N798UP

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

INSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY PACK DRAINED. EMERGENCY LIGHT BATTERY PACK REPLACED AND TESTED IAW DC8 AMM 33-50-01-2-4. FUNCTION TESTED SERVICEABLE.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS (2 EACH) OVER MAIN ENTRY DOOR INOP. RELAMPED (2 EACH) EMERGENCY EXIT BULBS REF MM 33-50-00. OPS CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A 2 EACH EMERGENCY LIGHT ABOVE ENTRY DOOR INOP. RELAMPED EMERGENCY LIGHTS, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. EMERGENCY EXIT BATTERY PACK REPLACED AND TESTED IAW AMM 30-50-01-2. OPS CHECK GOOD.

Part: SKIN — CORRODED (LT WING) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 LEFT WING UPPER SKIN AT XRS650 TO XRS659 OVER STR 7 REQUIRES REPAIR. REPAIR WING UPPER SKIN IAW SAA EA3 008-5730-01-A0655 AND UPS EO DC8-57 30-26300-A.

Part: SKIN — CORRODED (XRS 589 STR 1) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 LEFT UPPER WING SKIN AT XRS 589 BETWEEN STR 1 TO REAR SPAR REQUIRES REPAIR. REPAIRED WING UPPER SKIN IAW SAA EA 008-5730-01-A0656 AND UPS EO DC8-5730-26300-A.

Part: SKIN — CORRODED (LT WING) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 LEFT UPPER WING SKIN AT CANT 495 TO XRS 554 BETWEEN STR 5 AND 8 REQUIRES REPAIR. REPAIRED UPPER WING SKIN IAW SAA EA 008-5730-01-A0658 AND UPS EO DC8-5730-26300-A.

Part: SKIN — CORRODED (LT WING) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 LEFT WING UPPER SKIN AT CANT 495 TO XW408 OVER CENTER SPAR REQUIRES REPAIR. REPAIRED WING UPPER SKIN IAW SAA EA 008-5730-01-A0659 AND UPS EO DC8-5730-26300-A.

Part: SKIN — CORRODED (LT WING) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 LEFT WING UPPER SKIN AT XW 408 TP CANT 508 BETWEEN STR 6 AND REAR SPAR REQUIRES REPAIR. REPAIR WING UPPER SKIN IAW SAA EA 008-5730-01-A0660 AND UPS EO DC8-5 730-26300-A.

Part: INTERCOSTAL — CRACKED (BS 1781 L19R) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 - UPON REMOVAL OF LONGERON END FITTING FOUND ATTACHED BRACKET CRACKED AT 1781-L19R. REMOVED, FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-3-2, 51-1-21 AND DWG 5773844.

Part: SKIN — CRACKED (LT WING) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 LT STUB WING L/E ABOVE NR 2 HAS A CRACK ON UPPER O/B SIDE. REMOVED DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SAA EA 008-5710-01-A0615.

Part: SKIN — CRACKED (LWS 195) · airframe 68,243 hrs · 26,450 cycles

WHILE GETTING OK TO INSTALL LT AUX TANK. FOUND CRACK ON LT STUB WING LE UPPER IB SIDE. REPAIRED LT LE IB SLOT SUPPORT STRUCTURE SKIN STA XFS-195 IAW RAA DC8-57-20205 A.

Part: FITTING — CRACKED (WING) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 NR 2 MAIN FUEL TANK HAS STRINGER END FITTING CRACKED AT STRINGER 55 JUST INBOARD XRS74. REMOVED AND REPLACED STRINGER END FITTING IAW SRM 51-1-20D, 51-3-0 AND 51-01-15.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 STA 1700 LBL 26 UNDERSIDE OF FLOORBEAM HAS CORROSION. REMOVED CORROSION, FABRICATED AND INSTALLED STRAP AND 2 EA REPAIR ANGLES IAW SRM 51-1-21 AND 53-2-0.

Part: BULKHEAD — CRACKED (FS 1766 L2R-L3R) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 - FOUND AFT PRESSURE BULKHEAD STA 1766 HAS CRACK BTWN L2R & L3R. STOP DRILLED 2 ENDS OF CRACK, FABRICATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 53-2-0 FIG 24, 51-1-20D.

Part: LONGERON — CORRODED (FS1350-1490 L34L) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 L34L BETWEEN 1420-1440 HAS CORROSION UNDER REPAIR & ON LONGERON. REMOVED, FABRICATED AND INSTALLED LONGERON IAW SRM 53-02-02 FIG 4A, 51-1-20D, 51-1-21 AND DWG 4613495.

Part: LONGERON — CRACKED (FS1400-1440 L35R) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 LONGERON 35R CRACKED ALONG RADIUS AT FS 1400-1440. REMOVED, FABRICATED AND INSTALLED LONGERON IAW SRM 51-1-20D, 51-1-21 & DWG 3646937.

Part: LONGERON — CRACKED (FS1400-1410 L35L) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 LONGERON 35L CRACKED ALONG RADIUS AT FS 1400-1410. REMOVED, FABRICATED AND INSTALLED LONGERON IAW SRM 53-2-2 FIG 4A, 51-1-21, 51-1-20D.

Part: STIFFENER — CRACKED (BS 1916) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 - FOUND EMPENNAGE TAIL SECTION AT STA 1916 INSIDE 62 ACCESS HAT CHANNEL CROSS MEMBER STIFFENER HAS CRACK AT END RT SIDE. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 53-02-00 FIG 001B, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 TWO CRACKS IN END OF RIB AT INBOARD END F/O RIGHT OUTBOARD LEADING EDGE. STOP DRILLED CRACKS, FABRICATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 57-02-00-0 FIG 002, 51-1-21 AND 51-1-20D.

Part: FITTING — GOUGED (FS 1766 L11R) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 AFT FUSELAGE INSIDE 60 ACCESS AT STA 1766 L11R, LONGERON END FITTING HAS SEVERAL DEEP GOUGES. REMOVED, FABRICATED AND INSTALLED END FITTING IAW SRM 53-02-00 FIG 001F, 51-1-20D AND DWG 7531590.

Part: STIFFENER — CRACKED (FS 1944) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 - FOUND EMPENNAGE TAIL SECTION AT STA 1944 RT SIDE, HAT CHANNEL CROSS MEMBER STIFFENER HAS CRACK AT END. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SRM 51-1-21, 53-02-00.

Part: RIB — CRACKED (RT WING) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 CRACKED RIB BEHIND INTERCOSTAL IN RT OB L/E AT XFS 650 PANEL 519B. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-02-00 FIG 002 , 57-03-01 FIG 1, AND 51-1-21.

Part: SKIN — CRACKED (RT WING) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 LARGE DENT ON NOSE OF RT CTR L/E. CRACKED SKIN, BROKEN RIVETS XFS 392. CUT OUT DAMAGE, FABRICATED FILLER AND DOUBLER. INSTALLED CONICAL WASHERS, FILLER AND DOUBLER IAW SRM 57-02-01-0 FIG 0024, 51-1-21 AND 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 FITTING HEAVY CORROSION AT STA 940 L21R. REMOVED, FABRICATED AND INSTALLED FITTING IAW SAA EA 008-5320-01- A0594, UPS RAA DC8-53-20607, SRM 51-11-8 AND 51-1-20D.

Part: SKIN — WORN (L/E SLOT) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 INNER SKIN WORN/CHAFED AT OUTBOARD END OF RIGHT OUTBOARD SLOT VANE. FABRICATED AND INSTALLED INNER DOUBLER IAW SRM 57-3-1 FIG 9.

Part: RIB — CRACKED (RT WING) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 RIB CRACKED UNDER GUSSET IN RT CTR LE NEXT TO PANEL 523. STOP DRILLED CRACK. FABRICATED 2. REPAIR ANGLES AND INSTALLED IAW SRM 57-03-01, 57-02-00 FIG 002, 51-1-20 AND 51-1-21D.

Part: RIB — CRACKED (RT WING) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 CRACKED RIB IN RT CTR LE AT XFS 443. FABRICATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 57-02-00 FIG 002 51-1-20D AND 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 CRACKED RIB IN RT CTR LE AT XFS 410. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SRM 57-02-00 FIG 002, 51-1-21 AND 51-1-20D.

Part: FITTING — CORRODED (FS 960) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 - FOUND LONGERON TO FLOORBEAM FITTING HEAVY CORRODED AND CRACKED AT STA 960 L21R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: CUSP WEB — CORRODED (FS 1100-1140) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 MAIN CABIN CUSP HAS HEAVY CORROSION AT STA 1120 LT AROUND FITTING. REPAIRED LT CUSP/SKIN AT STA 1100-1140 IAW RAA DC8-53-20608.

Part: SKIN — CRACKED (LT WING) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 LEFT UPPER WING SKIN POSSIBLE CRACKED AT XCW69 AFT SPAR VERY I/B SIDE. CUT OUT DAMAGE, FABRICATED 2 EA DOUBLERS, 1 EA FILLER AND 1 EA ANGLE AND INSTALLED IAW SRM 57-02-01-0 FIG 020 AND 51-1-21.

Part: SKIN — CRACKED (BS 450-610 L31RL) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 HFEC & VISUAL INSP DETECTED A .335 INCH CRACK ON THE C-2 (B-PIT) LOWER AFT JAMB CORNER. CRACK EXTENDS FROM EDGE OF SKIN TO FASTENER HOLE AS MARKED. REMOVED AND REPLACED BELLY SKIN FROM FS 450 TO FS 610 L31R TO L31L IAW SRM 51-1-21, 51-1-20D, DWG 5779913.

Part: INTERCOSTAL — CRACKED (LT WING) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 - FOUND IB UPPER RIB OF OB SLOT DOOR STRUCTURE HAS 4" CRACK,CENTER LEADING EDGE LW ABOVE PNEUMATIC DUCT. REMOVED, STOP DRILLED CRACK, FABRICATED AND INSTALLED 1 INTERCOSTAL, AND 1 REPAIR ANGLE IAW SRM 51-1-20D, 57-03-01-0, 51-03-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD TO LONGERON INTERCOSTAL ATTACH ANGLE CRACKED AT STA 1766 L6L. REMOVED, FABRICATED AND INSTALLED ATTACH ANGLE IAW SRM 51-1-21, 51-3-2, 51-1-20D AND DWG 5773844.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 CAPTAIN`S AFT SEAT TRACK I/B WORN AND O/B HAS ELONGATED HOLES. REMOVE AND REPLACE CAPTAIN`S AFT I/B AND O/B SEAT TRACKS IAW SRM 51-1-20D, 51-03-02 AND 51-3-0.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD TO LONGERON INTERCOSTAL ATTACH ANGLE CRACKED AT STA 1766 L6R. REMOVED, FABRICATED AND INSTALLED ATTACH ANGLE IAW SRM 51-1-21, 51-3-2, 51-20D AND DWG 5773844.

Part: BULKHEAD — CRACKED (FS 1766 LBL 25) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD CRACKED AT STA 1766 LBL25. CUT OUT DAMAGE, FABRICATED AND INSTALLED 1 FILLER AND 2 DOUBLERS IAW SRM 53-2-5 FIG 14A.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 LONGERON CRACKED AT STA 1766 L14L. REMOVED DAMAGED LONGERON, FABRICATED AND INSTALLED REPLACEMENT LONGERON AND 2 EA SPLICES IAW SRM 51-1-21, 53-02-02-0 FIG 011, AND 51-1-20D.

Part: SKIN — CRACKED (FS 1350-1490) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 HFEC & VISUAL INSP DETECTED A .225 INCH CRACK ON THE C-4 (D-PIT) LOWER FORWARD JAMB CORNER AS MARKED ON PART. REMOVED AND REPLACED FUSELAGE SKIN IAW SRM 51-1-20D, 51-1-21, 51-1-22, FS 1350 - 1490 L31R - L31L.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 LONGERON CRACKED AT STA 1766 L14R. REMOVED CRACKED LONGERON, FABRICATED & INSTALLED REPLACEMENT LONGERON AND 2 EA REPAIR SPLICES IAW SRM 53-05-0, 51-02-00, 53-02-02, 51-3-0, 51-1-20D.

