1. AIRCRAFT SERIAL NUMBER8424004
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 26 Oct 16 3 07:12 PANOZZO, NICHOLAS
INTERIOR TAILCONE WORK PLATFORM RMVD FROM ACFT
5679.3 O G 2
ROBIE TANK INSTALLED, WORK PLATFORM IS LOCATED IN ACFT 84-24(004) PARTS BIN LOCATED AT AR AASF00 ,
Ⓧ A 15 Mar 17 1001 09:38 KLATT, STEVEN
USE OF PERSONAL RESTRAINT TETHER RESTRICTED PER H-60-17-ASAM-07
5749.8 O O 2
00 ,
― A 21 Jun 17 2 07:01 PANOZZO, NICHOLAS
"COMPLY WITH REQUIREMENTS OF H-60-17-ASAM-11 FUEL HOSE BORESCOPE INSPECTION, BY 22 APR 2021"
5799 O G 2
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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
/ A 25 Apr 18 3 12:08 MCNEAL, AARON
APR39 BOTH REAR QUADRANT RADAR DETECTORS FAIL DURING TEST
5897.9 G G 2
NEED APR-39 FSR 19 ,
Ⓧ A 07 Jan 19 1 07:39 Panozzo, Nicholas
AIRCRAFT RESTRICTED FROM KNOWN HOSTILE ENVIRONMENTS DUE TO FAILURE OF APR-39 SYSTEM.
5948.9 K G 2
NEED APR-39 FSR 02 ,
/ E 26 Feb 19 1 14:55 BREWER, COLE
HF radio inop. Displays RT-CDU COMM FAIL.
5974.3 G G 4
Need to hang test a RT 19D01 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 07 May 19 1 12:30 Panozzo, Nicholas
"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."
5987.7 O G 2
TO BE COMPLETED AT THE NEXT XMSN REMOVAL00 ,
/ A 08 Nov 19 1 09:10 JOHNSON, JEREMIAH
REMOVED SEALING COMPOUND FROM T/R BLADE, SN A009-02397 PER H-60-17-SOF-05 AT 6229.8 AIRCRAFT HOURS
6101 K G 2
00 ,
/ A 08 Nov 19 2 09:11 JOHNSON, JEREMIAH
REMOVED SEALING COMPOUND FROM T/R BLADE, SN A009-01689 PER H-60-17-SOF-05 AT 6229.8 AIRCRAFT HOURS
6101 K G 2
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 31 Jan 20 1 06:03 JOHNSON, JEREMIAH
DURING NEXT REMOVAL/DISASSEMBLY/PMI M/R SHAFT NUT REQUIRES SN# MSG19770 TO BE STAMPED ON NUT IAW H-60-19-ASAM-06
6120.9 O G 2
06A18 ,
/ A 11 Feb 20 1 16:22 SMITH, AIDAN
AFT XMSN SUPPORT BEAM HAS 2 (EA) LOOSE FASTENERS ON AFT SIDE LOCATED FS:362 WL:269 BL:2
6127.4 B G 2
00 ,
― A 01 Apr 20 1 08:59 RANEY, WINSTON
AHRS PIN FILTER ADAPTER REQUIRES REMOVAL PER H-60-20-AMAM-04 BY 04 MAR 21
6142.4 K G 2
02 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 06 May 20 1 09:31 JOHNSON, JEREMIAH
INITIATE DA FORM 2408-18 NUMBERS A860,A861,A862,A863 AT NEXT PMI 6229.8 BUT NOT TO EXCEED 20 APR 22.
6142.4 K G 2
05A02 ,
Ⓧ A 28 Aug 20 3 13:37 STACKS, MARCUS
OPERATE WITHIN LIMITATIONS AND RESTRICTIONS SPECIFIED IN AWR 980 R23 21 Jun 2019(HOIST EQUIPTMENT), AWR 1054 R21 1JUL20, 1127 R9 11 SEP 18 (HELI-BASKET); 1308 R13 24 APR 19 (GOODWRITCH -5 HOIST); 1309 R12 30 Jul 18 (OREGON AERO SEAT CUSHIONS); 1324 R15 25 SEP 18 (CMWS-ICMD);1348 R15 23 APR 20 (8 OR 12 POINT ICS); 1425 R22 13 JAN 20 (ICMD-CMWS); 1444 R10 29 MAY 20 (FOGS SINGLE CONFIGURATION); 1466 R9 23AUG19 (GARMIN GPSMAP); 1494 R12 14 JAN 20 (CMWS 5TH SENSOR A&B KITS); 1566 R7 01 FEB 19 (TITANIUM OR STAINLESS STEEL CABLE GUARD); 1692 R10 19MAR20 (NEW BLADE DE-ICE CONNECTOR); 1694 R7 29 JAN 20 DUAL STABILATOR CONTROLLER (DCS)); 1753 R9 17APR20 (DOPPLER GPS DGNS AN ASN128 B&D); 1800 R9 15 Jul 2019 (EDM AND BFT); 1858 R8 12JUN20 (ENCRYPTED AIRCRAFT WIRELESS INTERCOM SYS EWIS); AWR 2122 R5 9 Aug 2019 ( TECHNISONIC); 744 R11 24 JAN 19 (TOW BALLAST PLATES ); 1279 R9 20 MAY 20 (COCKPIT DOORS AND CABIN DOORS); 1452 R7 22 APR 19 (LC-6 DIGITAL CHRONOMETER); 1455 R9 10JUL20 (CAUTION ADVISORY PANEL CAP); 1500 R9 12JUL19 (IMPROVED ICS); 1513 R14 17APR20(INTERGRATED PERFORMANCE AND AIRCRAFT CONFIGURATION); 1532 R15 28JUL20 (200 GAL IFATS ); 1607 R11 13MAR20 (LCD CDU); 1682 R25 1 Aug 2019 (UH-60A W/ 701D OR 701C ENG W/AUTO RELIGHT & TRANSIENT DROOP); 1738 R6 18 JAN 19 (AN APX-118A);1763 R12 (HOIST); 1054 R21 1JUL20 (SEI BAMBI BUCKET); 1516 R12 07 FEB 19 (ELT EBC-406HM); 1787 R4 9 Aug 2019 (FM IMMUNE ARC-231); AWR 1967 R5 28 MAY 20 ( TALON FLIR);2002 R5 5OCT18 (IMMSS); AWR 2059 R3 13 AUG 19 (SHOUT NANO V), AWR 2120 R3 27SEP19 (GETAC V110 AV MSD), AWR 1750 R6 31MAR20 (ANVIS 6 NIGHT VISION GOGGLES)
6177.7 O G 1
00 ,
― A 01 Sep 20 4 13:37 JOHNSON, JEREMIAH
"ATTITUDE HEADING REFERENCE UNIT PN 765100-20 AND CONTROL UNIT PN 765200-20 REQUIRE REPLACEMEMNT PER H-60-20-AMAM-09 BY 25 AUG 22."
