N880UP

Part: CONTROL VALVE — DEFECTIVE (LT AC PACK)

INSPECTION TYPE:N/A BTB - WHEN STARTING NR 2 ENGINE ON PUSHBACK, DUCT OVERHEAT LIGHT ILLUMINATED, FOLLOWED BY PACK TRIP LIGHT ILLUMINATING, FOLLOWED BY SMOKE IN THE COCKPIT. SUPPLY DUCT LEAKING AT CLAMP IN FWD ACC. DEFERRED LT PACK PER MEL 21-38-1. DMP C/W M393740 ASSIGNED. REMOVED & REPLACED LT PACK SHUTOFF FLOW CONTROL VALVE IAW AMM 21-55-05-4. OPS CHECK NORMAL. THIS CLEARS M393740.

Part: ACTUATOR — FAILED (PITCH TRIM)

EMERGENCY DECLARED. PITCH TRIM FAILED IN EXTENDED POSITION IN FLIGHT. R&R PTC ACTUATOR PER MM 27-30-07-2

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 70,904 hrs · 27,826 cycles

INSPECTION TYPE:SP COMPLY WITH ATTACHED WAN NR 1421616 REGARDING CRACK ON L24L. NDT'D NEW CRACKS AND STOP DRILLED, INSTALLED REPAIR DOUBLER AND TAPERED SHIMS IAW SRM, EA 008-10-01-A1544, 51-1-20D, 51-1-8, UPS EO M-5100-27 80-E.

Part: BATTERY PACK — UNSERVICEABLE (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS UNSERVICEABLE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ASSY IAW AMM 33-50-01-02 AND FOUND SERVICEABLE.

Part: PANEL — CORRODED (LT WING)

LT WING PANEL CORROSION. REMOVED DAMAGED SKIN. ACCOMPLISHED STEPS 1-6 OF EO DC8-5720-29785 APPENDIX A. ACCOMPLISHED REPAIR STEPS 1-9 OF EO DC8-5720-29785-A.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTING SYSTEM INOP. REPLACED EMERGENCY LIGHT BATTERY PACK AND OPS CHECKED AS PER DC8 MM 33-50-01-2. OPS CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

ON PREFLT, FOUND EMERGENCY EXIT LTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK PER UPS AMM 33-50.

Part: LATCH — BROKEN (EVAC SLIDE)

INSPECTION TYPE:N/A EMERGENCY ESCAPE SLIDE HAS BROKEN LATCH. SLIDE INOP FOR CREW ENTRY DOOR. DEFERRED CREW ENTRY DOOR SLIDE PER MEL 52-7-4. SLIDE IS SECURED IN SUITCASE. REMOVED SLIDE COVER AND ROUTED TO SHEET METAL. REMOVED AND REPLACED LATCH REF DCI SRM 51-01-21. REINSTALLED ORIGINAL SLIDE INTO CONTAINER AND INSTALLED ON DOOR REF MM 25-60-01-2. M369243 CLEARED.

Part: STRUCTURE — MISSING (LT WING)

APPROX 3/8 BY 1 INCH PIECE OF SHEETMETAL MISSING ON T/E OF WING. LOCATED ON LT WING INBD OF NR 3 SPOILER PANEL. ACCOMPLISHED EO DC8-5730-28460A.

Part: SKIN — CHAFED (LT WING SPOILER)

LEFT WING INBOARD LATERAL CONTROL SPOILER LOWER SURFACE IS CHAFFED ALONG T/E. INSTALLED NEW SPOILER ASSEMBLY IAW DC8 AMM 27-61-01-2, PARAGRAPH 3B STEPS 1 THROUGH 6.

Part: FAN — FROZEN (LAV/CABIN)

DIVERSION, CREW SMELLED SMOKE IN CABIN. DISCHARGE HAND EXTINGUISHER IN LAV, CREW REPORTED LAV PUMP WAS TURNING. PARKED FOR FAA EVALUATION. FOUND RECIRCULATING FAN FROZE UP. REMOVED AND REPLACED IAW AMM 21-1-01-2. OPS CHECK GOOD. INSPECTED SURROUNDING AREA AND FOUND NO OTHER DEFECTS OR DAMAGE. A/C OK FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT FAILED PREFLIGHT TEST. REPLACED BATTERY AND RELAY UNIT W/REF M/M 33-50-01-2, OPS TEST GOOD.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT FAILED PREFLIGHT TEST. REPLACED BATTERY AND RELAY UNIT W/REF M 33-50-01-2, OPS TEST GOOD.

Part: ENGINE — FLAMED OUT (NR 4) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:N/A ATB - NR 4 ENGINE FLAMEOUT CLIMBING THROUGH 30,000FT. NOTICED FUEL PUMP IN OFF POSITION. RAN ENGINE FLAMEOUT CHECK LIST AND ENGINE RESTARTED. ALL INDICATIONS NORMAL FOR REMAINDER OF FLIGHT. PERFORMED NEG PRESSURE CHECK ON NR 4 ENG. FUEL FEEDLINES PRESSURE CHECK GOOD. FUEL STICKED TANKS, ALL READINGS NORMAL IAW MM 28-22-12-2. RESTART ENGINE NORMAL. REMOVED NR 4 ENG FUEL FILTER, NO CONTAMINATION. REMOVED AND REPLACED CFE BOOST PUMP NR 4 ENG, OPS CHECK GOOD IAW 73-10-01-2. REMOVED AND REPLACED NR 4 TANK SELECT VALVE. FOUND 6" X 12" RAG IN FUEL SUPPLY TUBE. REMOVED RAG. ENG RUN NORMAL, ALL CHECKS GOOD IAW 71-00-00-0.

Part: SKIN — CORRODED (FS 1640 L33R) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 EXFOLIATED CORROSION UNDER L33R AT STA 1620. REPAIRED SKIN AND FINGER DOUBLER AT STA 1620 L33R IAW SAA EA 008- 5330-00-A0885, UPS RAA DC8-53-20632, AND FAA FORM 8100-9.

Part: FITTING — CRACKED (FS 1690 L34R) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 END FITTING CRACKED AT STA 1690 L34R, 2.5 INCHES AT BARREL NUT HOLE. REMOVED CRACKED END FITTING AT STA 1690 L34R IAW SRM 51-01-20D. LOCATED, DRILLED UP, AND INSTALLED END FITTING AT STA 1690 L34R IAW SRM 51-03-02, AND SRM 51-01-20D.

Part: FRAME — GOUGED (FS 240 L31R) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 A-PIT, BELT FRAME GOUGED AT STA 240 L31R. TRIMMED OUT DAMAGED AREA AT STA 240 L31R IAW E0 DC8-5310-11728-B, FABRICATED AND INSTALLED REPAIR DOUBLER IAW EO DC8-5310-11728-B.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 L33R SPLICE BETWEEN STA 1640-1660 CRACKED. REMOVED AND REPLACED LONGERON SECTION FROM STA 1640-1660 L33R IAW SRM 51-01-20D, 51-1-21, AND 51-3-2.

Part: SKIN — CANNING (LT ELEVATOR) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 L/ELEVATOR UPPER SKIN ON INBD SIDE HAS DINGS AND SKIN HAS OIL CANNING. CUT OUT DAMAGED SKIN ON L/ELEVATOR AT STA XE 57.5 IAW SRM 55-02-01-0, FABRICATED, BONDED FINGER DOUBLER, AND INSTALLED REPLACEMENT SKIN ON L/ELEVATOR AT STA XE 57.5 IAW DWG 5654970, AND SRM 55-2-1 FIG 11.

Part: PRESSURE PANEL — MISREPAIRED (FS 863) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 VISUAL INSP OF PRESSURE WEB AT STA 863 RBL 42-48, FOUND DOUBLER TO BE TAPERED ON ENDS, WITH NO TAPERED SHIMS INSTALLED, REF: EO DC8- 5310-22195-B. INSTALLED CORRECT REPAIR AT STA 863 RBL 42-48 IAW SAA EA 008-5310- 01-A0841, UPS EO DC8-5310-22195-C, AND FAA FORM 8100-9.

Part: SKIN — CRACKED (FS 1690 L32L) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 FS 1690 L32L HAS A 1 INCH CRACK AND EXISTING REPAIR DOUBLER AT L30L SRM REPAIR WILL NOT BE INCOMPLIANCE WITH EO DC8-5330-20248. CUT OUT DAMAGED AREA AT STA 1690 L32L IAW SRM 53-2-0. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLERS, AND FILLERS AT STA 1690 L30L -L34R IAW UPS EO DC8-5330-20248, AND SRM 53-02-01 FIG 7.

Part: RIB — CRACKED (LT WING) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 LEFT WING CENTER RIB CRACKED AT XFS 409. STOP DRILLED CRACK. FABRICATED AND INSTALLED DOUBLER IAW SRM 57-02-00 51-1-21, AND 51-1-20D.

Part: DOUBLER — CRACKED (RT WING) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 CRACK ON INTERNAL DOUBLER ON RIGHT WING CENTER LEADING EDGE UPPER SURFACE I/B EDGE OF SLOT DOOR. REMOVED INTERNAL DOUBLER ON RIGHT WING CENTER LEADING EDGE IAW SRM 51-1-21. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIGHT WING LEADING EDGE IAW DWG 5718963-236, AND SRM 51-3-2.

Part: RIB — CRACKED (LT WING) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 LEFT WING CENTER L/E UPPER RIB CRACKED AT XFS 484. STOP DRILLED CRACK IAW SRM 57-02-00. FABRICATED AND INSTALLED 2 DOUBLERS IAW SRM 57-02-00, 51-1-21, AND 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 MAIN CABIN, CORROSION ON BELTFRAME END FITTING, STA 220 L21R. REMOVED AND REPLACED BELTFRAME FITTING AT STA 220 L21R IAW SRM 51-1-20D, AND SRM 51-3-0.

