N874UP

Part: ENGINE — FLAMED OUT (NR 3)

INSPECTION TYPE:N/A, NR 3 ENGINE FLAMEOUT. ***SDR FILED OPEN***

Part: FUEL — CONTAMINATED (TANK)

INSPECTION TYPE:N/A IFSD - NR 1 ENGINE FLAMED OUT AS POWER WAS BROUGHT TO IDLE FOR DESCENT OUT OF 380. PERFORMED FLAME OUT CK LIST AT FL 240 ENGINE STARTED AND INDICATED NORMAL OPERATION. PERFORMED STEPS IAW T/S TREE REF MM 71-00-00-1 FIG 139. REMOVED AND REPLACED FUEL FILTER AS PRECAUTIONARY REF MM 73-10-02-4. FOUND UNUSUAL AMOUNT OF WATER. DRAINED WATER FROM TANK AND GROUND RUN OPS NORMAL.

Part: FITTING — INOPERATIVE (HYD SYSTEM)

IN CRUISE, HYD QTY DROPPING RUN CK LIST, STOPPED AT AUX PUMP LEVEL. PRESS NEVER BELOW 3000 PSI. R/R HYD FITTING AT LT MLG AFT HYD MANIFOLD, FAR OB POS FOR BOGIE TR TRIM CYL. REPACKED FITTING W/REF TO AMM 2-13-00-2. SERVICED MAIN HYD RESERVIOR W/REF TO AMM 12-30-01-3. NO LEAKS NOTED. OK FOR SERVICE.

Part: SEAL — MISSING (PBE)

INSPECTION TYPE:N/A CREW PBE MISSING THE UPPER GREEN LOCKED SEAL. REPLACED LOCK SEAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK ASSY. OPS CHECK GOOD, REF AMM 33-50-01-2, P/N ON 60-1223-5, S/N ON 341.

Part: BATTERY PACK — NOT SEATED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT ARM. RESEATED BATTERY PACK. OPS CHECK NORMAL.

Part: BRACKET — CRACKED (LT WING) · airframe 80,171 hrs · 26,958 cycles

INSPECTION TYPE:SP BRACKET CRACKED AT 3 BOLT HOLES L/WING FRONT SPAR UPPER INBD CORNER STA 680. REMOVED, FABRICATED, AND INSTALLED REPAIR BRACKET AT L/WING FRONT SPAR STA 680 IAW SRM 51-1-21, AND DWG 5615800.

Part: BRACKET — BROKEN (FUSELAGE) · airframe 80,171 hrs · 26,958 cycles

INSPECTION TYPE:SP BROKEN BRACKET ON FUSELAGE ABOVE LEADING EDGE AUX TANK, L/WING. REMOVED, FABRICATED AND INSTALLED REPAIR BRACKET ON L/WING AUX TANK STA XCW 69.500 IAW SRM 51-3-00-01, AND DWG 5769482.

Part: HOUSING — OPEN (ESCAPE SLIDE)

ESCAPE SLIDE HOUSING IS PARTIALLY OPEN. SECURED ESCAPE SLIDE HOUSING PER MM 25-60-01-2.

Part: SKIN — CORRODED (FUSELAGE) · airframe 88,304 hrs · 25,808 cycles

INSPECTION TYPE:C1 CORROSION ON FUSELAGE EXTERIOR L35L, STA 1075. REPAIRED DAMAGED EXTERIOR FUSELAGE SKIN AT STA L35L, STA 1075 IAW SAA EA 008-5330-01-A1087, UPS RAA DC8-53-20656, AND FAA FORM 8100-9.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 FLOORBEAM AT STA 240 BL-0 HAS CORROSION OUT OF LIMITS. CUT OUT DAMAGED AREA OF FLOORBEAM AT STA 240 BL 0 IAW SRM 53-02-00 FIG 001. FABRICATED AND INSTALLED REPAIR ANGLES AND STRAP AT STA 240 BL 0 IAW SRM 53-02-00 FIG 001.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 INTERCOSTAL CRACKED AT STA 1650 LBL 3. STOP DRILLED CRACKED INTERCOSTAL AT STA 1650 LBL 3 IAW SRM 51-1-21, FABRICATED AND INSTALLED REPAIR DOUBLER ON INTERCOSTAL AT STA 1650 LBL 3 IAW DWG 3704315, AND SRM 53-02-00-0 FIG 001B.

Part: LONGERON SPLICE — CRACKED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 .25 INCH CRACK LWR ROW STA 1749 ON L28R SPLICE AND EXISTING REPAIR THAT IS NOT PER SRO8530032. REMOVED EXISTING REPAIR AND CUT OUT DAMAGED AREA OF L28R SPLICE AT STA 1749 IAW SRO8530032. FABRICATED AND INSTALLED REPAIR FILLERS AND DOUBLERS AT STA 1749 L28R IAW SAA EA 008-5330-01-A1044, UPS EO DC8- 5330-27492-A, AND FAA FORM 8100-9.

Part: FITTING — CORRODED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 MAIN CABIN FRAME FITTING HAS EXFOLIATION CORROSION AND CRACK AT STA 940 L21L. REPAIRED FRAME FITTING AT STA 940 L21L IAW SAA EA 008-5310-01-A1016 UPS RAA DC8-53-20651, AND FAA FORM 8100-9.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 MAIN CABIN FRAME FITTING CRACKED AT STA 980 L19L. REPAIRED MAIN CABIN FRAME FITTING AT STA 980 L19L IAW SAA EA 008- 5310-01-A1020, UPS RAA DC8-53-20655, AND FAA FORM 8100-9.

Part: SKIN — CORRODED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 MAJOR CORROSION BETWEEN STA 1620 - 1640 L31L - L31R, BETWEEN SKIN AND INTERNAL DOUBLER, CORROSION AROUND OUTFLOW VALVE. REMOVED AND REPLACED BELLY SKIN FROM STA 1490 - 1690 L31L - L31R IAW SRM 51-1-20D AND SRM 51-1-21.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 CORROSION UNDER NUT PLATES IN AFT CABIN SUBFLOOR, STA 1746-1756 ALONG RBL 17. REMOVED SUPPORT, REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED SUPPORT ANGLE SRM 51-1-8, 51-1-21, 53-02-00, 51-3-0 DWG 2652479-87. REF TR GMM188.

Part: WEB — DAMAGED (SERVICE DOOR) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 HOLE DRILLED THROUGH FASTENER AND INTO FWD CENTER WEB OF RIGHT FWD SERVICE DOOR INTERIOR. CUT OUT DAMAGED AREA FROM CENTER WEB ON RIGHT FWD SERVICE DOOR IAW SRM 52-02-00 FIG 4. FABRICATED AND INSTALLED REPAIR DOUBLER ON CENTER WEB OF THE RIGHT FWD SERVICE DOOR IAW SRM 52-03-01 FIG 3 AND SRM 52-02-00 FIG 4.

Part: WEB — DAMAGED (SERVICE DOOR) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 LARGE PUNCTURE AND 2EA CRACKS IN WEB AT AFT UPPER SECTION OF INTERIOR OF RIGHT FWD SERVICE DOOR. CUT OUT DAMAGED AREA FROM WEB ON RIGHT FWD SERVICE DOOR IAW SRM 52-02-00 FIG 4. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIGHT FWD SERVICE DOOR UPPER WEB IAW SRM 52-03-01 FIG 3 AND 4.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 FITTING CRACKED AT STA 1240 L20R. REMOVED CRACKED FITTING AT STA 1240 L20R IAW SRM 51-01-20D. FABRICATED AND INSTALLED REPAIR FITTING AT STA 1240 L20R IAW DWG 4750419, AND SRM 51-01-24-0 FIG 002.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 FITTING CRACKED AT STA 1260 L20R. REMOVED AND REPLACED FITTING AT STA 1260 L20R IAW SRM 51-01-20D AND SRM 51-3-2.

