N803UP

Part: FITTING — CRACKED (BS 1690 L26L) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE: SP WHILE WORKING REPAIR SEQ: NR 803-F1-126 FOUND CRACK FITTING AT STA. 1690- L26L. REMOVED AND INSTALLED REPAIR FITTING IAW SRM 51-1-20D, 51-1-24,51-1-8.

Part: FUEL TANK — DAMAGED (RGIHT AUX) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR 803-W4-23 RT AUX TANK, LOWER, XFS53, HAS NO SRM REF AND REQUIRES ENGINEERING DISPOSITION. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED REPAIR WITH UPS EO DC8-5730-31576-A.

Part: FUEL TANK — DAMAGED (RIGHT AUX) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQ 803-W4-24 RT WING L/E AUX TANK LWR SURFACE XFS 60 HAS NO SRM REF PER APPX G AND REQUIRES ENGINEERING. REMOVED EXISTING REPAIR, FABBED AND INSTALLED REPAIR DOUBLER IAW EA 00 8-5730-01-A1576 AND EO DC8-5730-31576-A.

Part: SKIN — MISREPAIRED (TE FLAP) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP SEQ 803-W3-23 LT O/B FLAP STA 340 SKIN PLATING EO DC8-5100-30418C APP X H STEP 1 MARKED NO REQUIRES ENGINEERING EVAL. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW SAA EA 008-5730-01-A 1578 AND EO3 DC8-5730-31635-A.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQ 803-F1-126 FS 1703 L24-26L ROUND FLUSH REPAIR 1.0 INCH DIA. HAS NO SRM. REF PER APPX G AND REQUIRES ENGINEERING. REMOVED 2 EXISTING REPAIRS, FABBED AND INSTALLED DOUBLER, FILLER, AND IA FINGER DOUBLER IAW EA 008-5330-01-A1577 AND EO DC8-5330-31577-A.

Part: LONGERON — CUT (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP AFTER REMOVAL OF REPAIR DOUBLER SEQ 803-F1-15, FOUND L26L WITH DEEP CUT AT FS 398. CUT OUT DAMAGED LONGERON AND INSTALLED REPAIR SPLICE IAW SRM 53-2-2 FIG 10, 51-1-24, 51-1-20D.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQUENCE 803-F1-64 REQUIRES AN SDR 4 X 9 INCH EXTERNAL DOUBLER REPAIR AT STA 1334-1349 L11L CORRELATES TO DC8 SRM 53-2-1 FIG 7.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQ 803-F1-131 REQUIRES AN SDR 7 X 8 INCH EXTERNAL DOUBLER REPAIR AT STA 1882-1890 L28L-L34L CORRELATES TO DC8 SRM 53-2-1 FIG 7 SHT 13.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQUENCE 803-F1-134 REQUIRES AN SDR 12 X 25 INCH EXTERNAL REPAIR DOUBLER AT STA 112-140 L34L-L35L CORRELATES TO DC8 SRM 53-2-1 FIG 7 SHT 3.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQUENCE 803-F1-63 REQUIRES AN SDR 15 X 21 INCH EXTERNAL DOUBLER REPAIR AT STA 1326-1348, L9L-L11L CORRELATES TO DC8 SRM 53-2-1 FIG 7.

Part: SKIN — CRACKED (LLT WING) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV LT WING O/B LEADING EDGE I/B SECTION LOWER EXTERIOR SKIN CRACKED AT DRAIN HOLE. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO DC8-5730-31529-A AND SAA EA 008-5720-01-A1571.

Part: RIB — CRACKED (LT WING) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP LT WING OUTBOARD LEADING EDGE INBOARD SECTION HAS CRACKED UPPER RIB ABOVE PNL 520A XFS 476. INSTALLED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-20D, 57-3-3 FIG 6 SHT 2.

Part: WEB — CRACKED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP WHILE WORKING NR 164443 FOUND WEB TO BE CRACKED AT PIT TORQUE BOX AREA STA 1390. REMOVED DAMAGED WEB AND INSTALLED FABRICATED WEB SECTION IAW SRM, 51-1-21, 51-1-8, FABBED PER DWG 5616674.

Part: DOUBLER — CRACKED (LT WING) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP LT WING O/B LEADING EDGE, I/B SEGMENT LOWER INTERNAL BEADED DOUBLER CRACKED NEAR PANEL 520A, XFS 452. FABRICATED AND INSTALLED REPAIR PER EO DC8-5730-31521-A AND EA 008-5720-01-A1569.

Part: RIB — CRACKED (LT WING) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP LT WING OUTBOARD LEADING EDGE INBOARD SECTION HAS CRACKED UPPER RIB ABOVE PANEL 579B XFS 584. FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-20D, 57-2-0 FIG 002 SHT 2.

Part: RIB — CRACKED (LT WING) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP LT WING OUTBOARD L/E INBOARD SECTION HAS CRACKED UPPER RIB ABOVE ACCESS PANEL 519A XFS 692. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-20D, 57-3-3 FIG 006, 57-2-0 FIG 002.

Part: STRUCTURE — CRACKED (RT WING) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP RT LEADING EDGE JUST OUTBOARD OF NR 4 PYLON SKIN CRACKED AT SCREW HOLE ABOVE REPAIR DOUBLER (XFS 533) FOUND DURING BUYBACK OF NR 164463. REMOVED EXISTING DOUBLER, CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-1, 51-1-21, 51-1-26.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP DURING REPAIR EVAL OF EFN 80320061044 FOUND ANOTHER CRACK ON CHANNEL D-PIT STA 1394 L34R. REMOVED DAMAGE AND FABBED AND INSTALLED REPAIR ANGLE AND DOUBLER IAW SRM 51-1-20D, 51-1-21, 53-2-0 FIG 1B AND DWG 5616674.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP AFTER REMOVAL OF DOUBLER AT STA 492 L24L (803-F1-18) FOUND BLENDOUT ON ON LOWER RADIUS OF L24L. NOT ALLOWED PER SRM. PERFORMED LONGERON SECTION SPLICE REPAIR PER SRM 53-2-2, DWG4613495.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-78 AT FS 1585 L24R HAS SRM 53-02-01 FIG 7 SHEET 11 IS A CAT B REPAIR. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-10 AT FS 190-198 L24-25L HAS SRM REF 53-02-01 FIG 7 SHEET 11 IS A CAT B REPAIR. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11.

Part: SKIN — DAMAGED (LT SLOT VANE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-08 LT OUTBOARD VANE SKIN PLATING EO DC8-5100 -30418-C APPX H STEPS 4, 5, 6 & 7 ARE MARKED NOT VISIBLE. REMOVED REPAIR DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 57-02-01 FIG 2H SHEET 1.

Part: SKIN — DAMAGED (LT WING) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-19 LT STUB WING PLATING XFS 516.5 EO DC8 -5100-30418-C APPX H STEP 6 & 7 ARE MARKED NOT VISIBLE. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW DC-8 SRM 57-02-01A FIG 1 SHEET 1 AND 57-03-00 FIG 12 SHEET 1.

Part: SKIN — DAMAGED (LT WING) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-06 AT LT STUB WING SKIN XFS 249.5 - 258.9 EO DC8-5100-30418-C APPX H STEP 4 IS MARKED NO AND STEP 6&7 ARE MARKED NOT VISIBLE. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO DC8-5730-31485-A AND FVCI DWG 57-08540-19.

Part: DOUBLER — DAMAGED (HORIZ STAB) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQ 803-S2-01 RT HORIZONTAL STAB XE 25.312 - XE 29.812, HAS NO SRM REF. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW EA 008-5500-01-A1585, AND EO DC8-5530-31694-A.

Part: STRUCTURE — DAMAGED (SLOT VANE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-05 LT SLOT VANE XFS 239.0 EO DC8-5100-30418 -C APPX H STEP 6&7 ARE MARKED NOT VISIBLE. REMOVED REPAIR DOUBLER, FABRICATED REPLACEMENT REPAIR DOUBLER, FILLER AND INTERNAL DOUBLER IAW DC-8 SRM 57-03-03 FIG 10 SHEET 1 AND 57-02-01-FIG 2H SHEET 1.

Part: DOUBLER — UNKNOWN (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQ 803-F1-136 AT STA 510, BETWEEN L29 TO 30L HAS NO SRM REF AND REQUIRES APPX F OF EO DC8-5100-30418C. ACCOMPLISH APPX F, REMOVED OLD REPAIR, FABBED NEW REPAIR AND INSTALLED IAW TR53-203 OF SRM 53-2-1 PARG 16 AS PER SAA EA 81427420.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQ 803-F1-139 F/S 558, L25L-L26L HAS NO SRM REFERENCE, & NEEDS APPX F OF EO DC8-5100-30418C. REMOVED EXISTING REPAIR, FABBED & INSTALLED DOUBLER SHT7075T6 .090 REF DWG5779913, 2779655, SRM 53-2-1 FIG 7 SHT 13, 51-1-8, 51-1-26, 51-1-20D, SAA ENG 81427390001.

Part: DOUBLER — UNKNOWN (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQ 803-F1-137 AT STA 518, BETWEEN L25L TO 26L HAS NO SRM AND REQUIRES APPX F OF EO DC8-5100-30418C. ACCOMPLISHED APPX F, REMOVED OLD REPAIR, FABBED AND INSTALLED NEW REPAIR IAW TR 53-203 OF SRM 53-2-1 PARG 16B AS PER SAA EA 81427410001.

Part: SKIN — DAMAGED (LT WING) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-11 LT WING O/B LEADING EDGE SKIN PLATING XFS 534.1 EO DC8-5100-30418-C APPX H IS MARKED NOT VISIBLE ON STEP 6&7. REMOVED REPAIR DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 57-02-01 FIG 2H.

Part: STRUCTURE — DAMAGED (LT WING) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-W3-15 LT INBOARD STUB WING AT STA XFS 239 - XFS 246 EO DC8-5100-30418-C APPENDIX H STEP A (6)&(7) MARKED AS NOT VISIBLE. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW DC-8 SRM 57-02-01A FIG 001 SHEET 1 AND 57-03-00 FIG 12 SHEET 1.

Part: SKIN — MISREPAIRED (RT WING) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-W4-02 RT WING STA XFS 265 - XFS 527 REPAIR DOUBLER THINNER THAN BASE STRUCTURE. REMOVED REPAIR DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 57-02-01 FIG 38 SHEET 1.

Part: STRUCTURE — DAMAGED (RT WING) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR 803-W4-10, RT WING L/E STA XFS650-662 REQUIRES ENGINEERING EVALUATION DUE TO APPX H STEP A6 & A7 MARKED NV. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED REPAIR REF SRM DC8 SRM 57-02-01 FIG 2H SHT 1.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-73 AT FS 1393.5 L17-18L HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR PARTS IAW UPS EO DC8-5330-31417-A AND FVCI DWG 53-08540-15.

Part: PRESSURE PANEL — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F3-02 AT FS -9 TO -15 LBL 5 TO RBL 23 HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR PARTS IAW UPS EO DC8-5330-31508-A AND SAA EA 008-5320-01-A1574.

Part: WEB — MISREPAIRED (FS-81 LBL37.5) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F3-06 AT FS -75/-83 LBL 37-42 HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW UPS EO DC8-5330-31487-A ANG FVCI DWG 53-08540-21.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-100 AT STA 1521 L27L HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 10.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR 803-F1-53, STA 1278-1285, L5R-L7R, HAS NO SRM REFERENCE AND REQUIRES EO APPX F. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED REPAIR REF EO DC8- 5330-31400-A AND DWG FVCI 53-08540-24.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-70 AT FS 1376.5-1379.5 L19-20L HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,266 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-68 FS 1381 L24L - L25L HAS NO SRM REF. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 10.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQUENCE 803-F1-92 AT STA 1430 L16L HAS NO SRM REF AND REQUIRES APPX F OF EO DC8-5100-30418C. REPAIRED PER FVC DRAWING 53-08540-12, EO DC8-5330-31414-A SA PER SAA EAR 81426850001.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REP SEQ 803-F1-105, STA 1477-1479, L31L-L32L HAS NO SRM REFERENCE AND REQUIRES APPX F OF EO DC8-5100-30418C. REMOVED OLD REPAIR. REPAIRED AREA REF DC8 SRM 53-2-1 FIG 7 PER SAA ENGINEERING 81426600001.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-59 AT STA 1294-1305 L14-17L HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-02-00 FIG 22A.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-87 AT STA 1748 L20R - L21R HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-56 AT STA 1157-1166 L27L HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 13.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-98 AT STA 1535 L14L HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED REPAIR DOUBLERS AND FILLERS IAW UPS EO DC8-5330-31413-A AND FVCI DWG 53-08540-11.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQ 803-F1-104, STA 1446 L31L-L32L HAS NO SRM REF & REQUIRES APPX F OF EODC8-5100-30418C. REMOVED OLD DOUBLER, FABBED & INSTALLED FILLER AND DOUBLER SHT7075T6 .071 & .080 REF SRM 53-4-1, 53-2-1 FIG 7, 51-1-8, 51-1-20D, SAA ENG 81426590001.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-103 AT STA 1472 L29-30L HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 10.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-72 AT FS 1406 L20-21L HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-85 AT STA 1718-1720 L19R-L20R HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-86 AT STA 1743 L16R - L17R HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW UPS EO DC8-5330-31415-A AND FVCI DWG 53-08540-13.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-115 AT STA 1607-1613 L22-23L HAS NO SRM REF. REMOVED REPAIR DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 13.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,266 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-95 AT STA 1446 L12L HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 10 TR 53-204.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR 803-F1-82, STA 1670 L8R HAS NO SRM REFERENCE AND REQUIRES EO APPX F. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED REPAIR REF SRM 53-02-01 FIG10 SHT 1.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,266 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-67 FS 1407.5 L26L - L27L HAS NO SRM REF. REMOVED INTERNAL REPAIR DOUBLER AND FILLER. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-77 FS 1530-1540 L16-18R HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-02-00 FIG 22A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-74 AT FS 1427 L19-20L HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 10.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-71 AT FS 1396 L20-21L HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 10.

Part: STRUCTURE — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQ 803-F1-94 AT STA 1457 L21L HAS NO SRM REF AND REQUIRES APPX F. REMOVED OLD REPAIR, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-8, 53-4-1 FIG 21C, 53-2-0 FIG 1D AS PER SAA EA 81426840001.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-02 AT STA 13 L15-16L HAS NO SRM REF. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW UPS EO DC8-5330-31402-A AND FVCI DWG 53-08540-1.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,266 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-66 FS 1385 L27L - L28L HAS NO SRM REF. REMOVED INTERNAL REPAIR DOUBLER AND FILLER. FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-0201 FIG 7 SHEET 10.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR 803-F1-11, STA 40-45, L28L-L29L HAS NO SRM REFERENCE AND REQUIRES EO APPX F. REMOVED EXISTING REPAIR. REPAIRED AREA PER TR 53-205 OF DC8 SRM 53-2- 00-0 PARA 22A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-112 AT STA 1607.5-1625.75 L14-15L HAS NO SRM REF. REMOVED REPAIR DOUBLER, CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-99 AT STA 1529 L23L HAS NO SRM REF. REMOVED FLUSH REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED EXTERNAL REPAIR DOUBLER AND FILLER IAW UPS EO DC8-5330-31419-A AND FVCI DWG 53-08540-17.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-89 AT STA -153/-156 L21R HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 10.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-57 AT STA 1217 L18L HAS NO SRM REF. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO DC8-5330-31420-A AND DWG 53-08540-18.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,266 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-45 AT STA 1418 L25R - L26R HAS NO SRM REF. REMOVED REPAIR DOUBLER AND FILLER. FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-35 AT STA 8-4 L32-34R HAS NO SRM REF. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR 803-F1-111, STA 1573-1595, L21L-L25L, WAS REPAIRED PER SRM 53-2-1 FIG 7 IS CAT B, AND REQUIRES ENGINEERING DISPOSITION. REMOVED EXISTING REPAIR. INSTALLED NEW REPAIR PER SRM 53-04-01 FIG 16 SHT 2

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-40 AT FS 1200-1218 L1-4R HAS SRM REF 53-02-01 FIG 7 SHEET 11 IS A CAT B REPAIR. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND TRIPLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 11.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-41 FS 1120-1135 L1-L4L HAS SRM REF 53-02-01 FIG 7 SHEET 11 IS A CAT B REPAIR. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-9 SRM 53-02-01 FIG 7 SHEET 10.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,266 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-55 FS 1358 - 1366 L11R - L12R HAS SRM REF 53-02-01 FIG 7 IS A CAT B REPAIR. REMOVED REPAIR DOUBLER AND FILLER. FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW UPS EO DC8-5330-31486-A AND FVCI DWG 53-08540-20.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR 803-F1-108, STA 1566-1573, L31L-L32L, WAS REPAIRED PER SRM 53-2-1 FIG 7, IS CAT B, AND REQUIRES ENGINEERING DISPOSITION. REMOVED EXISTING REPAIR. INSTALLED NEW REPAIR PER DC8 SRM 53-04-01-0 FIG 16 SHT 2.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-29 AT FS 160-180 L29-31R HAS SRM REF 53-02-01 FIG 7 SHEET 11 IS CAT B REPAIR. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER AND FILLER IAW DC-8 SRM 53-02-01 FIG 7 SHEET 15.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQ 803-F1-124, FS 1718, L20L-21L HAS NO SRM REF AND REQUIRES ENG DISPOSITION. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 53-2-1 FIG 7, 51-1-8, 51-1-21 AND SAA EA 81427030001.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQ 803-F1-119, FS 1701, L16-17L (ROUND FLUSH REPAIR 1.25 INCH) HAS NO SRM REF AND REQUIRES ENG DISPOSITION. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 51-1-8, 53-2-1 FIG 7 AND SAA EA81426990001.