Part: SKIN — MISREPAIRED (FS 1746 L26-30R) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 L28R AT FS 1746 HAS 2 EA EXISTING REPAIR DOUBLERS UPPER AND LWR OF L28R, NOT IN COMPLIANCE WITH EO DC8-5330-20248 NOR DWG SRO8530032. REPAIRED FUSELAGE TAIL SECTION SKINS AT STA 1746, L28R - L30R IAW SAA EA 008-5330-01-A0854, UPS EO DC8-5330-26800-A, AND FAA FORM 8100-9.

Part: RIB — CRACKED (LWS 591) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 LT WING OUTBD L/E RIB CRACKED AT XFS 591. NDT VERIFIED CRACK ENDS AT FASTENER HOLE IAW NDSPM 06-10-01-001. FABRICATED AND INSTALLED REPAIR ANGLE AT LT WING OUTBD L/E STA XFS 591 IAW SRM 57-03-03 FIG 6.

Part: BULKHEAD — CRACKED (FS 1766) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 AFT PRESS BULKHEAD CRACKED AT STA 1766 L10L, LBL 25 AND LBL 35. CUT OUT DAMAGED AREA AT STA 1766 LBL 25 AND LBL 35 IAW SRM 53-2-5 FIG 14A. FABRICATED AND INSTALLED REPAIR FILLERS, AND DOUBLERS AT STA 1766 LBL 25 AND LBL 35 IAW SRM 53-2-5 FIG 14, AND TR 53-194. THIS REPAIR REQUIRES DAMAGE TOLERENCE INSP WITH INITIAL AT 4,000 LANDINGS & REPETITVE INSP AT EVERY 4000 LANDINGS THERE AFTER PER TR 53-194.

Part: ATTACH ANGLE — CRACKED (FS 1766 L16L) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD TO L16L ATTACH ANGLE CRACKED AT STA 1766. REMOVED ATTACH ANGLE AT STA 1766 L16L IAW SRM 51-1-21. FABRICATED AND INSTALLED INTERCOSTAL CLIP AT STA 1766 L16L IAW DWG NR 5773844, AND SRM'S 51-1-20D, 51-3-2.

Part: RIB — CRACKED (LWS 798) · airframe 70,263 hrs · 27,365 cycles

C3 LT WING OB LE RIB CRACKED AT XFS 798. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SRM 57-07-00, 57-02-00, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (LWS 804) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 LT WING OB LE RIB CRACKED AT XFS 804. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2 REPAIR ANGLES IAW SRM 57-02-00, 51-01-21 AND 51-1-20D.

Part: RIB — CRACKED (LWS 876) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 LT WING OB LE CRACKED AT XFS 876. STOP DRILLED CRACK. FABRICATED AND INSTALLED 2. REPAIR ANGLES IAW SRM 57-02-00, 51-1-21 AND 51-1-20D.

Part: BULKHEAD — CRACKED (FS 1766 L10R) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 AFT PRESS BULKHEAD CRACKED 2 AREAS AT STA 1766 L10R, RBL 25 AND RBL 35. CUT OUT DAMAGED AREA AT ST 1766 L10R, RBL 25 AND RBL 35 IAW SRM 53-02-05 FIG 14A. FABRICATED & INSTALLED REPAIR DOUBLERS, & FILLERS AT STA 1766 L10R IAW SRM 53-02-05 FIG 14 AND TR 53-194. THIS REPAIR REQUIRES DAMAGE TOLERANCE INSP WITH INITIAL AT 4,000 CYCLES AND REPEAT INSP AT EVERY 4,000 CYCLES THERE AFTER IAW TR 53-194.

Part: LONGERON — CRACKED (FS 869 L24L) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 L24L 12 INCHES AFT OF BARREL NUT STA 869 CRACKED: VIEWED FROM TOP OF WING. STOP DRILLED CRACKED L24L AT STA 869 IAW SRM 53-2-2 VIEW G. STOP DRILLS TERMINATE CRACKS PER HFEC NDTS 06-10-01.001. FABRICATED AND INSTALLED -3, -5 DOUBLERS, -7, -9 REPAIR ANGLES, AND FILLERS AT STA 869 L24L IAW SRM 53-2-2 FIG 5, AND SRM TR 53-123 GEN NOTE 4.

Part: RIB — CRACKED (LWS 609) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 LT WING OUTBD L/E RIB CRACKED AT STA XFS 609. NDT VERIFIED CRACK TERMINATES AT FASTNER HOLE IAW NDSPM 06-10-01-001. FABRICATED AND INSTALLED REPAIR ANGLE AT L/WING L/E RIB STA XFS 609 IAW SRM 57-03-03 FIG 6.

Part: SKIN — CANNING (RUDDER) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 LEFT RUDDER SKIN OIL CANNING AT STA ZR 185. REPAIRED LEFT RUDDER SKIN AT STA ZR 185 IAW SAA EA 008-2720-01-A0856 DAC DWG 5655077 REV-S, AND FAA FORM 8100-9.

Part: SKIN — CORRODED (FS 310 L2R) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 FUSELAGE EXTERIOR SKIN CORRODED AT FS 310 L2R. CUT OUT DAMAGED AREA AT STA 310 L2R IAW SRM 53-02-01 FIG 7. FABRICATED AND INSTALLED REPAIR DOUBLER, FINGER DOUBLER, AND FILLER AT STA 310 L2R IAW SRM 53-02-01 FIG 7.

Part: SKIN — GOUGED (FUSELAGE) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 FUSELAGE EXTERIOR SKIN GOUGED AT STA 140 L22L. REPAIRED FUSELAGE SKIN AT STA 140 L22L IAW SAA EA 008-5330-01-A0849 UPS EO DC8-5330-26786-A, DOUGLAS DWG SRO8530027.

Part: SKIN — GOUGED (FS 520 L31R) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 FUSELAGE EXTERIOR EXISTING REPAIR DOUBLER HAS DEEP GOUGE AND FASTENER HEADS MISSING AT STA 520 L31R. REMOVED DAMAGED DOUBLER AND CUT OUT AREA AT STA 520 L31R IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLERS AT STA 520 L31R IAW SAA EA 008-5330-01-A0847, UPS RAA DC8-53-20626, AND FAA FORM 8100-9.

Part: SKIN — MISREPAIRED (FS 1400 L27R) · airframe 70,263 hrs · 27,365 cycles

INSPECTION TYPE:C3 REMOVE STEEL DOUBLER FROM THE C-4 (D-PIT) UPPER FWD CORNER AND REPAIR PER SRM 53-2-0 FIG 21. REMOVED AND REPLACED DOUBLER AT C-4 (D-PIT) UPPER FWD CORNER IAW SRM 53-02-00 FIG 21, AND SRM TR 53-140, & 53-188, THIS REPAIR REQUIRES AN MPI WITH INITIAL INSPECTION AT 14000 LANDINGS, & REPETITIVE INSP AT EVERY 4400 LANDINGS IAW TR 53-188.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A ON EMERGENCY EXIT LIGHTS TEST, NO LIGHTS WOULD OPERATE. STANDBY INSTRUMENTS OK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY POWER PACK ASSY & SYS. OPS CHECKED NORMAL IAW MM 33-50-01-2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK IAW 33-50-01-2.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT)

EMERGENCY LIGHTS DO NOT TEST. REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT)

INSPECTION TYPE:NA EMERGENCY EXIT/DISARM LIGHT INOP. RELAMPED, OPS CHECKED GOOD.

Part: FAN — MALFUNCTIONED (COCKPIT)

SMOKY ODOR NOTICED AT TOP OF DESCENT. SMOKE APPEARED WHEN DESCENDING THROUGH 18000'. AFTER FUMES EVACUATION PROCEDURE SMOKE DISSIPATED. SMELL RECURRED AT ABOUT 5000'. COCKPIT AND GALLEY AREA SMELL OF SMOKE AFTER SHUTDOWN. DEFERRED M324868. REMOVED AND REPLACED RECIRCULATION FAN IAW DC8 21-21-01 RECIRCULATING FAN OPERATES CHECKS NORMAL. THIS CLEARS M324868, PLACARD REMOVED.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS)

EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER DC8 MM 33-50-00. OPS CK GOOD.

Part: CASE — LEAKING (HYD SYSTEM)

INSPECTION TYPE:N/A EMERGENCY DECLARED, NR 3 ENGINE HYDRAULIC CASE DRAIN FILTER DUE INSPECTION DUE TO LOSS OF HYDRAULIC PRESSURE. LANDED UNEVENTFUL AND TOWED TO RAMP TWO. REMOVED AND REPLACED NR 3 ENGINE HYDRAULIC CASE DRAIN FILTER IAW MM 29-1 0-15-2, FILTER WAS CLEAN, LEAK CHECK DUE. LEAK CHECK OF NR 3 ENG HYDRAULIC CASE DRAIN FILTER OK IAW MM 29-10-00.

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE: C1, FOUND CORROSION AT AFT MANUFACTURING SPLICE 6 O`CLOCK. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-1 FIG 7, 53-5-3 FIG 1, 51-1-20D, AND 51-1-21.