Part: WEB — CRACKED (SERVICE DOOR) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 FWD LWR CORNER OF FWD RIGHT SERVICE DOOR HAS CRACK IN WEB. CUT OUT DAMAGED AREA ON FWD LWR CORNER WEB ON RIGHT FWD SERVICE DOOR IAW SRM 52-02-00 FIG 4. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIGHT FWD SERVICE DOOR FWD LWR CORNER IAW SRM 52-02-00 FIG 4, AND SRM 51-09-00 FIG 68.

Part: WEB — PUNCTURED (SERVICE DOOR) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 HOLE PUNCTURED IN INTERIOR WEB OF RIGHT FWD SERVICE DOOR FWD CENTER AREA. CUT OUT DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM5 2-02-00 FIG 4, SRM 52-03-01 FIG 3, 52-02-00, 51-01-21, AND 51-01-11.

Part: FINGER DOUBLER — CRACKED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 CENTER WING BOX SUBFLOOR FINGER DOUBLER CRACKED AT STA 890 LBL 5. REMOVED CRACKED FINGER DOUBLER AT STA 890 LBL 5 IAW SRM 51-1-20D, FABRICATED AND INSTALLED REPAIR FINGER DOUBLER AT STA 890 LBL 5 IAW SRM 53-07-03-0 FIG 004.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 STA 1060 FRAME FITTING IS GOUGED. REMOVED FRAME FITTING AT STA 1060 IAW SRM 51-3-0. LOCATED, DRILLED UP AND INSTALLED NEW FRAME FITTING AT STA 1060 IAW SRM 51-03-02 AND SRM 51-1-20D.

Part: WEB — CRACKED (SERVICE DOOR) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 WEB CRACKED ON RIGHT AFT SERVICE DOOR AFT SIDE BELOW BAYONET. STOP DRILLED END OF CRACK ON WEB IAW SRM 52-02-00 FIG 02. FABRICATED AND INSTALLED REPAIR DOUBLER ON RIGHT AFT SERVICE DOOR WEB IAW SRM 52-02- 00 FIG 02.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 SEAT TRACK GOUGED AT STA 317 RBL 60. REMOVED DAMAGED SEAT TRACK AT STA 317 RBL 60 IAW EO DC8-5340-7779. INSTALLED SEAT TRACK PLUG AT STA 317 RBL 60 IAW EO DC8-5340-7779 APPX A AND SRM 53-2-3 FIG 6D.

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 SEAT TRACK GOUGED OUT OF LIMITS AT STA 240 BL 0. REMOVED AND REPLACED SEAT TRACK SECTION FROM STA 230-250 BL 0 IAW SRM 53-02-03-0 FIG 014, 53-07-03 FIG 2B, AND DWG S2400463.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 FITTING CRACKED AT STA 1230 TO STA 1240 L19R. REMOVED CRACKED FITTING AT STA 1230 TO 1240 L19R IAW SRM 51-01-20D, FABRICATED AND INSTALLED REPAIR FITTING AT STA 1230 TO 1240 L19R IAW SRM 51-01-20D, AND DWG 3758513.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 902 L9L AFT. REMOVED AND REPLACED LONGERON END FITTING AT STA 902 L9L AFT IAW SRM 51-1-20D, AND SRM 51-3-1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 680 L9L FWD. REMOVED CRACKED END FITTING AT STA 680 L9L IAW SRM 51-1-21. LOCATED, DRILLED UP, AND INSTALLED NEW LONGERON END FITTING AT STA 680 L9L IAW SRM 51-01-20D, AND DWG 377972.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 AFT PRESS BULKHEAD CRACKED RBL 24 L10R TO L12R. CUT OUT DAMAGED AREA ON AFT PRESS BULKHEAD STA 1766 RBL 24 L10R TO L12R IAW SRM 53-2-5. FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER AT AFT PRESS BULKHEAD STA 1766 L10R TO L12R IAW SRM 53-2-5 FIG 14A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 LONGERON END FITTING CRACKED AT STA 680 L10R FWD. REMOVED AND REPLACED LONGERON END FITTING AT STA 680 L10R FWD IAW SRM 51-3-0, SRM 51-1-21D, AND 51-01-23.

Part: FITTING — CRACKED (FUSELAGE) · airframe 80,068 hrs · 26,879 cycles

INSPECTION TYPE:C1 FITTING CRACKED AT STA 1160 L19R FWD. REMOVED AND REPLACED LONGERON END FITTING AT STA 1160 L19R IAW SRM 51-1-20D, AND SRM 51-01-24.

Part: GIRT BAR — STIFF (ESCAPE SLIDE)

INSPECTION TYPE:N/A THE EMERGENCY ESCAPE SLIDE GIRT BAR IS VERY DIFFICULT TO ENGAGE & DISENGAGE. REPACKED EMERGENCY ESCAPE SLIDE IN ITS CONTAINER. GIRT BAR STOWS OK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

INSPECTION TYPE:N/A EMERGENCY LIGHTS DISARM CHECK FAIL. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK & CHARGED. OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHT BATTERY DEAD. FOUND DURING PRE-DEPARTURE CHECK. REPLACED PER MM 33-50-01-2, CHECKS OK.

Part: BATTERY PACK — ACTIVATED (EMERGENCY EXIT)

EMERGENCY EXIT LIGHTS DIM. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-01.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHTS DISARM CHECK LIGHT INOP. RELAMPED IAW 33-15-00-2. OPS CK GOOD.

Part: FLAP SYSTEM — SPLIT (WINGS)

RIGHT HAND INBD FLAP OUTBD HINGE BRACKET COVER FWD PANEL CRACKED. INSTALLED INTERIM AIRWORTHY PANEL IAW EO DC8-5720-23117-A. DEFERRAL D312507 PER EO. REPLACED PANEL IAW MM 57-30. THIS CLEARS D312507.

Part: RIB — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3 WHILE WORKING NR 808576, FOUND LT WING I/B FLAP LWR O/B SIDE 3RD RIB FROM LWR AT XW120 CRACKED. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 51-1-21, 57-2-0 FIG 2 SHT 2, 51-1-20D.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 79,190 hrs · 26,210 cycles

C3 - D-PIT DOOR INTERIOR FWD UPPER ANGLE CRACKED JUST BELOW UPPER STOP. REMOVED AND REPLACED DOOR UPPER ANGLE SUPPORT FITTING IAW SRM 51-1-2 AND 51-3-0.

Part: FITTING — CORRODED (FS 1153) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE: C3, DEEP CORROSION PITTING AROUND LOWER FASTENER THRU BATHTUB FITTING AT STA. 1153 ABOVE L33R. REMOVED BATHTUB FITTING, FABRICATED SPLICE ANGLES, INSTALLED FITTING AND SPLICE ANGLES IAW SRM 53-02-00 FIG 2D, 51-1-20D.

Part: LONGERON — CRACKED (BS 1756) · airframe 79,190 hrs · 26,210 cycles

FOUND CRACKED LONGERON AT STA 1756 L14L. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-3-0, 53-2-2 FIG 11 AND 51-1-20D.

Part: LONGERON — CRACKED (BS 1720-1776) · airframe 79,190 hrs · 26,210 cycles

C3 - CRACKED LONGERON AT STA 1736 L15R. CUT OUT DAMAGED LONGERON, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21, 51-1-20D, 53-2-2 FIG 10 AND DWG 5894025.