6177.7 O G 2
19E06 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 15 Sep 20 1 13:24 Generated, Computer
INSP A400 PMI-1.
6182.6 O O 1
00 ,
/ A 09 Oct 20 1 08:20 NEAL, BRANDON
MAIN MODULE DRIP PAN REMOVED TO FOM
6190.4 K G 2
02 ,
✕ A 09 Oct 20 6 12:46 Generated, Computer
INSP A110 PMS 40 HOUR INSPECTION FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 6190.9 AIRCRAFT HOURS
REFERENCE: TM 1-1520-237-PMS
6191.4 O O 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 09 Oct 20 7 12:50 SIMPSON, FREDERICK
MAIN MOD CHIP LIGHT ILLUMINATED DURING FLIGHT.
6191.4 K G 2
06A ,
✕ A 16 Oct 20 1 09:07 McCullough, Benjamin
REMOVAL OF PILOTS LEFT PEDAL MASTER BRAKE CYLINDER TO SLAVE CYLINDER ELBOW FITTING REQ FOR CONTROLLED EXCHANGE TO 8826036
6191.4 K O 2
03A02B ,
✕ A 16 Oct 20 2 12:31 ZIEMSKI, RYAN
CONTROL EXCHANGE IN PROGRESSO FTHE REMOVAL OF THE PILOTS AHRU TO AIRCRAFT 168
6191.4 K G 2
19
16 Oct 20 14:49 6191.4A 19E06A
REPLACED PILOT AHRU
FORDHAM, A.F 2.0
,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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
✕ E 16 Oct 20 1 14:46 ZIEMSKI, RYAN
pilot side gyro failure. gyro capsule light illuminated and stayed lit. gyro corrected itself when alt gyro switch was pressed.
6191.4 G G 3
19I ,
✕ A 17 Oct 20 1 10:15 lee, justin
#1 ENGINE REMOVED FOR MAINT
6191.4 K G 1
04A ,
✕ A 18 Oct 20 1 00:00 Generated, Computer
INSP A850 PMD DUE FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 17 OCT 2020
REFERENCE: LOCAL
6191.4 O O 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 18 Oct 20 3 10:43 Generated, Computer
#1 INLET REMOVAL
6191.4 O G 2
00 ,
✕ A 19 Oct 20 1 00:00 Generated, Computer
INSP A803 ANNUAL SN CHECK FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 18 OCT 2020
REFERENCE: LOCAL
6191.4 O O 1
00 ,
/ A 19 Oct 20 2 15:19 DOOLIN, PHILIP
AIRCRAFT REQ RMVL OF IMMSS PRIOR TO EXPORT TO BEST.
6191.4 S G 1
02 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 19 Oct 20 3 15:27 DOOLIN, PHILIP
R/H CARGO DOOR HANDLE WILL NOT UNLOCK.
6191.4 B G 2
02 ,
/ A 20 Oct 20 1 10:02 WIDEMAN, CHARLES
AIRCRAFT REQ RMVL OF EXTERNAL RESCUE HOIST PRIOR TO EXPORT TO BEST.
6191.4 E G 1
14B ,
✕ A 20 Oct 20 2 10:08 ZIEMSKI, RYAN
CONTROL EXCHANGE IN PROGRESS OF RADAR ALTIMETER ANTENNA CABLES FROM BOTH ANTENNAS TO RT
6191.4 K G 3
19E05 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 21 Oct 20 3 07:53 DOOLIN, PHILIP
CONTROLLED EXCHANGE OF CPLT PEDAL ADJUSTER ASSY TO AIRCRAFT 00-26851
6191.4 X G 1
11C02
27 Oct 20 00:00 6191.4N 11C02
CONTROLLED EXCHANGE CANCELLED DUE TO DAMAGED BEARING ON PEDAL ADJUSTER
,
✕ A 22 Oct 20 1 14:29 ZIEMSKI, RYAN
CONTROL EXCHANGE IN PROGRESS FOR THE REMOVAL OF THE POSITION LIGHT DIM AND BRIGHT TOGGLE SWITCH FOR UPPER CONSOLE
6191.4 K G 2
09C04E ,
✕ A 24 Oct 20 1 00:01 Generated, Computer
INSP A022 14 DAY FLYABLE STORAGE ENGINE RUN UP FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 23 OCT 2020
REFERENCE: TM 1-1520-237-23&P
6191.4 O O 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 27 Oct 20 2 08:10 WIDEMAN, CHARLES
UNIT EQUIPMENT/PROPERTY BOOK ITEMS REMOVAL REQUIRED FOR AIRCRAFT TRANSFER TO BEST
6191.4 X G 1
00 ,
✕ A 27 Oct 20 3 10:39 PARKER, CHARLES
CONTROLLED EXCHANGE OF #1 ENGINE AIR INLET COUPLING (ECCENTRIC) FROM ACFT 84-24004 TO ACFT 00-26862 PART DOC NUMBER W91FD993110002
6191.4 B G 1
02 ,
✕ E 29 Oct 20 1 10:05 SMITH, AIDAN
REMOVED TDFM-9000 TECHNISONIC RADIO
6191.4 B G 2
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 29 Oct 20 1 15:34 MURRAY, KOURTNEY
CONTROLLED EXCHANGE REQUIRED OF #1 ENG (SN: GE-E-375516C) WITH ACFT 83-23901 #1 ENG (SN: GE-E-762404C)
6191.4 B G 1
04A ,
✕ A 30 Oct 20 1 00:01 Generated, Computer
INSP A103 AIRCRAFT WASH DUE FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 29 OCT 2020
REFERENCE: TM 1-1500-344-23
6191.4 O O 1
00 ,
✕ E 30 Oct 20 1 00:01 Generated, Computer
INSP E220 EMERGENCY LOCATOR TRANSMITTER SELF-TEST (AS REQUIRED) FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 29 OCT 2020 OR 6307.6 AIRCRAFT HOURS
REFERENCE: AWR 1516 R12
6191.4 O O 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 30 Oct 20 2 00:01 Generated, Computer
INSP A115 LUBE REQUIRMENTS FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 29 OCT 2020 OR 6226.6 AIRCRAFT HOURS
REFERENCE: TM 1-1520-237-23&P
6191.4 O O 1
00 ,
✕ A 31 Oct 20 1 00:01 Generated, Computer
INSP A804 LOGBOOK RECON FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 30 OCT 2020
REFERENCE: LOCAL
6191.4 O O 1
00 ,
✕ A 01 Nov 20 1 00:00 Generated, Computer
INSP A177 90 DAY REVIEW/UPDATE OF 365-4 ENTRIES FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 31 OCT 2020
REFERENCE: AR 95-1
6191.4 O O 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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
✕ E 02 Nov 20 1 00:00 Generated, Computer
INSP E050 ARC-220 RADIO SET BATTERY INSPECTION OR REPLACE FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 01 NOV 2020
REFERENCE: TM 11-5821-357-12P
6191.4 O O 1
00 ,
✕ A 03 Nov 20 1 00:00 Generated, Computer
INSP A092 30 DAY SLAB BATTERY INSPECTION (D8565/11-1) FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 02 NOV 2020
