N779UP

Part: FASTENER — CORRODED (FUSELAGE)

INSPECTION TYPE:N/A SEVERAL FASTENERS CORRODED IN COMPARTMENT 60 HORZ STABILIZER ACTUATING MECHANISM AREA ITEM SUBMITTED BY FOG TEAM. REMOVED AND REPLACED FASTENERS. CLEANED CORROSION FROM MARKET BOTLS APPROX 120 EA HUCK FASTENERS EXTENDING THROUGH LIGHTENING HOLES. CLEANED 20 EACH FASTENERS AND HEADS.

Part: STIFFENER — CRACKED (FUSELAGE)

INSPECTION TYPE:B COMPARTMENT 60 AFT PRESS BULKHEAD J-BEAM 5TH FROM BOTTOM OF LT SIDE HAS CRACK AS MARKED. STOP DRILLED CRACK REF DC8-5310-15663-A14596. FABRICATED UPPER REPAIR BRACKET PER PRELIMINARY EO DC8-5310-15663-A DP 70236.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE)

INSPECTION TYPE:IN, CABIN DOOR EMERGENCY SLIDE BOTTLE PRESS LOW. REMOVED AND REPLACED CABIN DOOR EMERGENCY SLIDE AS PER MM 25-60-00.

Part: SKIN — DAMAGED (TE FLAP)

INSPECTION TYPE:PFLT LT WING INBD FLAP T/E HAS A 1/2 HOLE 2 INCHES INBD OF OUTBD EDGE. REPAIRED HOLE IN FLAP AS PER SRM 57-2-1. INSTALL A REPAIR DOUBLER.

Part: SLIDE — INOPERATIVE (DOOR)

INSPECTION TYPE:N/A, ESCAPE SLIDE WILL NOT ARM. ATTACHED GIRT BAR.

Part: LINE — LEAKING (COCKPIT OXYGEN)

INSPECTION TYPE:N/A, COURIER''S O2 REGULATOR PROBLEM. *S/D* REPLACED BROKEN O2 LINE, OPS CK NORMAL.

Part: LONGERON — CRACKED (CARGO BAY) · airframe 71,223 hrs · 46,980 cycles

INSPECTION TYPE:C1, STA 1350 LONG 34L IS CRACKED. REMOVED AND REPLACED LONGERON IAW DWG 3758593, AND SRM 51-1-20D, 51-1-21.

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 71,223 hrs · 46,980 cycles

INSPECTION TYPE:C1, STA 1690 - 1776 LONG 32L HAS HOLES IN RADIUS. REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG 5649329, AND SRM 51-1-20D.

Part: FITTING — DAMAGED (FUSELAGE) · airframe 71,223 hrs · 46,980 cycles

INSPECTION TYPE:C1, STA 1690 LONG 32L END HAS HOLES WITH NO EDGE DISTANCE. REMOVED AND REPLACED FITTING IAW DWG 4641324, AND SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (CARGO BAY) · airframe 71,223 hrs · 46,980 cycles

INSPECTION TYPE:C1, STA 240 - 260 LONG 33L INTERCOSTAL IS CRACKED. REMOVED, FABRICATED, AND REPLACED INTERCOSTAL IAW DWG 5750726, AND SRM 51-1-21.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 71,223 hrs · 46,980 cycles

INSPECTION TYPE:C1, STA 1760 LONG 28L - 28R 8 SHEAR TIES ARE CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED SHEAR TIES IAW 5612148, AND SRM 51-1-21.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 71,223 hrs · 46,980 cycles

INSPECTION TYPE:C1, STA 1705 LONG 30L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED, AND REPLACED LONGERON IAW DWG 5649329, AND SRM 51-1-20D.

Part: FINGER DOUBLER — CRACKED (FUSELAGE) · airframe 71,223 hrs · 46,980 cycles

INSPECTION TYPE:C1, STA 1690 - 1890 FINGER DOUBLERS IS CRACKED AT LONG 28R. REMOVED, FABRICATED, AND REPLACED DOUBLERS IAW DWG 5649328, AND SRM 51-1-21.

Part: RIB — CRACKED (LEFT WING) · airframe 71,223 hrs · 46,980 cycles

INSPECTION TYPE:C1, LEFT WING L/E LOWER RIB IS CRACKED AT XFS 310.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (LT WING) · airframe 71,223 hrs · 46,980 cycles

INSPECTION TYPE:C1, LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 335.25. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW DWG 5769589, AND SRM 51-1-20D, 51-1-21.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:P/F, ON PREFLIGHT LIGHTS DO NOT COME ON DURNIG TEST. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD.