Part: SKIN — CRACKED (L1 DOOR) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 - FOUND EXT FUSE SKIN HAS 1/4" CRACKED AT L1 DOOR HOLD OPEN RECPT. REMOVED EDGE DAMAGE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-02-00 FIG 001R, 51-3-0 AND EO DC8-5330-19684.

Part: DOUBLER — CORRODED (CARGO DOOR) · airframe 68,243 hrs · 26,450 cycles

INSPECTION TYPE:C3 REMOVE STEEL DOUBLER ON THE C-4 (D-PIT) UPPER AFT CORNER AND REPAIR IAW SRM 53-2-0 FIG 21 AND/OR DRAWING SRO8530019. REMOVED DOUBLER AND FILLER AND FOUND CORROSION OUT OF LIMITS. REPAIRED IAW EO DC8-5330-25873-A.

Part: LINE — LEAKING (RT MLG BRAKE)

ON LANDING TURNOFF, BRAKES HAD ABNORMAL FEEL TO THEM, HYDRAULIC FLUID LEVEL WENT TO AUX, SYSTEM PRESSURE WENT TO ZERO. HYDRAULIC BRAKE PRESSURE WENT TO ACCUMULATOR RED LINE. FOUND RMLG TRIM CYLINDER LINE BROKEN REMOVED LINE, REPLACED RIGHT MLG BOGIE TRIM UPPER HYDRAULIC LINE PER DC8 MM 20-12-00-2. LEAK CHECK OK.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ARE INOP. REMOVED AND REPLACED BATTERY PACK PER MM 33-50-01. OPS CHECKS GOOD.

Part: SMOKE GOGGLES — MISSING (COCKPIT)

INSPECTION TYPE:N/A SMOKE GOGGLES MISSING AT 2ND OBS STATION. INSTALLED SMOKE GOGGLES 1 EA.

Part: LIGHT — NO TEST (COCKPIT)

FOUND EMERG EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

INSPECTION TYPE:N/A DURING PREFLIGHT FOUND EMERGENCY LIGHTS INOP. REPLACED BATTERY/RELAY PACK IAW MM 33-50-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS WILL NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AND OPS CKS GOOD. REF AMM 33-50-01-2.

Part: SKIN — CORRODED (FUSLEAGE)

SKIN BULGING AT SEAM APPROX 6 FT AFT OF NOSE GEAR LEFT SIDE OF FX MARKED. DAMAGED FINGER 5 INOP FOUND CORRODED. REMOVED DAMAGE, INSPECTED AREA TO INSTALL REPAIR. FABRICATED NEW FINGER DOUBLER SECTION IAW PRELIM EO DC8-5330-22410-A. INSTALLED 80 PERCENT OF FASTENERS. COMPLETED PER EO 5330-22410-A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY LIGHTS NO ILLUMINATION. REMOVED AND REPLACED BATTERY PACK, OPS GOOD MM 33-50-00.

Part: DEFLECTOR — CRACKED (THRUST REVERSER) · airframe 67,297 hrs · 25,713 cycles

INSPECTION TYPE: C1, DEFLECTOR RING CRACKED INSIDE NR 1 T/R AT 7:00 POSITION. REMOVED TRANSLATING COWL PER MM78-30-03. STOP DRILLED CRACK AND VERIFIED SAME PER SPM06-10-01.001. FABRICATED AND INSTALLED REPAIR FROM AMS 5510/5515 PER SAA SK798-837, ESM78-31-41. INSTALLED TR PER MM78-30-03, OPS AND LEAK CHECK GOOD.

Part: SUPPORT FITTING — CRACKED (THRUST REVERSER) · airframe 67,297 hrs · 25,713 cycles

INSPECTION TYPE: C1, UPPER FWD SUPPORT FITTING CRACKED INSIDE NR 1 IB TR CORE COWL. REMOVED NR 1 IB TR PER MM78-30-00-4. REMOVED AND REPLACED DISCREPANT FITTING REF SRM 51-3-0, 51-1-21. INSTALLED TR PER MM78-30-00-4. RIG, OPS, AND LEAK CHECK OF TR GOOD PER MM78-30-00-4.

Part: ANGLE — CORRODED (RT MLG WW) · airframe 67,297 hrs · 25,713 cycles

VERTICAL STIFFENER CORRODED BEYOND LIMITS ON AFT SIDE OF WING REAR SPAR, RT W/W, STA 857 BULKHEAD XCW46. FABRICATED REPLACEMENT ANGLE FROM ACA41283 7075T6 EXT REF DWG 5643433. NDT PER DPS4.707, NO CRACKS NOTED. REMOVED AND REPLACED ANGLE PER SRM 51-1-21, 51-1-8, 51-3-0, 51-1-20D. FUEL LEAK CHECK GOOD ON UPS TC8000.

Part: SKIN — CORRODED (RT WING) · airframe 67,297 hrs · 25,713 cycles

RT WING UPPER SKIN CORRODED AROUND HILOCK AT XRS554, ABOVE S54. NDT VERIFIED MATERIAL THICKNESS AT CORROSION REMOVAL SITE RANGED FROM .090-0.125. CUT OUT CORROSION SITE REF SRM 57-2-1 FIG28. FABRICATED DOUBLER AND FILLER FROM SHT7075T6-.190, MACHINED FILLER TO MATCH THICKNESS, INSTALLED AND SEALED CONICAL WASHERS AND REPAIR PARTS REF SRM 57-2-1 FIG 28, 51-1-20D, 51-1-8, 51-1-20B, 51-1-15.

Part: ATTACH FITTING — CRACKED (TAILCONE) · airframe 67,297 hrs · 25,713 cycles

TAILCONE ATTACH FITTING CRACKED AT CROWN (L1) ON FWD SIDE OF STA 1890 FRAME IN 62 COMP'T. REMOVED FITTING REF 51-1-20D. FABRICATED REPLACEMENT FITTING FROM PLATE 7075T6 REF DWG 3652562. NDT PER DPS4.707, NO CRACKS NOTED. INSTALLED FITTING REF SRM 51-1-8, 51-1-20D, 51-3-0, 51-1-21, 51-1-15.

Part: SPAR — CRACKED (WING CENTER SECT) · airframe 67,297 hrs · 25,713 cycles

INSPECTION TYPE: C1, CENTER WING REAR SPAR LOWER CORD CRACKED IN RT W/W, STA 857, OB CORNER. NDT MAPPED CRACK REF SPMSPM06-10-01.001. STOP DRILLED AND VERIFIED BY NDT. FABRICATED AND INSTALLED REPAIR PARTS PER SRO8570009

Part: FITTING — CRACKED (CARGO BAY) · airframe 67,297 hrs · 25,713 cycles

BATH-TUB FITTING CRACKED AT STA 320, LONG 27L. REMOVED CRACKED FITTING REF 51-3-0, 51-1-21. FABRICATED REPLACEMENT FITTING FROM PLT7075T6 PER DWG3755822. NDT FITTING REF DPS7.707 NO CRACKS NOTED. FABRICATE SPLICE ANGLES FROM BAC1503-100163 AND INSTALLED ALL PARTS REF SRM 53-2-0 FIG 2D, 51-1-8, 51-3-0, 51-1-20, 51-1-15.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,297 hrs · 25,713 cycles

FLOORBEAM AT STA 55 RBL40 CORRODED BEYOND LIMITS. CUT OUT CORRODED AREA, NDT VERIFIED REF NDT SPM06-10-01.001 FABRICATED 2 FILLERS FROM 7075T6-.071. REPAIR ANGLE FROM AND 10136-2403, SPACER FROM 2024T3-.032. INSTALLED ALL REPAIR PARTS REF SRM 53-2-0 FIG1 F, 53-2-0 FIG 1B, 51-1-8.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,297 hrs · 25,713 cycles

LONGERON 34L CRACKED AT STA 1260-1280. REMOVED LONG SPLICES AT STA 1270 STA 1350 PER SRM 51-1-20D OPENED SKIN FROM STA 1250-1350 FOR ACCESS REF SRM 51-1-21, 51-1-20D. REMOVED, FABRICATED, AND REPLACED LONG 34L FROM STA 1270-1350 REF DWG3758593, AND CLOSED SKIN PER SRM 51-1-21 AND 51-1-20D. REINSTALLED SPLICE FITTINGS REF SRM 51-1-20D.

Part: FITTING — CRACKED (RT MLG WW) · airframe 67,297 hrs · 25,713 cycles

INSPECTION TYPE:C1 SHEAR WEB FITTING CRACKED IN RT MLG W/W AT STA 857 APPROX RBL12. REMOVED CRACKED FITTING REF SRM51-3-0. FABRICATED REPLACEMENT FITTING FROM PLATE7050T7 PER SAA SK798-657, BOEING SERVICE ID 1-48219038 AND DAC DWG3646874. INSTALLED FITTING REF SRM51-1-20D, 51-1-8, 51-1-11, 51-3-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,297 hrs · 25,713 cycles

C1 BATH-TUB FITTING CRACKED AT STA300 L27L-L28L. REMOVED CRACKED FITTING AND FABRICATED REPAIR PARTS REF SRM53-2-0 FIG 2D. INSTALLED REPLACEMENT FITTING AND SPLICE ANGLES REF SRM 53-2-0 FIG2D AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,297 hrs · 25,713 cycles

INTERCOSTAL ATTACH FITTING CRACKED ON FWD SIDE OF STA 1000 FRAME AT L30L. REMOVED 2 GUSSETS AT STA 1000 AND REMOVED CRACKED FITTING REF SRM 51-1-21, 51-1-20D, 51-3-0. INSTALLED REPLACEMENT FITTING AND 2 GUSSETS REF SRM 51-1-20D, 51-1-8.

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,297 hrs · 25,713 cycles

CORROSION ON FRAME AT STA 1080 ABOVE L36. REMOVAL EXCEEDED ALLOWABLE LIMITS. NDT VERIFIED MAT`L THICKNESS FROM 0.111- 0.154 REMOVED FRAME CAP AND 3 GUSSETS FROM L33R TO L35L REF SRM 51-1-21, 51-1-20D. FABRICATED AND INSTALLED REPAIR STRAP FROM 7075T7-.080 PER UPS RA NR DC8-53-20444, SAA SK798-748. RE-INSTALLED CAP AND GUSSETS REF SRM 51-1-21, 51-1-20D, 51-1-8.

Part: SUPPORT FITTING — CORRODED (T/E FLAP) · airframe 67,297 hrs · 25,713 cycles

RT FUSELAGE FLAP HINGE STA 3 SUPPORT FITTING CORRODED BEYOND LIMITS. REMOVED AND REPLACED SUPPORT ASSY REF SRM 51-1-20D, 51-1-21, UPS EO DC8-5740-21256A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,297 hrs · 25,713 cycles

FITTING CRACKED ON FRAME AT STA 1180, LONG 19R. REMOVED AND REPLACED FITTING REF SRM 51-1-20D, 51-1-8.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,297 hrs · 25,713 cycles

LONGERON 15R CRACKED AT STA 1750. REMOVED DAMAGED LONG SECTION FROM STA 1740-1766, SHEARTIE AT STA 1750, AND END FITTING AT STA 1766 PER SRM 53-2-2 FIG10, 51-1-20D, 51-1-21. FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION FROM S1616757 EXT AND 2 STRAPS FROM SHT7075T6-.080 PER SRM 53-2-2 FIG10, REINSTALLED END FITTING, SHEAR TIE, AND REPAIR SPILCE REF SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,297 hrs · 25,713 cycles

LONGERON 15L CRACKED AT STA 1750. REMOVED CRACKED LONGERON SECTION FROM 1740-1760, 2 SHEAR TIES AT STA 1750 END FITTING AT STA 1760 REF SRM 51-1-21 AND 53-2-3. FABRICATED REPLACEMENT LONG SECTION FROM S1616757 EXT AND STRAPS FROM 7075T6-.080 PER SRM 53-2-3. INSTALLED ALL PARTS AND NEW SPLICE FITTING PER SRM 53-2-3, 51-1-20D, AND 51-1-8.

