1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE1

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 30 Oct 14 1 07:59 LOWER, KEITH

COMPLY WITH REQUIREMENTS OF THE ADDENDUM TO H-60-15-SOF-01 AT 7121.0 ACFT HOURS.

5333.2 O O 2

AWAITING TBO OF OIL COOLER 06H23A

― A 19 Jan 17 1001 07:28 WIDEMAN, CHARLES

COMPLY WITH H-60-16-AMAM-07 (TAIL ROTOR SERVO SAFETY CABLE), BEFORE 5935.9 AIRCRAFT HOURS, BUT NOT TO EXCEED 15 MAY 20.

5575.5 H G 1

AWAITING NEXT PMI 05B

Ⓧ A 15 Mar 17 4 10:03 WIEDOWER, BRADLEY

USE OF PERSONAL RESTRAINT TETHER RESTRICTED PER H-60-17-ASAM-07

5577.5 K G 2

02

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 1 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE2

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ E 06 Sep 17 1 22:07 GANDOLPH, DONOVAN

HUD DOES NOT DISPLAY AT EITHER PILOT STATION

5667 G G 4

W/O/N- AV172500001 16

/ A 18 Oct 17 2 10:49 WIEDOWER, BRADLEY

BOTH CYCLIC STICK SUPPORTS REQUIRE LACQUER FOR COMPLETION OF AMAM

5674 K G 2

AWAITING PAINT ESTIMATED SHIP DATE 17 AUG 1802

/ A 15 Dec 17 2 09:58 JOHNSON, JEREMIAH

TAIL PYLON LOWER (SWING-OUT) STEP INTERNAL BRACKET (STEP STOP) CRACKED IN RADIUS OF ANGLE

5696.2 K G 2

AWAITING NEXT MAJOR MAINTENANCE 02

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 2 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE3

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

/ A 12 Jan 18 4 13:00 GRANTHAM, TREY

CABIN SKIN ABOVE BLADE DEICE AC JUNCTION BOX HAS A 1/2" CRACK. VERIFIED BY NDI. STA: 350 WL: 268 BL: 20R

5704.7 O G 2

DEFERRED TIL PMI-2 00

/ A 12 Jan 18 7 13:07 GRANTHAM, TREY

LOWER LH STRINGER HAS A 1/2" CRACK JUST FORWARD OF THE 565 FRAME. STA: 558 WL: 202 BL: 4.5

5704.7 O G 2

DEFERRED TIL PMI DEFERRED TIL PMI-2 CONTINUING TO MONITOR DURING 40 HR INSP

00

/ A 12 Jan 18 8 13:09 GRANTHAM, TREY

SHEAR DECK AT TAIL LANDING GEAR STRUT HAS SEPARATION IN METAL IN AFT R/H CORNER OF STRUT OPENING. (IMPROPER DEPOT REPAIR)

5704.7 O G 2

DEFERRED TIL PMI-2 CONTINUE TO MONITOR AT 40 HR19H

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 3 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE4

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

/ A 18 Apr 18 4 21:59 TRUBIANO, ROBERT

IVHUM DISPLAY DOES NOT DIM. CRT STAY BRIGHT WITH THE DIM REHOSTAT TURNED TO JUST BEFORE OFF

5735.2 G G 4

W.O. SUBMITTED 1 MAY 2018 08F01

― A 30 Apr 18 3 13:12 WIEDOWER, BRADLEY

COMPLY WITH REQUIREMENTS OF H-60-17-ASAM-11 FUEL HOSE BORESCOPE INSPECTION, BY 1 MARCH 2021.

5744.5 K G 2

10

― A 12 Jul 18 1 06:32 C, O

INSP A550 - REPLACE IVHMU AA LITHIUM BATTERY. DUE AT: 11-AUG-2018. UPGRADE TO X STATUS ON 11-SEP-2018

5781.3 O O 1

W/O SUBMITTED 12 JULY 2018 08F01

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 4 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE5

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

/ A 13 Jul 18 4 08:19 GRANTHAM, TREY

INSTALLATION OF APU IR FLAME DETECTOR SENSOR, PN 70310-00800-101, REQUIRED PER H-60-18-AMAM-04 BY 10 JULY 20.

5783.3 O G 2

00

/ A 13 Jul 18 5 08:22 GRANTHAM, TREY

INSTALLATION OF UPPER NO 1 ENGINE IR FLAME DETECTOR SENSOR, PN 70310-00800-101, REQUIRED PER H-60-18-AMAM-04 BY 10 JULY 20.

5783.3 O G 2

00

/ A 13 Jul 18 6 08:23 GRANTHAM, TREY

INSTALLATION OF LOWER NO 1 ENGINE IR FLAME DETECTOR SENSOR, PN 70310-00800-101, REQUIRED PER H-60-18-AMAM-04 BY 10 JULY 20.

5783.3 O G 2

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 5 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE6

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

/ A 13 Jul 18 7 08:24 GRANTHAM, TREY

INSTALLATION OF UPPER NO 2 ENGINE IR FLAME DETECTOR SENSOR, PN 70310-00800-101, REQUIRED PER H-60-18-AMAM-04 BY 10 JULY 20.

5783.3 O G 2

00

/ A 13 Jul 18 8 08:25 GRANTHAM, TREY

INSTALLATION OF LOWER NO 2 ENGINE IR FLAME DETECTOR SENSOR, PN 70310-00800-101, REQUIRED PER H-60-18-AMAM-04 BY 10 JULY 20.

5783.3 O G 2

00

Ⓧ A 26 Jul 18 2 09:19 JOHNSON, JEREMIAH

OPERATE WITHIN THE LIMITATIONS PRESCRIBED IN THE ENCLOSED AWR'S DATED: 980 R19 3 NOV 17 (HOIST EQUIPMENT), 1037 R15 21JUL17 (SATCOM), 1054 R19 18 OCT 17 (BAMBI BUCKET), 1127 R8 31 JAN 17 (HELI-BASKET WITH ELL), 1308 R12 21 APR17 (GOODRICH 42305-3 AND -5), 1346 R25 21 NOV 17 (IVHMS AND HUMS), 1425 R21 27 DEC 17 (CMWS, ICMD, P3I, OFP, TIE), 1444 R9 15MAY18 (FOGS SINGLE CONFIG), 1453 R6 07 JUN 17 (AIR WARRIOR BLOCK), 1466 R7 10AUG15 (GARMIN GPSMAP 696, 496, 495, 396, 296, 295), 1516 R11 13 FEB 18 (ELT EBC-406HM), 1566 R6 01SEP17 (TITANIUM OR STAINLESS STEEL CABLE GUARD), 1800 R7 23 MAR 17 (EDM AND BFT), 1858 R7 13 JUL 18 (EWIS), 1930 R9 28 MAR 18 (PMI), 1513 R11 29SEP17 (IPAC), 1520 R28 3 MAY 18 (SPONSEN MOUNTED FLIR), 1656 R4 23 JAN 17 (PHOENIX MADIFIED DRIP PAN), 1682 R24 1 DEC 17 (UH60A WITH 701D OR 701C), 1738 R5 24 FEB 17 (APX 118 COMMON TRANSPONDER), 1750 R5 27 FEB 18(ANVIS AVS-6 NVG), 1913 R3 26 JAN 18 (MSD V3 ,AWR 2002 R4 21 DEC 17 ( IMMSS), AWR 2120 R1 2 OCT 17

5799.6 K G 2

02

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 6 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE7

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

/ A 26 Jul 18 3 23:45 TRUBIANO, ROBERT

DOPPLER/GPS DISPLAYS DN 1G DURING SELF TEST.

5801.6 G C 4

19E04

/ A 26 Jul 18 4 23:47 TRUBIANO, ROBERT

IVHUMS HIT CHECK FAILED TEST. PROCEDURES CORRECT. NUMBERS CLOSE TO MANUAL CHECK. MANUAL CHECK PASSES JUST FINE.

5801.6 G D 4

08F01

― A 01 Aug 18 2 21:56 C, O

INSP A020 - PERFORM M/R SPINDLE LUGS, M/R CUFF, TIP CAPS INSPECTION. Due at: 5811.6 Hours. Upgrade to X Status on 5812.7 Hours

5806.6 O O 1

05A01I

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 7 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE8

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 01 Aug 18 3 21:56 C, O

INSP A210 - 120 HOUR INSPECTION REQUIREMENTS. Due at: 5816.2 Hours. Upgrade to X Status on 5821.3 Hours

5806.6 O O 1

00

― A 01 Aug 18 4 21:56 C, O

INSP A213 - ENGINE COMPRESSOR CLEANING. Due at: 5816.2 Hours. Upgrade to X Status on 5821.3 Hours

5806.6 O O 1

04A

― A 01 Aug 18 5 21:56 C, O

INSP A214 - CLEAN TAIL WHEEL ADAPTER . Due at: 5816.2 Hours. Upgrade to X Status on 5821.3 Hours

5806.6 O O 1

03B

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 8 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE9

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 02 Aug 18 1 06:36 C, O

ACE INSP REQUIRED

5806.6 O G 2

02

/ A 03 Aug 18 4 14:32 GRANTHAM, TREY

CABIN FLOOR AT FORWAR CARGO DOOR ENTRANCE HAS THREE LOOSE FASTENERS

5806.6 O G 2

02

/ A 03 Aug 18 5 14:33 GRANTHAM, TREY

R/S CENTER CONSOL FORWARD UPPER ANGLE BRACKET CRACKED IN HALF.

5806.6 O G 2

02

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 9 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE10

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 03 Aug 18 6 14:34 WIEDOWER, BRADLEY

FORWARD TAB FRAME 308 R/H SIDE CRACKED HALF INCH

5806.6 K G 2

02

/ A 03 Aug 18 7 14:35 WIEDOWER, BRADLEY

R/H 34.5 BEAM HAS APPROX. 1 INCH CRACK IN WEB JUST AFT OF 308 BEAM

5806.6 K G 2

02

✕ A 03 Aug 18 8 14:36 WIEDOWER, BRADLEY

FWD TRANSMISSION BEAM HAS APPROX. 1/4 CRACK IN TOP L/H CORNER

5806.6 K G 2

02

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 10 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE11

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 03 Aug 18 9 14:37 WIEDOWER, BRADLEY

SUPPORT BRACKET ON R/H INTERCOSTAL FOR CABIN VIBE ABSOBER WHERE ATTACHES TO FWD TRANSMISSION BEAM HAS 2 CRACKS

5806.6 K G 2

02

/ A 03 Aug 18 10 14:40 WIEDOWER, BRADLEY

#2 ENGINE FIREWALL HAS A 1/2" CRACK AT PREVIOUS REPAIR INBD OF ENG MOUNT

5806.6 K G 2

02

/ A 03 Aug 18 11 14:41 WIEDOWER, BRADLEY

TOP CAP ANGLE OF #2 ENGINE FIREWALL HAS 2 EA CRACKS ON UNDERSIDE, 2" LONG

5806.6 K G 2

02

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 11 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE12

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

Ⓧ A 09 Aug 18 1 15:30 WIEDOWER, BRADLEY

OPERATE WITHIN THE LIMITATIONS PRESCRIBED IN THE ENCLOSED AWR 1926R4

5806.6 K G 2

02

― A 09 Aug 18 4 15:32 C, O

INSP A850 - PMD DUE. Due at: 13-Aug-2018. Upgrade to X Status on 14-Aug-2018

5806.6 O O 1

02

✕ A 13 Aug 18 14:52 Generated, Computer

INSP A022 14 DAY FLYABLE STORAGE ENGINE RUN UP FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 09 AUG 2018

REFERENCE: TM 1-1520-237-23&P

5806.6 O O 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 12 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE13

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 13 Aug 18 14:52 Generated, Computer

INSP A302 LUBRICATE MAIN LANDING GEAR WHEEL BEARINGS FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 28 JUL 2018 OR 6055.5 AIRCRAFT HOURS

REFERENCE: TM 1-1520-237-23&P

5806.6 O O 1

00

✕ A 20 Aug 18 06:47 Generated, Computer

INSP A538 FAT/OAT GAUGE INSPECTION/TEST FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 18 AUG 2018

REFERENCE: TM 1-1520-237-23&P

5806.6 O O 1

00

/ A 20 Aug 18 12:50 YERTON, DAVID

Control exchange of Troop commanders antenna SN: 7803, with aircraft SN: 82-23750 to SN: 00-26851.