REFERENCE: TM 11-6140-203-23 P
6191.4 O O 1
00 ,
✕ A 03 Nov 20 2 08:25 TIMMS, JARED
CONTROLLED EXCHANGE REQUIRED FROM 84-24004 #1 ENG HIGH SPEED SHAFT (SN: C845-09420) TO AIRCRAFT 83-23901
6191.4 B G 1
04A
03 Nov 20 08:33 6191.41 04A
WRITE UP ENTERED IN ERROR
MURRAY, K.F 0.1
,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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
✕ A 03 Nov 20 3 08:38 TIMMS, JARED
CONTROLLED EXCHANGE REQUIRED ON #1 ENG HIGH SPEED SHAFT FROM AIRCRAFT 83-23901 (SN: C845-02089) TO AIRCRAFT 84-24004 #ENG HIGH SPEED SHAFT (SN: C845-09420)
6191.4 B G 1
04A ,
✕ A 03 Nov 20 4 08:51 Halvorson, John
#2 ENG REMOVED DUE TO CONTROLLED EXCHANGE
6191.4 K G 1
04A ,
✕ A 03 Nov 20 5 08:54 Halvorson, John
#2 ENG INLET REMOVED DUE TO CONTROLLED EXCHANGE
6191.4 K G 1
04A11A ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 03 Nov 20 6 14:41 WIDEMAN, CHARLES
TAIL WHEEL FORK ASSEMBLY BUSHING ELONGATED
6191.4 K G 1
03B05B ,
✕ A 03 Nov 20 7 14:44 WIDEMAN, CHARLES
TAIL WHEEL FORK ASSEMBLY WEAR PLATE INCORRECTLY BONDED
6191.4 K G 1
03B05B ,
✕ A 05 Nov 20 2 09:54 NEAL, LEWIS
CONTROLLED EXCHANGE REQUIRED ON TAIL ROTOR PADDLE FROM AIRCRAFT 89-26168 (SN: A009-12817) TO AIRCRAFT 84-24004 TAIL ROTOR PADDLE (SN: A009-01689)
6191.4 O G 2
05B02 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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
✕ A 11 Nov 20 1 00:01 Generated, Computer
INSP A501 MAIN ROTOR BLADE SPAR PRESSURE CHECK FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 10 NOV 2020
REFERENCE: TM 1-1520-237-23&P
6191.4 O O 1
00 ,
✕ A 15 Nov 20 1 00:01 Generated, Computer
INSP A230 INSPECT BATTERY COMPARTMENT FOR CORROSION (SLAB) FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 14 NOV 2020
REFERENCE: MWO 1-1520-237-50-77
6191.4 O O 1
00 ,
✕ A 19 Nov 20 1 00:00 Generated, Computer
INSP A100 LH/RH ENGINE HISTORY RECORDER READINGS DUE FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 18 NOV 2020
REFERENCE: DA PAM 738-751
6191.4 O O 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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
✕ A 20 Nov 20 1 00:00 Generated, Computer
INSP A858 APU METER READINGS DUE ( EVENTS, HOURS) FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 19 NOV 2020
REFERENCE: LOCAL
6191.4 O O 1
00 ,
✕ A 25 Nov 20 1 08:41 Martin, Sean
CONTROLLED EXCHANGE OF OVERSPEED DRAIN VALVE SN- APM973HK FROM ACFT 824004- ACFT 8423981
6191.4 B G 1
04A
25 Nov 20 11:05 6191.4A 04A
CONTROLLED EXCHANGE COMP REPLACED W/ OVERSPEED DRAIN VALVE SN-APM303JN
Martin, S. F 0.4
,
✕ A 25 Nov 20 2 09:11 Martin, Sean
REMOVAL OF OVERSPEED DRAIN VALVE REQ TO COMPLETE CONTROLLED EXCHANGE
6191.4 B G 1
00
25 Nov 20 11:04 6191.4A 04A
REPLACED OSDV W/ SN-APM303JN
Martin, S. F 2.0
,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 30 Nov 20 1 00:01 Generated, Computer
INSP A530 AIRCRAFT EQUIPMENT INVENTORY (DA FORM 2408-17) FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 29 NOV 2020
REFERENCE: DA PAM 738-751
6191.4 O O 1
00 ,
✕ A 02 Dec 20 3 14:26 HALE, THOMAS
CONTROLLED EXCHANGE ENGINE SER # GEE763167C TO ACFT 26607
6191.4 K G 1
04A ,
✕ A 02 Dec 20 4 14:28 HALE, THOMAS
CONTOLLED EXCHANGE # 2 HSS SER # C845-00837 TO ACFT 26607
6191.4 K G 1
04A ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 03 Dec 20 1 00:00 Generated, Computer
INSP A553 AIRCRAFT WEIGHING INVENTORY (365-1) FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 02 DEC 2020
REFERENCE: AR 95-1
6191.4 O O 1
00 ,
✕ A 03 Dec 20 2 00:00 Generated, Computer
INSP A621 AIRCRAFT WEIGHING CLASS 2 FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 02 DEC 2020
REFERENCE: AR 95-1
6191.4 O O 1
00 ,
/ A 09 Dec 20 1 13:49 RADLEY, JAMES
RH CARGO DOOR OUTBOARD HANDLE INOP
6191.4 B K 2
02B02E02 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 10 Dec 20 1 00:00 Generated, Computer
INSP A538 FAT/OAT GAUGE INSPECTION/TEST FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 09 DEC 2020
REFERENCE: TM 1-1520-237-23&P
6191.4 O O 1
00 ,
✕ A 13 Dec 20 1 00:00 Generated, Computer
INSP A533 PITOT STATIC SYSTEM INSPECTION FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 12 DEC 2020
REFERENCE: TM 1-1520-237-23&P
6191.4 O O 1
00 ,
✕ E 04 Jan 21 1 07:38 Generated, Computer
INSP E015 ASN 128D DOPPLER GPS BATTERY REPLACEMENT FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 03 JAN 2021
REFERENCE: MWO 1-1520-237-50-92
6191.4 O O 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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
✕ E 11 Jan 21 1 12:41 Generated, Computer
INSP E351 REPLACE APX-118 TRANSPONDER BATTERY FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 10 JAN 2021
REFERENCE: TM 11-5895-1841-13P
6191.4 O O 1
00 ,
✕ A 11 Jan 21 1 12:41 Generated, Computer
INSP A160 90 DAY CORROSION INSPECTION FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 05 JAN 2021
REFERENCE: TM 1-1520-237-23&P
6191.4 O O 1
00 ,
✕ A 11 Jan 21 2 12:41 Generated, Computer
INSP A222 AMSS SURVIVAL KIT INSPECTION FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 09 JAN 2021
REFERENCE: TM 1-1680-377-13 P