Part: FITTING — CRACKED (MAIN CABIN) · airframe 67,297 hrs · 25,713 cycles

END FITTING CRACKED ON L13L STA 840. REMOVED FITTING REF SRM 51-1-20D. FABRICATED REPLACEMENT FITTING PER DWG 3779874 FROM 7075-T6 PLATE ON SAA TRAVELER NR 0072. NDT C/W ON FINISHED PART PER DPS4.707, NO CRACKS NOTED. INSTALLED FITTING REF SRM 51-1-20D.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 67,297 hrs · 25,713 cycles

RT FUSELAGE FLAP HINGE SUPPORT FITTING CRACKED. DISSASEMBLED FLAP BUSS DRUM ASSY TO FOM PER MM27-51-06. REMOVED AND REPLACED SUPPORT ASSEMBLY REF SRM 51-1-21, 51-1-20D, 51-3-0 51-1-8, 51-1-15. REASSEMBLED AND RIGGED FLAP BUS PER 27-51-06. OPS CHK GOOD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,297 hrs · 25,713 cycles

C1 LONGERON 19 RT END FITTING CRACKED AT STA 860. REMOVED AND REPLACED L19R END FITTING REF SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,297 hrs · 25,713 cycles

LONGERON 11R END FITTING CRACKED AT STA 680. REMOVED AND REPLACED CRACKED FITTING PER SRM 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,297 hrs · 25,713 cycles

CORROSION ON FRAME AT STA -99 AT DOOR 90A NEAR L23L. REMOVED LIGHT CORROSION AT SITE. REMOVED .003 MAT FROM .088 THICK RIB, WITH IN LIMITS PER SRM53-2-0 FIG 1F, TREATED PER SRM 51-1-8. FOUND RIB CRACKED. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER (7075T6-.080) AND REPAIR ANGLE (7075O-.100 H.T. TO T6) REF SAA SK798-255, DPS 7.00-1, SRM51-1-26, 51-1-20D, 51-1-8.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM 33-50-01-2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHTS FAILED TO ILLUMINATE WHEN TESTED. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OP'S CHECKS NORMAL PER MM 33-50-01-2 ITEM 4.

Part: HYDRAULIC LINE — RUPTURED (HYD SYSTEM)

INSPECTION TYPE:N/A IN FLIGHT HYD QT INDICATOR DROPPED RAPIDLY TO AUX LEVEL. RAN CHECK LIST TO ISOLATED LOSS. QUANTITY REMAINED AT AUX LEVEL, BUT AFTER CONFIGURING FOR LANDING (LAST 5 MINUTES) QUANTITY DROPPED TO ZERO. PRESSURE FELL OFF AFTER LANDING. FOUND HYD LINE RUPTURED AT PITCH TRIM CONTROL VALVE (IPC 27-40-00/040 ITEM 35). REMOVED DAMAGE LINE AND INSTALLED FLEX LINE. DEFER CONTROL D273079.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

INSPECTION TYPE: PFLT, EMERGENCY EXIT LIGHTS BATTERY PACK IS DEAD. REPLACED BATTERY PACK, OPS OK.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE: PFLT EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK. OPS CHECK'S GOOD IAW MM 33-50-01. S/N ON 10886, S/N OFF 348.

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 2ND OBSERVER'S FWD SEAT TRACK LOCK PIN HOLES WORN. REMOVED OLD SEAT TRACK IAW DC8 SRM 51-3-0. DRILLED NEW SEAT TRACK IAW DC8 SRM 51-1-24. INSTALLED NEW SEAT TRACK IAW DC8 SRM 51-3-0.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,421 hrs · 2,499 cycles

INSPECTION TYPE:C-2 SHEAR TIE AT FS 1680 CRACKED AT LONG 18L. REMOVED AND REPLACED SHEAR TIE IAW DAC DWG 5640243-1.

Part: FITTING — CRACKED (LT WING) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 LT WING STR 51, O/B FWD STRINGER END FITTING IS CRACKED. RECEIVED NEW FITTING LOCATED & DRILLED FITTING IAW DC 8 SRM 51-1-24. INSTALLED IAW DC8 SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (LT WING) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 LT WING STR 51 I/B END, STR END FITTING CRACKED. RECEIVED NEW FITTING LOCATED AND DRILLED IAW DC8 SRM 51-1-24. INSTALLED IAW DC8 SRM 51-3-0 & 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 MAIN CABIN AT FS 1655 LONGERON 11R IS CRACKED. REMOVED AND REPLACED LONGERON PER DC8 SRM 51-1-21 AND 51-1-20D.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 AFT ACCY COMPARTMENT FS 1680 AT LBL 48 LOWER SURFACE OF UPPER FLOORBEAM FLANGE IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, BEYOND LIMITS IAW DC8 SRM 53-2-0 FIG 1F. FABRICATED REPAIR ANGLES AND FILLER IAW DC8 SRM 53-2-0 FIG 1B SHEET 3. INSTALLED IAW DC8 SRM 51-1- 20D.

Part: SKIN — CORRODED (LT WING) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 LT WING LOWER WING SKIN, O/B OF FUEL VENT PANEL, FWD OF REAR SPAR, IS CORRODED ON EXTERIOR SURFACE. CUT OUT DAMAGE, FABRICATED DOUBLER AND FILLER IAW REO G08852 AND DC8 SRM 57-2-0 FIG 2A, AND INSTALLED DOUBLER REPAIR IAW REO G08852 AND DC8 SRM 51-1- 20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE: C-2, R-1 FORWARD SERVICE DOOR CUTOUT, UPPER FORWARD CORNER HAS CRACK INDICATION ON EXTERNAL SKIN. FABRICATED -23 FILLER, -15 AND -17 DOUBLERS IAW DC8 SRM 53-2-0 FIG 1 4. ALODINED AND PRIMED FILLER AND DOUBLERS IAW DC8 SRM 51-1-8. INSTALLED -15, -17 DOUBLER AND -23 FILLER IAW DC8 SRM 53-2-0 FIG 14. INSTALLED UPPER FWD AND CENTER WEBS IAW DC8 SRM 51-1-20D, 51-1-21

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 AFT CARGO PIT AT FS 1150-1160 BETWEEN L35L-35R SKIN IS CORRODED. REMOVED EXISTING FITTING, LOCATE, DRILL & DEBURRED NEW FITTING AND FABRICATED DRILLED REPAIR SPLICES, AND INSTALLED FITTING AND REPAIR SPLICES IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 AFT CARGO PIT AT FS 1160 BETWEEN L33R-L34R Z FITTING IS CRACKED. REMOVED CRACKED Z FITTING TO FOM. RECEIVED NEW Z FITTING. FABBED FILLER IAW DC8 SRM 53-2-0 FIG 20. LOCATED DRILLED DEBURRED NEW FITTING IAW DC8 SRM 53-2-0 FIG 20.

Part: STRAP — CRACKED (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 L2 AFT PAX DOOR, UPPER FWD CORNER HAS CRACK INDICATION AT FRAME ATTACHMENT FOUND BY RADIOGRAPHIC INSPECTION. REMOVED AND REPLACED STRAP IAW DAC DWG 5750985 AND DC8 SRM 51-1-20D AND 51-1-21.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 AFT CARGO PIT AT FS 1160 BETWEEN L35R-36 Z FITTING IS CORRODED. REMOVED CORRODED ZEE FITTING, LOCATE NEW FITTING, DRILLED EXISTING FASTENER HOLES AND DEBURRED IAW DC8 SRM 51-3-2. FABRICATE REPAIR SPLICES IAW DC8 SRM 53-2-0. INSTALLED ZEE FITTING AND REPAIR SPLICES IAW DC8 SRM 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 R2 AFT SERVICE DOOR, UPPER AFT CORNER HAS CRACK INDICATION BETWEEN FASTENERS FOUND BY RADIOGRAPHIC INSPECTION. TRIMMED OUT CRACKED AREA. FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW DC8 SRM 53-2-0 FIG 16.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,421 hrs · 2,499 cycles

INSPECTION TYPE:C-2 STA 1600 L21L FLOORBEAM FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D, DRILLED NEW FITTING AND INSTALLED IAW DC8 SRM 51-1-20D AND DAC DWG 3751062.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 AFT ACCESSORY COMP AT STA 1660 FLOORBEAM ABOUT BL20 HAS CORROSION AND MISSING 4 EA ATTACHING BOLTS. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0 FIG 1F. REMOVED DAMAGED AREA & FABBED 1 EA FILLER & 2 EA REPAIR ANGLES IAW DC8 SRM 53-2-0 FIG 1B. INSTALLED FILLER AND REPAIR ANGLES IAW DC8 SRM 53-2-0 FIG 1B.

Part: FRAME — CORRODED (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 AFT ACCESSORY COMPT AT STA 1620 LONG 25R FRAME HAS CORROSION. REMOVED CORRODED FRAME SPLICE IAW DC8 SRM 51-1-20D. LOCATED AND DRIL LED NEW SPLICE IAW DC8 SRM 51-1-24. INSTALLED IAW DC8 SRM 51-1-20D

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 LT MLG W/W INBD WEB CRACKED ABOUT KEELBEAM AS STA 906.00 TO 910.00, JUST AFT OF MLG DOOR ACTUATOR MOUNT FITTING. CUT-OUT DAMAGED SECTION OF WEB IAW DAC DWG 5754125, FABBED AND LOCATED AND DRILLED REPAIR PARTS IAW DAC DWG 5614943 & 5754125, INSTALLED REPAIR IAW DAC DWG 5614943 & DC8 SRM 51-1-21.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,421 hrs · 2,499 cycles

INSPECTION TYPE:C-2 AFT LWR PIT BETWEEN STA 1440 TO 1460 AT LONG 27R IN TORQUE BOX WEB IS CORRODED. REMOVED WEB, INTERCOSTAL AND (2) ATTACH CLIPS IAW DC8 SRM 51-1-21A & 51-1-21. FAB NEW INTERCOSTAL, WEB, & REPAIR IAW DC8 SRM 53-2-0 & DAC DWG 5616674. REC'D LOCATED (2) NEW ATTACH CLIPS IAW DC8 SRM 51-1-2 4. INSTALLED IAW DC8 SRM 51-1- 20D & 51-1-21

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 FWD CARGO PIT ATTACH FITTING FOR MAIN CABIN FLOORBOARD CRACKED ON FWD SIDE OF FLOORBEAM STA 160 BL 0. FABRICATED ONE FITTING IAW DC8 DWG 4772359, LOCATED HOLES AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 A/C PRESS COMPT AT FS 56 AT L24R FRAME IS CRACKED AT AC DUCT STANDOFF ATTACH BRACKET. FABRICATED NEW FRAME SEGMENT AND SPLICES IAW DC8 SRM 53-2-0. INSTALLED IAW DC8 SRM 51-1-20D.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 AIR COND/PRESS COMPT AT FS 56 ABOVE L24L FRAME IS CRACKED AT A/C DUCT STANDOFF ATTACH BRACKET. REMOVED FRAME SECTION, FAB NEW FRAME SECTION AND SPLICE IAW DC8 SRM 53-2-0, INSTALLED FRAME SECTION AND SPLICES IAW DC8 SRM 51-1-20D.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 R2 DOOR JAMB LOWER FWD AND AFT CORNERS HAVE A REPAIR THAT DIFFERS FROM SRM. REMOVED AND REPLACED SKIN STA 1642 TO 1690 IAW DAC DWGS 5772776 AND 5772656. REPAIRED LOWER FWD CORNER IAW REO G08849.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 66,421 hrs · 24,990 cycles

INSPECTION TYPE:C-2 L2 DOOR JAMB LOWER FWD AND AFT CORNERS HAVE A REPAIR THAT DIFFERS FROM SRM. REMOVED AND REPLACED SKIN FROM STA 1642 TO 1690 IAW DAC DWG 5615775 AND 5750985. REPAIRED FWD LOWER CORNER IAW REO G08850.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:PFLT EMERGENCY LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK, OPS OK.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:IN EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED BATTERY PACK.