5806.6 K G 2

Part on order 02

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 13 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE14

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 22 Aug 18 09:25 WIEDOWER, BRADLEY

INSP A103 - AIRCRAFT WASH DUE. DUE AT: 28-AUG-2018. UPGRADE TO X STATUS ON 01-SEP-2018

5806.6 O O 1

00

― E 22 Aug 18 09:28 WIEDOWER, BRADLEY

INSP E220 - EMERGENCY LOCATOR TRANSMITTER SELF-TEST (AS REQUIRED). DUE AT 29-AUG-2018 OR 5921.6 . UPGRADE TO X STATUS ON 02-SEP-2018 OR 5926.6

5806.6 O O 1

19R

― A 22 Aug 18 09:30 WIEDOWER, BRADLEY

INSP A115 - LUBE REQUIREMENTS. DUE AT: 26-AUG-2018 OR 5841.6 HOURS. UPGRADE TO X STATUS ON 30-AUG-2018 OR 5845.6 HOURS

5806.6 O O 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 14 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE15

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 22 Aug 18 10:02 Macintire, Mitchell

CONTROLLED EXCHANGED M/R BLADE SN- A007-12237 WITH ACFT 8724600 M/R BLADE SN- A007-04330

5806.6 B G 2

00

✕ E 24 Aug 18 00:00 Generated, Computer

INSP E040 APR-39 RADAR/LASER WARNING OPNL CHECK, 5841-01-236-8951 FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 23 AUG 2018

REFERENCE: TM 11-5841-294-12

5806.6 O O 1

00

✕ E 24 Aug 18 00:00 Generated, Computer

INSP E125 KY-58 PMCS/OPNL CHECK FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 23 AUG 2018

REFERENCE: TM 11-5810-262-23

5806.6 O O 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 15 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE16

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ E 24 Aug 18 00:00 Generated, Computer

INSP E155 KY-58 BATTERY REPLACEMENT FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 23 AUG 2018

REFERENCE: TM 11-5810-262-23

5806.6 O O 1

00

✕ A 27 Aug 18 00:01 Generated, Computer

INSP A115 LUBE REQUIRMENTS FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 26 AUG 2018 OR 5841.6 AIRCRAFT HOURS

REFERENCE: TM 1-1520-237-23&P

5806.6 O O 1

00

✕ A 29 Aug 18 00:01 Generated, Computer

INSP A103 AIRCRAFT WASH DUE FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 28 AUG 2018

REFERENCE: TM 1-1500-344-23

5806.6 O O 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 16 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE17

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 29 Aug 18 00:01 Generated, Computer

INSP A501 MAIN ROTOR BLADE SPAR PRESSURE CHECK FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 28 AUG 2018

REFERENCE: TM 1-1520-237-23&P

5806.6 O O 1

00

✕ E 30 Aug 18 00:00 Generated, Computer

INSP E220 EMERGENCY LOCATOR TRANSMITTER SELF-TEST (AS REQUIRED) FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 29 AUG 2018 OR 5921.6 AIRCRAFT HOURS

REFERENCE: AWR 1516-R9 9MAR16

5806.6 O O 1

00

✕ A 31 Aug 18 00:01 Generated, Computer

INSP A850 PMD DUE FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 30 AUG 2018

REFERENCE: LOCAL

5806.6 O O 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 17 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE18

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ E 02 Sep 18 00:01 Generated, Computer

INSP E351 REPLACE APX-118 TRANSPONDER BATTERY FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 01 SEP 2018

REFERENCE: TM 11-5895-1841-13P

5806.6 O O 1

00

✕ E 02 Sep 18 00:01 Generated, Computer

INSP E145 AN/ARC-201A(V) SINCGARS HUB BATT REPL FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 01 SEP 2018

REFERENCE: TM 11-5821-333-12

5806.6 O O 1

00

✕ A 02 Sep 18 00:01 Generated, Computer

INSP A502 INSPECT AND TEST GROUND RECEPTACLE IAW TM 1-1500-204-23 FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 01 SEP 2018

REFERENCE: TM 1-1520-237-23&P

5806.6 O O 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 18 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE19

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ H 04 Sep 18 10:13 Kyle, Michael

CONTROLLED EXCHANGE RESCUE HOIST SN: 1417 ON ACFT SN:82-23750 WITH RESCUE HOIST SN: 1437 ON ACFT SN: 85-24435 / CABLE ON RESCUE HOIST SN:1437 FAILED LOOSENESS CHECK WITH NO REPLACEMENT

5806.6 O G 2

00

✕ A 06 Sep 18 00:01 Generated, Computer

INSP A092 30 DAY SLAB BATTERY INSPECTION (D8565/11-1) FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 05 SEP 2018

REFERENCE: TM 11-6140-203-23 P

5806.6 O O 1

00

✕ A 06 Sep 18 00:01 Generated, Computer

INSP A532 COMPASS SWING / RMI FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 05 SEP 2018

REFERENCE: TM 1-1500-204-23-4

5806.6 O O 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 19 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE20

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 11 Sep 18 11:09 Panozzo, Nicholas

ACFT PREPERATION REQUIRED FOR (MWO 1-1520-237-20-TDFM)

5806.6 K G 2

00

/ A 13 Sep 18 08:44 TAYLOR, BRANDON

CHART "C" ENTRY REQUIRED FOR REMOVAL OF CONTROL PANEL, VHF/FM C-11466A/ARC-201A(V). WEIGHT 2.0. ARM 224.00. MOMENT 0.4. CHANGE NOT ENTERED ON 365-3.

5806.6 S G 2

02

/ A 13 Sep 18 08:51 TAYLOR, BRANDON

CHART "C" ENTRY REQUIRED FOR REMOVAL OF COMMUNICATIONS SECURITY CONTROL PANEL KY-58/Z-AHP. WEIGHT 2.0. ARM 227.00. MOMENT 0.5. CHANGE NOT ENTERED ON 365-3.

5806.6 S G 2

02

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 20 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE21

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

/ A 13 Sep 18 08:54 TAYLOR, BRANDON

CHART "C" ENTRY REQUIRED FOR INSTALLATION OF COMMUNITCATIONS SECURITY CONTROL PANEL KY-58/Z-AHP. WEIGHT 2.0. ARM 214.00. MOMENT 0.4. CHANGE NOT ENTERED ON 365-3.

5806.6 S G 2

02

Ⓧ A 13 Sep 18 14:51 JOHNSON, JEREMIAH

OPERATE WITHIN LIMITATIONS AND RESTRICTIONS SPECIFIED IN AWR 2122 R2 DATED 30 JUL 2018 ( TECHNISONIC TDFM-9000NV RADIO INSTALLED)

5806.6 O G 2

02

✕ A 13 Sep 18 17:26 NEAL, LEWIS

CONTROLLED EXCHANGE M/R BLADE S/N: A007-01173 TO ACFT 86-24502 FOR M/R BLADE A007-07699

5806.6 O G 2

05

13 Sep 18 20:00 5806.6A 05

REPLACED BLADE

METHENY, N.F 1.5 NEAL, L. F 1.5

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 21 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE22

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 13 Sep 18 17:36 NEAL, LEWIS

MTF REQUIRED FOR REMOVAL AND REPLACEMENT OF BLACK M/R BLADE S/N: A007-01173

5806.6 O G 2

05

― A 13 Sep 18 17:38 NEAL, LEWIS

TRACK AND BALANCE REQUIRED FOR REMOVAL AND REPLACEMENT OF BLACK M/R BLADE

5806.6 O G 2

05

― A 18 Sep 18 07:20 GRANTHAM, TREY

mtf due on afcc system due to removal and installation of the afcc .

5806.6 B B 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 22 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE23

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 20 Sep 18 00:00 Generated, Computer

INSP A804 LOGBOOK RECON FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 19 SEP 2018

REFERENCE: LOCAL

5806.6 O O 1

00

✕ E 27 Sep 18 08:46 THARP, TIMOTHY

cargo hook emergency release thruster and cartridge assy rmvd for controled exchange to acft 901.thruster s/n:0758 cartridge s/n:7087.installed thruster s/n:0225 cartridg s/n:10731

5806.6 K G 2

16A02

✕ A 28 Sep 18 00:01 Generated, Computer

INSP A177 90 DAY REVIEW/UPDATE OF 365-4 ENTRIES FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 27 SEP 2018

REFERENCE: AR 95-1

5806.6 O O 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 23 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE24

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 28 Sep 18 00:01 Generated, Computer

INSP A160 90 DAY CORROSION INSPECTION FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 27 SEP 2018

REFERENCE: TM 1-1520-237-23&P

5806.6 O O 1

00

✕ A 23 Oct 18 00:01 Generated, Computer

INSP A230 INSPECT BATTERY COMPARTMENT FOR CORROSION (SLAB) FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 22 OCT 2018

REFERENCE: MWO 1-1520-237-50-77

5806.6 O O 1

00

✕ A 15 Nov 18 14:51 Panozzo, Nicholas

CO-PILOTS BAROMETRIC ALTIMETER REMOVED FOR TROUBLESHOOTING.

5806.6 K G 2

02

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 24 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE25

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 15 Nov 18 14:52 Panozzo, Nicholas

REMOVED AIR DATA TRANSDUCER FOR TROUBLESHOOTING.

5806.6 K G 2

02

✕ A 16 Nov 18 11:27 CHANDLER, TRAVIS

REMOVED AIRSPEED TRANSDUCER TO FACILITATE MAINTENANCE

5806.6 Q G 1

19

✕ A 30 Nov 18 12:40 Macintire, Mitchell

CONTROLLED EXCHANGE OF M/R BLADE S/N A007-12088 WITH ACFT 00-26866 M/R BLADE S/N A007-14166

5806.6 O G 2

DOC NO. W90CUL83340001 05A02

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 25 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE26

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ E 06 Dec 18 14:05 TAYLOR, BRANDON

controlled exchange of the ARN-123 receiver to ACFT 85-24435 required

5806.6 K G 2

W8119N83240001 19

✕ A 06 Dec 18 15:39 TAYLOR, BRANDON

avionics maintence in progess. refer to write up controlled exchange of the ARN-123 receiver to ACFT 85-24435 required

5806.6 K G 2

19

✕ A 27 Dec 18 15:07 WIEDOWER, BRADLEY

AIRCRAFT DISASSEMBLY REQUIRED FOR GROUND TRANSPORT TO MO-TASMG FOR DEPOT LEVEL REPAIRS

5806.6 K G 2

02

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 26 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE27

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 28 Dec 18 09:13 WIEDOWER, BRADLEY

#1 & #2 ENGINE INLET REMOVAL REQUIRED FOR TRANSPORT TO MO TASMG

5806.6 H O 2

02B13

✕ H 28 Dec 18 12:54 EVANS, TERRY

rescue hoist removal required to facilitate depot level maitenance

5806.6 K G 1

00

/ A 02 Jan 19 10:48 GRANTHAM, TREY

cabin overhead soundproofing requires removal for aircraft shipment to TASM-G

5806.6 O G 2

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 27 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE28

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 03 Jan 19 07:29 HARRIS, JOSHUA

"Inspect the MR De-ice Distributor Harness/Chip Detector Harness per H-60-19-AMAM-03, at or before 5816.2 Aircraft Hours."

5806.6 O O 1

02

03 Jun 19 09:09 5806.6T 02

MESSAGE OVERDUE UPDATED STATUS, SEE ENTRY BELOW

BROWN, M.F 0.2

/ A 03 Jan 19 10:18 Generated, Computer

"Install angle brackets for MR De-Ice Harness per H-60-19-AMAM-03, MR De-Ice/Chip Detector Harness Chafing and Re-Routing, at the NEXT main transmission removal."

5806.6 O O 1

00

― A 03 Jan 19 13:35 TAYLOR, BRANDON

MOC OF THE NO.1 RADAR ALTIMETER DUE TO REPLACEMENT

5806.6 K G 2

19

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 28 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE29

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 04 Jan 19 00:01 Generated, Computer

INSP A534 FIRST AID KIT INSPECTION FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 03 JAN 2019

REFERENCE: TM 1-1500-204-23-1

5806.6 O O 1

00

/ A 07 Jan 19 12:37 EVANS, TERRY

CONTROLLED EXCHANGE OF RED MR BLADE DEICE CABLE FROM AIRCRAFT 8223750 TO AIRCRAFT 8726001

5806.6 B G 2

02

/ A 09 Jan 19 13:39 GRANTHAM, TREY

BOTH L/H AND R/H EYEBROW FAIRING SEALS TORN

5806.6 K G 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 29 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE30

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 10 Jan 19 15:32 Generated, Computer

compass swing required

5806.6 O O 1

19E07

― A 11 Jan 19 10:03 BOWEN, THOMAS

CONTROLLED EXCHANGE OF OAT SENSOR P/N 132LU FROM ACFT 8223750 TO ACFT 8826036

5806.6 B G 1

02

11 Jan 19 12:53 5806.6S 00

CONTROLLED EXCHANGE OF OAT SENSOR P/N 132LU FROM ACFT 8223750 TO ACFT 8826036 COMPLETE

HALE, T. F 1.2

✕ A 17 Jan 19 10:18 BRILEY, AUSTIN

CONTROLLED EXCHANGED HYD PUMP S/N: 256139ABR TO ACFT 88-26036

5806.6 K G 2

DOC NO. W91FD990170001 07A01

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 30 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE31

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ E 18 Jan 19 00:01 Generated, Computer

INSP E320 EMERGENCY LOCATOR TRANSMITTER G-SWITCH (EBC-406HM) FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 17 JAN 2019

REFERENCE: AWR 1516 FOR ELT

5806.6 O O 1

00

✕ A 24 Jan 19 00:01 Generated, Computer

INSP A496 CF3BR FIRE EXTINGUISHER WEIGHT TEST INSPECTION FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 23 JAN 2019

REFERENCE: TM 1-1520-237-23&P

5806.6 O O 1

00

✕ A 13 Feb 19 00:01 Generated, Computer

INSP A100 LH/RH ENGINE HISTORY RECORDER READINGS DUE FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 12 FEB 2019

REFERENCE: DA PAM 738-751

5806.6 O O 1

00

15 Feb 19 00:00 5806.66 00

READINGS TAKEN

GRANTHAM, T.F 0.1

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 31 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE32

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 16 Feb 19 00:01 Generated, Computer

INSP A857 APU METER READINGS DUE ( EVENTS, HOURS) FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 15 FEB 2019

REFERENCE: LOCAL

5806.6 O O 1

00

20 Feb 19 08:15 5806.66 00

READINGS TAKEN

GRANTHAM, T.F 0.1

✕ E 20 Feb 19 00:01 Generated, Computer

INSP E015 ASN 128D DOPPLER GPS BATTERY REPLACEMENT FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 19 FEB 2019

REFERENCE: MWO 1-1520-237-50-92

5806.6 O O 1

00

― A 25 Feb 19 09:29 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF MAIN ROTOR TRANSMISSION S/N A26500684 INSTALLED IN ACFT 82-23750 WITH S/N A26500796 INSTALLED IN 85-24435

5806.6 B G 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 32 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE33

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 27 Feb 19 10:49 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF GENERATOR S/N 586E FROM ACFT 8523435 WITH GNERATOR S/N 1158E FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 10:50 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF GENERATOR S/N 84A1792 FROM ACFT 8523435 WITH GENERATOR S/N 1083E FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 10:51 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF HYDRAULIC PUMP S/N 197928 FROM ACFT 8523435 WITH HYDRAULIC PUMP S/N 273887A FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 33 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE34

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 27 Feb 19 10:53 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF ACC G/B S/N A258-01917 FROM ACFT 8523435 WITH ACC G/B S/N A258-00685 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 10:55 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF ACC G/B S/N A258-07111 FROM ACFT 8523435 WITH ACC G/B S/N A258-01027 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 11:01 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF INPUT G/B S/N A264-00430 FROM ACFT 8523435 WITH INPUT G/B S/N A264-00564 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 34 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE35

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 27 Feb 19 11:05 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF INPUT G/B S/N A264-01707 FROM ACFT 8523435 WITH S/N A264-04621 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 11:08 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF FWD BELLCRANK SUP ASSY S/N B367-03263 FROM ACFT 8523435 WITH FWD BELLCRANK SUP ASSY S/N B367-03466 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 11:10 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF FWD BELLCRANK S/N 66936-00677 FROM ACFT 8523435 WITH FWD BELLCRANK S/N G355-00128 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 35 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE36