6191.4 O O 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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
✕ E 11 Jan 21 2 12:41 Generated, Computer
INSP E040 APR-39 RADAR/LASER WARNING OPNL CHECK, 5841-01-236-8951 FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 06 JAN 2021
REFERENCE: TM 11-5841-294-12
6191.4 O O 1
00 ,
✕ A 12 Jan 21 1 00:00 Generated, Computer
INSP A534 FIRST AID KIT INSPECTION FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 01 JAN 2021
REFERENCE: TM 1-1500-204-23-1
6191.4 O O 1
00 ,
✕ E 14 Jan 21 1 00:01 Generated, Computer
INSP E145 AN/ARC-201A(V) SINCGARS HUB BATT REPL FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 13 JAN 2021
REFERENCE: TM 11-5821-333-12
6191.4 O O 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 14 Jan 21 1 00:01 Generated, Computer
INSP A532 COMPASS SWING / RMI FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 13 JAN 2021
REFERENCE: TM 1-1500-204-23-4
6191.4 O O 1
00 ,
✕ E 19 Jan 21 1 12:00 Generated, Computer
INSP E125 KY-58 PMCS/OPNL CHECK FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 15 JAN 2021
REFERENCE: TM 11-5810-262-23
6191.4 O O 1
00 ,
✕ A 21 Jan 21 2 13:22 REMILLARD, BARRY
CONTROLLED EXHANGE #2 ENGINE IPS BLOWER DUCT FROM AIRCRAFT 84-24004 TO AIRCRAFT 00-26851
6191.4 B G 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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
― A 21 Jan 21 3 14:22 REMILLARD, BARRY
NO.2 ENGINE IPS BLOWER DUCT HAS A 1/2 INCH CRACK JUST AFT OF SPINDLE CABLE ATTACHMENT POINT
6191.4 B G 1
00 ,
― A 27 Jan 21 1 16:22 Generated, Computer
SAFETY MESSAGE NUMBER: H-60-21-AMAM-01 DESCRIPTION: COMPLY WITH H-60-21-AMAM-01, MAIN LANDING GEAR DRAG BEAM INSPECTION, BY 06 JULY 2021.. IS DUE: 06 JUL 2021 CALENDAR
6191.4 O O 1
00 ,
✕ A 29 Jan 21 1 00:01 Generated, Computer
INSP A496 CF3BR FIRE EXTINGUISHER WEIGHT TEST INSPECTION FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 28 JAN 2021
REFERENCE: TM 1-1520-237-23&P
6191.4 O O 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 04 May 21 1 12:35 Generated, Computer
INSP A665 REPLACE FUEL CELL O-RING SEAL PN MS29513-215 FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 21 APR 2021
REFERENCE: H-60-14-AMAM-18
6191.4 O O 1
00 ,
✕ E 04 May 21 1 12:35 Generated, Computer
INSP E155 KY-58 BATTERY REPLACEMENT FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 08 FEB 2021
REFERENCE: TM 11-5810-262-23
6191.4 O O 1
00 ,
✕ A 04 May 21 2 12:35 Generated, Computer
INSP A304 LUBRICATE MIXER BELLCRANKS FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 21 APR 2021 OR 6234.8 AIRCRAFT HOURS
REFERENCE: TM 1-1520-237-23P
6191.4 O O 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 04 May 21 3 12:35 Generated, Computer
INSP A673 FUEL CELL CORROSION INSPECTION FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 21 APR 2021
REFERENCE: TM 1-1520-237-23P
6191.4 O O 1
00 ,
✕ A 04 May 21 4 12:35 Generated, Computer
INSP A675 FLIGHT CONTROL RODS INSPECTION FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 21 APR 2021
REFERENCE: TM 1-1520-237-23P
6191.4 O O 1
00 ,
✕ A 04 May 21 5 12:35 Generated, Computer
INSP A298 LUBRICATE TAIL WHEEL BEARINGS FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 21 MAR 2021 OR 6612.4 AIRCRAFT HOURS
REFERENCE: TM 1-1520-237-23P
6191.4 O O 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 May 21 6 12:35 Generated, Computer
INSP A670 CABIN TUB INSPECTION FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 21 APR 2021
REFERENCE: TM 1-1520-237-23P
6191.4 O O 1
00 ,
✕ A 04 May 21 7 12:35 Generated, Computer
INSP A502 INSPECT AND TEST GROUND RECEPTACLE IAW TM 1-1500-204-23 FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 WAS DUE. STATUS UPGRADED TO X ON: 21 MAR 2021
REFERENCE: TM 1-1520-237-23P
6191.4 O O 1
00 ,
― A 04 May 21 8 12:35 Generated, Computer
INSP A211 APU OIL SAMPLE FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 IS DUE. STATUS WILL UPGRADE TO X ON: 6627.4 AIRCRAFT HOURS OR 06 JUN 2021
REFERENCE: H-60-10-AMAM-11
6191.4 O O 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 04 May 21 9 12:35 Generated, Computer
INSP A116 INTERMEDIATE GEARBOX OIL SAMPLE FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 IS DUE. STATUS WILL UPGRADE TO X ON: 6627.4 AIRCRAFT HOURS OR 06 JUN 2021
REFERENCE: H-60-10-AMAM-11
6191.4 O O 1
00 ,
― A 04 May 21 10 12:35 Generated, Computer
INSP A117 TAIL GEARBOX OIL SAMPLE FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 IS DUE. STATUS WILL UPGRADE TO X ON: 06 JUN 2021 OR 6627.4 AIRCRAFT HOURS
REFERENCE: H-60-10-AMAM-11
6191.4 O O 1
00 ,
― A 04 May 21 11 12:35 Generated, Computer
INSP A302 LUBRICATE MAIN LANDING GEAR WHEEL BEARINGS FOR HCPTR UTILITY UH-60A CAGE: 78286 PN: UH-60A NSN: 1520010350266 SN: 8424004 IS DUE. STATUS WILL UPGRADE TO X ON: 6627.4 AIRCRAFT HOURS OR 10 JUN 2021
REFERENCE: TM 1-1520-237-23P
6191.4 O O 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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
✕ A 05 May 21 1 12:10 JUSTUS, NATHANIEL
Aircraft depaneled for BEST induction. Used TM 1-1520-237-23&P, SES GOP, and BEST SOW for reference.