Part: INTERCOSTAL — CORRODED (BS 1079) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3 HEAVY CORROSION ON INTERCOSTAL AT STA 1079 L35L. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW 51-1-20D AND DWG 9758 507.

Part: FITTING — CORRODED (FS 320) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3 CORROSION ON BACK UP FITTING AT STA 320 BETWEEN L33R-L34R. REMOVED BACK UP FITTING AND INSTALLED REPLACEMENT FITTING AND CLIPS IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CORRODED (BS 315) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3 DEEP CORROSION PIT OR DRILL START IN BATHTUB FITTING TA STA 315 BETWEEN L33R AND L34R. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 51-1-20D, 51-3-0 AND 51- 1-21.

Part: FITTING — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

LT WING XW 408 STRINGER NR 59 UNDER THE BOOST PUMP FITTING CRACKED. REMOVED AND REPLACED BOOST PUMP FITTING IAW SRM 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

LT WING XW 408 STRINGER NR 58 UNDER THE BOOST PUMP FITTING CRACKED. REMOVED AND REPLACED BOOST PUMP FITTING IAW SRM51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (BS 1766) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3 INSIDE 60 HOLE, LONGERON END FITTING CRACKED 2" LONG AT STA 1766 L10R. REMOVED AND REPLACED END FITTING IAW SRM 51-3-0, 51-1-21 AND 51-1-20D.

Part: FITTING — CRACKED (RT WING) · airframe 79,190 hrs · 26,210 cycles

RT WING FUEL TANK NR 4 ALTERNATE STA XW 408 LWR STR NR 58 END FITTING CRACKED 2" LONG. REMOVED AND REPLACED BATHTUB FITTING IAW SRM 51-1-20D.

Part: SKIN — CRACKED (1746) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE: C3, CRACK ON FUSEAGE SKIN STA 1746 L15R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER, FILLER AND FINGER DOUBLER IAW SRM 53-02-01, 53-05-03, 51-1-26, 51-1-20D AND 51-1-21.

Part: CUSP WEB — CRACKED (BS 1535) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3, MAIN DECK STA 1535 WEB AT CUSP AREA IS CRACKED APPROX .5 INCH. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-0 FIG 23 AND DWG 9753254.

Part: DOUBLER — CORRODED (FS 960-980) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3 MAIN CABIN CENTER WING BOX STA 960 TO 980 RBL 65 FINGER DOUBLER HAS CORROSION. REMOVED FINGER DOUBLER, REMOVED CORROSION FROM DOUBLER AND SUBFLOOR FOUND DOUBLER OUT OF LIMITS. FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 51-1-21, 53-02-0 AND 53-07-03.

Part: RIB — CRACKED (RT WING) · airframe 79,190 hrs · 26,210 cycles

C3 - RT WING LE UPPER RIB CRACKED AT XS 484.895. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA. REPAIR ANGLES IAW SRM 57-2-0 FIG 2, 53-3-3 FIG 5.

Part: STIFFENER — CRACKED (RW XW) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE: C3, RIGHT WING L/E, OUTBOARD STUB WING L/E STIFFENER CRACKED 1 INCH LONG AT XW 463.000 NR 4 PYLON UPPER. REMOVED CRACKED STIFFENER, FABRICATED AND INSTALLED REPLACEMENT STIFFENER IAW 51-3-0, 51-1-21A, AND DWG 5769891.

Part: RIB — CRACKED (RT WING) · airframe 79,190 hrs · 26,210 cycles

RT WING LE LOWER RIB IS CRACKED AT XFR 791.250. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 79,190 hrs · 26,210 cycles

C3 - RT WING LE UPPER RIB IS CRACKED AT XFS 347.750. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA. REPAIR ANGLES IAW SRM 57-2-0 FIG 2 AND 57-3-3 FIG 5.

Part: RIB — CHAFED (RT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3, RT WING L/E LOWER RIB IS CHAFED AT XFS 422.750. BLEND OUT OF LIMITS. FABRICATED AND INSTALLED 2 EA ANGLE REPAIRS IAW SRM 57-2-0 FIG 6, 57-3-3 FIG 5 AND 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 835.000. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3 RIGHT OUTER WING OUTBOURD EXTENDED LEADING EDGE UPPER RIB CRACKED AT XFS 722. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0 FIG 2, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 772.500. FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0, 51-1-20D AND 51-1-21.

Part: RIB — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3, LT WING L/E UPPER RIB IS CRACKED AT XFS 778.750. STOP DRILLED, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0.

Part: RIB — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C2, LT WING L/E LOWER RIB IS CRACKED AT XFS 653.750. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0, 5 1-1-20D AND 51-1-21.

Part: RIB — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3 LT WING LE LOWER RIB IS CRACKED AT XFS 622.500. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-3-0 FIG 1 AND 51-1-21.

Part: DOUBLER — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3 LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT DRAIN HOLE AT XFS 335.250. REMOVED INTERNAL DOUBLER. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-3-0, 51-1-20D AND 51-1-21.

Part: SKIN — CORRODED (LT WING) · airframe 79,190 hrs · 26,210 cycles

LEFT WING L/E UPPER SKIN HAS INTERGRANULAR CORROSION AT XFS 785.000. REMOVED CORROSION, FOUND OUT OF LIMITS. FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-8,51-1-21 AND EO DC8-5720-7767-A.

Part: RIB — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3 LT WING LE LOWER RIB PREVIOUS REPAIR IS CRACKED AT XFS 385.250. REMOVED REPAIR ANGLE, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 51 -1-20D, 57-3-3 FIG 5, 57-2-0 FIG 2 AND 51-1-15.

Part: RIB — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

LEFT WING LE LOWER RIB IS CRACKED AT XFS 616.250. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-3-0 FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 822.500. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-2-0, 51-1-21 AND 2-51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3 LT WING LE LOWER RIB PREVIOUS REPAIR IS CRACKED AT XFS 360.250. REMOVED REPAIR ANGLE, FABRICATED AND INSTALLED REPAIR ANGLE.IAW SRM 5 1-1-20D,57-3-3 FIG 5,57-2-0 FIG 2 AND 51-1-15.

Part: RIB — CRACKED (RT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3 RIGHT O/B LEADING EDGE UPPER RIB CRACKED AT XFS 846. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM.

Part: RIB — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE: C3, LT WING L/E UPPER RIB IS CRACKED AT XFS 803.750. STOP DRILLED, FABRICATED DOUBLER AND INSTALLED IAW SRM 51-1-21, 51-1-20D AND 57-2-0.

Part: RIB — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE:C3 LEFT WING L/E UPPER RIB IS CRACKED AT XFS 816.250. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE: C3, LT WING L/E LOWER RIB IS CRACKED AT XFS 660.000. STOP DRILLED CRACK, FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-2-0, 51-1-20D AND 51-1-21.

Part: RIB — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE: C3, LT WING L/E UPPER RIB IS CRACKED AT XFS 297.500. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 57-02-00 FIG 2 AND 51-01-20D.

Part: RIB — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE: C3, LT WING L/E UPPER RIB IS CRACKED AT XS 461.372. STOP DRILLED, FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 21.1.20D, 57-02-00 FIG 2, 57-03-03 FIG 5.

Part: SKIN — CRACKED (LT WING) · airframe 79,190 hrs · 26,210 cycles

INSPECTION TYPE: C3, LEFT WING L/E UPPER SKIN HAS A DAMAGED FASTENER HOLE AT XFS 347.750. FABRICATED AND INSTALLED DOUBLER IAW 57-03-03 FIG 005 PG 1,EO DC8-572 0-7767-A AND SRM 51-1-21.