Part: SKIN — MISREPAIRED (1740-45,L17-18L) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQ 803-F1-122, FS 1740.5 - 1745.5, L17L-18L (FLUSH REPAIR 3.5- 6.5 INCH) HAS NO, SRM REF AND REQUIRES ENG DISPOSITION. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 51-1-8, 53-2-1 FIG 7, AND SAA EA 81427010001.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-19 AT FS 663-677 L36 HAS SRM REF 53-02-01 FIG 7 SHEET 11 IS A CAT B REPAIR. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER IAW UPS EO DC8-5330-31489-A AND FVCI DWG 53-08540-23.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-15 FS 355-418 L25-27L HAS SRM REF 53-02-01 FIG 7 SHEET 11 IS A CAT B REPAIR. REMOVED REPAIR, FABRICATED AND INSTALLED REPAIR DOUBLER AND FINGER DOUBLERS IAW DC-8 SRM 53-02-01 FIG 7 SHEET 5.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQ 803-F1-128, FS 1746, L21L-22L HAS NO SRM REF AND REQUIRES ENG DISPOSITION. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 51-21-00, 51-1-8, 53-2-1 FIG 7 AND SAA EA 81427040001.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQ 803-F1-130 AT STA 1788-1791, L28L-30L HAS NO SRM REF AND REQUIRES ENG DISPOSITION. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 51-1-21, 51-1-8, 53-2-1 FIG 7 AND SAA EA 81426740001.

Part: SKIN — MISREPAIRED (FS1672,L22-23L) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQ 803-F1-121, FS 1672, L22L-23L (FLUSH REPAIR 1-1.5 INCH) HAS NO SRM REF AND REQUIRES ENG DISPOSITION. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 53-2-1 FIG 7, 51-1-8, AND SAA EA 81427360001.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR 803-F1-24, STA 270-278 L23R-L25R, HAS SRM 53-02-01 FIG 7 SHT 11, IS CAT B, AND REQUIRES ENGINEERING DISPOSITION. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED NEW REPAIR REF UPS EO DC8-5330-31561-A.

Part: SKIN — DAMAGED (MAIN CARGO DOOR) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-F1-08 STA 160-167 L15-17L AT MCD EXTERIOR WINDOW PLUG HAS NO SRM REF. REMOVED REPAIR DOUBLER AND TRIPLER, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-02-00 FIG 22A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR 803-F1-22, STA 490-510, L23R-L25R, HAS NO SRM REFERENCE AND REQUIRES EO APPX F. REMOVED EXISTING REPAIR. FABRICATED AND INSTALLED NEW REPAIR REF DC-8 SRM 53-02-01 FIG 7 SHT 4.

Part: STRUCTURE — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQ 803-F1-05 AT STA 74-83 L15-17L HAS NO SRM REF AND REQUIRES ENG DISPOSITION. REMOVED REPAIR, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-0 FIG 22A, TR53-205 AS PER SAA EA 81427430001.

Part: SKIN — GOUGED (TE FLAP) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-W4-33 RT OUTBOARD FLAP UPPER SKIN REPAIR DOUBLER GOUGED JUST O/B OF FLAP STA 219 HINGE. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW DC-8 SRM 57-02-00 FIG 2A AND 57-07-01 FIG 4.

Part: VANE — DAMAGED (LE SLOT) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR SEQUENCE 803-W4-30, NR 4 STUB WING, 2 LOOSE BLIND FASTENERS, 8 OVERSIZED HOLES WITH DIMPLE WASHERS, NEAR XFS 511, O/B END OF SLOT VANE. REMOVED SLOT VANE, REMOVED AND REPLACED 1 DAMAGED EXT & 1 DAMAGED INT REPAIR DOUBLER, RE-ASSEMBLED AS REQUIRED REF SRM 57-2-1 FIG 2H, 57-3-3 FIG 11, 51-1-8, 51-1-21, 57-20-05-2, DWG 5769933.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP LT FUSELAGE SKIN STA 1506 BETWEEN L29-31L HAS NUMEROUS PULLED FASTENERS. REMOVED EXISTING REPAIR DOUBLER, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-20D, 53-2-1 FIG 7, 51-1-26.

Part: PANEL — DAMAGED (TE FLAP) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP LT FLAP SURF BOARD PANEL HAS TWO DAMAGED SCREW HOLES. INSTALLED BONDED REPAIR IAW SRM 57-7-1, 51-1-9A PAR 11 FIG 9, 51-1-15 PAR 2.

Part: STRUCTURE — DAMAGED (RT WING) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SV REPAIR SEQUENCE 803-W4-25 RT WING NR 3 PYLON STUB WING HAS REPAIR DOUBLER WITH 1 SPINNING SCREW AND 10 OVERSIZED FASTENER HOLES WITH DIMPLE WASHERS INSTALLED O/B END AT SLOT VANE. REMOVED REPAIR DOUBLER, FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW DC-8 SRM 57-02-00 FIG 2A AND 57-03-03 FIG 10.

Part: STRUCTURE — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP ROUND FLUSH REPAIR 0.500 INCH DIA AT FS 1601.5, L8L HAS NO MINIMUM ROWS OF RIVETS REQUIRED BY SRM REPAIR SEQ 803-F1-113. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 51-1-8, 53-2-1 FIG 7 AND SAA EA 81426050001.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP REPAIR DOUBLER AT STA 53-65 L31R-L34R INSTALLED WITH BLIND RIVETS 803-F1-32. REMOVED EXISTING DOUBLER. FABRICATED & INSTALLED REPLACEMENT DOUBLER REF DC8 SRM 53-02-01 FIG 7 SHT 11.

Part: DOUBLER — MISINSTALLED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP 12-12 INCH REPAIR DOUBLER INSTALLED WITH BLIND FASTENERS FS 53-65 L31R TO 34R REPAIR SEQ 803-F1-32. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 51-1-8, 53-2-1 FIG 7 AND SAA EA 81425920001.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,226 hrs · 26,694 cycles

INSPECTION TYPE:SP EXTERIOR SKIN OVAL FLUSH REPAIR HAS 1 EACH RIVET WITH LESS THAN 1.5 E. D. AT STA 1445, L23R REPAIR SEQ 803-F1-46. REMOVED AND REPLACED REPAIR DOUBLER IAW SRM 51-1-8, 53-2-1 FIG 7 AND SAA EAA 81425910001.

Part: FITTING — CRACKED (FUSELAGE) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 ALT STRINGER 65 TO FRONT SPAR FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-24, 51-1-8, 51-1-20D, 51-1-1 2.

Part: FLOOR PANEL — CRACKED (COCKPIT) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 COCKPIT FLOOR PANEL 676D HAS ONE CORNER CRACKED AND ONE CORNER BROKEN OUT. FABBED AND INSTALLED REPAIR DOUBLERS IAW SRM 53-2-0 FIG1 B, 53-7-3, 5 1-1-8, 53-7-3 FIG1 A, 51-1-15.

Part: SEAT TRACK — CORRODED (BS 840 LBL 60) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 CABIN STA 840, LBL60, SEAT TRACK FLANGE HAS CORROSION CUT OUT CORROSION FABBED AND INSTALLED SEAT TRACK SPLICE IAW, SRM 53- 2-3, 510108, 5101020D.

Part: FITTING — CRACKED (BS 1771 L11L) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 END FITTING CRACKED IN 60 COMPARTMENT, L11L STA 1771. REMOVE AND REPLACE END FITTING IAW SRM 51-1-21, 51-1-8, 51-1-20D, 51 -3-2.

Part: SKIN — GOUGED (FUSELAGE) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 FUSELAGE EXTERIOR SKIN, 8 INCH GOUGE IN SKIN STA -15 TO -20 L18L. CUT OUT DAMAGE, FABBED AND INSTALLED DOUBLER AND FILLER IAW SRM 53-2- 0 FIG 1F, 53-2-1 FIG 7, 51-1-8, 51-1-20D53-2-1.

Part: FITTING — CORRODED (CARGO DOOR FRAME) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 BACK UP FITTING CORRODED AT MCD JAMB NR 3 SPOOL REMOVED AND REPLACED FITTING IAW SRM 51-3-0, 51-3-2, 51-1-21A.

Part: FITTING — CORRODED (DOOR FRAME) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 BACKUP FITTING CORRODED AT MCD JAMB NR 5 SPOOL REMOVED AND REPLACED CORRODED FITTING IAW SRM 51-1-8, 51-3-0, 51-3-2, RE F.DWR NR 47732951.

Part: FITTING — CORRODED (CARGO DOOR FRAME) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 BACK UP FITTING CORRODED AT MCD JAMB NR 1 SPOOL REMOVE AND REPLACE FITTING IAW, SRM 51-3-00.

Part: DOUBLER — WORN (NLG WW) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 RIGHT NOSE W/W TUNNEL REPAIR ON CEILING U-CHANNEL WORN THROUGH STA NEG 60 RBL 32. REMOVED OLD DOUBLER, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1 -21A, 53-3-3 FIG 6, 51-1-8, 53-2-0.

Part: FLOORBEAM — CORRODED (BS 1120) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 C-PIT RIGHT STA 1120, FLOORBEAM JUST I/B OF CUSP IS BLOWN OUT AT FASTENER HOLE WITH CORROSION. REMOVED CORROSION, FABBED AND INSTALLED REPAIR ANGLE IAW SRM 51-1-8, 51-3-0, 53-2-0 FIG 1F, 51-1-20D.

Part: FITTING — CORRODED (DOOR FRAME) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 A-PIT RT STA 280 L32R, OUTER AFT SIDE OF TORQUE BOX, FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED DOOR JAMB FRAME FITTING IAW SRM 51-1-8, 51-1-20D 51-3-2.

Part: FITTING — CORRODED (BS 270 L30R) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 A-PIT RT STA 270 L30R, END FITTING HAS CORROSION AROUND AND UNDER FASTENERS. REMOVED AND REPLACED FITTING IAW SRM 53-2-0, 51-1-21D, 51-1-8, 51-3-2, 51-1-20D.

Part: FITTING — CORRODED (BS 270 L32R) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 A-PIT RT STA 270 L32R, INSIDE A-PIT DOOR FWD TORQUE BOX IS CORRODED ON THE FITTING, AND AROUND FASTENERS. REMOVED CORRODED FITTING, FABBED AND INSTALLED REPAIR FITTING IAW SRM 51-1-8, 51-1-20D, 53-2-00 FIG 1F.

Part: STIFFENER — BULGED (FUSELAGE) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 RT NOSE TUNNEL CEILING STIFFENER IS BULGED AND HAS POPPED RIVETS STA - 32 RBL 40. REMOVED DAMAGED, FABBED AND INSTALLED REPAIR DOUBLER AND FILLER IAW, SRM 51-1-8, 51-1-21.

Part: FITTING — BROKEN (FUSELAGE) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 BROKEN FITTING ON TOP OF KEEL BEAM INSIDE LT BELLY STRESS PABEL STA 7 00 LBL 2. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-8, 51-3-0, 51-1-24.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 FLOOR PANEL F30A CRACKED AT END. STOP DRILLED CRACK, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1- 8, 53-2-3-FIG 10, 51-3-2, 51-1-26.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 SEAT TRACK STA 960 RIGHT, DAMAGED MDCC RBL48. CUT OUT DAMAGE AND INSTALL PLUG IAW SRM 51-1-8, 53-2-3 FIG 6D.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 SEAT TRACK LBL 45 DAMAGED IN SEVERAL AREAS AT MCD BALL MAT AREA. REMOVED AND REPLACED 3 EACH SEAT TRACK PLUGS IAW, SRM 53-2-3 FIG 6D, 51 -1-8.

Part: FITTING — BROKEN (FUSELAGE) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 MDCC STA 100, LEFT BELOW FLOOR LEVEL, LAMINATED SHIM IS DELAMINATED. REMOVED FLOORBOARD, FABBED AND INSTALLED BROKEN FITTING, CLOSED FLOORBOARD IAW SRM 53-21-1, 51-1-21, 51-3-0, 51-1-8.

Part: ATTACH FITTING — GOUGED (BS 742) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 MDCC LEFT STA 742, CUSP AREA FRAME ATTACH FITTING GOUGED. REMOVED FITTING, FABBED AND INSTALLED FITTING IAW SRM 51-1-8, 51-3-0, 51-1-20D, 51-1-15.

Part: FRAME — BENT (FS 1580) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 MAIN CARGO COMPT STA 1580 RT SIDEWALL STRUCTURE FRAME IS BENT 10" ABOVE CUSP. REMOVED FRAME SECTION FABRICATED FRAME SECTION AND 2 SPLICES. INSTALLED FRAME SECTION AND 2 SPLICES.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 FLIGHT COMPARTMENT, FIRST OFFICERS LWR APT SEAT TRACK HAS ELONGATED HOLES. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-1-20D, 51-1-8, 53-0-1.

Part: ANGLE — BROKEN (LWS 436) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 LT WING T/E STA 436, RIB JUST O/B OF AILERON BUS CABLE SPRING ASSY HAS APPROX 4 INCHES BROKE OFF. FABBED AND INSTALLED REPAIR ANGLE 51-1-21, 51-1-20D, 51-1-8.

Part: SKIN — CRACKED (FUSELAGE) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 AFT EXTERIOR FUSELAGE STA 1690, L34L, FUSE SKIN BULGED AND CRACKED. CUT OUT DAMAGE, FABBED AND INSTALLED NEW DOUBLER IAW SRM 51-1-21D, 51 -1-8, 53-2-0 FIG 007, 51-1-26.

Part: LONGERON — CORRODED (BS 1690-1776) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 LT AFT EXTERIOR FUSELAGE STA 1766, LONG 28L, FUSE SKIN SEAM BULGING. REMOVED CORRODED LONGERON 28L, CLEANED AREA. REMOVED AND REPLACED INTERNAL DOUBLER AND REPLACED L28L SECTION 1690-1766 IAW SRM 51-1-8, 51-1-21, 53-2-0 FIG 1F, 51-1-20D53-5-3.

Part: LONGERON — CORRODED (BS 1766 L28L) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 LT AFT EXTERIOR FUSELAGE STA 1766 L28L FUSELAGE SKIN SEAM BULGING. REMOVED LONGERON, FABBED LONGERON AND INTERNAL DOUBLER, INSTALLED LONGERON AND INTERNAL DOUBLER IAW DC8 SRM 51-1-21, 51-1-20D 53-05-03, AND 51-1-8.

Part: SKIN — DAMAGED (RT WING TIP) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 3 SCREWS PULLING THRU SKIN BOTTOM OF RT WING TIP. REMOVED SCREWS, FABBED AND INSTALLED REPAIR DOUBLER. REINSTALLED SCREWS IAW SRM 51-3-0, 57-3-3 FIG 23, 51-1-8,51-1-21A, 51-1-11.