6191.4 E G 1
00 ,
✕ A 05 May 21 2 12:12 JUSTUS, NATHANIEL
Removed CMWS junction box SN: 1672 per customer request IAW TM 1-1520-237-23&P WP 1915.
6191.4 E G 1
00 ,
✕ A 05 May 21 3 12:13 JUSTUS, NATHANIEL
Removed CMWS Safe/Arm control panel S/N 0536 per customer request IAW TM 1-1520-237-23&P WP 1911.
6191.4 E G 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 05 May 21 4 12:16 JUSTUS, NATHANIEL
Removed CMWS safety switch S/N 0003588 per customer request IAW TM 1-1520-237-23&P WP 1917.
6191.4 E G 1
00 ,
✕ A 05 May 21 5 12:19 JUSTUS, NATHANIEL
Removed CMWS relay box S/N 1672 per customer request IAW TM 1-1520-237-23&P WP 1913.
6191.4 E G 1
00 ,
✕ A 05 May 21 6 12:22 JUSTUS, NATHANIEL
Removed ARC-201 amplifier S/N 294BB per customer request IAW TM 1-1520-237-23&P WP 4225.
6191.4 E G 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 05 May 21 7 12:24 JUSTUS, NATHANIEL
Removed ARC-220 HF ampilier S/N 3374AA per customer request IAW TM 1-1520-237-23&P WP 4255.
6191.4 E G 1
00 ,
✕ A 05 May 21 8 12:27 JUSTUS, NATHANIEL
Removed ARC-220 HF radio control S/N A760AA per customer request IAW TM 1-1520-237-23&P WP 4262.
6191.4 E G 1
00 ,
✕ A 05 May 21 9 12:31 JUSTUS, NATHANIEL
Removed HUD converter S/N C00133 per customer request IAW TM 1-1520-237-23&P WP 4044.
6191.4 E G 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 05 May 21 10 12:35 JUSTUS, NATHANIEL
Removed cargo hook explosive cartridge S/N 12313 per customer request IAW TM 1-1520-237-23&P WP 1504.
6191.4 E G 1
00 ,
✕ A 05 May 21 11 12:37 JUSTUS, NATHANIEL
Removed DAGR/PLGR S/N 3342 per customer request IAW UH-60A/L BFT GPS Message Router.
6191.4 E G 1
00 ,
✕ A 05 May 21 12 12:40 JUSTUS, NATHANIEL
Removed Transponder control S/N 2310 per customer request IAW TM 1-1520-237-23&P WP 4337.
6191.4 E G 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 05 May 21 13 12:42 JUSTUS, NATHANIEL
Removed APR-39 Indicator S/N 2408AA per customer request IAW TM 1-1520-237-23&P WP 4188.
6191.4 E G 1
00 ,
✕ A 05 May 21 14 12:44 JUSTUS, NATHANIEL
Removed APR-39 Receiver (FWD) S/N CWC1592 and (AFT) S/N 3448 per customer request IAW TM 1-1520-237-23&P WP 4177, 4178.
6191.4 E G 1
00 ,
✕ A 05 May 21 15 12:47 JUSTUS, NATHANIEL
Removed APR-39 Detecting Control S/N 0301 per customer request IAW TM 1-1520-237-23&P WP 4180.
6191.4 E G 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 05 May 21 16 12:51 JUSTUS, NATHANIEL
Removed RH spiral antennas FWD S/N 7641 AFT S/N 4830AA per customer request IAW TM 1-1520-237-23&P WP 4186, 4187.
6191.4 E G 1
00 ,
✕ A 05 May 21 17 12:54 JUSTUS, NATHANIEL
Removed LH spiral antennas FWD S/N 4997AA AFT S/N 4294AA per customer request IAW TM 1-1520-237-23&P WP 4186, 4187.
6191.4 E G 1
00 ,
✕ A 05 May 21 18 12:55 JUSTUS, NATHANIEL
Removed Aux fuel quantity control head S/N 773 per customer request IAW TM 1-1520-237-23&P WP 1742.
6191.4 E G 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 05 May 21 19 12:58 JUSTUS, NATHANIEL
Removed UHF control head S/N 21156 per customer request IAW TM 1-1520-237-23&P WP 4189.
6191.4 E G 1
00 ,
✕ A 05 May 21 20 13:00 JUSTUS, NATHANIEL
Removed DOPPLER SDC S/N 2200 per customer request IAW TM 1-1520-237-23&P WP 4079, 4086.
6191.4 E G 1
00 ,
✕ A 05 May 21 21 13:02 JUSTUS, NATHANIEL
Removed DOPPLER CDU S/N 0880B per customer request IAW TM 1-1520-237-23&P WP 4073.
6191.4 E G 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 05 May 21 22 13:03 JUSTUS, NATHANIEL
Removed DOPPLER antenna S/N 2707B per customer request IAW TM 1-1520-237-23&P WP 4076.
6191.4 E G 1
00 ,
✕ A 05 May 21 23 13:05 JUSTUS, NATHANIEL
Removed BFT Pallet Assy S/N 10696-P per customer request IAW UH-60A/L BFT GPS Message Router.
6191.4 E G 1
00 ,
✕ A 07 May 21 1 10:37 BROWN, MICHAEL
AIRCRAFT INDUCTED INTO BEST PROGRAM ON 7-May-2021, NO SCHEDULED MAINTENANCE PERFORMED AFTER THIS DATE.
6191.4 E G 1
02 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 07 May 21 2 10:38 BROWN, MICHAEL
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.