Part: BULKHEAD — CRACKED (FUSELAGE)

STAB ACCESS COMPT FWD BULKHEAD LEDGE NR 3 CRACKED AT ANGLE ATTACH, LWR (MARKED). REMOVED LT AFT BULKHEAD WALL PANEL OF MAIN CARGO DECK TO FACILITATE SHEET METAL REPAIR. CONT. TO LP 414978 NR 2: REMOVED RIVETS AND BOLTS FROM PRESS BULKHEAD TO FACILITATE REPAIR. BEGAN FABRICATION OF REPAIR PARTS PER EO DC8-5310-6598C. REPAIRED IN STAB COMP AFT PRESS BULKHEAD "J" BEAM PER EO DC8-5310-6598C.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS)

EMERGENCY EXIT LIGHTS FAIL PRE-DEPARTURE CHECK. SWITCH NOT LEFT ENGAGED OVER W/E. REPLACED BATTERY PER MM 33-50-01-2.

Part: WINDOW — FAILED (COCKPIT)

CAPTAINS LEFT SIDE FWD WINDOW SHATTERED DURING CRUISE. DECLARED EMERGENCY DESCENDED TO 10,000 FEET AND DIVERTED TO DFW. R & R CAPTAINS SIDE WINDSHIELD IAW 56-10-02-2.

Part: REGULATOR — LEAKING (O2 BOTTLE)

DURING OXYGEN TEST, NOISE HEARD COMING FROM OXYGEN BOTTLES. REMOVED AND REPLACED CREW 02 BOTTLE REGULATOR WITH REF TO MM 35 10 04 2. OPS CKS OK. OK FOR SERVICE.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY EXIT LIGHTS ARM SWITCH INTERMITTENT. REMOVED AND REPLACED EMERGENCY EXIT LIGHTS ARM SWITCH. OPS CHECK GOOD PER DC8 MM33-50.

Part: WEB — CRACKED (FUSELAGE) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE:C2 LEFT UPPER CUSP IS CRACKED AT STA. 1180 LONG.21L NDT VERIFIED CRACKED AREA, CUTOUT DAMAGE BETWEEN STA. 1170 TO 1190, FABRICATED AND INSTALLED REPAIR DOUBLER AND SPLICES I.A.W. SRM. 53-2-5 FIG. 15

Part: LONGERON — CRACKED (FUSELAGE) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE: C2 STATION 1754 LONG. 14R IS CRACKED. REMOVED DAMAGED LONGERON SECTION BETWEEN STA. 1742 TO 1765, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION I.A.W. SRM. 53-2-2 FIG. 10

Part: FRAME — CORRODED (AFT CABIN) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE: C2, MAIN CABIN CANTED FRAME IS CORRODED BEYOND LIMITS AT STA 1746 AT LONG 26L. REMOVED CANTED FRAME BETWEEN LONG 26L TO 36, FABRICATED AND INSTALLED FRAME AND SPLICES IAW DWG 5612148 AND SRM 53-2-0 FIG 2.

Part: SKIN — CORRODED (HORIZ STAB) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE:C2 RIGHT HORIZONTAL STAB L/E UPPER SKIN IS CORRODED BEYOND LIMITS BETWEEN XFS 172.5 TO XFS 178. CUT OUT CORRODED AREA, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW SRM 55-2-0 FIG 2, 51-1-21 FIG 33.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE:C2 MAIN CABIN LONGERON 16L IS CRACKED AT STA 1750. REMOVED LONGERON SECTION STATION 1742 TO 1765, FABRICATED AND INSTALLED LONGERON SECTION, SPLICE FITTING AND STRAPS IAW SRM 53-2-2 FIG 11.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE: C2 STATION 1750 LONGERON 15R IS CRACKED. CUTOUT DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLE I.A.W. SRM. 53-2-2 FIG. 12

Part: LONGERON — CORRODED (FUSELAGE) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE:C2 MAIN CABIN LONGERON 5R IS CORRODED BEYOND LIMITS AT STA. 1745. CUTOUT DAMAGED AREA,FABRICATED AND INSTALLED FILLER AND REPAIR ANGLE IAW SRM. 53-2-2 FIG. 12

Part: WEB — CORRODED (COCKPIT SUBFLOOR) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE: C2, VERTICLE WEB IN COCKPIT SUBFLOOR IS CORRODED BEYOND LIMITS AT STA -80 LBL 50 AT FUSELAGE SKIN. REMOVED, FABRICATED AND REPLACED WEB/DOUBLER IAW DWG 5613785 AND SRM 51-1-20D, 51-1-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE:C2 MAIN CABIN SEAT TRACK IS CORRODED BEYOND LIMITS AT STA 260 AT LBL 60. CUT OUT DAMAGE AND INSTALLED SEAT TRACK PLUG IAW SRM 53-2-3 FIG 6D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE:C2 LEFT AFT HEAT EXCHANGER EXTERNAL FUSELAGE SKIN LOWER AFT CORNER IS CRACKED STA. -12 AT LONG. 27L CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED DOUBLER AND FILLER I.A.W. E.O. DC8-5330-4732

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE:C2 FUSELAGE SKIN IS CRACKED AT STA. -12 AT LONG. 27R. CUTOUT DAMAGE,NDT VERIFIED NO CRACKS AT CUTOUT,FABRICATED AND INSTALLED DOUBLER AND FILLER I.A.W. E.O. DC8-5330-4732-D

Part: FITTING — CRACKED (FUSELAGE) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE:C2 STATION 1690 LONG. 24L TO FRAME FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. SRM. 51-1-21,53-1-0,AND DWG. 4641324

Part: LONGERON — CRACKED (FUSELAGE) · airframe 78,372 hrs · 25,542 cycles

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

Part: LONGERON — CRACKED (FUSELAGE) · airframe 78,372 hrs · 25,542 cycles

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

Part: ATTACH ANGLE — CRACKED (HORIZ STAB) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE:C2 RT HORIZONTAL STAB. FRONT SPAR AT STA. XFS322. RIB ATTACH ANGLE IS CRACKED REMOVED, FABRICATED AND REPLACED ATTACH ANGLE I.A.W. DWG.4653025 AND SRM. 51-1-20D.

Part: FITTING — CRACKED (FWD. LOWER CARGO) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE: C2, CRACKED BATH TUB FITTING STATION 320 BETWEEN LONG 28L AND 29L. REMOVED AND REPLACED FITTING IAW DWG 3755822 AND SRM 53-2-0 FIG 2D.

Part: WEB — CRACKED (RUDDER) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE:C2 INSIDE RUDDER NR 2 HINGE CUTOUT WEB IS CRACKED AT ZR 159.094. REMOVED, FABRICATED AND REPLACED WEB IAW DWG 5656229 AND SRM 51-1-21, 51-1-20D.

Part: SKIN — CRACKED (RUDDER) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE:C2 SKIN CRACKED LT SIDE OF RUDDER AT BASE AT ZR 61. STOPDRILLED CRACK, NDT VERIFIED STOPDRILL TERMINATES CRACK, FABRICATED AND INSTALLED DOUBLER AND BALANCED RUDDER IAW SRM 55-2-0 FIG 2 AND 51-4-6.

Part: SKIN — CRACKED (AFT FUSELAGE) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE: C2, RADIOGRAPHIC (X-RAY) INSPECTION REVEALED A CRACK ON THE R-2 DOOR UPPER AFT CORNER APPROX. .375 INCH IN LENGTH,STA. 1660 LONG. 11R CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER I.A.W. SRM. 53-2-0 FIG. 16

Part: ANGLE — CRACKED (HORIZ STAB) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE:C2 LEFT HORIZONTAL STAB AT XFS 32 L-ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE IAW DWG 5654501 AND SRM 51-1-20D, 51-1-21.