Part: LINK — GOUGED (LT WING TE FLAP) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 LEFT WING I/B ATTACH LINK AT STA XW 106 HAS DEEP GOUGE. BLENDED GOUGE, REWORKED FINISH AND HFEC, FLAP PEENED IAW SRM EO 008-2 760-01-A1360, DPS 4.999-2, 57-2-0.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 FE,S FWD SEAT TRACK WORN. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-1-20D, 51-1-24, 51-3-0.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 STOP HOLES WORN IN F/E'S AFT SEAT TRACK. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-3-0, 51-1-24, 51-1-8.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 BOTH UPPER SEAT TRACKS WORN AT PILOTS SEAT. REMOVED AND REPLACED SEAT TRACKS IAW SRM 51-1-20D, 51-3-1, 51-1-24.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 COMPLY WITH MPI P19472 NON CONFORMING REPAIR AT L28L IAW ATTACHED WAN 1372778, MPI SUMMARY REPORT, AND EO DC8-5330-20248-E APPX D. REMOVED OLD DOUBLER, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1 -8, 53-2-0, 51-1-26, 51-3-1, EO DC8-5330-20248 APPX D.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 81,122 hrs · 26,618 cycles

INSPECTION TYPE:C1 COMPLY WITH MPI P 19473 REGARDING NON CONFORMING REPAIR AT L28R IAW WA N 1322729, MPI SUMMARY REPORT, AND EO DC8-5330-20248-E APPX E. REMOVED, FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-8, 51-1-26, 51-3-1, EO DC8-5330-20248 APPEX E.

Part: LANYARD — DISCONNECTED (EVAC SLIDE)

INSPECTION TYPE:N/A EMERGENCY SLIDE WILL NOT ATTACH TO FLOOR. DEFERRED IAW MEL 52-7-4, M372513 INSTALLED. RECONNECTED INFLATION LANYARD TO QUICK - DISCONNECTION FITTING IAW MM 25-60-01-2. THIS CLEARS M372513. REMOVED PLACARD.

Part: PUMP — FAILED (NR 2 ENGINE)

INSPECTION TYPE:N/A HYDRAULIC FAILURE. ON DESCENT HYD QTY WAS NOTED TO HAVE DROPPED TO THE AUX LEVEL. APPROPRIATE CHECK LIST ACCOMPLISHED. REMOVED AND REPLACED NR 2 ENG DRIVEN HYD PUMP ASSY PER MM 29-10-12-2.

Part: GIRT BAR — DIRTY (ESCAPE SLIDE)

GIRT BAR JAMS ON RIGHT SIDE. CLEANED DEBRIS FROM GIRT BAR FLOOR LATCH AND LUBED. OPS CHECKS GOOD.

Part: DETECTOR — MALFUNCTIONED (CARGO BAY)

INSPECTION TYPE:N/A LIGHT ON THE LOWER CARGO FIRE MODULE ILLUMINATED. REPAIRED SDU AD1283 PER MM 26-18-01-5. SYSTEM OPS CHECKS NORMAL.

Part: SLIDE — UNSECURE (PAX DOOR)

MAIN DOOR ESCAPE SLIDE NEEDS TO BE REPACKED. RE-SECURED ESCAPE SLIDE.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT TEST. ON PREVIOUS FLIGHT, NEW BATTERY INSTALLED. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT AND WARNING LIGHT DIMMING BOX. OPS CHECK GOOD IAW MM 33-50-01 AND WDM 33-50-01.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY AND RELAY UNIT AND TESTED OK PER MM 33-50-01.

Part: THRUST REVERSER — INOPERATIVE (NR 2 ENGINE)

NUMBER 2 ENG DUE TO THRUST REVERSER WOULD NOT STOW COMPLETED ALL CHECKLIST. PER CAPTAIN ENGINE HAD POSITIVE OIL PRESSURE REMAINDER OF FLIGHT. DEF NR M 355263 OPENED. DEFERRED NR 2 ENG THRUST REVERSER ACCOMPLISHED DEACTIVATION PROCEDURES REF MEL 78-1 AND M/M 78-00-00-2 A/C OK TO CONTINUE. REVISED REACTIVATED NR 2 THRUST REVERSER, INSPECTED WIRING ON ENGINE, TESTED, PER MM 78-00-00-2. BOTH NORMAL & EMERGENCY STOW ALL CHECK GOOD. OPS CHECKED GOOD, NO LEAKS NOTED. THIS CLEARS M355263.

Part: PACKING — LEAKING (HYDRAULIC SYS)

AT CRUISE FL 350 HYD PRESS SENT TO ZERO AND HYD QTY WENT TO EMER/AUX POSITION. LOSS OF HYD QTY AND PRESS CHECKLIST ACCOMPLISHED. REPLACED PACKINGS & RETAINER RINGS REF IPC 29-11-24 ITEM 175,180,185 ON WING SLOT CONTROL VALVE IAW MM 27-80-04-2. LEAK AND OPS CHECKED GOOD. NO CONTROL VALVE ARM WAS DISCONNECTED OR ADJUSTED.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. NOW OPS CK OK, REF 33-50-00.

Part: CUSP WEB — CRACKED (FUSELAGE)

RT CUSP WEB AT POS NR 2 CRACKED. REPAIRED IAW EO DC8-5330-2159.

Part: SWITCH — UNSERVICEABLE (EMERGENCY LIGHTS)

INSPECTION TYPE: N/A EMERGENCY EXIT LIGHT SWITCH IS STILL BAD. WHEN ON BATTERY POWER CAN GET LIGHT TO COME ON BY GIGGLING SWITCH IN THE ARMED POS. WHEN SWITCH TO EXTERNAL POWER THEN BACK BATTERY EMERGENCY LIGHT DOES NOT COME ON. EMERGENCY LIGHT TOGGLE SWITCH REPLACED IAW WDM 33-50-01 PG 5. EMERGENCY LIGHT BATTERY PACK REPLACED IAW AMM 33-50-01-2. OPS CHECK SERVICEABLE. P/N ON: 5708458-503, S/N ON: FTL I58.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS)

INSPECTION TYPE: N/A EMERGENCY LIGHT WOULD NOT COME ON (ANY) WHEN ARMED AND EXTERNAL POWER WAS REMOVED. CYCLED EMERGENCY LIGHT SWITCH SEVERAL TIMES. SYSTEM FOUND SERVICEABLE IAW AMM 33-50-01-2.

Part: CONNECTOR — DAMAGED (NLG)

ON UPLATCH, GEAR NOT LATCHED LIGHT IS ILLUMINATED. SAT DOING REPAIR, XFRD TO NRC 996802. DURING T/S FOUND NLG UP LIMIT SWITCH INOP. INSTALLED JUMPER WIRE CONNECTOR P1-218 PINS 7 AND 5 LIGHT CAME ON. REMOVED JUMPER WIRE AND GEAR NOT LATCH LIGHT WENT OFF. T/S PERFORMED IAW WDM 32-60-01. CK'D RT AND LT MLG GEAR UPLATCH CLEARANCES AND OPERATION AND CKS GOOD PER DC8 MM 32-31-03-2. CK'S NLG UPLATCH CLEARANCES AND OPERATION AND CKS GOOD.

Part: ACTUATOR — CRACKED (TE FLAP) · airframe 80,100 hrs · 22,594 cycles

WHEN FLAPS EXTENDED TO 23 DEGREES OUTER NEEDLE INDICATED 12 DEGREES INNER NEEDLE INDICATED 23 DEGREES, REQUIRED 4 UNITS OF RT AILERON TRIM FOR LEVEL FLIGHT. UPON INSPECTION FOUND LT STA 98 FLAP ACTUATOR PISTON ROD CRACKED IN TWO. REMOVED AND REPLACED STA 98 LT FLAP ACTUATOR.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 80,092 hrs · 25,938 cycles

INSPECTION TYPE: C3 COMPT 60 L17L HAS A 3 INCH CRACK STA 1770 (GOING UNDER END FITTING). REMOVED LONGERON, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-20D, 53-5-03 FIG 5.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 80,092 hrs · 25,938 cycles

INSPECTION TYPE: C3 60 COMPT L17R HAS 3 INCH CRACK STA 1770 (GOING UNDER END FITTING). REMOVED LONGERON AT STA 1770 L17R. FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21, 51-1-20D, 51-3-0 AND 53-5-03 FIG 5.

Part: RIB — CRACKED (L/E SLAT) · airframe 80,092 hrs · 25,938 cycles

C1, 3 RT CENTER LEADING EDGE UPPER RIB AT XFS 415 IS CRACKED. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 002, 51-1-21 AND 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,092 hrs · 25,938 cycles

C2 D-PIT STA 1394 L34R FRAME IS CRACKED. REMOVED DAMAGED AREA. FABRICATED AND INSTALLED REPAIR ANGLES IAW 53-2-0 FIG 1F, 53-04-01-0 FIG 051, 51-01-21 AND 51-01-20D.

Part: RIB — CRACKED (L/E SLAT) · airframe 80,092 hrs · 25,938 cycles

C1, 3 RT OB LEADING EDGE UPPER RIB CRACKED AT XFS834. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-02-00 FIG 002, 51-1-21 AND 51-1-20D.

Part: SKIN — CORRODED (FUSELAGE) · airframe 80,092 hrs · 25,938 cycles

INSPECTION TYPE: C2 REMOVE AND REINSTALL C-4 DOOR SCUFF PLATE TO FOM NDT. REMOVED CORROSION AND REPAIRED IAW EA 008-5312-01-A0287 AND UPS EO DC8-5330-24719-A.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 80,092 hrs · 25,938 cycles

INSPECTION TYPE:C2 C-PIT LONGERON 35R STA 1260-1280 CRACKED ON IB SIDE. REMOVED AND REPLACED LONGERON CHANNEL. IAW SRM 51-3-0 AND 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,092 hrs · 25,938 cycles

INSPECTION TYPE:C2 BATH-TUB FITTING CRACKED AT STA 1180 BETWEEN L34R TO L35R. REMOVE BATHTUB FITTING. FABRICATED SPLICES AND INSTALLED BATHTUB AND SPLICES IAW SRM 51-01-20D, 53-2-0 FIG 2G.

Part: SEAT TRACK — GOUGED (FS 820-900) · airframe 80,092 hrs · 25,938 cycles

FOUND GOUGE ON SEAT TRACK AT FS 900 RBL 46 IN MAIN CARGO COMPT. CUT OUT DAMAGED SEAT TRACK FROM FS 820-900 RBL 46 IAW SRM 53-2-3, FABRICATED AND INSTALLED SEAT TRACK SPLICE FROM FS 820-900 IAW SRM 53-02-03 FIG 13 AND UPS EO DC8-5320-8309-D.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 80,092 hrs · 25,938 cycles

INSPECTION TYPE:C2 SEAT TRACK GOUGED AT FS 880 RBL 46 IN MAIN CARGO DECK. CUT OUT DAMAGED SEAT TRACK AT STA 880 RBL 46 IAW SRM 53-02-03 FIG 006D. DRILLED UP AND INSTALLED SEAT TRACK PLUG AT STA 880 RBL 46 IAW SRM 51-3-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,092 hrs · 25,938 cycles

INSPECTION TYPE:C2 HEAVY CORROSION ON SEAT TRACK AT STA 1290 LBL 60, MAIN CARGO DECK CUTOUT DAMAGED SEAT TRACK AT STA 1290 LBL 60 IAW SRM 53-02-03 FIG 006. LOCATED, DRILLED UP HOLES IN SEAT TRACK PLUG REPAIR IAW SRM 51-3-2. INSTALLED SEAT TRACK PLUG AT STA 1290 LBL 60 IAW SRM 51-3-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 80,092 hrs · 25,938 cycles

INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK AT STA 465 LBL 60 HAS EXFOLIATION CORROSION. CUT OUT DAMAGED SEAT TRACK AT STA 460-600 LBL 60 IAW SRM 53-2-0 FIG 12. LOCATED, DRILLED UP AND INSTALLED REPLACEMENT SEAT TRACK AT STA 460-600 LBL 60 IAW SRM 51-1-21 AND SRM 51-3-0

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 80,092 hrs · 25,938 cycles

INSPECTION TYPE:C2 CABIN SEAT TRACK AT STA 240 RBL 44 IS GOUGED AND SCALLOPS ARE DAMAGED. CUT OUT DAMAGED SEAT TRACK IAW EO DC8-5340-7779 AT STA 240 RBL 44 INSTALLED SEAT TRACK PLUG AT STA 240 RBL 44 IAW SRM 51-3-0, AND EO DC8-5340-7779.

Part: RIB — CRACKED (RT WING LE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE: C-3, RT CENTER L/E HAS CRACKED RIB AT APPROX STA 304.600. REMOVED EXISTING REPAIR IAW DC8 SRM 51-1-211. MAT ID FOR REPAIR ANGLE BAC 1503-100147 EXTRUSION 7075-T6 PO 437138. STOP DRILLED CRACKED. LOCATED, DRILLED & DEBURRED REPAIR ANGLE. ALODINED & PRIMED. INSTALLED REPAIR ANGLE IAW DC8 SRM 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE: C-3, RT CENTER 4E HAS CRACKED RIB AT APPROX STA 448.00. REMOVED FASTENERS IN REPAIR AREA RT CENTER L/E AT STA 448.00 & STOP DRILL CRACK. MAT ID FOR REPAIR ANGLE 9751065-33 EXTRUSION 7075-T6 PO 387706. PERFORMED HFEC IAW MD NDT SPM 06-10-01.001, NO CRACKS INDICATED BEYOND STOP DRILL. CUTOUT, FAB, LOCATED, DRILLED & DEBURRED REPAIR ANGLE. ALODINED & PRIMED ANGLE. INSTALLED REPAIR ANGLE IAW DC8 SRM 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE:C-3, RIGHT WING CTR L/E RIB CRACKED AT APPROX STA XFS 304 VERIFIED BY NDT. PERFORMED AFEC IAW DAC SPM NDT 06-10-001-01 TO VERIFY CRACK END AT FASTENER HOLE. MAT THICKNESS FOR RIB AT STA XFS 304 .063 7075-T6, MAT ID FOR REPAIR ANGLE 7075-T6 .080 PO 437138.5. FAB REPAIR ANGLE IAW DC8 SRM 57-2-0, ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0.

Part: RIB — CRACKED (RT WING) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE:C-3, RIGHT CENTER L/E RIB CRACKED AT APPROX STA 379.000 VERIFIED BY NDT. STOP DRILL CRACK. MAT ID FOR RIB AT XFS 379 .063 7075-T6. MAT ID FOR REPAIR ANGLE 7075-T6 .080 PO 437138.5. ACCOMPLISHED HFEC INSP OF STOP DRILL IAW DAC NTSPM 06 10-01.001. FAB REPAIR ANGLE, ALODINED & PRIMED REPAIR ANGLE IAW DC8 SRM 51-1-8 AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0.

Part: SEAT TRACK — CORRODED (600 RBL 60) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE: C-3, FWD PIT FS 600 MIDDLE ROW OF FASTENERS IN SEAT TRACK SPLICE (AS SEEN FROM BELOW) LOCATED AT BC 60 R- CORROSION AROUND FASTENERS & SPACER. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-3. MAT ID FOR SEAT TRACK SPLICES A & B 7075-T6 .160 PO 333834.1 IAW DC8 SRM 53-2-3. FABBED CENTER SEAT TRACK SPLICES A & B, OB & I/B C, D & E SPLICES IAW DC8 SRM 51-1-8, INSTALLED CENTER SEAT TRACK & SPLICES A & B, I/B & O/B & C, D & E. INSTALLED FLOOR PANEL STA 580-608 RBL 60, AIR GRILL STA 513-702.

Part: FITTING — CRACKED (FUSLEAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE:C-3 MAIN CABIN FS 25 LONGERON 22 END FITTING CRACKED. REMOVED FITTINGS IAW DC8 SRM 51-3-0, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-3-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTINGS IAW DC8 SRM 51-1-20D, 51-3-0, 51-3-1.

Part: DOUBLER — BROKEN (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE:C, NOSE EXT PWR RECEPTICAL DOOR PNL CUTOUT HAS BROKEN SECTION. REMOVED INNER DOUBLER IAW DC8 SRM 51-1-21. MAT ID FOR NEW DOUBLER 7075-T6 .063 PO 428102.3 IAW DC8 DWG 5613862 & DC8 SRM 51-9-0 FIG 68A. FAB NEW DOUBLER, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER IAW DC8 SRM 51-1-21 & 51-1-21A.

Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE: C, EXISTING REPAIR DOUBLER AT EXT PWR RECEPTICAL FOUND TO HAVE PREVIOUS DAMAGE ON FAYING SURFACE (GOUGE). REMOVED DOUBLER. MAT ID FOR NEW DOUBLER 7075-T6 .063 PO 442690.4 IAW DC8 SRM 53-2-0 & 51-9-0 FIG 68A. FAB DOUBLER IAW DC8 SRM 51-1-8, INSTALLED DOUBLER IAW DC8 SRM 51-1-2 & 51-1-21A.

Part: RIB — GOUGED (RT WING) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE: C-3, RT WING OUT BOUND L/E INBOARD END RIB HAS DEEP GOUGE. BLENDED GOUGE AREA, FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 2G. FAB DOUBLER REPAIR IAW DC8 SRM 57-2-0 AND 51-1-4. LOCATED & DRILLED DOUBLER IAW DC8 SRM 51-1-24 & 51-2-0. ALODINED & PRIMED DOUBLER IAW DC 8 SRM 51-1-8. INSTALLED DOUBLER REPAIR IAW DC8 SRM 51-1-20D AND 51-2-0 FIG 2.

Part: FRAME — CORRODED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE: C-3, STA 35 AT LONGERON 22R CORRODED AT FRAME. REMOVED FRAME SECTION TO FOM FAB NEW FRAME SECTION AND SPLICES INSTALLED NEW FRAME SECTION AND SPLICES IAW DAC DWG 5613836 AND REO GO9859 AND DC8 SRM 51-1-21, 51-1-20D, 51-1-8.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE:C, LBL 25 SEAT TRACK SCALLOPS GOUGED AT BS 1138 & 1144 APPROX MAIN CARGO. BLENDED GOUGE IAW DC8 SRM 53-2-0, FOUND OUT OF LIMITS. CUT OUT SEAT TRACK FROM STA 1115 TO 1215 LBL 25. MAT ID P/N 60-15176 PO SPO 980402 ID FITTING SPLICE P/N DC8-53B-003-501 IAW EO DC8-5320-5167-C. LOCATED, DRILLED & DEBURRED SEAT TRACK & FITTING SPLICE. ALODINED SEAT TRACK, INSTALLED SEAT TRACK & FITTING SPLICE IAW DC8 SRM 51-3-0.

Part: RIB — CHAFED (RT WING) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE: C-3, RIGHT WING LEADING EDGE INTERIOR RIB CHAFED ABOVE PNEUMATIC SHUT OFF VALVE. INSTALLED REPAIR DOUBLER IAW 57-2-0.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE:C, SEAT TRACK GOUGED AT FS 860 45 RBL. BLEND GOUGE IAW DC8 SRM 53-2-0, FOUND OUT OF LIMITS. LOCATED & DRILLED DC8-53B-007-006 CHANNEL & DC8 53B-007-002 PLUG. OK TO INSTALL, REMOVED DAMAGED IAW DC8 SRM 53-2-3, INSTALLED PLUG & U-CHANNEL IAW DC8 SRM 51-3-0 AND 51-3-1.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE: C, GOUGE ON SEAT TRACK AT FS 1310 45 LBL. BLEND GOUGE AREAS IAW DC8 SRM 53-2-0, OUT OF LIMITS. LOCATED & DRILLED SEAT TRACK PLUG DC8-53B-007-002 & DC8-53B-007-006, CHANNEL IAW DC8 UPS EO DC8-5340-7779. ALODINED & PRIMED IAW SRM 51-1-8, INSTALLED PLUG & CHANNEL IAW DC8 SRM 51-3-0.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE:C-3, CABIN SEAT TRACK LBL 25 STA 850- 870 CORROSION MARKED DOT C 6580. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-3. REMOVED SEAT TRACK MAT ID FOR NEW SEAT TRACK 2772660/60-15176 PO SPO771694 IAW DC8 SRM 53-7-3 & UPS EO DC8-5320-5167C. MAT ID FOR SEAT TRACK SPLICE FITTING PO DC8-53B-003-501, PO SPO990445. FAB SEAT TRACK & FITTINGS. LOCATED, DRILLED & DEBURRED. ALODINED & PRIMED. INSTALLED SEAT TRACK & FITTINGS.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE:C, CABIN SEAT TRACK LBL 50 FROM STA 740 TO STA 770 WW & GOUGED AREAS. REMOVED GOUGE AND WORN SPOTS, FOUND TO BE OUT OF LIMITS. CUT OUT DAMAGE ON TRACK. LOCATED & DRILLED 745295-3 PLUGS & DC8-53B-007-006 CHANNEL IAW DC8 SRM 53-2-3 & UPS EO DC8-5340-7779B, ALODINED & PRIMED, INSTALLED 2 PLUGS AND 2 CHANNELS IAW DC8 SRM 51-3-0.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE:C-3 CABIN SEAT TRACK BL 0 AT STA 850 TO 870 WORN & GOUGED SCALLOPS. BLENDED GOUGE IAW DC8 SRM 53-2-0. FOUND OUT OF LIMITS, CUT OUT DAMAGE IN TRACK IAW DC8 SRM 53-2-3 & EO DC8 5340-7779B. ALODINED & PRIMED SEAT TRACK, MAT ID SEAT TRACK P/N DC8-53B-007-002, PO SP0906208, CHANNEL SEAT TRACK, LOCATED AND DRILLED, PLUG AND CHANNEL ON SEAT TRACK. INSTALLED PLUG SEAT TRACK CHANNEL SEAT TRACK ON SEAT TRACK.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE:C-3, FS 1580, RBL 24 FLOOR TRACK GOUGED (DOT B7269). BLENDED GOUGED AREA, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-3. MAT ID FOR SEAT TRACK 60-15176/2772660 PO SP0916641. LOCATED & DRILLED HOLES. ALODINED & PRIMED, TRANSFERRED SPACERS 2 EACH FROM OLD TO NEW SEAT TRACK, INSTALLED SEAT TRACK TO WEB & FLOORBEAMS. DRILLED HOLES FROM FLOORBOARD. REINSTALLED FLOORBOARDS STA 1520-1600, RBL 20, 1600-1680 RBL 24.

Part: LONGERON — GOUGED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE:C-3 FWD PIT STA 460-480 L31L GOUGED. REMOVED GOUGES, FOUND OUT OF LIMITS, GEN RFTS, REC'D RFTS W/ REO GO98956, FAB LONGERON SPLICES IAW REO-G098956, ALODINED & PRIMED, FAB NEW LONGERON SEC & REPAIRED. REC'D HEAT TREAT, LOCATED, DRILLED & PRIMED. INSTALLED STA 460 & 480, INSTALLED LONGERON SEC STA 450-470 IAW REO GO9895 6 & DC8 SRM 51-1-20D, 51-1-21, 51-1-24, 53-2-0, & 53-4-1.

Part: FITTING — CORRODED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE: C-3, FWD PIT STA 270 TORQUE BOX ATTACH FITTING HAS CORROSION BETWEEN L33R AND L34R. REMOVED CORRODED FITTING, LOCATE NEW FITTING AND DRILL EXISTING FASTENER HOLES FAB REPAIR ANGLES, LOCATE, DRILL, FASTENER HOLES, TRIM ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND 51-1-21, 51-3-2. INSTALLED FITTING AND REPAIR ANGLES IAE DC8 SRM 51-1-21 AND 53-2-0.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE: C-3, MAIN CARGO AREA STA 25 RT SIDE CUSP MEMBRANE HAS CORROSION. REMOVED 2 FITTINGS FROM FS 25, REMOVED FLOOR SUPPORT ANGLES, REMOVED WEB, REMOVED CUSP ANGLES. FABBED CUSP ANGLES IAW DAC DWG 5615180. ALODINED & PRIMED. INSTALLED SUPPORT ANGLE, 2 ANGLE, FLOOR SUPPORT ANGLE, WEB IAW DC8 SRM 51-1-21, 51-20D, 51-3-0, 51-3-1. TWO FITTING FS 25 REMOVED FOM REPLACED ON UPS NR 712495 141495.

Part: FITTING — CORRODED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE:C-3 AFT PIT STATION 1200 FITTING IN TORQUE BOX 1 FT INBD OF DOOR CUTOUT IS CORRODED. REMOVED CRACKED Z-FITTING IAW DC8 SRM 51-1-20D. REC'D, LOCATED, & DRILL NEW Z-FITTING AND -3, -5 REPAIR ANGLES IAW DC8 SRM 51-1-24. FAB -7 & -9 IAW DC8 SRM 53-2-0. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D.

Part: DOUBLER — CORRODED (RT WING) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE: C-3, RT WING L/E CENTER SECTION HAS CORROSION AROUND STALL WARNING SWITCH AND NUT PLATES. BASE DOUBLER FOR STALL WARNING SWITCH IS FOUND TO BE OUT OF LIMITS IAW DC8 SRM 57-2-0. MAT ID 7075-T6 .063 PO 442960.4 FOR FAB OF NEW DOUBLER IAW DAC DWG 5769589. FAB NEW -89 DOUBLER. ALODINED AND PRIMED. INSTALLED DOUBLER. REMOVED STALL TRANSDUCER IAW DC8 MM 34-16-01. REINSTALLED STALL TRANSDUCER. OPS CHECKED GOOD IAW DC8 MM 34-16-00.

Part: FRAME — CORRODED (FUSLEAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE:C-3 FWD PIT FRAME HAS CORROSION FWD SIDE AT STA 140 BETWEEN L34L AND L34R. REMOVED FASTENER TO FRAME IAW DC8 SRM 51-1-21D, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED AND REPLACED FRAME SECTION. LOCATED AND DRILLED SPLICE ANGLE REPAIR AND FRAME IAW DC8 SRM 51-1-24. ALODINED AND PRIMED. INSTALLED FRAME, SPLICE AND GILLINER ATTACH IAW DC8 SRM 51-1-20D.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 792,231 hrs · 25,248 cycles

INSPECTION TYPE: C-3, FWD PIT L31R HAS CORROSION AT STA 85 AROUND FASTENERS. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53-9-0. FAB REPAIR ANGLE IAW DC8 SRM 51-2-1 TR51-130, REMOVED FASTENERS FOR ACCESS IAW DC8 SRM 51-1-2D & 51-1-21. ALODINED & PRIMED. INSTALLED REPAIR ANGLE & FASTENERS THAT WERE REMOVED FOR ACCESS IAW DC8 SRM 51-1-20D AND 51-1-21.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE:C-3 LEFT W/W AT KEEL BEAM AT FS 922 TO 936 HAS A CRACK. REPAIRED IAW REO GO9853.

Part: FITTING — CORRODED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE: C-3, R/S CUSP FRAME 35 FWD & AFT CUSP FITTING ARE CORRODED AT FLOOR AT BOLTS B6 69. REMOVED CUSP FITTINGS FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. DRILLED NEW FITTING IAW DC8 SRM 51-3-2. ALODINED & PRIMED IAW DC8 SRM 51-1- 8. INSTALLED FITTING IAW DC8 SRM 51-1-20D, 51-3-0, 51-3-1.

Part: FRAME — CORRODED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE: C-3, AC COMPT STA 55 LONG 30-31 RIGHT CORR AT INTERSECTION OF FRAME TO T/R BOX LEG ANGLE. RECEIVED FRAME SECTION AND SPLICES FROM STRUCTURE CENTER WORK ACCOMPLISHED ON TIMCO N/R 5001. FAB 4 EA SPLICES 2-19 & 2-17 IAW TR 53-125, THEN HEAT TREATED. LOCATED, DRILLED, DEBURRED FRAME & SPLICE SECTION. ALODINED & PRIMED FRAME & SPLICES. INSTALLED REPAIRED ANGLES. INSTALLED TR PUMP BOX & TRANSFORMER. REMOVED CORROSION FOUND OUT OF LIMITS.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE: C-3, MID ACC COMPT CORRODED LONG 31 RT STA 640-668. REMOVED CORROSION, FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0. REMOVED SECTION LONGERON STA 610 TO 710 IAW DC8 SRM 51-1-20D. RECEIVED, LOCATED & DRILLED UP LONGERON NR 2646610, IAW DC8 SRM 51-1-24, ALODINED & PRIMED IAW DC8 SRM 51-1-8, INSTALLED LONGERON IAW DC8 SRM 51-1-20D.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 79,223 hrs · 25,248 cycles

INSPECTION TYPE: C, LUG BROKEN POS 3 LEFT O/B SEAT TRACK PLANK NEXT TO LOCK. REMOVED AND REPLACED SEAT TRACK PLANK SECTION FS-200 TO FS-265-00.

Part: WINDOW FRAME — CORRODED (COCKPIT)

INSPECTION TYPE:N/A SEVERAL AREAS OF CORROSION ON CTR WINDSHIELD LOWER FRAME. CHECKED CORROSION PITTING WITH DIAL DEPTH GAUGE, DEEPEST FITTING IS .020 REMOVED ALL PITTING IAW SRM 51-1-4-8. ULTRASOUND AREAS. FOUND .077 REMAINING. BLEND CORROSION IAW SRM 53-02-00 FIG 1F WITHIN LIMITS

Part: BATTERY PACK — INOPERATIVE (FLIGHT DECK)

EMERGENCY LIGHTS WILL NOT TEST. REPLACED BATTERY PACK, OPS CHECK NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

ON PREFLIGHT EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW DC8 MM 33-50-01. EMERGENCY EXITS OPS CK NORMAL.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

EMERGENCY LIGHTS INOP ON PREFLIGHT. C/BS OUT AND SWITCH IN OFF POSITION AFTER WEEKEND. REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK OK.

Part: CONTROL VALVE — MALFUNCTIONED (LT MLG)

INSPECTION TYPE:N/A ON TAXI OUT A/C FELT LIKE LEFT BRAKES WERE DRAGGING. REMOVED AND REPLACED WHEEL BRAKE CONTROL VALVES PER MM 32-42-02. PERFORMED ADJ /TEST OF SYSTEM, ALL BRAKES OPERATE NORMALLY. A/C OK TO SERVICE.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,503 cycles

INSPECTION TYPE:C1, L1 DOOR UPPER FWD DOOR JAMB CORNER CRACKED, FOUND BY X-RAY INSPECTION. ROUTED OUT CRACKED SKIN IAW DC8 SRM 53-2-0 FIG 15. VERIFIED CRACK REMOVAL IAW HFEC WPM 06-10-01.001. REMOVED EXISTING DOUBLER, TRIPLER DOOR SILL, OVERHEAD WEB AND DOOR CORNER PAN, FABBED FILLER DOUBLER TRIPLER IAW 53-2-0 FIG 15. INSTALLED REPAIR PARTS IAW 51-1-20 D AND 51-1-21.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 78,333 hrs · 24,503 cycles

INSPECTION TYPE:C1 L31L STA 620-650 HAS EXFOL CORROSION. FABBED NEW LONGERON IAW DAC DWG 3750575. FABBED LONGERON CLIP IAW DAC DWG 5610416. LOCATE NEW SPLICE FITTING, DRILLED EXISTING FASTENER HOLES, INSTALLED NEW LONGERON SPLICE FITTING.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 78,333 hrs · 24,503 cycles

INSPECTION TYPE:C1 AC COMPT FS 24 L35R STRAP UNDER SHEAR TIE SKIN UNDER STRAP IS CORRODED. REMOVED AND REPLACED DOUBLER 2 SHEAR TIES STRAP LONGERONS L36, L35 AND L35R IAW DC8 SRM 53-2-1 PG 113, 51-1-21, 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 R1 DOOR AFT DOOR JAMB CRACKED AT FASTENER HOLE APPROX LENGTH .375 INCH LONG ON FUSELAGE SKIN. ROUTED OUT CRACK IN EXTERIOR SKIN VERIFIED CRACK REMOVAL IAW HFEC NDT SPM 06-16-01-001. FABBED FILLER DOUBLER AND TRIPLER IAW DC8 SRM 53-2-0 FIG 14. INSTALLED DOUBLER AND TRIPLER REPAIR IAW 5 3-2-0 FIG 14, 51-1-20C, 51-1-21 & 51-1-20D.

Part: INTERCOSTAL — CRACKED (R1 DOOR) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 R1 DOOR FWD TORQUE BOX INTERCOSTAL JUST ABOVE LOWER CLEAR HINGE IS CRACKED. REMOVED INTERCOSTAL, FAB INTERCOSTAL IAW DAC DWG 5615700, ALODINED & PRIMED IAW DC8 SRM 51-1-21 & 511-20D.