Part: PRESSURE PANEL — CORRODED (RT MLG WW) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 CORROSION ON RT W/W CEILING AT STA 863 RBL 42 AND 48 UNDER LONGERONS, ON WEB, AND DOUBLER IN MAIN CABIN IS BULGED. CUT OUT CORROSION, FABRICATED AND INSTALLED REPAIR IAW SAA SK 880-7620 56 AND EO DC-8-5310-22195-A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 C-PIT DOOR STOP FWD SIDE BANANA FITTING CRACKED AT STA 1180 L26L. REMOVED AND REPLACED BANANA FITTING IAW DC-8 SRM 51-1-20D, 51-1-21, AND 51-1-20A.

Part: FITTING — CORRODED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 LONGERON SPLICE FITTING HAS HEAVY CORROSION AT STA 1270 L35R. REMOVED AND REPLACED LONGERON SPLICE FITTING IAW DC-8 SRM 51-1-20D.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 B-PIT BETWEEN STA 480-460 L31L SPLICE FITTING CRACKED. REMOVED CRACKED SPLICE FITTING, FABRICATED REPLACEMENT FITTING IAW DWG 3750257, AND INSTALLED IAW DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 673 L8L. REMOVED AND REPLACED LONGERON END FITTING IAW DC-8 SRM 51-1-20D AND 51 -1-21.

Part: BRACE — CORRODED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 FLOORBEAM & BRACE APPEAR HEAVILY CORRODED IN COCKPIT SUBFLOOR AT FWD PRESSURE WEB STA -129 LBL 33. REMOVED FLOORBEAM BRACE, FABRICATED REPLACEMENT FLOORBEAM BRACE IAW DWG 5597992, AND INSTALLED IAW DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 C-PIT DOOR CUTOUT BANANA FITTING CRACKED AT STA 1160 L32R. REMOVED AND REPLACED BANANA FITTING IAW DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 INSIDE DOOR 62 POGO STICK FITTING CRACKED .5 INCH LONG AT STA 1875 L36. REMOVED AND REPLACED POGO STICK FITTING IAW DC-8 SRM 51-1-20D AND 51-3 -0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 CRACKED FLOORBEAM FITTING AT A-PIT DOOR JAMB AT FS 340. REMOVED CRACKED FLOORBEAM FITTING, FABRICATED REPLACEMENT IAW DWG 975 4022, AND INSTALLED IAW DC-8 SRM 51-1-20D.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE: C1, SEVERE CORROSION ON FRAME/ANGLE AT FS 380 (LONGERON) LBL 33. REMOVED CORROSION ON LONGERON AND FOUND OUT OF LIMITS IAW DC-8 SRM 51-1-8. INSTALLED LONGERON SPLICE FITTING IAW DC-8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 A CARGO DOOR CUTOUT LOWER AFT BANANA FITTING HAS .5 INCH CRACK. REMOVED AND REPLACED BANANA FITTING IAW DC-8 SRM 51-1-20D.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 MAIN CABIN CENTER WING BOX SUBFLOOR FINGER DOUBLER HAS SHEAR HEAD FASTENERS AND POSSIBLE CORROSION UNDER THE DOUBLER AT STA 915 BL 0. REMOVED FINGER DOUBLER AND FOUND OUT OF LIMITS. CENTER WING BOX PRESSURE WEB FOUND WITHIN LIMITS AFTER CORROSION REMOVAL. FABRICATED REPLACEMENT FINGER DOUBLER IAW DWG 5645332 AND INSTALLED IAW DC-8 SRM 51-1-21.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 MAIN CABIN CENTER WING BOX FINGER DOUBLER HAS SEVERAL SHEAR HEAD FASTENERS AND POSSIBLE CORROSION UNDER THE DOUBLER AT STA 865 BL 0. REMOVED FINGER DOUBLER AND FOUND OUT OF LIMITS, CENTER WING BOX PRESSURE WEB FOUND IN LIMITS AFTER CORROSION REMOVAL. FABRICATED REPLACEMENT FINGER DOUBLER IAW DWG 5645332, AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-21, AND DWG 5645332.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 LONGERON CRACKED .5 INCH LONG AT STA 1746 L5R. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE: C1, MAIN CABIN FRAME TO CUSP FITTING HAS HEAVY CORROSION AT STA 1580 L21L. REMOVED AND REPLACED CUSP FITTING AT STA 1580 L21L IAW DC-8 SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 A CARGO DOOR CUTOUT LOWER FWD BANANA FITTING CRACKED. REMOVED AND REPLACED BANANA FITTING IAW DC-8 SRM 51-1-20D AND 51-3-2.

Part: FITTING — CORRODED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 MAIN CABIN CENTER WING BOX AT STA 879.375 L20L SIDE FRAME FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED STA 879 FUSELAGE FRAME FITTING IAW DC-8 SRM 51-1-20D AND 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 LONGERON CRACKED 1 INCH LONG AT STA 1746 L15L AND STA 1726 L15L. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTINGS IAW DC-8 SRM 53-2-2 FIG 10 AND 51-3-2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 MAIN CABIN STA 1180 L20R FRAME ATTACH FITTING CRACKED .5 INCH LONG. REMOVED AND REPLACED FITTING IAW DC-8 SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 LONGERON 15R CRACKED 1 INCH LONG AT STA 1757. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D.

Part: ANGLE — CORRODED (MAIN CARGO DOOR) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 MAIN CARGO DOOR UNDER THRESHOLD 17 INCHES FWD OF AFT CUTOUT LWR ANGLE ATTACH JUST FWD OF AFT LATCH SPOOL HAS EXFOLIATION CORROSION. REMOVED AND REPLACED ANGLE IAW DC-8 SRM 51-1-21 AND 51-3-0.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 LONGERON CRACKED .5 INCH LONG AT STA 1746 L16L. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 MAIN CABIN AT STA 1280 L18R FRAME ATTACH FITTING CRACKED .5 INCH LONG. REMOVED CRACKED FITTING, FABRICATED REPLACEMENT FITTING IAW DWG 475041 9, AND INSTALLED IAW DC-8 SRM 51-1-20D.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 MAIN CABIN AT STA 1160 L19R FRAME ATTACH FITTING CRACKED .5 INCH LONG. REMOVED AND REPLACED FRAME ATTACH FITTING IAW DC-8 SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 RIGHT LONGERON 16R CRACKED 2 INCHES LONG AT STA 1756. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 MAIN CABIN AT STA 1160 L18R FRAME ATTACH FITTING CRACKED 1 INCH LONG. REMOVED AND REPLACED FRAME ATTACH FITTING IAW DC-8 SRM 51-1-20D.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 MAIN CABIN STA 1230 L18R FRAME ATTACH FITTING .5 INCH CRACK. REMOVED CRACKED FITTING, FABRICATED REPLACMENT FITTING IAW DWG 4750419, AND INSTALLED IAW DC-8 SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 LONGERON 14R CRACKED .25 INCH LONG AT STA 1757. REMOVED AND REPLACED LONGERON SECTION AND INSTALLED SPLICE FITTING IAW DC-8 SRM 53-2-2 FIG 10 AND 51-1-20D.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE:C1 MAIN CABIN FLOORBEAM HEAVY CORRODED AT STA 1700 RBL 34. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 FIG 1F. FABRICATED AND INSTALLED FLOORBEAM REPAIR IAW DC-8 SRM 53-2-0 FIG 1G, 51-1-20D, AND 51-3-0.

Part: RIB — CRACKED (RH XFS) · airframe 69,301 hrs · 26,662 cycles

INSPECTION TYPE: C1, RT WING L/E UPPER RIB CRACKED 1 INCH LONG AT XFS 841.25. REPAIRED IAW DC-8 SRM 57-3-3 AND SRM 51-1-21.

Part: PUMP — LEAKING (HYD SYSTEM)

NR 3 ENGINE HYDRAULIC LEAK. TROUBLESHOT & FOUND PT LEAKING IN NR 3 ENG PYLON & LEAKING INTO DRAIN LINES, TO DRAIN MAST. REMOVED AND REPLACED PART. OPS CK'D GOOD, LEAK CK'D GOOD, PERFORMED ENG RUN, & HYD SYS OP'S OF FLIGHT CONTROLS. SVC'D HYD RES PER MM 12-00-00.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS WILL NOT CAME ON. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-01-2. ALL OPS CHECK NORMAL.

Part: ENGINE — FLAMED OUT (NR 1)

NR 1 ENGINE FLAMED OUT AT TOP OF DESCENT WHEN POWER REDUCED. ENGINE READINGS WERE NORMAL W/ WINDMILLING RPM OF 22 PERCENT N2. RESTART AT FL 200 WAS NORMAL. T/S IAW MM 71-00-00 FAULT 51 GEN. INSP CK FLT IDLE, SPECIFIC GRAVITY SETTING. MAGNETIC CHIP DETECTORS & FUEL FILTER. NO DEFECTS. CLEANED PAINT & PAINT STRIPPER OFF CDP TUBE DRAIN HOLES. RAN ENGINE TO MAX PWR . OPS WERE NORMAL

Part: ENGINE — FLAMED OUT (NR 1)

UPON THROTTLE REDUCTION TO IDLE FOR DESCENT FROM FL 370 M .80, NR 1 ENGINE FLAMED OUT. ENG READINGS WERE NORMAL WITH WINDMILLING RPM OF 22 PERCENT N2. RESTART AT FL300 WAS NORMAL. T/S IAW MM 71-00-00 FAULT 51 GENERAL INSP, CK FLT IDLE, SPECIFIC GRAVITY SETTING, MAGNETIC CHIP DETECTORS AND FUEL FILTER. NO DEFECTS WERE NOTED. CLEANED PAINT & PAINT STRIPPER OFF OF CDP TUBE DRAIN HOLES. RAN ENGINE TO MAX POWER, OPS WAS NORMAL.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE: C2, INSIDE 60 PANEL STA 1766 AFT SIDE SHEAR TIE ABOVE LONG 9R IS CRACKED. CUT OFF CRACKED SHEAR TIE, FABRICATED SHEAR TIE AND INSTALLED IAW SRM 53-2-0 FIG 2A.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE: C2, AFT FUSELAGE SECTION APPROX STA 1500 AT LONG 25L TO 26L EXISTING DOUBLER HAS BLIND FASTENERS. REMOVED BLIND FASTENERS, FOUND SKIN BULGED AND DRILL STARTS OUT OF LIMITS AT STA 1505 AT LONG 26L. CUT OUT DAMAGED SKIN, NDT VERIFIED NO CRACKS AT CUTOUT. REMOVED, FABRICATED AND INSTALLED LONGERON SECTION, DOUBLER, FILLER, FINGER DOUBLERS AND INSTALLED LONGERON SPLICES IAW SRM 53-2-2 FIG 10 AND 53-2-1 FIG 7.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE: C2, BLENDOUT JUST BELOW CUSP LINE AT STA -67 IS BEYOND LIMITS. CUT OUT DAMAGED SKIN, FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLER IAW SRM 53-2-1 FIG 7.