Part: DOUBLER — CORRODED (RT WING) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE:C2 RIGHT WING LOWER SKIN DOUBLER AT XW 408 IS CORRODED BEYOND LIMITS BETWEEN CENTER AND REAR SPAR. REMOVED, FABRICATED AND INSTALLED DOUBLER IAW DWG 3887776 AND SRM 51-1-20D.

Part: SKIN — CORRODED (RT WING LE) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE: C2, RT WING UPPER SKIN HAS INTERGRANULAR CORROSION BETWEEN XFS 195 TO XFS 220.190. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER AND FILLER IAW EO DC8-5720-7767-A AND SRM 57-3-3 FIG 3.

Part: RIB — CRACKED (RT WING) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE:C2 RIGHT L/E LOWER RIB IS CRACKED AT XFS 347.750. REMOVED EXISTING REPAIR ANGLE, NDT VERIFIED CRACK IS TERMINATED AT STOPDRILL, FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 78,372 hrs · 25,542 cycles

INSPECTION TYPE:C2 COMPLY WITH PERMANENT REPAIR IAW EO DC8-5330-14974-A AT L-1 FWD UPPER CORNER STA 25 AT LONG 10L. REMOVED EXISTING REPAIR, NDT VERIFIED NO CRACKS AT CUTOUT, FABRICATED AND INSTALLED DOUBLER, TRIPLER AND FILLER IAW SRM 53-2-0 FIG 15.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

ON DEPARTURE THE EMERGENCY EXIT LIGHTS WERE DEAD, FOUND BATTERY PACK POWER LOW AFTER TIME OF CHARGER. NEED BATTERY PACK REPLACED. REMOVED & REPLACED EMERGENCY LIGHT BATTERY PACK IAW 33-60-00. LIGHT OPS CK GOOD.

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS DO NOT STAY ON. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT PER MM 33-50-01, OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT FAILED DURING PREFLIGHT. REMOVED AND REPLACED LIGHT ASSY.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 440-460 LONG 14L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3887799,AND SRM. 51-1-20D, 51-1-21

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA -67 FLOORBEAM IS CORRODED BEYOND LIMITS AT LBL 60. REPAIRED FLOORBEAM IAW 8110-3 APPROVED DH SK 874-130

Part: RIB — CRACKED (RT WING) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 RIGHT WING LE LOWER RIB IS CRACKED AT XFS 609. REPAIRED RIB IAW SRM 57-2-0 FIG 2

Part: RIB — CRACKED (RT WING) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 RIGHT WING LE UPPER RIB IS CRACKED AT XFS 585. REPAIRED RIB IAW SRM 57-2-0 FIG 2

Part: RIB — CRACKED (RT WING) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C2 RIGHT WING LE UPPER RIB IS CRACKED AT XFS 641. REPAIRED RIB IAW SRM 57-2-0 FIG 2

Part: WEB — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 1550 AT LONG 21L CUSP MEMBRANE IS CRACKED. REPAIRED MEMBRANE IAW EO DC8-5330-2159

Part: RIB — CRACKED (RT WING) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 RIGHT WING LE UPPER RIB IS CRACKED AT XFS 760. REPAIRED RIB IAW SRM 57-2-0 FIG 2

Part: RIB — CRACKED (RT WING) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 RIGHT WING LE UPPER RIB RIB IS CRACKED AT XFS 691.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2

Part: RIB — CRACKED (RT WING) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 RIGHT WING LE UPPER RIB IS CRACKED AT XFS 697.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA -77 LT NOSE TUNNEL PRESSURE WEB IS CRACKED AT LBL 60. REPAIRED WEB IAW SRO 8530026

Part: RIB — CRACKED (RT WING) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C2 RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 622.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 RIGHT WING LE UPPER RIB IS CRACKED AT XFS 672.5. REPAIRED RIB IAW SRM 57-2-0 FIG 2

Part: RIB — CRACKED (RT WING) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 RIGHT WING LE LOWER RIB IS CRACKED AT XFS 616. REPAIRED RIB IAW SRM 57-2-0 FIG 2

Part: FITTING — CORRODED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 280 LONG 33R BANANA FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755827,AND SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 1180 BATHTUB FITTING IS CRACKED BETWEEN LONG 27L-28L. REMOVED AND REPLACED FITTING IAW DWG 3755842,AND SRM 53-2-0 FIG 2D

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 FINGER DOUBLER IS CORRODED BEYOND LIMITS AT STA -60 AT LBL 16. REMOVED,FABRICATED,AND REPLACED DOUBLER IAW DWG 5612298,AND SRM 51-1-21

Part: FITTING — CORRODED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 1180 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 31L-32L. REMOVED AND REPLACED FITTING IAW DWG 3755844,AND SRM 53-2-0 FIG 2D

Part: FITTING — CORRODED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 1220 BATHTUB FITTING IS CORRODED BEYOND LIMITS BETWEEN LONG 33R-34R. REMOVED AND REPLACED FITTING IAW DWG 3755841,AND SRM 53-2-0 FIG 2D

Part: WEB — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 1447 D-PIT TORQUE BOX WEB IS CRACKED AT LONG 32R. REPAIRED WEB IAW SRM 53-2-0 FIG 1D

Part: LONGERON — CORRODED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 1160-1180 LONG 28L IS CORRODED BEYOND LIMITS. REPAIRED LONGERON IAW SRM 53-2-2 FIG 10

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 1188 LONG 20R UPPER CUSP FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW 3754918 AND SRM 53-1-0, 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 902-920 LONG 8R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659,AND SRM 53-1-0,51- 1-20D,51-1-21

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 1350 LONG 35L-35R FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED,FABRICATED,AND REPLACED DOUBLER IAW DWG 5779915,AND SRM 51-1-20D,51-1-21

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 1260 LONG 20R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED,AND REPLACED FITTING IAW DWG 3755872,AND SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 660-680 LONG 10R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762,AND SRM 51-1-20D, 51-1-21

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 660-680 LONG 11R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 5750540, AND SRM 51-1-20D

Part: FITTING — CORRODED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 8 LONG 33R END FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 4612650U,AND SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 440-460 LONG 17L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3887799,AND SRM 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 798 LONG 18R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4751639,AND SRM 51-1-21

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 857 LONG 19L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779498,AND SRM 51-3-0

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 1200 LONG 20R INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750419,AND SRM 51-1-20D

Part: CLIP — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 680 LONG 18R INTERCOSTAL ATTACH CLIP IS CRACKED. REMOVED,FABRICATED,AND REPLACED CLIP IAW DWG 5887375,AND SRM 51-1-20D

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 1620 LT AFT ENTRY DOOR FRAME WEB IS CRACKED BELOW LOWER HINGE. REPAIRED WEB IAW SRM 53-2-0 FIG 1B

Part: SKIN — CRACKED (FUSELAGE) · airframe 77,242 hrs · 24,753 cycles

INSPECTION TYPE:C1 STA 1723 LONG 15R FUSELAGE SKIN IS CRACKED. REPAIRED SKIN IAW SRM 53-2-1 FIG. 7

Part: CONNECTOR — LOOSE (NR 4 ENGINE)

INSPECTION TYPE:N/A CREW PREFLT- NR 4 ENGINE FIRE DETECTOR FAILED TEST, SECURED NR 4 ENGINE FIRE DETECTOR CORE LOOP CONNECTOR.

Part: HYDRAULIC SYSTEM — LEAKING (FUSELAGE)

INSPECTION TYPE:N/A, HYD QTY LOSS IN FLT.

