT DOOR JETTISONABLEWINDOWS. C/W @ 4021.7 ACFT HRS.

08-Oct-2008 1


OB967082

CCADH-60-08-ASAM-12, ALL H-60 SERIESAIRCRAFT, PARKER AEROSPACE AIRTURBINE STARTER (ATS). N/A THISAIRCRAFT.

09-Oct-2008 1


OB967082

CCADUH-60-05-ASAM-03, AIRCREW RESTRAINTSYSTEM COMPATIBILITY.

09-Oct-2008 2


OB967082

CCADH-60-08-AMAM-08, FLIGHT CONTROL RIGGINGUPDATE, ALL H-60 SERIES ACFT. INSPECTFOR LINK, P/N 70400-02270-048, & ACTUATOR,P/N 70400-02301-042.

09-Oct-2008 3


OB967082

CCADH-60-08-ASAM-10, ALL H-60 SERIESAIRCRAFT, ELECTRICAL WIRE CHAFE ISSUES.

09-Oct-2008 4


OB967082

CCADH-60-08-ASAM-06, MAIN ROTOR PYLONSLIDING FORWARD FAIRING. C/W @ 4021.7ACFT HRS.

09-Oct-2008 5


OB967082

CCADH-60-08-AMAM-07, AN/ASN=128B/D DOPPLERGPS NAVIGATION SET (DGNS).

09-Oct-2008 6


OB967082

CCADUH-60-07-ASAM-01, RE-ROUTING OF #1 & #2ENGINES, WHITE/AIRFRAME HARNESSASSEMBLIES.

10-Oct-2008 1


OB967082



8.7.DATE

6.REMARKS

4. 5.



CCADUH-60-07-ASAM-02, RE-ROUTING OF #1 & #2ENGINES, WHITE/AIRFRAME HARNESSASSEMBLIES.

10-Oct-2008 2


FD8493

CCADUH-60-05-ASAM-11, WIRING HARNESSCHAFFING.

10-Oct-2008 3


OB967082

CCADUH-60-07-AMAM-01, COMMON MISSILEWARNING SYSTEM (AN/AAR-57 SYSTEM). N/ATHIS ACFT.

19-Oct-2008 1


OB967082

CCADH-60-08-AMAM-06, COMMON MISSILEWARNING SYSTEM (CMWS). N/A TO THISACFT. C/W @ 4021.7 ACFT HRS.

19-Oct-2008 2


OB967082

CCADH-60-08-AMAM-05, ALL H-60/UH-1 AIRCRAFT,GOODRICH INTERNAL RESCUE HOISTS. N/ANO HOIST INSTALLED. C/W @ 4021.7 ACFTHRS.

21-Oct-2008 1


OB967082

CCADAIRCRAFT STRIPPED & PAINTED I/A/W TM 55-1500-345-23 DTD 12JUN89 UTILIZING THEAPPLICABLE PAINT, DECAL & STENCILWORKBOOK, CCAD FORM 110, PAINTSCHEME SHALL BE: EXTERIOR GREEN(CARC) MIL-DTL-53039 CREW COMPARTMENT,LUSTERLESS BLACK, (CARC) MIL-DTL-53039,TROOP CARGO AREA LUSTERLESS GRAY(CARC) MIL-DTL-53039.

22-Oct-2008 1


OB967082

CCADH-60-09-SOF-02, ALL H-60 & H-64 SERIESAIRCRAFT, AN/ALQ-144 INFRA-REDCOUNTERMEASURES SYSTEM (IRCMS). C/W@ 4021.7 ACFT HRS.

10-Nov-2008 1


LG981422

CCADUH-60-01-SOF-02/TB 1-1520-237-20-227, INITIAL& RECURRING INSPECTION OF THE MAINLANDING GEAR DRAG BEAM ASSEMBLY &DECREASE TORQUE ON THE JACK PAD NUT.

12-Nov-2008 1


OB967082

CCADH-60-08-AMAM-01, MAIN LANDING GEARSHOCK STRUTS SERVICING CHECK, ALL H-60SERIES AIRCRAFT.

12-Nov-2008 2


OB967082

CCADUH-60-07-ASAM-06, INTERNAL RESCUE HOISTCABLE DEFLECTOR. N/A THIS ACFT.

12-Nov-2008 3


OB967082

CCADH-60-08-ASAM-01, TROOP/GUNNER SEATSUPPER ENERGY ATTENUATING WIRESINSPECTION.

12-Nov-2008 4


OB967082

CCADUH-60-97-ASAM-08/TB 1-1520-237-20-187,AIRCRAFT WITH THE CONNECTING LINKASSEMBLY, P/N: 70400-08155-056, MFD BYPURDY MACHINE COMPANY, CAGE 15152.

12-Nov-2008 5


OB967082

CCADH-60-08-ASAM-02, POWER AVAILABLECONTROL CABLE.

12-Nov-2008 6


OB967082



8.7.DATE

6.REMARKS

4. 5.



CCADUH-60-04-ASAM-04, FUEL SYSTEM INTEGRITYCHECKS.

12-Nov-2008 7


OB967082

CCADUH-60-07-ASAM-07, INSTALLATION OF STATICBONDING JUMPERS ON CEFS FUEL HOSES.N/A THIS ACFT.

12-Nov-2008 8


OB967082

CCADH-60-08-ASAM-03, CHANGES TO CURRENTFUEL SYSTEM INTEGRITY CHECKS.

12-Nov-2008 9


OB967082

CCADH-60-08-ASAM-04, PILOT LOWER SEAT RAILCHAFING ELECTRICAL HARNESS. PCW

12-Nov-2008 10


OB967082

CCADECP 340, MODIFICATION OF OIL COOLERDUCT. (VENTED)

12-Nov-2008 11


OB967082

CCADAED 2298 (11 MAR 03) (TB 1-1520-237-20-193),INCORPORATION OF CORROSIONRESISTANCE ENHANCEMENT MODIFICATIONIN CORROSION PRONE AREAS.

12-Nov-2008 12


OB967082

CCADH-60-09-SOF-01, TECHNICAL, ALL H-60 & H-64SERIES AIRCRAFT, HYDRO-MECHANICALUNIT (HMU). C/W @ 4021.7 ACFT HRS.

14-Nov-2008 1


JB860690

CCADH-60-08-SOF-01, ALL H-60 SERIES AIRCRAFT,MAIN ROTOR BLADE EXPANDABLE PININSPECTION CHANGE. C/W @ 4021.7 ACFTHRS.

14-Nov-2008 2


JB860690

CCADH-60-09-SOF-03, TECHNICAL, ALL H-60 SERIESAIRCRAFT, POSSIBLE RETIREMENT LIFEOVER-FLIGHT. C/W @ 4021.7 ACFT HRS.

17-Nov-2008 1


LG981422

CCADAIRCRAFT COMPLETED PMI-1 AND PMI-2 AT4021.7 ACFT HRS. NEXT PHASE IS DUE AT4381.7 ACFT HRS.

03-Dec-2008 1


OB967082

CCADJACE/ACE INSPECTION COMPLETED AT4029.0 ACFT HRS BY CCAD, CORPUS CHRISTI,TEXAS 78419-5260.

03-Dec-2008 2


OB967082

CCADAIRCRAFT COMPLETED UH-60A TO ARECAPITALIZATION/REBUILD PROGRAMONTHIS AT 4029.0 ACFT HRS.

03-Dec-2008 3


OB967082

AASF, MDARNGACFT TRANSFERED TO C.CO. 2/224, MDARNG 20-Dec-2008 1

EDGEWOOD, MD

PM884815

AASF,MDARNGT/R RIG CK AT 4044.3 AIRCRAFT HRS BIASBLU P/C ROD 4.028 AFTER 4 TURNS 4.361 REDP/C ROD 4.732 AFTER 4 TURNS 5.069 BLK P/CROD 4.077 AFTER 4 TURNS 4.403 YEL P/C ROD4.702 AFTER 4 TURNS 5.045 DIFFERENCE BLU.333 RED .337 BLK .326 YEL .345 T/R CABLETENSION 155 BOTH SIDES @ 19.8 DEGREES.TS026891

14-Jan-2009 1

EDGEWOOD, MD

TS026891



8.7.DATE

6.REMARKS

4. 5.



AASF, MDARNGH-60-09-ASAM-01 (701 GG ROTOR) COMPLIEDWITH

29-Jan-2009 1

EDGEWOOD, MD

PM884815

AASF, MDARNGH-60-09-ASAM-05 ( UPDATE TO LIFE LIMITCHANGE FOR TAIL ROTOR QUADRANTSPRING CAPSULES ) COMPLIED WITH

10-Mar-2009 1

EDGEWOOD, MD

PM884815

DS2ACE COMPLETED AT 4099.3 A/C HRS BY ACETEAM MEMBERS G/BB. AMCOM-AFMD.

24-Mar-2009 1

EDGEWOOD, MD

JG389608

AASF, MDARNGH-60-09-ASAM-04 ( RESCUE HOIST MARK 44MOD 0 CARTRIDGE ACTIVATION DEVICE)COMPLIED WITH

26-Mar-2009 1

EDGEWOOD, MD

PM884815

AASF, MDARNGH-60-09-ASAM-06 ( ICS CORD RE-ROUTINGALL UH-60M ) COMPLIED WITH

26-Mar-2009 2

EDGEWOOD, MD

PM884815

AASF, MDARNGH-60-09-ASAM-07 (FIRE EXTINGUISHERWIRING) COMPLIED WITH

16-Apr-2009 1

EDGEWOOD, MD

TS026891

AASF,MDARNGH-60-09-ASAM-09 (FIRE EXTINGUISHERWIRING BREAKAWAY THREAD) COMPLIEDWITH.

27-May-2009 1

EDGEWOOD, MD

TS026891

AASF, MDARNGH-60-09-ASAM-08 (ENG. DOOR WT.RESTRICTION) COMPLIED WITH.

03-Jun-2009 1

EDGEWOOD, MD

TS026891

AASF, MDARNGH-60-09-ASAM-11(CARGO DOOR WINDOWEMERGENCY JETTISON HANDLE ASSY)COMPLIED WITH.

25-Jun-2009 1

EDGEWOOD, MD

TS026891

AASF MD-ARNGCOMPLIED WITH REQUIREEMNTS OF H-60-09-AMAM-04 (SEAT INTERFR WITH AIRBORNECOMMAND AND CONTROL SYSTEM (A2C2S)SYSTEM NOT INSTALLED

25-Aug-2009 1

EDGEWOOD, MD

ED703987

AASF MDARNGH-60-09-AMAM-06 (CARGO HOOK THRUSTERLIFE LIMIT CHANGE) COMPLIED WITH

28-Aug-2009 1

EDGEWOOD, MD

RH026085

AASF MDARNGH-60-09-AMAM-07 (HHFE) COMPLIED WITH 16-Sep-2009 1

EDGEWOOD, MD

RH026085

AASF MDARNGH-60-10-AMAM-04 COMPLIED WITH (SDCSOFTWARE VERIFICATION)

17-Nov-2009 1

EDGEWOOD, MD

ED703987

AASF MDARNGH-60-10-ASAM-03 COMPLIED WITH (FIREBOTTLE DISCHARGE LINE & NOZZLE)

17-Nov-2009 2

EDGEWOOD, MD

RH026085

AASF MDARNGFAST ROPE INSERTION/EXTRACTION SYSTEM(FRIES) INSTALLED I/A/W AWR 1477R2 DATED09JUN09.

24-Nov-2009 1

EDGEWOOD, MD

TS026891

AASF MDARNGH-60-10-ASAM-04 (SAS LINK INSP) COMPLIEDWITH.

23-Dec-2009 1

EDGEWOOD, MD

RH026085

AASF, MDARNGH-60-10-AMAM-05 (AMCOM CHG60B)COMPLIED WITH.

04-Feb-2010 1

EDGEWOOD, MD

DD824171

AASF, MDARNGGEN-10-AMAM-02 (TABLET PC) COMPLIEDWITH.

04-Feb-2010 2

EDGEWOOD, MD

DD824171

AASF, MDARNGH-60-10-AMAM-11 (OIL SAMPLING INTERVAL)COMPLIED WITH.

04-Feb-2010 3

EDGEWOOD, MD

DD824171



8.7.DATE

6.REMARKS

4. 5.



AASF MDARNGH-60-10-ASAM-06 (AUTO-IGNITION ANDTRANSIENT DROOP MODIFICATION)COMPLIED WITH.

16-Feb-2010 1

EDGEWOOD, MD

TS026891

CSCACE COMPLETED AT 4267.5 A/C HRS. BY ACETEAM MEMBERS B/G. AFMA RASM-E, AMCOM.

25-Mar-2010 1

EDGEWOOD, MD

JG389608

AASF, MDARNGH-60-10-ASAM-07 STABILATOR HINGE FITTINGCOMPLIED WITH.

27-Apr-2010 1

EDGEWOOD, MD

TS026891

AASF, MDARNGH-60-10-ASAM-08 APU BURNER DRAIN VALVECLEARANCE FROM LOWER FIRE WALLCOMPLIED WITH.

27-May-2010 1

EDGEWOOD, MD

TS026891

CSC FT HOOD AFMAPASSTHROUGH HOLE STA 443.5 BLL 30.75 WL249.82 INSTALL ON ACFT IAW MEC # F107097DTD 7 APR 10.APPLIED AT 4267.5 ACFT HRS.

28-May-2010 1

KILLEEN TX 76543

BS469665

CSC FT HOOD AFMASTA 379 BLL10 FORMER WARPED. REPAIREDIAW MEC F107844 DTD 22 APR 10. APPLIED AT4267.5 ACFT HRS.

28-May-2010 2

KILLEEN TX 76543

BS469665

CSC FT HOOD AFMAAIRWORTHINESS RELEASE FOR UH-60A/LHELICOPTERS EQUIPPED WITH THEELECTRONIC DATA MANGER(EDM) AND BLUEFORCE TRACKING (BFT) SYSTEM. AWR 1347DTD 5 0CT 09 R10. APPLIED AT 4267.5 ACFTHRS.

28-May-2010 3

KILLEEN TX 76543

BS469665

CSC FT HOOD AFMAAIRWORTHINESS RELEASE FORINSTALLATION AND OPERATION OF AIRWARRIOR BLOCK I ON UH-60 A/LHELICOPTERS. AWR 1453 DTD 4 MAR 10 R1.APPLIED AT 4267.5 ACFT HRS.

28-May-2010 4

KILLEEN TX 76543

BS469665

CSC FT HOOD AFMAAIRWORTHINESS RELEASE FOR UH/HH-60A/LHELICOPTERS WITH INTEGRATED VEHICLEHEALTH MANAGEMENT SYSTEM (IVHMS)HEALTH USAGE MANAGEMENT SYSTEM(HUMS) AWR 1346 DTD 30 MAR 10 R16.APPLIED AT 4267.5 ACFT HRS.

28-May-2010 5

KILLEEN TX 76543

BS469665

CSC FT HOOD AFMAINTERIM STATEMENT OF AIRWORTHINESSQUALIFICATION(ISAQ) FOR UH-60A/LHELICOPTERS EQUIPPED WITH APX-118COMMON TRANSPONDER (CXP) ISAQ 116 DTD22 NOV 06 R2. APPLIED AT 4267.5 ACFT HRS.

28-May-2010 6

KILLEEN TX 76543

BS469665

CSC FT HOOD AFMAAIRWORTHINESS RELEASE FOR ALL UH-60A/L/M AND HH-60A/L HELICOPTERSEQUIPPED WITH THE PROTECTIVEMATERIALS COMPANY BALLISTIC ARMORPROTECTION SYSTEM (BAPS) AWR 1524 DTD27 OCT 08 R1. APPLIED AT 4267.5 ACFT HRS.

28-May-2010 7

KILLEEN TX 76543

BS469665

CSC FT HOOD AFMAAIRWORTHINESS RELEASE FOR UH-60A/LAND HH-60A/L HELICOPTERS TO OPERATEWITH ENGINE INLET BARRIER FILTER (EIBF)INSTALLED. USING AUTOMATEDPERFORMANCE PLANNING SOFTWARE(PPC)IN SUPPORT OF DESERT COMBATOPERATIONS AWR 1270 DTD 13 NOV 09R6.APPLIED AT 4267.5 ACFT HRS.

28-May-2010 8

KILLEEN TX 76543

BS469665



8.7.DATE

6.REMARKS

4. 5.



CSC FT HOOD AFMAAIRWORTHINESS RELEASE FOR UH-60A/LHELICOPTERS EQUIPPED WITH THE COMMONMISSILE WARNING SYSTEM (CMWS) 5THSENSOR A AND B KIT. AWR 1494 DTD 20 AUG09 R4. APPLIED AT 4267.5 ACFT HRS.

28-May-2010 9

KILLEEN TX 76543

BS469665

CSC FT HOOD AFMAAIRWORTHINESS RELEASE FOR THEOPERATION OF COMMON MISSILE WARNINGSYSTEM (CMWS) IMPROVEDCOUNTERMEASURES DISPENSER (ICMD) ANDPRE-PLANNED PRODUCT IMPROVEMENT (P3I)ON UH-60A/L HELICOPTERS AWR 1425 DTD 30OCT 09 R12. APPLIED AT 4267.5 ACFT HRS.

28-May-2010 10

KILLEEN TX 76543

BS469665

AASF, MDARNGH-60-10-SOF-02 SPINDLE LUG NON-DESTRUCTIVE INSPECTION (NDI) ANDRETIREMENT LIFE CHANGES COMPLIED WITH

24-Jun-2010 1

EDGEWOOD, MD

TS026891

AASF MD ARNGH-60-10-AMAM-16 (GUARDED CMWS REDPUSH BUTTON) COMPLIED WITH

08-Jul-2010 1

EDGEWOOD, MD

ED703987

AASF MDARNGH-60-10-ASAM-15 (ESSS VENT ELBOW)COMPLIED WITH

11-Aug-2010 1

BLDG E-4081EDGEWOOD, MD 21010

TS026891

AASF MD ARNGH-60-10-ASAM-12 (T700 SERIES ENG COMMONCOMPONENT TIME CHANGE) COMPLIED WITH

27-Aug-2010 1

EDGEWOOD, MD

RH026085

AASF MD ARNGH-60-10-ASAM-11 (COMMON COMPONENTTIME CHANGE) COMPLIED WITH

31-Aug-2010 1

EDGEWOOD, MD

RH026085

AASF MDARNGH-60-10-ASAM-16 (RESCUE HOIST CABLE CUTHARNESS CONNECTOR) COMPLIED WITH

09-Sep-2010 1


TS026891

CSC FT HOOD AFMAAIRWORTHINESS RELEASE (AWR) FOR UH/HH-60A/L/M HELICOPTERS EQUIPPED WITHAEROSPACE FILTRATION SYSTEM (AFS)AUXILIARY POWER UNIT (APU) INLETBARRIER FILTERS AWR 1539 DTD 30 AUG2010 REV 1 APPLIED AT 4317.2 ACFT HRS.