Part: FITTING — CRACKED (LEFT WING TANK) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE: C2, NR 2 MAIN FUEL TANK HAS STRINGER END FITTING CRACKED AT OUTBOARD SIDE OF XRS 50 AT STRINGER 51. REMOVED, FABRICATED AND INSTALLED FITTING IAW DWG 3704841 AND SRM 51-1-20D.

Part: SKIN — CORRODED (FUSELAGE) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE: C2, FUSELAGE SKIN EXTERNAL MATING SURFACE FOR MARKER BEACON ANTENNA HAS CORROSION STA 660-680 LONG 35L TO 36. REMOVED CORROSION, NDT VERIFIED CORROSION. REMOVED IN AREA, FABRICATED AND INSTALLED DOUBLER IAW SAA SK 880-356.

Part: FITTING — CORRODED (FUSELAGE) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE: C2, LONGERON 24L HAS A FITTING CORRODED BEYOND LIMITS AT STA 920. REMOVED AND REPLACED FITTING, FABRICATED AND INSTALLED SPLICES, DOUBLERS AND FILLERS IAW SRM 53-2-0 FIG 8 AND DWG 5753113.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE:C2, 1 EA FASTENER PULLED THRU STRAP ON INTERCOSTAL AT STA 1135 LT SIDE AT LONG 35L. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATED CRACK. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-0 FIG 23.

Part: FITTING — CRACKED (HORIZONTAL STAB) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE: C2, RT STAB I/B LEADING EDGE ANGLE FITTING IS CRACKED AT XRS 0. REMOVED AND REPLACED FITTING IAW DWG 3701427 AND SRM 51-1-20D, 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE: C2, LONG 17R AND END FITTING ARE CRACKED AT STA 1766. REMOVED, FABRICATED AND REPLACED LONGERON 17R AND END FITTING IAW DWG 5649327 AND 4772397 AND SRM 51-1-20D, 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE: C2, LONGERON 17L AND END FITTING ARE CRACKED AT STA 1766. REMOVED LONGERON AND END FITTING, FABRICATED LONGERON IAW DWG 5649327. REPLACED FITTING AND INSTALLED LONGERON IAW DWG 4772397 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CARGO BAY) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE:C2 LONG 31L SPLICE FITTING IS CRACKED AT STA 600-640. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE:C2 LT UPPER HORIZONTAL STAB MOST I/B SKIN SURFACE IS CORRODED AT STA XE 29.812. REMOVED, FABRICATED AND REPLACED SKIN PANEL ASSY BETWEEN XE 29.812 AND XE75.62 IAW DWG 5651747,8110-3 APPROVED SAA SK 880-658, UPS ENGINEERING FILE NUMBER DC8-55-20012 AND SRM 51-1-21.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE: C2, LT UPPER HORIZONTAL STAB SKIN IS CRACKED AND CORRODED AREAS MARKED BETWEEN XE 77 TO XE 99.879. REMOVED, FABRICATED AND REPLACED SKIN PANEL ASSY BETWEEN XE 75.672 TO XE149 IAW DWG 5651747, 8110-3 APPROVED SAA SK 880-658, UPS ENGINEERING FILE NUMBER DC8-55-20012 AND SRM 51-1-21.

Part: RIB — CRACKED (LT WING LE) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE: C2 LEFT WING L/E LOWER RIBS ARE CRACKED AT FASTENER END AT XFS 616.25 AND XFS 622.5 FWD OF PANEL OPENING. STOP DRILLED CRACKS, NDT VERIFIED STOP DRILLS TERMINATED CRACKS. FABRICATED AND INSTALLED DOUBLERS IAW SRM 57-2-0 FIG 2.

Part: SKIN — CORRODED (LEFT WING LE) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE:C2 LEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION BETWEEN XFS 766.25 TO XFS 772.5. CUT OUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED FILLERS AND DOUBLER IAW SRM 57-2-1 FIG 38.

Part: SHAFT — CORRODED (EMERG EXIT HANDL) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE: C 2, LEFT OVERWING EMERGENCY EXIT DOOR HANDLE AFT LATCH SHAFT FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 2702833 AND SRM 51-3-0.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 68,460 hrs · 25,963 cycles

INSPECTION TYPE: C2, SHEAR TIE IS CRACKED AT STA 640 BETWEEN LONG 26L AND 27L. REMOVED SHEAR TIE SPLICE, FABRICATED AND INSTALLED SPLICE IAW SRM 53-2-0 FIG 2B.

Part: DOOR — DAMAGED (NLG DOOR)

INSPECTION TYPE: PFLT, RT FUSELAGE NOSE W/W BELOW VENT DOOR SHEET METAL REPAIR. FERRIED TO TCO. REMOVED DAMAGE IAW DC8 SRM 51-1-21,OUT OF LIMITS IAW DC8 SRM 53-2-0. HEAT TREATED SPLICE CHANNEL & REPAIR SPLICE FABBED SPLICE CHANNEL & REPAIR SPLICE IAW DC8 DWG 5613861 & DC8 SRM 53-2-0, OK TO ALODINE. ALODINED SPLICE CHANNEL & REPAIR SPLICE IAW DC8 SRM 51-1-8. PRIMED SPLICE CHANNEL & REPAIR SPLICE IAW DC8 SRM 51-1-8, OK TO INSTALL.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ON AT ALL TIMES. DISARM CHECK NORMAL. REMOVED AND REPLACED EMERGENCY BATTERY PACK.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ON AT ALL TIMES. DISARM CHECK NORMAL. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW 33-50-01.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS ON AT ALL TIMES. DISARM CHECK NORMAL. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT IAW 33-50-01, CHECKS GOOD.

Part: PUMP — FAILED (NR 2 & 3 ENGINE)

INSPECTION TYPE:N/A AFTER 2 HOURS IN FLIGHT LOST HYD QUANTITY TO STANDPIPE LEVEL, FOLLOWED EMERGENCY PROCEDURES, LANDING NORMAL FLAPS 23. REMOVED AND REPLACED NR 2 AND NR 3 ENGINE DRIVEN PUMPS AND ASSOCIATED FILTERS.

Part: BATTERY — INOPERATIVE (CABIN)

EMERGENCY LIGHTS WILL NOT TEST. REPLACED BATTERY PACK TESTS GOOD.

Part: BATTERY PACK — FAILED (CABIN)

EMERGENCY LIGHTS WILL NOT TEST. REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-01, TESTS GOOD.

Part: PANEL — CRACKED (NR 1 PYLON)

INSPECTION TYPE:PFLT NR 1 ENGINE PYLON RT SIDE AT FORWARD EDGE OF REMOVED PANEL. STRUCTURE UNDERNEATH HAS A CRACK ON LOWER FORWARD CORNER. PANEL HAS PREVIOUS DOUBLER INSTALLED AND SECURED, REFERENCE EO DC8-5430-0461C TRANSFERRED TO FERRY PERMIT FOR PERMANENT REPAIR.

Part: BATTERY — DISCHARGED (SMOKE DETECTOR)

INSPECTION TYPE:IN LOWER FWD BELLY SMOKE DETECTOR INOP. REMOVED AND REPLACED BATTERIES IN SMOKE DETECTOR UNIT S/N 4706 PERFORMED CHECK AS PER M/M 26-18-01 OPS CHECK NORMAL.

Part: FAN — FAILED (COCKPIT)

INSPECTION TYPE:N/A, STRONG ELECTRICAL BURNING SMELL SUSPECTED PACK SMOKE. WITH LEFT PACK AND RECIRC FAN OFF SMELL DISSIPATED. RAN ALL 4 ENGINES, OPERATED BOTH PACKS PER MM 21-55-00. NO ABNORMALITIES NOTED. FOUND RECIRC FAN INOP AND TO BE SOURCE OF ODOR. DEFERRED RECIRC FAN PER MEL 21-16.

Part: SKIN — CORRODED (RT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 RIGHT WING L/E LOWER SKIN IS CORRODED BEYOND LIMITS AT XFS 372.75 TO XFS 379. REPAIRED SKIN IAW 8110-3 APPROVED DH SK 880-554.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 RT NOSE TUNNEL UPPER PRESSURE WEB IS CORRODED BEYOND LIMITS STA-16 AT RBL 20. REPAIRED WEB IAW 8110-3 APPROVED DH SK 880-304.