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 27 Feb 19 11:22 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF AFT WALKING BEAM S/N B3112-00187 FROM ACFT 8523435 WITH AFT WALKING BEAM S/N B346-00345 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 11:24 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF LAT SERVO BELLCRANK S/N F337-04911 FROM ACFT 8523435 WITH LAT SERVO BELLCRANK S/N F337-05690 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 11:26 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF LAT SWASHPLATE LINK S/N A380-02879 FROM ACFT 8523435 WITH LAT SWASHPLATE LINK S/N C380-00346 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 36 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE37

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 27 Feb 19 11:30 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF LEFT TIE ROD ASSY S/N 344-01055 FROM ACFT 8523435 WITH LEFT TIE ROD ASSY S/N 344-01439 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 11:33 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF RIGHT TIE ROD ASSY S/N 288-00040 FROM ACFT 8523435 WITH RIGHT TIE ROD ASSY S/N D366-10260 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 11:34 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF AFT BELLCRANK S/N C345-02414 FROM ACFT 8523435 WITH AFT BELLCRANK S/N C345-02827 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 37 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE38

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 27 Feb 19 11:36 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF AFT BELLCRANK SUP ASSY S/N 390-02821 FROM ACFT 8523435 WITH AFT BELLCRANK SUP ASSY S/N 390-01545 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 11:38 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF SWASHPLATE ASSY S/N A107-00541 FROM ACFT 8523435 WITH SWASHPLATE ASSY S/N 015152-1720 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 11:41 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF M/R SHAFT EXT S/N 6350600001 FROM ACFT 8523435 WITH M/R SHAFT EXT S/N 015152-01697 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 38 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE39

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 27 Feb 19 11:42 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF BIFILAR ASSY S/N A327-00313 FROM ACFT 8523435 WITH BIFILAR ASSY S/N AIM00345 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 11:44 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF M/R HUB S/N C308-00224 FROM ACFT 8523435 WITH M/R HUB S/N 015152-00830 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 11:47 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF M/R SPINDLE S/N A001-01598 FROM ACFT 8523435 WITH M/R SPINDLE S/N A001-07424 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 39 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE40

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 27 Feb 19 11:48 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF M/R SPINDLE S/N A001-05869 FROM ACFT 8523435 WITH M/R SPINDLE S/N A001-05741 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 11:51 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF M/R SPINDLE S/N D00112489 FROM ACFT 8523435 WITH M/R SPINDLE S/N A001-08085 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 11:51 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF M/R SPINDLE S/N A001-01725 FROM ACFT 8523435 WITH M/R SPINDLE S/N A001-03651 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 40 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE41

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 27 Feb 19 11:53 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF M/R DAMPER S/N A106-08873 FROM ACFT 8523435 WITH M/R DAMPER S/N A106-09884 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 11:55 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF M/R DAMPER S/N WG3005800638 FROM ACFT 8523435 WITH M/R DAMPER S/N R10601525 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 27 Feb 19 11:56 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF M/R DAMPER S/N WG106-02926 FROM ACFT 8523435 WITH M/R DAMPER S/N A106-03386 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 41 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE42

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 27 Feb 19 11:58 WIDEMAN, CHARLES

CONTROLLED EXCHANGE OF M/R DAMPER S/N WG3005-800588 FROM ACFT 8523435 WITH M/R DAMPER S/N WG106-01467 FROM ACFT 8223750AS PART OF ROTOR HEAD AND 5-PACK SWAP

5806.6 B G 1

00

― A 28 Feb 19 14:36 Macintire, Mitchell

CONTROL EXCHANGE OF #2 ENGINE S/N GE-E-991767 WITH ACFT 8724600 S/N GE-E-374391C DUE TO B SUMP LEAKING BEYOND LIMITS

5806.6 B G 2

02

― A 28 Feb 19 15:22 Macintire, Mitchell

CONTROL EXCHANGE OF #2 ENGINE HIGH SPEED SHAFT S/N C845-05482 WITH ACFT 8724600 #2 ENGINE HIGH SPEED SHAFT S/N C845-11448

5806.6 B G 2

02

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 42 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE43

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 02 Mar 19 00:01 Generated, Computer

INSP A299 LUBRICATE SWASHPLATE FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 01 MAR 2019 OR 6197.7 AIRCRAFT HOURS

REFERENCE: TM 1-1520-237-23&P

5806.6 O O 1

00

✕ A 02 Mar 19 00:01 Generated, Computer

INSP A298 LUBRICATE TAIL WHEEL BEARINGS FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 6197.7 AIRCRAFT HOURS OR 01 MAR 2019

REFERENCE: TM 1-1520-237-23&P

5806.6 O O 1

00

✕ A 06 Mar 19 11:27 Generated, Computer

INSP A298 LUBRICATE TAIL WHEEL BEARINGS FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 6197.7 AIRCRAFT HOURS OR 01 MAR 2019

REFERENCE: TM 1-1520-237-23&P

5806.6 O O 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 43 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE44

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 06 Mar 19 11:27 Generated, Computer

INSP A299 LUBRICATE SWASHPLATE FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 WAS DUE. STATUS UPGRADED TO X ON: 6197.7 AIRCRAFT HOURS OR 01 MAR 2019

REFERENCE: TM 1-1520-237-23&P

5806.6 O O 1

00

― A 07 Mar 19 06:53 GRANTHAM, TREY

Comply with requirements of H-60-19-ASAM-03, Parker Turbine Starter Removal, by 12 MAR 19.

5806.6 O G 1

00

03 Jun 19 09:21 5806.6T 02

MESSAGE STATUS UPGRADED TO "X" FOR OVERDUE COMPLIANCE

BROWN, M.F 0.2

✕ A 12 Mar 19 11:16 Darmon, Stephen

COMPLY WITH H-60-19-ASAM-03, PARKER AIR TURBINE STARTER REMOVAL, BY 12 MAR 19

5806.6 O O 1

07D01

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 44 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE45

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 02 Apr 19 08:39 Keen, Scotty

REMOVAL R/H MLG STRUT TO FOM

5806.6 K G 2

03A01

✕ A 10 Apr 19 08:58 Macintire, Mitchell

CONTROL EXCHANGE STABILATOR ACTUATOR SN U0914 WITH ACFT 0026866 SN 2416

5806.6 B G 2

02

✕ A 10 Apr 19 08:59 Macintire, Mitchell

CONTROL EXCHANGE STABILATOR ACTUATOR SN B292-01168 WITH ACFT 0026866 SN 2415

5806.6 B G 2

02

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 45 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE46

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 10 Apr 19 09:01 Macintire, Mitchell

REMOVED STABILATOR ACTUATORS SN B292-01168 AND U0914

5806.6 B G 2

02

✕ A 24 Apr 19 07:45 Keen, Scotty

DEMOD OF MWO 1-1520-237-50-108 EXTERNAL STORES SUPPORTS SYSTEM MOUNTED RESCUE HOIST REQUIRED.

5806.6 K G 1

00

✕ A 24 Apr 19 08:08 Keen, Scotty

DEMOD OF MWO 1-1520-237-20-5 INTERIM MEDEVAC MISSION SUPPORT SYSTEM (IMMSS) PATIENT. A&B KIT

5806.6 K G 2

02

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 46 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE47

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 24 Apr 19 09:07 Keen, Scotty

DEMOD OF MWO 1-1520-237-20-TDFM REQUIRED

5806.6 K G 2

19

✕ A 24 Apr 19 09:13 Keen, Scotty

DEMOD OF MWO 1-1520-237-50-115 TALON FORWARD LOOKING INFRARED (FLIR) SPONSON MOUNT REQUIRED.B KIT

5806.6 K G 2

16S

✕ A 26 Apr 19 09:00 Darmon, Stephen

REMOVAL OF MAIN AND RESERVE FIRE BOTTLES REQUIRED

5806.6 K G 2

12

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 47 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE48

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 05 May 19 00:01 Generated, Computer

INSP A541 REPLACE DIGITAL CLOCK BATTERY FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 IS DUE. STATUS WILL UPGRADE TO X ON: 04 JUL 2019

REFERENCE: TM 1-1520-237-23&P

5806.6 O O 1

00

― A 14 May 19 07:51 ROBERTSON, TAYLOR

REMOVAL OF UNIT PROPERTY EQUIPMENT REQUIRED FOR ACFT TRANSITION TO BEST PROGRAM

5806.6 B G 2

19

― A 16 May 19 10:10 EVANS, TERRY

control exchange of pilots armored wing assembly required from aircraft 8726001

5806.6 B G 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 48 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE49

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

/ A 16 May 19 10:13 EVANS, TERRY

DELAMINATION PRESENT ON RH PILOT ARMORED WING ASSY

5806.6 B G 2

02

✕ A 22 May 19 09:29 CERRATO, BRYAN

REMOVED APX-118 S;N 0675

5806.6 B A 1

00

✕ A 29 May 19 08:04 Simmons, Timothy

RH LOWER MLG SHOCK STRUT AIR VALVE REQUIRES REPLACEMENT DUE TO FAILURE TO HOLD AIR PRESSURE IAW TM 1-1520-237-23&P WP 0648

5806.6 E G 2

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 49 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE50

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

― A 30 May 19 00:01 Generated, Computer

INSP A553 AIRCRAFT WEIGHING INVENTORY (365-1) FOR HELICOPTER, UTILITY CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8223750 IS DUE. STATUS WILL UPGRADE TO X ON: 29 JUL 2019

REFERENCE: AR 95-1

5806.6 O O 1

00

― A 30 May 19 09:09 Generated, Computer

SAFETY MESSAGE NUMBER: H-60-19-AMAM-07 DESCRIPTION: DIAGONAL SEAT STRUT ASSEMBLY INTERNAL PRIMER APPLICATION INSPECTION. IS DUE: 06 JUN 2019 CALENDAR

5806.6 O O 1

00

✕ A 30 May 19 09:11 Generated, Computer

SAFETY MESSAGE NUMBER: H-60-19-ASAM-05 DESCRIPTION: "COMPLY WITH H-60-19-ASAM-05, MAIN ROTOR SPINDLE HARDWARE NON-CONFORMANCE, BY 16 MAYT 2019.". WAS DUE: 16 MAY 2019 CALENDAR

5806.6 O O 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 50 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE51

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 30 May 19 09:12 Generated, Computer

SAFETY MESSAGE NUMBER: H-60-19-AMAM-04 DESCRIPTION: INSPECTION OF T700 SERIES ENGINE IGNITION EXCITERS. WAS DUE: 23 APR 2019 CALENDAR

5806.6 O O 1

00

✕ A 30 May 19 15:37 Generated, Computer

REMARK/NOTICE TO BUYER: PRIOR TO DELIVERY OF THE AIRCRAFT TO THE BUYER THE FOLLOWING ITEMS WILL BE REMOVED FROM THE AIRCRAFT AT THE DIRECTION OF THE US GOVERNMENT; TO INCLUDE BUT NOT LIMITED TO: CMWS JUNCTION BOX; SA-26669/ALE-47 (V) CMWS SEQUENCER; SENSOR ELECTRO-OPTIC MISSLE CM-SU-202/AAR-57 (V); DIGITAL COCKPIT DISPLAY UNIT (CMWS); SAFE/ARM CONTROL PANEL (CMWS); CMWS RELAY BOX; MEMORY CARD PMCIA (UDM) MU-1126/AAR-57(V) (CMWS); RECEIVER/TRANSMITTER, RT-1477/ARC-201; CONTROL, C-11466A/ARC-201; KY-58(3EA); KY-58 CONTROL HEAD (3EA); KY-100 AIRTERM; ARC-220/AMP; ARC-220 RT; ARC-220 CONTROL HEAD; AN/AVS-7 B-KIT CONTROL HEAD; AN/AVS-7 B-KIT SDC HUD; UHF RDO-XMTR RT-1518C/ARC-164 HAVEQUICK; NAV DOPPLER/GPS AN/ASN-128B/D; CARGO HOOK, CARTRIDGE EXPLOSIVE (SQUIB); 12 POINT ICS MODULE; AUX FUEL QUAN CONTROL HEAD; AN/PSN-14(A) DAGR (BFT); TRANSPONDER AN/APX 118 OR 123; MCU COOLING GARMENTS AND HOSES; MICRO COOLING UNIT; APR 39 UDM CARD; APR 39 PROCESSOR; APR 39 JUNCTION BOX; APR 39 DISPLAY; APR 39 CONTROL HEAD; PINTLE MOUNT ASSY-L/H; PINTLE MOUNT ASSY-R/H; M240/M60 MACHINE GUN MOUNT RHS; M240/M60 MACHINE GUN MOUNT LHS; AUX FUEL QUANTITY CONTROL HEAD; FLIR MONITORS-AVALAX DISPLAY AND MOUNTING HARDWARE; IVHMU; CONTROL DISPLAY UNIT (IVHMS) 10150-0204; AM-7189 FM AMPLIFIER; ARC-231 R/T; ARC 231 AMP; BFT PALLET WITH DAGR AN/PSN-14(A); INTERFACE UNIT, DATA (IVHMS) 30201-0501.

5806.6 W G 1

00

― A 30 May 19 15:39 BRIDGES, ROBERT

AIRCRAFT INDUCTED INTO BEST PROGRAM ON 30 MAY 2019, NO SCHEDULED MAINTENANCE PERFORMED AFTER THIS DATE.

5806.6 E G 2

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 51 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE52

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 31 May 19 08:15 Simmons, Timothy

RMVD ENGINE AIR INLETS FOR BEST PROGRAM SN CHECK IAW TM 1-1520-237-23&P WP 0688

5806.6 E G 2

00

✕ A 31 May 19 11:42 Wright, Kevin

Removed cartridge, impulse P/N: 1512AS121 S/N: 12350 iaw TM 1-1500-328-23 as per gov request.

5806.6 B G 1

00

✕ E 03 Jun 19 08:38 FRANSAW, RONNIE

RMVD AN/AAR-57 SAFE/ARM BOX

5806.6 E G 2

00

03 Jun 19 13:39 5806.6B 00

WRITTEN IN ERROR

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 52 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE53

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 03 Jun 19 09:12 BROWN, MICHAEL

H-60-19-AMAM-03 DTD 2 JAN 19, MR DEICE/CHIP DETECTOR HARNESS CHAFFING NOT COMPLIED WITH

5806.6 B G 2

02

✕ A 03 Jun 19 09:27 BROWN, MICHAEL

COMPLY WITH H-60-18-SOF-02, TR BLADE INSPECTIONS, BY 28 APR 18.