Part: GEARBOX — INOPERATIVE (HORIZONTAL STAB)

INSPECTION TYPE:N/A, HORIZONTAL STABILIZER STOPPED MOVING AFTER LANDING AT 4.0 DEGREES. FOUND RIVET STUCK IN HORZ STAB GEARBOX ASSY. REMOVED AND REPLACED GEARBOX ASSY AND BOTH JACKSCREW ASSYS.

Part: LANYARD — BROKEN (SLIDE)

INSPECTION TYPE:N/A, SLIDE COVER LANYARD BROKEN AT CABLE (SLIDE AT ENTRY DOOR). REPLACED MAIN ENTRY DOOR SLIDE COVER LANYARD AND SECURED SLIDE LANYARD INSTALLED PER IPC 25-62-00.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTING WILL NOT TEST. REPLACED EMERGENCY EXIT LIGHT BATTERY PACK.

Part: CLIP — BROKEN (ESCAPE SLIDE)

INSPECTION TYPE:N/A, MAIN CABIN ESCAPE SLIDE INOP, MOUNTING BRACKET BOTTOM CLIP BROKEN. REMOVED AND REPLACED CLIP AND INSTALLED ESCAPE SLIDE.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY EXIT LIGHTS FAILED TO COME ON DURING PREFLIGHT CHECK. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK PN ON 5208458-503, PN OFF 570845 8-503 SN ON 976 SN OFF 2054, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS DID NOT OPERATE WHEN TESTED. REMOVED AND REPLACED EMERGENCY BATTERY PACK ASSY PER M/M 33-50-01, OPS CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION TYPE:N/A, FUSELAGE SKIN DAMAGE JUST AFT OF THE NLG W/W HAS AN 11 INCH CRACK. DUE TO LEFT NOSE TIRE TREAD SEPARATION. *S/D* DAMAGE REMOVED AS REQ'D RHODES 75705 RSB 0596 1 QC 2, FABRICATED AND DRILLED DOUBLER PER UPS DRAWING UPS-SDF-9900296 F BPT 92716. OK TO INSTALL RSB 05961 QC3. INSTALLED 98 PERCENT OF FASTENERS IN DOUBLER SEATED EXTERIOR OF DOUBLER, COMPLETE D INTERIM REPAIR.

Part: SKIN — CRACKED (BS 1704-1717)

INSPECTION TYPE:N/A, 13.25 INCH CRACK LOCATED AT LONGERON L28 ON SKIN OF AIPLANE FS 1704 TO FS 1717 (FOR AND AFT). *S/D* REMOVED DAMAGED SECTION, FABRICATED REPAIR PARTS IAW DC8 SRM 53-2-1 FIG 4. INSTALLED PARTS IAW SRM 53-2-1, 51-1-23 D AND 51-1-21.

Part: DOUBLER — CRACKED (WS 598.375)

INSPECTION TYPE-C3, RT WING L/E LWR SKIN AT XFS 598.375 THE INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED THE INTERNAL DOUBLER IAW DWG 5769600 AND SRM 51-1-20D & 51-1-21.

Part: ANGLE — CRACKED (NR 1 STUB WING)

INSPECTION TYPE-D, VERTICAL ATTACHMENT ANGLE ON THE I/B SIDE OF THE NR 1 STUB WING CRACKED IN RADIUS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-21 AND DWG 9753297.

Part: JAMB — CRACKED (PAX DOOR)

INSPECTION TYPE-D, DOOR JAMB AFT ENTRY DOOR AFT LOWER CORNER HAS 2 INCH CRACK. REPAIRED IAW SRM 53-2-0.

Part: INTERCOSTAL — CRACKED (BS 1120 - 1140)

INSPECTION TYPE-C3, FS 1120 TO 1140 AT LONG 33L THE INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9753792 AND SRM 51-1-20D & 51-1-21.

Part: FITTING — CORRODED (BS 1752)

INSPECTION TYPE-D, FITTING CORRODED FS 1752 BL 0. REMOVED AND REPLACED FITTING IAW SRM 51-1-21D.

Part: FITTING — CRACKED (BS 1150)

INSPECTION TYPE-D, BATHTUB FITTING IS CRACKED AT STA 1150 L-34R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 280)

INSPECTION TYPE-D, FITTING AT FS 280 L-34R CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 385)

INSPECTION TYPE-D, CRACKED RIB AT XFS 385.25 LWR RIB LT L/E. REPAIRED IAW SRM 57-2-0.

Part: FITTING — CRACKED (RT HORZ STAB)

INSPECTION TYPE-C3, RT HORIZONTAL STAB O/B CENTER STA XFA 178 FRONT SPAR SHEAR TIE IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3653802 AND SRM 51-1-20D, 51-1-21 AND 51-3-0.

Part: FRAME — CRACKED (BS 1746)

INSPECTION TYPE-D, FRAME 1746 LOWER FLANGE CRACKED AND CORRODED AT L-35R. REPAIRED IAW SRM 53-2-0.