29-Oct-2010 1

KILLEEN TX 76543

BS469665

AASF MDARNGH-60-11-AMAM-03 ( OIL COOLER FAN AXIALBEARING) C/W @ 4317.2 ACFT HRS

02-Nov-2010 1


DW156906

1109TH AVCRADH-60-11-AMAM-04 LCF CHANGE 61REQUIREMEMNTS C/W

26-Nov-2010 1

GROTON, CT

JA580641

1109TH AVCRADLATE ENTRY H-60-10-SOF-01 DEPOT REPAIROF LEGACY MAIN ROTOR BLADES C/W

26-Nov-2010 2

GROTON, CT

JA580641

1109TH AVCRADLATE ENTRY H-60-09-AMAM-04 A2C2S C/W 26-Nov-2010 3

GROTON, CT

JA580641

1109TH AVCRADH-60-11-ASAM-03 HAMILTON STANDARDHYDRO-MECHANICAL UNIT (HMU) C/W

30-Nov-2010 1

GROTON, CT

JA580641

1109TH AVCRADH-60-11-ASAM-04 AN/ARN-153 TCN-500RECEIVER BEARING ERROR COMPLIED WITH

02-Dec-2010 1

GROTON, CT

JA580641

1109TH AVCRADH-60-10-AMAM-12 IMPROVED DRAG BEAM,COMPLIED WITH

08-Dec-2010 1

GROTON, CT

JA580641



8.7.DATE

6.REMARKS

4. 5.



1109TH AVCRADT/R RIG PERFORMED. BLADE BIAS SET AT,RED 4.703-5.029=.326, BLUE 4.016-4.350=.334,YELLOW 4.700-5.032=.334, BLACK 4.023-4.361=.335. CABLE TENSION L/H 140, R/H 140,TEMP 70 DEG.

21-Dec-2010 1

GROTON, CT

JA58061

1109TH AVCRADH-60-11-ASAM-06 CYCLIC STICK STOP BOLTS,COMPLIED WITH

22-Dec-2010 1

GROTON, CT

JA580641

1109TH AVCRADPMI 1 COMPLETED AT 4378.2 ACFT HRS NEXTDUE 5098.2 ACFT HRS

06-Jan-2011 1

GROTON, CT

JA580641

D CO. 2-224 DET-1H-60-11-AMAM-06 MEDEVAC CAROUSELREFERBISHMENT, COMPLIED WITH

17-Feb-2011 1


DET 1 D CO. 2-224THAVN

H-60-11-ASAM-08 APX-118 SAFETY, COMPLIEDWITH

17-Feb-2011 2


CN154690

D CO 2-224TH AVN100% FOD CHECK COMPLETED ON THISAIRCRAFT ASSIGNED TO 2-224TH AVN FORLOST 1/4" DEEP WELL 1/4" DRIVE SOCKETPER COMMANDER AND QUALITY CONTROL.TOOL WAS NEVER FOUND AS OF 22 MAR2011. SSG G. DELA PENA QC D-CO 2-224THAVN.

22-Mar-2011 1

FT HOOD, TX

GD331784

D CO 2-224TH AVNH-60-11-ASAM-09 (IAFTS) COMPLIED WITH 29-Mar-2011 1

FT HOOD, TX

CN154690

D CO 2-224TH AVNAIRWORTHINESS RELEASE (AWR) DTD30JUN2010 FOR THE CREWCHIEF/DOORGUNNER M4 CARBINE MOUNT SYSTEMINSTALLED ON UH-60A/L/M HELICOPTERSAPPLIED THIS DATE (AWR1615 R-1)

13-Apr-2011 1

FT HOOD, TX

GD331784

D CO 2-224TH AVNAIRWORTHINESS RELEASE (AWR) DTD01FEB2011 FOR THE VERTICAL PILOT ANDCOPILOT M4 CARBINE MOUNT SYSTEMINSTALLED ON UH-60A/L HELICOPTERSAPPLIED THIS DATE (AWR1667 R-3)

13-Apr-2011 2

FT HOOD, TX

GD331784

D CO 224TH AVNH-60-11-AMAM-09 (ENG HIST RECORDERREADINGS REPORTING)

18-Apr-2011 1


DB299818

D CO 224TH AVNH-60-11-AMAM-11 COMPLIED WITH (AWR) 19-Apr-2011 1


DB299818

D CO 2-224TH AVNAWR 1524 BAPS R3 DTD 4JAN11 APPLIED ONTHIS DATE

11-May-2011 1

UDAIRI, KUWAIT

GD331784

D CO 2-224TH AVNAWR 1270 EIBF R7 DTD 24NOV2010 APPLIEDON THIS DATE.

11-May-2011 2

UDAIRI, KUWAIT

GD331784

D CO 2-224TH AVNAWR 1223 IR ANTI-COLLISION LIGHT R515MAY09 APPLIED ON THIS DATE

11-May-2011 3

UDAIRI, KUWAIT

GD331784

D CO 2-224TH AVNAIRCRAFT DEPLOYED IN SUPPORT OFOPERATION NEW DAWN

11-May-2011 4

UDAIRI, KUWAIT

GD331784



8.7.DATE

6.REMARKS

4. 5.



D CO 2/224TH AVNMODIFICATION OF EIBF UPPER LEFT HANDAND RIGHT HAND SUPPORT TUBE P/N 107220-103 & LOWER LEFT HAND AND RIGHT HANDSUPPORT TUBE P/N 107230-101 MEO NOA5851 REV C

15-May-2011 2


TK820960

D CO 2-224TH AHBH-60-11-AMAM-13 (EXTERNAL RESCUE HOISTMOUNT FITTING) COMPLIED WITH

08-Jun-2011 1

COB TAJI IRAQ, APO AE09378

CN154690

D CO 2-224TH AVNH-60-11-ASAM-11 ANTI-ICE/START BLEEDVALVE ACTUATOR SHAFTS COMPLIED WITH

09-Jul-2011 1


TK820960

D CO 2-224TH AHBH-60-11-ASAM-13(ENGINE AIR INLET ANTI-ICING/MODULATING VALVE) COMPLIED WITH

10-Jul-2011 1


CN154690

D CO 2-224TH AHBH-60-11-SOF-01(DISCREPANT SELF LOCKINGDOUBLE HEXAGON NUTS) COMPLIED WITH

14-Jul-2011 1


CN154690

D CO 2-224TH AVNAWR 1694 DUAL STABILATOR CONTROLLER(DSC) COMPLIED WITH

18-Jul-2011 1


TK820960

D CO 2-224TH AHBH-60-11-ASAM-14 (ENG COWLING) COMPLIEDWITH

23-Aug-2011 1


CN154690

TASM-EA3T INSPECTION COMPLETED AT 4724.8 ACFTHRS BY ACE TEAM MEMBER "S"

31-Aug-2011 1


WC643445

D CO 2-224TH AVNH-60-11-AMAM-15 INTEGRATED VEHICLEHEALTH MANAGEMENT SYSTEM (IVHMS)

12-Sep-2011 1


TK820960

L3PMI-2 COMPLETED @ 4729.3 ACFT HRS. PMI-1DUE @ 5089.3 ACFT HRS.

15-Sep-2011 1

CAMP TAJI, IRAQ

LA829930

L3T/R 3 DEGREE BIAS RED 4.576-4.915= .339,YELLOW 4.509- 4.831= .322, BLUE 3.895- 4.214=.319, BLACK 3.887-4.214= .327 T/R CABLETENSION TEMP. 30 *C @ L/H 176 LBS / R/H175 LBS. DIFF BETWEEN HIGH AND LOWCOLL. IS 15.98LOW COLL. 90* 8.60 / 180* -1.90 /270* -9.70 / 0* 0.70 / TOTAL* -2.30 / AVG* -0.575HIGH COLL. 90* 19.00 / 180* 12.00 / 270*11.80 / 0* 18.80 / TOTAL* 61.60 / AVG*15.40FULL UP COLL., FWD CYCLIC. 90* -2.00 /270* 31.60 / TOTAL* 33.60FULL UP COLL. AFTCYCLIC. 90* 25.00 / 270* 5.30 / TOTAL*19.70FULL DOWN COLL. LEFT CYCLIC. 180*8.60 / 0* 6.50 / TOTAL* 15.10FULL DOWN COLL.RIGHT CYCLIC. 180* 6.80 / 8.70 / TOTAL* 15.50

16-Sep-2011 1

CAMP TAJI, IRAQ

LA829930



8.7.DATE

6.REMARKS

4. 5.



L3T/R 3 DEGREE BIAS RED 4.576-4.915= .339,YELLOW 4.509- 4.831= .322, BLUE 3.895- 4.214=.319, BLACK 3.887-4.214= .327 T/R CABLETENSION TEMP. 30 *C @ L/H 176 LBS / R/H175 LBS. DIFF BETWEEN HIGH AND LOWCOLL. IS 15.98LOW COLL. 90* 8.00 / 180* -1.50 /270* -9.10 / 0* 0.20 / TOTAL* -2.40 / AVG* -0.600HIGH COLL. 90* 19.00 / 180* 12.00 / 270*11.80 / 0* 18.80 / TOTAL* 61.60 / AVG*15.40FULL UP COLL., FWD CYCLIC. 90* -2.00 /270* 31.60 / TOTAL* 33.60FULL UP COLL. AFTCYCLIC. 90* 25.00 / 270* 5.30 / TOTAL*19.70FULL DOWN COLL. LEFT CYCLIC. 180*8.60 / 0* 6.50 / TOTAL* 15.10FULL DOWN COLL.RIGHT CYCLIC. 180* 6.80 / 8.70 / TOTAL* 15.50

16-Sep-2011 2

CAMP TAJI, IRAQ

LA829930

L3T/R CHIP LIGHT CAME ON DURING INITIALGROUND RUN, CHECK T/R G/B CHIPDETECTOR FOUND FUZZ, FINE HAIR LIKEPARTICLES BUILD UP IN CHIP DETECTOR.ACTION TAKEN SERVICEABILITY CHK, DRAINT/R G/B 3 TIMES, CLEAN T/R CHIP DETECTORAND TOOK OIL SAMPLE AFTER THE SECONDRUN UP.

18-Sep-2011 1

CAMP TAJI, IRAQ

LA829930

D CO 2-224TH AVNAWR 1682 T700-GE-701D/CC WITH AUTORELIGHT AND TRANSIENT DROOPIMPROVEMENTS COMPLIED WITH

18-Sep-2011 2


TK820960

D CO 2-224TH AVNAWR 1529 FIBER OPTIC GYRO SYSTEMCN-1716/A ATTITUDE HEADING REFERENCE UNIT(FOGS /AHRU) COMPLIED WITH

18-Sep-2011 3


TK820960

D CO 2-224THH-60-11-AMAM-20(AN/ASN-128D SOFTWAREUPGRADE) COMPLIED WITH

21-Sep-2011 1


CN154690

CO D 1/171ST GSABAIRCRAFT UPGRADED TO ULLS-A(E) VERSION6.14 ON THIS DATE

06-Oct-2011 1


JH578940

CO D 1/171ST GSABH-60-11-AMAM-19, INTEGRATED MATERIALMANAGEMENT CENTER (IMMC) LEGITIMATECODE FILE (LCF) CHANGE 62, COMPLIEDWITH ON THIS DATE. AMCOM CHANGE 62

06-Oct-2011 2


JH578940

D CO 2-224TH AHBH-60-12-SOF-01(TAIL ROTOR INTERMEDIATEGEARBOX) COMPLIED WITH

08-Oct-2011 1


CN154690


11-Oct-2011 1


CN154690


16-Oct-2011 1


CN154690

AASF MDARNGH-60-12-SOF-04 (BREEZE EASTERN EXTERNALHOIST OPS) C/W

06-Apr-2012 1


RH026085



8.7.DATE

6.REMARKS

4. 5.



AASF MDARNGH-60-12-AMAM-03 (TRANSPONDER AND CMWSINSTALLATION) C/W

02-May-2012 1


RH026085

AASF MDARNGH-60-12-ASAM-06 (FUEL SYS BREAKAWAYVALVE) C/W

03-May-2012 1


RH026085

L-3ACE COMPLETED AT 5047.8 A/C HRS. BY ACETEAM MEMBERS B/G. AFMA, RASM-E,AMCOM.

05-Jun-2012 1


JG389608

AASF MDARNGH-60-12-ASAM-08 COMPLIED WITH. 19-Jul-2012 1


TS026891

1109TH TASMGH 60-12-ASAM-01 TAIL ROTOR OUTPUT BEVELGEAR NDI. COMPLIED WITH. NEW T/R/ G/BINSTALLED DURING RESET. NDI OK

13-Aug-2012 1

GROTON, CT

JA580641

1109TH TASMGH-60-12-ASAM-09 BREEZE EASTERNEXTERNAL RESCUE HOIST CARTRIDGEACTUATED DEVICE. COMPLIED WITH

22-Aug-2012 1

GROTON, CT

JA580641

MDARNGH-60-12-ASAM-09 COMPLIED WITH 28-Aug-2012 1


PM884815

1109TH TASMGH-60-12-AMAM-15 TRIM ACTUATORSCOMPLIED WITH

29-Aug-2012 1

GROTON, CT

JA580641

1109TH TASMGH-60-12-ASAM-11 HYDRO MECHANICAL UNIT.COMPLIED WITH

06-Sep-2012 1

GROTON, CT

JA580641

1109TH TASMGH-60-11-AMAM-17 TAIL ROTOR RETENTIONPLATE SHIMS COMPLIED WITH

06-Sep-2012 2

GROTON, CT

JA580641

1109TH TASMGH-60-12-ASAM-01 TAIL ROTOR GEAR BOXBEVEL GEAR NDI. COMPLIED WITH

06-Sep-2012 3

GROTON, CT

JA580641

1109TH TASMGH-60-12-AMAM-16 MAIN ROTOR SPINDLE SUB-COMPONENT TRACKING REQUIREMENTS.COMPLIED WITH

12-Sep-2012 1

GROTON, CT

JA580641

1109TH TASMGH-60-12-AMAM-09 HYDRAULIC LINE CHAFEDUE DUE MISSING CLAMPS. COMLIED WITH

21-Sep-2012 1

GROTON, CT

JA580641

1109TH TASMGH-60-12-AMAM-12 RESCINDED COMMONCOMPONENT REMOVAL DATES. COMPLIEDWITH

21-Sep-2012 2

GROTON, CT

JA580641

1109TH TASMGH-60-12-ASAM-07 ELECTRIC WIRE CHAFE.COMPLIED WITH

21-Sep-2012 3

GROTON, CT

JA580641

1109TH TASMGRESET COMPLETED AT 5085.6 ACFT I/A/W TB1-1520-237-30-1 DESERT OPERATIONSSPECIAL INSPECTION AND CLEANINGREQUIREMENT.

27-Sep-2012 1

GROTON, CT

JA580641

1109TH AVCRADPMI 1 AND PMI 2 COMPLETED DURING RESETAT 5085.6 ACFT HOURS NEXT PMI 1 DUE AT5445.6 ACFT HOURS

27-Sep-2012 2

GROTON, CT

JA580641



8.7.DATE

6.REMARKS

4. 5.



1109TH TASMG M/R RIG COMPLETED DURING RESET AT5085.6 ACFT HOURS. BIAS SET AT, FWD -1.5FLATS. AFT +1.5 FLATS, LAT -3 FLATS.

27-Sep-2012 3

GROTON, CT

JA580641

1109TH TASMGT/R RIG COMPLETED DURING RESET. BIASSET AT, RED .326, BLUE .327, YELLOW .346,BLACK .336. CABLE TENSION WAS, LEFT 133AND RIGHT 168 LBS AT 68F.

27-Sep-2012 4

GROTON, CT

JA580641

AASF MDARNGT/R RIG CHK COMPLETED 3 DEGREE BIAS:RED 5.067, 4.752, .315 BLK 4.397, 4.079, .318YEL 5.068, 4.738, .330 BLUE 4.386, 4.073,.313T/R CABLE TENSION: 148 LBS @ 24 C

01-Nov-2012 1


ED703987

AASF, MDARNGH-60-13-ASAM-01 (ANTI-COLLISION LIGHTPOWER SUPPLY) COMPLIED WITH

28-Nov-2012 1


AASF MDARNGH-60-13-AMAM-02 (AHRS) COMPLIED WITH. 28-Nov-2012 2


TS026891

AASF MDARNGH-60-13-AMAM-03 (DECU TGT BIAS) COMPLIEDWITH.

28-Nov-2012 3


RH026085

AASF, MDARNGH-60-13-AMAM-04 (ULLS-A(E) LCF CHG 63)COMPLIED WITH

28-Dec-2012 1


DD824171

AASF MDARNGH-60-13-AMAM-06 (CEFS) COMPLIED WITH. 21-Feb-2013 1


RH026085

AASF, MDARNGH-60-13-AMAM-05 (MAIN LANDING GEARWHEEL BRAKE ASSY.) COMPLIED WITH

01-Mar-2013 1


PM884815

AASF MDARNGH-60-13-ASAM-04 (PMB) COMPLIED WITH. 22-Mar-2013 1


RH026085

AASF # 1ACFT TEMPORARILY TRANSFERRED TO AASF#1 JACKSON MS, UIC: WTQGA0

27-Mar-2013 1

JACKSON, MS 39209-3436

AB198454

AASF # 1H-60-13-AMAM-07, LOAD DEMAND SPINDLECABLE CLEARANCE, COMPLIED WITH.PASSES - INSP OK.

03-Apr-2013 1


AB198454

AASF # 1H-60-13-AMAM-08, AN/AVR-2B MANUALUPDATE, DOES NOT APPLY TO THIS ACFT.

04-Apr-2013 1


AB198454

AASFH-60-13-ASAM-05, BREEZE EASTERNVARIABLE SPEED ELECTRIC RESCUE HOISTC/W. (N/A THIS ACFT)

08-Apr-2013 1


JL178322

AASF # 1H-60-13-ASAM-06, PHASED MAINTENANCEINSPECTION CHECKLIST CHANGES,COMPLIED WITH AT 5270.8 ACFT HRS

16-May-2013 1


AB198454



8.7.DATE

6.REMARKS

4. 5.