5806.6 B G 2

02

✕ E 03 Jun 19 09:29 FRANSAW, RONNIE

RMVD AN/AAR-57 SAFE/ARM BOX. PN: A102853-101, NSN: 5930-01-576-8081, SN:006, AS PER GOV REQ IAW TM 1-1520-237-23&P WP3655

5806.6 E G 2

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 53 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE54

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 03 Jun 19 09:29 BROWN, MICHAEL

COMPLY WITH H-60-19-AMAM-05, T700 SERIES ENGINE LUBE MANIFOLD GROMMET, BY XXXX AIRCRAFT HOURS BUT NOT TO EXCEED 30 APR 19.

5806.6 B G 2

02

✕ E 03 Jun 19 09:53 FRANSAW, RONNIE

RMVD RECEIVER TRANSMITTER, RT1518C/ARC-164 (4). PN: 901974-806, NSN: 5821-01-352-7209, SN:MO1146 AS PER GOV REQ IAW TM 1-1520-237-23&P WP4437

5806.6 E G 2

00

✕ E 03 Jun 19 10:55 FRANSAW, RONNIE

RMVD DISPLAY UNIT,RADAR CP-1252C/ASN-128. PN: SM-D-858886, NSN: 5841-01-399-5513 AS PER GOV REQ IAW TM 1-1520-237-23&P WP4423

5806.6 E G 2

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 54 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE55

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ E 03 Jun 19 11:49 FRANSAW, RONNIE

RMVD CONTROL TRANSMITTER, RADAR C-12664/APX. PN: 1008940P-4, NSN: 5841-01-493-8789 , SN: 0918 AS OER GOV REQ IAW TM 1-1520-237-23&P

5806.6 E G 2

00

✕ E 03 Jun 19 12:04 FRANSAW, RONNIE

RMVD RECEIVER TRANSMITTER, RADAR RT-1193/ASN-128 PN: SM-D-858489-2, NSN: 5841-01-318-0654 , SN: 316C. AS PER GOV REQ IAW TM 1-1520-237-23&P WP4423

5806.6 E G 2

00

✕ E 03 Jun 19 12:19 FRANSAW, RONNIE

RMVD CHAFF CONTROL PANEL AN/AAR-57PN: A102859-101, NSN: 1055-01-576-8810 , SN: 0254. AS PER GOV REQ IAW TM 1-1520-237-23&P WP3656

5806.6 E G 2

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 55 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE56

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ E 03 Jun 19 12:33 FRANSAW, RONNIE

RMVD AN/AAR-57 RELAY BOX. PN: A100604-101, SN:0658, AS PER GOV REQ IAW TM 1-1520-237-23&P WP3308

5806.6 E G 2

00

✕ E 03 Jun 19 12:45 FRANSAW, RONNIE

RMVD AN/AAR-57 RELAY BOX. PN: A100604-101, SN:1579, AS PER GOV REQ IAW TM 1-1520-237-23&P WP3308

5806.6 E G 2

00

03 Jun 19 13:37 5806.6B 00

WRITTEN IN ERROR

✕ E 03 Jun 19 12:46 FRANSAW, RONNIE

RMVD AN/AAR-57 RELAY BOX. PN: A100605-101, SN:1579, AS PER GOV REQ IAW TM 1-1520-237-23&P WP3308

5806.6 E G 2

00

03 Jun 19 14:47 5806.6B 00

ENTERED IN ERROR

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 56 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE57

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ E 03 Jun 19 14:49 FRANSAW, RONNIE

RMVD DISTRBUTION BOX CWMS PN:A100605-101 NSN: 6110-01-576-2486 SN:0658 AS PER GOV REQ TM 1-1520-237-23&P WP1939

5806.6 E G 2

00

✕ E 03 Jun 19 14:58 FRANSAW, RONNIE

RMVD DISTRBUTION BOX CWMS PN:A100605-101 NSN: 6110-01-576-2486 SN: 1579 AS PER GOV REQ TM 1-1520-237-23&P WP1939

5806.6 E G 2

00

✕ E 03 Jun 19 15:06 FRANSAW, RONNIE

RMVD CONVERTER SIGNAL, DATA PN: P320A002-3 NSN: 5895-01-518-8783 SN: 2183 AS PER GOV REQ TM 1-1520-237-23&P WP4423

5806.6 E G 2

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 57 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE58

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

/ W 04 Jun 19 07:57 FRANSAW, RONNIE

RMVD MACHINE GUN MOUNT ASSY RH. PN: 70751-02023-044, NSN: 1005-01-141-3813 SN: N/A, AS PER GOV REQ IAW TM 1-1520-237-23&P WP1816

5806.6 E G 2

00

/ W 04 Jun 19 08:03 FRANSAW, RONNIE

RMVD MACHINE GUN MOUNT ASSY LH. PN: 70751-02023-044, NSN: 1005-01-141-3813 SN: N/A, AS PER GOV REQ IAW TM 1-1520-237-23&P WP1816

5806.6 E G 2

00

― A 04 Jun 19 14:44 HARPER, JAMES

DURING THE BEST INPROCESS PROCEDURE, THE FOLLOWING COMPONENTS WERE UNABLE TO HAVE THE S/N’S VERIFIED. ALL OF THESE COMPONENTS HAVE BEEN S/N MATCHED AGAINST MCDS AND THE RECORDS MATCH BETWEEN ULLS-A AND MCDS. THESE COMPONENTS REQUIRE S/N VERIFICATION AT THE NEXT MAJOR MAINT EVENT. ACCUMULATOR S/N: B407-00693; T/R PC SHAFT S/N: 233-02645; AFT TIE ROD SUPT FITTING S/N: A391-00409; AXIAL FAN BEARING S/N’S UNK1524 #2, UNK 1524 #1.

5806.6 W G 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 58 of 127 04 Jun 2019 1859 UTC

1. AIRCRAFT SERIAL NUMBER8223750

2. MODELUH-60A

3. DATE 4. PAGE59

PART I - FAULT INFORMATIONSTATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

STATUS SYS DATE NO TIME PID

FAULTS/REMARKS

ACFT HRS WHEN DISC HOW REC MAL EFF

DELAY WUC

PART II - CORRECTING INFORMATIONDATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

DATE TIME ACFT HRSROUNDS ACTION CODE WUCACTION

PID CAT HRS PID CAT HRS PID CAT HRS

TIPID TI MANHOURS

✕ A 04 Jun 19 14:48 HARPER, JAMES

UPON BEST ACCEPTANCE IT WAS FOUND THAT THE FIVE PACK ASSEMBLY, #1 AND #2 ENGINES WERE FOUND TEMP INSTALLED. ALL APPLICABLE LOGBOOK ENTRIES WERE MADE BY UNIT.

5806.6 W G 1

00

✕ A 04 Jun 19 14:55 HARPER, JAMES

UPON BEST ACCEPTANCE IT WAS FOUND THAT M/R SPINDLE ASSY SPINDLE NUT S/N: D001-12489 WAS NOT INSTALLED IN MCDS. VERFICATION REQUIRED UPON NEXT INSPECTION.

5806.6 B G 1

00

DA FORM 2408-13-1, OCT 1997 AIRCRAFT INSPECTION AND MAINTENANCE RECORDDA FORM 2408-13-1, OCT 91, MAY BE USED For use of this form, see DA PAM 738-751; the proponent agency is DCSLOG

APD PE v3.00

page 59 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

/ 8223750 A

18 Apr 18 4

21:59

IVHUM DISPLAY DOES NOT DIM. CRT STAY BRIGHT WITH THE DIM REHOSTAT TURNED TO JUST BEFORE OFF

✕ H✕ H✕ H― C― C✕

✕

✕

REMOVED HARDWARE SECURING IVHMU DISPLAY. (4 EACH)DISCONNECTED CANNON PLUG FROM IVHMU DISPLAY.REMOVED IVHMU DISPLAY SN: 80260.

TOOL BOX INV REQUIRED.

FOD CHECK REQUIRED.

Removed hardware securing IVHMU display (4 each)

Disconnected cannon plug from IVHMU display

Remuved IVHMU display SN: 81714

REINSTALLED HARDWARE. (4 EACH)

RECONNECTED CANNON PLUG.

REPLACED IVHMU DISPLAY WITH SN: 81714.Complete

Complete

Reinstalled Hardware

Reconnected Cannon plug

Replaced with SN: 80238

MOFFETT, A.

YERTON, D.

YERTON, D.

CERRATO, B.

CERRATO, B.

FORDHAM, A.

FORDHAM, A.

FORDHAM, A.

F

F

F

F

F

F

F

F

0.2

0.2

0.2

0.1

0.1

0.5

0.3

0.5

page 60 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

― 8223750 A

12 Jul 18 1

06:32

INSP A550 - REPLACE IVHMU AA LITHIUM BATTERY. DUE AT: 11-AUG-2018. UPGRADE TO X STATUS ON 11-SEP-2018

✕ H✕ H✕ H― C― C

REMOVED HARDWARE FROM IVHMU BATTERY COVER. (14 EACH)REMOVED BATTERY COVER.

REMOVED IVHMU BATTERY.

FOD CHECK REQUIRED.

TOOL BOX INV REQUIRED.

REINSTALLED HARDWARE. (14 EACH).REINSTALLED BATTERY COVER.

REPLACED BATTERY

FOD CHECK COMPLETE

TOOL BOX INVENTORY COMPLETE

MOFFETT, A.

MOFFETT, A.

MOFFETT, A.

ROBERTSON, T.

ROBERTSON, T.

F

F

F

F

F

0.2

0.2

0.2

0.1

0.1

page 61 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

/ 8223750 A

26 Jul 18 3

23:45

DOPPLER/GPS DISPLAYS DN 1G DURING SELF TEST.

✕ H✕ H― C― C

REMOVED GPS SDC BATTERY COVER.

REMOVED BATTERY.

FOD CHECK REQUIRED.

TOOL BOX INV REQUIRED.

REINSTALLED BATTERY COVER.

REPLACED BATTERY.

FOD CHECK COMPLETE

TOOL BOX INVENTORY COMPLETE

YERTON, D.

YERTON, D.

ROBERTSON, T.

ROBERTSON, T.

F

F

F

F

0.2

0.2

0.1

0.1

page 62 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

― 8223750 A

02 Aug 18 1

06:36

ACE INSP REQUIRED

/

✕

✕

/

/ C/ C✕ C✕ C✕ C✕

✕

✕ C/ C

RMVD XMSN DRIP PAN

LOWERED CABIN SOUND PROOFING

RMVD (2EA) AFT BULK HEAD PANELS

OPENED TAIL ROTOR DRIVE SHAFT COVERS

RMVD T/R G/B COVER

RMVD INTER G/B COVER

RMVD (2EA) BROOM CLOSET SOUND PROOFING PANELSRMVD L/H TAILBOOM ACCESS PANEL

RMVD R/H TAILBOOM ACCESS PANEL

DISCONNECTED RECEPTACLE FROM #4 DRIVE SHAFT COVERRMVD SECTION 4 DRIVE SHAFT COVER ( FM ANTENNA)RMVD 5 IN ROUND PANLE ON BOTTOM SIDE OF T/R PYLONOPENED AFT M/R PYLON DOOR

INSTALLED COVER

INSTALLED COVER

INSTALLED PANELS

INSTALLED PANEL

INSTALLED PANEL

INSTALLED PANEL

CLOSED

GRANTHAM, T.

GRANTHAM, T.

GRANTHAM, T.

GRANTHAM, T.

GRANTHAM, T.

GRANTHAM, T.

GRANTHAM, T.

F

F

F

F

F

F

F

0.2

0.2

0.8

0.3

0.4

0.2

0.1

page 63 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 2

― 8223750 A

02 Aug 18 1

06:36

ACE INSP REQUIRED

―

―

✕ C✕ C✕ C/ C/ C✕ C✕ C✕ C✕ C✕ C✕ J

FOD CHECK REQUIRED PRIOR TO INSTALLATION OF PANELSTOOL BOX INVENTORY REQUIRED

RECLINED 2 EA PILOT SEATS

RMVD L/H SHOCK STRUT/ ESSS UPPER FAIRING

RMVD R/H SHOCK STRUT/ ESSS UPPER FAIRING

RMVD TROOP SEATS (IF APPLICABLE)

OPENED FORWARD ELECTRONIC COMPARTMENT DOOR (NOSE)REMOVED 2 EA HDWR SECURING CABIN VIBE ABSORBER STOPREMOVED CABIN VIBE ABSORBER STOP

REMOVED 2 EA BOLTS SECURING L/H CABIN ASORBER SPRINGS TO AIRFRAMEREMOVED BOLT SECURING R/H CABIN ABSORBER SPRING TO AIRFRAMEREMOVED CABIN VIBE ABSORBER

REMOVED SOUNDPROOFING STRIP FROM FWD TRANSMISSION BEAM

RAISED AND SECURED

INSTALLED FAIRING

N/A EXTERNAL HOIST INSTALLED

N/A

CLOSED

REINSTALLED HARDWARE, TQD TO 47 IN LBSREINSTALLED STOP

REINSTALLED BOLTS, TQD TO 50-100 IN LBSREINSTALLED BOLT, TQD TO 50-100 IN LBSREINSTALLED VIBE ABSORBER

REINST SOUNDPROOFING

GRANTHAM, T.

GRANTHAM, T.

GRANTHAM, T.

GRANTHAM, T.

GRANTHAM, T.

RIDER, J.

RIDER, J.

RIDER, J.

RIDER, J.

RIDER, J.

GRANTHAM, T.

F

F

F

F

F

F

F

F

F

F

F

0.2

0.2

0.1

0.1

0.1

0.2

0.2

0.2

0.2

0.2

1.0

page 64 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 3

― 8223750 A

02 Aug 18 1

06:36

ACE INSP REQUIRED

✕

✕

✕

REMOVED 2 EA BOLTS ATTACHING L/H CABIN VIBE ABSORBER SPRINGS TO AIRFRAMEREMOVED BOLT SECURING R/H VIBE ABSORBER SPRING TO AIRFRAMEREMOVED CABIN VIBE ABSORBER

page 65 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

/ 8223750 A

20 Aug 18

12:50

Control exchange of Troop commanders antenna SN: 7803, with aircraft SN: 82-23750 to SN: 00-26851.