Part: ANGLE — CRACKED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 LT WING L/E. VERTICAL ATTACH ANGLE IS CRACKED AT XS 520. REMOVED,FABRICATED, AND REPLACED ANGLE

Part: INTERCOSTAL — CRACKED (RT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C2,3 RIGHT WING L/E INTERCOSTAL IS CRACKED AT XS 454.976. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 5769857 AND SRM 57-1-0, 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 683 AT L36R SIDE FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA -99 LT SIDE BULKHEAD CAP ANGLE IS CRACKED. REPAIRED ANGLE IAW 8110-3 APPROVED DH SK 880-270.

Part: SKIN — CORRODED (AILERON) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 LT I/B AILERON FWD UPPER SKIN CUTOUT AT XA 458 IS CORRODED BEYOND LIMITS. REPAIRED SKIN

Part: WEB — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 80 SUBFLOOR IS CRACKED AT LBL 10. REPAIRED SUBFLOOR.

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 60 FRAME CRACKED UNDER DOUBLER AT RBL 24 REPAIRED FRAME.

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 RIGHT NOSE TUNNEL UPPER PRESSURE WEB IS CORRODED BEYOND LIMITS AT STA -80 TO -99 AT RBL 36. REPAIRED WEB IAW SRM 53-2-0 FIG 1D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 1240 L35L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758498 AND SRM 51-1-21

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 1677 INTERCOSTAL IS CRACKED AT LT CUSP. REMOVED,FABRICATED,AND REPLACED INTERCOSTAL IAW DWG 9753254 AND SRM 51-1-20D

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C2,3 STA 1400 FRAME IS CRACKED AT LONG 34R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 830 L22L FITTING IS CRACKED. REMOVED AND REPALCED FITTING IAW DWG 4753360 AND SRM 51-1-20D, 51-1-21

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 1140 FRAME IS CORRODED AND HAS MISDRILED HOLES BETWEEN LONG 32L TO 32R. REPAIRED FRAME IAW 8110-3 APPROVED DH SK 880-085.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 1230 BANANA FITTING IS CRACKED AT L33R. REMOVED AND REPLACED FITTING IAW DWG 3755847 AND SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 1240 L33R FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514,AND SRM. 51-1-20D

Part: FRAME — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C2,3 STA 1394 FRAME IS CRACKED AT LONG 34R. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 1340-1360 L31L INTERCOSTAL IS CORRODED BEYOND LIMITS. REMOVED,FABRICATED,AND REPLACED INTERCOSTAL IAW DWG 5751516 AND SRM 51-1-20D

Part: RIB — CRACKED (RT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 RT WING L/E. UPPER RIB IS CRACKED AT XILD .7095. REPAIRED RIB

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 280-300 L11R INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 3704510 AND SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 680 L11R ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751625 AND SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 680 L11R ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751625,AND SRM 51-1-20D

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 80-100 L33R INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 5750726 AND SRM 51-1-20D

Part: RIB — CRACKED (RT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 RT WING L/E. UPPER AND LOWER RIBS ARE CRACKED AT XFS 885. REMOVED, FABRICATED, AND REPLACED RIBS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 857 L18L INTERCOSTAL TO FRAME ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750423 AND SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 857 L5R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659 AND SRM 51-1-20D

Part: DOUBLER — CRACKED (RT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 RT WING OB L/E. LOWER INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED, AND REPLACED DOUBLER

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 879-902 RBL 65 FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED,FABRICATED,AND REPLACED DOUBLER.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 680 L11L ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG.4751625,AND SRM. 51-1-20D

Part: RIB — CRACKED (RT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 RIGHT WING OB. L/E. UPPER RIB IS CRACKED AT XFS 841.25 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: RIB — CRACKED (RT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 RT WING L/E. UPPER RIBS ARE CRACKED AT XFS 603.75, XFS 616.25, XFS 622.5. REPAIRED RIBS.

Part: ANGLE — CRACKED (RT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 RT WING L/E. VERTICAL ATTACH ANGLE IS CRACKED AT XS 520. REMOVED, FABRICATED, AND REPLACED ANGLE.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 857-879 LBL 63 FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED,FABRICATED,AND REPLACED DOUBLER.

Part: RIB — CRACKED (RT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 RT WING L/E. UPPER RIBS ARE CRACKED AT XFS 678.75, XFS 666.25, XFS 603.75. REPAIRED RIBS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 834-857 L1 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750521 AND SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 902-920 L3R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659,AND SRM 51-1-20D, 51-1-23

Part: PRESSURE PANEL — CORRODED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C2,3 STA 4 RBL 58 PRESSURE WEB IS CORRODED BEYOND LIMITS. REPAIRED WEB IAW SRO 8530026.

Part: RIB — CRACKED (RT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 316.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CORRODED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 830 FRAME FITTING BELOW LONG 21L AFT FACE IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3616945,8110-3 APPROVED DH SK 880-861, SRM 53-1-0, 51-1-20D.

Part: SPLICE — CRACKED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 LT WING L/E. LOWER INNER SPLICE IS CRACKED AT XS 520.168. REMOVED, FABRICATED, AND REPLACED DOUBLER AND PLATE.

Part: SKIN — CORRODED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE: C1, 3. LEFT WING OB L/E. UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 628.75 ***CPCP*** REPAIRED SKIN I.A.W. SRM. 57-2-1 FIG. 38

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 1240 L20R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750418 AND SRM 51-1-20D

Part: RIB — CRACKED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE: C1 ,3. LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 766.25 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 FUSELAGE SKIN STA 1150 - 1230 LONG 28R - 33R IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SKIN SECTION IAW 8110-3 APPROVED DH SK 880-559.

Part: SKIN — CORRODED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 LT WING CENTER L/E. UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 391.5. REPAIRED SKIN.

Part: RIB — CRACKED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 741.25. REPAIRED RIB.

Part: RIB — CRACKED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 828.75. REPAIRED RIB

Part: RIB — CRACKED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 791.25. REPAIRED RIB

Part: SKIN — CHAFED (PAX DOOR) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C2,3 STA 45 FWD ENTRY DOOR SKIN IS CHAFED BEYOND LIMITS ABOVE HANDLE OPENING. REPAIRED SKIN IAW SRM 52-2-0 FIG 2.

Part: RIB — CRACKED (LEFT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1, 3. LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 778.750 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: RIB — CRACKED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 728.75. REPAIRED RIB.

Part: RIB — CRACKED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 660. REPAIRED RIB.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 702 RBL 6 FRAME SHEAR TIE IS CRACKED. REPAIRED SHEARTIE IAW SRM 53-2-0 FIG 1B AND DWG 5753158

Part: SKIN — CORRODED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 LT WING CENTER L/E. UPPER SKIN IS CORRODED BEYOND LIMITS AT XFS 304 AND XFS 335.25. REPAIRED SKIN

Part: RIB — CRACKED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 816.25. REPAIRED RIB.

Part: RIB — CRACKED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XOLD 067. REPAIRED RIB

Part: RIB — CRACKED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 722.5. REPAIRED RIB

Part: RIB — CRACKED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1, 3. LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 772.5 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: RIB — CRACKED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE: C1, 3. LEFT WING L/E. UPPER RIB IS CRACKED AT XFS 750 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: RIB — CRACKED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1, 3. LEFT WING L/E. LOWER RIB IS CRACKED AT XFS 397.750 REPAIRED RIB I.A.W. SRM. 57-2-0 FIG. 2

Part: DOUBLER — CRACKED (RT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 RT WING L/E. INTERNAL DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED, AND REPLACED DOUBLER.

Part: RIB — CRACKED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 LT WING L/E. UPPER RIB IS CRACKED AT XFS 810. REPAIRED RIB.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 1240 L18R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D

Part: ANGLE — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 1766 LONG 10R BULKHEAD ANGLE/CHORD IS CRACKED. REPAIRED ANGLE IAW SRM 53-2-5 FIG 9.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 270 - 370 LONG 28R - 33R FUSELAGE SKIN IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED SKIN SECTION IAW 8110-3 APPROVED DH SK 880-334.

Part: FITTING — CORRODED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 70 L21R CUSP JOINT ATTACH FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3610130 AND SRM 51-1-20D, 51-1-21

Part: SKIN — CORRODED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE: C1, 3. LEFT WING L/E. LOWER SKIN IS CORRODED BEYOND LIMITS AT XFS 635 ***CPCP*** REPAIRED SKIN I.A.W. E.O. DC8-5720-4087-B APPX. C

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 660-680 L11R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5750540 AND SRM 51-1-20D, 51-1-23

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE:C1,3 STA 683 PRESSURE BULKHEAD IS CRACKED RBL 6-24. REMOVED AND REPLACED BULKHEAD IAW DWG 9753751, AND SRM 53-1-0, 51-1-20D, 51-1-21.

Part: SKIN — CORRODED (LT WING) · airframe 67,397 hrs · 25,286 cycles

INSPECTION TYPE: C1, 3. LEFT WING OB. L/E. LOWER SKIN HAS INTERGRANULAR CORROSION BETWEEN XFS 710-716.25 ***CPCP*** REPAIRED SKIN I.A.W. E.O. DC8-5720-4087,AND SRM. 51-1-20D,51-1-21

Part: WARNING LIGHT — ILLUMINATED (NR 2 ENGINE)

INSPECTION TYPE:PRE, CREW PREFLT - NR 2 ENG FIRE WARNING HANDLE LIGHT ILLUM.

Part: FRAME — CRACKED (BS 25)

INSPECTION TYPE:SP, STA 25 LT FRAME CRACKED AT LONG 17L APPROX 1 INCH ABOVE SNUBBER ATTACH POINT. REPAIRED PER SRM 53-2-0 FIG 2.