6191.4 E G 1
02 ,
― A 07 May 21 3 13:36 Generated, Computer
SAFETY MESSAGE NUMBER: H-60-21-AMAM-03 DESCRIPTION: AUXILIARY POWER UNIT (APU) GENERATOR DA FORM 2410 TRACKING. IS DUE: 31 MAY 2021 CALENDAR
6191.4 O O 1
00 ,
✕ A 07 May 21 4 13:36 Generated, Computer
SAFETY MESSAGE NUMBER: H-60-21-SOF-01 DESCRIPTION: T700 SERIES ENGINE COMPRESSOR SPLIT LINE AND COMPRESSOR FORWARD AND AFT FLANGE INSPECTION . WAS DUE: 12 APR 2021 CALENDAR
6191.4 O O 1
00 ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
1. AIRCRAFT SERIAL NUMBER8424004
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 10 May 21 1 13:53 BROWN, MICHAEL
During records review with MCDS/2410 Hotline it was discovered that O/S Drain Valve Assy (s/n: APM303JN) was removed for leak and reinstalled with no correction.
6191.4 E G 2
04A05N ,
/ A 10 May 21 2 13:57 BROWN, MICHAEL
#2 ENG oil cooler data plate missing, unable to verify component serial number.
6191.4 E G 1
04A08B ,
DA FORM 2408-13-1-SG, 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 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
/ 8424004 E
26 Feb 19 1
14:55
HF radio inop. Displays RT-CDU COMM FAIL.
✕ T/ F― F✕ T― F― F/ F✕ T✕ T― T― T
DISCONNECTED HF CONTROL (1 CANNON PLUG 2 FILL PLUGS)LOOSENED 4 DZUSK FASTNERS ON HF CONTROL
LOOSENED 4 DZUSK FASTNERS ON KY-100
DISCONNECTED 2 EA CANNON PLUGS FROM KY 100
TOOLBOX INV REQ
FOD CHECK REQ
LOOSENED 4 DZUSK FASTNERS ON KY-100
REMOVED MOUNTING HARDWARE FROM UHF ANTENNA DISCONNECTED ARC-220 RT
FOD CHECK REQ
TOOLBOX INV REQ
RECONNECTED CONNECTORS
TIGHTNED AND SECURED 4 DZUSK FASTNERS STATUS SYMBOL WRITEN IN ERROR
RECONNECTED KY 100
INV COMPLETE
FOD CHECK COMPLETE
TIGHTNED 4 DZUSK FASTNERS
REINSTALLED MOUNTING HARDWARERECONNECTED ARC-220 RT
CHECK COMPLETE
CHECK COMPLETE
CHANDLER, T.
CHANDLER, T.
CHANDLER, T.
CHANDLER, T.
ZIEMSKI, R.
ZIEMSKI, R.
CHANDLER, T.
FORDHAM, A.
FORDHAM, A.
TAYLOR, B.
TAYLOR, B.
F
F
F
F
F
F
F
F
F
F
F
0.3
0.1
0.1
0.3
0.2
0.2
0.2
0.3
0.2
0.2
0.1
page 41 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
✕ 8424004 A
16 Oct 20 1
09:07
REMOVAL OF PILOTS LEFT PEDAL MASTER BRAKE CYLINDER TO SLAVE CYLINDER ELBOW FITTING REQ FOR CONTROLLED EXCHANGE TO 8826036
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
REMOVED PILOT LEFT PEDAL BOOT HDWR
REMOVED PILOTS LEFT PEDAL BOOT
REMOVED PILOTS LEFT PEDAL BOOT HDWR
REMOVED PILOT LEFT PEDAL BOOT
REMOVED PILOT CENTER PEDAL PANELS
REMOVED PILOT CENTER PEDAL PANEL HDWR
LOOSENED HDWR ON LEFT AND RIGHT HAND RAISED PILOT PANELREMOVED PILOT AFT CYCLIC PANEL HDWR
REMOVED PILOT AFT CYCLIC PANEL
REMOVED CYCLIC BOOT HDWR
REMOVED CYCLIC BOOT
REMOVED CYCLIC PANEL HDWR
REMOVED CYCLIC PANEL
page 42 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 2
✕ 8424004 A
16 Oct 20 1
09:07
REMOVAL OF PILOTS LEFT PEDAL MASTER BRAKE CYLINDER TO SLAVE CYLINDER ELBOW FITTING REQ FOR CONTROLLED EXCHANGE TO 8826036
✕
✕
✕
✕
DISSCONNECTED MASTER CYLINDER HOSE FROM ELBOW FITTINGDISCONNECTED CLAVE CYLINDER HOSE FROM ELBOW FITTINGREMOVED ELBOW FITTING HDWR
REMOVED ELBOW FITTING
page 43 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
✕ 8424004 A
16 Oct 20 2
12:31
CONTROL EXCHANGE IN PROGRESSO FTHE REMOVAL OF THE PILOTS AHRU TO AIRCRAFT 168
✕
✕
✕
✕
― F― F
REMOVED MOUNTING HARDWARE FROM PILOT SIDE AHRUDISCONNECTED (2) CANNON PLUGS FROM PILOT AHRU REMOVED ADDEL CLAMPS FROM PILOT AHRU
REMOVED PILOT AHRU SN:10815
FOD CHECK REQUIRED
TOOLBOX CHECK REQUIRED
REINSTALLED MOUNTING HARDWARE TO PILOT SIDE AHRURECONNECTED (2) CANNON PLUGS TO PILOT AHRUREINSTALLED ADDEL CLAMPS TO PILOT AHRUREPLACED WITH PILOT AHRU SN:00081INSPECTION COMPLETE
INSPECTION COMPLETE
FORDHAM, A.
FORDHAM, A.
FORDHAM, A.
FORDHAM, A.
ZIEMSKI, R.
ZIEMSKI, R.