Part: SEAL — FAILED (PAX DOOR)

INSPECTION TYPE:N/A COULD NOT MAINTAIN CABIN PRESSURE WITH BOTH PACKS ***SUPPLEMENTAL MRR*** SEALED R2 DOOR AND R1 WINDOW PRESS CHECKED GOOD IAW 21-31-00

Part: PANEL — FAILED (CABIN)

INSPECTION TYPE:N/A, RTR-NR 4 GEN PWR FAIL ILLUM, LWR CGO FIRE LIGHT ILLUM ALL PANEL LIGHTS WENT OUT, SMOKE OF UNKNOWN ORIGIN FILLED COCKPIT AND CABIN. SHUTDOWN 1, 2 AND 4 ENGINES. *S/D* T/S AND FOUND NR 4 VRG FAILED PREVENTING NR 1 BTR CLOSURE. REMOVED AND REPLACED NR 4 VRG PANEL. RAN ALL ENGINES. AC GEN SYST PREF CK AND OP CK NORMAL MM 24-20- 00. P/N ON/OFF 51508-000, S/N ON: 937ABC, OFF: 265ABC.

Part: UNKNOWN — ODOR (FLIGHT DECK)

INSPECTION TYPE:N/A BURNING SMELL IN COCKPIT DURING DEPARTURE NR 1 XFER RECTIFIER SHORTED DUE TO WATER INTRUSION DRIED OUT WATER AND DEFERED

Part: PACKING — FAILED (FLAP CONTROL)

INSPECTION TYPE:N/A, AFTER TAKEOFF FLAPS STOPPED AT 10 DEG, HYDRAULIC PRESSURE DECREASED TO 0 PSI, AND HYDRAULIC QUANTITY DEPLEATED TO EMERGENCY AUX LEVEL. CREW RAN RES LOW PRESS LIGHT CHECKLIST AND LOSS OF HYDRAULIC PRESSURE EMERGENCY CHECKLIST. FOUND LT AIL PWR CNTRL VALVE HYD MANIFOLD LEAKING DUE TO LOOSE ATTACH BOLTS AND BLOWN SEAL. REMOVED AND REPLACED SEALS, TIGHTENED BOLTS AND OPS CK AIL HYD PACK PER MM 27-10-07. SEAL P/N ON NAS1611-112A. SERVICED HYD FLUID IAW MM 12-30-01.

Part: SPLICE — CRACKED (PRESSURE BLKHD) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, STA 8 RT PRESS BULKHEAD REPAIR SPLICE AT TOP CRACKED NOSE WW RT TUNNEL AREA. REMOVED AND REPLACED PACK DOORS ACTUATOR. REMOVED AND REPLACED TWO LOUVER PACK DOORS. REMOVED AND REPLACED REPAIR SPLICE FTG.

Part: FITTING — CRACKED (CARGO BAY) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, AFT PIT FS 1180 FITTING AT L35R - L34R CRACK. REMOVED FITTING RCVD NEW FITTING (P/N 3755843-501N) MAT ID FOR REPAIR ANGLE 60-436 .125 7075-T6 ANGLE PO 288271 IAW DC8 SRM 53-2-0. FABED REPAIR ANGLES IAW DC8 SRM 53-2-0 LOCATED AND DRILLED IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED IAW DC8 SRM 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, FS 80 AT L1L & L2L FRAME HAS EXFOLIATED CORROSION ON FWD SIDE. REPAIRED IAW DC8 SRM 53-2-0 FIG 2.

Part: RIVET — SHEARED (NLGWW) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, EVIDENCE OF CORROSION 3 RIVETS SHEARED OFF STA 12 CEILING STIFFENER AT FRAME NOSE WW RT TUNNEL AREA. REPAIRED IAW REO G07615.

Part: SKIN — CRACKED (RT WING) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, RT WING LOWER SKIN I/B OF NR 4 PYLON AND I/B OF MOLD LINE DOUBLER HAS APPROXIMATELY 1 INCH CRACK IN SKIN. FABED AND INSTALLED INTERNAL DOUBLER, TRIPLER AND FILLERS IAW REO-G07 605. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, RT INBOARD PRESSURE PANEL LWR ATTACH ANGLE IS CRACKED, STA 857.0 ABOVE CTR WING TANK UPPER SKIN RWW. CLEANED SEALANT FROM AREA, FABED REPAIR ANGLE AND STRAPS IAW DC8 SRM 53-2-5. ALODINED AND PRIMED IAW 51-1-8, INSTALLED REPAIR PARTS IAW 51-1-20D, REINSTALLED ALL CABLES IAW 20-12-00.

Part: FITTING — CRACKED (CABIN) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, MAIN CABIN LONG END FITTING CRACK BETWEEN STA 900 AND STA 920 AND L10L. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, STA 360 L33R FITTING ON FRAME HAS CORROSION. REMOVED CORROSION IAW 51-1-8 FOUND TO BE OUT OF LIMITS IAW 53-2-0. LOCATE NEW FITTING P/N 4759281-503 AND DRILLING EXISTING HOLES IAW DC8 SRM 51-1-20D, INSTALLED FITTING IAW 51-1-20D.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, IN FWD LWR CARGO COMPT STA 580 - 600 L33R INTERCOSTAL IS BENT CRACKED AND GOUGED. REMOVED INTERCOSTAL, FABBED NEW INTERCOSTAL, ALODINED AND PRIMED. INSTALLED IAW DC8 SRM 51-1-8, 51-1-21, 51-1-20D & DAC DWG 5753650.

Part: FITTING — CORRODED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, STA 350 L36 FITTING HAS CORROSION GEN AND RECD RFTS 798UP-11-21713 W/ REO G07628. TRIMMED OUT CORROSION IAW REO G07628, ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, STA 680, L10R SPLICE FITTING CRACKED. REMOVED CRACKED FITTING AND REPLACED IAW DAC DWG 3779762 & 5615718.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, AFT PIT FS 1380 FRAME CORRODED AT LONGERON 36. REMOVED DAMAGED AREA ACQUIRED MAT ID FOR REPAIR ANGLE DOUBLER STRIP FILLER, FABBED REPAIR PARTS AND HEAT TREATED REPAIR ANGLE, ALODINED AND PRIMED REPAIR PARTS SEALED AND INSTALLED.

Part: FITTING — CORRODED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, AFT LWR CARGO COMPT STA 1180 L35R FITTING HAS CORROSION. REMOVED CORRODED FITTING, FABED REPAIR ANGLES IAW DC8 SRM 53-2-0, ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED NEW FITTING AND REPAIR ANGLES IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, STA 680 L5R SPLICE FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-3-0 AND 51-1-24, LOCATED AND DRILLED NEW FITTING IAW DAC DWG 3779762, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-1-21 AND 51-3-0 FITTING (P/N 3779762-501).

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, STA 680L7R SPLICE FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D AND 51-3-0, RECEIVED NEW FITTING (P/N 3779762-501), DRILLED IAW DC8 SRM 51-1-24, INSTALLED IAW DC 8 SRM 51-1-20D, 51-1-21 AND 51-3-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, STA 680 L4R SPLICE FITTING CRACKED. REMOVED CRACKED FITTING IAW DC8 SRM 51-3-0 & 51-1-24, LOCATED AND DRILLED NEW FITTING (P/N 3779762-501) IAW DAC DWG 3779762, INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-1-21 AND 51-3-0.

Part: FITTING — CRACKED (NLG) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, NWW LT NLG DOOR RETRACT ACTUATOR SUPPORT FITTING HAS 5 INCH CRACK ON FWD END LHS ABOVE PANEL NR 696. REPAIRED AREA IAW REO G07656.

Part: FITTING — CRACKED (CARGO BAY) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, IN THE AFT LOWER CARGO COMPT STA 1150 L35R, FITTING IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D, LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, FABRICATED DOUBLERS IAW DC8 SRM 53-2-0, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED FITTING AND DOUBLERS IAW DC8 SRM 51-1-20D.

Part: FRAME — CORRODED (CARGO BAY) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, THE AFT CARGO COMPT STA 1160 - 1220 L35L - L36 AREA FRAME UPPER SURFACE HAS CORROSION SEVERAL PLACES. REMOVED CORR IAW DC8 SRM 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 5 3-2-0. GEN AND RECD RFTS N798UP REO G07632. FAB DOUBLER AND FILLER IAW REO G07632. ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, AFT LWR CARGO COMPT STA 1180 L33R FITTING CRACKED. REMOVED FITTING IAW 51-1-20D, RECEIVED NEW FITTING P/N 3755841-501N PO SP0470 579 RECEIVED DOOR JAMB FITTING DOUBLERS 3755841-5U, LOCATED AND DRILLED NEW FITTING DOUBLERS IAW DC8 SRM 51-1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED FITTING AND FITTING DOUBLERS IAW DC8 SRM 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, AFT LOWER PIT TRANVERSE FLOORBEAM END FITTING HAS CORROSION FS 1220 BL 64L. REMOVED CORROSION IAW 51-1-8, FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2 -0, REMOVED FITTING IAW DC8 SRM 51-1-20 & 51-3-0, RCVD LOCATED AND DRILLED FITTING IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-1-20D & 51-3-0.

Part: FITTING — CORRODED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, FITTING CORRODED BEYOND LIMITS. REPLACED FITTING IAW DC8 SRM 51-1-20D.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, FLC INTERCOSTAL CORRODED BTW STA 70R, 71R AND L33R. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 51-1-8 & 53-2-0. FABED FILLER AND ANGLE DOUBLER IAW DC8 SRM 53-2-0. ALODINED AND PRIMED INSTALLED IAW DC8 SRM 53-2-0 & 51-1-8.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, AFT LOWER PIT TRANSVERSE FLOORBEAM END FITTING CRACKED BETWEEN BOLT HOLES FS 1160 BL 66R AT FWD UPPER CORNER OF C-PIT DOOR. REMOVED TRANSVERSE FLOORBEAM END FITTING IAW DC8 SRM 57-1-20D END FITTING FOUND TO BE CRACKED RCVD. ORDERED NEW FITTING (P/N 3754946-501N) (S/N 0 113), P/O 337650 LOCATED AND DRILLED HOLES INTO NEW FITTING IAW DC8 SRM 5 1-1-20, INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, 51-3-0, 51-1-20. REMOVED FLOORBOARD FOR ACCESS AND REINSTALLED FLOORBOARD IAW DC8 SRM 51-3-0.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, INTERCOSTAL CRACKED AT STA 150 & L10RT. REMOVED INTERCOSTAL IAW DC8 SRM 51-1-20D, FABED NEW IAW DAC DWG 56157 00, ALODINED AND PRIMED IAW 51-1-8.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, LONGERON 16L CRACKED AT FS 1774. REPLACED LONGERON 16L FS 1774 IAW DC8 SRM 51-1-20D, 51-1-21 & 51-3-0.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, LWR FUSELAGE LONG 34 LT SIDE END FTG AT STA 780 IS CRACKED. REMOVED AND REPLACED END FITTING IAW DC8 SRM 51-1-24 51-1-20D.