Part: LIGHT — INOP (RT WING)

ON APPROACH TO ONT, RIGHT WING LANDING LIGHT FAILED TO ILLUMINATE WITH SWITH ON. PERFORMED T/S PER FIM 33-42-00 FIG 107, RELAMPED PER MM 33-42-03.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, DURING MX INSPECTION EMERGENCY LIGHT FAILED TO TEST. *S/D* REMOVED AND REPLACED BATTERY PACK.

Part: WIRE — BROKEN (LT MLG)

INSPECTION TYPE:N/A, LEFT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE ON LANDING IN ONT. AFTER CHECKLIST COMPLETE, A NORMAL LANDING WAS MADE. GEAR PINNED. REPLACED BROKEN WIRE BETWEEN TERMINAL BOARD S3-5 AND L/G DOWN LIMIT SWITCH. WIRE G322E24. LEFT LANDING GEAR LIGHT OPERATED NORMAL REF WDM 3201 SHEET 2 PG 2.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK.

Part: FITTING — CORRODED (BS 280)

INSPECTION TYPE:C2 FITTING AT FS 280 AND LONGERON 34L IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-3-0.

Part: SKIN — CRACKED (WS 761)

INSPECTION TYPE:C2, RT O/B LEADING EDGE SKIN IS CRACKED BETWEEN FASTENERS AT XW 761. REPAIRED SKIN IAW SRM 57-2-1 FIG 2H.

Part: LONGERON — CORRODED (BS 1160 - 1180)

INSPECTION TYPE:C2, LONG 28L FS 1160 TO 1180 IS CORRODED BEYOND LIMITS. REPAIRED IAW DH SK880-651.

Part: STRAP — CORRODED (BS 610)

INSPECTION TYPE:C2 FS 610, LONGERON 31L TO 31R, THE STRAP IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED STRAP IAW DWG 5779913 CPCP.

Part: DOUBLER — CORRODED (BS 610)

INSPECTION TYPE:C2 FS 610, LONGERON 31L TO 31R, THE FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED FINGER DOUBLER IAW DWG 5779913 AND SRM 51-1-21. CPCP

Part: SPLICE — CRACKED (BS 1490)

INSPECTION TYPE:C2 LONGERON 35L SPLICE AT FS 1490 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-1-21.

Part: FRAME — CORRODED (BS 1000)

INSPECTION TYPE:C2 FS 1000 FRAME UPPER FLANGE, LWR SURFACE AT LONGERON 36, IS CORRODED BEYOND LIMITS. REPAIRED FRAME IAW SRM 53-2-0 FIG 2.

Part: LONGERON — CRACKED (BS 1350 - 1347)

INSPECTION TYPE:C2, LONGERON 36 IS CRACKED BETWEEN FS 1350 AND 1347. REPAIRED LONGERON IAW DH SK880-592.

Part: LONGERON — CORRODED (BS 1360)

INSPECTION TYPE:C2 LONG 36 FLANGE AT FS 1360 IS CORRODED BEYOND LIMITS. REPAIRED LONGERON 36 IAW DHC SK880-514.

Part: RIB — CRACKED (WS 467.323)

INSPECTION TYPE:C2, RT WING L/E RIB AT XS 467.323 IS CRACKED AT THE AFT LWR END. STOP DRILLED, AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 461 & 484)

INSPECTION TYPE:C2, RT WING L/E RIBS AT XS 461.372 AND XS 484.895 ARE CRACKED AAND& REPAIRED IAW SRM 57-2-0.

Part: ANGLE — CORRODED (BS 280)

INSPECTION TYPE:C2, NUT PLATE ANGLE HAS HEAVY CORROSION ON THE UNDERSIDE, FS 280 LONG 34L TO 34R. REMOVED, FABRICATED AND REPLACED NUT PLATE ANGLE IAW DHC SK880-410 AND SRM 51-1-21.

Part: SKIN — CRACKED (WS 710)

INSPECTION TYPE:C2 RT WING L/E LWR SKIN AT XFS 710 IS CRACKED BETWEEN SCREW HOLES. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-4087B.

Part: SEAT TRACK — CORRODED (BS 55-80)

INSPECTION TYPE:C2 SEAT TRACK FLANGE AT RBL 48, FS 55 TO 80 IS CORRODED BEYOND LIMITS. REMOVED DAMAGED SEAT TRACK FS 55 TO 110, FABRICATED AND REPLACED IAW SRM 53-2-3.

Part: SKIN — CORRODED (WS 38.75-45)

INSPECTION TYPE:C2 RT WING L/E LWR SURFACE BETWEEN XFS 38.75 AND 45.00 IS CORRODED BEYOND LIMITS. REPAIRED IAW DHC SK880-933. CPCP

Part: FITTING — CORRODED (BS 340)

INSPECTION TYPE:C2 FS 340 BETWEEN LONGERON 36 AND 34L, THE FRAME FITTING IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED FITTING IAW DHC SK880-410 AND SRM 51-1-20D AND 51-3-0.

Part: DOUBLER — CORRODED (BS 1350)

INSPECTION TYPE:C2 FINGER DOUBLER, FS 1350, LONGERON 35L TO 35R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND INSTALLED FINGER DOUBLER IAW DWG 5750322 AND SRM 51-1-20D AND 51-1-21.

Part: SHEAR TIE — CRACKED (BS 1360)

INSPECTION TYPE:C2 SHEAR TIE AT FS 1360, BETWEEN LONGERON 31R AND 33R IS CRACKED. REMOVED, FABRICATED, AND INSTALLED SHEAR TIE IAW DWG 9755821-507 AND SRM 51-1-20D AND 51-1-21.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE:C2, RT WING L/E RIBS AT XFS 566.25, 855.0, 885.0, 878.75, 829.75, 816.25 803.75, 785.0, 766.25, 747.5, 728.75, 722.5, AND 716.25 ARE CRACKED. STOP DRILLED CRACKS AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FRAME — CRACKED (BS 1446)

INSPECTION TYPE:C2, FS 1446 FRAME AT LONG 34R IS CRACKED. REMOVED DAMAGED AREA AND REPAIRED IAW SRM 53-2-0 FIG 13.

Part: WEB — CORRODED (VERT STAB)

INSPECTION TYPE:C2 VERT STAB BASE, FS 1781 THROUGH 1818, RT WEB BETWEEN THE CENTER AND REAR SPARS HAS HEAVY EXFOLIATION CORROSION. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 51-1-9A. CPCP

Part: SKIN — CRACKED (BS 1240-1280)

INSPECTION TYPE:C2 FUSELAGE SKIN AT FS 1240 TO 1280, APPROX LONG 33R, AT THE D-PIT DOOR CUT OUT IS CRACKED AND HAS HEAVY CORROSION. REMOVED AND REPLACED THE SKIN IAW SRM 51-1-20D AND 51-3-0. CPCP

Part: FITTING — CRACKED (LT HORIZ STAB)

INSPECTION TYPE:C2 LT HORIZ STAB LWR BATHTUB FITTINGS (3 EA.) AT XFS 47 IS CRACKED. REMOVED, FABRICATED, AND INSTALLED 3 EA FITTINGS IAW DWG 4653888, 4653760; AND SRM 51-1-20D.

Part: ANGLE — CORRODED (BS 62)

INSPECTION TYPE:C2, FS -62, LBL 60, THE CUSP TEE ANGLE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED THE TEE ANGLE IAW DWG 5613857 AND SRM 51-1-20D.

Part: SKIN — CORRODED (BS 1620)

INSPECTION TYPE:C2, FUSELAGE EXTERNAL SKIN AT FS 1620, LONG 20L IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED AREA AND REPAIRED IAW DHC SK880-113.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:C2 FITTING TOP OF CENTER WING BOX AT FS 680 AND LONGERON 22R IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3642974 AND SRM 51-1-20D.

Part: SPLICE — CRACKED (BS 450)

INSPECTION TYPE:C2 LONGERNON 31L SPLICE AT FS 450 IS CRACKED. REMOVED AND REPLACED SPLICE IAW SRM 51-1-20D.

Part: FITTING — CRACKED (RT HORIZ STAB)

INSPECTION TYPE:C2 RT HORIZ STAB L/E AT XFS 47, THE UPPER BATHTUB FITTING IS CRACKED. REMOVED, FABRICATED, AND INSTALLED FITTING IAW DWG 4653888 AND SRM 51-1-20D.

Part: SKIN — CORRODED (WS 347.75-370)

INSPECTION TYPE:C2 LT WING UPPER L/E SKIN AT XFS 347.75 TO 370 IS CORRODED BEYOND LIMITS, AT THE T/E. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1.

Part: SHEAR TIE — CRACKED (BS 1834)

INSPECTION TYPE:C2 FS 1834 SHEAR TIE CRACKED AT LONGERON 3L. REMOVED DAMAGED SHEAR TIE, FABRICATED, AND REPLACED IAW SRM 53-2-0.

Part: SKIN — CORRODED (WS 38.75 & 45)

INSPECTION TYPE:C2, RT WING L/E LWR SURFACE BETWEEN FS 38.75 AND 45.00 IS CORRODED BEYOND LIMITS. REPAIRED IAW DHC SK880-933.

Part: FITTING — CRACKED (CARGO DOORWAY)

INSPECTION TYPE:C2, FS 1180, THE 'C' PIT DOOR FRAME FWD STOP FITTING IS CRACKED AT LONG 26L. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: DOUBLER — CRACKED (LT HORIZ STAB)

INSPECTION TYPE:C2 LT HORIZ STAB INBD SIDE OF THE STA XE 221.0 FRAME IS CRACKED AND TORN. REMOVED, FABRICATED, AND INSTALLED FINGER DOUBLER IAW DWG 5644310 AND SRM 51-1-21.