Part: LONGERON — CORRODED (BS 1140)

INSPECTION TYPE:C LONGERON 33L CORRODED AT F/S 1140. REPAIRED IAW SRM 53-2-2.

Part: BULKHEAD FITTING — CRACKED (WS 74)

INSPECTION TYPE-D, NR 3 MAIN TANK AT THE XRS 74 BULKHEAD STRINGER 51 AFT ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: RIB — CRACKED (VERT STAB)

INSPECTION TYPE-C3, VERTICAL STAB L/E RIB AT ZFS 223 IS CRACKED AT THE LT AFT END. STOPPED DRILLED CRACK AND REPAIRED RIB IAW SRM 55-2-0.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE-D, FS 70 LONGERON 27R END FITTING CORROSION REMOVAL BEYOND SRM LIMITS. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: DOUBLER — CRACKED (BS 1060)

INSPECTION TYPE-C3, FS 1060, JUST BELOW LONG 21R THE FINGER DOUBLER IS CRACKED. REPAIRED FINGER DOUBLER IAW DHC SK 779-268.

Part: RIB — CRACKED (WS 741)

INSPECTION TYPE-D, RT WING L/E RIB AT XFS 741.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: SPLICE — CRACKED (BS 640-660)

INSPECTION TYPE-D, FS 640 TO 660 STRINGER 1 SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 585)

INSPECTION TYPE-C, 3 LT WING L/E RIB AT XFS 585.0 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED L/E RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 822.5)

INSPECTION TYPE-D, RT WING L/E RIB AT XFS822.5 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 778)

INSPECTION TYPE-D, RT WING L/E RIB AT 778.75 IS CRACKED AT THE AFT LWR END. REPAIRED IAW SRM 57-2-0.

Part: DOUBLER — CRACKED (WS 570)

INSPECTION TYPE-C, 3 RT WING L/E LWR SKIN AT XFS 570.75, THE INTERNAL DOUBLER IS CRACKED AT THE DRAIN HOLE. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D AND 51-1-21.

Part: FITTING — CORRODED (BS 320)

INSPECTION TYPE-C, 3 BULGING CORROSION ON BATHTUB FITTING FWD SIDE FS 320 BETWEEN LONG 32L AND 33L. REMOVED AND REPLACED FITTING IAW SRM 53-2-0, 51-1-20D.

Part: RIB — CRACKED (WS 635)

INSPECTION TYPE-D, LT WING L/E RIB AT XFS 635.0 IS CRACKED AT AFT LWR END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 791.25)

INSPECTION TYPE-D, LT WING L/E RIB AT XFS 791.25 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE-C, CRACKED FRAME FITTING AT LONG 11L FS 680. REMOVED AND REPLACED FITTING IAW SRM 51-1-21D.

Part: RIB — CRACKED (WS 760)

INSPECTION TYPE-D, LT WING L/E RIB AT XFS 760 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: ANGLE — CRACKED (BS 798)

INSPECTION TYPE-C, 3 LWR FLOORBEAM WEB ATTACH ANGLE CRACKED AT FS 798 AND LBL 49. REMOVED AND REPLACED ANGLE IAW SRM 51-1-20D.

Part: RIB — CRACKED (WS 484.895)

INSPECTION TYPE-D, LT WING L/E RIB AT XS 484.895 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 810)

INSPECTION TYPE-D, LT WING L/E RIB AT XFS 810.0 IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 335.25)

INSPECTION TYPE-C, 3 LT WING L/E RIB AT XFS 335.25 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED RIB IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 566.25)

INSPECTION TYPE-C, 3 RT WING L/E RIB AT XFS 566.25 IS CRACKED AT THE AFT LWR END. STOP DRILLED AND REPAIRED RIB IAW SRM 57-2-0.

Part: GUSSET — BROKEN (FUSELAGE)

INSPECTION TYPE-C, 3 FRAME GUSSET AT UPPER AFT CORNER OF F/O'S EYEBROW WINDOW IS BROKEN. REMOVED, FABRICATED AND REPLACED GUSSET IAW DWG 5313856 AND SRM 51-1-21.

Part: RIB — CRACKED (WS 797.5)

INSPECTION TYPE-C, 3 LT WING L/E RIB AT XFS 797.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 304)

INSPECTION TYPE-C, 3 LT WING L/E RIB AT XFS 304.0 IS CRACKED AT THE FWD PNEU DUCT SUPPORT FITTING. STOP DRILLED CRACK AND REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: INTERCOSTAL — CRACKED (BS 857)

INSPECTION TYPE-D, CRACKED INTERCOSTAL FITTING AT LONGERON 19L FS 857. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 822)

INSPECTION TYPE-D, CRACKED FRAME CUSP FITTING AT FS 822 LT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21 AND DWG 3616945.