Part: DOOR FRAME — DAMAGED (CARGO DOOR) · airframe 78,333 hrs · 24,503 cycles

INSPECTION TYPE:C1 RT FWD DOOR UPPER FWD ELONGATED HOLE ON FRAME. FABBED DOUBLER IAW DAC DWG 5615762 AND INSTALLED SAME IAW DC8 SRM 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 STA 940 RT FRAME FITTING AT PRESSURE WEB IS CRACKED. REMOVED INTERCOSTAL AND FITTING L21 LOCATED & DRILLED NEW FITTING IAW DAC DWG 5751966 INSTALLED END FITTING AND INTERCOSTAL IAW DC8 SRM 51-1-20D.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 AFT LWR ATTACH STRUCTURE FOR RADIO RACK CLOSEOUT PANEL HAS LIGHT CORROSION AND BARE METAL ON INTERNAL AND EXTERNAL SIDES. REMOVED ANGLE IAW DC8 SRM 53-2-9 AND IAW DAC DWG 564057 1. FABBED IAW DAC DWG 5640571, INSTALLED CHANNEL IAW DC8 SRM 51-2-21 & 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 MAIN CABIN 680 S11L LONGERON FITTING CRACKED. REMOVED FITTING, ALODINED, PRIMED & INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 51-1-20D & 51-1-24.

Part: FITTING — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,503 cycles

INSPECTION TYPE:C1 MAIN CABIN 680 S11L LONGERON FITTING CRACKED. REMOVED FITTING, ALODINED, PRIMED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-8, 51-1-20D, 51-1-24.

Part: FITTING — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 AFT PIT FS 1160 C3 DOOR RAMP PANEL SUPPORT FITTING AT L27L - L34 IS CRACKED. REMOVED SUPPORT FITTING LOCATED & DRILLED HOLES IAW DC8 SRM 51-1-24 INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 AFT PIT FS 1160 C3 DOOR RAMP PANEL SUPPORT FITTING AT L27L L36 IS CRACKED. REMOVED SUPPORT FITTING LOCATED AND DRILLED HOLES IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB CORNER CRACKED AT FASTENER HOLE EXTERNAL FUSELAGE SKIN LENGTH APPROX .25 TO .3125 INCH LONG. FOUND BY EDDY CURRENT. REPAIRED DOOR JAMB IAW DC8 SRM 53-2-0 FIG 16.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 MAIN CABIN STA STA 1334 AND BL 0 SEAT TRACK IS CRACKED. R&R DAMAGED SECTION OF SEAT TRACK IAW UPS EO DC8-5320-5767

Part: PLATE — CRACKED (CARGO DOOR) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 MCD AFT VERT SCUFF PLATE AND DOUBLER ARE CRACKED STA 272 AND L10L. FABBED DOUBLER IAW DC8 SRM 51-1-8, INSTALLED DOUBLER IAW DC8 SRM 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 LONGERON FITTING CRACKED STA 680-11R. R&R FITTING IAW DC8 MM 51-1-21 & 51-1-24.

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 FLOORBEAM AT STA 759 CHAFED BETWEEN RBL 0-24. REPAIRED FLOORBEAM IAW DC8 SRM 532-0 TR 53-124.

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 FLOORBEAM AT STA 717 CHAFED BETWEEN RBL 0-24. REPAIRED FLOORBEAM IAW DC8 SRM 53-2-0 TR 53-124.

Part: FLOORBEAM — CHAFED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 FLOORBEAM AT STA 742 CHAFED BETWEEN RBL 0-24. REPAIRED FLOORBEAM IAW DC8 SRM 53-2-0 TR 53-124.

Part: SKIN — DENTED (HORIZ STAB) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 DENT IN RT HORIZ STAB LE 35 INCHES O/B AT ROOT. REMOVED DAMAGED AREA DENT FOUND TO BE OUT OF LIMITS. FABBED REPAIR DOUBLER IAW SRM 55-2-1. INSTALLED DOUBLER IAW SRM 51-1-21.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 MAIN CABIN FLOORBEAM CORRODED AROUND NUTPLATE STA 980 LBL 10. REPLACED SECTION OF FLOORBEAM CAP IAW DC8 SRM 53-2-0 TR 53-124

Part: WEB — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 AFT PIT STA 1400 L33R & L34R WEB LIGHTENING HOLE CRACKED/SPLIT. CUT OUT DAMAGE PER DC8 SRM 53-2-0. INSTALLED PER DC8 SRM 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 AFT PIT FS 1480 L34L LONGERON IS CRACKED. REMOVED CRACKED LONGERON AND REPLACED LONGERON SECTION IAW DC8 SRM 53-2-2 FIG 4A & 51-1-20D.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 L2 DOOR LWR FWD CORNER CRACKED, FOUND BY X-RAY INSPECTION. REPAIRED AREA IAW DC8 SRM 53-2-0 FIG 18.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 AFT PIT FS 1480 L34L LONGERON IS CRACKED. REMOVED CRACKED LONGERON AND REPLACED LONGERON SECTION IAW DC8 SRM 53- 2-2 FIS 4A & 51-4-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1, LONGERON 36 IS CRACKED UNDER FLANGE AT APPROX FS 1272. REMOVED LONGERON SECTION, 2 LONGERON SPLICES, SPLICES FOUND IN LIMITS IAW 53-2-0. LOCATED & DRILLED NEW LONGERON SECTION, INSTALLED NEW LONGERON SECTION AND 2 LONGERON SPLICE IAW DC8 SRM 51-1-20D.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 MAIN CABIN FLOOR SUPPORT AT STA 1762 RBL 11 HAS DRILL STARTS WITH CORROSION. REMOVED FLOOR BOARD SUPPORT IAW DC8 SRM 51-1-20D. FABBED FLOOR BOARD SUPPORT IAW DC8 SRM 53-7-1 AND INSTALLED SUPPORT IAW DC8 SRM 51-1-20D

Part: DOOR FRAME — DAMAGED (R1 DOOR) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 RT FWD DOOR UPPER FWD ELONGATED HOLE ON FRAME. FABBED DOUBLER IAW DAC DRW 5615762 AND INSTALLED SAME IAW DC8 SRM 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 LONGERON 36 CRACKED UNDER FLANGE AT APPROX FS 1272. REMOVED LONGERON SECTION (2) LONGERON SPLICES, SPLICES FOUND TO BE IN LIMITS IAW SRM 53-2-0. LOCATED & DRILLED NEW LONGERON SECTION, INSTALLED NEW LONGERON SECTION AND 2 LONGERON SPLICES IAW SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 AFT CARGO BAY FRAME CAP IS CORRODED STA 1060 STRINGER 36. CORROSION OUT OF LIMITS IAW 53-2-0. REMOVED FRAME CAP. FAB REPAIR ANGLE IAW UPS EO DC8-5310-11728-A. INSTALLED FRAME CAP REPAIR IAW DC8 SRM 51-1-20D & 51-1-21E.

Part: OUTFLOW VALVE — CORRODED (CABIN PRESSURE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 AFT ACCY COMPT CABIN AIR OUTFLOW NOZZLE VALVE HAS CORROSION AROUND AREA. CORROSION ON NOZZLE VALVE OUT OF LIMITS. REMOVED AND REPLACED NOZZLE IAW DC8 MM 21-31-04, OPS CHECKED IAW DC8 MM 21-31-04.

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 AFT CARGO BAY FRAME IS CORRODED STA 1100 STR 36. REMOVED CORROSION, REMOVED DAMAGED SECTION OF FRAME, FABBED REPAIR ANGLE FILLERS & REPAIR STRAP LOCATED DRILLED REPAIR PARTS & INSTALLED REPAIR ANGLE FILLERS & REPAIR STRAP IAW UPS EO DC8-5310-117 28 APP B DC8 SRM 51-1-8 53-2-0 51-1-24 & DAC DWG 2537716

Part: FRAME — CORRODED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 AFT CARGO BAY CORRODED UNDER NUTPLATE ON FRAME STA 1020 STRINGER 34R. REMOVED CORROSION, OUT OF LIMITS. FABBED DOUBLER & FILLERS. INSTALLED DOUBLERS & FILLER GUSSETS & CLIP IAW EO DC8-5310-11728 DWG DC8-53A-011 SRM 53-2-0 51-1-8 51-1-24 51-1-20D

Part: ANGLE — CRACKED (RT WING) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 RT WING FLAPWELL ATTACH ANGLE AT XW0 REAR SPAR CRACKED. FABBED ANGLE IAW DAC DWG 5651221 & INSTALLED ANGLE AND SKIN PANEL IAW DC8 SRM 51-1-21 51-3-0.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 78,333 hrs · 24,523 cycles

INSPECTION TYPE:C1 AFT PIT C3 DOOR RAMP PANEL FOLDING DOOR SUPPORT FITTING IS CRACKED. REMOVED PANEL AND FOUND SKIN CRACK FABRICATE NEW SKIN IAW DAC DWG 97540 58. ALODINED & PRIMED IAW DC8 SRM 51-1-8. REMOVED SUPPORT FITTING LOCATED NEW FITTING AND DRILLED EXISTING FASTENERS IAW DC8 SRM 51-1-24, INSTALLED SUPPORT FITTING AND SKIN IAW DC8 SRM 51-1-24.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 78,333 hrs · 24,503 cycles

INSPECTION TYPE:C1 POS 13 O/B SEAT TRACK DAMAGED AT SPLICE INTERIM REPAIR C/W PER EO DC8 -5310-15957A. CUT OUT DAMAGED TRACK IAW DC8 SRM 53-2-3. LOCATED AND DEBURRED SPLICE, ALODINED & PRIMED, FABBED, LOCATED, DRILLED & INSTALLED.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A GLARESHIELD AND EMERGENCY OVERHEAD LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK PER MM 33-50-01. OPS CHECKS GOOD.

Part: DOOR — DAMAGED (NLG)

INSPECTION TYPE:N/A VIBRATION FROM NOSE GEAR AREA. CREW DECLARED EMERGENCY. A/C LANDED SAFELY. LT NLG AFT DOOR HAS 8 INCH CRACK ON AFT END OF DOOR. DOOR REMOVED NLG DOORS REQUIRE ADJ AND TEST MM 32-22-01. FOUND LT AND RT NLG AFT DOORS BROKEN. LT DOOR WAS CRACKED. RT GEAR DOOR AFT HINGE BROKE OFF AT DOOR CAUSING PROBLEM. REMOVED AND REPLACED RT NLG AFT DOOR. PERFORMED NLG DOOR ADJ/TEST PROCEDURES, OPS CKS OK IAW MM 32-22-01.

Part: O-RING — LEAKING (NR 3 ENGINE)

INSPECTION TYPE:N/A NR 3 ENGINE FLAME-OUT CLIMBING THRU FL 350. RESTARTED DESCENDING THRU FL240. FOUND 2 GHAMMA COUPLING O-RINGS LEAKING DURING FUEL LINE NEG PRESS CHECK. O-RINGS WERE REPLACED AND ENGINE RUN ACCOMPLISHED PER 28-22-12.

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE:N/A CRACKS RT WING INBOARD OF INBOARD FUELING CAP (MARKED LOWER WING) BETWEEN NR 3 & 4 PYLON LWR WING) 28 INCHES FROM L/E & 3 INCHES FROM ACCESS PNL 1206. HFEC VERIFIED CRACK-CRACK TERMINUS CENTER PUNCH MARKED EP QC 70100 10-13-01. COMPLIED WITH EO DC8-5720-4087-B PERFORMED INTERIM REPAIR.

Part: CONTROL UNIT — FAILED (NR 2 ENGINE)

INSPECTION TYPE:NA DEPLOYED REVERSERS IN FLIGHT (280 KIAS) TO MEET CROSSING RESTRICTION, NR 2 WOULD NOT STOW. RAN CHECKLISTS THROUGH INFLIGHT SHUTDOWN. SLOWING THROUGH 200 KIAS, REVERSER STOWED. THREE ENGINE LANDING. INFLIGHT WINDMILLING. REMOVED NR 2 ENGINE THRUST REVERSER HYDRAULIC CONTROL UNIT PER MM 78- 31-01. INSTALLED NR 2 T/R HCE IAW MM 78-31-01. OPS AND LEAK CHECKS GOOD.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 77,439 hrs · 23,975 cycles

INSPECTION TYPE:SP STA 1668 SKIN IS BULGED RT SIDE OF A/C, STA 1655 BETWEEN LONG 29R AND 30R INTERNAL DOUBLER IS CORRODED BEYOND LIMITS. REPAIRED DOUBLER IAW 8110-3 APPROVED DH SK 803-121.

Part: CONTROL VALVE — INOPERATIVE (LT A/C PACK)

INSPECTION TYPE:N/A, LEFT PACK RUNS CONSTANTLY UNABLE TO CONTROL, CREW REPORTED SMOKE IN THE COCKPIT. FOUND AIR CONDITIONING FLOW CONTROL VALVE INOP. REMOVED AND REPLACED VALVE PER MM 21-55-05. SYS OPS CK NORMAL.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS DO NOT TEST APPROPRIATELY ON BITE CHECK BATTERY TEST. REPLACED EMERGENCY LIGHT PACK PER MM 33-60-00, CHECKS OK. P/N ON-OFF 60- 1223-3, S/N ON 259, S/N OFF 1125.

Part: LIGHT — SHORTED (COCKPIT)

INSPECTION TYPE:N/A, CREW PREFLIGHT-CREW REPORTED SMOKE IN COCKPIT. *S/D* DEFERRED AND DEACTIVATED VOLT AND FREQ SELECT SW BACKGROUND LIGHT PL ATE.

Part: FLANGE — MISDRILLED (DOOR SEAL) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE: C2 R-2 DOOR SEAL DEPRESSOR, LWR SECTION HAS BAD HOLES. LOCATED & DRILLED NEW SEAL DREPRESSOR IAW DC8 SRM 51-1-24. ALODINE & PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW SEAL DEPRESSOR IAW DC8 S RM 51-1-20D & 51-1-21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, FUSELAGE SKIN CRACKED AT R2 DOOR, FWD LWR CORNER. ROUTED OUT CRACK IAW DC8 SRM 53-2-0 FIG 16. FABBED AND INSTALLED REPAIR DOUBLERS AND FILLERS IAW DC8 SRM 53-2-0 FIG 16 AND 51-1-20D AND 5 1-3-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: STRINGER — CRACKED (RT WING) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, RT WING STRINGER 64 IS CRACKED PERFORM/COMPLY WITH S/B DC8-57-100 REV 1 DOUBLER REPAIR AS REQUIRED. FABBED REPAIR DOUBLER AND FILLER IAW EO DC8-5730-9004E MAT ID FOR DOUBLER 7075-T6 .160 PO NR 327307, INSTALLED FILLER AND DOUBLER IAW DC8 51-1- 20D & EO DC8-5730-9004E, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. LEAK CHECK TO BE DONE ON TC 8000/ OPS 400.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, INTERCOSTAL STA 1720 - 1740 L33R IS CRACKED. REMOVED INTERCOSTAL IAW DC8 SRM 51-1-21 & 51-1-20D. FABRICATED, INTERCOSTAL, LOCATED, AND DRILLED IAW DAC DWG NR 5649329 & DC8 SRM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED WITH HI-LOKS IAW DC8 SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, AFT PIT FS 1000 CORROSION ON LOWER SURFACE OF UPPER FRAME FLANGE AT L28R-L29R. REMOVED CORROSION, FABRICATED REPAIR STRAPS, ALODINED AND PRIMED REPAIR STRAP AND REPAIR AREA. INSTALLED REPAIR STRAPS IAW REO-G07379 & DC8 S RM 51-1-8, 51-3-0.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, AFT PRESSURE BULKHEAD LT SIDE CRACKED LBL 32 APPROX L11L. REPAIRED AREA IAW DAC DWG SR08530007. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: STRINGER — CRACKED (LT WING) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, LT WING STRINGER 64 IS CRACKED. PERFORM DC8 S/B 57-100 REV 1 DOUBLER REPAIR AS REQUIRED. FABBED DOUBLER AND FILLER IAW EO DC8 5730-9004. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED DOUBLER REPAIR IAW DC8 SRM 51-1-20 & 51-1-15.