Part: SKIN — CORRODED (RT HORIZ STAB)

INSPECTION TYPE:C2, RT HORIZ STAB OTBD L/E, INBD FWD SECTION, STA. XFS 210, HAS BULGING CORROSION. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 55-2-1, FIG 4.

Part: FITTING — CRACKED (BS 1150)

INSPECTION TYPE:C2 FS 1150 TORQUE BOX BATHTUB FITTING BETWEEN LONGERON 35R AND 34R IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 53-2-0.

Part: RIB — CRACKED (WS 6.225)

INSPECTION TYPE:C2 LEFT WING INBOARD RIB AT XOLDI 6.225 IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.

Part: FITTING — CRACKED (BS 1240)

INSPECTION TYPE:C2, INTERCOSTAL AT LONG 35R ATTACH FITTING IS CRACKED AT FS 1240. REMOVED, AND REPLACED FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 603.75)

INSPECTION TYPE:C2, LT WING L/E RIB AT FS 603.75 IS CRACKED AT THE AFT LOWER FASTENER. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 628.75)

INSPECTION TYPE:C2, LT WING L/E RIB AT XFS 628.75 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 635)

INSPECTION TYPE:C2, LT WING L/E RIB AT XFS 635.0 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 641.25)

INSPECTION TYPE:C2, LT WING L/E RIB AT XFS 641.25 IS CRACKED AT THE AFT UPPER FASTENER STOP DRILLED AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (RT TE FLAP)

INSPECTION TYPE:C2, THE RT STA 410 FLAP CANOE FITTING, OTBD SIDE FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-3-0.

Part: ANGLE — CRACKED (WS 98)

INSPECTION TYPE:C2, THE RT STA 98 FLAP ACTUATOR ATTACH FITTING INBD MOUNT ANGLE IS CRACKED AT THE LWR END. REMOVED, FABRICATED, AND REPLACED THE ANGLE IAW DWG 3643319 AND SRM 51-1-20D AND 51-3-0.

Part: RIB — CRACKED (WS 628.75)

INSPECTION TYPE:C2, LT WING L/E RIB AT XFS 628.75 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 622.5)

INSPECTION TYPE:C2, LT WING L/E RIB AT XFS 622.5 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 491.193)

INSPECTION TYPE:C2, RT WING L/E RIB AT XS 491.193 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 691.25)

INSPECTION TYPE:C2 RT WING L/E RIB AT XFS 691.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE:C2 RT WING L/E, INBD STA XOLDI 6.225 RIB IS CRACKED ABOVE THE PNEU DUCT. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 616.25)

INSPECTION TYPE:C2, LT WING L/E RIB AT XFS 616.25 IS CRACKED AT THE AFT UPPER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (WS 710)

INSPECTION TYPE:C1, LT WING L/E SKIN AT FS 710 IS CRACKED AT THE AFT LWR CORNER. REPAIRED SKIN IAW SRM 51-2-1.

Part: SKIN — CORRODED (WS 708)

INSPECTION TYPE:C2 RT WING L/E, LWR SKIN AT XFS 708 IS CORRODED OUT OF LIMITS AT 1 EA SCREW HOLE. REPAIRED SKIN IAW EO DC8-5720-7787.

Part: SKIN — CRACKED (WS 710)

INSPECTION TYPE:C2, RT WING L/E UPPER SKIN AT XFS 710.0 IS CRACKED AT 1 SCREW HOLE. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.

Part: SKIN — CRACKED (BS 40)

INSPECTION TYPE:C2 EXTERIOR FUSELAGE SKIN CRACKED AT FS 40, LONGERON 30L AT DOOR CUTOUT. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-2-0 FIG 13.

Part: LONGERON — CRACKED (BS 55-70)

INSPECTION TYPE:C2 LONGERON 27R IS CRACKED BETWEEN FS 55 AND 70. REMOVED DAMAGED LONGERON, FABRICATED, AND REPLACED IAW DWG 3648666 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FRAME 660)

INSPECTION TYPE:C2 FRAME 660 ATTACH FITTING AT LONG 36 IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: ANGLE — CRACKED (BS 680)

INSPECTION TYPE:C2, CABIN FLOORBEAM SUPPORT ATTACH ANGLE IS CRACKED FS 680, RBL 24. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 4645517 AND SRM 51-1-20D.

Part: SKIN — CORRODED (LT WING)

INSPECTION TYPE:C2, LT I/B SLOT VANE I/B END HAS MODERATE CORROSION. CUT OUT DAMAGED AREA AND REPAIRED IAW EO DC8-5720-7767A.

Part: SKIN — CRACKED (WS 761.695)

INSPECTION TYPE:C2 RT WING L/E LWR SKIN AT XW 761.695 IS CRACKED AT 1 SCREW HOLE. REPAIRED SKIN IAW EO DC8-5720-4087.

Part: SKIN — CRACKED (WS 710)

INSPECTION TYPE:C2, RT WING L/E LWR SKIN AT XFS 710 IS CRACKED AT 1 FASTENER HOLE. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 57-2-0 FIG 24.

Part: SKIN — CRACKED (WS 660)

INSPECTION TYPE:C2, LT WING L/E UPPER SKIN AT XFS 660 IS CRACKED AT 1 FASTENER. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.

Part: FRAME — CRACKED (BS 55)

INSPECTION TYPE:C2 FS 55 FRAME IS CRACKED AT LONGERON 24L, AROUND THE ROD ATTACHMENT. CUT OUT DAMAGED AREA AND REPAIRED SRM 53-2-0 FIG 2.

Part: FITTING — CORRODED (BS 660)

INSPECTION TYPE:C2, HEAVY CORROSION ON T FITTING, FS 660 AT LONG 36. REPAIRED FITTING IAW DHC SK880-110. CPCP

Part: FRAME — CRACKED (BS 55)

INSPECTION TYPE:C2, FS 55 FRAME IS CRACKED AT LONG 24R, AROUND THE ROD ATTACHMENT. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 53-2-0 FIG 2.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE DURING BITE CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CHECK OK.

Part: SKIN — CRACKED (WS 257)

INSPECTION TYPE:C, LT WING L/E SKIN AT STA XW257 UPPER SURFACE IS CRACKED AT 1 SCREW HOLE. REPAIRED IAW SRM 57-2-1 AND 51-1-21.

Part: SKIN — CORRODED (WS 486)

INSPECTION TYPE:C LT WING L/E SKIN AT STA XW486, AT THE L/E, HAS HEAVY EXFOLIATED CORROSION. CORROSION EXTENDS UNDER REPAIR DOUBLER. REMOVED EXISTING REPAIR DOUBLER, CUTOUT DAMAGE, AND REPAIRED IAW SRM 57-2-1 AND 51-1-21.

Part: FITTING — CRACKED (BS 692)

INSPECTION TYPE:C, FWD ACCY COMPT, KEEL BEAM END FITTING RBL 5 AT FS 692 AFT SIDE CRACKED. REMOVED AND REPLACED FITTING IAW SRM 57-3-0.

Part: RIB — CHAFED (WS 422.75)

INSPECTION TYPE:C, LT WING L/E LWR RIB AT STA XFS 422.75 IS CHAFTED BEYOND LIMITS BY THE TAI FLEX DUCT. REPAIRED IAW SRM 57-3-0 AND 57-2-0.

Part: SKIN — CORROSION (WS 710.5)

INSPECTION TYPE:C LT WING L/E SKIN AT STA 710.5 HAS MODERATE EXFOLIATION CORROSION AT THE L/E. REPAIRED IAW SRM 57-2-1 AND 51-1-21.

Part: ANGLE — CRACKED (LT WING)

INSPECTION TYPE:C, LT WING L/E, INBD END, AFT UPPER CORNER, THE L/E ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-3-0 AND DWG 5769632.

Part: SPOILER PUMP — FAILED (MLG WW)

INSPECTION TYPE: 3+3C. BLOCK TURN BACK, SPOILER PUMP ABNORMAL, LOW PRESSURE. SDN: LOG BOOK PG. 565487. REPLACED SPOILER PUMP AND OPS CHECK GOOD, P/N 27-60-00.

Part: LONGERON — CRACKED (FS 1163)

INSPECTION TYPE 'C', LONGERON 36 LT FS 1163 CRACKED. REPLACED LONGERON SECTION PER SRM 51-1-20D.

Part: ANGLE — CRACKED (BS 781)

INSPECTION TYPE 'C', T-ANGLE CRACKED AT FS 781 XLW LONGERON 23R. REPAIRED ANGLE PER SRM 53-2-0.

Part: FITTING — CORRODED (FS 1200)

HEAVY CORROSION ON B/T FITTING FS 1200 LONGERON 34L AND 33L. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CORRODED (FS 1180)

HEAVY CORROSION ON B/T FITTING 1180 LONGERON 33L AND 34L. REPLACED FITTING PER SRM 53-2-0.

Part: SPLICE — CRACKED (FS 1350)

LONGERON 31L SPLICE CRACK AT FS 1350. REPLACED SPLICE PER SRM 51-1-20D.

Part: RIB — CRACKED (RUDDER STA XR120)

INSPECTION TYPE: C. RUDDER NOSE RIB, STA XR120, LT CRACKED. REPAIRED RIB PER UPS EO DC8-55-0083.

Part: SKIN — CORROSION (LT HORIZ STAB)

INSPECTION TYPE: C. LEFT HORIZONTAL STABILILZER, LOWER SURFACE INBOARD T/E SKIN PANEL HAS CORROSION BULGES. REPLACED SKIN PANEL PER SRM 51-1-21.

Part: DOOR — CRACKED (CARGO BAG BIN)

CARGO BAG BIN DOOR HAS CRACK ABOUT 3 INCHES AT LWR FWD AREA OF FRAME BETWEEN FITTING AND END BUMPER. REPAIRED PER UPS EO DC8-52-0124.