AASF # 1H-60-13-AMAM-01, FLIGHT CONTROL RIGGINGPROCEDURES, COMPLIED WITH @ 5278.6ACFT HOURS. YELLOW BLADE SET - 0.5, REDBLADE SET - 0.5, BLUE BLADE SET - 0.5,BLACK BLADE SET - 0.5

21-May-2013 1


AB198454

AASF # 1TAIL ROTOR RIG COMPLETED. T/R SERVOPISTON TRAVEL EXT-INT OUT 3.50/3.47/0.40.T/R BIAS CHECK RED BLADE INT 4.71, W/BIAS5.03, DIF 0.32. BLACK BLADE INT 4.07, W/BIAS4.39, DIF 0.32. YELLOW BLADE INT 4.78,W/BIAS 5.11, DIF 0.33. BLUE BLADE INT 4.03,W/BIAS 4.38, DIF 0.35. T/R TENSION L/H 150,R/H 151, TEMP 25*C.

22-May-2013 1


AB198454

AASF # 1H-60-13-AMAM-09, NUMBER 6R STRINGER,DOES NOT APPLY TO THIS AIRFRAME. UH-60M ONLY.

29-May-2013 1


AB198454

AASF # 1H-60-13-SOF-01, ATTITUDE HEADINGREFERENCE SET, COMPLIED WITH. ACFT HASDUAL AHRS INSTALLED.

31-May-2013 1


AB198454

AASF # 1H-60-13-ASAM-07, DYNAMIC COMPONENTRECORDS REVIEW, DOES NOT APPLY TO THISACFT (MH-60M ONLY)

17-Jun-2013 1


AB198454

AASF MDARNGH-60-13-AMAM-11 (MAIN XMSN FILTER BOWLHARDWARE) COMPLIED WITH.

12-Jul-2013 1


RH026085

AASF MDARNGH-60-13-AMAM-10 (AMCOM CHG 64) COMPLIEDWITH

04-Sep-2013 1


DD824171

AASF, MDARNGH-60-13-AMAM-15 (CRASHWORTHY EXTERNALFUEL SYSTEM (CEFS) RIGHT HAND FUELCELL COVER PLATE) COMPLIED WITH

22-Oct-2013 1


PM884815

AASF MDARNGH-60-14-SOF-01 (EXT HOIST) COMPLIED WITH 01-Nov-2013 1


RH026085

AASF MDARNGCOMPLIED WITH REQUIREMENTS OF H-60-14-ASAM-02 (HEALTH USAGE MONITORINGSYSTEMS (HUMS) ACCELEROMETERS.

26-Nov-2013 1


ED703987

AASF MDARNGH-60-14-AMAM-03 (LATERAL SWASHPLATELINK) COMPLIED WITH

24-Dec-2013 1


RH026085

AASF MDARNGH-60-14-ASAM-03 (ENGINE INLET BARRIERFILTER BRACKET REMOVAL) COMPLIED WITH

29-Jan-2014 1


ED703987

L-3ACE COMPLETED AT 5443.8 A/C HRS. BY ACETEAM MEMBERS B/G. AFMA, RASME, AMCOM.

04-Mar-2014 1


JG389608

AASF MDARNGH-60-14-AMAM-08 AN / ASE-15E(COMMUNICATION CONSOLE CIRCUITBREAKER) COMPLIED WITH.

19-Mar-2014 1


MG064943



8.7.DATE

6.REMARKS

4. 5.



AASF MDARNGH-60-14-AMAM-10 (HONTEK COATED M/RBLADE REMOVAL) COMPLIED WITH

15-Apr-2014 1


RH026085

AASF MDARNGAWR 1444 DATED 14APR14 (SINGLE AHRU)APPLIED

16-Apr-2014 1


RH026085

AASF MDARNGT/R RIG COMPLETED: RED BLADE SET .9 BIAS5.09 3 - 4.780 =.313 @ 3.0 DEGREE'S, BLACKBLADE SET .9 BIAS4.402 - 4.076 = .326 @ 3.1DEGREE'S, YELLOW BLADE SET .8 BIAS 5.058- 4.730 = .328 @ 3.0, BLUE BLADE SET .5 BIAS4.479 - 4.150 = .329 @ 3.1T/R CABLE TENTIONCHECK: 139 RIGHT 138 LEFT @ 68 DEGREE'S

17-Apr-2014 1


TS026891

AASF MD SRNGH-60-14-AMAM-12 (M/R SPINDLE RETENTIONNUT TBO CHANGE) COMPLIED WITH

24-Apr-2014 1


ED703987

AASF MDARNGH-60-14-ASAM-06 (FLIGHT CONTROL MIXERASSY) COMPLIED WITH

25-Apr-2014 1


RH026085

AASF MDARNGPMI-1 COMPLETED @ 5445.1 ACFT HRS, PMI-2DUE @ 5805.1 ACFT HRS

30-Apr-2014 1


RH026085

MD ARNG AASFH-60-14-AMAM-05, ULLS-A(E) LCF CHANGE 65COMPLIED WITH @ 5447.8 ACFT HRS

14-May-2014 1


DD824171

AASF MDARNGH-60-14-AMAM-14 (IVHMS CABLING BY 4 JUN14) COMPLIED WITH

04-Jun-2014 1


JH949017

AASF-MDH-60-14-SOF-03 (DISCREPANT SELF LOCKINGDOUBLE HEXAGON NUTS) C/W @ 5456 ACFTHRS

27-Jun-2014 1


DW156906

MDARNG AASFH-60-14-AMAM-16 (AHRU 2410) COMPLIEDWITH

19-Jul-2014 1


CN154690

AASF MDARNGH-60-14-ASAM-09 (ENG OUTPUT SHAFT)COMPLIED WITH

13-Aug-2014 1


RH026085

AASF MDARNGH-60-14-SOF-04 (CREW CHECKLIST)COMPLIED WITH

27-Aug-2014 1


RH026085

AASF MDARNGH-60-14-ASAM-10 (PLANETARY CARRIERASSEMBLY) COMPLIED WITH

09-Sep-2014 1


DW156906

AASF MDARNGAWR 1823 DTD 29MAY14, UH/HH-60A/LHELICAOPTER WITH INTEGRATED VEHICLEHEALTH MANAGEMENT SYSTEM (IVHMS)HEALTH USAGE MANAGEMENT SYSTEM(HUMS) SOFTWARE BLOCK 5.0 APPLIED

24-Oct-2014 1




8.7.DATE

6.REMARKS

4. 5.



AASF MDARNGH-60-14-AMAM-19 (ULLS-A(E) LCF CHANGE 66)COMPLIED WITH

27-Oct-2014 1


DD824171

AASF, MDARNGH-60-15-SOF-01 (OIL COOLER FAN AXIALBEARING) COMPLIED WITH

31-Oct-2014 1


PM884815

AASF MDARNGH-60-15-ASAM-01 (LED CAUTION ADVISORYPANEL) COMPLIED WITH

01-Dec-2014 1


RH026085

AASF MDARNGH-60-15-AMAM-05 (AHRS EMERGENCYPROCEDURES) COMPLIED WITH

18-Dec-2014 1


RH026085

AASF MDARNGH-60-15-AMAM-02 (IVHMS WIRINGMANAGEMENT) COMPLIED WITH

05-Feb-2015 1


RH026085

L-3ACE COMPLETED AT 5533.7 A/C HRS. BY ACETEAM MEMBE3RS B/G. AFMA, RASME,AMCOM.

04-Mar-2015 1


JG389608

AASF MDARNGH-60-15-AMAM-06 (IDENTIFICATION OF ASE)COMPLIED WITH

09-Mar-2015 1


RH026085

AASF, MDARNGH-60-15-ASAM-03 (TROOP/GUNNER SEATENERGY ATTENUATORS) COMPLIED WITH

28-May-2015 1


PM884815

AASF MDARNGH-60-15-AMAM-11 (MODE-S TRANSPONDERADDRESS REVIEW) COMPLIED WITH

24-Jun-2015 1


TS026891

AASF MDARNGH-60-15-AMAM-14 (LEGITIMATE CODE FILECHANGE 67 REQUIREMENTS) COMPLIED WITH

12-Aug-2015 1


SH784152

AASF-MDH-60-15-SOF-02 (FRIES RELEASE CABLE)COMPLIED WITH

24-Sep-2015 1


DW156906

AASF, MDARNGH-60-16-AMAM-01 (ENGINE INLET BARRIERFILTER) COMPLIED WITH.

27-Oct-2015 1


TS026891

AASF, MDARNGH-60-16-ASAM-01 (INBOARD RETENTIONPLATE TORQUE CHECKS) COMPLIED WITH

12-Nov-2015 1


PM884815

AASF MDARNGH-60-16-AMAM-03 (PERSONNEL LOCATOR SETREMOVAL) COMPLIED WITH

23-Nov-2015 1


SH784152

AASF MDARNGH-60-16-ASAM-02, DEFECTIVE FUEL HOSESCOMPLIED WITH

06-Jan-2016 1


SH784152



8.7.DATE

6.REMARKS

4. 5.



AASF MDARNGAIRCRAFT TRANSFERRED TO BESTPROGRAM ON 28 APR 2016 FOR ARMY/BESTPROGRAM BY C CO 2-224TH AVN REG AT5610.8 AIRCRAFT HOURS DATA PLATEREMAINED INSTALLED

29-Apr-2016 1


SH784152

SCIENCE &ENGINEERINGSERVICES

H-60-16-AMAM-04 (T-CLIP INSTALLATION) NOTCOMPLIED WITH

05-May-2016 1

HUNTSVILLE

MS901824

SCIENCE &ENGINEERINGSERVICES

H-60-15-ASAM-07 (MAIN ROTOR BLADEDEBONDING AND TIP RIB CRACKING) NOTCOMPLIED WITH

05-May-2016 2

HUNTSVILLE

MS901824


UNIT UNIQUE INVENTORY ITEMSSES BEST

4. EQUIPMENT CHECKLIST

7822971 UH-60A

3. AREA NAME 2. MODEL 1. SERIAL NUMBER

Report Date: 1/205-May-2016

1BFT PALLET ASSEMBLY (040537-001)

Unt

UUUUUUnt

Unt

Un

Unt

Un0

66

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER

QTY REQ:NOMENCLATURITEM NO

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

AIRCRAFT INVENTORY RECORDDA FORM 2408-17 E, NOV 91

2/2Report Date: 05-May-2016AREA NAMEMODELSERIAL NUMBER

UNIT UNIQUE INVENTORY ITEMSSES BEST7822971 UH-60A

NAME OR PIDNUMBER DATE

db c

DATE NUMBER RANKRANK NAME OR PID

CHECK CHECK

ba ad

5. VERIFICATION

c

b. LOCATION/REMARKSCHECK NO.

6. LOCATION OR REMARKS

a. ITEM NUMBER

Nomenclature

BFT PALLET ASSEMBLY(040537-001)

1 not installed66

REVERSE OF DA FORM 2408-17 E, NOV 91

DATE AC HRS SHAFT VERTICAL REASON FOR VIB CHECKLONGITUDINALLATERAL

IPS READINGS4.

7822971HELICOPTER, UTILITYUH-60A3. AIRCRAFT SERIAL NUMBER2. NOMENCLATURE1. AIRCRAFT MODEL

Report Date: 05-May-2016 1/4

100 HR.31-May-2000 #1 ENGINE 0.32002665

100 HR.31-May-2000 #2 ENGINE 0.28002665

100 HR.31-May-2000 AXIAL FAN 0.010.0702665

100 HR.20-Sep-2000 #1 ENGINE 0.48002766.5

100 HR.20-Sep-2000 #2 ENGINE 0.5002766.5

100 HR.20-Sep-2000 T/R 0.14002766.5

100 HR.20-Sep-2000 AXIAL FAN 0.280.302766.5

100 HR.23-Jul-2002 AXIAL FAN 0.220.403068

100 HR.23-Jul-2002 T/R 0.08003068

100 HR.23-Jul-2002 #2 ENGINE 0.28003068

100 HR.23-Jul-2002 #1 ENGINE 0.36003068

REMOVAL & REINSTALLATION01-Aug-2002 #1 ENG 0.43003071.7

D/S REMOVAL AND REINSTALL13-Sep-2002 AXIAL FAN 0.480.1903071.7

TAIL PYLON REPLACEMENT04-Sep-2003 T/R 0.09003249

INBOARD RET PLATE RETQ17-Sep-2003 T/R 0.11003259.1

100 HR.03-Oct-2003 #1 ENGINE 0.41003266.3

100 HR.03-Oct-2003 #2 ENGINE 0.23003266.3

100 HR.03-Oct-2003 OIL COOLER 0.310.1703266.3

100 HR.03-Oct-2003 T/R 0.12003266.3

POST PMS-225-Aug-2004 T/R 0.17003327.3

POST PMS-225-Aug-2004 #1 HSS 0.19003327.3

POST PMS-225-Aug-2004 #2 HSS 0.25003327.3

POST PMS-225-Aug-2004 OIL COOLER 0.180.103327.3

INBOARD RET PLATE RETQ23-Jan-2005 T/R 0.17003257.3

INSTALLATION OF ENG23-Feb-2005 #2 HSS 0.41003384.3

100 HR23-Mar-2005 #2 HSS 0.22003423

100 HR23-Mar-2005 T/R 0.11003423

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 HR23-Mar-2005 OIL COOLER 0.140.103423

100 HR30-Mar-2005 #1 HSS 0.19003423

120 HR INSPECTION03-May-2006 OIL COOLER 0.10.2503659.8

120HR INSPECTION03-May-2006 #2 ENGINE 0.15003659.8

120 HR INPSECTION03-May-2006 TAIL ROTOR 0.04003659.8

120HR INSPECTION03-May-2006 #1 ENGINE 0.02003659.8

POST PMI-127-Jun-2006 AXIAL FAN 0.150.2203731

POST PMI-127-Jul-2006 TAIL ROTOR 0.07003731

POST PMI-127-Jul-2006 #1 ENG HSS 0.35003731

POST PMI-127-Jul-2006 #2 ENG HSS 0.12003731

120HR01-Nov-2006 TAIL 0.1003846.4

120HR01-Nov-2006 OIL COOLER 0.110.2503846.4

120HR01-Nov-2006 #1HSS 000.273846.4

120HR01-Nov-2006 #2HSS 000.123846.4

REMOVAL OF DRIVESHAFT AND VISCOUS MOUNT07-Mar-2007 OIL COOLER 0.20.5803882.2

REMOVAL OF BOOT07-Mar-2007 TAIL ROTOR 0003882.2

T & B FOR M/R P/C ROD NUT REPLACE ASAM13-Jun-2007 M/R 0.05003932.4

120 HR12-Jul-2007 #1 HSS 0.21003965.3

120 HR12-Jul-2007 #2 HSS 0.11003965.3

120 HR12-Jul-2007 TAIL ROTOR 0.01003965.3

120 HR12-Jul-2007 OIL COOLER 0.20.3803965.3

120 HR REQ10-Nov-2008 OIL COOLER 0.11004021.7

120 HR REQ12-Nov-2008 ENG 1 0.37004021.7

120 HR REQ12-Nov-2008 ENG 2 0.16004021.7

120 HR REQ12-Nov-2008 T/R 0.07004021.7

AFTER RE-TQ REQ26-Nov-2008 T/R 0.01004028

120 HR03-Mar-2010 #1ENG 0.29004261.7




IPS READINGS4.



120 HR03-Mar-2010 #2ENG 0.18004261.7

120 HR03-Mar-2010 OIL COOLER 0.4004261.7

120 HR03-Mar-2010 T/R 0.09004261.7

TEST FLIGHT31-May-2011 #1 ENG 0.38004471.1

TEST FLIGHT31-May-2011 #2 ENG 0.13004471.1

TEST FLIGHT31-May-2011 TAIL ROTOR 0.11004471.1

120 HR REQ27-Jul-2011 #1 ENG 0.34004613.3

120 HR REQ27-Jul-2011 #2 ENG 0.12004613.3

120 HR REQ27-Jul-2011 OIL COOLER 0.220.3604613.3

POST PMI - 217-Sep-2011 #1 ENG HSS 0.19004729.3

POST PMI - 217-Sep-2011 #2 ENG HSS 0.27004729.3

POST PMI - 217-Sep-2011 OIL COOLER 0.080.2804729.3

POST PMI - 217-Sep-2011 TAIL ROTOR 0.06004729.3

120 HR13-Nov-2011 TAIL ROTOR 0.1004968.4

120 HR13-Nov-2011 OIL COOLER 0.3900.614968.4

120 HR13-Nov-2011 ENG#1 0.48004968.4

120 HR13-Nov-2011 #2ENG 0.32004968.4

PORT OPS11-Apr-2012 TAIL ROTOR 0.02005020

REQ FOR COMPLETION OF RESET09-Oct-2012 #1 ENG 0.13005086.6

REQ FOR COMPLETION OF RESET09-Oct-2012 #2 ENG 0.08005086.6

REQ FOR COMPLETION OF RESET09-Oct-2012 OIL COOLER 0.010.0505086.6

REQ FOR COMPLETION OF RESET09-Oct-2012 TAIL ROTOR 0.07005086.6

POST T/R RIG CHK08-Nov-2012 TAIL ROTOR 0.03005096.9

120 HR15-Mar-2013 #1 ENG 0.18005206.3

120 HR15-Mar-2013 #2 ENG 0.14005206.3

120 HR15-Mar-2013 OIL COOLER 0.090.2905206.3

120 HR15-Mar-2013 TAIL ROTOR 0.03005206.3




IPS READINGS4.



T/R BLADE REPLACEMENT23-May-2013 TAIL ROTOR 0.01005278.6

T/R PADDLE REINSTALL02-Jul-2013 T/R 0.05005305.1

120 HR07-Aug-2013 #2 ENG 0.24005324.7

120 HR07-Aug-2013 #1 ENG 0.14005324.7

120 HR07-Aug-2013 OIL COOLER 0.10.2205324.7

120 HR07-Aug-2013 TAIL ROTOR 0.1005324.7

PMI107-May-2014 ENG#1 0.18005446.8

PMI107-May-2014 ENG #2 0.2005446.8

PMI107-May-2014 OIL COOLER 0.10.205446.8

PMI107-May-2014 TAIL ROTOR 0.06005446.8

6. Remarks



PIDMWODATE HRS

DATEORAPPLYINGMWO TITLEAND MAN

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

TAIL ROTOR PITCH CHANGE SHAFT 7822971233035751. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


24-Jan-2014 FT

DW15690629-Jan-2014

2AASF-MD, APG-EA MD 21010

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

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

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

360

360

5553

7822971 524.8 5086

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

UH-60A A00604489 Days

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

HELICOPTER, UTILITY TAIL ROTOR GEARBOX ASSY Hrs

a. NOMENCLATURE AND TYPEa. NOMENCLATUREFREQUENCY

COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b

SAMPLE DATE PIDSAMPLELAST OILEND ITEM

RESULTSDATE RESULTS RECEIVED7. 8.6. REASON FORHOURS5.4.