Part: DOOR — MALFUNCTIONED (RT MLG)

INSPECTION TYPE:N/A, RT MLG DOOR OPENING IN FLT. ACCOMPLISHED GEAR SWING AND UPLATCH CHECK PER M/M 32-31-04. ALL LIGHTS AND INDICATIONS NORMAL.

Part: FRAME — CRACKED (CARGO DOOR)

INSPECTION TYPE:IN P32 DOOR UPPER AFT RADIUS FRAME CRACK. *S/D* REMOVED AND REPLACED NR 32 PIT DOOR ASSY PER DC8-MM 52-32-01, OPS CHK AND LEAK CK GOOD.

Part: AILERON — BINDING (WINGS)

INSPECTION TYPE:IN AILERONS BINDING CYCLED AILERONS, POWER AND FLIGHT SPOILER HYDRAULIC PUMP AND CYCLED FLAPS, AILERONS, AND SPEEDBRAKES. OPS CK OK. NO BINDING FOUND. A/C OK FOR SERVICE. IAW MM 27-10-00

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE)

INSPECTION TYPE:PFLT CREW PREFLT - EMERGENCY ESCAPE SLIDE PRESSURE LOW. SERVICED ESCAPE BOTTLE PER DC-8 MM 25-68-04

Part: FIRE DETECTOR — WILL NOT TEST (NR 4 ENGINE)

INSPECTION TYPE:N/A, PILOT REPORT NR 4 ENGINE FIRE WARNING NO TEST EITHER POSITION. FOUND LOOSE FIRELOOP CONNECTOR. CLEANED AND TIGHTENED CONNECTOR, OPS CK GOOD.

Part: CONNECTOR — LOOSE (BATTERY PACK)

ON CLIMBOUT, EMERGENCY LIGHTING ILLUMINATED. ALL ELECTRICAL BUSSES VOLTS / FREQS WERE NORMAL, BATTERY VOLTAGE NORMAL. FOUND EMERGENCY EXIT LIGHTING CONTROL CB POPPED. RESET WITHOUT FURTHER PROBLEMS.(DC BUS 1) FOUND EMERGENCY LIGHT BATTERY PACK ELECTRICAL CONNECTOR PARTIALLY CONNECTED. RE-CONNECTED ELECTRICAL CONNECTOR AND SYSTEM OPS CHECKED NORMAL AS PER M/M 33-50-01.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY BATTERY PACK.

Part: FITTING — CORRODED (CABIN)

INSPECTION TYPE:N/A, 9G NET ATTACH FITTINGS CORRODED BEYOND REPAIR.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY EXIT LIGHT SWITCH WAS FOUND ON, BATTERY FOUND DEAD. REMOVED AND REPLACED EXIT LIGHT BATTERY PACK. OPS CK GOOD. WORK IAW MM 33-50-01 PN ON AND OFF 5708458-503 SN ON 10886 OFF 10382.

Part: RIB — CRACKED (WS 69)

INSPECTION TYPE:C123, RT WING L/E RIB AT XCW 69 IS CRACKED AT THE UPPER END. STOP DRILLED CRACK AND REPAIRED IAW 57-2-0 FIG 2.

Part: LONGERON — CORRODED (BS 65)

INSPECTION TYPE:C123, LONGERON 23R AT FS 65 IS CORRODED BEYOND LIMITS. CUT OUT DAMAGED SECTION AND SPLICED IN A LONGERON IAW SRM 53-2-2 AND 51-1-20D.

Part: SKIN — CRACKED (WS 438)

INSPECTION TYPE:C123, LT WING LWR SKIN AT APPROX XRS 438, AND STRINGER 68, IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW EO DC8-5730-9004.

Part: RIB — CRACKED (WS 428.75)

INSPECTION TYPE:C123, LT WING L/E RIB AT XFS 428.75 IS CRACKED AT THE AFT LOWER FASTENER. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CORRODED (BS 1540)

INSPECTION TYPE:C123, FS 1540, AT LONGERON 33L, THE SEAT TRACK ATTACH FITTING IS CORRODED BEYOND LIMITS. REMOVED, FABERICATED, AND REPLACED FITTING IAW DH SK874-181 AND SRM 51-1-21 AND 51-3-0.

Part: SPAR CHORD — CRACKED (WS 17)

INSPECTION TYPE:C123, RT WING FWD LWR SPAR CAP, LWR TAG IS CRACKED AT THE FASTENER HOLE AT XFS 17. CUT OUT DAMAGED AREA AND REPAIRED IAW SB 57-30 AND DWG SRO8570012.

Part: DOUBLER — CRACKED (WS 597.5)

INSPECTION TYPE:C123, LT WING L/E LWR SKIN AT XFS 597.5, THE INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21.

Part: SKIN — CRACKED (RT AILERON)

INSPECTION TYPE:C123, RT INBD AILERON UPPER L/E SKIN IS CRACKED JUST OTBD OF THE POWER CYL ATTACH FITTING. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-7767A.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE:C123, LT WING L/E LWR RIBS ARE CRACKED AT XFS 822.5, 797.5, 791.25, 785.0, 778.75; UPPER RIBS ARE CRACKED AT XFS 727.5, 760.0, 766.25, 785.0, AND 828.75. STOP DRILLED CRACKS AND REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: CLIP — CRACKED (WS 267)

INSPECTION TYPE:C123, RT WING L/E, ABOVE THE NR 3 PYLON, APPROX STA XFS 267, THE RIB FWD ATTACH CLIP IS CRACKED. REMOVED, FABRICATED, AND REPLACED THE CLIP IAW DWG 9753294 AND SRM 51-1-20D.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE:C123, LT WING L/E UPPER RIBS CRACKED AT XS 484.895 AND 448.58. STOP DRILLED CRACKS AND REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE:C123, LT WING L/E HAS RIBS CRACKED AT XFS 672.5, 660.0, 641.25 AT THE UPPER RIB; AND LOWER RIB AT XFS 603.75. STOP DRILLED CRACKS AND REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (RT WING)

INSPECTION TYPE:C123, NR 3 MAIN TANK INBD AFT ACCESS PANEL LAND IS CRACKED AT 2 FASTENER HOLES, (ACCESS PANEL 505F). CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 36.

Part: DOUBLER — CORRODED (BS 5)

INSPECTION TYPE:C123, SEVERAL POPPED RIVETS AND BULGING IN FINGER DOUBLER, FS 5, LBL 65. REMOVED, FABRICATED, AND REPLACED FINGER DOUBLER IAW SRM 53-3-3 FIG 6 AND 51-1-21.

Part: DOUBLER — CRACKED (WS 597.5)

INSPECTION TYPE:C123, RT WING L/E AT XFS 597.5, THE SKIN INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED, AND REPLACED THE DOUBLER IAW DWG 5769600 AND SRM 51-1-21.

Part: RIB — CRACKED (LT HORIZ STAB)

INSPECTION TYPE:C123, LT HORIZ STAB L/E RIB AT XFS 141.25 IS CRACKED AT THE AFT LOWER END. STOP DRILLED CRACK AND REPAIRED IAW SRM 55-2-0 FIG 2.

Part: ANGLE — CRACKED (BS 760)

INSPECTION TYPE:C123, ANGLE CRACKED, LT SIDE LWR CENTER WING AT FS 760, XCW 69. REMOVED, FABRICATED, AND REPLACED ANGLE IAW DWG 5649893 AND SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1225)

INSPECTION TYPE:C123, LONGERON 32L AT FS 1225 HAS HEAVY CORROSION. REPAIRED IAW EO DC8-5310-11651A AND DH SK874-683.

Part: FITTING — CRACKED (BS 781)

INSPECTION TYPE:C123, FWD SIDE OF THE FS 781 FRAME, AT LONGERON 18R, THE INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D.