Part: SPAR — CRACKED (RT WING) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, RT WING LOOKING I/B TO O/B AT WING TIP AREA, STATIC WICKS 2 AND 3 HAVE DAMAGED T/E SKIN. REMOVED WEDGE PNL, FOUND T/E SPAR CRACKED. FAB NEW WEDGE PNL AND T/E SPAR CHANNEL IAW DAC DWG NR 5644654. ALODINED AND PRIMED IAW DC8 SRM 51-1- 8. INSTALLED WEDGE PNL AND T/E SPAR CHANNEL IAW DC8 SRM 51-1-21A AND SEAL AREA IAW DC8 SRM 51-1-15.

Part: COVER — CRACKED (CARGO DOOR) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, C-PIT CROSS SLIDE DOOR COVER HAS 2 HOLES WITH A CRACK, ALSO CRACKED AROUND THE CORNER. FAB REPAIR DOUBLER IAW DC8 SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-21 AND 51-3-0.

Part: RIB — CRACKED (SLIDE COVER RAMP) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, C-PIT CROSS SLIDE DOOR COVER ON THE RAMP HAS RIB WITH 1 INCH CRACK. ORDERED NEW RIB, LOCATED AND DRILLED HOLES AND INSTALLED NEW RIB IAW DC8 SRM 51-1-21.

Part: SKIN — CORRODED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, CORROSION ON SKIN ABOVE LONG 25L STA 1640 AFT ACCESSORY COMP. REMOVED DAMAGED AREA, FAB EXTERNAL DOUBLER FILLER AND SHEAR TIE SPLICE. ALODINED AND PRIMED, REC''D LOCATED AND DRILLED 3 NEW LONG SPLICES (P/N DC8-53B-009-367). INSTALLED LONG AND 4 LONG SPLICES EXTERNAL DOUBLER, FILLER AND SHEAR TIE AND SPLICE.

Part: SEAT TRACK — SCORED (CABIN) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, FS 1000 - 1700 LBL 25 TRACK SCORED AS MARKED. INSTALLED PLUG STA 1700 IAW DC8 SRM 53-2-3. REMOVED AND REPLACED TRACK ON UPS N/R''''S 157912/157913. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2 CORROSION AROUND CLIP NUTS ON SEAT TRACK BETWEEN STA FS 1000 AND STA FS 1020 LBL 40L. REMOVED CLIP NUTS, REMOVED CORROSION IN AREA, ALODINED AND PRIMED AREA IAW DC8 SRM 51-1-8, AND INSTALLED CLIP NUTS IAW DC8 SRM 51-3-0.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, C-PIT CROSS SLIDE DOOR, TRACK COVER CRACKED. REMOVED DAMAGED FITTING, DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED NEW FITTING IAW DC8 SRM 51-3-0.

Part: SEAT TRACK — MISSING (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2 CORROSION ON SEAT TRACK BETWEEN STA FS 980 - 1000 AND SPLICES REPAIR MISSING AT OL (CENTER) IN AFT PIT. REMOVED CORROSION, ALODINED AND PRIMED AREA IAW DC8 SRM 51-1-8. FAB REP AIR SPLICE IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-3-0.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, CORROSION ON LONGERON 31R STA 1600 AFT ACCESSORY. REMOVED CORROSION FOUND OUT OF LIMITS. FABRICATED REPAIR ANGLE AND TAPERED FILLER. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. REPAIRD PARTS IAW DC8 SRM 51-1-8, 51-3-0, & REO G07401(A).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, AFT PIT SEAT TRACK HAS CORRODED FASTENERS FS 1500 THRU FS 1540 RBL 57. REMOVED CORROSION MATL OUT OF LIMITS IAW DC8 SRM 53-2-3. DRILLED SEAT TRACK (P/N S2772660-13500N) TO FIT FS1390 - 1580 IAW DC8 SRM 51-1-24. DRILLED SPLICE IAW UPS EO DC8-5320-5167. INSTALLED SEAT TRACK AND SPLICE IAW DC8 SRM 51-3-0.

Part: WEB — CRACKED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, FWD ACCESS STATION 65 L21L LOWER CUSP CRACKED. REMOVED, FABBED AND REPLACED CRACKED ANGLE IAW DC7 SRM 51-1-20D, 51-1-21A, 51-1-21, 51-1-8 AND DAC DWG 5597464.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2 AFT LWR CARGO PIT AT FS 1540 VERTICAL INTERCOSTAL ATTACHED TO LONG 30R IS CORRODED AT ATTACH POINT. REMOVED FASTENER FOR ACCESS TO CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0. FAB REP ANGLE AND SPLICES IAW DAC DWG 5646608 & DAC SRM 53-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-21, 51-1-20D AND 51-3-0.

Part: SUPPORT BRACKET — CORRODED (CARGO BAY) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, FWD LWR CARGO PIT AT FS 240 STANCHION IS CORRODED UNDER AND AROUND NUT PLATE. STANTION FOUND TO BE OUT OF LIMITS. REMOVED BAD SECTION, FAB DOUBLERS AND FILLER. ALODINED AND PRIMED REPAIR PARTS IAW DC8 SRM 51-1-8. INSTALLED REPAIR PARTS AND INSTALLED STANCHION.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, AFT PIT FS 1040 CORROSION ON LOWER SURFACE OF UPPER FRAME FLANGE AT L36. REMOVED CORROSION, FOUND OUT OF LIMITS REPAIR FRAME IAW UPS EO DC8-53-11728B & REO G07412. ALODINED AND PRIMED IAW DC8 51-1-8. REINSTALLED FRAME CAP, 2 INTERCOSTALS AND FRAME ANGLE IAW DC8 SRM 51-3-0.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, STA 917 BOTTOM KEEL BEAM AT PANEL ATTACH HAS CORROSION. REMOVED CORRODED ANGLE IAW DC8 SRM 51-1-21. MAT ID FOR -69 ANGLE IS .09 0 7075-0 PO 326167 IAW DAC DWG 5616306. FABBED NEW ANGLE IAW DAC DW G 5616306. LOCATED, DRILLED, DEBURRED IAW DAC DWG 5616306. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21 & 51-1-20D.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, FWD LWR CARGO PIT AT FS 70 DOOR LWR FRAME IS CORRODED ON LWR FLANGE. REMOVED ANGLE, FAB NEW ANGLE IAW DAC DWG 5613064. ALODINED AND PRIMED IAW 51-1-8. INSTALLED ANGLE IAW DC8 SRM 51-1-20.

Part: ANGLE — CRACKED (HORIZONTAL STAB) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, LT HORIZONTAL STAB ANGLE FWD OF FRONT SPAT AT HORIZONTAL ROOT CRACKED. REMOVED CRACKED ANGLE VERTICAL TRACK PER DC8 SRM 51-3-0, 51-1-21, 51-1-20D. FABBED AND INSTALLED NEW ANGLE PER DAC DWG 5654501 AND DC8 SRM 51- 1-21-, 51-1-20D. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: SKIN — CORRODED (ACCESS DOOR) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, AFT ACCESSORY COMPARTMENT ACCESS DOOR AT FS 1540 HAS CORROSION ON SKIN. REMOVED CORROSION SECTION OF SKIN. FABRICATED REPAIR DOUBLER IAW DC8 SRM 52-2-0. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, CORROSION ON SEAT TRACK A BETWEEN FS 40 TO 70. CUT OUT DAMAGED SECTION OF TRACK, SPLICED IN NEW SECTION IAW DC8 SRM 51-1-24 & UP EO DC8-53B-003.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, CORROSION IN SEAT TRACK AT APPROX FS 815. REMOVED DAMAGE, INSTALLED PLUG REPAIR IAW DC8 SRM 53-2-3.

Part: FRAME — CORRODED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, AFT PIT FS 1020 CORROSION ON LOWER SURFACE OF UPPER FRAME FLANGE AT L36. REMOVED DAMAGE SECTION OF FRAME FLANGE. FABRICATED AND INSTALL REPAIR ANGLE, STRAP, FILLER, FRAME CAP, INTERCOSTALS, GUSSETS & ''L'' ANGLES IAW DC8 SRM 51-1-21 & 51-1-20D. REPAIR TO FRAME FLANGE ACCOMPLISHED IAW UPS EO DC8-5310-1172-A & UPS DWG DC8-53A-010.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, INTERCOSTAL CRACKED FWD OF BULKHEAD 680 ATTACHED TO STR 23L. FOUND MAT ID 7075 F6 .016 PO NR 322196 FOR ZEE ANGLE -25 IAW DC8 DWG 57 03478. FAB NEW ZEE ANGLE -25 IAW DC8 DWG 5703478, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED ZEE ANGLE IAW DC8 SRM 51-1-21A.

Part: SKIN — GOUGED (LT ELEVATOR) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, LEFT ELE I/B LWR INSP HOLE GOUGED AND CRACKED. FAB AND INSTALLED DOUBLER IAW DAC DWG 5654970 & DC8 SRM 51-1-21.

Part: BRACKET — CRACKED (THRUST REVERSER) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, NR 4 ENG I/B TR INNER HEAT SHEILD ATTACH BRACKET ON AFT END 12 O''CLOCK POSITION IS CRACKED ON TOP SIDE OF BRACKET. REMOVED BRACKET FOR WELD SHOP, WELD REPAIRED IAW DC8 SRM 51-1-3. INSTALLED BRACKET IAW DC8 SRM 51-1-20A.

Part: PRESSURE PANEL — DAMAGED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, MLG WW PRESSURE DECK TOP SIDE, STA 960 - 980 CENTERLINE SPLICE DOUBLER HAS SEVERAL POPPED FASTENERS. REMOVED DOUBLER, FOUND CORROSION OUT OF LIMITS IAW DC8 SRM 53-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER IAW REO-G07384 & DAC DWG 5645332, DC8 SRM 51-1-21.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, AFT PRESSURE BULKHEAD RT SIDE CRACKED RBL 32, L11R. REPAIRED IAW DAC SRO DWG 8530007.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, ''2'' FITTING STA 1225 BETWEEN L33R & L34R FWD SIDE LWR HOLE CRACKED INSIDE TORQUE BOX. REMOVED CRACKED FITTING, RECEIVED, LOCATED AND DRILLED NEW FITTING (P/N 3755841-2) AND REPAIR PARTS -3, -5, -7, -9 DC8 SRM 53-2-0 FIG 2G. INSTALLED NEW FITTING AND REPAIR PARTS.

Part: FITTING — CRACKED (TE FLAP) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, STA 339.7332 LT WING D/B FLAP BASE FITTING HAS CRACK AT ABOUT .5 INCH ABOVE FROM SPAR OF FLAP. LOCATED AND DRILLED NEW BASE FITTING IAW DC8 SRM 51-3-2 & DAC DWG 5894 377 & 5751174. FABRICATED AND INSTALLED BUSHING IAW DAC DWG 5894377. LOCATED AND DRILLED NEW CTR FITTINGS IAW DC8 SRM 51-1-24. INSTALLED NEW BASE FITTING, ICE BREAKER AND SPRING PANELS IAW DC8 SRM 51-3-0 & 5 1-1-21 & 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,822 hrs · 23,635 cycles

INSPECTION TYPE:C2, FS 1754 L36, AFT PRESSURE PANEL VERT BEAM LWR ATTACHMENT FITTING CRACKED BOTH SIDES. REMOVED AND REPLACED FITTING IAW DAC DWG 5753522 AND DC8 SRM 51-1-20D & 51-3-0.

Part: LIGHT — INOP (FLIGHT DECK)

INSPECTION TYPE:IN, EMERGENCY EXIT LIGHT IN COCKPIT DOME AND ENTRY INOP. REMOVED AND REPLACED BATTERY PACK, CK OK. ON (P/N 5708458-503) (S/N 10389), OFF (S/N 339) (P/N 60-1223-5).

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTS BATT PACK, OPS CHECK GOOD. (P/N 60-1223-5), (S/N 339) ON, (S/N 337) OFF.

Part: WIRE — BROKEN (COCKPIT)

INSPECTION TYPE-N/A, THE EMER LIGHT OVER THE COCKPIT DOOR WILL NOT COME ON WHEN TESTED. FOUND BROKEN WIRE AT BATT PACK BUSS TERMINAL NR 2. REPAIRED WIRE AND EMER LIGHTS, OPERATED NORMAL.

Part: AUTO PILOT PANEL — FAILED (COCKPIT)

AUTOPILOT ROLL FUNCTION WOULD NOT ENGAGE, AIR ABORT, DUMPED 45,000 POUNDS OF FUEL, FUEL DUMP WIRE HAS BEEN CUT. FOUND NO VOLTAGE AT SERVO CLUTCH CONN. REMOVED AND REPLACED AUTO PILOT PANEL PER MM 22-10-02 OPS CK'D SYS PER 2200 SYS. CHK'S GOOD, P/N ON 622-6208-503 S/N ON 1140 OFF 622-6208-503 OFF 974.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMER BATTERY PACK IAW DC8 MM 33-50-01. OPS CHECKS GOOD P/N ON 5 7-08458-503 P/N OFF 60-1223-5 S/N ON FLT 135 S/N OFF 322.

Part: ANGLE — CORRODED (BS 1320)

INSPECTION TYPE-C, STA 1320 LWR FWD FLANGE OF FLOORBEAM HAS EXFOLIATION CORROSION BL 0 TO RBL 36. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW DWG 9887940 AND SRM 51-9-0.

Part: SKIN — CORRODED (BS 25-35)

INSPECTION TYPE:D, FUSELAGE SKIN EXFOLIATED BELOW EXISTING CUTOUT AT LG 27R BETWEEN F/S 25-35. REPAIRED IAW DHC SK-803-047.

Part: FORMER — CRACKED (BS 55)

INSPECTION TYPE:D F/S 55 FRAME FORMER CRACKED BETWEEN LONGERON 27-28 RT. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FORMER IAW SRM 53-2-0.

Part: LONGERON — CORRODED (BS 35-70)

INSPECTION TYPE-D, LONGERON 27R EXFOLIATED FS 35 TO 70. REMOVED AND REPLACED LONGERON IAW SRM 51-1-21.

Part: LONGERON — CORRODED (BS 8-70)

INSPECTION TYPE:D, CORROSION REMOVAL BEYOND LIMITS LONGERON 31R F/S 8-70. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21 AND DWG 5613861.

Part: FITTING — CRACKED (BS 70)

INSPECTION TYPE:C, INBD LONGERON TO BULKHEAD FITTING IS CRACKED F/S 70 L-31R. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: DOUBLER — CORRODED (BS 35-55)

INSPECTION TYPE:D, F/S 35-55 A/C DOUBLER HAS HEAVY CORROSION UNDER NUTPLATES UNDER O/B FLANGE OF LONGERON 30R. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW SRM 51-1-20D AND DWG 5649028.

Part: DOUBLER — CRACKED (BS 8-70)

INSPECTION TYPE-C, FINGER DOUBLER IS SPLIT IN HALF FROM STA 8 TO STA 70 AT STR 31R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER IAW DWG 5644931 AND SRM 53-3-3 FIG 1.

Part: SKIN — CORRODED (BS 850)

INSPECTION TYPE-C, THE FUSELAGE SKIN AT STA 850 AND STR 24L JUST ABOVE THE WING HAS HEAVY CORROSION. REPAIRED AREA IAW 8110-3 APPROVED DHC SK803-975.

Part: ANGLE — CRACKED (BS 310-330)

INSPECTION TYPE-C, WEB SUPPORT ANGLE IS CRACKED IN 2 PLCS AT STA 310 AND 330 STR 26L. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLES IAW DWG 9751879 AND SRM 51-1-21.

Part: ANGLE — CRACKED (WS 252)

INSPECTION TYPE:D, RIB SUPPORT ANGLE CRACKED AT RT STUB WING XFS 252.00. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20 D AND 9753294.

Part: FITTING — CORRODED (BS 1600)

INSPECTION TYPE:D, RT AFT SERVICE DOOR F/S 1600 AT CUSP AREA THE FRAME TO CUSP ATTACH ANGLE IS HEAVILY CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 858)

INSPECTION TYPE-C, RT WING L/E O/B SECTION AT STA XFS858.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.

Part: FITTING — CORRODED (BS 560)

INSPECTION TYPE-C, MAIN CABIN AT STA 560 AND STR 21R, THE FRAME TO CUSP TIE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND DWG 3753488.