COMPONENTCHANGE

PM88481516-Oct-2012NORMALBASELINE0.0508611-Oct-2012

ED70398729-Oct-2013ABNORMALROUTINE322.0322540822-Oct-2013

ED70398705-Nov-2013ABNORMALLAB REQUES322.0322540830-Oct-2013

PM88481504-Feb-2014NORMALLAB REQUES359.1333.55417.729-Jan-2014

CN15469024-Mar-2014ABNORMALROUTINE359.1359.15445.111-Mar-2014

CN15469015-May-2014NORMALLAB REQUES359.1359.15445.102-May-2014

CN15469006-Apr-2015ABNORMALROUTINE91.1450.25536.211-Mar-2015

CT26498628-Apr-2015NORMALSPECIAL4.6471.65557.622-Apr-2015

28 OCT 2013. HIGH WEAR METAL CONTENT. RESAMPLE AT END OF NEXT FLIGHT DAY/CYCLE. FT BRAGG AOAP LAB. CHRISTOPHER.NINER APG-EA, MD2101004 NOV 2013. WATER EXCEEDS PPM LIMIT, HIGH WEAR METAL CONTENT. DRAIN AND FLUSH, RESAMPLE AT END OF NEXT FLIGHT DAY/CYCLE. FT BRAGGAOAP LAB. CHRISTOPHER.NINER APG-EA, MD 2101024 MAR 2014. HIGH WEAR METAL CONTENT. RESAMPLE AT END OF NEXT FLIGHT DAY/CYCLE. FT BRAGG AOAP LAB. CHRISTOPHER.NINER APG-EA, MD2101006 APR 2015. HIGH WEAR METAL CONTENT. DRAIN AND FLUSH, RESAMPLE AT END OF NEXT FLIGHT DAY/CYCLE. FT BRAGG AOAP LAB.CHRISTOPHER.NINER APG-EA, MD 21010

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

PIDMWODATE HRS



TAIL ROTOR GEARBOX ASSY 7822971A006044891. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


21-Mar-2013 FM

ED70398722-Mar-2013

1AASF MDARNGONE-TIME INSPECTION OF SUSPECTSERIAL NUMBERED COMPONENTSFOR PLASTIC MEDIA BLAST (PMB)AND OXIDE FLAKE RESIDUE

H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR BLADE ASSY 7822971A009079831. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


26-Oct-1994 FM

WW980305-Aug-2010

2CCAD/WOMUAAALL UH-60 AIRCRAFT SHALLREQUIRE RE-SHIMMING OF TAILROTOR PIVOT BEARINGS PERREVISED PROCEDURES ANDCERTAIN BLADE ASSEMBLIES WILLBE INSPECTED FOR SPECIFIEDSERIAL NUMBERS WHICH CONTAINCOMPOSITE PIVOT BEARINGRETAINERS

UH-60-95-ASAM-03 TB 1-MWO:

Priority Mnt Level

14-Nov-2001 CO

WW980305-Aug-2010

1CCAD/WOMUAARECURRING INSPECTION OF TAILROTOR FAIRING ASSY.

UH-60-O2-ASAM-01MWO:

Priority Mnt Level

15-Sep-2005 DR

WW980305-Aug-2010

151CCAD/WOMUAARECAPPED1-1615 287 C1MWO:

Priority Mnt Level



PIDMWODATE HRS



TAIL ROTOR BLADE ASSY 7822971A009041031. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


01-Oct-1994 DM

LM674928-Dec-2010

1CCAD W0MUAARESHIMMING OF PIVOT BEARINGASSEMBLY

SOF MSF UH-60-95 ASAM-MWO:

Priority Mnt Level

26-Oct-1994 DM

MF203418-Jan-2012

2CCADALL UH-60 AIRCRAFT SHALLREQUIRE RE-SHIMMING OF TAILROTOR PIVOT BEARINGS PERREVISED PROCEDURES ANDCERTAIN BLADE ASSEMBLIES WILLBE INSPECTED FOR SPECIFIEDSERIAL NUMBERS WHICH CONTAINCOMPOSITE PIVOT BEARINGRETAINERS

UH-60-95-ASAM-03MWO:

Priority Mnt Level

14-Nov-2001 OM

MF203418-Jan-2012

1CCADINITIAL AND RECURRINGINSPECTION OF THE TAIL ROTORFAIRING ASSEMBLY

UH-60-02-ASAM-01 TB 1-1MWO:

Priority Mnt Level

25-Jan-2005 DE

LM674928-Dec-2010

1CCADRECURRING INSPECTION OF TAILROTOR FAIRING ASSY

ASAMA UH-60-02-ASAM-0MWO:

Priority Mnt Level

15-Sep-2005 DR

LM674928-Dec-2010

151CCADRECAPPEDDMWR 1-1615-287 C1MWO:

Priority Mnt Level

15-Sep-2005 DM

MF203418-Jan-2012

151CCADRECAPPEDDMWR 1-1615-187-287 C1 MWO:

Priority Mnt Level



PIDMWODATE HRS



SWASHPLATE ASSY 7822971015152-14291. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


18-Dec-1996 OU

OB96708224-Sep-2008

1CCAD, CORPC,TX 78419(AS1216)

REMOVAL OF CERTAIN REWORKEDMAIN ROTOR SWASHPLATEASSEMBLIES UH-60A, UH-60L, EH-60A, MH-60K AIRCRAFT

1-1520-237-20-185MWO:

Priority Mnt Level

08-Sep-1997 OM

OB96708224-Sep-2008


ALL UH-60A, UH-60L, EH-60A, ANDMH-60K HELICOPTERS, REMOVALOF SPECIFIC SUSPECT REWORKEDMAIN ROTOR SWASHPLATEASSEMBLIES


Priority Mnt Level

30-Oct-1997 OM

OB96708224-Sep-2008


ALL H-60 AIRCRAFT WITH THESWASHPLATE LINK ASSEMBLY, P/N70400-08110-054, MANUFACTUREDBY TEK (CAGE CODE 65780)


Priority Mnt Level

30-Apr-1998 OM

OB96708224-Sep-2008


ALL H-60 AIRCRAFT WITH THESWASHPLATE LINK ASSEMBLY, P/N70400-08110-054/-061,MANUFACTURED BY TEK (CAGECODE 65780)


Priority Mnt Level

02-Nov-1998 OM

OB96708224-Sep-2008


ALL H-60 AIRCRAFT, RESTORATIONOF FULL SERVICE LIFE ON THESWASHPLATE LINK ASSEMBLY, P/N70400-08110-054/-061,MANUFACTURED BY TEK (CAGECODE 65780)


Priority Mnt Level

12-Jun-2006 OM

OB96708229-Sep-2008

1CCAD, CORPC,TX 78419

ALL H-60 SERIES AIRCRAFT,SWASHPLATE DUPLEX BEARING


Priority Mnt Level



PIDMWODATE HRS



STABILATOR ACTUATOR 7822971B292060551. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


28-Aug-1996 OM

OB96708202-Aug-2008

1CCAD, CORPC,TX 78419(RL0519)

ALL EH/UH/MH-60 AIRCRAFTSTABILATOR ACTUATOR CLEVISES


Priority Mnt Level



SECTION V TAIL ROTOR PYLONSES BEST


7822971 UH-60A



1CU-2457/ARC(405-11-1), VHF-FM #1 COUPLER ANTENNA

Unt

UUUUUUnt

Unt

Un

Unt

Un0

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

Un0

4

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER





SECTION V TAIL ROTOR PYLONSES BEST7822971 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c



a. ITEM NUMBER

Nomenclature

CU-2457/ARC(405-11-1), VHF-FM #1 COUPLER ANTENNA

1 not installed2


SECTION IV TAIL CONESES BEST


7822971 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 BEST7822971 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c



a. ITEM NUMBER

Nomenclature

IFM AMPLIFIER - AM-7189A/ARC

1 not installed2


SECTION III TRANSITION SECTIONSES BEST


7822971 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

Un1

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ANTENNA, L-BAND (BFT) S65-8282-301

Unt

UUUUUUnt

Unt

Un

Unt

Un1

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

Un1

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 BEST7822971 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c



a. ITEM NUMBER

Nomenclature

PUMP FUEL SAMPLER -82829/4P156-3

1 not installed4

HF AMPLIFIER - AM-7531/URC1 not installed8

MOUNT, IFM AMPLIFIER-MT-6592/ARC

1 not installed42


SECTION II CABINSES BEST


7822971 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


1FM HOMING ANTENNA ASSY - 70600-02017-105

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

Un0

5

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2FIRE EXTINGUISHER - FR23-4-11848

Unt

UUUUUUnt

Unt

Un

Unt

Un1

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


3INTERPHONE CONTROL - C6533/ARC

Unt

UUUUUUnt

Unt

Un

Unt

Un0

10

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


1ADAPTER FUEL DRAIN - 70307-03018-102

Unt

UUUUUUnt

Unt

Un

Unt

Un1

11

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


4LOCK ASSY BLADE TIEDOWN - 70700-20369-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

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

Un0

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

Un1

15

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






7822971 UH-60A



1COVER ASSY OIL COOLER - 70700-20511-041

Unt

UUUUUUnt

Unt

Un

Unt

Un0

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

Un2

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

Un3

20

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


10RESTRAINT SYSTEM - 70500-02153-103

Unt

UUUUUUnt

Unt

Un

Unt

Un10

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


2RESTRAINT SYSTEM - 70500-02156-102

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

Un2

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






7822971 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 BEST7822971 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c



a. ITEM NUMBER

Nomenclature

FIRST AID KIT - 6545-00919-6650

1 not installed5

FIRE EXTINGUISHER - FR23-4-11848

1 one installed6

INTERPHONE CONTROL -C6533/ARC

1 not installed10

LOCK ASSY BLADE TIEDOWN- 70700-20369-041

1 not installed12

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

1 not installed13

PLUG ASSY EXHAUST - HIRSS- 70700-20515-043

1 not installed14

COVER ASSY OIL COOLER -70700-20511-041

1 not installed16

ICS WALK-AROUND CORD -70602-02016-041

1 not installed28


SECTION I COCKPITSES BEST


7822971 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

Un0

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






7822971 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

Un0

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






7822971 UH-60A



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

Unt

UUUUUUnt

Unt

Un

Unt

Un0

35

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER


2CONTROL - C-10604(V)6/ARN-184

Unt

UUUUUUnt

Unt

Un

Unt

Un1

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

Un1

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


1ARMOR WING PANEL - 70500-01152-094

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

Un2

60

1211109.8.7.6.5.4.3.2.1.CHECK NUMBER






7822971 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

Un2

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 BEST7822971 UH-60A


db c


CHECK CHECK

ba ad

5. VERIFICATION

c



a. ITEM NUMBER

Nomenclature

DISPLACEMENT GYRO - CN-1314/A (9000C)

1 not installed2

GYRO, DIRECTIONAL - CN-998/ASN-43

1 not installed3

MOUNTING FOR KIT-1A/1C/TSEC - MT-3949A/U

1 not installed5

RATE GYRO - TRU-2A/A1 one installed with fogs14

FIRST AID KIT - 6545-00-919-6650

1 not installed24

CONTROL RADIO SET - C-7392/ARN-89

1 not installed35

CONTROL - C-10604(V)6/ARN-184

1 one installed36


PIDMWODATE HRS



RIGHT TIE ROD ASSY 7822971288-012761. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


01-Jun-2005 DO

OB96708224-Sep-2008

1CCAD, CORPC,TX 78419(EO9788)

H-60 SERIE AIRCRAFT, TIE RODASSEMBLY REINSPECTION, UH-60-05-ASAM-08.


Priority Mnt Level



REMARKS

APD LF v1.00DA FORM 2410, JAN 97, IS OBSOLETEDA FORM 2410, MCDS

COMPONENT REMOVAL / REPAIR / INSTALL / GAIN / LOSS RECORD

For use of this form, see DA PAM 738-751; the proponent agency is DCS, G-4

SECTION I - MAINTENANCE ACTION

SECTION II - IDENTIFICATION

INSTALL REMOVE REPAIR GAIN/LOSS

5. MII 6. CAGE CODE 7. LANDINGS 8. NO. OF PREV

O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE

4. SERIAL NUMBER3. PART NUMBER2. NSN1. NOMENCLATURE

21. VERSION

d. OP HOURSc. TTIb. LCF 2a. LCF 1

17. COMPONENT CUMULATIVE COUNT / HOURS16. CONFIG CODE13. METER HRS

18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H

SECTION III - NEXT HIGHER ASSEMBLY (NHA) INSTALL / REMOVE INFORMATION

X

24. NHA PART NUMBER23. NHA NSN22. NHA NOMENCLATURE

25. NHA SERIAL NUMBER 26. NHA HOURS 27. START METER 28. METER HRS

31. WHEN DISCOVERED30. MALFUNCTION CODE29. HISTORY RECORDER SN

32. HISTORY RECORDER READING 33. NHA CUMULATIVE COUNT / HOURS

SECTION IV - GAIN / LOSS / REPAIR / ADMIN INFORMATION

d. OP HRSc. TTIb. LCF 2a. LCF 1d. OP HRSc. TTIb. LCF 2a. LCF 1

44. DATE

47. LOST / SHIPPED TO 48. LOCATION

45. PID AND TELEPHONE NUMBER 46. AKO USER NAME

43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL

38. ACTUAL FAILURE CODE 39. MAINTENANCE LEVEL

MWO

RECAP

40. MANHOURS 41. SRA 42. UIC

37. NEW NSN36. NEW PART NUMBER35. GAIN OR

LOSS CODE

34. INSPECTION ACTION CODES

X

22-Apr-2016 JL1978 912-217-7683 joshua.lines

1 W4QUAAF381

6182 7224

7224 0 0

T700-GE-700 ENGINE ASSY 2840010701003 6035T00G01

GEE306860

CAO01235 9 V

0 0

04A05N 0 0

98391 0 0 1816 5944 0 381

APM880RS4076T64G012915011717761POU ASSY-O/S DRAIN VALVE

5944

UNCLASSIFIED For Official use Only (FOUO)


REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

01-Feb-2016 SH4152 410-436-3831 scott.hash

1 WP37AAF

0 0 0 0 0 0 0 3881

3881 0 0

HELICOPTER, UTILITY 1520012984532 UH-60L

8926162

1 B

0 0 0 0 0

05A02 0 0

78286 0 0 565 3921 0 567

A0071042870150-09100-0431615011061903MAIN ROTOR BLADE ASSY

3921



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

01-Feb-2016 SH4152 410-436-3831 scott.hash

1 WP37AAF

0 0 0 0 0 0 0 3881

3881 0 0


8926162

1 B

0 0 0 0 0

05A02 0 0

78286 0 0 206 3437 0 567


3437



REMARKS

DAMAGED IN SHIPMENT








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H








44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

25-Aug-2015 SH4152 410-436-3831 scott.hash

1 WP37AAF

0 0 0 0 0 0 0

0 0

0 0 0 0 0

05A02 0 0

78286 0 0 0 4362 0 924


4362



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

13-Jan-2016 SH4152 410-436-3831 scott.hash

1 WP37AAF

0 0 0 0 0 0 0 5761

5761 0 0

HELICOPTER, UTILITY 1520010350266 UH-60A

8123610

1 O

0 0 0 0 0

05A02 0 0

78286 0 0 232 2968 0 021


2968



0

720

5610.8

7822971 4066.8 4022


UH-60A A26501119 Days


HELICOPTER, UTILITY MAIN TRANSMISSION MODULE Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

OB96708213-Nov-2008NORMALBASELINE0.02485402913-Nov-2008

OB96708226-Nov-2008NORMALROUTINE7.02485402925-Nov-2008

PM88481520-Feb-2009NORMALROUTINE40.02518406211-Feb-2009

PM88481506-Apr-2009NORMALROUTINE80.02558410227-Mar-2009

ED70398726-May-2009NORMALROUTINE120.02598414215-May-2009

PM88481521-Aug-2009ABNORMALROUTINE158.02636418014-Aug-2009

26-Jan-2010NORMALROUTINE199.02724426819-Jan-2010

JT79391229-Sep-2011ABNORMALPOST PH707.03185472918-Sep-2011

CN15469020-Oct-2011NORMALLAB REQUES731.03209475330-Sep-2011

PM88481530-Jul-2012NORMALROUTINE1064.03542508626-Jul-2012



CN15469024-Mar-2014NORMALROUTINE1423.43901.15445.111-Mar-2014

SL13733825-Nov-2015SUBMITTEDBASELINE0.54066.85610.825-Nov-2015

LAB REQUES1.04066.85610.801-Dec-2015

21 AUG 2009. PARTICLE COUNT EXCESSIVE. RESAMPLE AT END OF NEXT FLIGHT DAY/CYCLE. FT BRAGG AOAP LAB. CHRISTOPHER.NINER APG-EA, MD2101018 SEP 2011. SAMPLING TECHNIQUE, PARTICLE COUNT EXCESSIVE. RESAMPLE AT END OF NEXT FLIGHT DAY/CYCLE. FT BRAGG AOAP LAB.CHRISTOPHER.NINER APG-EA, MD 21010

9. REMARKS:



PIDMWODATE HRS



MAIN TRANSMISSION MODULE 7822971A265011191. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


01-May-2002 OT

OB96708224-Sep-2008

1CCAD, CORPC,TX 78419(EP9788)

MAIN MODULE PLANETARYCARRIER ASSEMBLY, UH-60A/EH-60A/UH-60Q SERIES AIRCRAFT

UH-60-02-07MWO:

Priority Mnt Level

04-May-2002 OT

OB96708224-Sep-2008


MAIN MODULE PLANETARYCARRIER ASSEMBLY, UH-60A, EH-60A AND UH-60Q SERIES AIRCRAFT

UH-60-02-08MWO:

Priority Mnt Level

22-May-2002 OT

OB96708224-Sep-2008


MAIN MODULE PLANETARYCARRIER ASSEMBLY, ALL UH-60A,EH-60A AND UH-60Q SERIESAIRCRAFT

UH-60-02-09MWO:

Priority Mnt Level

16-Jun-2003 OU

OB96708224-Sep-2008


MAIN MODULE PLANETARYCARRIER ASSEMBLY RETIREMENETLIFE, ALL UH-60A, EH-60A AND UH-60Q SERIES AIRCRAFT

1-1520-237-20-265MWO:

Priority Mnt Level

10-Nov-2009 OT

RH02608519-Oct-2009

1AASF MDARNGALL H-60 SERIES AIRCRAFTREDESIGNED PLANETARY GEARCARRIER RETIREMENT LIFE

H-60-10-AMAM-02MWO:

Priority Mnt Level

21-Mar-2013 FM

ED70398722-Mar-2013


H-60-13-ASAM-04MWO:

Priority Mnt Level

26-Mar-2014 FM

TS02689116-Apr-2014

2AASF MDARNGMAIN TRANSMISSION FILTER BOWLAND CHIP DETECTOR ATTACHMENTHARDWARE REPLACEMENT.