Part: RIB — CRACKED (WS 250)

INSPECTION TYPE-C, 3 RT WING L/E RIB AT XS 250.089 IS CRACKED 6 INCHES FWD OF THE SPAR. STOP DRILLED AND REPAIRED RIB IAW SRM 57-2-0.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE-C, 3 LONG 3R END FITTING AT FS 857 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-21, 51-3-0.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE-C, 3 LONG 7R END FITTING AT FS 857 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-21, 51-3-0.

Part: ANGLE — CRACKED (WS 256)

INSPECTION TYPE-C, 3 RT WING L/E RIB AT XW 256, ABOVE THE NR 3 PYLON, THE RIB FWD ATTACH CLIP IS CRACKED. REMOVED, FABRICATED AND REPLACED CLIP IAW DWG 9753294 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE-D, LONGERON 9L END FITTING CRACKED FS 680. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21 AND DWG 3779762.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE-C, 3 LONG 8R END FITTING IS CRACKED AT FS 857. REMOVED AND REPLACED FITTING IAW SRM 5-1-20D, 51-1-21 AND 51-3-0.

Part: FITTNG — CRACKED (BS 857)

INSPECTION TYPE-C, 3 LONG 5L END FITTING CRACKED AT FS 857. REMOVED AND REPLACED LONG END FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: RIB — CRACKED (WS 372.75)

INSPECTION TYPE-C, 3 RT WING L/E RIB AT XFS 372.75 IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED RIB IAW SRM 57-2-0.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE-C, 3 LONG 7L END FITTING CRACKED AT FS 857. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE-C, 3 LONG 4R END FITTING AT FS 857 IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-21 AND 51-3-0.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE-C, 3 LONG 6L END FITTING CRACKED AT FS 857. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 51-1-21, 51-3-0.

Part: RIB — CRACKED (WS 360.25)

INSPECTION TYPE-C, 3 RT WING LWR L/E RIB AT XFS 360.25 IS CRACKED BEYOND THE DOUBLER. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (BS 1160)

INSPECTION TYPE-C, 3 INTERCOSTAL END FITTING CRACKED AT FS 1160, LONG 18R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (RT WING)

INSPECTION TYPE-C, 3 RT WING T/E, THE WING JACK POINT FITTING IS CRACKED AT THE UPPER END. REMOVED AND REPLACED THE WING JACK POINT FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTNG — CRACKED (BS 857)

INSPECTION TYPE-C, 3 LONG 8L END FITTING CRACKED AT FS 857. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D AND 51-3-0.

Part: FITTING — CRACKED (BS 859)

INSPECTION TYPE-D, LONGERON 10L END FITTING CRACKED FS 859. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: ANGLE — CRACKED (BS 1230)

INSPECTION TYPE-C, 3 FS 1230 LONG 36 TO L34L THE ATTACH ANGLE IS CRACKED AND GOUGED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9754920 AND SRM 51-1-21 AND 51-1-20D.

Part: FRAME — CORRODED (BS 1280)

INSPECTION TYPE-D, FRAME CORRODED OUT OF LIMITS FS 1280 AT LONGERON 35R-36. REPAIRED IAW SRM 53-2-0.

Part: FITTING — CORRODED (BS 1392)

INSPECTION TYPE-D, FS 1392 L-30R FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: CHORD — CORRODED (WS 10-26)

INSPECTION TYPE-D, RT WING I/B LEADING EDGE UPPER CHORD XFS 10.0 TO 26.25 HAS HEAVY EXFOLIATION CORROSION. REPAIRED IAW SRM 57-2-1.

Part: TRIPLER — CRACKED (RT WING)

INSPECTION TYPE-C, 3 RT WING L/E INTERNAL TRIPLER ABOVE THE NR 3 PYLON AT THE L/E OF THE PYLON CUT OUT IS CRACKED. REPAIRED L/E SKIN IAW EO DC8-5720-4087.

Part: SKIN — CRACKED (WS 622&628&635)

INSPECTION TYPE-D, LT WING L/E UPPER SKIN CRACKED 3 PLACES 2 FWD OF T/E XFS 628.75, 622.5 AND 635.0. REPAIRED IAW SRM 57-2-1.

Part: SKIN — CORRODED (WS 690)

INSPECTION TYPE-C3, LT WING LWR SKIN JUST O/B OF THE NR 1 PYLON AND FWD OF THE CENTER SPAR HAS HEAVY CORROSION. REMOVED CORROSION AND REPAIRED WING SKIN IAW DWG 5802630.

Part: LONGERON — CORRODED (BS 660)

INSPECTION TYPE-D, FWD END OF LONGERON 36 AT FS 660 HAS PITTING CORROSION. REPAIRED IAW DHC SK-779-169.