F
F
F
F
F
F
0.5
0.2
0.3
0.2
0.1
0.1
page 44 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
✕ 8424004 A
17 Oct 20 1
10:15
#1 ENGINE REMOVED FOR MAINT
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
DISCON MAIN FUEL HOSE FROM ELBOW (#1 ENG)
DISCON (2EA) ENGINE DRAIN HOSES FROM REAR ENGINE DECK COMPARTMENT ELBOWDISCON (2EA) CANNON PLUGS FROM FIREWALL
DISCON P/A/S FROM HMU
DISCON L/D/S FROM HMU
DISCON BLEED AIR TUBE COUPLING FROM STARTER
LOOSENED (2EA) STARTER BLEED AIR TUBE CLAMPS FROM FIREWALLLOOSENED LOWER CROSS BLEED AIR TUBE CLAMP FROM FIREWALLLOOSENED IPS BLOWER DUCT CLAMP
RMVD IPS BLOWER DUCT
UNCLAMPED LOOP CLAMP FROM DESWIRL DUCT
DISCON HIGH SPEED SHAFT FROM GIMBAL
RMVD FORWARD SUPPORT TUBE (6EA) MOUNT BOLTS
page 45 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 2
✕ 8424004 A
17 Oct 20 1
10:15
#1 ENGINE REMOVED FOR MAINT
✕
✕
✕
✕
✕
✕
✕
✕
―
―
―
✕
✕
RMVD INBOARD ENGINE MOUNT BOLTS
RMVD OUTBOARD ENGINE MOUNT BOLTS
RMVD CENTER ENGINE MOUNT BOLT
RMVD #1 ENGINE
RMVD #1 ENGINE CROTCH ASSY FROM SUPPORT TUBERMVD AFT MOUNT LINK (2EA) BOLTS FROM ENGINE COMBUSTOR SECTIONRMVD (2EA) AFT MOUNT LINKS
INSTALLED ENGINE SWIRL CAGE
INPUT MODULE FLANGE NUT TQ CHECK REQUIRED PRIOR TO ENGINE INSTALLATIONTOOLBOX INVENTORY REQUIRED
FOD CHECK REQUIRED
LOOSENED CHIP DETECTOR (2EA) MOUNT BOLTS
RMVD #1 ENG CHIP DETECTOR
page 46 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 3
✕ 8424004 A
17 Oct 20 1
10:15
#1 ENGINE REMOVED FOR MAINT
―
✕
ELECTRICAL CHIP DETECTOR CIRCUIT TEST REQUIRED
BROKE TQ ON FUEL LINE ELBOW HDWR IN ERROR. RETQ REQ.
page 47 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
✕ 8424004 A
18 Oct 20 3
10:43
#1 INLET REMOVAL
✕
✕
✕
✕
✕
✕
―
―
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
page 48 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
/ 8424004 A
19 Oct 20 2
15:19
AIRCRAFT REQ RMVL OF IMMSS PRIOR TO EXPORT TO BEST.
✕
✕
✕
✕
✕
✕
✕
✕
L/H CREW CHIEF SEAT RMVD WITH HDWR AND RAIL STOP.R/H CREW CHIEF SEAT RMVD WITH HDWR AND RAIL STOP.L/H CREW CHIEF BASE RMVD WITH ATTACHING HDWR AND BRACKETS.R/H CREW CHIEF BASE RMVD WITH ATTACHING HDWR AND BRACKETS.RMVD L/H LITTER PALLET ASSY WITH 2EA AMBULATORY SEATS AND ALL ATTACHING HDWR AND BRACKETS.RMVD R/H LITTER PALLET ASSY WITH 2EA AMBULATORY SEATS AND ALL ATTACHING HDWR AND BRACKETS.RMVD L/H INTERCOSTAL ASSY WITH TBAR, ATTACHING HDWR, BRACKETS, AND SHIMS.RMVD R/H INTERCOSTAL ASSY WITH TBAR, ATTACHING HDWR, BRACKETS, AND SHIMS.
page 49 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
/ 8424004 A
20 Oct 20 1
10:02
AIRCRAFT REQ RMVL OF EXTERNAL RESCUE HOIST PRIOR TO EXPORT TO BEST.
/ REMOVED EXTERNAL RESCUE HOIST
page 50 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
✕ 8424004 A
20 Oct 20 2
10:08
CONTROL EXCHANGE IN PROGRESS OF RADAR ALTIMETER ANTENNA CABLES FROM BOTH ANTENNAS TO RT
✕
✕
✕
✕
✕
✕
removed (8) screws and (2) radar altimeter antennas
cut safeties and disconnected radar altimeter antenna connectionsremoved adel clamps from radar altimeter antenna cableremoved both radar altimeter jacks from lower center junction boxremoved (4) radar altimeter antenna cables
disconnected (4) cannon plugs and removed CDU
page 51 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
/ 8424004 A
21 Oct 20 3
07:53
CONTROLLED EXCHANGE OF CPLT PEDAL ADJUSTER ASSY TO AIRCRAFT 00-26851
✕
✕
✕
✕
✕
✕
✕
✕
✕
✕
RMVD CPLT PEDAL BOOTS 2EA WITH HDW
RMVD CPLT PEDAL BOOT CENTER PLATE WITH 4EA SCREWSRMVD SCREWS 4EA FROM CONTROL ROD COVER ON SIDE OF CPLT FLOOR IN CHIN BUBBLERMVD HDW WITH COTTER PIN FROM YAW CONTROL ROD IN CHIN BUBBLERMVD 2EA RAISED FLOOR PANELS WITH SCREWS FROM UNDER CPLT YAW PEDALSRMVD HDW WITH COTTER PIN FROM CPLT LEFT PEDAL PUSH ROD AT PEDALRMVD HDW WITH COTTER PIN FROM (CPLT) RIGHT PEDAL PUSH ROD AT PEDALRMVD BOLTS 4EA FROM CPLT PEDAL ADJUSTER UPPER BEARINGRMVD BOLTS 4EA FROM CPLT PEDAL ADJUSTER LOWER BEARINGRMVD PEDAL ADJUSTER ASSEMBLY
page 52 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
✕ 8424004 A
22 Oct 20 1
14:29
CONTROL EXCHANGE IN PROGRESS FOR THE REMOVAL OF THE POSITION LIGHT DIM AND BRIGHT TOGGLE SWITCH FOR UPPER CONSOLE
✕
✕
✕
✕
DROPPED UPPER CONSOLE
DISCONNECTED 6 TERNIMALS FROM POSITION LIGHT BRT/DIM SWITCHREMOVED UPPER CONSOLE FACE PLATE
REMOVED POSITION LIGHT DIM/BRT TOGGLE SWITCH
page 53 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
/ 8424004 A
27 Oct 20 2
08:10
UNIT EQUIPMENT/PROPERTY BOOK ITEMS REMOVAL REQUIRED FOR AIRCRAFT TRANSFER TO BEST
✕
✕
✕
✕
✕
✕
✕
―
―
✕
✕
✕
DISCONNECTED AND REMOVED 2 ARC 201 RECIEVER TRANSMITERSDISCONNECTED AND REMOVED KY-100
DISCONNECTED AND REMOVED APR-39 PROCESSOR
DISCONNECTED AND REMOVED KY-58 CONTROL HEADDISCONNECTED AND REMOVED ARC-220 RECIEVER TRANSMITTERDISCONNECTED AND REMOVED HUD SDC
DISCONNECTED AND REMOVED APX 123 TRANSPONDERFOD CHECK REQUIRED
TOOLBOX CHECK REQUIRED
REMOVED MOUNTING HARDWARE FROM UHF ANTENNAREMOVED MOUNTING HARDWARE TO PILOTS KICK PANELREMOVED PILOTS KICK PANEL
REINSTALLED MOUNTING HARDWARE TO UHF ANTENNAREINSTALLED MOUNTING HARDWARE TO PILOTS KICK PANELREINSTALLED PILOTS KICK PANEL
FORDHAM, A.
