Upload
others
View
10
Download
0
Embed Size (px)
Citation preview
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
✕
―
―
―
✕
✕
―
✕
✕
✕
✕
✕
✕
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
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
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
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
―
―
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
―
✕
✕
―
✕
✕
✕
✕
✕
✕
✕
✕
✕
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
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
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
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
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
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
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
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
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
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
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
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
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
✕
✕
✕
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
✕
✕
✕
✕
✕
✕
―
―
✕
✕
✕
✕
✕
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
✕
✕
―
―
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
✕
✕
✕
✕
―
―
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
/
/
✕
/
/
✕
✕
✕
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
✕
✕
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
✕
✕
✕
―
―
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
TOOLBOX INVENTORY DUE IAW GOP
page 119 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
12:19
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
✕
✕
―
―
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
✕ 8223750 E
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
✕
✕
―
―
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
TOOLBOX INVENTORY DUE IAW GOP
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
✕ 8223750 E
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
✕
✕
―
―
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
TOOLBOX INVENTORY DUE IAW GOP
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
✕ 8223750 E
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
✕
✕
―
―
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
TOOLBOX INVETORY DUE IAW GOP
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
✕ 8223750 E
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
✕
✕
―
―
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
TOOLBOX INVENTORY DUE IAW GOP
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
✕ 8223750 E
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
✕
✕
―
―
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
TOOLBOX INVENTORY DUE IAW GOP
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
/ 8223750 W
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
/
―
―
―
RMVD NUT AND COTTER PIN IAW TM 1-1520-237-23&P WP1816FOD CHECK DUE IAW GOP
TOOLBOX INVENTORY DUE IAW GOP
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
/ 8223750 W
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
/
―
―
―
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