Part: SKIN — CRACKED (WS 6)

INSPECTION TYPE-C, 3 LT WING UPPER SKIN CRACKED AT FUEL PROBE AT XRS 6 AND STR 8. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM 57-2-1.

Part: AIR DISTRIBUTION — SMOKE (FLIGHT DECK)

INSPECTION TYPE-N/A, WHEN STARTING NR 3 ENGINE SMOKE OF UNKNOWN ORIGIN ENTERED THE FLIGHT DECK. SHUTDOWN ENGINE AND ALL ELECTRICAL AND EVACUATED AIRCRAFT. FIRE DEP WAS CALLED, OPENED MAIN ENTRANCE DOOR. SMOKE WAS DETECTED, CHECKED ALL AC PACKS RAN ENGS. OPERATED BOTH PACKS RECIR FAN, ALL SMOKE TAKEN OUT OF CABIN. FOUND SMOKE COMING FROM EXTERNAL AIR SOURCE, AIRCRAFT SECURE OK.

Part: PRECOOLER — DIRTY (NR 2 PYLON)

INSPECTION TYPE:C, AIR TURNBACK DUE TO FUMES IN THE COCKPIT. TROUBLESHOT SYSTEM FOUND DEBRIS IN THE NR 2 PRECOOLER. REMOVED AND REPLACED THE NR 2 ENG PRECOOLER AND THE LT WATER SEPARATOR COALESCER BAG IAW MM 36-13-05 AND 21-55-02.

Part: AIR DISTR — SMOKE (COCKPIT)

INSPECTION TYPE:C, AIR TURNBACK DUE TO SMOKE AND FUMES IN COCKPIT (FROM LOG PG 773468 ITEM 1). TROUBLESHOT PROBLEM, RAN PACKS WITH RECIRC FAN ON AND OFF WITH GROUND AIR AND ENGINES RUNNING. PRESSURIZED AIRCRAFT, ONLY DEFECT NOTED WAS CLOSE PROXIMITY OF INSULATION TO DUCTS IN A/C COMPT NEAR RECIRC FAN INLET SCREEN. REPOSITIONED INSULATION, OPS CK OK. CHECKED WTR SEPARATOR BAGS FOR CONTAMINATION, NONE NOTED.

Part: LONGERON — CRACKED (BS 1480)

INSPECTION TYPE:C, LONGERON 34R AT F/S 1480 HAS CRACK UNDER PRODUCTION SPLICE. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION OF LONGERON IAW SRM 53-2-0, 53-4-1, AND 53-2-2.

Part: FRAME — CRACKED (BS 620)

INSPECTION TYPE:C, FRAME LWR FLANGE CRACKED AT F/S 620 AT LONG 36. INSTALLED REPAIR IAW SRM 53-2-0 FIG 2 AND 51-1-20D.

Part: CLIP — CRACKED (MID TE FLAP)

INSPECTION TYPE:C, BOTTOM CLIP CRACK ON MIDDLE FLAP ATTACH AT NR 1 MAIN TANK. REMOVED, FABRICATED AND INSTALLED CLIP IAW DWG 3642189, SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1230)

INSPECTION TYPE:C, FITTING CRACKED AT LONG 33R F/S 1230. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, 53-1-0.

Part: DOUBLER — CORRODED (BS 1450-1510)

INSPECTION TYPE:C, REF NR 634974 FINGER DOUBLER CORRODED AND CRACKED BEYOND LIMITS AT F/S 1450 TO 1510 LONG 31L. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21, 51-1-20D AND 53-4-1.

Part: WEB — CRACKED (NR 1 PYLON)

INSPECTION TYPE:C, NR 1 PYLON O/B SIDE AT FWD ACCESS PANEL, PYLON WEB HAS A 3 INCH CRACK. AREA WAS MAPPED AND SUBMITTED TO ENRG ON N/R 634322. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DHC SK-779-322 (REF UPS ENRG FILE NR DC8-54-0038).

Part: LONGERON — CRACKED (BS 1400)

INSPECTION TYPE:C, LONGERON CRACKED 35L F/S 1400. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPLACEMENT SEC IAW SRM 51-1-21, 51-1-20D.

Part: LONGERON — CRACKED (BS 1420-1440)

INSPECTION TYPE:C, LONGERON 35 HAS 2, 4 INCH CRACKS ON I/B VERT WALL AT F/S 1420 TO 1440. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21, 51-1-20D, AND DWG 3646937.

Part: LONGERON — CORRODED (BS 1376)

INSPECTION TYPE:C LONGERON 36 AT STA 1376 BLOWN OUT AND CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21, 51-1-20D, AND DWG 3646937.