Part: FRAME — CORRODED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, FRAME LIP CORRODED (EXFOLIATION) AT STA 55, BETWEEN STR 2L-5L DOT I769. REMOVED GILLINER SUPPORT FOR ACCESS TO CORROSION REMOVED CORROSION IAW DC8 SRM 51-1-8, REMOVAL HAS FRAME OUT OF LIMITS. REMOVED DAMAGE SECTION OF FRAME IAW DC8 SRM 53-2-0 FIG 2 MAT ID FOR FRAME -61 SEGMENT 7 075-0 .071 PO 336613 IAW DC8 SRM 51-2-0 FIG 52 53-2-0 MAT ID FOR -1 7 & -19 SPLICE ANGLES IAW TPS 1003 REV A ALODINED AND PRIMED 51-1-8.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, FRAME STA 740R L13R HAS A CRACKED FITTING ON AFT SIDE. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20. RECEIVED NEW FITTING P/N 4 751643-1, DRILLED NEW FITTING IAW DAC DWG 4751643, INSTALLED IAW DC8 SRM 51-3-0 & DC8 SRM 51-1-21D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, FRAME SECTION 680R L14R HAS A CRACKED FITTING ON AFT SIDE OF INTERCOSTAL. REMOVED CRACKED FITTING, FABED FITTING IAW DAC DWG 2651707, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED WITH HI-LOKS IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (PYLON) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, NR 1 PYLON FWD OF FWD V-BLOCK SUPPORT FTG FOR PYLON PLANK PNL IS CRACKED P/N 5756790-1. REMOVED CRACKED V-FITTING IAW DC8 SRM 51-1-20D & 51-3-0. INSTALLED FWD V-BLOCK IAW DC8 SRM 51-1-20D & 51-3-0. LEAK CHECK OF FWD V-BLOCK TO BE PERFORMED ON UPS TASK CARD 8000 ECA 25131 ITEM 22. INSTALLED 575679 9 FAIRING IAW DC8 SRM 51-3-0. INSTALLED LOWER CLOSEOUT PANEL IAW DC8 SRM 51-3-0.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, INNER LIP OF STR 8L CORRODED (EXFOLIATION) AT STA 80 & 9G NET FTG DOT I777. REMOVED DAMAGED LONGERON L8L FROM STA 70 - 100 MACHINED NEW LONGERON IAW DAC DWG 5610118, LOCATED AND DRILL UP NEW LONGERON IAW DC8 SRM 51- 1-24, ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED IAW DC8 SRM 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, FITTING CRACKED. INSTALLED NEW FITTING AT FS 680 RT L11 IAW DC8 SRM 51-1-20D AND 51-3-0.

Part: SKIN — CORRODED (FUSELAGE) · airframe 64,943 hrs · 24,058 cycles

INSPECTION TYPE:C123, CORROSION IN FASTENER HOLE THROUGH FUSELAGE SKIN STA 1030 L23R. REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW DC8 SRM 53-2-0 MAT ID FOR EXTERNAL DOUBLER .140 7075-T6 PO 283708 MAT ID FOR FINGER DOUBLER .050 7075-T6 PO 332573 IAW DC8 SRM 53-4-1 & 53-2-1. FABED DOUBLER AND FINGER DOUBLER IAW DC8 SRM 53. ALODINED AND PRIMED DOUBLERS IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: REGULATOR — STUCK (COCKPIT)

CAPTAINS O2 REGULATOR STUCK ON REMOVED AND REPLACED CAPTAINS REGULATOR

Part: PANEL — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A, ATB- NR 4 GEN LOW VOLTAGE, CREW REPORTED SMOKE IN COCKPIT (DFW. *S/D* REMOVED AND REPLACED BUS PROTECTION PANEL.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE:SV 1 CRACK IN WING SKIN LT WING 18 I/B OF NR 1 PYLON. FABRICATED AND INSTALLED ALL BUSHINGS IAW REO 06799. FABBED STRAPS, SPLICES, DOUBLER, TRIPLER AND SKIN FILLER. CUT INTERNAL DOUBLER AND FABBED REPLACEMENT SEGMENT OF INTERNAL DOUBLER, TRIPLER. REAMED AND COINED HOLES AS MARKED IAW REO 06799. INSTALLED REPAIR PARTS IAW REO 06799.

Part: SKIN — CRACKED (LT WING)

1 INCH CRACK LEFT WING LWR SURFACE (18 INCHES INBOARD NR 1 PYLON).

Part: FUEL DUMP — CORRODED (FUEL SYSTEM)

INSPECTION TYPE:N/A, CORROSION AND METAL DISTRESS FOUND ON LEFT FUEL DUMP. ACCOMPLISHED INTERIM REPAIR PER EO DC-8-5720-1158-A, ITEM DEFERRED PER EO DC8-5720-11858-A. SPEED TAPE APPLIED, OK FOR CONTINUED SERVICE.

Part: BEAM — CRACKED (FUSELAGE)

AT C-CHECK, CRACKS WERE FOUND IN THE J-BEAM WHICH IS ATTACHED TO THE AFT FACE OF THE AFT PRESSURE BULKHEAD. THE CRACKS ORIGINATE IN THE RADII ADJACENT TO ATTACH BOLTS APPROXIMATELY 1 INCH EACH SIDE OF THE ACFT CENTERLINE. THE CRACKS APPEAR TO OCCUR UNDER NORMAL OPERATING CONDITIONS AND ARE POSSIBLY CAUSED BY THE COMBINED FORCES OF CABIN PRESSURE AGAINST THE FRONT FACE OF THE BULKHEAD AND TENSION FROM THE 13 FLIGHT CONTROL CABLES WHICH ARE ROUTED THROUGH PULLEYS ATTACHED TO THE J-BEAM. SUBMITTER RECOMMENDED THE FOLLOWING: PERFORM PERIODIC INSPECTIONS OF ALL DC-8 ACFT WITH FLAT AFT PRESSURE BULKHEADS, AND, REPAIR CRACKS PER DC-8 SRM 53-2-5 FIG 26.

Part: SKIN — CORRODED (WS 590-582)

INSPECTION TYPE:C2 RT WING LEADING EDGE LWR SURFACE BULGED XFS 590-582/FWD OF FWD SPAR. REMOVED CORROSION ALODINED AND PRIMED IAW DC8 SRM 51-1-8. FABBED INNER DOUBLER IAW DC8 ADDENDIUM 5720-4087-B. FABRICATED OUTER DOUBLER IAW DAC DWG 5641225. INSTALLED DOUBLER IAW DC8 SRM 1-1-21.

Part: INTERCOSTAL — CORRODED (BS 680-702)

INSPECTION TYPE:C2 INTERCOSTAL, FS 680-702 CORRODED RBL 20. REMOVED CORRODED WEB FABBED AND INSTALLED IAW DAC DWG 5773275, DC8 SRM 51-1-21, 51-1-8.

Part: SKIN — CORRODED (TAIL CONE)

INSPECTION TYPE:C2 TAILCONE LT LOWER SKIN CORRODED. REMOVED SKIN, FABBED NEW SKIN IAW DAC DWG 5764650. INSTALLED SKIN IAW DC8 SRM 51-1-21.

Part: FLOORBEAM — CRACKED (BS 902)

INSPECTION TYPE:C2 FLOORBEAM, STA 902 CRACKED AT RT O/B FLANGE. ROUTED OUT DAMAGE, FABBED FILLER AND SHIM IAW REO-05489 REV A FABBED. REPAIR STRAP ON UPS N/R 809637, DRILLED AND INSTALLED IT, FILLER AND SHIM IAW DC8 SRM 51-1-20D, 51-1-24 AND REO 05489 REV A.

Part: FRAME — CORRODED (BS 1971)

INSPECTION TYPE:C2 TAILCONE FRAME, STA 1971 CORR, BLO TO RBL 6. REMOVED FRAME SECTION, FABBED NEW SECTION, AND SPLICES IAW DC8 SRM 5 3-2-0 AND DAC DWG 5704650. INSTALLED REPAIR IAW DC8 SRM 51-1-20D.

Part: SKIN — CORRODED (BS 1190)

INSPECTION TYPE-C2, FUSELAGE EXTERIOR SKIN CORRODED STA 1190 AND LONG 22R. REPAIRED AREA IAW DC8 SRM 53-2-1 FIG 7. REMOVED CORROSION PER DC8 SRM 51-1-8. BLEND OUT WAS BEYOND LIMITS PER DC8 SRM 53-2-0. TRIMMED OUT DAMAGE, FABBED FILLER AND DOUBLER PER DC8 SRM 53-2-1 FIG 7 AND REO 05 451. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED PER REO-05451 AND DC8 S RM 53-2-1 FIG 7.

Part: FRAME — CRACKED (BS 1933)

INSPECTION TYPE:C2 CRACKED TAIL CONE FRAME, STA 1933 RIGHT OF L36. REMOVED DAMAGE, FABBED REPAIR FRAME AND SPLICES IAW DC8S RM 53-2-0 FI G 2, 51-3-2. INSTALLED REPAIR IAW DC8 SRM 53-2-0 FIG 2, 51-1-20D AND 51-1-8.

Part: EXTRUSION — CORRODED (TAIL CONE)

INSPECTION TYPE:C2 TAIL CONE, L36 EXTRUSION CORRODED, STA 1890-1940. REMOVED AND REPLACED EXTRUSION IAW DC8 SRM 51-1-24.

Part: SKIN — CORRODED (BS 1912-1950)

INSPECTION TYPE:C2 TAILCONE RT SKIN CORRODED, L33R TO L36 FS 1912-1950. REMOVED SKIN, FABBED AND INSTALLED NEW ONE IAW DAC DWG 5644500 AND DC8 SRM 51-1-8, 51-1-21.

Part: FRAME — CRACKED (BS 1919)

INSPECTION TYPE-C2, TAIL CONE FRAME STA 1919 RT SIDE OF LONGERON 36 CRACKED. REMOVED DAMAGED SECTION OF FRAME, FORMED FRAME SECTION IAW DAC DWG 5 704650. HEAT TREATED ANGLES, SPLICES, FORMED FRAME IAW TPS-1003 AND DC8 SRM 51-1-1. FAB FRAME AND SPLICE ANGLES AND DRILLED IAW DC8 SRM 53-2 -9. DAC DWG 5704650 AND DC8 SRM 51-3-2. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 795)

INSPECTION TYPE-C2, RT SIDE CENTER WING, STA 795 AND XCW46R FITTING IS CRACKED. REMOVED FITTING CRACKED AT RT CENTER WING STA 759 AND XCW46R. RECEIVED NEW FITTING 3641125-507 PO 270648. DRILLED HOLES IAW DC8 SRM 51-1 -24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1220)

INSPECTION TYPE:C2 AFT PIT AFT SIDE OF TORQUE BOX BOTTOM AFT CORNER OF CARGO DOOR FRAME, TORQUE BOX FITTING CRACKED AT 2 PLACES (BANANA FTGS). REMOVED AND REPLACED FITTINGS, STA 1220 AND 1228 IAW DC8 SRM 51-1-20 D, 51-1-21 AND 51-3-0.

Part: BULKHEAD BEAM — CRACKED (AFT PRESS BLKHD)

INSPECTION TYPE-C2, AFT FACE OF PRESSURE BULKHEAD STA 1766, 4TH HORIZONTAL BEAM HAS 2 CRACKS, 1 TOP AND 1 BOTTOM CENTER BEHIND CONTROL CABLES APPROX STA 36 (E824). VERIFIED CRACK IAW MIL STD 271F. STOP DRILLED CRACK AND FABRICATED REPAIR ANGLE IAW DC8 SRM 53-2-5 FIG 26. ALODINED AND PRIMED ANGLE IAW DC8 SRM 51-1-8. INSTALLED ANGLE IAW DC8 SRM 1-1-20D.

Part: ANGLE — CORRODED (BS 280)

INSPECTION TYPE-C2, CORROSION AROUND NUT PLATE ON TORQUE BOX RAMP ATTACH ANGLE AT FS 280, LONGERON 33L. REMOVED CORROSION ON GUIDE RAIL IAW DC8 SRM 51-1-8, OUT OF LIMITS. REMOVED RAIL, MAT ID 7075-0 .063 PO 265649 IAW REO-05501. FAB ANGLE DOUBLER IAW REO-05501. HEAT TREAT TO T-6 IAW DC8 SRM 51-1-1. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-20D, 51-1-21, 51-3-0.

Part: FLOORBEAM — GOUGED (BS 160)

INSPECTION TYPE:C2 FWD LWR CARGO STA 160 RBL 50 FLOORBEAM HAS GOUGE AROUND THE HI-LOK REPAIRED IAW REO5465.

Part: FRAME — CRACKED (BS 1920)

INSPECTION TYPE:C2 LT FRAME IN TAILCONE CRACKED AT CROSS STIFFENER FS 1920. STOP DRILLED FRAME, FABBED DOUBLER IAW DC8 SRM 53-2-0. INSTALLED DOUBLER IAW DC8 SRM 51-1-20D AND 51-1-21.