H-60-14-AMAM-09MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 7822971D001011021. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Sep-2012 FM

JA58064112-Sep-2012

0.51109TH TASMGALL H-60 SERIES AIRCRAFT, MAINROTOR SPINDLE SUB-COMPONENTTRACKING REQUIREMENTS

H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

RH02608526-Feb-2013

0.2AASF, MDARNGPERFORM ONE-TIME INSPECTIONFOR SUSPECT MAIN ROTORSPINDLE ANTI-FLAP BRACKETASSEMBLIES

H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 7822971B001002901. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Sep-2012 FM

JA58064112-Sep-2012


H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

RH02608526-Feb-2013


H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SPINDLE ASSY 7822971A001059051. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


05-Sep-2012 FM

JA58064112-Sep-2012


H-60-12-AMAM-16MWO:

Priority Mnt Level

26-Feb-2013 FM

RH02608526-Feb-2013


H-60-13-ASAM-03MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR SHAFT EXTENDER 7822971C286-003751. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


22-Jan-1997 OM

OB96708218-Sep-2008

1CCAD, CORPC,TX 78419(WH0217)

ALL H-60 AIRCRAFT WITH THE MAINROTOR SHAFT EXTENSIONASSEMBLY, P/N 70351-08186-043,MANUFACTURED BY FENNMANUFACTURING COMPANY (CAGECODE 82001) OR THE PURDYCORPORATION (CAGE CODE 15152)


Priority Mnt Level

01-Oct-1997 OM

OB96708218-Sep-2008

1CCAD, CORPC,TX 78419(WH0217)

ALL H-60 AIRCRAFT, MAIN ROTORSHAFT EXTENSION ASSEMBLY, P/N70351-08186-043 MANUFACTUREDBY FENN MANUFACTURINGCOMPANY (CAGE CODE 82001) ORTHE PURDY CORPORATION (CAGECODE 15152)


Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR PRIMARY SERVO 7822971B303060951. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


10-Mar-1998 OM

OB96708212-Nov-2008


ALL H-60 AIRCRAFT, LOOSE HUCKBOLTS ON OVERHAULED PRIMARYSERVOS, YAW BOOST SERVOS,COLLECTIVE BOOST SERVOS ANDTAIL ROTOR SERVOS


Priority Mnt Level

03-Mar-2000 OR

OB96708212-Nov-2008


INSPECTION AND REMOVAL OFSUSPECT PRIMARY SERVOASSEMBLIES ALL H-60 AIRCRAFT

1-1520-237-20-217MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR PRIMARY SERVO 7822971B303023321. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


10-Mar-1998 OM

OB96708212-Nov-2008




Priority Mnt Level

03-Mar-2000 OR

OB96708212-Nov-2008



1-1520-237-20-217MWO:

Priority Mnt Level



PIDMWODATE HRS



MAIN ROTOR PRIMARY SERVO 7822971B30300913B1. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


10-Mar-1998 OM

OB96708212-Nov-2008

1CCAC, CORPC,TX 78419



Priority Mnt Level

03-Mar-2000 OR

OB96708212-Nov-2008



1-1520-237-20-217MWO:

Priority Mnt Level



360

360

5445.1

7822971 2854.8 4022


UH-60A A005-02324 Days


HELICOPTER, UTILITY INTERMEDIATE GEARBOX Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

OB96708213-Nov-2008NORMALBASELINE7.01273402913-Nov-2008


PM88481520-Feb-2009NORMALROUTINE40.01306406211-Feb-2009

PM88481506-Apr-2009NORMALROUTINE80.01346410227-Mar-2009

ED70398726-May-2009NORMALROUTINE120.01386414215-May-2009

PM88481521-Aug-2009ABNORMALROUTINE158.01424418014-Aug-2009

26-Jan-2010NORMALROUTINE199.01465422119-Jan-2010

DW15690619-Jan-2011NORMALROUTINE358.01624438011-Jan-2011

JT79391229-Sep-2011ABNORMALPOST PH707.01973472918-Sep-2011

CN15469020-Oct-2011NORMALLAB REQUES731.01997475330-Sep-2011



ED70398728-Oct-2013NORMALROUTINE1386.02652540822-Oct-2013

CN15469024-Mar-2014NORMALROUTINE1423.42689.15445.112-Mar-2014

CN15469006-Apr-2015NORMALROUTINE91.12780.25536.211-Mar-2015

21 AUG 2009. WATER EXCEEDS PPM LIMIT. RESAMPLE AT END OF NEXT FLIGHT DAY/CYCLE. FT BRAGG AOAP LAB. CHRISTOPHER.NINER APG-EA, MD2101027 SEP 2011. WATER EXCEEDS PPM LIMIT. RESAMPLE AT END OF NEXT FLIGHT DAY/CYCLE. FT BRAGG AOAP LAB. CHRISTOPHER.NINER APG-EA, MD21010

9. REMARKS:



PIDMWODATE HRS



INTERMEDIATE GEARBOX 7822971A005-023241. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


28-Oct-2011 OT

RH02608528-Oct-2011

0.1AASF MDARNGTAIL ROTOR INTERMEDIATEGEARBOX SUSPECT DEFECT INGEARBOXS WITH LESS 50 TSN ORTSLR.

H-60-12-AMAM-02MWO:

Priority Mnt Level

21-Mar-2013 FM

ED70398722-Mar-2013


H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



INPUT MODULE 7822971A264036331. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


02-Aug-2000 OT

OB96708224-Sep-2008


ALL H-60 SERIES AIRCRAFT,REMOVAL OF INPUT MODULE GEARBOX ASSEMBLIESWITHPOTENTIALLY CRACKED BEVELGEARS

UH-60-00-02MWO:

Priority Mnt Level

21-Mar-2013 CM

ED70398722-Mar-2013

1AASF MDARNGH-60 SERIES AIRCRAFT, PLASTICMEDIA BLAST (PMB) AND OXIDEFLAKE RESIDUE H-60-13-ASAM-04

H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



INPUT MODULE 7822971A264024911. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


02-Aug-2000 OT

OB96708224-Sep-2008


ALL H-60 SERIES AIRCRAFT,REMOVAL OF INPUT MODULE GEARBOX ASSEMBLIESWITHPOTENTIALLY CRACKED BEVELGEARS

UH-60-00-02MWO:

Priority Mnt Level

21-Mar-2013 CM

ED70398722-Mar-2013

1AASF MDARNGH-60 SERIES AIRCRAFT, PLASTICMEDIA BLAST (PMB) AND OXIDEFLAKE RESIDUE H-60-13-ASAM-04

H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



HUB, M/R ROTOR ASSY 7822971D308000111. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


30-Dec-2013 FM

ED70398702-Jan-2014

0.5AASF MDARNGMAIN ROTOR HUB ASSEMBLYH-60-14-ASAM-04MWO:

Priority Mnt Level



REMARKS








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

04-Dec-2015 DR6695 410-436-4191

0 WUAXC0F

5239

5239


8926131

4 G

19E05C 0

80063 0 262 262 0 281

108EEA30605915841012459093INDICATOR,HEIGHT

262




CAO01519

78229716035T00G01ENGINE ASSY, TURBINEGE-E-306443

4864

4864

25716

25716

14809

14809

3232

3232

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

T700-GE-700

**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

10-May-2016 2/12

04A 6035T00G01 ENGINE ASSY, TURBINE GE-E-306443

434825429127082963

279227103113731041GE-C-7074326035T02G01COLD SECTIONMODULE

COND

COND

0000

0000GGMR61056039T58G02COMBUSTION LINER

COND

COND

434825429127082963

121771294146872MRS083226055T20G05MTCHDROTOR/STATOR ASSY

COND

COND

2513000

4622000AMDA00815043T24G14STAGE 1 NOZZLEASSEMBLY

COND

COND

393424912116662766

558316821113583117GE-L-0061586064T98G01POWER TURBINEMODULE

COND

COND

0000

0000GE-D-0064436035T01G01ACCESSORY MODULE

COND

COND

2219000

2973000SUSJ39216034T62P13PARTICLESEPARATOR BLOWER

COND

COND

4864000

4283000133499044046T52G39FUEL CONTROL

COND

COND

3447000

1391000APM588RT4076T64G01POU ASSY-O/S DRAINVALVE

COND

COND

4348000

5372000ECD005314046T29G13ELECTRICALCONTROL UNIT

COND

COND

0000

0000CAO015194046T26G03HISTORY RECORDER

COND

COND

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

OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


10-May-2016 3/12


2512000

778000UDC059174046T25G01OIL COOLER

COND

COND

2895000

0000COMH68864046T28G14ANTI-ICE VALVE

COND

COND

14. SIGNIFICANT HISTORICAL DATA



CAO01519

GE-E-3064436035T02G01COLD SECTION MODULEGE-C-707432

2614

2792

25429

27103

12708

11373

2963

1041

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




OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


10-May-2016 5/12

04A01 6035T02G01 COLD SECTION MODULE GE-C-707432

278826924113601038

180864057930870SAPT44425056T66G02POWER TAKE OFFASSEMBLY

COND

COND

278826924113601038

278826924113601038GLH234896035T77G19COMPRESSORROTOR ASSEMBLY

COND

COND

278826924113601038

0000GATHWN256035T88P07GAS GENERATORTURBINE SHAFT

13610

11000

278826924113601038

0000WESR42635036T95P01INNER BALANCEPISTON SEAL

COND

COND

278826924113601038

0000MLEWF6876035T79P04COMPRESSORDISCHARGE SEAL

COND

COND

278826924113601038

0000FIAAW67F6035T83P01COMPRESSOR REARSHAFT

7610

5000

278826924113601038

294262704137VAEA89095044T07P01NO 3 LABYRINTHSEAL

COND

COND

278826924113601038

39031442859041540BIWBN8485035T57P02VORTEX SPOILER

COND

COND

278826924113601038

10799812045552GATHJ0WP5043T04P02TIE ROD,COMPRESSOR

11531

10000

278826924113601038

506917003129102473GAT6907N5066T79P01RING, SPACERCOMPRESSOR

7541

10000

278826924113601038

0000GLHTNNM16055T59P01COMPRESSORIMPELLER

7610

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:


10-May-2016 6/12


278826924113601038

45762044289363263GGA743256039T56G04OUTPUT SHAFTASSEMBLY

COND

COND

278826924113601038

0000GLHTNJFD6032T26G09STAGE 1 BLISK

7610

5000

278826924113601038

0000GLHTNW3W6032T27P08STAGE 2 BLISK

7610

5000

278826924113601038

0000GLHTNW976038T08P04STAGE 3 & 4 BLISK

7610

5000

278826924113601038

0000GLHTP0CW6038T09P04STAGE 5 BLISK

7610

5000

278826924113601038

0000FCAP92916064T35P02NO 3 BALL BEARING

COND

COND

278826924113601038

0000FCAY22846064T15P03NO 4 ROLLERBEARING

COND

COND




CAO01519

GE-C-7074326039T56G04OUTPUT SHAFT ASSEMBLYGGA74325

2614

4580

25429

20621

12708

8949

2963

3266

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:


10-May-2016 8/12

04A01G 6039T56G04 OUTPUT SHAFT ASSEMBLY GGA74325

45762024289363265

0000TMKAFDOV6064T34P01NO 1 BALL BEARING

COND

COND

45762024289363265

0000FCAV66845035T69P02NO 2 ROLLERBEARING

COND

COND




CAO01519

GE-E-3064436055T20G05MTCHD ROTOR/STATORASSY

MRS08322

2614

1217

25429

7129

12708

4146

2963

872

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:


10-May-2016 10/12

04A02B 6055T20G05 MTCHD ROTOR/STATOR ASSY MRS08322

121771294146872

121771294146872GATV38276043T62P02STAGE 1 TURBINEDISK

3897

2500

121771294146872

121771294146872GGA063716039T57G18G/G STATOR ASSY

COND

COND

121771294146872

121771294146872GATV52576043T63P01STAGE 2 TURBINEDISK

3897

2500

121771294146872

23611127210288947MA000206039T53P04STAGE 1 FWDCOOLING PLATE

4253

4000

121771294146872

121771294146872GATU54336039T50P04STAGE 1 REARCOOLING PLATE

5397

4000

121771294146872

121771294146872GATT77556039T52P03STAGE 2 FWDCOOLING PLATE

5397

4000

121771294146872

84250841801436BIWCK3086039T51P03STAGE 2 REARCOOLING PLATE

4272

2500

121771294146872

121771294146872GGA083226039T54G13G/G ROTORASSEMBLY

COND

COND




CAO01519

GE-E-3064436064T98G01POWER TURBINE MODULEGE-L-006158

2200

5583

24912

16821

11666

11358

2766

3117

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:


10-May-2016 12/12

04A03 6064T98G01 POWER TURBINE MODULE GE-L-006158

558116742113523115

558116742113523115GGA080245043T75G07POWER TURBINEROTOR

COND

COND

558116742113523115

33101381683631945GATKR7576038T32P01STAGE 3 TURBINEDISC

3888

5000

558116742113523115

33101381683631945GATNE5826038T34P05STAGE 4 TURBINEDISC

3888

5000

558116742113523115

0000GATHRGE25125T92G01POWER TURBINESHAFT

7198

5000

558116742113523115

0000TMKAGKCA5034T27P01NO 5 ROLLERBEARING ALT

COND

COND

558116742113523115

3382833155131623MABU07916064T36P01NO 6 BALL BEARING

COND

COND




CAO01335

78229716035T00G01ENGINE ASSY, TURBINEGE-E-306353

5917

5747

31621

23604

12328

13443

3627

3267

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:


10-May-2016 2/8


37662977194352884

35921700585432284GE-C-0076086035T02G01COLD SECTIONMODULE

COND

COND

37662977194352884

3458000GGMV52966039T58G02COMBUSTION LINER

COND

COND

37662977194352884

2608000AMDA01295043T24G14STAGE 1 NOZZLEASSEMBLY

COND

COND

37662977194352884

1651412843371297GE-L-0068436064T98G01POWER TURBINEMODULE

COND

COND

37662977194352884

3597000GE-D-0070116035T01G01ACCESSORY MODULE

COND

COND

37662977194352884

2655000SUSJ55406034T62P13PARTICLESEPARATOR BLOWER

COND

COND

56152977194352884

1609000WYG549084046T52G39FUEL CONTROL

COND

COND

56802977194352884

2972000EMDE05494046T29G13ELECTRICALCONTROL UNIT

COND

COND

37662977194352884

359521754105502524CAO013354046T26G03HISTORY RECORDER

COND

COND

37662977194352884

3720000UDC052634046T25G01OIL COOLER

COND

COND

37662977194352884

0000COMH92174046T28G14ANTI-ICE VALVE

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:


10-May-2016 3/8




CAO01335

GE-E-3063536035T02G01COLD SECTION MODULEGE-C-007608

3595

3592

21754

17005

10550

8543

2524

2284

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




OP HRSd.

T/T Ic.

LCF-2

b.

a.

LCF-1(Histrcdrhr)

13.REPLACE-MENTDUE

MENTLIFE

REPLACE-


11.

O/H OR

10.


8.

ReportDate:


10-May-2016 5/8


35921700585432284

26091613647081513AGRA30515056T66G02POWER TAKE OFFASSEMBLY

COND

COND

35921700585432284

35921700585432284GLB003496035T77G10COMPRESSORROTOR ASSEMBLY

COND

COND

35921700585432284

33281050566691869GATW47946035T88P03GAS GENERATORTURBINE SHAFT

11267

11000

35921050566691869

0000WESN53755036T95P01INNER BALANCEPISTON SEAL

COND

COND

35921050566691869

0000MMTF56036035T79P04COMPRESSORDISCHARGE SEAL

COND

COND

35921050566691869

2803282231971288GATSF1526035T83P01COMPRESSOR REARSHAFT

5792

5000

35921050566691869

0000VAEA95175044T07P01NO 3 LABYRINTHSEAL

COND

COND

35921050566691869

1465188054903663FMC006725035T57P02VORTEX SPOILER

COND

COND

35921050566691869

2571331829143GATHG9DN5043T04P02TIE ROD,COMPRESSOR

13338

10000

35921050566691869

2571331829143BJWE61405066T79P01RING, SPACERCOMPRESSOR

13338

10000

35921050566691869

0000GLHTJD696055T59P01COMPRESSORIMPELLER

8595

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:


10-May-2016 6/8


35921050566691869

0000GLHTJMP56032T26G09STAGE 1 BLISK

8595

5000

35921050566691869

0000GLHTJ7K16032T27P08STAGE 2 BLISK

8595

5000

35921050566691869

0000GLHTJT4F6038T08P04STAGE 3 & 4 BLISK

8595

5000

35921050566691869

0000GLHTK02F6038T09P04STAGE 5 BLISK

8595

5000

35921050566691869

0000FCAL76096064T35P02NO 3 BALL BEARING

COND

COND

35921050566691869

5187198FCAG93086064T15P03NO 4 ROLLERBEARING

COND

COND




CAO01335

GE-E-3063536064T98G01POWER TURBINE MODULEGE-L-006843

3595

1651

21754

4128

10550

4337

2524

1297

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:


10-May-2016 8/8

04A03 6064T98G01 POWER TURBINE MODULE GE-L-006843

1651412843371297

1651412843371297GGA093535043T75G07POWER TURBINEROTOR

COND

COND

1651412843371297

1651412843371297GATEF1286038T32P01STAGE 3 TURBINEDISC

6944

5000

1651412843371297

1651412843371297GATEB0026038T34P03STAGE 4 TURBINEDISC

6944

5000

1651412843371297

19574956175GATHARE55125T92G01POWER TURBINESHAFT

8400

5000

1651412843371297

0000FCAL89415034T27P02NO 5 ROLLERBEARING

COND

COND

1651412843371297

0000FCAL79876064T36P02NO 6 BALL BEARING

COND

COND



PIDMWODATE HRS



DRIVESHAFT ASSY SECT II 7822971WG30011-001851. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


16-Nov-2001 OT

OB96708211-Jul-2008

1CCAD(R5847)

ALL H- 60 SERIES AIRCRAFT,INSPECTION FOR IMPROPER ORUNINSTALLED HARDWARE ON THEOIL COOLER FAN SHAFT ASSEMBLYFORWARD MOUNT (PART NUMBER70361-03009-047)

UH-60-02-01MWO:

Priority Mnt Level



PIDMWODATE HRS



7822971UH-60AHELICOPTER, UTILITY

3. AIRCRAFT SERIAL NUMBER2. MODEL1. NOMENCLATURE


DN30-Apr-1997

DYN COPR OLRKILEEN, TX(NM8992)

3201-Dec-2000

CIV CONTROL ,QUALITY

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

1-1520-237-50-56MWO:

Mnt LevelPriority

DN01-Oct-1982

LSSI (AV4588) 2801-Oct-1982


INCORPORATION OF A ENGINEPRIME/BOOST SYSTEM (UH-60AHELICOPTERS)