Part: FITTING — CRACKED (FS 902)

INSPECTION TYPE: C. RIGHT TRAP FITTING AFT OUTBOARD VERTICAL FLANGE HAS .75 INCH CRACK, FS 902, LONGERON 24R. REPLACED FITTING PER DRAWING NR 5750092.

Part: WEB — CRACKED (BS 781)

INSPECTION TYPE 'C', WEB CRACKED AT STA 781 LONGERON 23R. REPAIRED WEB PER DC8-5350-7876.

Part: WEB — CRACKED (BS 800)

INSPECTION TYPE 'C', WEB CRACKED AT STA 800 XCW LONG 5L. REPAIRED WEB PER DC8-5350-7876.

Part: SPAR — CRACKED (WS 60)

INSPECTION TYPE 'C', REAR SPAR UPPER CHORD ANGLE 9 CRACK APPROX XCW60 FS 850 LT W/W. REPAIRED SPAR CHORD PER SRM 53-2-5 FIG 2 AND DOUBLER DRAWING 3646971.

Part: WEB — CRACKED (FS 790)

INSPECTION TYPE 'B', WEB CRACKED AT FS 790 XLW LONGERON 23R. REPLACED WEB PER SRM 53-2-0.

Part: SHEAR TIE — CRACKED (BS 700)

INSPECTION TYPE 'C', SHEAR TIE CRACKED AT STA 700XLW LONGERON 10R. REPAIRED SHEAR TIE PER SRM 53-2-0 FIG 2.

Part: BELT FRAME — CORRODED (FS 1460)

FS 1460 LONGERON 31L TTO 34R BELT FRAME HAS HEAVY CORROSION. REPAIRED FRAME PER SRM 53-2-0.

Part: DOUBLER — CORRODED (FS 1120-1100)

HEAVY CORROSION ON DOUBLER FS 1120 TO 1100 LONGERON 35L TO 34L. REPLACED DOUBLER PER SRM 51-1-20D AND 51-1-21.

Part: FRAME — CORRODED (FS 1340)

UPPER SURFACE OF LOWER FLANGE OF BELT FRAME HAS CORROSION OUT OF LIMITS AT STA 1340 LONGERON 36. REPAIRED FRAME PER SRM 53-2-0 FIG 2.

Part: DOUBLER — CORRODED (FS 15)

INSPECTION TYPE: C. COCKPIT SUBFLOOR FINGER DOUBLER HAS CORROSION DAMAGE AT FS 15, LONGERON 22L. REPLACED FINGER DOUBLER SECTION PER SRM 51-1-20D.

Part: DOUBLER — CORRODED (FS 1340-1360)

MODERATE CORROSION ON LONGERON 31L FS 1340 TO 1360 AT DOUBLER. FABRICATED AND REPLACED DOUBLER PER SRM 51-1-21D.

Part: FITTING — CRACKED (FS 940)

INSPECTION TYPE 'B', T-ANGLE SUPPORT FITTING CRACKED AT FS 940 LONGERON 24R. REPLACED FITTING PER SRM 51-1-20D.

Part: BRACKET — CRACKED (RUDDER LE)

INSPECTION TYPE 'C', 2ND RUDDER HINGE POINT 2, 2 INCH LONG CRACK ON BRACKETS ALONG TOP AND BOTTOM ENDS. REPLACED BRACKETS PER SRM 51-1-20D.

Part: LONGERON — CORRODED (FS 460)

MODERATE TO HEAVY CORROSION IN LONGERON 31L FWD SIDE AT FS 460. REPAIRED PER EO DC8-53-1622.

Part: SKIN — DELAMINATED (NR 3 SPOILER)

INSPECTION TYPE 'B', NR 3 SPOILER LT WING DELAMINATION ON BOTTOM SIDE. REPLACED SPOILER PNL PER MM 27-61-01.

Part: FLAP TRACK — CORRODED (RT TE FLAP)

INSPECTION TYPE: C. RIGHT WING FLAP HAS CORROSION AT STA XW 428. REPLACED TRACK PER MM 27-51-03.

Part: FLAP TRACK — CORROSION (RT TE FLAP)

INSPECTION TYPE: C. RIGHT WING FLAP TRACK HAS CORROSION AT STA STA 98. REPLACED TRACK PER MM 27-51-03.

Part: FITTING — CORRODED (FS 878)

INSPECTION TYPE 'C', HEAVY CORROSION ON VERTICAL FITTING ABOVE LONGERON 24L FS 878. REPLACED ANGLE PER SRM 51-1-20D.

Part: WING TRACK — CORRODED (RT TE FLAP)

INSPECTION TYPE: C. RIGHT WING FLAP HAS CORROSION AT STA XW3. REPLACED TRACK PER MM 27-51-03.

Part: RIB — CRACKED (LT WING LE)

INSPECTION TYPE 'C', 4 RIBS CRACKED LT WING L/E ABOVE I/B FUELING PORT. REPAIRED RIBS PER SRM 57-2-0.

Part: WEB — CORRODED (FS 240-260)

INSPECTION TYPE: C. FS 240 - FS 260, TUNNEL WEB CRACKED AND CORRODED. REPLACED DOUBLER WEB SECTION PER SRM 51-1-20D.

Part: FITTING — CRACKED (FS 878)

INSPECTION TYPE 'B', VERTICAL FITTING ABOVE LONGERON 24R CRACKED FS 878. REPLACED FITTING PER SRM 51-1-20D.

Part: FLAP TRACK — CORRODED (RT TE FLAP)

INSPECTION TYPE: C. RIGHT WING FLAP TRACK HAS CORROSION AT STA XW340. REPLACED TRACK PER MM 27-51-03.

Part: FITTING — CRACKED (FS 680)

INSPECTION TYPE 'B', FITTING CRACKED AT LONGERON 21R AFT SIDE OF FS 680. REPLACED FITTING PER SRM 51-1-20D.

Part: FLAP TRACK — CORRODED (RT TE FLAP)

INSPECTION TYPE: C. RIGHT WING FLAP TRACK HAS CORROSION AT STA XW219. REPLACED TRACK PER MM 27-51-03.

Part: SEAT TRACK — CORROSION (FS 300-320)

INSPECTION TYPE: C. MODERATE CORROSION DAMAGE ON BOTTOM SIDE OF THE SEAT TRACK. SPLICE BETWEEN STA 300-320. REPLACED SPLICES PER SRM 51-3-0.

Part: HINGE — CRACKED (NR 4 BELLY DOOR)

INSPECTION TYPE 'C', BELLY DOOR SKIN HINGE CRACKED AND BROKEN LUGS. REPLACED HINGE PER SRM 51-1-21.

Part: FITTING — CORROSION (FS 878)

INSPECTION TYPE 'C', HEAVY CORROSION ON VERTICAL FITTING ABOVE LONG 24L FS 878. REPLACED FITTING PER SRM 53-2-0 FIG 8.

Part: SPAR — CRACKED (WS 624)

INSPECTION TYPE: C. RIGHT WING REAR SPAR UPPER CHORD ANGLE CRACKS AT STA XRS624. REPAIRED PER UPS EO DC8-57-0671.

Part: DOUBLER — CORRODED (RT WING TE)

RT WING O/B WEDGE CORROSION DAMAGE ON LWR INNER SKIN DOUBLER. REPLACED DOUBLER PER SRM 51-1-21.

Part: SKIN — CRACKED (NR 4 BELLY DOOR)

INSPECTION TYPE 'C', 34 BELLY SKIN DOOR HAS A CRACK BEYOND SCOPE OR EO REPAIR. REPAIRED SKIN PER SRM 52-2-0 AND EO NR DC8-5530-6643D.

Part: LONGERON — CRACKED (FS 857)

INSPECTION TYPE: C. HIGH FREQUENCY EDDY CURRENT INSPECTION INDICATES CRACK AT LONGERON 24R, FS 857 AT BOLT ATTACH HOLE. REPLACED LONGERON SECTION PER DRAWING NR 575198 AND NR 5750127.

Part: PANEL — DELAMINATED (NR 1 SPOILER)

INSPECTION TYPE 'C', RT WING NR 1 SPOILER PANEL DELAMINATION ON BOTTOM SIDE. REPLACED SPOILER PANEL PER MM 27-01-00.

Part: BATTERY WIRE — BROKEN (ESCAPE SLIDE)

WHILE ON GROUND IN EAST MIDLANDS, MAINTENANCE FOUND PIREP-EMERGENCY ESCAPE SLIDE BATTERY PACK WIRING BROKEN. MAINTENANCE REMOVED THE SLIDE AND DEFERRED PER E.O. MRR FILED OPEN.

Part: BATTERY WIRE — BROKEN (ESCAPE SLIDE)

SUPPLEMENTAL MRR: WHILE ON THE GROUND IN EAST MIDLANDS, MAINTENANCE FOUND THE EMERGENCY ESCAPE SLIDE BATTERY PACK WIRING BROKEN. MAINTENANCE REMOVED THE SLIDE AND DEFERRED EPR EO. MAINTENANCE ALSO SECURED SLIDE PACK AS REQUIRED.

Part: EMERG BATT PACK — DISCHARGED (FLIGHT DECK)

WHILE ON GROUND, MAINTENANCE FOUND ON PREFLIGHT BOTH EMERG LIGHTING BATTERY PACK AND MAIN SHIPS BATTERY LOW. REMOVED AND REPLACED BOTH EMERG LIGHTING BATTERY PACK AND MAIN SHIPS BATTERY, OPS CKS GOOD.