Part: FRAME — CORRODED (BS 712)

INSPECTION TYPE-C2, CORROSION ON FRAME STA 712 AT SEAT TRACK BOLT HOLES RBL 26. REMOVED AND REPLACED BOLTS IAW DC8 SRM 51-3-0. REMOVED CORROSION, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. FOUND WITHIN LIMITS IAW DC8 SRM 53-2-0.

Part: FITTING — CRACKED (BS 280)

INSPECTION TYPE:C2 FWD PIT X-SLIDE DOOR TORQUE BOX Z FITTING CRACKED AT FS280 LONGERON 32R. REMOVED AND REPLACED Z FITTING (BANANA FITTING) PT NR 3755827-501, REMOVED AND REPLACED FITTINGS PART NR 3754914-501 AND 3754914-501N. REMOVED AND REINSTALLED LONGERON END TIES 30R AND 32R. REMOVED LONGERON SECTION FS 250-280 L32R. INSTALL SPLICE AT FS 250 32R REINSTALL LONG SECTION FS 250-280 L32R.

Part: FITTING — CORRODED (BS 280)

INSPECTION TYPE:C2 CORROSION AROUND NUTPLATE HOLES INSIDE X-SLIDE DOOR TORQUE BOX FS 280 LONGERON 31-32R. REMOVED CORROSION IAW DC8 SRM 51-1-8. FOUND FITTING TO BE OUT OF LIMITS. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (BS 980)

INSPECTION TYPE:C2 WW PRESS PNL AREA, STA 980 AND XCW 64L FITTING IS CRACKED. REMOVED CRACKED FITTING, FITTING PN NR 4647365-1, FABBED ON NR 50004 LOCATED AND DRILLED IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D AND 51-1-17. ALODINED AND PRIMED FITTING MATING SURFACES IAW DC8 SRM 51-1-8.

Part: FITTING — CRACKED (BS 1220)

INSPECTION TYPE:C2 AFT LOWER CARGO PIT STA 1220 BELOW CUSP AT LONG 21R FITTING CRACKED. BLEND OUT CRACK IAW DC8 SRM 51-1-8. OUT OF LIMITS, PERFORMED HFEC IAW MIL-STD-271R TO VERIFY CRACK. REMOVED OLD FITTING. REMOVED AND REPLACED NEW FITTING FROM BORING P/N 375496-502N, DRILLED HOLES IN NEW FITTING IAW DC8 SRM 51-3-2. INSTALLED FITTING IAW DC8 SRM 51-1-21, 51-1-20D. ALODINED AND PRIMED IAW DC8 SRM 51-1-8.

Part: FLOORBEAM — CORRODED (BS 902)

INSPECTION TYPE:C2 STA 902 X.64 FLOORBEAM CORRODED. REMOVED 2 CORRODED ANGLES, DRILLED AND INSTALLED REPLACEMENT ANGLES IAW REO 05483, DC8 SRM 51-1-20D, 51-1-8.

Part: FITTING — CORRODED (BS 902)

INSPECTION TYPE-C2, STA 902 AND XCW64L, FUSELAGE FRAME FITTING AND FLOORBEAM IS CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS. INSTALLED NEW FITTING AND ALL PARTS IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: PRESSURE PANEL — CORRODED (BS 889)

INSPECTION TYPE-C2, STA 889 TO 900 XCW 10L SKIN HAS A GOUGE AND IS CORRODED, CENTERWING. BLENDED OUT GOUGE AND CORROSION IAW DC8 SRM 53-2-0. ORIG .063 IAW 53-7-2. REMAIN .043. FAB REPAIR DOUBLER IAW REO-05478 AND DRILLED IAW DC8 S RM 51-1-24. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW DC8 SRM 51-1-21, 51-1-15.

Part: BRACKET — CRACKED (WS 223)

INSPECTION TYPE-C2, RT WING LEADING EDGE NR 3 PNEU SHUT-OFF AFT ATTACH BRACKET AT XW223 CRACKED. REMOVED BROKEN BRACKET IAW DC8 SRM 51-3-0. MAT ID FOR NEW BRACKET 302 STAINLESS STEEL .063 IN ANNEALED CONDITION IAW DAC DWG NR 5802881 AND DC8 SRM 51-9-0. FAB NEW BRACKET IAW DAC DWG 5802881. INSTALLED NEW BRACKET IAW DC8 SRM 51-3-0.

Part: LONGERON — CORRODED (BS 110)

INSPECTION TYPE:C2 FWD CARGO COMPARTMENT LONG 27 RT CORRODED AT STA 110. REMOVED CORROSION IAW DC8 SRM 51-1-8. FABBED AND INSTALLED REPAIR IAW DWG DC08-53-0229.

Part: FITTING — CORRODED (BS 1690)

INSPECTION TYPE:C2 FS 1690 LONG 28L AND 32L END FITTINGS ARE CORRODED. REMOVED AND REPLACED FITTING L32L. REMOVED CORROSION FROM L28L IAW D C8 SRM 51-1-8. ALODINED AND PRIMED.

Part: BEAM — CRACKED (BS 1600)

INSPECTION TYPE:C2 IN AFT ACC COMP FLOORBEAM TO FUSELAGE FITTING LOWER ANGLE AFT SIDE AT FUSELAGE STA 1600 AND -X57 IS CRACKED AND CORRODED. REMOVED CORRODED FITTING AT STA 1600, RECIEVED NEW FITTING P/N 37510 62-506U AWR 50003. DRILLED AND DEBURRED IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1766)

INSPECTION TYPE:C2 AFT FACE OF PRESSURE BULKHEAD STA 1766 1ST HORIZONTAL BEAM LT OF C ENTER BEAM FITTING HAS CORR. REMOVED DAMAGED FITTING DRILLED NEW FITTING IAW DC8 SRM 51-1-24. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: FRAME — CRACKED (BS 1580)

INSPECTION TYPE:C2 BOTTOM OF FRAME AT STA 1580 LT IS BENT AND CRACKED. REMOVED EXISTING SHEAR TIE, AND FABRICATED NEW IAW REO 05454, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED IAW REO-05454.

Part: SKIN — CORRODED (WS 711)

INSPECTION TYPE:C2 RT WING L/E CORRODED AT XRS 711 FAST HOLES. CUT OUT CORROSION, FABBED REPAIR DOUBLER IAW DC8 SRM 57-2-1 ALODINED AND PRIMED REPAIR IAW DC8 SRM 51-1-8. INSTALLED REPAIR IAW DC8 SRM 51 -1-20D, 51-1-21 AND 51-1-21A.

Part: DOOR — OUT OF ADJUST (LT MLG)

RED DOOR NOT LATCHED, LIGHT ILLUMINATED IN FLT. LEFT ALT MAIN GEAR DOOR LIGHT ALSO ILLUMINATED IN FLT SEVERAL, ATTEMPTS WERE MADE TO RECYCLE GEAR TO NO AVAL. DIVERTED TO CAE PER DISPATCH REQUEST. CHECKED MLG DOOR LT FOLLOW UP PER 323105, CHECKED OK, CHECKED LT MLG DOOR UPLATCH PER 323104. REMOVED SHIMS FROM DOOR ROLLERS CHECKS OK, ALL DIMENSIONS WITHIN LIMITS PER 323104.

Part: ENGINE — FAILED (NR 4)

NR 4 ENGINE FLAMEOUT AT FL350, SUCCESSFUL RESTART WITH MILD VIBRATION. FLAMEOUT WITH THROTTLE ADVANCE. FIRE TEST INDICATED SHORT CIRCUIT, MA N-O-TEMP(270DEG. C). NR 4 BLEED OFF, TEMP DECREASE ENG FIRE, SEVERE DAMAGE CHECKLIST ACCOMPLISHED. DISCHARGED BOTH FIRE BOTTLES.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS BATTERY DEAD. CHARGED AND REINSTALLED EMERGENCY BATTERY, OP CHKS GOOD.

Part: SKIN — CORROSION (VERT STAB)

INSPECTION TYPE:C/CK, CORROSION AND DAMAGED NUT PLATES INSIDE AREA OF VERTICAL STAB LOWER LT AT REMOVED SKIN PANEL. REMOVED DAMAGED FABED FILLER AND DOUBLER IAW REO 036197, ALODINED AND PRIMED IAW DC8 SRM D51-1-8, INSTALLED FILLER AND DOUBLER IAW DC 8 SRM 51-1-250D, SEALED IAW DC8 SRM 51-1-15.

Part: TRAPEZOIDAL FTG — CRACKED (RT MLG WW)

INSPECTION TYPE:C/CK, RIGHT HAND MAIN LANDING GEAR TRAPEZOIDAL FITTING IS CRACKED AT FWD SIDE VERTICAL. REPAIRED FITTING IAW UPS EO DC8 5340 0748 PER APPENDIX D AND E USING KIT 78010659-509 IB AND O/B SPLICE RIGHT HAND.

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION TYPE:C/CK, FUSELAGE SKIN CRACKED AT FWD UPPER CORNER OF RIGHT HAND AFT TYPE I DOOR. PERFORMED HFEC AND FOUND CRACK AND MARKED REMOVED FASTENERS, PAINT AND CORROSION IAW DC8 SRM SD 51-1-8D AND 51-1-21, FABED DOUBLER AND TRIPLER AND FILLER IAW REO 036166, ALODINED AND PRIMED IAW DC8 SRM 51-1-8SD, INSTALLED REPAIR FILLER, DOUBLER AND TRIPLER IAW DC8 SRM SD51-1-20B AND SEALED REPAIR IAW DC8 SRM 51-1-16 AND 51-1-17.

Part: SKIN — CORRODED (HORIZ STAB)

INSPECTION TYPE:C/CK, LEFT HAND LOWER HORIZONTAL STAB INBOARD SIDE SKIN HAD CORROSION. REMOVED LT LOWER FAIRING AND I/B LOWER SKIN PANEL IAW DC8 SRM D581-3-0. REMOVED CORROSION IN SKIN PANEL AND REPAIRED SKIN PANEL AS PER REO 03183 REV A, ALODINED AND PRIMED IAW DC8 SRM 51-1-8. REINSTALLED FAIRING AND SKIN PANEL IAW DC8 SRM D51-3-0, 51-1-20D AND 51-1-20B.

Part: AUX FUEL TANK — CORRODED (RT WING)

INSPECTION TYPE:C/CK, RIGHT HAND FWD AUX TANK, LEADING EDGE HEAVILY CHAFED AT FILLET FAIR ING ATTACH POINT. REMOVED DAMAGED IAW REO 013173, FABED FILLER AND DOUBLERS IAW REO 03173, ALODINED AND PRIMED ALL PARTS, REPAIRED IAW DC8 SRM 51-1-8, INSTALLED ALL REPAIR PARTS WET IAW REO 03173 DC8 51-1-12, 51-1-21 AND 51-1-20B.

Part: FUEL PUMP — CRACKED (NR 1 ENGINE)

INSPECTION TYPE-N/A, NR 1 ENGINE MAIN ENGINE DRIVEN FUEL PUMP FILTER ASSY CAP UNSEATED WITH HELICOIL. A/C DECLARED FUEL LOSS IN INBD FLIGHT TO DTW. A/C HAD 12.4K LBS REMAINING. AIRPORT EMERGENCY EQUIPMENT WAS DISPATCHED. NR 1 ENGINE FIRE HANDLE WAS PULLED BY CREW TO S/O POSITION. ALSO, HELICOILS WERE STILL THREADED, FUEL FILTER CAP CRACKED. NR 1 ENGINE FUEL PUMP ASSY WILL REQUIRE REMOVAL AND REPLACEMENT.

Part: SPAR — CRACKED (RT AILERON)

INSPECTION TYPE N/A, RT INB AILERON, INB AILERON ATTACH HINGE, INB SET OF HOLES 2 HAVE CRACK INDICATIONS. INB HOLES ALL LAYERS CRACKED, 1ST 3 LAYERS INDICATIONS ON INB SIDE, AFT LAYER OUTB SIDE. OUTB HOLE FIRST 2 LAYERS HAVE CRACK INDICATIONS INB SIDE OF HOLE. OUTB SET OF HOLES, NO CRACKS NOTED. REPAIRED RT I/B AILERON HINGE ATTACH FITTING, I/B SET OF HOLES ON LOWER SPAR IAW REO-02070. TORQUED 6 AILERON STUD MOUNT BOLTS IAW DC8 SRM 51-3-1. INSTALLED WEB IAW DC8 SRM 51-3-6, 51-1-20D.