Part: FRAME — CRACKED (BS 55)

INSPECTION TYPE:C123, FS 55 FRAME AT LONGERON 24R IS CRACKED AT THE DUCT SUPPORT BRACKET. CUT OUT DAMAGED SECTION AND REPAIRED IAW SRM 53-2-0 FIG 2.

Part: FRAME — CRACKED (BS 55)

INSPECTION TYPE:C123, FS 55 FRAME AT LONGERON 24L IS CRACKED AT THE DUCT SUPPORT BRACKET. CUT OUT DAMAGED SECTION AND REPAIRED FRAME IAW SRM 53-2-0 FIG 2.

Part: LONGERON — CRACKED (FS 894)

INSPECTION TYPE:C123, FS 894, LONGERON 24R IS CRACKED. REPAIRED LONGERON IAW DH SK874-640.

Part: FITTING — CRACKED (BS 1160)

INSPECTION TYPE:C123, FS 1160, BETWEEN LONGERON 34R AND 33R, THE BATHTUB FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (BS 980)

INSPECTION TYPE:C123, FLOORBEAM ATTACH FITTING IS CRACKED AT FS 980 BULKHEAD AT LBL 24. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG 3751514 AND SRM 51-1-20D.

Part: FITTING — CORRODED (BS 72)

INSPECTION TYPE:C123, LONGERON 30R AT FS 72 HAS MODERATE CORROSION. REMOVED AND REPLACED THE FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 280)

INSPECTION TYPE:C123, FLOORBEAM ATTACH FITTING AT FS 280, RBL 57, IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (WS 410)

INSPECTION TYPE:C123, THE RT STA 410 FLAP UP STOP FITTING IS CRACKED. REMOVED AND REPLACED STOP FITTING IAW SRM 51-3-0.

Part: SKIN — CRACKED (WS 330)

INSPECTION TYPE:C123 RT WING L/E UPPER SKIN AT XFS 330, AT THE SPAR, HAS INTERGRANNULAR CORROSION AND IS CRACKED. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1 FIG 38.

Part: RIB — CRACKED (WS 453)

INSPECTION TYPE:C123, RT WING OTBD SLOT, UPPER OTBD CLOSURE RIB AT XW 453 IS CRACKED AT THE AFT END. REMOVED AND REPLACED RIB IAW SRM 51-1-20D AND 51-3-0.

Part: SKIN — CRACKED (WS 257.5)

INSPECTION TYPE:C123, RT WING L/E UPPER SKIN AT XW 257.5, 33 FWD OF THE SPAR, IS CRACKED BETWEEN 2 FASTENER HOLES. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1.

Part: SKIN — CORRODED (WS 761.75)

INSPECTION TYPE:C123, RT WING L/E LWR SKIN, AT THE L/E, STA XW 761.75 HAS INTERGRANNULAR CORROSION AROUND 2 SCREWS. CUT OUT DAMAGED AREA AND REPAIRED IAW EO DC8-5720-4087B.

Part: SKIN — CRACKED (WS 422.75)

INSPECTION TYPE:C123, LT WING L/E LWR SKIN AT XFS 422.75 IS CRACKED AT A FASTENER. STOP DRILLED CRACK AND REPAIRED IAW EO DC8-5720-4087B.

Part: FITTING — CORRODED (BS 320)

INSPECTION TYPE-C, STA 320 BETWEEN STR 35L TO 36, THE BACK-UP FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D.

Part: CARGO TRACK — CORRODED (BS 360-440)

INSPECTION TYPE-C, STA 360 TO 440 ABOVE STR 33R, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 52955978 AND SRM 51-3-0.

Part: CARGO TRACK — CORRODED (BS 1140)

INSPECTION TYPE-C, STA 1140 ABOVE STR 33R, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 5759223 AND SRM 51-3-0.

Part: FITTING — CRACKED (BS 1260-1280)

INSPECTION TYPE:C, STA 1260-1280, STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 51-1-20.

Part: CARGO TRACK — CORRODED (BS 1140)

INSPECTION TYPE-C, STA 1140, ABOVE STR 33L, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 5759223.

Part: SPLICE — CRACKED (BS 1040-1060)

INSPECTION TYPE-C, FS 1040 TO 1060 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-3-0.

Part: LONGERON — CORRODED (BS 1160-1220)

INSPECTION TYPE-C, LONGERON 31L AND FINGER DOUBLER HAVE CORROSION BTWN STA 1160 TO 1220. REMOVED CORROSION FROM DOUBLER AND REPAIRED LONGERON 31L IAW 8110- 3 APPROVED DHC SK 874-770.

Part: CARGO TRACK — CORRODED (BS 1240-1260)

INSPECTION TYPE-C, STA 1240 TO 1260 ABOVE STR 33L, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 5759223 AND SRM 51-3-0.

Part: RIB — CRACKED (WS 666.25)

INSPECTION TYPE:C, RT WING L/E AT STA XFS.666.250, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 635)

INSPECTION TYPE:C, RT WING L/E AT STA XFS635.000, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: STRAP — CRACKED (WS 621)

INSPECTION TYPE:C, RT WING L/E AT STA XFS621.000, THE L/E RIB TIE STRAP IS CRACKED. REMOVED, FABRICATED AND REPLACED STRAP IAW DWG 5655441 AND SRM 51-1-21.

Part: RIB — CRACKED (WS 616.25)

INSPECTION TYPE:C, RT WING L/E AT STA XFS 616.250, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 397.75)

INSPECTION TYPE:C, RT WING L/E AT STA XFS397.750, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 621)

INSPECTION TYPE:C, RT WING L/E AT STA XFS.621.000, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 440-460)

INSPECTION TYPE:C, STA 440-460, STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3750257 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1040-1060)

INSPECTION TYPE:C, STA 1040-1060, STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW DWG.3750257 QND SRM 51-3 -0.

Part: DOUBLER — CRACKED (BS 426)

INSPECTION TYPE:C, STA 426 AT LONGERON 34L, THE FINGER DOUBLER IS CRACKED. REPAIRED THE AREA IAW 8110-3 APPROVED DHC SK 874-569.

Part: CARGO TRACK — CORRODED (BS 70-260)

INSPECTION TYPE-C,STA 70 TO 260 ABOVE STR 33L, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 5759223 AND SRM 51-3-0.

Part: LONGERON — CORRODED (BS 280-340)

INSPECTION TYPE:C, LONGERON 29L AND 30L BETWEEN STA 280-340 EACH HAVE HEAVY CORROSION. REPAIRED AREAS IAW SRM 53-2-2 AND SRM 51-1-20D.

Part: SKIN — CRACKED (WS 598)

INSPECTION TYPE:C, LT WING L/E LWR SKIN AT STA XFS598.000 IS CRACKED AT THE DRAIN HOLE AND 1 SCREW. STOP DRILLED CRACKS AND REPAIRED IAW SRM ADD DC8-5320-4087.

Part: CARGO TRACK — CORRODED (BS 70-260)

INSPECTION TYPE-C, STA 70 TO 260 ABOVE STR 33R, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 5759223 AND SRM 51-3-0.

Part: CARGO TRACK — CORRODED (BS 470-640)

INSPECTION TYPE-C, STA 470 TO 640 ABOVE STR 33L, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 5759223 AND SRM 51-3-0.

Part: FITTING — CRACKED (LT WING)

INSPECTION TYPE-C, LT WING NR 4 FLAP HINGE ACTUATOR MOUNT FITTING IS CRACKED. REMOVED AND REPLACED CANOE FITTING IAW MM 27-51-00.