✕

✕

✕

Removed mounting hardware (8 each) from troop commanders antenna. Disconnected connector from troop commanders antenna. Removed troop commanders antenna SN: 7803.

page 66 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

22 Aug 18

10:02

CONTROLLED EXCHANGED M/R BLADE SN- A007-12237 WITH ACFT 8724600 M/R BLADE SN- A007-04330

✕

✕

✕

✕

✕

―

―

REMOVED COTTER PINS 2 EA FROM BLADE PINS

DISCONNECTED ANTI-FLAP SPRING

DISCONNECTED DE-ICE CANNON PLUG FROM BLADEREMOVED BLADE PINS 2 EA

REMOVED MR BLADE SN - A007-12237

FOD CHECK REQUIRED

TOOL BOX INVENTORY DUE

page 67 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

― 8223750 A

11 Sep 18

11:09

ACFT PREPERATION REQUIRED FOR (MWO 1-1520-237-20-TDFM)

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

DISC CANNON PLUG FROM R/H IMMSS ASSY

RMVD AMBULATORY PATIENT SEATS 2 EA FROM R/H IMMSS ASSYRMVD HDWR AND FLOOR BRACKETS ON R/H IMMSS

RMVD QUICK RELEASE PINS FROM R/H UPPER ACFT INTERFACE FITTING RMVD HDWR FROM R/H LOWER ACFT INTERFACE FITTING RMVD R/H IMMSS ASSY

RMVD SHIMS (4 EA) FROM HARD POINT ADAPTERS ON FORWARD CABIN FLOORING DISC CANNON PLUG FROM L/H IMMSS ASSY

RMVD AMBULATORY PATIENT SEATS 2 EA FROM L/H IMMSS ASSYRMVD HDWR AND FLOOR BRACKETS ON L/H IMMSS

RMVD QUICK RELEASE PINS FROM L/H UPPER ACFT INTERFACE FITTING RMVD HDWR FROM L/H LOWER ACFT INTERFACE FITTING RMVD L/H IMMSS ASSY

page 68 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 2

― 8223750 A

11 Sep 18

11:09

ACFT PREPERATION REQUIRED FOR (MWO 1-1520-237-20-TDFM)

✕

✕

✕ S✕ S✕

✕ J✕ J/

✕

✕ J✕ S✕ S✕ J

RMVD HDWR AND R/H CABIN FLOOR REAR SEAT KICKPANEL RMVD HDWR AND CENTER CABIN FLOOR KICKPANEL

DISC CANNON PLUG FROM JUNCTION BOX

RMVD HDWR AND JUNCTION BOX FROM ACFT

DISC BATTERY POWER CONNECTOR FROM ACFT BATTERY RMVD COPPER SAFTEY AND LOOSENED ACFT BATTERY STRAP BOLTSRMVD ACFT BATTERY

RMVD FWD CABIN UPPER SOUNDPROOFING

RMVD H-BAR MOUNTS (3 EA) FROM FWD UPPER CABIN CELING RMVD L/H BROOM CLOSET

RMVD HDWR AND L/H BROOM CLOSET COLLECTIVE CONTROL ROD RMVD HDWR AND L/H BROOM CLOSET PITCH CONTROL ROD RMVD HDWR AND L/H BROOM CLOSET ROLL CONTROL ROD

RECONNECTED CANNON PLUG

REINST BOX

safetied battery

installed battery

installed broom closet

WRITE UP ENTERED IN ERROR, CONTROL ROD NEVER REMOVEDWRITE UP ENTERED IN ERROR, CONTROL ROD NEVER REMOVEDREINST ROD TQ HDWR TO 40 IN/LBS, COTTERPINNED

WIEDOWER, B.

WIEDOWER, B.

GRANTHAM, T.

GRANTHAM, T.

GRANTHAM, T.

WIEDOWER, B.

WIEDOWER, B.

GRANTHAM, T.

F

F

F

F

F

F

F

F

0.3

0.2

0.1

0.1

0.1

0.2

0.2

0.4

page 69 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 3

― 8223750 A

11 Sep 18

11:09

ACFT PREPERATION REQUIRED FOR (MWO 1-1520-237-20-TDFM)

✕ J✕ J―

―

✕ J✕ S✕ S✕

✕ S✕ S✕ S✕ S✕ S

RMVD HDWR AND L/H BROOM CLOSET YAW CONTROL ROD RMVD HDWR AND FWD CABIN FLOOR PANEL

TOOLBOX INV DUE

FOD CHECK DUE

LOOSENED BATTERY RELAY COVER

RMVD L/H AFT HEATING DUCT WORK (2 EA)

RMVD L/H RELAY PANEL FROM CABIN CELING

RMVD AFCC FLIGHT COMPUTER FROM ACFT

DISCONNECTED CONNECTORS (4 EACH) FROM #2 FM RT. REMOVED #2 FM RT SN: 02511.

DISCONNECTED CANNON PLUG FROM #2 FM CONTROL HEAD. REMOVED #2 FM CONTROL HEAD SN: 02506A

disconnected apr-39 control, detecting set

REINST ROD TQ HDWR TO 40 IN/LBS, COTTERPINNEDREINST FLOOR AND HDWR

REINST COVER

REINST HEATER DUCT

REINST L/H RELAY PANEL

reconnected connectors to FM2 RT

reinstalled FM2 RT sn: 02511

#2 control head removed

replaced with TDFM-9000 MULTIBAND TRANSCEIVER SN: FTA11274RECONNECTED APR-39 CONTROL

GRANTHAM, T.

WIEDOWER, B.

GRANTHAM, T.

WIEDOWER, B.

CERRATO, B.

YERTON, D.

YERTON, D.

CERRATO, B.

YERTON, D.

YERTON, D.

F

F

F

F

F

F

F

F

F

F

0.4

2.0

0.5

0.5

1.0

0.5

0.2

1.0

0.5

0.3

page 70 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 4

― 8223750 A

11 Sep 18

11:09

ACFT PREPERATION REQUIRED FOR (MWO 1-1520-237-20-TDFM)

✕ S✕ S✕ S✕ S✕ S✕ S✕ S/ S✕ S✕ S

removed apr-39 control, detecting set sn: A1380CC

disconnected ky-58 control

removed ky-58 control sn: B04376

disconnected AN/AAR-57 chaff control panel

removed AN/AAR-57 chaff control panel sn: 0254

disconnected IBF control panel

removed IBF control panel sn: L0718

BAG AND STOW FM2 KY-58 CONTROL CANNON PLUG REQREMOVED KY-58 SN: B04376 FROM FM2 POSITION

DISCONNECTED FM2 KY-58 SN:B04376

REINSTALLED APR-39 CONTROL

RECONNECTED KY-58 CONTROL

REINSTALLED KY-58 CONTROL

RECONNECTED CHAFF CONTROL PANELREINSTALLED CHAFF CONTROL PANELRECONNECTED IBF CONTROL PANELREINSTALLED IBF CONTROL

BAGGED AND STOWED CANNON PLUGREINSTALLED KY-58 SN: BO4376 INTO THE UHF POSITION.DUMMY PLUGGED CONNECTOR TO KY-58 MOUNT

YERTON, D.

YERTON, D.

YERTON, D.

YERTON, D.

YERTON, D.

YERTON, D.

YERTON, D.

YERTON, D.

YERTON, D.

YERTON, D.

F

F

F

F

F

F

F

F

F

F

0.3

0.7

0.3

0.3

0.3

0.3

0.3

0.4

0.5

0.2

page 71 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

13 Sep 18

17:26

CONTROLLED EXCHANGE M/R BLADE S/N: A007-01173 TO ACFT 86-24502 FOR M/R BLADE A007-07699

✕

✕

✕

✕

― N― N✕

REMOVED COTTER PINS (2 EA) FROM BLADE PINS

REMOVED BLADE PINS (2 EA) FROM BLACK M/R BLADE REMOVED DEICE CABLE FROM BLACK M/R BLADE

REMOVED BLACK M/R BLADE S/N: A007-07699 FROM M/R SPINDLEFOD CHECK DUE

TOOLBOX INVENTORY DUE

DISCONNECTED SPRING FROM ANTIFLAP CAM

COMPLETED

COMPLETED

NEAL, L.

NEAL, L.

F

F

0.4

0.4

page 72 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

15 Nov 18

14:51

CO-PILOTS BAROMETRIC ALTIMETER REMOVED FOR TROUBLESHOOTING.

✕ J✕ J✕ J― T― T

REMOVED HARDWARE (3 EACH) SECURING CO-PILOTS BAROMETRIC ALTIMETER.DISCONNECTED CONNECTIONS (2 EACH) ON CO-PILOT BAROMETRIC ALTIMETER.REMOVED CO-PILOTS BAROMETRIC ALTIMETER.

FOD CHECK REQUIRED.

TOOL BOX INV REQUIRED.

REINSTALLED HARDWARE.

RECONNECTED CONNECTIONS.

REINSTALLED

complete

complete

CHANDLER, T.

CHANDLER, T.

CHANDLER, T.

TAYLOR, B.

TAYLOR, B.

F

F

F

F

F

0.2

0.2

1.0

0.2

0.2

page 73 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

15 Nov 18

14:52

REMOVED AIR DATA TRANSDUCER FOR TROUBLESHOOTING.

✕ J✕ J✕ J― T― T

DISCONNECTED CONNECTIONS (3 EACH) ON AIR DATA TRANSDUCER.REMOVED MOUNTING HARDWARE (4 EACH) FROM AIR DATA TRANSDUCER.REMOVED AIR DATA TRANSDUCER.

FOD CHECK REQUIRED.

TOOL BOX INV REQUIRED.

RECONNECTED CONNECTIONS.

REINSTALLED HARDWARE.

REINSTALLED AIR DATA TRANSDUCER. complete

complete

CHANDLER, T.

CHANDLER, T.

CHANDLER, T.

TAYLOR, B.

TAYLOR, B.

F

F

F

F

F

0.2

0.2

1.0

0.2

0.2

page 74 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

16 Nov 18

11:27

REMOVED AIRSPEED TRANSDUCER TO FACILITATE MAINTENANCE

✕ J✕ J― C― C

DISCONECTED 3 CONNECTIONS ON AIRDPEED TRANSDUCERREMOVED 4 SCREWS FROM AIRSPEED TRANSDUCER

FOD CHECK REQ

TOOLBOX INV REQ

RECONNECTED TRANSDUCER

REINSTALLED SCREWS

COMPLETE

COMPLETE

CHANDLER, T.

CHANDLER, T.

TAYLOR, B.

TAYLOR, B.

F

F

F

F

1.0

0.4

0.2

0.2

page 75 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

30 Nov 18

12:40

CONTROLLED EXCHANGE OF M/R BLADE S/N A007-12088 WITH ACFT 00-26866 M/R BLADE S/N A007-14166

✕

✕

✕

✕

✕

―

―

DISCONNECTED BLADE DE-ICE ELEC CONNECTOR

DISCONNECTED ANTI FLAP SPRING

REMOVED 2 EA BLADE PIN COTTER PINS

REMOVED 2 EA BLADE PINS

REMOVED BLADE ASSY

FOD CHECK DUE

TOOL BOX INV

page 76 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 E

06 Dec 18

14:05

controlled exchange of the ARN-123 receiver to ACFT 85-24435 required

✕

✕

✕

✕

✕

✕

removed mounting hardware from no.2 kick panel

removed no.2 kick panel

disconnected GS, MB, and NR connectors

disconnected 2 ARN-123 receiver radio connectors

loosened fasteners on receiver radio

removed ARN-123 receiver radio SN:1569

reinstalled mounting hardware

reinstalled kick panel

page 77 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

27 Dec 18

15:07

AIRCRAFT DISASSEMBLY REQUIRED FOR GROUND TRANSPORT TO MO-TASMG FOR DEPOT LEVEL REPAIRS

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

REMOVED L/H STAB HINGE FAIRING

REMOVED R/H STAB HINGE FAIRING

DISCONNECTED 2 EA STAB TO PYLON GROUNDS AT PYLONDISCONNECTED 2 EA STAB FORMATION LIGHT CANNON PLUGS AT PYLONREMOVED LOWER AFT TAIL PYLON FAIRING

DISCONNECTED J3, J4, J5 CONNECTORS ON AFT APR-39 BOX IN LOWER AFT T/R PYLON FAIRINGREMOVED STAB LIMIT SWITCH HDWR

REMOVED STAB TO STAB ACTUATOR ATTACHING HDWRREMOVED R/H STAB MOUNT BOLT

REMOVED L/H STAB MOUNT BOLT

REMOVED STABILATOR ASSY

REMOVE HARDWARE FROM FWD END SECTION III DRIVESHAFT REMOVE HARDWARE FROM AFT END OF SECTION III DRIVE SHAFT

page 78 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 2

✕ 8223750 A

27 Dec 18

15:07

AIRCRAFT DISASSEMBLY REQUIRED FOR GROUND TRANSPORT TO MO-TASMG FOR DEPOT LEVEL REPAIRS

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

REMOVE SECTION III DRIVE SHAFT

DISCONNECTED 2 EA T/R CABLES AT QUICK DISCONNECTSREMOVED L/H TAILCONE ACCESS PANEL

REMOVED R/H TAILCONE ACCESS PANEL

REMOVED PITCH BEAM NUT RETAINING SCREWS

REMOVED PITCH BEAM RETAINING NUT

REMOVED T/R PITCH BEAM

DISCONNECTED 4 EA T/R P/C LINKS AT PITCH BEAM

REMOVED OUTER RETENTION PLATE BOLTS

REMOVED OTBD RETENTION PLATE

REMOVED 2 EA T/R PADDLE ASSY

DISCONNECTED 4 EA T/R PADDLE DEICE CANNON PLUGSDRAINED T/R GEARBOX

page 79 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 3

✕ 8223750 A

27 Dec 18

15:07

AIRCRAFT DISASSEMBLY REQUIRED FOR GROUND TRANSPORT TO MO-TASMG FOR DEPOT LEVEL REPAIRS

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

DRAINED INTERMEDIATE GEARBOX

REMOVED T/R PYLON PIVOT BOLTS 2 EA

REMOVED 4 EA T/R PYLON TO TAILCONE BOLTS

REMOVED T/R PYLON ASSY

DISCONNECTED 11 EA ELECTRICAL CONNECTORS ON TAIL PYLON TO TAILCONE ATTACHMENTDISCON #2 MAIN FUEL HOSE FROM ELBOW

DISCON (2EA) #2 ENGINE DRAIN HOSES FROM REAR ENGINE DECK COMPARTMENT ELBOWSDISCON (2EA) #2 CANNON PLUGS FROM FIREWALL

DISCON P/A/S FROM #2 HMU

DISCON L/D/S FROM #2 HMU

DISCON BLEED AIR TUBE COUPLING FROM STARTER

LOOSENED (2EA) STARTER BLEED AIR TUBE CLAMPS FROM FIREWALLLOOSENED LOWER CROSS BLEED AIR TUBE CLAMP FROM FIREWALL

page 80 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 4

✕ 8223750 A

27 Dec 18

15:07

AIRCRAFT DISASSEMBLY REQUIRED FOR GROUND TRANSPORT TO MO-TASMG FOR DEPOT LEVEL REPAIRS

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

RMVD (2EA) CLAMPS SECURING ENGINE CONTROL CABLES TO IPS DUCTLOOSENED #2 IPS BLOWER DUCT CLAMP

RMVD #2 IPS BLOWER DUCT

UNCLAMPED LOOP CLAMP FROM #2 DESWIRL DUCT

DISCON #2 HIGH SPEED SHAFT FROM GIMBAL

RMVD #2 FORWARD SUPPORT TUBE (6EA) MOUNT BOLTSRMVD INBOARD ENGINE MUNT BOLT From #2 engineRMVD OUTBOARD ENGINE MOUNT BOLT FROM #2 ENGINERMVD CENTER ENGINE MOUNT BOLT FROM #2 ENGINERMVD #2 ENGINE