55-1520-237-50-7MWO:

Mnt LevelPriority

DN26-Mar-1984

LSSI (AV4588) 601-Oct-1983


INCORPORATION OF IMPROVEDDROOP STOP CAM ASSEMBLIES (UH-60A HELICOPTERS)

55-1520-237-50-16MWO:

Mnt LevelPriority

DN26-Mar-1984

LSSI (AV4588) 401-Oct-1985


BLADE DE-ICE CHECKOUT APU (UH-60A HELICOPTERS)

55-1520-237-50-4MWO:

Mnt LevelPriority

DN01-Oct-1991

LSSI (AV43588) 301-Oct-1989


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

1-1520-237-50-54MWO:

Mnt LevelPriority

DN01-Sep-1986

LSSI (AV4588) 133101-Sep-1987


INCORPORATION OF ANVISCOMPATIBLE LIGHTING SYSTEM

55-1520-237-50-20MWO:

Mnt LevelPriority

DN24-Oct-1984

SIKORSKY(AV4588)

1003-Oct-1984


MAIN ROTOR DAMPER CABLES55-1520-237-50-17MWO:

Mnt LevelPriority

DN28-Oct-1996

CCAD (XT4634) 806-Jan-1999


MODIFICATION OF CHIP DETECTORWIRING FOR UH-60A HELICOPTERS

1-1520-237-50-26MWO:

Mnt LevelPriority

DM15-Nov-1989

LSSI/OLR(AV4588)

1906-Sep-1990


MODIFICATION OF DOWEL PINRETENTION MAIN GEARBOX

55-1520-237-50-43MWO:

Mnt LevelPriority

DN16-Oct-1989

LSSI, FT.EUSTIS, VA.(AV4588)

2006-Sep-1990


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

55-1520-237-50-49MWO:

Mnt LevelPriority


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

PIDMWODATE HRS






DN17-Jan-1989

LSSI/OLR(AV4588)

207-Aug-1989


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

55-1520-237-50-52MWO:

Mnt LevelPriority

DU10-Aug-1987

LSSI (AV4588) 808-Oct-1987


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

55-1520-237-50-46MWO:

Mnt LevelPriority

DN05-Oct-1994

DYNCORP(TH2243)

18409-Dec-1998


INSTALLATION OF HEADS UP DISPLAY(HUD) AN/AVS-7 FOR UH-60AHELICOPTERS AND UH-60LHELICOPTERS

1-1520-237-50-62MWO:

Mnt LevelPriority

DN31-Oct-1996

DYNCORP(TH2243)

3509-Dec-1998


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

1-1520-237-50-74MWO:

Mnt LevelPriority

DR08-Nov-1996

DYNCORP(TH2243)

17809-Dec-1998


INSTALLATION OF AN/ASN-128BDOPPLER/GPS NAVIGATION SYSTEMIN UH-60A/L HELICOPTER

1-1520-237-50-75MWO:

Mnt LevelPriority

DN08-Nov-1984

SIKORSKY(AV4588)

1010-Apr-1984


STAB. GROUND55-1520-237-50-29MWO:

Mnt LevelPriority

DN24-Oct-1984

SIKORSKY(AV4588)

010-Apr-1985


MIXER RET55-1520-237-50-27MWO:

Mnt LevelPriority

DN08-Nov-1984

SIKORSKY(AV4588)

3010-Apr-1985


KICK PLATES55-1520-237-50-10MWO:

Mnt LevelPriority

DN08-Nov-1984

SIKORSKY(AV4588)

1010-Apr-1985


RES. HOIST PROVISIONS55-1520-237-50-9MWO:

Mnt LevelPriority

DU13-Jun-1985

LSSI (AV4588) 410-Aug-1985


MODIFICATION OF IMPROVED MAINROTOR-TAIL ROTOR PITCH CONTROLROD BOLTS (UH-60A HELICOPTERS)

55-1520-237-50-31MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN08-Nov-1984

SIKORSKY(AV4588)

1010-May-1985


CHAFF DISP.55-1520-237-50-30MWO:

Mnt LevelPriority

DN24-Mar-1988

LSSI, FT.EUSTIS, VA.(AV4588)

6711-May-1987


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

55-1520-237-50-47MWO:

Mnt LevelPriority

DN30-Apr-1987

CCAD, CORPC,TX 78419

112-Nov-2008

CIV BANZACA,OPHELIA

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

55-1520-237-50-24MWO:

Mnt LevelPriority

DN04-Mar-1999


112-Nov-2008

CIV BANZACA,OPHELIA

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

1-1520-237-50-74 C1MWO:

Mnt LevelPriority

DN02-Aug-2001


112-Nov-2008

CIV BANZACA,OPHELIA

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

1-1520-237-50-56 C5MWO:

Mnt LevelPriority

DN01-Jun-1988


112-Nov-2008

CIV BANZACA,OPHELIA

CRASHWORTHY ARMORED CREWSEATS/IMPROVED SEATINGRESTRAINT SYSTEM

55-1680-237-50-1MWO:

Mnt LevelPriority

FR18-Nov-2009

YULISTA AVN 1413-Apr-2011

CIV JOHNSON,JON B

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF M4 GUNMOUNT ON THE UH-60A/L/M MODELBROOM CLOSET

1-1520-237-20-95MWO:

Mnt LevelPriority

DR29-Nov-2010

YULISTA AVN 1413-Apr-2011

CIV JOHNSON,JON B

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE M4 GUNMOUNT OF THE UH-60A/L MODELVERITCAL MOUNTS

1-1520-237-50-106MWO:

Mnt LevelPriority

DN15-Jan-1989

LSSI (AV4588) 1213-Aug-1993


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

1-5945-237-50-1MWO:

Mnt LevelPriority



PIDMWODATE HRS






DM18-Feb-2008

L-3 VERTEX 5014-Sep-2011

SGT ARRIOLA,LEX C

INSTALLATION OF T700-GE-701DENGINES AND SUPPORTCOMPONENTS ON UH-60A AND HH-60A AIRCRAFT

1-1520-237-20-3MWO:

Mnt LevelPriority

OO25-Jan-2007


SGT ARRIOLA,LEX C

MODIFICATION INSTRUCTIONS FORDUAL INSTALLATION OF ATTITUDEHEADING REFERENCE UNITS (AHRU)ON THE UH-60A/L HELICOPTER

1-1520-237-20-94 (FOGS)MWO:

Mnt LevelPriority

FR23-Jun-2008


SGT ARRIOLA,LEX C

INSTALLATION OF AUTO RELIGHT &TRANSIENT DROOP IMPROVEMENTFOR T700-GE-701D ENGINES ON UH-60A/HH-60A AIRCRAFT

MWO 1-1520-237-30-3MWO:

Mnt LevelPriority

DN01-Oct-1990

LSSI/OLR(AV4588)

715-Apr-1990


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

55-1520-237-50-39MWO:

Mnt LevelPriority

DN15-May-1984

LSSI (AV4588) 19615-Jan-1985


INCORPORATION OF WATERINTEGRITY IMPROVEMENTS (UH-60AHELICOPTERS)

55-1520-237-50-18MWO:

Mnt LevelPriority

DN26-Mar-1984

LSSI (AV4588) 4815-Jan-1985


INCORPORATION OF BLADE DEICEFAULT MONITOR FIXED PROVISIONS

55-1520-237-50-2MWO:

Mnt LevelPriority

DN26-Mar-1984

LSSI (AV4588) 415-Jan-1985


IMPROVED ANTI-ICING MODULATINGVALVE SENSE LINE INSTALLATION(UH-60A HELICOPTERS)

55-1520-237-50-3MWO:

Mnt LevelPriority

DN26-Mar-1984

LSSI (AV4588) 19815-Jan-1985


MODIFICATION TO INSTALL ROTORBLADE DE-ICE KIT (UH-60AHELICOPTERS)

55-1520-237-50-5MWO:

Mnt LevelPriority

DM01-Apr-1985

LSSI (AV4588) 15015-Jun-1985


INCORPORATION OF FUEL BOOSTPUMP SYSTEM

55-1520-237-50-25MWO:

Mnt LevelPriority



PIDMWODATE HRS






DM18-Apr-1988

CCAD,CORPC,TX. (AV4588)

115-May-1988


INSTALLATION OF IMPROVEDCARTRIDGE ACTUATED DEVICE

55-4030-237-50-1MWO:

Mnt LevelPriority

FN13-Jun-2013

AASF MDARNG 416-APR-2014

SGT HAMILTON,RICHARD A

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

DR15-Jul-1985

LSSI (AV4588) 1217-Apr-1986


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

55-1520-237-50-34MWO:

Mnt LevelPriority

DU30-Nov-1983

AVN OFFICE FT.EUSTIS, VA(AV4588)

118-Jan-1984


CARGO HOOK EXTERNAL SPRINGRETROFIT KIT

55-1520-237-50-28MWO:

Mnt LevelPriority

DR04-Jun-2001

DYN CORP OLRKILEEN, TX(JC8143)

30018-Jun-2001


INSTALLATION OF HFCOMMUNICATION SYSTEM AN/ARC-220(V) AND TSEC/KY-100 IN UH60/LHELICOPTER NSN 1520-01-035-0266UH-60A NSN 1520-01-298-4532 UH-60L

1-1520-237-50-76MWO:

Mnt LevelPriority

DN01-Mar-1989

LSSI (AV4588) 519-Dec-1990


INCORPORATION OF IMPROVEDTIEDOWN FITTINGS

1-1520-237-50-53MWO:

Mnt LevelPriority

DO04-Apr-1986

LSSI (AV4588) 519-Dec-1990


INSTALLATION OF MODIFIED OILSHIELDS

55-1520-237-50-53MWO:

Mnt LevelPriority

DN25-May-1983

LSSI (AV4588) 120-Jun-1994


MODIFICATION OF MAIN ROTORSERVO INPUT PUSHROD ASSEMBLY(UH-60A HELICOPTERS)

55-1520-237-50-13MWO:

Mnt LevelPriority

DR13-Apr-2001

DYNCORP(XJ1803)

8020-Jun-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

1-1520-237-50-77MWO:

Mnt LevelPriority



PIDMWODATE HRS






FR20-Mar-2006


120-Oct-2008

CIV BANZACA,OPHELIA

INSTALLATION OF UH-60, EH-60, ANDHH-60 SERIES HELICOPTERS FORBODY PLUG CORROSIONINSPECTION.

1-1520-237-23-10MWO:

Mnt LevelPriority

FR20-May-2006


120-Oct-2008

CIV BANZACA,OPHELIA

FUEL CELL CORROSION INSPECTIONOF UH-60, EH-60, AND HH-60 SERIESHELICOPTERS.

1-1520-237-23-9MWO:

Mnt LevelPriority

DM12-Aug-1983

LSSI (AV4588) 4822-Aug-1984


UPPER CARGO TRACK ASSEMBLY55-1520-237-50-12MWO:

Mnt LevelPriority

DN17-Jun-1989


622-Dec-1987


INCOROPORATION OF EXHAUSTEXTENDER DOUBLERS

55-1520-237-50-51MWO:

Mnt LevelPriority

DN04-Apr-1994


296922-Dec-1997


INCORPORATION OF UH-60AREFURBISHMENT/STANDARDIZATIONPROGRAM

1-1520-237-55-7MWO:

Mnt LevelPriority

DN07-Mar-1995


6122-Dec-1997


INCORPORATION OF IMPROVEDAIRSPEED SYSTEM (UH-60AHELICOPTERS)

1-1520-237-50-22MWO:

Mnt LevelPriority

DN01-May-1994

CCAD, CORPC,TX, (AV4588)

12822-Dec-1997


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

1-1520-237-50-66MWO:

Mnt LevelPriority

DN01-Feb-1993

LSSI (AV4588) 40022-Dec-1997


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

1-1520-237-50-69MWO:

Mnt LevelPriority

DN29-Jul-1994


18622-Dec-1997


INSTALLATION OF ELECTRICALLYHEATED GLASS CENTER WINDSHIELD(UH-60A HELICOPTER)

1-1520-237-50-70MWO:

Mnt LevelPriority



PIDMWODATE HRS






DN31-May-1996


3022-Dec-1997


INSTALLATION OF STABILATORINSPECTION PORTS (UH-60AHELICOPTER)

1-1520-237-50-72MWO:

Mnt LevelPriority

DN30-Sep-1987


51522-Dec-1997


INSTALLATION OF CRASHWORTHYFLIGHT DATA RECORDER ANDSTATUS INDICATOR LIGHT

55-1520-237-55-3MWO:

Mnt LevelPriority

DR11-Aug-2000

DYN CORP OLRKILEEN, TX(AV4588)

322-Nov-2000


INSTALLATION OF THEPILOT/COPILOT SEATS MA-16(IMPROVED) INERTIA REEL IN ALL UH-60 HELICOPTERS

1-1520-237-50-79MWO:

Mnt LevelPriority

DN23-Jan-1989


3023-Jan-1989


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

55-1520-237-50-44MWO:

Mnt LevelPriority

DN15-Dec-1984

LSSI (AV4588) 225-Mar-1985


MODIFICATION OF MAIN ROTORSLIDING COVER (UH-60AHELICOPTERS)

55-1520-237-50-32MWO:

Mnt LevelPriority

DM11-Oct-1983

LSSI (AV4588) 125-Mar-1985


IMPROVED CARGO HOOK KEEPERINSTALLATION FOR UH-60AHELICOPTERS

55-1520-237-50-15MWO:

Mnt LevelPriority

DN09-Jun-1988

LSSI/OLR(AV4588)

225-Oct-1989


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

55-1520-237-50-42MWO:

Mnt LevelPriority

DU30-Mar-1987

LSSI (AV4588) 0.527-Feb-1987


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

55-1520-237-50-36MWO:

Mnt LevelPriority

DU31-May-1995


2427-Jul-1996


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

1-1520-237-50-73MWO:

Mnt LevelPriority



PIDMWODATE HRS






DR21-Jun-2004

CSC FT HOODAFMA

7528-May-2010

CIV SOWA ,BRUCE M

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE AN/APX-118 TRANSPONDER MODE STRANSPONDER (CXP) ON UH-60A/LAIRCRAFT (NSN 1520-01-035-0266)(NSN 1520-01-298-4532)

1-1520-237-50-84MWO:

Mnt LevelPriority

DR18-May-2007

CSC FT HOODAFMA

9428-May-2010

CIV SOWA ,BRUCE M

MODIFICATION INSTRUCTIONS FORTHE INSTALLATION OF THE AIRWARRIOR MICROCLIMATE COOLINGSYSTEM AND MASK BLOWER WIRINGASSEMBLY ON THE UH-60A/L

1-1520-237-50-85 (D)MWO:

Mnt LevelPriority

DR24-Apr-2008

CSC FT HOODAFMA

21528-May-2010

CIV SOWA ,BRUCE M

INSTALLATION INSTRUCTIONS FORTHE BLUE FORCE TRACKING SYSTEMON THE UH60A/L AIRCRAFT (1520-02-035-0266) (1520-01-298-4532).

1-1520-237-50-85BFT60-001.MWO:

Mnt LevelPriority

CR03-Mar-2006

CSC FT HOODAFMA

36128-May-2010

CIV SOWA ,BRUCE M

INSTRUCTION OF ENGINE INLETBARRIER FILTER (IBF) SYSTEM FIXEDPROVISIONS ON UH-60-A/L/Q HH-60-LHELICOPTERS

1-1520-237-50-90-EIBF (D)MWO:

Mnt LevelPriority

DR10-Oct-2008

CSC FT HOODAFMA

25028-May-2010

CIV SOWA ,BRUCE M

AN/AAR-57 IMPROVEDCOUNTERMEASURE DISPENSERSYSTEM ICMD COMMON MISSILEWARNING SYSTEM CMWSMODERNIZATION P3I ON THE UH-60A/L

1-1520-237-50-97-REVCMWO:

Mnt LevelPriority

DR01-Jul-2008

CSC FT HOODAFMA

7628-May-2010

CIV SOWA ,BRUCE M

MODIFICATION INSTRUCTION FORTHE INSTALLATION OF CMWS FIFTHSENSOR ON UH-60A AND UH-60LHELICOPTERS

1-1520-237-50-99 (D)MWO:

Mnt LevelPriority

DR21-Jul-2006

CSC FT HOODAFMA

90028-May-2010

CIV SOWA ,BRUCE M

INSTALLATION OF THE AN/AAR-57(V)3COMMON MISSILE WARNING SYSTEM(CMWS) AND IMPROVEDCOUNTERMEASURES DISPENSER(ICMD) SYSTEM MODIFICATION.

1-1520-237-50-CMWS CH 4MWO:

Mnt LevelPriority



PIDMWODATE HRS






DR01-Jul-2008

CSC FT HOODAFMA

3928-May-2010

CIV SOWA ,BRUCE M

ELECTRONIC DATA MANAGEMENT(EDM) SYSTEM FOR BLUE FORCETRACKING (BFT) INSTALLATIONINSTRUCTION LSF01106

1-1520-237-50-EDM REV PMWO:

Mnt LevelPriority

KR09-Jun-2006

CSC FT HOODAFMA

91228-May-2010

CIV SOWA ,BRUCE M

INSTALLATION OF INTEGRATEDVEHICLE HEALTH MANAGEMENTSYSTEM (IVHMS) HEALTH USAGEMANAGEMENT SYSTEM (HUMS) FORUH-60 A/L HELICOPTERS

1-1520-237-50-100 (IVHMS)MWO:

Mnt LevelPriority

DR06-Jun-2003

CSC FT HOODAFMA

1028-May-2010

CIV SOWA ,BRUCE M

INSTALLATION OF BALLISTICPROTECTION SYSTEM (BPS) ON UH-60A MEDIVAC HELICOPTERS

ISAQ 108-UH60-BPSMWO:

Mnt LevelPriority

DR30-Apr-1991

LSSI (AV4588) 13929-Apr-1993


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

1-1520-237-50-63MWO:

Mnt LevelPriority

OE30-Apr-1986

AVN. CIV. FT.EUSTIS, VA.(AV4588)

0.530-Apr-1986


RELOCATION OF THE AUTOMATICFLIGHT CONTROL SYSTEM (AFCS)PANEL

55-1520-237-20-1MWO:

Mnt LevelPriority

DM01-Sep-1991

LSSI (AV4588) 231-Jan-1994


IMPROVED ENGINE COWLINGRELEASE HANDLE ASSEMBLY

1-1520-237-50-64MWO:

Mnt LevelPriority

DM15-Jan-1991

LSSI (AV4588) 631-Jan-1994


INCORPORATION OF ENGINEDRIVESHAFT BALANCE PROCEDURE

1-1520-237-50-58MWO:

Mnt LevelPriority

DM22-Feb-1991

LSSI (AV4588) 63831-Jan-1994


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

1-1520-237-50-59MWO:

Mnt LevelPriority

DN15-Nov-1990

LSSI (AV4588) 831-Jan-1994


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

1-1520-237-50-61MWO:

Mnt LevelPriority



365

360

5445.1

7822971 7 0


UH-60A 896124 Days


HELICOPTER, UTILITY AUXILIARY POWER UNIT Hrs


COMPONENT

3.2.SAMPLEEND ITEM

1.


a b

SUBMITTED

c a b



COMPONENTCHANGE

OB96708213-Nov-2008ABNORMALSPECIAL7.01209402913-Nov-2008



ED70398726-May-2009ABNORMALROUTINE120.01209414215-May-2009

04-Jun-2009NORMALSPECIAL127.01209414928-May-2009

DW15690612-Nov-2010NORMALBASELINE0.01209431702-Nov-2010

CN15469020-Oct-2011NORMALROUTINE412.01209472918-Sep-2011



ED70398729-Oct-2013NORMALROUTINE1091.01209540822-Oct-2013

CN15469024-Mar-2015NORMALROUTINE1127.93295445.111-Mar-2014

MG06494329-Apr-2015ABNORMALROUTINE107.9353555310-Apr-2015

22 MAY 2009. INSUFFICIENT AMOUNT OF OIL. RESAMPLE AT END OF NEXT FLIGHT DAY/CYCLE. FT BRAGG AOAP LAB. CHRISTOPHER.NINER APG-EA, MD21010

9. REMARKS:



PIDMWODATE HRS



AUXILIARY POWER UNIT 78229718961241. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


03-May-2006 DR

BS46966529-Oct-2010

30CSC FT HOODAFMA

APU INLET BARRIER FILTERSYSTEM

1-1520-237-50 APU AIBFMWO:

Priority Mnt Level




7822971116305-302AUXILIARY POWER UNIT896124

1209

1209

6837

6837

7

7

2

2

5=


COMPONENT/MODULE1+

PREVIOUS COUNTS OF

4=

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13.REPLACE-MENTDUE

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10.