Part: FITTING — CRACKED (BS 1160)

INSPECTION TYPE-C, STA 1160 JUST ABOVE STR 33R, THE SHEAR TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3755847 AND SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (BS 300)

INSPECTION TYPE-D, SHEAR TIE FITTING AT FS 300 BETWEEN L36 AND L-35L IS CRACKED AND CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 53-2- 0.

Part: SKIN — CORRODED (WS 227.333)

INSPECTION TYPE:C LT WING L/E SKIN AS STA XS 227.333 ON TOP HAS HEAVY CORROSION AROUND FASTENER HOLE. REPAIRED AREA IAW SRM 57-3-3 AND ADD 5720-7767.

Part: FITTING — CORRODED (BS 1540)

INSPECTION TYPE-C, STA 1540 AT STR 21L, THE FLOOR TO CUSP TIE FITTING IS CORRODED BEYOND LIMITS. REMOVE AND REPLACED FITTING IAW DWG 4640162 AND SRM 53-2-0 FIG 20.

Part: FITTING — CRACKED (BS 759)

INSPECTION TYPE-C, MAIN CABIN AT STA 759 LBL 47, ON TOP OF CENTER WING BOX, TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3641125 AND SRM 51-1-21.

Part: CLIP — CRACKED (BS 1540)

INSPECTION TYPE-C, INTERCOSTAL TIE CLIP IS CRACKED AT STA 1540 AND STR 10. REMOVED FABRICATED AND INSTALLED REPLACEMENT CLIP IAW SRM 51-1-21 AND DWG 5779936.

Part: INTERCOSTAL — CRACKED (BS 1480-1500)

INSPECTION TYPE-C, MAIN CABIN AT STA 1480 TO 1500 AT STR 2R, THE INTERCOSTAL AND ATTACH CLIP BOTH ARE CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL AND ATTACH CLIP IAW DWG 5704408 AND SRM 53-4-1 FIG 49.

Part: FLOORBEAM — CORRODED (BS 880)

INSPECTION TYPE:D, F/S 880 FLOORBEAM NUT PLATE HOLES CORRODED RBL 5 TO RBL 35. REPAIRED IAW DHC SK-803-780.

Part: FLOORBEAM — CORRODED (BS 717)

INSPECTION TYPE:D, F/S 717 FLOORBEAM RT SIDE RBL 35 UPPER CAP CORROSION REMOVAL BEYOND LIMITS. REPAIRED IAW DHC SK-803-786.

Part: WEB — CORRODED (BS 80)

INSPECTION TYPE-C, LT NOSE W/W TUNNEL PRESSURE WEB AT STA -80 AND LBL 36 TO 48 IS CORR. REPAIRED AREA IAW SRM 53-3-3 FIG 6 AND 52-2-0 FIG 23.

Part: DOUBLER — CORRODED (BS 59)

INSPECTION TYPE:D LT NOSE W/W TUNNEL HAS CORROSION OUT OF LIMITS ON SUB FRAME ATTACH DOUBLER F/S -59 L 22L-23L. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1- 20D AND 53-3-0.

Part: DOUBLER — CORRODED (BS 10-30)

INSPECTION TYPE-C, COCKPIT SUB FLOOR AT STA -30 TO -10 LBL 16 TO 24, THE FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5612298-77 AND SRM 51-1-20D.

Part: ANGLE — CRACKED (WS 240.126)

INSPECTION TYPE:D RT I/B STUB WING ATTACH ANGLE XS 240.126 LWR O/B END HAS CRACK IN RADIUS. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-21 AND DWG 5739859.

Part: RIB — CRACKED (WS 497.491)

INSPECTION TYPE:C LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA XFS 497.491. STOP DRILLED CRACK AND REPAIRED IAW SRR57-2-0 FIG 2.

Part: RIB — CRACKED (WS 610)

INSPECTION TYPE-C, RT WING L/E O/B OF NR 4 ENG, XFS610.00, THE L/E RIB IS CRACKED FWD LWR FLANGE. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (BS 1600)

INSPECTION TYPE-D, SKIN CRACKED AND CORRODED AT SHEAR TIE UNDER FRAME FS 1600 BTWN LONG 25R AND 24R AFT ACCY COMPT. REPAIRED IAW DHC SK-803-679.

Part: TIE CLIP — CRACKED (BS 1725)

INSPECTION TYPE:C STA 1725, BETWEEN STR 32R-33R, INTERCOSTAL FRAME TIE CLIP IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT CLIP IAW DWG 5649329 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 672.5)

INSPECTION TYPE:C RT WING L/E O/B NR 4 ENG RIB IS CRACKED AT STA XFS.672.500. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE-D, RT WING I/B STUB WING I/B RIB FWD LWR CORNER HAS CRACK IN RADIUS. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FRAME — CRACKED (BS 1180)

INSPECTION TYPE-C, STA 1180 FRAME AT STR 9R HAS A SMALL CRACK. REPAIRED AREA IAW DWG 9754919 AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (LT WING)

INSPECTION TYPE:D, LT WING IB STUB WING INNER DOUBLER AROUND SLOT PANEL CRACKED BTWN RIBS JUST OB OF SLOT PANEL. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND DWG 5769895. REMOVED AND REPLACED FITTING P/N 4640162- 502 IAW SRM 51-1-21.

Part: PRESURE WEB — CORRODED (BS 12)

INSPECTION TYPE:D RT NOSE W/W TUNNEL PRESSURE WEB HAS HEAVY CORROSION AT F/S -12 UNDER STIFFENER RBL 35-46. REPAIRED IAW DHC SK-803-617.

Part: RIB — CRACKED (BS 347.75)

INSPECTION TYPE:C LT WING L/E RIB UPPER ARM IS CRACKED BY THE AFT FASTENER AT STA XFS 347.750. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: PRESURE WEB — CORRODED (BS 52-67)

INSPECTION TYPE:D, RT NOSE W/W TUNNEL PRESSURE WEB HAS HEAVY CORROSION FROM F/S -52 TO -67. REPAIRED IAW DHC SK 803-610.

Part: SPLICE — CORRODED (BS 1580-1600)

INSPECTION TYPE:C, SEAT TRACK SPLICE CORRODED BEYOND LIMITS F/S 1580-1600 RBL 48 AFT ACCY COMP. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT SPLICE IAW SRM 51-3-0 AND DWG 3889621.

Part: DOUBLER — CRACKED (WS 230.089)

INSPECTION TYPE-C, RT I/B STUB WING DOUBLER AT STA XS230.089 IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5769859 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 759)

INSPECTION TYPE-C, MAIN CABIN AT STA 759 AND STR 13R, FRAME TO STR TIE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 37798874 AND SRM 51-1-21.

Part: FITTING — CRACKED (BS 700)

INSPECTION TYPE:C MAIN CABIN AT STA 700, STR 18R, THE FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779978 AND SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 25-60)

INSPECTION TYPE-C, STA 25 TO 60 RBL36 TO 48, THE DOUBLER UNDER THE LAV FLOOR IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-2-0.

Part: FITTING — CRACKED (BS 700)

INSPECTION TYPE:C MAIN CABIN AT STA 700, STR 13L, THE FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779978 AND SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 10-30)

INSPECTION TYPE-C, COCKPIT SUB FLOOR AT STA -30 TO -10, RBL 24 TO 29, THE FINGER DOUBLER HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5612298 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 781)

INSPECTION TYPE-C, MAIN CABIN AT STA 781 STR 18L, THE FRAME TO STR TIE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21 AND DWG 3779978.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE-C, STA 1140 AT STR 22R, SHEAR TIE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 4750419 AND SRM 51-1-21.

Part: INTERCOSTAL — CRACKED (BS 80)

INSPECTION TYPE-C, COCKPIT SUB FLOOR AT STA -80, LBL 59, THE VERTICAL INTERCOSTAL IS CRACKED AT THE LWR END. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW DWG 5613785 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1220)

INSPECTION TYPE-C, STA 1220 AT STR 33R, THE FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND DWG 3755847.

Part: FITTING — CRACKED (BS 1220)

INSPECTION TYPE-C, STA 1220 AT STR 27L, THE DOOR OPEN STOP FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 3755854-1.

Part: SHEAR TIE — CORROSION (BS 320)

INSPECTION TYPE-D, SHEAR TIE FITTING FS 320 BETWEEN STR 30L TO 29L HAS CORROSION. REMOVED AND REPLACED FITTING IAW SRM 52-2-0.

Part: FITTING — CRACKED (BS 1520)

INSPECTION TYPE-C, STA 1520 ON PIT CEILING AT BL 0, THE SEAT TRACK SUPPORT-T FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 4772359 AND SRM 51-1-21.

Part: SUPPORT — CORRODED (BS 100)

INSPECTION TYPE-D, FLOORBEAM SUPPORT FITTING FS 100 L-27R LWR I/B FLANGE HAS HEAVY EXFOLIATION CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 3773077.

Part: FITTING — CRACKED (BS 1480)

INSPECTION TYPE:D, F/S 1480 ABOVE STR 27L - FLOORBEAM SUPPORT FITTING HAS HEAVY CORROSION/CRACKING ON BOTTOM. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D.

Part: LONGERON — DAMAGED (BS 1500-1520)

INSPECTION TYPE-C, STA 1500 TO 1520, STR 29L TOP FLANGE IS PART MISSING. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW DWG 5615377 AND SRM 51-1-21.

Part: FITTING — CORRODED (BS 1300)

INSPECTION TYPE-C, STA 1300 AT STR 27R, THE FLOORBEAM SUPPORT FITTING HAS HEAVY CORROSION, CRACKING. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 3773077 AND SRM 51-1-21.

Part: FITTING — CRACKED (BS 700)

INSPECTION TYPE-C, MAIN CABIN AT STA 700, STR 13R, FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND DWG 3779978.

Part: FRAME — CRACKED (LT COCKPIT)

INSPECTION TYPE-C, FRAME CRACKED IN RADIUS, JUST FWD OF CAPT'S WINDSHIELD. INSIDE RAIN REMOVAL PLENUM ACCESS PLATE #94L, UPPER INBD CORNER. REPAIRED IAW SRM 53-2-0 FIG 1B.

Part: FITTING — CORRODED (BS 902)

INSPECTION TYPE-C, MAIN CABIN AT STA 902 AND LONG 6L, THE LONG END FITTING IS CRACKED AND HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW DWG 3779659 AND SRM 51-1-21.

Part: SKIN — CORRODED (LT HORIZ STAB)

INSPECTION TYPE-D, LT HORZ STAB INBD L/E HAS FILLIFORM CORROSION OUTBD END L/E XFS 197.5. REPAIRED IAW SRM 55-2-1.

Part: FITTING — CRACKED (BS 680-700)

INSPECTION TYPE-C, MAIN CABIN STA 680 TO 700 AT STR 1, THE SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21 AND DWG 4750521.

Part: RIB — CRACKED (WS 622.5)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER XFS 622.500. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CORRODED (WS 193)

INSPECTION TYPE:C, RT WING L/E AUX TANK UPPER AFT SKIN ON O/B END IS PULLING THROUGH (INTERNAL CORROSION) XFS 193.00. REPAIRED IAW DHC SK 803-363.

Part: SKIN — CORRODED (WS 1.25-7.50)

INSPECTION TYPE-C, RT WING L/E AUX TANK I/B END ON TOP SKIN HAS HEAVY CORROSION UNDER THE SURFACE. REPAIRED THE AREA IAW SRM 57-2-1 FIG 37.

Part: SKIN — CORRODED (BS 282.5)

INSPECTION TYPE:C RT WING L/E SKIN ON TOP AT STA XFS 282.500 HAS HEAVY CORROSION UNDER THE SURFACE. REPAIRED AREA IAW SRM 57-3-0.

Part: RIB — CRACKED (WS 735.00)

INSPECTION TYPE-C, RT WING L/E AT STA XFS.735.00, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CORRODED (WS 250.089)

INSPECTION TYPE:C LT WING LWR SURFACE OF I/B STUB WING HAS HEAVY CORROSION AROUND FASTENER XS 250.089. REPAIRED AREA IAW SRM 57-2-1.

Part: FITTING — CRACKED (LT WING)

INSPECTION TYPE:D, LT WING T/E THE LWR REAR SPAR TO AUX SPAR TIE FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW DHC SK- 803-491 WITH REF TO UPS EO DC8-5720-10228-E.

Part: SKIN — CORRODED (WS 772.5)

INSPECTION TYPE-C, RT WING L/E SKIN ON TOP AT STA XFS 772.500 HAS HEAVY CORROSION UNDER THE SURFACE AT 2 SCREWS. REMOVED DAMAGE AND REPAIRED IAW SRM 57-2-1 FIG 38.

Part: SKIN — CORRODED (WS 20-45)

INSPECTION TYPE-C, LT WING L/E UPPER SURFACE HAS HEAVY CORROSION AROUND FASTENERS AT FRONT SPAR BTWN STA XFS20 TO XFS45. REPAIRED AREA IAW SRM 57-2-1 FIG 37.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE-D, LT WING L/E UPPER SURFACE CRACKED AT FASTENER HOLE BTWN REPAIR DOUBLERS ON SECTION JUST O/B OF NR 1 ENG. SUSPECT HEAVY CORROSION UNDER SKIN. CUT OUT CORRODED AND DAMAGED AREA AND REPAIRED IAW DHC SK-803-156. WITH REF TO UPS EO DC8-5720-10402-A.

Part: SKIN — CRACKED (BS 160)

INSPECTION TYPE-D, RT SIDE FWD SERVICE DOOR UPPER FWD CORNER CRACKED. REPAIRED IAW SRM 53-2-0.

Part: SKIN — CORRODED (WS 74)

INSPECTION TYPE-C, LT WING UPPER SURFACE IS CRACKED AT STA XRS 74 JUST FWD OF STR 9. REPAIRED AREA IAW SRM 57-2-1 FIG 10.

Part: SKIN — CORRODED (WS 126.5-107.5)

INSPECTION TYPE-C, LT WING L/E UPPER SURFACE HAS HEAVY CORROSION AROUND FASTENERS AT FRONT SPAR BTWN STA'S XFS126.250 TO XFS107.500. REPAIRED AREA IAW SRKM 57-2-1 FIG 37.

Part: FLOORBEAM — CORRODED (BS 1520)

INSPECTION TYPE-D, FS 1520 FLOORBEAM FWD SIDE HAS HEAVY CORROSION ON TANG LBL 59. REPAIRED IAW DHC SK-803-070.

Part: BULKHEAD FITTING — CRACKED (BS 1818)

INSPECTION TYPE:D, F/S 1818 CANTED BULKHEAD FITTING AT LONGERON 1R CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21 AND DWG 5612149.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE-C, LT WING LOWER SURFACE SKIN HAS A .5 INCH CRACK APPROX 15.5 I/B OF NR 1 PYLON 4.5 AFT OF FWD SPAR. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW DC8 SERVICE BULLETIN DC8-57-100.

Part: FITTING — CORRODED (BS 1180)

INSPECTION TYPE-C, FS 1180 BTWN S 34R TO 35R BACKUP FITTING HAS CORROSION BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 53-2-0.

Part: FLOORBEAM — CORRODED (BS 822)

INSPECTION TYPE-C, FLOORBEAM AT FS 822 RBL 32 CORRODED OUT OF LIMITS UPPER FLANGE. REPAIRED IAW DHC SK 803-466.

Part: FITTING — CORRODED (BS 1220-1230)

INSPECTION TYPE-C, FITTING BTWN FS 1220 AND 1230 AT LONG 31R HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-21, 51-3-0.

Part: SHEAR TIE — CORRODED (BS 1240)

INSPECTION TYPE-C, SHEAR TIE LWR SURFACE AT F/S 1240 FROM 32L-34R HAS CORROSION. FABRICATED, AND INSTALLED REPLACEMENT SHEAR TIE FROM 34L TO 36 IAW SRM 53-2-0.

Part: INTERCOSTAL — CORRODED (BS 1240-1260)

INSPECTION TYPE-C, INTERCOSTAL BTWN F/S 1240 AND 1260 HAS HEAVY CORROSION AT LONG 33R. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 53-4-1, 51-1-20, AND 51-1-21.

Part: FITTING — CRACKED (BS 1240)

INSPECTION TYPE-C, FS 1240 AT LONGERON 35R FITTING HAS 3 CRACK. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1220)

INSPECTION TYPE-C, FS 1220 BTWN STR 32R TO 33R BACKUP FITTING HAS SEVERE CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1220)

INSPECTION TYPE-C, BACKUP FITTING HEAVY CORROSION FS 1220 BTWN S 35R AND 36. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 53-2-0.