RMVD #2 ENGINE CROTCH ASSY FROM SUPPORT TUBERMVD AFT MOUNT LINK (2EA) BOLTS FROM ENGINE COMBUSTOR SECTION FROM #2 ENGINERMVD (2EA) AFT MOUNT LINKS FROM #2 ENGINE

page 81 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 5

✕ 8223750 A

27 Dec 18

15:07

AIRCRAFT DISASSEMBLY REQUIRED FOR GROUND TRANSPORT TO MO-TASMG FOR DEPOT LEVEL REPAIRS

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INSTALLED ENGINE SWIRL CAGE ON #2 ENGINE

INPUT MODUEL FLANGE NUT TQ CHECK REQUIRED PRIOR TO ENGINE INSTALLATION ON #2 SIDEFOD CHECK REQUIRED

TOOLBOX INVENTORY REQUIRED

LOOSENED CHIP DETECTOR (2EA) MOUNT BOLTS

RMVD #2 ENGINE CHIP DETECTOR

ELECTRICAL CHIP DETECTOR CIRCUIT TEST REQUIRED

REMOVED HARDWARE FROM MAIN TRANSMISSION FORWARD SHROUD REMOVED MAIN TRANSMISSION FORWARD SHROUDREMOVED HARDWARE FROM FWD LH XMSN SHROUD REMOVED FWD LH XMSN SHROUD

REMOVED HARDWARE FROM L/H UPPER AFT EIBF BRACKETREMOVED L/H UPPER AFT EIBF BRACKET

page 82 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 6

✕ 8223750 A

27 Dec 18

15:07

AIRCRAFT DISASSEMBLY REQUIRED FOR GROUND TRANSPORT TO MO-TASMG FOR DEPOT LEVEL REPAIRS

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DISCONNECTED PRESSURE AND RETURN QD'S (6EA) FROM HYDRAULIC PUMPS (3EA)REMOVED HARDWARE FROM AFT XMSN SCHROUD

REMOVED AFT XMNS SHROUD

DISCON MAIN FUEL HOSE FROM ELBOW (#1 ENG)

DISCON (2EA) ENGINE DRAIN HOSES FROM REAR ENGINE DECK COMPARTMENT ELBOW (#1 ENG)DISCON (2EA) CANNON PLUGS FROM FIREWALL (#1 ENG)DISCON P/A/S FROM HMU (#1 ENG)

DISCON L/D/S FROM HMU (#1 ENG)

DISCON BLEED AIR TUBE COUPLING FROM STARTER (#1 ENG)LOOSENED (2EA) STARTER BLEED AIR TUBE CLAMPS FROM FIREWALL (#1 ENG)LOOSENED LOWER CROSS BLEED AIR TUBE CLAMP FROM FIREWALL (#1 ENG)LOOSENED IPS BLOWER DUCT CLAMP (#1 ENG)

RMVD IPS BLOWER DUCT (#1 ENG)

page 83 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 7

✕ 8223750 A

27 Dec 18

15:07

AIRCRAFT DISASSEMBLY REQUIRED FOR GROUND TRANSPORT TO MO-TASMG FOR DEPOT LEVEL REPAIRS

✕

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―

―

UNCLAMPED LOOP CLAMP FROM DESWIRL DUCT (#1 ENG)DISCON HIGH SPEED SHAFT FROM GIMBAL (#1 ENG)

RMVD FORWARD SUPPORT TUBE (6EA) MOUNT BOLTS (#1 ENG)RMVD INBOARD ENGINE MOUNT BOLTS (#1 ENG)

RMVD OUTBOARD ENGINE MOUNT BOLTS (#1 ENG)

RMVD CENTER ENGINE MOUNT BOLT (#1 ENG)

RMVD #1 ENGINE

RMVD #1 ENGINE CROTCH ASSY FROM SUPPORT TUBERMVD AFT MOUNT LINK (2EA) BOLTS FROM ENGINE COMBUSTOR SECTION (#1 ENG)RMVD (2EA) AFT MOUNT LINKS (#1 ENG)

INSTALLED ENGINE SWIRL CAGE (#1 ENG)

INPUT MODULE FLANGE NUT TQ CHECK REQUIRED PRIOR TO ENGINE INSTALLATION (#1 ENG)TOOLBOX INVENTORY REQUIRED

page 84 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 8

✕ 8223750 A

27 Dec 18

15:07

AIRCRAFT DISASSEMBLY REQUIRED FOR GROUND TRANSPORT TO MO-TASMG FOR DEPOT LEVEL REPAIRS

―

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―

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FOD CHECK REQUIRED

LOOSENED CHIP DETECTOR (2EA) MOUNT BOLTS (#1 ENG)RMVD #1 ENG CHIP DETECTOR

ELECTRICAL CHIP DETECTOR CIRCUIT TEST REQUIRED (#1 ENG)REMOVED HARDWARE FROM FWD R/H XMNS SCHROUDDISCONNECTED BLEED AIR LINE (METAL TUBE)(5/8 NUT) AT L/H "T" ON BLEED AIR TUBE ON #2 SIDE OF AIRCRAFT. REMOVED BLEED AIR TUBE COUPLING AT HEATER MIXER VALVE.REMOVED BLEED AIR TUBE COUPLING AT CONNECTION JUST RIGHT OF XMSN.REMOVED FWD R/H XMSN SCHROUD

REMOVED HARDWARE SECURING P899 TO L/H FWD XMSN SHROUD (IBF CONNECTION)REMOVED HARDWARE SECURING P*** TO R/H FWD XMSN SHROUD (IBF CONNECTION)DISCONNECTED IVHMS ELEC CONN P8327 AT CONNECTION AT #2 ENGINE FIREWALLDISCONNECTED IVHMS ELEC CONN P8329 AT CONNECTION JUST TO THE RIGHT OF R/H MAIN XMSN MOUNT FOOT

page 85 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 9

✕ 8223750 A

27 Dec 18

15:07

AIRCRAFT DISASSEMBLY REQUIRED FOR GROUND TRANSPORT TO MO-TASMG FOR DEPOT LEVEL REPAIRS

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REMOVED BRACKET AND HARDWARE (3EA) FROM BOTTOM OF #2 GIMBLE DISCONNECTED BLEED AIR TUBE AT COUPLING ON CROSSBLEED TUBEREMOVED LOOP CLAMP SECURING BLEED AIR TUBE TO #2 ENG FIREWALLDISCONNECTED TAIL TAKE OFF IVHMS ELECTRICAL CONNECTOR P8325 AT XMSN DIP STICKREMOVED LOOP CLAMP SECUREING IVHMS WIRING HARNESS TO XMSN DIP STICKDISCONNECTED ELECTRICAL CONNECTOR P8337R FROM CONNECTION AT GUST LOCK BRACKETREMVOED NUT AND WASHER SECURING ELECTRICAL CONNECTOR P8337R FROM STUD JUST FWD OF CONNECTION AT GUST LOCK BRACKETDISCONNECTED STATIONARY SWASHPLATE ACCELOROMETER MOUNT (3/4 NUT)REMOVED 2EA LOOP CLAMP SECURING SWASHPLATE INTERRUPTER WIRING HARNESS TO STATIONARY SWASHPLATE.DISCONNECTED INTERRUPTER ELECTRICAL CONNECTOR P8333 FROM L/H SIDE OF STATIONARY SWASHPLATE CONNECTIONDISCONNECTED R/H MAIN XMNS WIRING HARNESS P400 FROM DECH BELOW #2 INPUT/ACCESSORY MOD.DISCONNECTED L/H MAIN XMNS WIRING HARNESS P401 FROM DECH BELOW #1 INPUT/ACCESSORY MOD.DISCONNECTED IVHMS ELECTRICAL CONNECTOR FROM CONNECTION AT FWD OIL COOLER COMPARTMENT FRAME. (WHERE THE AFT SCHROUD ATTACHES

page 86 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 10

✕ 8223750 A

27 Dec 18

15:07

AIRCRAFT DISASSEMBLY REQUIRED FOR GROUND TRANSPORT TO MO-TASMG FOR DEPOT LEVEL REPAIRS

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DISCONNECTED ELEC CONNECTOR P432 FROM NO. 2 HYDRAULIC PUMPDISCONNECTED ELEC CONNECTOR P447 FROM NO. 1 HYDRAULIC PUMPDISCONNECTED LEADS (4EA) FROM NO. 2 GENERATORREMOVED LOOP CLAMP SECURING NO. 2 GEN WIRING HARNESS TO GENERATORDISCONNECTED ELEC CONNECTOR P277 FROM NO. 2 GENERATORDISCONNECTED ELEC CONNECTOR P250 FROM NO. 2 GENERATORREMOVED BRACKET AND HARDWARE (3EA) FROM BOTTOM OF #1 GIMBLE DISCONNECTED IVHMS ELEC CONN P8338R AT CONNECTION JUST TO THE LEFT OF L/H MAIN XMSN MOUNT FOOTDISCONNECTED #2 ACCESSORY MOD IVHMS ELEC CONNECTOR P8330 FROM CONNECTION JUST BELOW #2 GENERATORDISCONNECTED #1 ACCESSORY MOD IVHMS ELEC CONNECTOR P8339 FROM CONNECTION ON #1 GENERATORREMOVED LOOP CLAMP ATTACHING #1 ACCESSORY MOD IVHMS ELEC CONNECTOR WIRE P8339 FROM #1 GENERATOR BRACKETDISCONNECTED LEADS (4EA) FROM NO. 1 GENERATORREMOVED LOOP CLAMP SECURING NO. 1 GEN WIRING HARNESS TO GENERATOR

page 87 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 11

✕ 8223750 A

27 Dec 18

15:07

AIRCRAFT DISASSEMBLY REQUIRED FOR GROUND TRANSPORT TO MO-TASMG FOR DEPOT LEVEL REPAIRS

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DISCONNECTED ELEC CONNECTOR P278 FROM NO. 1 GENERATORDISCONNECTED ELEC CONNECTOR P251 FROM NO. 1 GENERATORREMOVED SPRING PIN AND SAFETY SUCURING #1 LDS CABLE TO CLEVIS AT MIXER. *****(REINSTALLED SPRING PIN IN ORIGINAL HOLE ON CLEVIS)*****REMOVED SPRING PIN AND SAFETY SUCURING #2 LDS CABLE TO CLEVIS AT MIXER. *****(REINSTALLED SPRING PIN IN ORIGINAL HOLE ON CLEVIS)*****REMOVED HARDWARE FROM #1 ACCESSORY MOD BRACKET SECURING LDS CABLE TO BRACKETREMOVED HARDWARE FROM #2 ACCESSORY MOD BRACKET SECURING LDS CABLE TO BRACKETDISCONNECTED DRAIN TUBE FROM BOTTOM OF #1 HYDRAULIC PUMPDISCONNECTED DRAIN TUBE FROM BOTTOM OF #2 HYDRAULIC PUMPREMOVED COTTER PIN FROM FWD PRIMARY SERVO INPUT CONTROL ROD AT PRIMARY SERVOREMOVED COTTER PIN FROM AFT PRIMARY SERVO INPUT CONTROL ROD AT PRIMARY SERVOREMOVED COTTER PIN FROM LATERAL PRIMARY SERVO INPUT CONTROL ROD AT PRIMARY SERVOREMOVED HARDWARE FROM FWD PRIMARY SERVO INPUT CONTROL ROD AT PRIMARY SERVOREMOVED HARDWARE FROM AFT PRIMARY SERVO INPUT CONTROL ROD AT PRIMARY SERVO

page 88 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 12

✕ 8223750 A

27 Dec 18

15:07

AIRCRAFT DISASSEMBLY REQUIRED FOR GROUND TRANSPORT TO MO-TASMG FOR DEPOT LEVEL REPAIRS

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REMOVED HARDWARE FROM LATERAL PRIMARY SERVO INPUT CONTROL ROD AT PRIMARY SERVODISCONNCECTED #1 INPUT MOD TO MAIN XMSN FLANGE IVHMS ELECTRICAL CONNECTOR AT CONNECTION AT HYDRAULIC TUBING BELOW #1 ACCESSORY MOD.REMOVED COTTER PIN FROM AFT WALKING BEAM PIVOT BOLTREMOVED HARDWARE FROM AFT WALKING BEAM PIVOT BOLTREMOVED COTTER PIN FROM AFT WALKING BEAM AT LONG CONTROL RODREMOVED HARDWARE FROM AFT WALKING BEAM AT LONG CONTROL RODremoved hardware(3ea) connecting section 1 drive shaft flex coupling to tail takeoff flangeremoved hardware(3ea) connecting section 1 drive shaft flex coupling to oil cooler input flangeremoved hardware(3ea) connecting section 1 drive shaft flex coupling to aft end of drive shaftremoved main transmission mount hardware (8ea)

disconnected oil cooler (2ea) from at transmission

removed oil cooler compartment doors (2ea)

removed gust lock hardware and bushing at gust lock rod terminal.