Part: TRIGGER — NOT LOCKED (NLG)

CLIMBING THROUGH 25K AT 340IAS, NOSE GEAR DOOR POSSIBLY FELL OPEN, CONFIRMED BY LOUD COCKPIT NOISE AND VIBRATION. IMMEDIATELY DECLARED AN EMERGENCY AND RAN GEAR DOOR UNLOCKED CHECKLIST IN THE QRH. RECTIFIED THE PROBLEM. NOSE GEAR LINK RELEASE TRIGGER WAS NOT FULLY LOCKED.

Part: FITTING — CRACKED (FS 1220)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FWD LOWER FLANGE OF FITTING CRACKED FS 1220 BETWEEN LONGERON 34R AND 35R. REMOVED DAMAGED FITTING ON FS 1220 LONGERON 34R - 35R AND REPLACED NEW FITTING PER SRM 53-2-0.

Part: FRAME — CRACKED (BS 99)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT FRAME CHORD CRACKED BELOW SPLICE, STA 99 AT WBL 4750 AS SEEN THROUGH PANEL 90B. MAINTENANCE INSTALLED LOWER CAP WBL ANGLE CHORD REPAIR AT STA 99 PER DHC SK 798-093 REV A (RT SIDE).

Part: FLOOR BEAM — CORRODED (BS 1600)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND THE FLOOR BEAM AT STA 1600 RBL 40 LOWER SIDE OF HORIZ. FLANGE WAS BEYOND LIMITS AFTER CORROSION REMOVAL. MAINTENANCE FABRICATED AND INSTALLED REPAIR PARTS PER DC8-5310-7457A.

Part: FLOOR BEAM — EXFOLIATED (BS 1560)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND THE FLOOR BEAM UPPER CAP EXFOLIATED AT LBL 3.0 TO LBL 6.0 AT STA. 1560. MAINTENANCE CUT OUT THE DAMAGED SECTION, FABRICATED REPAIR ANGLE AND FILLER AND INSTALLED PER DC8-5310-7446A.

Part: FRAME — CORRODED (BS 1240)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1240 LONGERON 36 FRAME CORRODED BEYOND ALLOWABLE LIMITS. MAINTENANCE REPAIRED FRAME IAW DHC SK 798-179.

Part: FRAME — CORRODED (BS 1260)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME FORMER CORRODED AT STA 1260 BETWEEN LONGERONS 35L AND 35R. MAINTENANCE FABRICATED REPLACEMENT SECTION AND INSTALLED IAW SRM 53-2-02B AND 53-4-1, FIGURE 51 AT STA 1260.

Part: FRAME — CORRODED (BS 99)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT FRAME CHORD SPLICE FITTING CORRODED AT STA 99 AS SEEN THROUGH PANEL 90B. MAINTENANCE FABRICATED SPLICE AND INSTALLED IAW SRM 51-1-20D, 51-1-20, 51-1-21, AND DC8-53-1476.

Part: INTERCOSTAL — CORRODED (BS 980-1000)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND THE INTERCOSTAL CORRODED AT STA 980 TO 1000 LONGERON 30R. MAINTENANCE FABRICATED INTERCOSTAL PER UPS DC8-53-1465, INSTALLED FABRICATED INTERCOSTAL IAW SRM 51-1-20.

Part: BLKHD ANGLE — CRACKED (CTR WING)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND THE CENTER WING LOWER SURFACE LT AFT CORNER BULKHEAD ATTACH ANGLE CRACKED. MAINTENANCE REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20 AND 51-3-0.

Part: FLOOR BEAM — CORRODED (BS 1640)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FLOOR BEAM STA 1640 RBL 29.5 TO BE OUT OF LIMITS. MAINTENANCE FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-1-20 AND DC8-53-1463.

Part: FRAME — CRACKED (BS 180)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND THE FORWARD SIDE OF THE FRAME CRACKED, LONGERON 34R AT STA. 180. MAINTENANCE INSTALLED FRAME REPAIR IAW SRM 53-2-0, FIGURE 2.

Part: FRAME — CORRODED (BS 1260)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME 1260 BETWEEN LONGERONS 35L AND 35R IS OUT OF LIMITS AFTER CORROSION REMOVAL. MAINTENANCE REMOVED CORROSION, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-2-0 AND 51-1-20.

Part: FITTING — CORRODED (BS 759)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME 759 RT, WHERE ATTACHED TO TOP OF OUTER WING SECTION HAS HEAVY CORROSION. MAINTENANCE REMOVED AND REPLACED FITTING PER SRM 51-1-21.

Part: INTERCOSTAL — MISINSTALLED (BS 270-280)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 270 TO 280 MCD FRAME HAS 2 INTERCOSTAL AT LONGERON 12 AND BETWEEN LONGERON 13 AND 14 LT. MAINTENANCE FABRICATED AND INSTALLED INTERCOSTAL IAW SRM 51-1-21, 51-1-20.

Part: STRINGER — CORRODED (BS 1740)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND STRINGER 20L AT STATION 1740 CORRODED. MAINTENANCE REMOVED THE DAMAGED STRINGER AND FABRICATED REPLACEMENT STRINGER, LOCATED AND INSTALLED IAW SRM 53-5-1.

Part: RIB — CRACKED (WS 810)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING OUTBOARD L/E RIB, STA XFS 810.00 IS CRAKCED AT THE AFT UPPER RIVET. MAINTENANCE INSTALLED ANGLE REPAIR IAW SRM 57-2-0 AND 51-1-20D.

Part: LE RIB — CRACKED (WS 353)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING L/E, STA XFS 353.0 UPPER L/E RIB CRACKED. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 57-2-0 AND 51-1-20D.

Part: FITTING — CRACKED (BS 1160)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME ATTACH FITTING CRACKED AND CORRODE, STA 1160 LONG 34R. MAINTENANCE INSTALLED REPAIR SPLICE IAW SRM 52-2-0 FIGURE 20 AND 51-1-20D.

Part: SEAT TRACK — CRACKED (BS 1030-1140)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND SEAT TRACK FS 1030 TO 1140 CORRODED BEYOND LIMITS AND STRESS CRACKED. MAINTENANCE REMOVED DAMAGED SECTION OF TRACK AND INSTALLED NEW SECTION IAW SRM 53-2-3 FIGURE 14.

Part: LONGERON — CRACKED (BS 68)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 32R FS 68 CRACKED AND CORRODED. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT LONGERON PER SRM 53-31 FIGURE 2, 51-1-21 AND 51-1-21D.

Part: STIFFENER — CORRODED (RT WING)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING ROOT JUST I/B OF I/B SPOILER T/E VERTICAL STIFFENER IS CORRODED. MAINTENANCE REMOVED, FABRICATED AND INSTALLED A NEW PART IAW SRM 51-1-20D.

Part: ANGLE — CRACKED (RT WING)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND SPAR WEB ATTACH ANGLE CRACKED ON O/B SLOT AREA, RT WING. MAINTENANCE FABRICATED REPLACEMENT ANGLE IAW SRM 54-3-2 AND REMOVED AND REPLACED PER SRM 51-1-20D AND 51-3-0.

Part: FITTING — CORRODED (BS 680)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND ATTACH FITTING FRAME 680 LT, WHERE ATTACHED TO CENTER WING HAS HEAVY CORROSION. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20 AND 51-3-0.

Part: FITTING — CRACKED (BS 1241)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1241 LONG 35R INTERCOSTAL ATTACH FITTING IS CRACKED. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: WEB — CORRODED (BS 860)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND WEB CORRODED AT STA 860, WHERE CENTER WING BOX MEETS WITH W/W PRESSURE PANEL BETWEEN RBL 24, 2ND AND 3RD SEAT TRACK FROM RT SIDE OF FUSELAGE. MAINTENANCE REPAIRED WEB IAW SRM 53-2-0, FABRICATED AND INSTALLED VERTICAL STIFFENER AND END CLIP PER SRM 53-1-0.

Part: INTERCOSTAL — CORRODED (BS 1245)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND INTERCOSTAL, STA 1245 LONG 33R HAS CORROSION AROUND THE NUTPLATE. MAINTENANCE REMOVED, FABRICATED AND REPLACED INTERCOSTAL STA 1245 LONG 33R IAW SRM 53-4-1 AND 51-1-20.

Part: DOUBLER — CORRODED (BS 1240)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1240 LONG 36, INTERNAL DOUBLER BULGED AND CORRODED. MAINTENANCE REPLACED EXTERNAL FUSELAGE SKIN PER DRAWING 5750322, SRM 51-1-21, 51-1-20D, 51-3-0 AND UPS EO DC8-5310-7442A.

Part: SUPPORT — CRACKED (BS 70)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FLIGHT DECK ENTRYWAY, STA 70 RBL 10 FLOOR SUPPORT INTERCOSTAL CRACKED AT AFT END. MAINTENANCE REMOVED ANGLE FABRICATED AND INSTALLED IAW SRM 51-1-21.

Part: LONGERON — CORRODED (BS 721)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 31R BS 721, SEVERELY CORRODED. MAINTENANCE REMOVED DAMAGED LONGERON, FABRICATED AND INSTALLED NEW ONE PER SRM 53-4-1 AND 51-1-21.

Part: FITTING — CORRODED (BS 1230)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND BS 1230 FRAME FITTING LONGERON 33R AND 34R, SEVERELY CORRODED. MAINTENANCE REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SUPPORT — CORRODED (BS 180)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND C1 CARGO COMPARTMENT FLOORBEAM SUPPORT, STA 180 RT CORRODED OUT OF LIMITS. MAINTENANCE FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 51-1-20D.

Part: FLOORBEAM — CORRODED (BS 1580)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FLOORBEAM SEVERELY CORRODED, BS 1580 LBL 45 TO 60. MAINTENANCE REPAIRED IAW EO DC-8-5310-7441A.

Part: FITTING — CORRODED (BS 960)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION ON FITTING BETWEEN UPPER WEB AND SKIN, LT MLG W/W STA 960. MAINTENANCE REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIGURE 8.

Part: SPLICE — CRACKED (BS 1270)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1270 LONG 35R SPLICE FITTING, CRACKED AND CORRODED. MAINTENANCE REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 118)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FWD PIT CORROSION AROUND NUT, LONG 36 STA 118. MAINTENANCE REMOVED THE DAMAGED SECTION, FABRICATED AND INSTALLED LONGERON SPLICE IAW SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 480-500)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG 29L CORRODED AT STA 480 TO 500. MAINTENANCE CUT OUT THE DAMAGED AREA PER SRM 53-2-2 FIGURE 10, SPLICED IN NEW SECTION.

Part: LONGERON — GOUGED (BS 1220)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1220 LONGERON 33R, WEB WAS GOUGED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0. MAINTENANCE COMPLIED WITH EO DC8-5310-7450A, FOR PERMANENT REPAIR.

Part: DOUBLER — CORRODED (BS 120)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FUSELAGE FRAME STA 120 LONG 36, HAS CORROSION UNDER DOUBLER ON FWD SIDE OF FRAME. MAINTENANCE REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PARTS IAW SRM 53-2-0, 51-1-21 AND 51-1-20D.

Part: FRAME — CORRODED (FS 1000)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION AT FS 1000 L31 LT AND L31 RT. AFTER CORROSION REMOVAL, FRAME CAP WAS FOUND TO BE OUT OF LIMITS. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT CAP IAW SRM 51-1-8 AND 51-1-20.

Part: SUPPORT — CRACKED (BS 70)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FLIGHT DECK ENTRY WAY, STA 70 RBL 10 FLOOR SUPPORT INTERCOSTAL CRACKED AT THE AFT END. MAINTENANCE FABRICATED AND INSTALLED REPAIR IAW SRM 51-1-21.