8.

ReportDate:


05-May-2016 2/2

15B 116305-302 AUXILIARY POWER UNIT 896124

1208683072

0000V42-C79484502902WHEEL,COMPRESSOR

12830

6000

1208683072

0000H2164503991WHEEL, TURBINE

12830

6000


10/7/200812:00:00 AM

1 24MAY07 OVERHAULED APU IAW DMWR 55-2835-209. REPLACEDTURBINE,CARRIER,OUTPUT SHAFT,FUELCONTROL,ALL FILTERS ANDCOUNTER 0/0. MOC COMPLETED AT 6837SSN 1209TSN. RR5649 ESRAFTCKY

OB665754 CCAD, CORPUSCHRISTI

TX 78419-5260

10/29/201012:00:00 AM

1 MWO 1-1520-237-50-AIBF APPLIED AT 0086 APU HRS, 0497 STARTS

BS469665 CSC FT HOOD AFMA KILLEEN TX76543


REMARKS

H-60-15-AMAM-14 COMPLIANCE








O/Hs

9. TIME SINCE

LAST INST

10. TIME SINCE

NEW

11. TIME SINCE

O/H

12. FAIL CODE


21. VERSION



18. POS 19. STARTS

SINCE NEW

14. HSF 15. WUC

20. STARTS

SINCE O/H


X







44. DATE



43. CONTRACT NUMBER

UNSERVICEABLE

SERVICEABLE REPAIR

OVERHAUL


MWO

RECAP



LOSS CODE


X

28-Jul-2015 RH0260 410-436-4191

0 WUAXC0O

5574

5574

HELICOPTER, UTILITY 1520010350266 UH-60A

7822971

1 O

11D11 0

78286 0 488 488 0 998

B3460065170400-08104-0461680011092511AFT WALKING BEAM

488



PIDMWODATE HRS



ACCESSORY MODULE 7822971A258070121. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


21-Mar-2013 FM

ED70398722-Mar-2013


H-60-13-ASAM-04MWO:

Priority Mnt Level



PIDMWODATE HRS



ACCESSORY MODULE 7822971A258-008491. NOMENCLATURE 3. AIRCRAFT SERIAL NUMBER2. COMPONENT SERIAL NUMBER


21-Mar-2013 FM

ED70398722-Mar-2013


H-60-13-ASAM-04MWO:

Priority Mnt Level



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


78229711520010350266 00HELICOPTER, UTILITY

156001095713502C12D

23682368UNK297170219-05001-042TAIL CONE FITTING CCCC COND COND

162001231183103A01

231742033293715570250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001231183103A01

04378BEM163570250-12051-045FWD FIXED GEAR SHOCK CCCC COND COND

162001421089003B01

5774022BMC89070250-13101-044SHOCK ABSORBER (TAIL) CCCC COND COND

165001285302405A01Z YELLOW

6664022A106-0916770106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z BLACK

10004022A10602199A70106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z BLUE

9324022A1060709370106-08100-046DAMPER ASSY, M/R CCCC COND COND

165001285302405A01Z RED

11344022WG106-0267370106-08100-046DAMPER ASSY, M/R CCCC COND COND

531501537465205A02H RED LAG

05086B9411387870103-08108-041SOLID BLADE PIN CCCC COND COND

531501537465205A02H RED LAG


531501537465205A02H YELL LEAD


531501537465205A02H BLUE LEAD


531501537465205A02H BLUE LAG


531501537465205A02H YELL LAG


531501537465205A02H BLK LEAD


531501537465205A02H BLK LAG


161501199764605A03A

3184022015152-142970104-08000-050SWASHPLATE ASSY CCCC COND COND

161501383899206A11 L/H

36674022A258-0084970351-08080-045ACCESSORY MODULE CCCC COND COND

161501383899206A11 R/H

4764022A2580701270351-08080-045ACCESSORY MODULE CCCC COND COND

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

24784022A2650111970351-08100-076MAIN TRANSMISSIONMODULE

CCCC COND COND

161501353382506E R/H

53044022A2640249170351-08001-049INPUT MODULE CCCC COND COND

161501353382506E L/H

12944022A2640363370351-08001-049INPUT MODULE CCCC COND COND

168001074515206F

12664022A005-0232470357-06300-042INTERMEDIATE GEARBOX CCCC COND COND

161501376508906G01

05086A0060448970358-06600-046TAIL ROTOR GEARBOXASSY

CCCC COND COND

161501081277506H06 #1

04022WG30032-00108

70361-03001-045SHAFT ASSY, T/R DRV SEC1

CCCC COND COND

161501158951706H08 #2

04022WG30011-00185

70361-03009-047DRIVESHAFT ASSY SECT II CCCC COND COND

161501158952206H09 #3

04022WG30024-00496

70361-05001-051SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501158952206H09 #4

04022WG30024-00585

70361-05001-051SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501158952206H09 #5

04022WG30024-00605

70361-05001-051SHAFT ASSY, T/R SEC3,4,5

CCCC COND COND

161501083295306H11

27244022A2730106470361-05002-045SHAFT ASSY, T/R DRV SEC6

CCCC COND COND

161501158578806H12

47604022A2740065070361-06002-047SHAFT ASSY, T/R DRV SEC7

CCCC COND COND

432001207722807A01 R/H

2264022232933ABT53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01 BACKUP

4994022255537ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

432001207722807A01 L/H

6584022255542ABR53023-06PUMP MODULE ASSY,HYDRAUL

CCCC COND COND

481001102247307B05A #1

05086207473213850-3-1VALVE, SOLENIOD CCCC COND COND

481001102247307B05A

5883508631953213850-3-1VALVE, SOLENIOD CCCC COND COND

165001250376707B11

04022C4010247470651-03201-104ACCUMULATOR CCCC COND COND

168001342049608B20 L/H

04022554170450-01043-124PANEL INDICATOR (PDU) CCCC COND COND



h

CONDITION ITEMS

kjifdcba g.

RMVL HR


NOMEN

O/HLOCATIONNSN

eAND (ACFTLIFE


REPLACE






168001342049608B20 R/H

04022555470450-01043-124PANEL INDICATOR (PDU) CCCC COND COND

611501114969609A01 R/H

7894022589228B302-8-DMGENERATOR CCCC COND COND

611501114969609A01 L/H

8684022906E28B302-8-DMGENERATOR CCCC COND COND

168001310225911C21

05445TMD04843748112

70400-02300-048MIXER ASSEMBLY CCCC COND COND

168001261204411D25

29385086B2920407770400-06641-117STABILATOR ACTUATOR CCCC COND COND

168001261204411D25

11654022B2920605570400-06641-117STABILATOR ACTUATOR CCCC COND COND

599601547345211D26

0472926866981011445-1STABILATOR AMPLIFIER(DUAL)

CCCC COND COND

299501496368615A04

137454814074504587ENGINE SEQUENCINGUNIT

CCCC COND COND

589501245909019E05A LFT

054081725ASM-C-967292RECEIVER-TRANSMITTERRADAR

CCCC COND COND

660501503528419E06A

0546710250765100-20ATTITUDE HEADINGREFERENCE UNIT

CCCC COND COND

661001490516852A

990402204123479825050-1-001AUTOMAT FLT CONTCOMPUTER

CCCC COND COND

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 COMPONENTS4/910-May-2016

00

156001081924402C15J20331

UNK3489 3691402270209-06051-043TAIL PYLON FITTING 0020000

161501450483405A01A10186

D30800011 0508670103-08112-047HUB, M/R ROTOR ASSY 005100

161501442692605A01I YELLOW10083

A00105905 1403508670102-08200-069MAIN ROTOR SPINDLEASSY

006400

161501442692605A01I BLACK10499

B00100290 987508670102-08200-069MAIN ROTOR SPINDLEASSY

006400

161501442692605A01I BLUE10807

D00101102 679508670102-08200-069MAIN ROTOR SPINDLEASSY

006400

161501442692605A01I11845

D00112206 0544570102-08200-069MAIN ROTOR SPINDLEASSY

006400

161501074515105A01L14248

C286-00375 3774402270351-08186-043MAIN ROTOR SHAFTEXTENDER

0014000

161501127738805A01T18086

R32700423 0508670107-08400-046BIFILAR, M/R ROTORASSY

0013000

161501113818805B0210238

A00904103 5041527970101-31000-043TAIL ROTOR BLADEASSY

0010000

161501113818805B0213261

A00907983 1825508670101-31000-043TAIL ROTOR BLADEASSY

0010000

161501083681206G01B12077

C25700026 3945402270102-11101-042O/B RETENTION PLATE(T/R)

0012000

414101329342806H236542

9E930054SB 3894550270361-03005-107FAN AXIAL 148012520

156001129125607A2413729

B112-07246 4716544570410-02500-049SAS ACTUATOR 0013000

156001129125607A2414826

B112-07307 3260508670410-02500-049SAS ACTUATOR 0013000

161501141753211C237246

23303575 2251508670400-06100-042TAIL ROTOR PITCHCHANGE SHAFT

022160

165001305695411C2512545

B30001503 2833437870410-06520-046SERVO ASSY, TAILROTOR

0011000

165001143122611D0121267

B30300913B 7155402270410-02820-054MAIN ROTOR PRIMARYSERVO

0024400

165001143122611D0124751

B30302332 3671402270410-02820-054MAIN ROTOR PRIMARYSERVO

0024400

165001143122611D0125306

B30306095 3116402270410-02820-054MAIN ROTOR PRIMARYSERVO

0024400

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


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 COMPONENTS5/910-May-2016

00

156001158968511D0413000

34501729 4316431670400-08102-045AFT BELLCRANK 0013000

156001164416111D0521022

E391-02139 0402270400-08112-045AFT TIE ROD SUPTFITTING

0017000

168001164416011D066222

M39200121 0402270400-08111-042AFT TIE ROD ASSY 002200

156001286887011D079486

390-01841 0508670400-08117-049AFT BELLCRANK SPTASSY

004400

304001287243811D0814886

A38003795 1200508670400-08151-061LATERAL SWASHPLATELINK

0011000

168001221286311D0925086

F33704797 0508670400-08166-041LATERAL SERVOBELLCRANK

0020000

156001289269711D1319086

344-02401 0508670400-08115-046LEFT TIE ROD 0014000

156001296948611D147522

288-01276 0402270400-08114-051RIGHT TIE ROD ASSY 003500

168001158965211D1520086

1887 0508670400-08101-046FORWARD BELLCRANK 0015000

156001221261911D1611211

B367-04408 0561170400-08162-042FWD BELLCRANK SPTASSY

005600

SIGNIFICANT HISTORICAL EVENTS7.

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

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 7822971 004. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 6 of 9

10-May-2016

COND COND

156001095713502C12D

23682368TAIL CONE FITTING UNK297170219-05001-042 CCCC

20000 20331

156001081924402C15J

36914022TAIL PYLON FITTING UNK348970209-06051-043 00

COND COND

162001231183103A01

23174203FWD FIXED GEARSHOCK

3293715570250-12051-045 CCCC

COND COND

162001231183103A01


BEM163570250-12051-045 CCCC

COND COND

162001421089003B01

5774022SHOCK ABSORBER(TAIL)

BMC89070250-13101-044 CCCC

5100 10186

161501450483405A01A

05086HUB, M/R ROTOR ASSY D3080001170103-08112-047 00

6400 10083

1615014426926 YELLOW05A01I

14035086MAIN ROTOR SPINDLEASSY

A0010590570102-08200-069 00

6400 10499

1615014426926 BLACK05A01I


B0010029070102-08200-069 00

6400 10807

1615014426926 BLUE05A01I


D0010110270102-08200-069 00

6400 11845

161501442692605A01I


D0011220670102-08200-069 00

14000 14248

161501074515105A01L

37744022MAIN ROTOR SHAFTEXTENDER

C286-0037570351-08186-043 00

13000 18086

161501127738805A01T

05086BIFILAR, M/R ROTORASSY

R3270042370107-08400-046 00

COND COND

1650012853024 YELLOW05A01Z

6664022DAMPER ASSY, M/R A106-0916770106-08100-046 CCCC

COND COND

1650012853024 BLACK05A01Z

10004022DAMPER ASSY, M/R A10602199A70106-08100-046 CCCC

COND COND

1650012853024 BLUE05A01Z

9324022DAMPER ASSY, M/R A1060709370106-08100-046 CCCC

COND COND

1650012853024 RED05A01Z

11344022DAMPER ASSY, M/R WG106-0267370106-08100-046 CCCC

COND COND

5315015374652 RED LAG05A02H

05086SOLID BLADE PIN B9411387870103-08108-041 CCCC

COND COND

5315015374652 RED LAG05A02H


COND COND

5315015374652 YELL LEAD05A02H


COND COND

5315015374652 BLUE LEAD05A02H


COND COND

5315015374652 BLUE LAG05A02H


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 7 of 9

10-May-2016

COND COND

5315015374652 YELL LAG05A02H


COND COND

5315015374652 BLK LEAD05A02H


COND COND

5315015374652 BLK LAG05A02H


COND COND

161501199764605A03A

3184022SWASHPLATE ASSY 015152-142970104-08000-050 CCCC

10000 10238

161501113818805B02

50415279TAIL ROTOR BLADEASSY

A0090410370101-31000-043 00

10000 13261

161501113818805B02

18255086TAIL ROTOR BLADEASSY

A0090798370101-31000-043 00

COND COND

1615013838992 L/H06A11

36674022ACCESSORY MODULE A258-0084970351-08080-045 CCCC

COND COND

1615013838992 R/H06A11

4764022ACCESSORY MODULE A2580701270351-08080-045 CCCC

COND COND

161501503311506A

24784022MAIN TRANSMISSIONMODULE

A2650111970351-08100-076 CCCC

COND COND

1615013533825 R/H06E

53044022INPUT MODULE A2640249170351-08001-049 CCCC

COND COND

1615013533825 L/H06E

12944022INPUT MODULE A2640363370351-08001-049 CCCC

COND COND

168001074515206F

12664022INTERMEDIATEGEARBOX

A005-0232470357-06300-042 CCCC

COND COND

161501376508906G01

05086TAIL ROTOR GEARBOXASSY

A0060448970358-06600-046 CCCC

12000 12077

161501083681206G01B

39454022O/B RETENTION PLATE(T/R)

C2570002670102-11101-042 00

COND COND

1615010812775 #106H06

04022SHAFT ASSY, T/R DRVSEC 1

WG30032-0010870361-03001-045 CCCC

COND COND

1615011589517 #206H08

04022DRIVESHAFT ASSY SECTII

WG30011-0018570361-03009-047 CCCC

COND COND

1615011589522 #306H09

04022SHAFT ASSY, T/R SEC3,4,5

WG30024-0049670361-05001-051 CCCC

COND COND

1615011589522 #406H09


WG30024-0058570361-05001-051 CCCC

COND COND

1615011589522 #506H09


WG30024-0060570361-05001-051 CCCC

COND COND

161501083295306H11


A2730106470361-05002-045 CCCC

COND COND

161501158578806H12


A2740065070361-06002-047 CCCC




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 8 of 9

10-May-2016

2520 6542

414101329342806H23

38945502FAN AXIAL 9E930054SB70361-03005-107 14801

COND COND

4320012077228 R/H07A01

2264022PUMP MODULE ASSY,HYDRAUL

232933ABT53023-06 CCCC

COND COND

4320012077228 BACKUP07A01


255537ABR53023-06 CCCC

COND COND

4320012077228 L/H07A01


255542ABR53023-06 CCCC

13000 13729

156001129125607A24

47165445SAS ACTUATOR B112-0724670410-02500-049 00

13000 14826

156001129125607A24

32605086SAS ACTUATOR B112-0730770410-02500-049 00

COND COND

4810011022473 #107B05A

05086VALVE, SOLENIOD 207473213850-3-1 CCCC

COND COND

481001102247307B05A

58835086VALVE, SOLENIOD 31953213850-3-1 CCCC

COND COND

165001250376707B11

04022ACCUMULATOR C4010247470651-03201-104 CCCC

COND COND

1680013420496 L/H08B20

04022PANEL INDICATOR (PDU) 554170450-01043-124 CCCC

COND COND

1680013420496 R/H08B20

04022PANEL INDICATOR (PDU) 555470450-01043-124 CCCC

COND COND

6115011149696 R/H09A01

7894022GENERATOR 589228B302-8-DM CCCC

COND COND

6115011149696 L/H09A01

8684022GENERATOR 906E28B302-8-DM CCCC

COND COND

168001310225911C21

05445MIXER ASSEMBLY TMD0484374811270400-02300-048 CCCC

2160 7246

161501141753211C23

22515086TAIL ROTOR PITCHCHANGE SHAFT

2330357570400-06100-042 02

11000 12545

165001305695411C25

28334378SERVO ASSY, TAILROTOR

B3000150370410-06520-046 00

24400 21267

165001143122611D01

71554022MAIN ROTOR PRIMARYSERVO

B30300913B70410-02820-054 00

24400 24751

165001143122611D01


B3030233270410-02820-054 00

24400 25306

165001143122611D01


B3030609570410-02820-054 00

13000 13000

156001158968511D04

43164316AFT BELLCRANK 3450172970400-08102-045 00

17000 21022

156001164416111D05

04022AFT TIE ROD SUPTFITTING

E391-0213970400-08112-045 00




HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 9 of 9

10-May-2016

2200 6222

168001164416011D06

04022AFT TIE ROD ASSY M3920012170400-08111-042 00

4400 9486

156001286887011D07

05086AFT BELLCRANK SPTASSY

390-0184170400-08117-049 00

11000 14886

304001287243811D08

12005086LATERAL SWASHPLATELINK

A3800379570400-08151-061 00

20000 25086

168001221286311D09

05086LATERAL SERVOBELLCRANK

F3370479770400-08166-041 00

14000 19086

156001289269711D13

05086LEFT TIE ROD 344-0240170400-08115-046 00

3500 7522

156001296948611D14

04022RIGHT TIE ROD ASSY 288-0127670400-08114-051 00

15000 20086

168001158965211D15

05086FORWARD BELLCRANK 188770400-08101-046 00

5600 11211

156001221261911D16

05611FWD BELLCRANK SPTASSY

B367-0440870400-08162-042 00

COND COND

168001261204411D25

29385086STABILATOR ACTUATOR B2920407770400-06641-117 CCCC

COND COND

168001261204411D25

11654022STABILATOR ACTUATOR B2920605570400-06641-117 CCCC

COND COND

599601547345211D26

04729STABILATOR AMPLIFIER(DUAL)