Part: HINGE — CRACKED (RT AILERON)

INSPECTION TYPE-C, RT O/B AILERON, O/B HINGE FITTING CRACKED. REMOVED AND REPLACED AILERON IAW MM 27-11-02.

Part: SPLICE — CORRODED (BS 1270)

INSPECTION TYPE-C, STRINGER SPLICE FITTING HAS HEAVY CORROSION AT F/S 1270 STR 35L. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: INTERCOSTAL — CORROSION (BS 1260-1280)

INSPECTION TYPE-C, INTERCOSTAL BTWN F/S 1260 TO 1280 AT LONG 33R HAS CORROSION AROUND NUT PLATES. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-1-21, 53-4-1, AND 51-1-20.

Part: SHEAR TIE — CORROSION (BS 520-530)

INSPECTION TYPE-C, HEAVY CORROSION INSIDE B-PIT DOOR FRAME CUTOUT LOWER FOWARD F/S 520 TO 530 STR 32 TO 33R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE IAW SRM 51-1-21, 53-4-0, 53-2-0.

Part: SHEAR TIE — CORRODED (BS 1150-1151)

INSPECTION TYPE:C, F/S 1150-1151 BTWN LONG 33 AND 34R SHEAR TIE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 53-2-0.

Part: SPLICE — CORRODED (BS 1580-1600)

INSPECTION TYPE-C, F/S 1580 TO 1600 LBL 44 SEAT TRACK SPLICE HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SPLICE IAW SRM 53-2-3.

Part: SHEAR TIE — CORRODED (BS 1151)

INSPECTION TYPE-C, F/S 1151 BTWN LONG 34 AND 35L SHEAR TIE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SHEAR TIE IAW SRM 51-1-20D AND 51-1-11.

Part: FITTING — CORRODED (BS 1150)

INSPECTION TYPE-C, FS 1150 BTWN STR 34L TO 35L BACKUP FITTING HAS MODERATE CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20, 53-2-0.

Part: FRAME — CORRODED (BS 70)

INSPECTION TYPE-C, F/S 70 FRAME CHORD FWD LOWER FLANGE EXFOLIATED BETWEEN LONGERONS 32 AND 33R. REMOVED DAMAGED SECTION OF CHORD AND INSTALLED REPLACEMENT SECTION IAW SRM 53-2-5 FIG 8C, 51-1-20, AND 51-1-21.

Part: FITTING — CRACKED (BS 717)

INSPECTION TYPE-C, WING BOX FRAME TO SEAT TRACK FITTING CRACKED FS 717 RBL 24. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 923)

INSPECTION TYPE-C, WING BOX VERT FITTING CRACKED F/S 923 LBL 68. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO DOOR)

INSPECTION TYPE-C, NR 1 PIT CARGO DOOR FRAME, ADJACENT TO AFT OPEN STOP FITTING (INSIDE DOOR) IS CRACKED. REPAIRED IAW DHC SK-803-40.

Part: DOUBLER — CORRODED (BS 857-879)

INSPECTION TYPE-C, CENTER WING BOX FINGER DOUBLER BETWEEN F/S 857 TO 879 BL 0 HAS 2 POPPED RIVETS AND CORROSION UNDER DOUBLER. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 51-1-20D.

Part: DOUBLER — CORRODED (BS 920-940)

INSPECTION TYPE-C, CENTER WING BOX FINGER DOUBLER BETWEEN F/S 920 TO 940 HAS SEVERAL POPPED RIVETS AND HEAVY CORROSION UNDER DOUBLER BL 0. REPAIRED IAW DHC SK-803-433.

Part: DOUBLER — CORRODED (BS 879-902)

INSPECTION TYPE-C, CENTER WING BOX FINGER DOUBLER BETWEEN F/S 879 TO 902 HAS NUMEROUS POPPED RIVETS AND CORROSION UNDER DOUBLER. REPAIRED IAW DHC SK-803-433.

Part: SPLICE — CRACKED (BS 440-460)

INSPECTION TYPE-C, F/S 440 TO 460 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (BS 70)

INSPECTION TYPE-C, F/S 70 BULKHEAD IN NR 1 PIT LT UPPER HORZ INTERCOSTAL IS CRACKED AND CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-1-21 AND DWG 5613064.

Part: FITTNG — CRACKED (BS 340)

INSPECTION TYPE-C, F/S 340 ABOVE STR 27R FLOORBEAM SUPPORT FITTING IS CRACKED BTWN LWR ATTACH FASTENERS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1060)

INSPECTION TYPE-C, F/S 1060 RT SIDE CUSP TO FRAME FITTING CORRODDED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 4640162.

Part: SPLICE — CRACKED (BS 380-400)

INSPECTION TYPE-C, FS 380 TO 400 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 798)

INSPECTION TYPE-C, FLOORBEAM TO SEAT TRACK FITTING IS CRACKED F/S 798 LBL 24. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: ANGLE — CRACKED (WS 6.225)

INSPECTION TYPE-C, L/WING L/E UPPER ANGLE CLIP AT STA XOLD 6.225 CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 57-3-0, DWG 5769948.

Part: FITTING — CORRODED (BS 1159)

INSPECTION TYPE-C, F/S 1159 ABOVE STR 35R HOLD DOWN FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: FITTING — CRACKED (BS 1360)

INSPECTION TYPE-C, F/S 1360 AT RT CUSP LWR SURFACE CUSP TO FLOORBEAM TIE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21D, 51-3-0, AND DWG 3773479.

Part: DOUBLER — CRACKED (BS 1536)

INSPECTION TYPE-C, F/S 1536 AT STR 31L FINGER DOUBLER IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 51-1-20D AND DWG 5615374.

Part: SPLICE — CORROSION (BS 1042)

INSPECTION TYPE-C, F/S 1042 STR 35L SPLICE FITTING HAS HEAVY CORROSION AROUND FASTENERS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (BS 1141)

INSPECTION TYPE-C, FS 1141 ABOVE STR 35R INTERCOSTAL TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SPLICE — CORRODED (BS 1040-1060)

INSPECTION TYPE:C, F/S 1040-1060 STR 35R SPLICE FITTING HAS HEAVY CORROSION AT EACH END. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 597.5)

INSPECTION TYPE-C, L/WING UPPER L/E RIB CRACKED AT STA 597.500. REPAIRED IAW SRM 57-2-0, 57-3-3, AND 51-1-20D.

Part: FRAME — CRACKED (BS 660)

INSPECTION TYPE-C, F/S 660 BELOW STR 21R FRAME FORMER IS CRACKED IN THE RADIUS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D AND DWG 3646688.

Part: RIB — CRACKED (WS 748)

INSPECTION TYPE-C, RT WING L/E STA XFS 748.00 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0, 51-1-20D, 51-1-21.

Part: RIB — CRACKED (WS 603)

INSPECTION TYPE-C, L/WING LWR L/E RIB CRACKED AT STA 603.750. REPAIRED IAW SRM 57-2-0, 57-3-3, AND 51-1-20D.

Part: RIB — CRACKED (WS 703.75)

INSPECTION TYPE-C, L/WING L/E UPPER RIB CRACKED AT STA 703.750. REPAIRED IAW SRM 57-2-0, 57-3-3, AND 51-1-20D.

Part: RIB — CRACKED (WS 787.5)

INSPECTION TYPE-C, L/WING L/E UPPER RIB CRACKED AT STA 787.500. REPAIRED IAW SRM 57-2-0, 57-3-3, AND 51-1-20.

Part: RIB — CRACKED (WS 803.750)

INSPECTION TYPE-C, L/WING L/E UPPER RIB CRACKED AT STA 803.750. FABRICATED AND INSTALLED REPAIR IAW SRM 57-3-3, 57-2-0, 51-1-20D.

Part: RIB — CRACKED (WS 828.75)

INSPECTION TYPE-C, L/WING UPPER L/E RIB CRACKED AT STA 828.750. REPAIRED IAW SRM 57-2-0, 51-1-21 AND 51-1-29D.

Part: SKIN — CRACKED (RT TE FLAP SLOT)

INSPECTION TYPE-C, RT O/B SLOT VANE I/B L/E SKIN HAS HEAVY CORROSION UNDER SURFACE AND 3 CRACKS. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE-C, RT WING L/E SECTION BTWN PYLONS AT I/B END HAS 3 CRACKS AROUND FASTENERS (LWR L/E SKIN). REPAIRED IAW SRM 57-2-0, 51-1-21, AND ADDN DC8-5720-4087-B.

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE-C, RT WING L/E O/B SECTION AT O/B END SKIN HAS SEVERAL CRACKS AROUND FASTENERS. REPAIRED IAW SRM ADDN DC8-5720-4087 AND SRM 57-2-0.

Part: SKIN — CORRODED (BS 1160)

INSPECTION TYPE-C, BELLY SKIN CORROSION F/S 1160 STR 36. REMOVED AND REPLACED SKIN AND INTERNAL DOUBLER IAW SRM 51-1-21 AND DWG 5750322 INTERNAL DOUBLER (P/N 9754924-1N).

Part: STIFFENER — CRACKED (BS 1160)

INSPECTION TYPE-C, FS 1160 ON CEILING RT SIDE AT C-3 PIT DOOR OPENING FLOORBEAM VERT STIFFENER IS CRACKED ON EDGE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT STIFFENER IAW SRM 53-2-0, 51-1-20D, AND DWG 9754002.

Part: SPLICE CAP — CRACKED (WS 408.343)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING STA 408.343 HAS 4.5 INCH CRACK JUST ABOVE RADIUS BETWEEN STR 51 AND 52. REPAIRED XW 408.343 LWR SPLICE CAP ON RT WING THAT HAD 2 CRACKS IN VERT LEG BETWEEN STR 51 AND 52 IAW UPS EO DC8-5710-8090A.

Part: SUPPORT — CRACKED (BS 1900)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED STA 1900 NR 4 HORIZONTAL SUPPORT RT AND LT SIDE ATTACH CRACKED, SEEN FROM AFT SIDE. FAB REPAIR DOUBLERS AND INSTALLED IA W DC-8 SRM 51-9-0 AND 53-2-0.

Part: SKIN — LEAKING (LT REARSPAR)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED REAR SPAR LEAKING ALONG LT SIDE 57 TO 88, BETWEEN REAR SPAR CAP AND WING SKIN. REPAIRED BUSHINGS, LT WING SKI FITTING.

Part: SKIN — CRACKED (RT WING)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING T/E PNL CRACKED AND LIFTING FWD OF NR 1 SPOILER I/B HINGE. REPAIRED T/E PNL AT HINGE FITTING CUTOUT IAW UPS EO DC8-57-0654.

Part: SPAR — CRACKED (RT WING)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT WING LWR SPAR HOLE NR 6 FOUND CRACKED WHILE PERFORMING EO DC8-5710-7761-A. FAB REPAIR DOUBLER, FILLER AND BUSHINGS AND INSTALLED IAW DAC DWG J060232 AND EO DC8-5710-7761A.

Part: SKIN — CRACKED (LT AILERON)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT WING BOTTOM I/B AILERON, SKIN AT MIDDLE FWD GOUGED CRACKED AND DENTED. STOP DRILLED CRACKS, FAB REPAIR DOUBLERS AND INSTALLED IAW DC8-SRM 57-2-1 AND 57-8-0.

Part: FLOOR BEAM — CORRODED (BS 1540)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED AFT ACCESSORY COMP FLOOR BEAM STA 1540 LT SIDE CORRODED AT TOP. REPAIRED FUSELAGE STA 1540 FLOOR BEAM THAT WAS CORRODED BEYOND 50 PERCENT IAW UPS EO DC8-53-1605.

Part: RIB — CRACKED (NR 2 PYLON)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT STUB WING AT NR 2 PYLON RIB CRACKED ON UPPER SIDE APPROX AT STA XRS 440. STOP DRILLED CRACK, FAB REPAIR DOUBLERS AND INSTALLED IAW DC8-SRM 57-2-0 AND 57-3-0.

Part: FITTING — BROKEN (NR 2 PYLON)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED EO DC8-5710-40-80-E, WING FRONT SPAR PYLON SUPPORT FITTING REPLACEMENT OF NR 2 PYLON. REPAIRED NR 2 PYLON FOOTSTOOL, T-DOUBLER, SKATE ANGLE IAW UPS EO DC8-57-0660.

Part: GROMMET — BROKEN (NR 2 PYLON)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 2 PYLON WIRING SUPPORT GROMMETS ARE BROKEN, 2 EACH. REMOVED AND REPLACED IAW DC8 MM 20-11-0 AND UPS EO DC8- 71-0036.

Part: RIB — CRACKED (RT WING LE)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT CENTER L/E RIB CRACKED AT APPROX STA XFS 353 UPPER SIDE. STOP DRILLED CRACKS, FAB REPAIR ANGLES AND INSTALLED IAW DC8-SRM 57-3-0 AND 57-2-0.

Part: DRAIN LINE — DENTED (NR 1 ENGINE)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED DRAIN LINE FOR NR 1 ENGINE OIL FUEL HEAT EXCHANGER DENTED. REMOVED LINE, FAB AND PRESSURE TESTED LINE IAW DPS 3.805, FOUND NO LEAKAGE. INSTALLED SERVICEABLE LINE IAW DC8-MM 75-20-02.

Part: SLIDE — DAMAGED (EMER ESCAPE)

WHILE ON THE GROUND, MAINTENANCE FOUND THE EMERGENCY ESCAPE SLIDE PRESSURE INDICATION WITH OPEN COVER. REPOSITIONED INDICATOR, SLIDE INFLATED, NEEDS REPLACED. MAINTENANCE REPLACED THE EMERGENCY ESCAPE SLIDE PER MM 25-60-01.

Part: EEL BULB — FAILED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY LIGHT WILL NOT DISARM PROPERLY. REPLACED EMERGENCY LIGHT DISARM BULB. OPS CHECK SYSTEM NORMAL IAW M/M 33-50-00.

Part: EEL SOCKET — INOPERATIVE (CABIN)

UPON ARRIVAL, CREW REPORTS EMERGENCY LIGHT SOCKET SPRING CONTACT STUCK IN DEPRESSED POSITION. REPAIRED SPRING CONTACT.

Part: FITTING — CRACKED (NR 3 PYLON)

WHILE ON GROUND IN SDF, MAINTENANCE FOUND NR 3 PYLON FRONT SPAR SUPPORT FITTING CRACKED. MAINTENANCE REMOVED FOOTSTOOL FITTING AND INSTALLED NEW FOOTSTOOL IAW EO DC8-5710-4080D.

Part: EEL — INOP (FLIGHT DECK)

ON PREFLIGHT CHECK, FLIGHT CREW FOUND EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED LIGHT ASSY. OPS CHECK OK.

Part: LONGERON — CRACKED (FS 1270-1275)

DURING 'SPECIAL VISIT', MAINTENANCE REPORTED LONGERON 36 CRACKED FROM STA 1270-1275. FABRICATED AND INSTALLED REPAIR PER SRM 53-2-2.

Part: WEB — CRACKED (PRESS BULKHEAD)

DURING 'B' CHECK, MAINTENANCE FOUND 3.5 INCH CRACK IN LOWER LEG OF J3 WEB OF AIRPLANE AFT PRESSURE BULKHEAD COMPARTMENT 60. STOP DRILLED CRACK, FABRICATED DOUBLER AND INSTALLED REPAIR.

Part: SKIN — CORRODED (FS 1220-1240)

DURING 'B' CHECK, MAINTENANCE FOUND FUSELAGE SKIN BULGED AND PULLING RIVET 6 O'CLOCK POSITION BETWEEN 1ST AND 2ND CIRCUMFERENTIAL AFT OF NR 3 PIT DOOR STATION 1220-1240. FABRICATED AND INSTALLED REPAIR IAW EO DC8-5330-6670A.

Part: BULB SOCKETS — FAILED (RT MLG)

PILOT REPORTED ON APPROACH AFTER LOWERING L/G, DID NOT GET ANY LIGHTS. RESET L/G AND WARNING INTERLOCK C/B AFTER IT POPPED. LOWERED GEAR AGAIN, GOT 3 GREEN SAFE INDICATORS. REPAIRED UPPER BULB SOCKET OF RIGHT L/G LIGHT ASSY. OPS CHECK SYSTEM NORMAL IAW 32-60-00.