Part: LONGERON — CORRODED (BS 100/120)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FWD PIT, EXFOLIATED AND SURFACE CORROSION ON AND IN LONGERON 34R STA 100 TO 120.

Part: FITTING — CORRODED (FS 782)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND MAIN CABIN EXFOLIATED CORROSION ON BOTTOM OF INTERCOSTAL FWD FITTING, STA 782 LONG 18L. MAINTENANCE REMOVED, FABRICATED AND INSTALLED NEW FITTING IAW SRM 51-1-20D.

Part: FRAME — CORRODED (BS 920)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION ON THE FWD SIDE OF FRAME, STA 920 ABOVE LONG 20L. MAINTENANCE REMOVED SURFACE CORROSION, TREATED AND PRIMED AREA PER SRM 51-1-8.

Part: FRAME — CORRODED (BS 1060)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION, FS 1060 LONG 33R TO 33L. AFTER CORROSION REMOVAL FRAME CAP WAS FOUND TO BE BEYOND LIMITS. MAINTENANCE REMOVED CORROSION, FABRICATED REPAIR PART AND INSTALLED IAW SRM 53-4-1, 53-2-0 AND 51-1-8.

Part: FITTING — CRACKED (BS 204)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FWD PIT LONGERON 28L STA 204 SPLICE CRACKED. MAINTENANCE REMOVED, FABRICATED AND INSTALLED REPLACEMENT SPLICE PER SRM 51-1-20D, 51-1-21 AND 51-1-11.

Part: RIB — CRACKED (WS 6.225)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING L/E RIB AT WS 6.225 CRACKED AT THE AFT LOWER END. MAINTENANCE FABRICATED REPAIR AND INSTALLED IAW SRM 57-2-0 AND 51-1-20D.

Part: FITTING — CORRODED (BS 98)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND SHOVEL FITTING CORRODED AT LONGERON 36 FS 98. MAINTENANCE REMOVED AND REPLACED SHOVEL FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 390)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND SPLICE FITTING CRACKED, STA 390 LONGERON 28L. MAINTENANCE FABRICATED SPLICE FITTING PER SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1740)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON ATTACH FITTING SEVERELY CORRODED AND PITTED, STA 1740 LONG 222. MAINTENANCE REMOVED AND REPLACED IAW SRM 51-3-8 AND 51-1-20A.

Part: LONGERON — CORRODED (BS 1740)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON ATTACH FITTING SEVERELY CORRODED AND PITTED, LONGERON 21L STA 1740. MAINTENANCE REMOVED AND REPLACED FITTING IAW SRM 51-3-8 AND 51-1-20A.

Part: STRINGER — CORRODED (BS 1740)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND STRINGER 22L AT FRAME 1740 CORRODED. MAINTENANCE REMOVED THE DAMAGED STRINGER AND FABRICATED REPLACEMENT STRINGER, LOCATED AND INSTALLED IAW SRM 53-5-1.

Part: STRINGER — CORRODED (BS 1740)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND STRINGER 21L AT STA 1740 CORRODED. MAINTENANCE REMOVED THE DAMAGED STRINGER, FABRICATED REPLACEMENT STRINGER AND INSTALLED IAW SRM 53-5-1.

Part: FRAME FTG — CORRODED (BS 440)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND EXFOLIATED CORROSION ON FWD SIDE OF FRAME FITTING IN MAIN CABIN, STA 440 LONG 21L. MAINTENANCE REMOVED AND REPLACED FITTING PER DCI SRM 51-1-21D AND 51-3-1.

Part: FITTING — CORRODED (FS 1200)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND C-3 FITTING AT LONGERON 33R, FLS 1200 CORRODED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE FITTING IAW SRM 53-1-0.

Part: FITTING — CORRODED (BS 390)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND SPLICE FITTING CORRODED BEYOND LIMITS, LONGERON 32L AT STA 390. MAINTENANCE FABRICATED SPLICE FITTING PER SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1120)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME FITTING CORRODED, STA 1120 WHERE LT FRAME ATTACHES TO THE CUSP. MAINTENANCE REMOVED AND REPLACED FRAME FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: LE RIB — CRACKED (WS 749)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING L/E, STA XFS 749 UPPER L/E RIB CRACKED AT AFT END. MAINTENANCE FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-3-2 AND 51-1-20D.

Part: LONGERON — CORRODED (BS 1160)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1160 LONGERON 27L HAS HEAVY CORROSION. DAMAGED AREA CUT OUT ON NR 297388, INSTALLED REPAIR PARTS IAW DC8-53-1464 AND SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 870)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FINGER DOUBLER CORRODED BS 870 AT LONGERON 31R. MAINTENANCE FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-3-1 FIGURE 1.

Part: LONGERON — CORRODED (BS 27/53)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONGERON 31R HAS EXFOLIATION CORROSION BEYOND LIMITS, BS 27 AND 53. MAINTENANCE REMOVED AND INSTALLED REPLACEMENT SECTION IAW SRM 53-3-1 FIGURE 2, 51-1-21 AND 51-1-21D.

Part: FRAME — CORRODED (BS 1020)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION, FS 1020 LONG 33R TO 33L. AFTER CORROSION REMOVAL FRAME CAP WAS FOUND TO BE BEYOND ALLOWABLE LIMITS. MAINTENANCE REMOVED CAP, FABRICATED REPAIR PART AND INSTALLED IAW SRM 53-4-1 AND 53-2-0 AND INSTALLED CAP IAW SRM 51-1-21.

Part: RIB — CRACKED (RT WING)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING T/E LOWER MOST INBOARD RIB AT WING ROOT, CRACKED AT THE BOTTOM FLANGE. MAINTENANCE REPAIRED IAW SRM 57-2-0 FIGURE 1.

Part: FITTING — CORRODED (BS 680)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND BS 680 FRAME TO CENTER WING TANK FITTING RBL 65 TO 70, HAS HEAVY CORROSION AND CAN BE SEEN FROM CABIN UNDER FLOOR. MAINTENANCE REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 51-1-20.

Part: FITTING — CORRODED (BS 1150)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND BS 1150 FRAME FITTING, LONGERON 33R TO 34R IS SEVERELY CORRODED. REMOVED AND REPLACED FITTING IAW SRM 53-2-0.

Part: RIB — CRACKED (WS 322)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND RT WING L/E AT STA XFS 322.0 THE UPPER L/E RIB, CRACKED AT THE AFT END. MAINTENANCE REPAIRED RIB IAW SRM 57-2-0.

Part: LONGERON — CORRODED (BS 500)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LONG 35 CORRODED BEYOND LIMITS AT FS 500. MAINTENANCE CUT OUT DAMAGED AREA AND INSTALLED REPAIR PARTS IAW SRM 53-2-2, 51-1-20D AND 53-2-2.

Part: FRAME — CORRODED (BS 1420)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME CORRODED AT STA 1420 LONG 33L TO 36. MAINTENANCE REMOVED DAMAGED FRAME, FABRICATED REPLACEMENT SEGMENT AND INSTALLED REPAIR SPLICE IAW SRM 53-4-1.

Part: FRAME — CORRODED (BS 1420)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FRAME CORRODED, STA 1420 LONG 36 TO 34R. MAINTENANCE REMOVED THE CORRODED FRAME SEGMENT AND FABRICATED REPLACEMENT IAW SRM 53-4-1, AND INSTALLED PER SRM 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (BS 754)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 759 LONGERON 19R, INTERCOSTAL TO FRAME ATTACH FITTING CRACKED. MAINTENANCE REMOVED FITTING, RECEIVED AND INSTALLED IAW SRM 51-1-20D AND DRAWING 3379874.

Part: LE RIB — CRACKED (WS 647.5)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT OUTBD WING L/E RIB AT STA XFS 647.5, CRACKED AT THE AFT UPPER END. MAINTENANCE FABRICATED AND INSTALLED NEW REPAIR ANGLES IAW SRM 57-2-0 AND 51-1-21.

Part: SUPPORT — CORROSION (FS 99)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND PRESSURE FLOOR SUPPORT CHORD BS 99 CORRODED BEYOND LIMITS, AT VARIOUS LOCATIONS FROM LBL 70 TO RBL 70. FABRICATED AND INSTALLED NEW CHORD PER SRM 51-1-21.

Part: DOUBLER — CORROSION (FS 45-65)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND COCKPIT SUB FLOOR AT FS 45 TO 65 RBL 16 TO 24, FINGER DOUBLER CORRODED BEYOND LIMITS. REMOVED AND FABRICATED FINGER DOUBLER IAW SRM 53-3-1 AND INSTALLED PER SRM 51-1-21.

Part: FITTING — CORROSION (BS 1160)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FITTING AT FRAME 1160, WHERE IT ATTACHES TO THE CUSP LT SIDE HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-3-0 AND 51-1-20D.

Part: RIB — CRACKED (WS 628.75)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING OUTBOARD L/E RIB AT STA XFS 628.75 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0.

Part: LONGERON — CORROSION (FS 420)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND CORROSION ON LONGERON 34L STA 420. INSTALLED REPLACEMENT LONGERON PER SRM 51-1-21 AND 51-1-20D.

Part: SPLICE FITTING — CORROSION (BS 1270)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND FS 1270 LONG 34L, SPLICE FITTING CORRODED BEYOND LIMITS. INSTALLED NEW FITTING AT STA 1270 LONG 34L IAW SRM 51-1-20D.

Part: FITTING — CORROSION (BS 460)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND EXFOLIATED CORROSION ON AFT SIDE OF FRAME FITTING, LONGERON 21L STA 460. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: SKIN — CRACKED (RT HORZ STAB)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND SKIN CRACKED AND APPEARS TO HAVE CORROSION O/B L/E AT I/B END OF RT HORZ STAB. INSTALLED REPAIR PER SRM 55-2.

Part: DOUBLER — CORROSION (FS 25-45)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND COCKPIT SUB FLOOR AT FS 25 TO 45 RBL 16 TO 24, FINGER DOUBLER CORRODED BEYOND LIMITS. REMOVED AND FABRICATED NEW FINGER DOUBLER IAW SRM 53-3-1 AND 53-1-0, INSTALLED DOUBLER IAW SRM 51-2-21.

Part: FRAME — CORROSION (BS 220)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND EXFOLIATION CORROSION ON LWR FLANGE OF FRAME STA 200 LONG 35L. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS PER DC8 SRM 53-2-0. TREATED AREA, FABRICATED AND INSTALLED REPAIR PARTS PER DC8 SRM 53-2-0, 53-2-0 FIG 2 AND 51-1-21.

Part: SPLICE FITTING — CORROSION (BS 1270)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND SPLICE FITTING CORRODED BEYOND LIMITS, STA 1270 LONG 34R. REPLACED SPLICE FITTING, STA 1270 LONG 34R IAW SRM 51-2-20D.

Part: FITTING — CORROSION (FS 35)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND STA 35 AT RT CUSP FRAME TO CUSP TIE FITTING HAS HEAVY CORROSION AROUND FASTENER HOLE. REMOVED AND INSTALLED NEW FITTING IAW SRM 51-1-21 AND 51-3-0.

Part: SKIN — CORROSION (WS 765-766)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING L/E LOWER SKIN STA XFS 765.0 TO 766.5 HAS EXFOLIATION AND INTERGRANULAR CORROSION. FABRICATED DOUBLER AND INSTALLED IAW SRM 57-20, 51-1-21.

Part: LE RIB — CRACKED (WS 448.581)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING L/E RIB AT STA XS 448.581 IS CRACKED AT THE AFT UPPER END. REPAIRED CRACKED IAW SRM 51-2-0.

Part: LE RIB — CRACKED (WS 442.185)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND LT WING L/E RIB AT STA XS 442.185 IS CRACKED AT THE AFT UPPER END. REPAIRED CRACK IAW SRM 57-2-0.

Part: RIB — CRACKED (HORIZ STAB)

WHILE IN FOR D-CHECK, MAINTENANCE FOUND I/B RIB CRACKED ON I/B LEADING EDGE OF RT HORIZ STAB. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 55-2-0.