26866981011445-1 CCCC

COND COND

299501496368615A04

1374548ENGINE SEQUENCINGUNIT

14074504587 CCCC

COND COND

5895012459090 LFT19E05A

05408RECEIVER-TRANSMITTER RADAR

1725ASM-C-967292 CCCC

COND COND

660501503528419E06A

05467ATTITUDE HEADINGREFERENCE UNIT

10250765100-20 CCCC

COND COND

661001490516852A

9904022AUTOMAT FLT CONTCOMPUTER

04123479825050-1-001 CCCC




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

16136 SESI

2. Organization

CSGLD-1052

REQUIREMENT CONTROL SYMBOL(Julian)1. PERIOD ENDING DATE


1GE-E-306353 CAO0133557592364213456327956117822971

2GE-E-306443 CAO0151948772574114851323756117822971

1GEE307962 ECD00980513511917856667923323

2GEE307426 ECD01537470242414456667923323

1GE-E-207878 ECD0336441252618811716284655238023432

2GE-E-307570 ECDH0497240497096544156155238023432

1GE-E-306531 CAO0106273371177310192332452678223704

2GE-E-207409 ECD0055858152402217718315752678223704


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

Workers

Highlight


HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70400-06100-042 23303575 11C234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-May-2016

2160 7246

311001113828811C23A

02251BRNG T/R PITCH CHGSHAFT

C84010082SB1162-102 RCRC

COND COND

534001094578911C23C

22512251CLEVIS, ROD END 23303570311201170400-06702-041 CCCC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70400-06100-042 23303575 11C234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

10-May-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



4141013293428FAN AXIAL 70361-03005-107 9E930054SB 06H234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-May-2016

2520 6542

311001127300506H23A

14803894BALL BRNG ANN (OILCOOLER FWD)

3515210SFFC3 RCRC

2520 6542

311001127300506H23A

14803894BALL BRNG ANN (OILCOOLER FWD)

3699210SFFC3 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



4141013293428FAN AXIAL 70361-03005-107 9E930054SB 06H234. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

10-May-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615013765089TAIL ROTORGEARBOX ASSY

70358-06600-046 A00604489 06G014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-May-2016

12000 17086

161501074515306G01C

00I/B RETENTION PLATET/R

K2591193670358-06612-042 RCRC

5000 10086

304001292161706G01D

00GEARSHAFT, BEVEL G3200086270358-06620-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615013765089TAIL ROTORGEARBOX ASSY

70358-06600-046 A00604489 06G014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

10-May-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70351-08100-076 A26501119 06A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-May-2016

17000 20994

161501078571106A08

10923542SWASHPLATE GUIDE AER0024570351-08227-041 RCRC

3000 7022

161501110149106A13

02478HOUSING ASSY MGB F2110006570351-08110-045 RCRC

6919 10860

304001415838806A18

812478MAIN ROTOR SHAFT E2530463370351-08131-048 RCRC

12000 14800

161501497725706A19

12222478PLANETARY CARRIERASSY

A2400123570351-08175-046 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70351-08100-076 A26501119 06A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

10-May-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615011997646SWASHPLATE ASSY 70104-08000-050 015152-1429 05A03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-May-2016

COND COND

161501087160205A03A01

13821382STATIONARYSWASHPLATE

2220156670104-08010-044 CCCC

11000 13021

161501357508905A03A02

2001318ROTATINGSWASHPLATE

A326-0132770104-08001-045 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615011997646SWASHPLATE ASSY 70104-08000-050 015152-1429 05A03A4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

10-May-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND



1615014426926MAIN ROTORSPINDLE ASSY

70102-08200-069 D00112206 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-May-2016

COND COND

311001158960705A01I02C

12133014THRUST BEARING B32529467SB7002-048 CCCC

COND COND

161501161437305A01I02

12133014SPHERICAL BEARINGASSY

B32420992ASB7001-048 CCCC

13000 18445

531001126944405A01I04

00M/R SPINDLE NUT F4790552970102-08105-102 RCRC

6400 11845

530601460602005A01I06

00TIE ROD (M/R SPINDLE) C5041151138023-10372-101 RCRC

20000 25445

161501214914005A01I07

00HORN ASSEMBLY G2410224070102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

10-May-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 1 of 2

10-May-2016

COND COND

3110011589607 BLUE05A01I02C


COND COND

1615011614373 BLUE05A01I02


B32421816SB7001-048 CCCC

13000 17407

5310011269444 BLUE05A01I04

00M/R SPINDLE NUT C4791419070102-08105-102 RCRC

6400 10807

5306014606020 BLUE05A01I06

00TIE ROD (M/R SPINDLE) C5040557838023-10372-101 RCRC

1300 5707

1615012149140 BLUE05A01I07

00CONTROL HORN ASSY E2410088470102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND





Report Date:

Page 2 of 2

10-May-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-069 B00100290 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-May-2016

COND COND

3110011589607 BLACK05A01I02C


COND COND

1615011614373 BLACK05A01I02


LK9088SB7001-048 CCCC

13000 17099

5310011269444 BLACK05A01I04

00M/R SPINDLE NUT F479005370102-08105-102 RCRC

6400 10499

5306014606020 BLACK05A01I06

00TIE ROD (M/R SPINDLE) C504-0399238023-10372-101 RCRC

20000 24099

1615012149140 BLACK05A01I07

515515HORN ASSEMBLY A241-1700370102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-069 B00100290 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

10-May-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-069 A00105905 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-May-2016

COND COND

3110011589607 YELLOW05A01I02C


COND COND

1615011614373 YELLOW05A01I02


C32410334SB7001-048 CCCC

13000 16683

5310011269444 YELLOW05A01I04

00M/R SPINDLE NUT C4791236970102-08105-102 RCRC

6400 10083

5306014606020 YELLOW05A01I06

00TIE ROD (M/R SPINDLE) B5040413338023-10372-101 RCRC

20000 23683

1615012149140 YELLOW05A01I07

931931HORN ASSEMBLY A2411545070102-08111-047 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70102-08200-069 A00105905 05A01I4. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

10-May-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 BEM1635 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-May-2016

9000 13378

165001125090703A01A

00PISTON, MAIN L/GEARSTR

BEM163570250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 BEM1635 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

10-May-2016





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 32937155 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 1 of 2

10-May-2016

9000 10886

165001125090703A01A

23172317PISTON, MAIN L/GEARSTR

42123170250-12067-102 RCRC





HRS)O/HLOCATIONNSN


PREVSER NO. OAND




70250-12051-045 32937155 03A014. SERIAL NUMBER2. NSN 3. PART NUMBER OR MODEL 5. WUC1. NOMENCLATURE

Report Date:

Page 2 of 2

10-May-2016





7822971HELICOPTER, 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

A020 5620.810TM 1-1520-237-PMDPERFORM M/R SPINDLE LUGS,M/R CUFF, TIP CAPSINSPECTION

5610.8H

A022 09 Dec 201514TM 1-1520-237-23-914 DAY FLYABLE STORAGEENGINE RUN UP

25 Nov 2015D

A092 25 Dec 201530TM 11-6140-203-23&P30 DAY SLAB BATTERYINSPECTION (D8565/11-1)

25 Nov 2015D

A100 13 Feb 201630DA PAM 738-751#1 ENGINE HISTORY RECORDERREADING DUE

14 Jan 2016D

A101 13 Feb 201630DA PAM 738-751#2 ENGINE HISTORY RECORDERREADING DUE

14 Jan 2016D

A103 08 Jan 201630TM 1-1500-344-23AIRCRAFT WASH DUE 09 Dec 2015D

A110 5644.540TM 1-1520-237-PMSPMS 40 HOUR INSPECTION 5604.5H

A115 15 Jan 201630TM 1-1520-237-23-12LUBE REQUIRMENTS 16 Dec 2015D

A115 5650.840TM 1-1520-237-23-12LUBE REQUIRMENTS 5610.8H

A116 5896.2360H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

5536.2H

A116 11 Mar 201612H-60-10-AMAM-11INTERMEDIATE GEARBOX OILSAMPLE

11 Mar 2015M

A117 5896.2360H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 5536.2H

A117 11 Mar 201612H-60-10-AMAM-11TAIL GEARBOX OIL SAMPLE 11 Mar 2015M

A140 5685.1120AWR 1346R16, IVHMSIN ACF

DOWNLOAD AND REVIEW IVHMSDATA

5565.1H

A160 25 Jan 201690TM 1-1520-237-23-1290 DAY CORROSIONINSPECTION

27 Oct 2015D

A177 01 Mar 201690AR 95-190 DAY REVIEW/UPDATE OF 365-4 ENTRIES

02 Dec 2015D

A210 5685.1120TM 1-1520-237-23-12120 HOUR INSPECTIONREQUIREMENTS

5565.1H

A211 5909.9360H-60-10-AMAM-11APU OIL SAMPLE 5549.9H

A211 12 Mar 201612H-60-10-AMAM-11APU OIL SAMPLE 12 Mar 2015M

A213 5690.1120TM 1-2840-248-23ENGINE COMPRESSORCLEANING

5570.1H

A214 5685.1120TM 1-1520-237-23-12CLEAN TAIL WHEEL ADAPTER 5565.1H

A222 04 Apr 2016360TM 1-1680-377-13&PAMSS SURVIVAL KITINSPECTION

10 Apr 2015D

A230 25 Feb 2016120MWO 1-1520-237-50-77INSPECT BATTERYCOMPARTMENT FORCORROSION (SLAB)

28 Oct 2015D

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

A295 5805.1360TM 1-1520-237-23-12STABILATOR ACTUATOR ASSYLUBE

5445.1H

A296 5805.1360TM 1-1520-237-23-12STABILATOR INSPECTION 5445.1H

A298 5941.1360TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 5581.1H

A298 07 Oct 201612TM 1-1520-237-23-12LUBE TAIL WHEEL BEARING 07 Oct 2015M

A299 5941.1360TM 1-1520-237-23-12SWASHPLATE LUBE 5581.1H

A299 07 Oct 201612TM 1-1520-237-23-12SWASHPLATE LUBE 07 Oct 2015M

A320 5805.1360TM 1-2840-248-23ENGINE INSPECTION &CLEANING

5445.1H

A400 6165.1720TM 1-1520-237-PMIPMI-1 5445.1H

A401 5805.1720TM 1-1520-237-PMIPMI-2 5085.1H

A408 5805.1720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-2, AREA 5 AND 6)

5085.1H

A410 6165.1720TM 1-1520-237-PMI720 HOUR LUBE REQUIRMENTS(PMI-1, AREA 1 THRU 4)

5445.1H

A415 6165.1720H-60-10-AMAM-11MAIN GEARBOX OIL SAMPLE-PART # 073, 074, 076

5445.1H

A440 5805.1720TM 1-1520-237-23-12CLEAN TAIL WHEEL LOCKPIN 5085.1H

A470 6585.11500TM 1-1520-237-23-12REPLACE NUMBER TWOCROSSFEED VALVE

5085.1H

A471 7245.62160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (FWD)

5085.6H

A472 7245.62160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (CENTER)

5085.6H

A473 7245.62160TM 1-1520-237-23-12REPLACE T/R SHAFT SUPPORTBEARINGS (AFT)

5085.6H

A476 10085.65000TM 1-1520-237-23-12REPLACEMENT OF RIGHT HANDTIE ROD ATTACHMENT BOLTS

5085.6H

A477 10085.65000TM 1-1520-237-23-12REPLACEMENT OF STABILATORACTUATOR BOLTS

5085.6H

A480 10085.65000TM 1-1520-237-23-12REPLACE PIVOT BOLT 70400-08159-101,102,103,104

5085.6H

A485 10085.65000TM 1-1520-237-23-12REPLACE BELLCRANK BOLT70400-08159-105,106,107,108

5085.6H

A496 30 Mar 20166TM 1-1500-204-23-1CF3BR FIRE EXTINGUISHERWEIGHT TEST & INSPECTION

30 Sep 2015M

A501 22 Apr 20166TM 1-1520-237-23-12MAIN ROTOR BLADE PRESSURECHECK

22 Oct 2015M

A502 30 Mar 20166TM 1-1520-237-23-12INSPECT AND TEST GROUNDRECEPTACLE IAW TM 1-1500-204-23

30 Sep 2015M






7. FREQUENCY 4.




INSP

A530 09 Dec 201512DA PAM 738-751AIRCRAFT EQUIPMENTINVENTORY (DA FORM 2408-17)

09 Dec 2014M

A532 02 Jul 201612TM 1-1500-204-23-4COMPASS SWING / RMI 02 Jul 2015M

A533 02 Oct 201612TM 1-1520-237-23-12PITOT STATIC SYSTEMINSPECTION

02 Oct 2015M

A534 15 Apr 201724TM 1-1500-204-23-1FIRST AID KIT INSPECTION 15 Apr 2015M

A538 02 Oct 201612TM 1-1520-237-23-12FAT/OAT GAUGEINSPECTION/TEST

02 Oct 2015M

A541 19 Nov 201612TM 1-1520-237-23, C4REPLACE DIGITAL CLOCKBATTERY

19 Nov 2015M

A550 02 Oct 201612AWR1346R16IVHUMS BATTERYREPLACEMENT

02 Oct 2015M

A553 17 Dec 201612AR 95-1AIRCRAFT WEIGHINGINVENTORY (365-1)

17 Dec 2015M

A580 11 Jun 201724TM 11-6140-203-23&PRETURN SLAB TO AVIM FORCAPACITY CHECK (VEREY 24MONTH)

11 Jun 2015M

A621 09 Dec 201624AR 95-1AIRCRAFT WEIGHING CLASS 2 09 Dec 2014M

A625 13 Jun 201860TM 11-6140-203-23&PREPLACEMENT OF SLABBATTERY (SLAB)

13 Jun 2013M

A630 01 Apr 2018114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 Oct 2008M

A633 01 Apr 2018114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #1,CARTRIDGE, DODIC MH92

01 Oct 2008M

A638 01 Apr 2018114TB 9-1300-385 CHG 22RESERVE FIRE BOTTLE #2,CARTRIDGE, DODIC MH92

01 Oct 2008M

A640 01 Apr 2018114TB 9-1300-385 CHG 22MAIN FIRE BOTTLE #2,CARTRIDGE, DODIC MH92

01 Oct 2008M

A648 25 Oct 2023180TM 1-1520-237-23REPLACE T/R SPRING CAPSULEASSY

25 Oct 2008M

A660 01 Sep 201772TB 9-1300-385REPLACE THRUSTEREMERGENCY RELEASE CARGOHOOK, MJ20

01 Sep 2011M

A665 02 Oct 201648H-60-14-AMAM-18REPLACE FUEL CELL O-RINGSEAL PN MS29513-215

02 Oct 2012M

A670 02 Oct 201648TM 1-1520-237-23-1CABIN TUB INSPECTION 02 Oct 2012M

A673 02 Oct 201648TM 1-1520-237-23-12FUEL CELL CORROSIONINSPECTION

02 Oct 2012M

A675 02 Oct 201648TM 1-1520-237-23-12FLIGHT CONTROL ROD INSP 02 Oct 2012M

A695 5805.1720H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

5085.1H

A695 24 Apr 201848H-60-14-ASAM-06MIXER ASSEMBLY LUBRICATIONINSPECTION

24 Apr 2014M






7. FREQUENCY 4.




INSP

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

0H

E015 17 May 2016180MWO 1-1520-237-50-92ASN 128D DOPPLER GPSBATTERY REPLACEMENT

19 Nov 2015D

E040 13 Feb 201690TM 11-5841-294-12APR-39 RADAR/LASERWARNING OPNL CHECK, 5841-01-236-8951

15 Nov 2015D

E125 10 Feb 201690TM 11-5810-262-23KY-58 PMCS/OPNL CHECK 12 Nov 2015D

E135 22 Apr 20166TM 11-5821-333-12AN/ARC-201(V) SINCGARSRADIO HUB BATT REPL

22 Oct 2015M

E155 17 May 2016180TM 11-5810-262-23KY-58 BATTERY REPLACEMENT 19 Nov 2015D

E300 25 Dec 201530AWR 1516R3 FOR ELTEMERGENCY LOCATORTRANSMITTER SELF TEST (EBC-406HM)

25 Nov 2015D

E300 5730.3120AWR 1516R3 FOR ELTEMERGENCY LOCATORTRANSMITTER SELF TEST (EBC-406HM)

5610.3H

E320 05 Apr 2016360AWR 1516 FOR ELTEMERGENCY LOCATORTRANSMITTER G-SWITCH (EBC-406HM)

11 Apr 2015D

E330 28 May 20166AWR1346R16UNDER WATER ACOUSTICBEACON BATTERYREPLACEMENT

28 May 2010Y

E351 13 May 20166TM 11-5895-1841-13PREPLACE APX-118TRANSPONDER BATTERY

13 Nov 2015M




Documents

Report Date: MAJOR COMPONENT LISTING Sorted By ... 70102-08105-102 M/R SPINDLE NUT F47905529 5610.8 18445 12834.2 D00112206 70102-08111-047 HORN ASSEMBLY G24102240 5610.8 25445 19834.2