Part: RIB — CRACKED (WS 397.75)

INSPECTION TYPE:C, LT WING L/E AT STA XFS397.750, THE LWR L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (WS 409)

INSPECTION TYPE-C, THE RT WING FLAP HINGE SUPPORT FITTING AT STA XF 409.6673, INBOARD SIDE HAS A CRACK. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: BATT PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS ILLUMINATED DURING TAXI OUT W\SWITCH IN THE ARMED POSITION. REMOVED AND REPLACED BATTERY PACK, EMERG LIGHT CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS WILL NOT TURN OFF WITH SWITCH. REPLACED BATTERY PACK.

Part: SKIN — CRACKED (SERVICE DOOR)

INSPECTION TYPE-S/N, CRACK FOUND IN FWD LOWER CORNER OF LEFT AFT UPPER DECK SERVICE DOOR. INSTALLED TEMP REPAIR IAW SRM 53-2-1 PERMANENT REPAIR TO BE ACCOMPLISHED WITH IN 1000 CYCLES.

Part: TE BOX — CRACKED (WHEEL WELL)

INSPECTION TYPE-N/A, CRACK IN TRAILING EDGE BOX INBD TO OUTBD WHEEL WELL. DEFERRED AS D138752 PER MMOC AND PER EO DC8-5720-9758-A PERMANENT REPAIR TO BE ACCOMPLISHED NEXT B OR BEFORE.

Part: SKIN — CRACKED (LT WING)

INSPECTION TYPE-N/A, LEFT WING UNDER SIDE SKIN JUST FWD OF FUEL DUMP SHOOT CRACKED AROUND FASTENERS. REMOVED DAMAGED SKIN CUT OUT APPROX 8 BY 6, 75839 2 FABRICATED DOUBLER AND SHIMS 66193 3, INSTALLED DOUBLER IAW SRM DC-8-5350-7376A.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE-N/A, CORROSION AROUND MARKER BEACON (AFT SECTION ON BELLY SKIN). REPAIRED IAW SRM 53-2-1 AND EO DC8-5330-8271-B.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS INOP ON PRE-DEPARTURE CK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CK OK.

Part: DRAIN CAP — LOOSE (NR 4 ENGINE)

INSPECTION TYPE-N/A, DURING 2.5 HR FLIGHT MONITORED NR 4 OIL QTY DROP TO JUST OVER 2 QTS. PERFORMED INFLIGHT ENGINE SHUTDOWN IAW QRH, AIR DIVERT TO BOS. FOUND NR 4 ENG QAD PAD DRAIN FITTING CAP BACKED OFF, TORQUES CAP AND RAN ENG, NO FURTHER LEAKS NOTED 80-10-01 IAW.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS FAILED, BATTERY PACK LOW. REMOVED AND REPLACED EMERGENCY LIGHTS BATERY PACK PER M/M 33-50.

Part: PLUG PACKING — DETERIORATED (NR 2 ENG STARTER)

CREW REPORTED, NR 2 ENGINE IN FLIGHT SHUTDOWN AND DECLARED EMERGENCY DUE TO LOSS OF OIL QUANTITY AND PRESSURE. REMOVED AND REPLACED STARTER SVC PLUG PACKING.

Part: FITTING — CORRODED (FS 160)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON END FITTING, LONGERON 21R, FS 160. REPLACED FITTING PER SRM 51-1-20D.

Part: DOUBLER — CRACKED (FS 80-100)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON FINGER DOUBLER AT FS 80 TO 100, LONGERON 28R. REPLACED DOUBLER PER SRM 51-1-21, 51-1-20D.

Part: SPAR — CRACKED (LT WING)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON LT WING REAR SPAR T-ANGLE AT XSF 64. INSTALLED REPAIR PER UPS EO FILE NR DC8-57-0558.

Part: ANGLE — CRACKED (FS 640)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK AND CORROSION IN B-BAY BIN, AFT BULKHEAD, FS 640, LBL 24, LT TUNNEL VERTICAL ANGLE NEXT TO MAIN CARGO FLOOR. INSTALLED REPAIR PER SRM 53-2-0.

Part: FITTING — CRACKED (FS 160)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON END FITTING AT LONGERON 21R, FS 160. REPLACED PER SRM 51-1-20D.

Part: FRAME — CRACKED (FS 720)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON BELT FRAME AT STA 720, LONGERON 34L. INSTALLED REPAIR PER SRM 53-2-0.

Part: FITTING — CRACKED (NR 2 PYLON)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON NR 2 PYLON FOOT STOOL FITTING AT LWR I/B CORNER. REPLACED FITTING PER UPS EO FILE NR DC8-57-0551.

Part: SKIN — CRACKED (RT WING LE)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON RT WING L/E LWR SURFACE XFS 320. REPAIRED SKIN PER SRM 57-2-1.

Part: SKIN — CRACKED (RT WING LE)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON RT WING L/E UPPER SKIN AT XFS 220. INSTALLED REPAIR PER UPS EO DC8-57-0557.

Part: SKIN — CRACKED (LT WING LE)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON LT WING L/E UPPER SKIN, STA XFS 285. REPAIR SKIN PER SRM 57-20-0.

Part: FITTING — CRACKED (FS 902/870)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON VERTICAL LEG OF TRAP FITTING AT STA 902 AFT SIDE, AND AT FWD LEG FS 870. REPLACED FITTING PER SRM 51-1-20D.

Part: LONGERON — CRACKED (FS 386-390)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON LONGERON 35L AT FS 386 TO 390. REPLACED LONGERON SECTION PER SRM 51-1-20D.

Part: LE RIB — CRACKED (LT WING)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON 3 RIBS ON LT WING L/E AT XFS 291, 354, AND 201. REPAIRED RIBS PER SRM 57-2-0.

Part: SKIN — CRACKED (LT WING LE)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON LT WING L/E, UPPER SURFACE, APPROX 12 FROM I/B SLOT, 28 FWD OF FRONT SPAR. INSTALLED REPAIR PER SRM 57-20-0.

Part: FITTING — CRACKED (FS 702)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON LT BELT FRAME END FITTING FS 702 LONGERON 21L. REPLACED FITTING PER SRM 51-1-20D.

Part: SKIN — CRACKED (RT WING LE)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK (2EA) ON RT WING L/E LWR SURFACE AT XFS 591 AND 240. REPLACED SKIN PER SRM 57-2-0.

Part: FRAME — CORRODED (FS 1000)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON BELT FRAME FS 1000, BETWEEN LONGERONS 35L TO 35R. INSTALLED REPAIR PER UPS EO DC8-5310-6966A.

Part: DOUBLER — CORRODED (FS 220-400)

DURING 'C' CHECK, MAINTENANCE FOUND INNER DOUBLER CORRODED AT FS 220 TO 400, LONGERONS 35L TO 31R. REPLACED DOUBLERS PER DOUGLAS DRAWING NR 5755271, 9755878.

Part: DOUBLER — CORRODED (FS 190-450)

DURING 'C' CHECK, MAINTENANCE FOUND SKIN CORRODED AT FS 190 TO 450. REPLACED SKIN PANEL PER DOUGLAS DRAWING NR 5755271.

Part: SKIN — CORRODED (WS 307)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION AT LOWER SURFACE SKIN OF RT WING STA XFS 307. REPAIRED SKIN PER SRM 57-2-1, 51-1-8, 57-2-0.

Part: DOOR — CRACK (NR 4 PIT DOOR)

MAINTENANCE REPORTED,NR 4 PIT DOOR HAS CRACK IN LOWER AFT BOTTOM OF DOOR APPROX 1 INCH LONG. INSTALLED REPAIR IAW SRM 52-2-0.