Part: DOUBLER — CORRODED (BS 1560-1620)

INSPECTION TYPE-C, FINGER DOUBLER BETWEEN FS 1560 AND 1620 ALONG LONG. 31L HAS EXFOLIATED CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW 51-1-21, 53-4-1 FIG 17.

Part: FITTING — CRACKED (BS 820)

INSPECTION TYPE:C, F/S 820 LBL 69 BELOW FLOOR ABOVE TANK INTERCOSTAL CLIP IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-01-20D AND 53-1-0.

Part: FITTING — CRACKED (BS 835)

INSPECTION TYPE:C, F/S 835 AT LBL 68 BELOW FLOOR, ABOVE TANK INTERCOSTAL CLIP IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-1-0.

Part: FITTING — CRACKED (BS 120)

INSPECTION TYPE:C, FRAME TIE FITTING AT F/S 120 BETWEEN STRINGERS 31 TO 32L WAS CRACKED. REMOVED, FABRICATED AND INSTALLED FITTING IAW SRM 51-1-21 AND DWG 3751096.

Part: CLIP — CRACKED (BS 832)

INSPECTION TYPE:C, F/S 832 RBL 69 BELOW FLOOR ABOVE TANK, INTERCOSTAL CLIP IS CRACKED. REMOVED AND REPLACED CLIP IAW SRM 51-1-29D AND FABRICATED DWG475336O.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE:C, F/S 8 TO 40 BETWEEN STR 28L TO 31L SKIN CORRODED HEAVY AFTER INTERNAL DOUBLER REMOVAL. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 53-2-0 FIG 1D.

Part: INTERCOSTAL — CRACKED (BS 250)

INSPECTION TYPE:C, INTERCOSTAL IS CRACKED AT F/S 250 BETWEEN STRINGERS 34 AND 35L. STIFFENER AT ANTENNA MOUNT. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-1-21 AND DWG 9750425.

Part: LONGERON — CORRODED (BS 480)

INSPECTION TYPE:C, LONG 36 LT AND RT FLANGES CORRODED AND BLOWN OUT AT BOLT HOLES F/S 480. REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPLACEMENT SECTION IAW SRM 53-2-2 FIG 10, 53-4-1.

Part: SPLICE — CRACKED (BS 600-620)

INSPECTION TYPE:C, LONGERON 31L SPLICE FITTING CRACKED BETWEEN F/S 600 TO 620. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: ANGLE — CORRODED (BS 904)

INSPECTION TYPE:C, F/S 904 LBL 50 TO 69 FLOOR ANGLE IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-20D AND 53-1-0.

Part: FITTING — CRACKED (BS 1139)

INSPECTION TYPE:C, F/S 1139 AT STR 33R TIE FITTING IS CRACKED AT BOTTOM. REMOVED AND REPLACED FITTING IAW SRM 53-1-0 AND 51-1-20D.

Part: FITTING — CRACKED (BS 1239)

INSPECTION TYPE:C, F/S 1239 AT STR 33R INTERCOSTAL TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING PER SRM 53-1-0.

Part: FITTING — CRACKED (BS 1241)

INSPECTION TYPE:C, F/S 1241 AT STR 35L INTERCOSTAL TIE FITTING IS CRACKED. REMOVED, FABRICATED AND INSTALLED FITTING IAW SRM 51-1-20D AND DWG 3758498.

Part: SPLICE — CORRODED (BS 1400)

INSPECTION TYPE:C FRAME SPLICE ON FWD SURFACE OF F/S 1400 AT LONGERON 36 HAS BLOWN OUT CORROSION REMOVED, FABRICATED AND INSTALLED REPLACEMENT SPLICE IAW SRM 51-1-21 , 51-1-20D, AND DWG 5640229-7

Part: SPLICE — CRACKED (BS 1260-1280)

INSPECTION TYPE:C, F/S 1260 TO 1280, STR 34R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: FITTING — CRACKED (BS 1260-1280)

INSPECTION TYPE:C, F/S 1260 TO 1280 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-1-0 AND 51-1-20D.

Part: ACTUATOR — CORRODED (RT MLG)

INSPECTION TYPE:C, RT MAIN LANDING GEAR ACTUATOR PIN BOSS INTERNAL BORE HAS CORROSION. REMOVED LIGHT CORROSION IAW SRM 51-1-8, REWORKED BOSS PER DHC SK 779-178 IR (REF UPS ENRG FILE NR DC8-32-0046).

Part: SPLICE — CRACKED (BS 1040-1060)

INSPECTION TYPE:C, F/S 1040 TO 1060 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 53-1-0 AND 51-1-20D.

Part: SKIN — CORRODED (BS 1360-1380)

INSPECTION TYPE:C, FINGER DOUBLER HAS BLOWN OUT CORROSION AT LONGERON 31L BETWEEN F/S 1360 AND 1380. REMOVED, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-21, AND 53-2-4.