page 89 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 13

✕ 8223750 A

27 Dec 18

15:07

AIRCRAFT DISASSEMBLY REQUIRED FOR GROUND TRANSPORT TO MO-TASMG FOR DEPOT LEVEL REPAIRS

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removed hardware securing gust lock lever to transmissiondisconnected upper hardware from aft tie rod

removed safeties (3ea) from forward support mounting hardwareremoved (3ea) hardware securing forward support to deckremoved transmission 5 pack. transmission SN: A265-00684REMOVED UPPER AND LOWER STRUT PANELS FROM LEFT AND RIGHT SIDES.DISCONNECTED FLIR ELECTRICAL CONNECTOR P23766R FROM AIRFRAMEREMOVED HARDWARE FROM CLAMP SECURING FLIR CABLE P23766R TO AIRCFRAMEREMOVED SAFETIES (4EA) FROM SCREWS ATTACHING FLIR TO MOUNT.REMOVED HARDWARE (8EA) ATTACHING FLIR TO MOUNT.REMOVED FLIR SN: CE0493 FROM MOUNT

STOWED LOWER ANTI COLLISION LIGHT

removed tail strut and jackpad fairings

page 90 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 14

✕ 8223750 A

27 Dec 18

15:07

AIRCRAFT DISASSEMBLY REQUIRED FOR GROUND TRANSPORT TO MO-TASMG FOR DEPOT LEVEL REPAIRS

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removed safeties from screws on rear middle support head for the HF antenna tubeloosened locking nuts from both sides of rear support for HF antennaloosened coupling nut between rear and front HF antenna tubesloosened screws on rear middle support head on HF antennaremoved rear HF antenna tube from supports

loosened locking nuts from both sides of front support for HF antenna tuberemoved safeties from front middle support for HF antenna tubeloosened screws on front middle support head for HF antenna tuberemoved front HF antenna tube from front support

removed 6 screws from VHF/UHF COMANT antenna

disconnected the VHF/UHF COMANT antenna

removed VHF/UHF COMANT antenna

REMOVED SAFETY FROM BATTERY TIEDOWNS

page 91 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 15

✕ 8223750 A

27 Dec 18

15:07

AIRCRAFT DISASSEMBLY REQUIRED FOR GROUND TRANSPORT TO MO-TASMG FOR DEPOT LEVEL REPAIRS

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LOOSENED 2 EA BATTERY TIEDOWNS

DISCONNECTED BATTERY RECEPTACLE

REMOVED ACFT BATTERY FOR STORAGE IN BATTERY SHOP

page 92 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

28 Dec 18

09:13

#1 & #2 ENGINE INLET REMOVAL REQUIRED FOR TRANSPORT TO MO TASMG

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―

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DISCON P823 FROM INLET (#1 ENG)

DISCON BLEED AIR COUPLING CLAMP FROM INLET

UNCLAMPED WATER WASH HOSE ASSY FROM INLET

DISCON FIRE EXTINGUISHER DISCHARGE TUBE FROM FIREWALLLOOSENED INLET COUPLING

RMVD #1 INLET

FOD CHECK REQUIRED

TOOLBOX INVENTORY REQUIRED

DISCON ICE DETECTOR CANNON PLUG P819 FROM FIREWALLDISCON P818 FROM ENGINE INLET

DISCON BLEED AIR COUPLING CLAMP FROM INLET

UNCLAMPED WATER WASH HOSE ASSY FROM INLET

DISCON FIRE EXTINGUISHER DISCHARGE TUBE FROM FIREWALL

page 93 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 2

✕ 8223750 A

28 Dec 18

09:13

#1 & #2 ENGINE INLET REMOVAL REQUIRED FOR TRANSPORT TO MO TASMG

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―

―

LOOSENED INLET COUPLING

RMVD #2 INLET

FOD CHECK REQUIRED

TOOLBOX INVENTORY REQUIRED

page 94 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 H

28 Dec 18

12:54

rescue hoist removal required to facilitate depot level maitenance

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DISCONNECTED ELECTRICAL CONNECTORS 2 EA

REMOVED EXPANDABLE PINS 3 EA

REMOVED BONDING JUMPERS 2 EA

REMOVED UPPER RIGHT HAND STEP FAIRING 1 EA

FOD CHECK REQUIRED

TOOL BOX INVENTORY REQUIRED

page 95 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

/ 8223750 A

02 Jan 19

10:48

cabin overhead soundproofing requires removal for aircraft shipment to TASM-G

/

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REMOVED FWD L/H SOUNDPROOFING

REMOVED FWD R/H SOUNDPROOFING

REMOVED "H" BAR BRACKETS 4 EACH

REMOVED CENTER SOUNDPROOFING FWD OF TROOP SEATSREMOVED SOUNDPROOFING FROM L/H AND R/H OF DRIP PANREMOVED AFT L/H AND R/H SOUND PROOFING SUPPORTSremoved aft soundproofing support (just behind drip pan)removed fwd soundproofing support (just behind "H" bar)

page 96 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

/ 8223750 A

07 Jan 19

12:37

CONTROLLED EXCHANGE OF RED MR BLADE DEICE CABLE FROM AIRCRAFT 8223750 TO AIRCRAFT 8726001

✕ H✕ H✕ H― E― E

DISCONNECTED RED MR BLADE DEICE CABLE CANON PLUGS, 3 EARMVD HARDWARE SECURING RED MR BLADE DEICE CABLE TO MAIN ROTOR SPINDLE BRACKETS, 2EARMVD RED MR BLADE DEICE CABLE

TOOLBOX INV DUE

FOD CHECK DUE

RECONNECTED CANON PLUGS, 2 EA (RED MR BLADE NOT INSTALLED)REPLACED HARDWARE, TQD TO 1/6TH TO 1/3RD TURN PAST SHARP RISE IN TQinstalled green tag cable from 26-001 on aircraft (failed continuity check)INV COMP

FOD CHECK COMP

RIDER, J.

RIDER, J.

RIDER, J.

RADLEY, J.

RADLEY, J.

F

F

F

F

F

0.2

0.2

0.2

0.2

0.2

page 97 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

/ 8223750 A

09 Jan 19

13:39

BOTH L/H AND R/H EYEBROW FAIRING SEALS TORN

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REMOVED L/H FAIRING

REMOVED R/H FAIRING

page 98 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

― 8223750 A

11 Jan 19

10:03

CONTROLLED EXCHANGE OF OAT SENSOR P/N 132LU FROM ACFT 8223750 TO ACFT 8826036

― B― B✕

✕

✕

FOD CK REQ'D

TOOLBOX INVENTORY REQ'D

DISCONNECTED ELECTRICAL CONNECTOR P1021R FROM OAT SENSORRMVD HDWR SECURING OAT SENSOR

RMVD OAT SENSOR

FOD CHECK COMPLETE

INVENTORY COMPLETE

RECONNECTED CONNECTOR TO OAT SENSOR SWAPPED FROM ACFT 8826036 FROM CONTROLLED EXCHANGEREINSTALLED HARDWARE

INSTALLED OAT SENSOR FROM ACFT 8826036 PER CONTROLLED EXCHANGE

SMITH, A.

SMITH, A.

HALE, T.

HALE, T.

HALE, T.

F

F

F

F

F

0.4

0.4

0.4

0.5

0.6

page 99 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

17 Jan 19

10:18

CONTROLLED EXCHANGED HYD PUMP S/N: 256139ABR TO ACFT 88-26036

✕

✕

―

―

LOOSENED HDWR SECURING NO. 1 HYD PUMP MODULEREMOVED NO. 1 HYD PUMP MODULE SN: 256139ABRFOD CHECK DUE

TOOLBOX INV DUE

page 100 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

02 Apr 19

08:39

REMOVAL R/H MLG STRUT TO FOM

✕

✕

✕

✕

✕

REMOVED 2EA COTTER PINS FROM UPPER AND LOWER MOUNTING HARDWARE.REMOVED 2EA NUTS FROM UPPER AND LOWER MOUNTING HARDWARE.REMOVED BOLTS AND WASHERS FROM STRUT

REMOVED STRUT S/N C001-00709

DESERVICED NITO SIDE OF STRUT.

REPLACED

REINSTALLED, TORQUED TO 110-220 FOOT-POUNDS TQ WR S/N 15047REINSTALLED BOLTS AND WASHERSREINSTALLED STRUT S/N C001-00709RESERVICED

Keen, S.

Keen, S.

Keen, S.

Keen, S.

Keen, S.

F

F

F

F

F

0.1

0.5

0.5

0.5

0.5

page 101 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

10 Apr 19

09:01

REMOVED STABILATOR ACTUATORS SN B292-01168 AND U0914

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

―

―

REMOVED HARDWARE FROM CAMBERED FAIRING

REMOVED CAMBERED FAIRING

REMOVED HARDWARE FROM T/R UPPER RIGHT EOMS SENSOR COVERREMOVED SECTION IV DRIVE SHAFT COVER

REMOVED ELECTRICAL CONNECTOR FROM SECTION IV DRIVE SHAFT COVERREMOVED HARDWARE CONNECTING STAB ACTUATOR TO STABREMOVED HARDWARE FROM GROUNDING STRAP

REMOVED HARDWARE FROM UPPER STAB ACTUATOR TO AIRFRAMEDISCONNECT ACTUATOR ELECTRICAL CONNECTORS 2 EAREMOVED SCREWS 6 EA FROM ELECTRICAL CONNECTOR CANISTERFOD CHECK REQUIRED

TOOL BOX INVENTORY REQUIRED

page 102 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

24 Apr 19

07:45

DEMOD OF MWO 1-1520-237-50-108 EXTERNAL STORES SUPPORTS SYSTEM MOUNTED RESCUE HOIST REQUIRED.

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

REMOVED CONNECTORS P38 AND P20 FROM R/H BEADED PANEL DISCONNECTED K34 RELAY AND REMOVED RELAY PNL ASSY AND MOUNTING BRACKETS FROM R/H CABIN CEILING APPROX STA: 379 RBL: 20REMOVED DUMMY RECEPTACLES (2EA) FROM TOP OF R/H ESSS MOUNT APPROX STA: 300 RBL: 38 WL: 265REMOVED CONNECTORS J34 AND J35 FROM BRACKET ON TOP OF R/H ESSS MOUNT APPROX STA: 300 RBL: 35 WL: 265REMOVED WIRING FROM R/H MAIN BUNDLE STARTINIG AT K34 RELAY FORWARD TO J35 AND REMOVED THEM FROM J35REMOVED WIRING FROM CONNECTOR P39 AT K34 F.O.M.CUT WIRE FROM SPLICE AT J229 AND BOMBED REMAINING STUBREMOVED SCREWS FROM FWD FLOOR SECTION AND REMOVED FLOOR F.O.M.REMOVED L/H CP DUCT AND L/H 247 DUCT

REMOVED HOIST CONTROL BOX AND MOUNT

REMOVED L/H AND R/H BROOM CLOSETS

INSTALLED

INSTALLED

page 103 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

24 Apr 19

08:08

DEMOD OF MWO 1-1520-237-20-5 INTERIM MEDEVAC MISSION SUPPORT SYSTEM (IMMSS) PATIENT. A&B KIT

✕

✕

✕

✕

✕

✕

✕

REMOVED 60HZ CONVERTER HARNESS AT L/H AND R/H WALL STA: 276 AND PULLED WIRE BUNDLE UNDER THE FWD SECTION OF FLOOR AND STOWED WIRING AT APPROX STA: 276REMOVED ICS RELOCATION HARNESS FROM BACK OF CP SEAT AFT TO STA: 343 L/H MAIN CABIN WIRING HARNESSREMOVED 10 EA HARDPOINT ADAPTER SUBPLATES

REMOVED L/H GUNNER'S WINDOW INTERCOSTAL ASSEMBLYREMOVED R/H GUNNER'S WINDOW INTERCOSTAL INTERFACE ASSEMBLYREMOVED TROOP COMMANDER ICS ADAPTER

REMOVED ICS RELOCATION KIT

page 104 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

24 Apr 19

09:07

DEMOD OF MWO 1-1520-237-20-TDFM REQUIRED

✕ REMOVED TDFM9000 RADIO

page 105 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

24 Apr 19

09:13

DEMOD OF MWO 1-1520-237-50-115 TALON FORWARD LOOKING INFRARED (FLIR) SPONSON MOUNT REQUIRED.B KIT

✕

✕

✕

REMOVED JCU JOYSTICK ASSEMBLY

REMOVED 6 EA BOLTS FROM FWD MOUNT ASSEMBLYREMOVED FWD MOUNT ASSEMBLY

page 106 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

26 Apr 19

09:00

REMOVAL OF MAIN AND RESERVE FIRE BOTTLES REQUIRED

✕

✕

✕

✕

✕

✕

✕

DISCONNECTED WIRES FROM #1 AND #2 DISCHARGE OUTLET CARTRIDGES ON MAIN FIRE BOTTLEDISCONNECTED WIRES FROM #1 AND #2 DISCHARGE OUTLET CARTRIDGES ON RESERVE FIRE BOTTLEDISCONNECTED OVERBOARD DISCHARG TUBES FROM MAIN AND RESEVRE FIRE BOTTLESDISCONNECTED DISCHARGE TUBES FROM MAIN FIRE BOTTLEDISCONNECTED DISCHARGE TUBES FROM RESERVE FIRE BOTTLERMVD MAIN FIRE BOTTLE SN: 12617B2, AND HARDWARERMVD RESERVE FIRE BOTTLE SN: 18890B2, AND HARDWARE

page 107 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

― 8223750 A

14 May 19

07:51

REMOVAL OF UNIT PROPERTY EQUIPMENT REQUIRED FOR ACFT TRANSITION TO BEST PROGRAM

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

REMOVAL OF ARC-201 FM#1 R/T SER: 02511

REMOVAL OF ARC-201 FM#2 R/T 01882A

REMOVAL OF AUX FUEL QTY PANEL SER:03416

REMOVED IVHMU INDICATOR SER:80238

REMOVED APR-39 INDICATOR SER: SEE INSIDE

REMOVED HF CONTROL SER:2260

REMOVED KY-58 CONTROL SER:B04376

REMOVED KY-58 CONTROL SER:D01091

REMOVED HUD CONTROL SER:C04407

REMOVED ARC-201 FM#1 CONTROL SER: 02529A

REMOVED APR-39 AFT RECEIVER SER :1733

REMOVED APR-39 SPIRAL ANTENNA 4 EACH

REMOVED HARDWARE FROM 4 EACH APR-39 SPIRAL ANTENNAS 16 EACH SCREWS

INSTALLED BLANKING PLATES AND HARDWARE

ROBERTSON, T.F 1.0

page 108 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 2

― 8223750 A

14 May 19

07:51

REMOVAL OF UNIT PROPERTY EQUIPMENT REQUIRED FOR ACFT TRANSITION TO BEST PROGRAM

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

―

―

REMOVED KY-58 R/T SER:28191

REMOVED KY-58 R/T SER:27158

REMOVED ARP-39 RECEIVER SER:5332 AND 4 EACH HARDWAREREMOVED APR-39 PROCESSOR SER:1123AA AND 4 EACH HARDWARE REMOVED IFM AMP SER:18135R

REMOVED HF R/T SER:223AA

REMOVED HUD SDC SER:E01742

REMOVED IVHMU BOX SER:00539 AND 4 EACH HARDWARE REMOVED HF AMP SER:2483AA

REMOVED QUADBAY ANTENNA AND MOUNTING HARDWARE DROPPED BFT PALET ASSY. TO REMOVE UNIT PROPERTY TOOL BOX INVENTORY DUE

FOD CHECK DUE

REINSTALLED ANTENNA

REINSTALLED BFT PALLET

ROBERTSON, T.