FORDHAM, A.
FORDHAM, A.
F
F
F
0.5
0.5
0.2
page 54 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
✕ 8424004 A
27 Oct 20 3
10:39
CONTROLLED EXCHANGE OF #1 ENGINE AIR INLET COUPLING (ECCENTRIC) FROM ACFT 84-24004 TO ACFT 00-26862 PART DOC NUMBER W91FD993110002
✕
✕
REMOVED HARDWARE SECURING ECCENTRIC COUPLING TO AIRFRAMEREMOVED ECCENTRIC COUPLING ASSY FROM AIRFRAME
page 55 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
✕ 8424004 E
29 Oct 20 1
10:05
REMOVED TDFM-9000 TECHNISONIC RADIO
✕ DISCONNECTED ELECTICAL CONNECTORS 5 EA
page 56 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
✕ 8424004 A
03 Nov 20 4
08:51
#2 ENG REMOVED DUE TO CONTROLLED EXCHANGE
✕
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✕
✕
✕
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✕
✕
✕
DISCON MAIN FUEL HOSE FROM ELBOW
DISCON (2EA) ENGINE DRAIN HOSES FROM REAR ENGINE DECK COMPARTMENT ELBOWSDISCON (2EA) CANNON PLUGS FROM FIREWALL
DISCON P/A/S FROM HMU
DISCON L/D/S FROM HMU
DISCON BLEED AIR TUBE COUPLING FROM STARTER
LOOSENED (2EA) STARTER BLEED AIR TUBE CLAMPS FROM FIREWALLLOOSENED LOWER CROSS BLEED AIR TUBE CLAMP FROM FIREWALLRMVD (2EA) CLAMPS SECURING ENGINE CONTROL CABLES TO IPS DUCTLOOSENED IPS BLOWER DUCT CLAMP
RMVD IPS BLOWER DUCT
UNCLAMPED LOOP CLAMP FROM DESWIRL DUCT
DISCON HIGH SPEED SHAFT FROM GIMBAL
reconnected tq outbored to 250 in lbs, tq inbored to 150 in lbs
reconnected shaft tq to 140 in lbs
POWELL, R.
POWELL, R.
F
F
0.2
0.3
page 57 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 2
✕ 8424004 A
03 Nov 20 4
08:51
#2 ENG REMOVED DUE TO CONTROLLED EXCHANGE
✕
✕
✕
✕
✕
✕
✕
✕
✕
―
―
―
✕
RMVD FORWARD SUPPORT TUBE (6EA) MOUNT BOLTSRMVD INBOARD ENGINE MUNT BOLT
RMVD OUTBOARD ENGINE MOUNT BOLT
RMVD CENTER ENGINE MOUNT BOLT
RMVD #2 ENGINE
RMVD #2 ENGINE CROTCH ASSY FROM SUPPORT TUBERMVD AFT MOUNT LINK (2EA) BOLTS FROM ENGINE COMBUSTOR SECTIONRMVD (2EA) AFT MOUNT LINKS
INSTALLED ENGINE SWIRL CAGE
INPUT MODUEL FLANGE NUT TQ CHECK REQUIRED PRIOR TO ENGINE INSTALLATIONFOD CHECK REQUIRED
TOOLBOX INVENTORY REQUIRED
LOOSENED CHIP DETECTOR (2EA) MOUNT BOLTS
installed tq to 180 inlbs POWELL, R. F 0.3
page 58 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 3
✕ 8424004 A
03 Nov 20 4
08:51
#2 ENG REMOVED DUE TO CONTROLLED EXCHANGE
✕
―
RMVD #2 ENGINE CHIP DETECTOR
ELECTRICAL CHIP DETECTOR CIRCUIT TEST REQUIRED
page 59 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
✕ 8424004 A
03 Nov 20 5
08:54
#2 ENG INLET REMOVED DUE TO CONTROLLED EXCHANGE
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✕
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✕
✕
―
―
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 FIREWALLLOOSENED INLET COUPLING
RMVD #2 INLET
FOD CHECK REQUIRED
TOOLBOX INVENTORY REQUIRED
page 60 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
✕ 8424004 A
25 Nov 20 2
09:11
REMOVAL OF OVERSPEED DRAIN VALVE REQ TO COMPLETE CONTROLLED EXCHANGE
✕
✕
✕
✕
― M― M
DISCONNECTED #1 OSDV ELECTRICAL CONNECTOR
REMOVED #1 OSDV MANIFOLD CAPTIVE BOLTS (2EA)
REMOVED (2EA) CAPTIVE BOLTS SECURING OSDV -ACCESSORY GBREMOVED OSDV SN-APM973HK FROM ACFT 24004
FOD CHECK REQ
TOOLBOX INV REQ
CONNECTED EC
REIINSTALLED TQ- 50 IN LBS
REINSTALLED TQ'D - 50 IN LBS
REPLACED WITH OSDV SN-APM303JNFOD CHECK COMP
TOOLBOX INV COMP
Martin, S.
Martin, S.
Martin, S.
Martin, S.
REMILLARD, B.
REMILLARD, B.
F
F
F
F
F
F
0.3
0.3
0.3
0.4
0.3
0.3
page 61 of 62 11 May 2021 1418 UTC FOUO
DA FORM 2408-13-2-SG, 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
11 May 21 1
― 8424004 A
21 Jan 21 3
14:22
NO.2 ENGINE IPS BLOWER DUCT HAS A 1/2 INCH CRACK JUST AFT OF SPINDLE CABLE ATTACHMENT POINT
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/
/
prepared cloth and resin
toolbox inventory due
fod check due
applied fiberglass POLITE, G. F 1.0
page 62 of 62 11 May 2021 1418 UTC FOUO