Part: TIE CLIP — CRACKED (BS 1140)

INSPECTION TYPE:C, F/S 1140 AT STR 33R INTERCOSTAL/STR TIE CLIP IS CRACKED. REMOVED AND REPLACED FITTING IAW 53-1-0.

Part: DOUBLER — CORRODED (BS 1480-1500)

INSPECTION TYPE:C, FINGER DOUBLER BETWEEN F/S 1480 TO 1500 AND BETWEEN LONGERON 32L TO 32R HAS CORROSION. REMOVED, FABRICATED AND INSTALLED DOUBLER IAW SRM 51-1-21 AND DWG 5615372.

Part: RIB — CRACKED (RT WING LE)

INSPECTION TYPE:C, RT WING L/E SECTION BETWEEN PYLONS HAS 1 UPPER L/E RIB CRACKED AT AFT END. STOP DRILLED AND REPAIRED IAW SRM 53-2-0 AND 51-1-20D.

Part: SEAT TRACK — WORN (BS 322-327)

INSPECTION TYPE:C, F/S 322 TO 327 BL 0 SEAT TRACK IS WORN BEYOND LIMITS IN 2 PLACES. FABRICATED AND INSTALLED REPAIR IAW SRM 51-3-0 AND DC8-5320-5167.

Part: RIB — CRACKED (WS 6.225)

INSPECTION TYPE:C, RT WING L/E AT F/S XOLDI 6.225 THE UPPER L/E RIB IS CRACKED. INSTALLED REPAIR IAW SRM 57-2-0, 53-2-0, 51-1-21.

Part: FITTING — CRACKED (BS 1240)

INSPECTION TYPE:C, F/S 1240 AT STR 21R FRAME TO CUSP TIE FITTING IS CRACKED ON BOTTOM LEG. REMOVED AND REPLACED FITTING IAW SRM 53-1-0, 51-3-0, 51-1-20 AND DWG 4640162.

Part: JAMB — CRACKED (ENTRY DOOR)

INSPECTION TYPE:C, LT AFT ENTRY DOOR CUTOUT AFT JAMB WEB CRACKED AND HOLE BROKEN OUT APPROX LONGERON 20L. REPAIRED PER UPS EO DC8-5350-7876-A.

Part: TRIPLER — CRACKED (WS 6.225)

INSPECTION TYPE:, RT WING L/E AT STA XOLDI 6.225 TO THE INTERNAL TRIPLER IS CRACKED IN HALF. REMOVED, FABRICATED AND INSTALLED TRIPLER IAW SRM 57-3-1 AND DWG 5769891 AND SRM 51-1-20.

Part: DOUBLER — CRACKED (WS 6.225)

INSPECTION TYPE:C, RT WING L/E AT STA XOLDI 6.225 THE LWR SKIN DOUBLER INTERNAL HAS A 17 INCH CRACK. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 57-3-1, 51-1-20, AND DWG 5769891-41.

Part: DOOR FRAME — MISDRILLED (L1 DOOR)

INSPECTION TYPE:C, FWD ENTRY DOOR HAS 16 DOUBLE DRILLED HOLES, ENLONGATED HOLES AND HOLES TO CLOSE TO RIVET HOLES, ALL AROUND THE FRAME AREA. REMOVED ALL INNER WEBS, FABRICATED AND INSTALLED REPAIR ANGLES -1 THRU -13 IAW SRM 52-2-2, 51-1-21, AND 51-1-20A. FABRICATED AND INSTALLED INNER WEBS -14 THRU -20 IAW SRM 52-2-3 FIG 10, 51-1-21.

Part: FRAME — CRACKED (BS 55)

INSPECTION TYPE:C, F/S 55 AT STR 24L FRAME HAS LARGE CRACK IN RADIUS, LWR FLANGE. FABRICATED AND INSTALLED REPAIR IAW SRM 53-2-0 AND 51-1-20D.

Part: AIR DISTR — ODOR (COCKPIT)

INSPECTION TYPE N/A, AT TOP OF DECENT CREW SMELLED FUMES, SUSPECT RIGHT PACK. RAN RT PACK, OPS CHECKED NORMALLY. CHECKED LEFT PACK, OPS CHECK NORMAL. COULD NOT DUPLICATE. PACKS OPS CHECKED NORMAL IAW 21-55-00.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE: C. COCKPIT EMERGENCY EXIT LIGHTS FAIL TO ILLUMINATE WHEN TESTED. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT BATTERY PACK.

Part: BLKHD J-BEAM — CRACKED (BS 1766)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND 5TH J-BEAM ON AFT SIDE OF PRESSURE BULKHEAD FS 1766 CRACKED AT RADIUS RT CORNER. REPAIRED PER UPS EO DC8-5310-7630-A.