ROBERTSON, T.

F

F

1.0

1.0

page 109 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 3

― 8223750 A

14 May 19

07:51

REMOVAL OF UNIT PROPERTY EQUIPMENT REQUIRED FOR ACFT TRANSITION TO BEST PROGRAM

✕

✕

✕

REMOVED BFT MOUNTING BOLTS AND WASHERS TWO EACH REMOVED APR-39 BLADE ANTENNA AND 6 EACH HARDWARE REMOVED APR-39 CONTROL SER:A1380CC

REINSTALLED MOUNTING BOLTS AND HARDWARE TRQ: 480-690 IN LBS. BOLTS TRQ SET AT 550 IN LBSINSTALLED HARDWARE AND BLANKING PLATE

ROBERTSON, T.

ROBERTSON, T.

F

F

1.0

1.0

page 110 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

29 May 19

08:04

RH LOWER MLG SHOCK STRUT AIR VALVE REQUIRES REPLACEMENT DUE TO FAILURE TO HOLD AIR PRESSURE IAW TM 1-1520-237-23&P WP 0648

✕

✕

✕ B✕ B―

―

REMVED YELLOW CAP FROM SERVICE PORT IAW TM 1-1520-237-23&P WP 0648LOOSENED OUTER HEXNUT TO DE-SERVICE STRUT IAW TM 1-1520-237-23&P WP 0648REMOVED AIR VALVE FROM STRUT IAW TM 1-1520-237-23&P WP 0648RMVD O-RING FROM AIR VALVE IAW TM 1-1520-237-23&P WP 0648FOD CHECK DUE IAW GOP

TOOLBOX INVENTORY DUE IAW GOP

Replaced IAW TM 1-1520-237-23&P WP 0648 Replaced IAW TM 1-1520-237-23&p wp 0648

BULLOCK, M.

BULLOCK, M.

F

F

0.3

0.3

page 111 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

31 May 19

08:15

RMVD ENGINE AIR INLETS FOR BEST PROGRAM SN CHECK IAW TM 1-1520-237-23&P WP 0688

✕

✕

✕

✕

✕

✕

✕

✕

✕

✕

―

―

RMVD CLAMP SECURING BLEED AIR TUBE TO LH ENGINE AIR INLET IAW TM 1-1520-237-23&P WP 0688RMVD CLAMP SECURING BLEED AIR TUBE TO RH ENGINE AIR INLET IAW TM 1-1520-237-23&P WP 0688RMVD CLAMP SECURING WATER WASH HOSE TO LH ENGINE AIR INLET IAW TM 1-1520-237-23&P WP 0688RMVD CLAMP SECURING WATER WASH HOSE TO RH ENGINE AIR INLET IAW TM 1-1520-237-23&P WP 0688RMVD FIRE EXTINGUISHER TUBE FROM LH ENGINE AIR INLET IAW TM 1-1520-237-23&P WP 0688RMVD FIRE EXTINGUISHER TUBE FROM RH ENGINE AIR INLET IAW TM 1-1520-237-23&P WP 0688DISCONNECTED ELECTRICAL CONNECTOR FROM LH ENGINE AIR INLET IAW TM 1-1520-237-23&P WP 0688DISCONNECTED ELECTRICAL CONNECTORS 2EA FROM RH ENGINE AIR INLET IAW TM 1-1520-237-23&P WP 0688RMVD V-BAND CLAMP SECURING LH ENGINE AIR INLET IAW TM 1-1520-237-23&P WP 0688RMVD V-BAND CLAMP SECURING RH ENGINE AIR INLET IAW TM 1-1520-237-23&P WP 0688FOD CHECK DUE IAW GOP

TOOLBOX INVENTORY DUE IAW GOP

page 112 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 A

31 May 19

11:42

Removed cartridge, impulse P/N: 1512AS121 S/N: 12350 iaw TM 1-1500-328-23 as per gov request.

―

―

fod check due as per gop

tool check due as per gop

page 113 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 E

03 Jun 19

08:38

RMVD AN/AAR-57 SAFE/ARM BOX

✕

✕

―

―

LOOSEN TURNLOCKS FASTENERS SECURING CHAFF CONTROL PENALDISCONNECT ELECTRICAL CONNECTOR P147 FROM J1FOD INSPECTION DUE

TOOL BOX INSPECTION DUE

page 114 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 E

03 Jun 19

09:29

RMVD AN/AAR-57 SAFE/ARM BOX. PN: A102853-101, NSN: 5930-01-576-8081, SN:006, AS PER GOV REQ IAW TM 1-1520-237-23&P WP3655

✕

✕

―

―

LOOSENED TURNLOCK FASTENERS SECURING COMPONENT TO ACFT IAW TM 1-1520-237-23&P WP1934DISCONNECTED ELECTRICAL CONNECTOR FROM SAFE ARM BOX. IAW TM 1-1520-237-23&P WP1934FOD CHECK DUE IAW GOP

TOOLBOX INVENTORY DUE IAW GOP

page 115 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 E

03 Jun 19

09:53

RMVD RECEIVER TRANSMITTER, RT1518C/ARC-164 (4). PN: 901974-806, NSN: 5821-01-352-7209, SN:MO1146 AS PER GOV REQ IAW TM 1-1520-237-23&P WP4437

✕

✕

―

―

LOOSEN TURN LOCKS SECURING COMPONENTTO ACFT IAW TM 1-1520-237-23&P WP 4213DISCONNECT CONNECTORS 2EA IAW TM 1-1520-237-23&P WP4213FOD CHECK DUEIAW GOP

TOOLBOX INVENTORY DUE IAW GOP

page 116 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 E

03 Jun 19

10:55

RMVD DISPLAY UNIT,RADAR CP-1252C/ASN-128. PN: SM-D-858886, NSN: 5841-01-399-5513 AS PER GOV REQ IAW TM 1-1520-237-23&P WP4423

✕

✕

―

―

―

LOOSEN TURN LOCKS 8 EA, SECURING COMPONENTS TO ACFT IAW TM 1-1520-237-23&P WP4110DISCONNECT CONNECTORS 3 EA IAW TM 1-1520-237-23&P WP4110FOD CHECK DUE IAW GOP

TOOLBOX INVENTORY DUE IAW GOP

SN 0564B Swearengin, J.F 0.1

page 117 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 E

03 Jun 19

11:49

RMVD CONTROL TRANSMITTER, RADAR C-12664/APX. PN: 1008940P-4, NSN: 5841-01-493-8789 , SN: 0918 AS OER GOV REQ IAW TM 1-1520-237-23&P

✕

✕

―

―

LOOSEN TURNLOCKS SECURING COMPONENT TO ACFT IAW TM 1-1520-237-23&P WP4361DISCONNECT CONNECTOR FROM CONPONENT 1 EA IAW TM 1-1520-237-23&P WP 4361 FOC CHECK DUE IAW GOP

TOOLBOX INVENTORY DUE IAW GOP

page 118 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

✕ 8223750 E

03 Jun 19

12:04

RMVD RECEIVER TRANSMITTER, RADAR RT-1193/ASN-128 PN: SM-D-858489-2, NSN: 5841-01-318-0654 , SN: 316C. AS PER GOV REQ IAW TM 1-1520-237-23&P WP4423

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RMVD SCREWS AND WASHERS 8 EA FROM COMPONENT IAW TM 1-1520-237-23&P WP4108RMVD SCREW AND WASHER FROM GORUNDING POINT FROM COMPONENT IAW TM 1-1520-237-23&P WP4108DISCONECT CONNECOTER FROM COMPONENT IAW TM 1-1520-237-23&P WP4108FOD CHECK DUE IAW GOP

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DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

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03 Jun 19

12:19

RMVD CHAFF CONTROL PANEL AN/AAR-57PN: A102859-101, NSN: 1055-01-576-8810 , SN: 0254. AS PER GOV REQ IAW TM 1-1520-237-23&P WP3656

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LOOSEN TURN LOCKS 2 EA, SECURING COMPONENTS TO ACFT IAW TM 1-1520-237-23&P WP1942DISCONNECT CONNECTOR FORM CONPONENT IAW TM 1-1520-237-23&P PW1942FOD CHECK DUE IAW GOP

TOOLBOX INVENTORY DUE IAW GOP

page 120 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

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03 Jun 19

12:33

RMVD AN/AAR-57 RELAY BOX. PN: A100604-101, SN:0658, AS PER GOV REQ IAW TM 1-1520-237-23&P WP3308

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RMVD SCREWS AND WASHERS 4 EA FROM CONPONENT IAW TM 1-1520-237-23&P WP1936DISCONNECT ELECTRICAL CONNECTOR 5EA FROM CONPONENT IAW TM 1-1520-237-23&P WP1936FOD CHECK DUE IAW GOP

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page 121 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

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03 Jun 19

12:46

RMVD AN/AAR-57 RELAY BOX. PN: A100605-101, SN:1579, AS PER GOV REQ IAW TM 1-1520-237-23&P WP3308

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RMVD SCREWS AND WASHERS 4 EA FROM CONPONENT IAW MWO 1-1520-237-50-93DISCONNECT ELECTRICAL CONNECTOR 5EA FROM CONPONENT IAW MWO 1-1520-237-50-93FOD CHECK DUE IAW GOP

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page 122 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

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03 Jun 19

14:49

RMVD DISTRBUTION BOX CWMS PN:A100605-101 NSN: 6110-01-576-2486 SN:0658 AS PER GOV REQ TM 1-1520-237-23&P WP1939

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RMVD SCREWS AND WASHERS 4 EA FROM CONPONENT IAW TM 1-1520-237-23&P WP1939DISCONNECT ELECTRICAL CONNECTOR 5EA FROM CONPONENT IAW TM1-1520-237-23&P WP1939FOD CHECK DUE IAW GOP

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page 123 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

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03 Jun 19

14:58

RMVD DISTRBUTION BOX CWMS PN:A100605-101 NSN: 6110-01-576-2486 SN: 1579 AS PER GOV REQ TM 1-1520-237-23&P WP1939

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RMVD SCREWS AND WASHERS 4 EA FROM CONPONENT IAW TM 1-1520-237-23&P WP1939DISCONNECT ELECTRICAL CONNECTOR 5EA FROM CONPONENT IAW TM1-1520-237-23&P WP1939FOD CHECK DUE IAW GOP

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page 124 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

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03 Jun 19

15:06

RMVD CONVERTER SIGNAL, DATA PN: P320A002-3 NSN: 5895-01-518-8783 SN: 2183 AS PER GOV REQ TM 1-1520-237-23&P WP4423

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DISCONNECT ELECTRICAL CONNECTORS AND COAXIAL CONNECTOR IAW TM 1-1520-237-23&P WP4110RMVD SCREWS, LOCKWASHERS, AND WASHERS 4 EA FROM CONPONENT IAW TM 1-1520-237-23&P WP4110FOD CHECK DUE IAW GOP

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page 125 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

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04 Jun 19

07:57

RMVD MACHINE GUN MOUNT ASSY RH. PN: 70751-02023-044, NSN: 1005-01-141-3813 SN: N/A, AS PER GOV REQ IAW TM 1-1520-237-23&P WP1816

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RMVD NUT AND COTTER PIN IAW TM 1-1520-237-23&P WP1816FOD CHECK DUE IAW GOP

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SN 1533212 Swearengin, J.F 0.1

page 126 of 127 04 Jun 2019 1859 UTC

DA FORM 2408-13-2, OCT 97 RELATED MAINTENANCE ACTIONS RECORDDA FORM 2408-13-2, NOV 91, MAY BE USED For use of this form see DA PAM 738-751, the proponent agency is DCSLOG

DATE ____________________ PAGE ______1. STATUS 2. SERIAL NUMBER 3. SYSTEM CODE 4. TIME

5. FAULT DATE 6. FAULT NUMBER

7. FAULT

8. STA 9. RELATED MAINTENANCE ACTIONS 10. ACTION 11. PID 12. CAT 13. MMH

04 Jun 19 1

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04 Jun 19

08:03

RMVD MACHINE GUN MOUNT ASSY LH. PN: 70751-02023-044, NSN: 1005-01-141-3813 SN: N/A, AS PER GOV REQ IAW TM 1-1520-237-23&P WP1816

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RMVD NUT AND COTTER PIN IAW TM 1-1520-237-23&P WP1816FOD CHECK DUE IAW GOP

TOOLBOX INVENTORY DUE IAW GOP

SN 1533516 Swearengin, J.F 0.1

page 127 of 127 04 Jun 2019 1859 UTC