Part: FITTING — CRACKED (BS 1200)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK AT STOP FITTING FWD AND AFT SIDES, LONGERON 27L FS 1200. REPLACED FITTING PER SRM 51-1-20D.

Part: SKIN — CRACK (RT LE FLAP)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING INBD SLOT PANEL HAS 1 INCH LONG CRACK ON TOP SIDE. REPLACED SLOT PANEL PER MM 27-80-01.

Part: SKIN — DELAMINATION (NR 4 SPOILER)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT WING NR 4 SPOILER LOWER SURFACE DELAMINATED. REPLACED SPOILER ASSY PER MM 27-61-01.

Part: FITTING — CRACKED (BS 350)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING CRACKED AT FS 350, BETWEEN LONG 35L TO 36. REPLACED FITTING PER SRM 51-1-20D.

Part: VANE — DELAMINATION (RT WING)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING NR 2 VANE DELAMINATED. REPLACED VANE ASSY PER MM 27-51-14.

Part: ANGLE — CORROSION (BS 1610)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND MODERATE CORROSION DAMAGE BETWEEN FLOOR WEB AND STIFFENER IN AFT ACCY COMPT FS 1610, ABOVE LONG 23R. REPLACED STIFFENER PER SRM 51-1-20D.

Part: ANGLE — CRACKED (VERT STAB/FUS)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT VERTICAL STAB TO FUSELAGE ATTACH ANGLE CRACKED AT REAR SPAR, LOWER FWD SCREW HOLE. REPAIRED PER UPS EO DC8-5310-7584-A.

Part: LONGERON — CORROSION (BS 1220-1240)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON LONGERON 30L ANGLE FS 1200 TO 1240. REPAIRED PER UPS EO DC8-5310-7645-A.

Part: DOUBLER — CRACKED (BS 1583)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND FINGER DOUBLER CRACKED AT FS 1583 LONGERON 31R. REPLACED DOUBLER SECTION PER SRM 51-1-21.

Part: FITTING — CRACKED (BS 270)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING CRACKED AT FS 270 LONGERONS 35R TO 36. REPLACED FITTING PER SRM 51-1-20D.

Part: FRAME — CRACKED (BAGGAGE DOOR)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND D-BAG BIN DOOR HAS A 2 INCH LONG CRACK ON LOWER FRAME TOWARDS AFT CORNER. REPAIRED PER UPS EO AND DC8-5230-6643-A.

Part: FITTING — CRACKED (BS 2100)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING CRACKED AT FS 2100, ABOVE LONERON 28L. REPLACED FITTING PER SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (BS 1600)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BELT FRAME TO FLOORBEAM ATTACH FITTING BRACKET CRACKED AT FS 1600 LONGERON 21L. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1180)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING CRACKED AT FS 1180 LONGERON 35R. REPLACED FITTING PER SRM 53-2-0 FIG 2D.

Part: FITTING — CRACKED (BS 1250)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING CRACKED BETWEEN LONGERONS 33R TO 34 FS 1250. REPLACED FITTING PER SRM 53-2-0 FIG 2D.

Part: FITTING — CORROSION (FS 1200)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION ON B/T FITTING LONGERON 29L FS 1200. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CORROSION (FS 1160)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING CRACKED AT FS 1160, LONGERON 35R. REPLACED FITTING PER SRM 51-1-20D AND SRM 53-2-0.

Part: FITTING — CRACK (FS 1180)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING CRACKED AT FS 1180, LONG 33R. REPLACED FITTING PER SRM 51-1-20D.

Part: FITTING — CRACK (FS 340)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING CRACKED AT FS 340, BETWEEN LONGERONS 33L TO 34R. REPLACED FITTING PER SRM 53-2-0 FIG 20.

Part: FITTING — CORROSION (FS 879)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND BATH TUB FITTING ABOVE LONG 24R HEAVY CORROSION AT FS 879. REPLACED FITTING PER SRM 51-1-20D.

Part: CONTAINER — DAMAGED (ESCAPE SLIDE)

WHILE ON GROUND, MAINTENANCE FOUND ESCAPE SLIDE CONTAINER CLIP BROKEN. REMOVED AND REPLACED ESCAPE SLIDE CONTAINER.

Part: DOOR LIGHT — ILLUMINATED (LT MLG DOOR)

PILOT REPORTED DURING GO AROUND, GEAR DOOR NOT LATCHED INDICATION, CYCLED GEAR. ALSO, ALT LEFT GEAR DOOR LIGHT ILLUMINATED. CHECKED SYSTEM PER MM 32-31-04. COULD NOT DUPLICATE PROBLEM.