N715UP

Part: DOUBLER — MISREPAIRED (RUDDER) · airframe 80,117 hrs · 52,450 cycles

INSPECTION TYPE: SV RUDDER RT SIDE APPROX STA ZR 259.9 HAS A DOUBLER THAT IS 2.5 X 1.7 THA T DOES NOT CORRELATE TO THE SRM SURVEY SEQUENCE NR715-54-06. REPAIRED IAW UPS EO DC8-5570-31778-A.

Part: SKIN — MISREPAIRED (BS 1450 L34R) · airframe 80,117 hrs · 52,450 cycles

INSPECTION TYPE: SV REFERENCE UPS NRC 105041-EFN NR715RA1018 DOES NOT MATCH THE REPAIR CURRENTLY INSTALLED ON THE ACFT (715-F1-43). REPAIR LOCATED AT L34R STA 1458-1489). REPAIRED IAW UPS EO DC8-5330-31779A.

Part: DOUBLER — GOUGED (TE FLAP) · airframe 80,117 hrs · 52,450 cycles

INSPECTION TYPE: SV STA 340 LT WING OTBD FLAP STA 340 OTBD SIDE OF FLAP HINGE COVER EXISTING DOUBLER GOUGED. REPAIRED IAW UPS EO 5720 31755A.

Part: DOUBLER — GOUGED (TE FLAP) · airframe 80,117 hrs · 52,450 cycles

INSPECTION TYPE: SV RT WING OTBD FLAP INBD HINGE COVER DOUBLER GOUGES. REPAIRED IAW EO 5720 31754A.

Part: DOUBLER — GOUGED (TE FLAP) · airframe 80,117 hrs · 52,450 cycles

INSPECTION TYPE: SV RT WING OTBD FLAP INBD HINGE COVER OTBD SIDE DOUBLER GOUGED (ALSO INVESTIGAT E CAUSE). REPAIRED IAW UPS EO DC8-572031745A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,117 hrs · 52,450 cycles

INSPECTION TYPE: SV VALIDATE APPENDIX G FOR REPAIR SURVEY SEQUENCE NR 715-F1-41, STA 1438 T O 1454 AT L29R TO L31R. REPAIRED IAW UPS EO DC8-5330-31569A.

Part: CONNECTOR — BROKEN (FIRE BOTTLE) · airframe 80,074 hrs · 52,410 cycles

INSPECTION TYPE:SV LEFT WING LEADING EDGE INBOARD FIRE BOTTLE QTY CONNECTOR WIRE BROKEN. REPLACE CONNECTOR 20-31-09.

Part: SKIN — MISREPAIRED (RT WING) · airframe 80,076 hrs · 52,410 cycles

INSPECTION TYPE:SV SURVEY SEQUENCE 715-W4-28 STA XFS 310.750 RT WING LEADING EDGE DOUBLER IS STAINLESS STEEL AND IS NOT IN COMPLIANCE WITH SRM APP G. REPAIRED PER EO DC8 5720-31062A.

Part: SKIN — MISREPAIRED (AILERON) · airframe 80,118 hrs · 52,450 cycles

INSPECTION TYPE:SV APPENDIX G SURVEY SEQ 715-W4-01 EXTERNAL DOUBLER DOES NOT MATCH SRM 57-02-01-0 FIG 002Y UPPER SURFACE RW OUTBOARD AILERON. REPLACED DOUBLER IAW SRM 57-02-01 FIG 002Y REV 78.

Part: SKIN — DAMAGED (TE FLAP) · airframe 80,076 hrs · 52,410 cycles

INSPECTION TYPE:SV REF UPS EO APPENDIX H STEP A (7) REPAIR FAILS. SURVEY SEQUENCE 715-W3-27. INSTALLED DOUBLER IAW DC8 SRM 57-02-01-0.

Part: FASTENER — IMPROPER PART (RT WING) · airframe 80,076 hrs · 52,410 cycles

INSPECTION TYPE:SVN/ SEQ 715-W4-100 RIGHT WING STA XRS 366.300 UPPER LEADING EDGE DOUBLER HAS BLIND FASTENERS NOT CALLED OUT IN SRM. REPLACED FASTENERS AS IAW 57-02-01 FIG 38.

Part: DOUBLER — GOUGED (TE FLAP) · airframe 800,765 hrs · 2,410 cycles

INSPECTION TYPE:SV APPENDIX D SURVEY SEQUENCE 715-W4-02 EXTERNAL DOUBLER ON RT WING FLAP UPPER SURFACE AT STA XF 255 IS GOUGED. INSTALLED DOUBLER IAW DC8 SRM 51-1-21.

Part: SKIN — GOUGED (TE FLAP) · airframe 800,765 hrs · 2,410 cycles

INSPECTION TYPE:SV APPENDIX D SURVEY SEQ 715-W4-03 EXTERNAL DOUBLER AT STA XF 240 RT WING FLAP UPPER SURFACE IS GOUGED. INSTALLED DOUBLER IAW DC8 SRM 51-1-21.

Part: HOOK — CRACKED (CARGO DOOR) · airframe 80,074 hrs · 52,410 cycles

INSPECTION TYPE:SV FWD PIT DOOR LATCH HOOK CRACKED. INSTALLED NEW LATCH 52-31-01-5 AND 51-01-21.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 80,076 hrs · 52,410 cycles

INSPECTION TYPE:SV FLUSH DOUBLER C3 DOOR SKIN BS 1228 L23R NEEDS VALIDATION FOR REPAIR SEQ 715-F1-55. REPAIRED 52-02-00 FIG 4 SHEET 3 AND 52-04-01.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,076 hrs · 52,410 cycles

INSPECTION TYPE:SV EXT DOUBLER NOSE GEAR DOOR CUTOUT BS 6.5 TO BS 11 NEEDS VALIDATION. REPAIRED TO SRM 53-02-01 FIG 7.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 80,076 hrs · 52,410 cycles

INSPECTION TYPE:SV EXT DOUBLER BS 8 TO BS 3 L33R CORNER OF NOISE LANDING GEAR DOOR. REPAIRED AS PER 53-03-01.

Part: SKIN — DAMAGED (LT WING) · airframe 800,765 hrs · 2,410 cycles

INSPECTION TYPE:SV LT WING CENTER L/E UPPER AFT EDGE HAS A STEEL REPAIR DOUBLER INSTALLED AT STA XFS 396-404. INSTALLED CONICAL WASHER REPAIR DOUBLER AND FILLER 4 EA IAW DC8 SRM 57-2-1 REV 78.

Part: DOUBLER — GOUGED (TE FLAP) · airframe 80,076 hrs · 52,410 cycles

INSPECTION TYPE:SV LT WING OUTBOARD FLAP TOP SKIN HAS A REPAIR DOUBLER THAT IS GOUGED. REMOVED, FABRICATED AND INSTALLED NEW DOUBLER IAW DC8 SRM 57-2-0 TR57- 84.

Part: SKIN — DAMAGED (LT WING) · airframe 800,765 hrs · 2,410 cycles

INSPECTION TYPE:SV LT WING CENTER L/E UPPER AFT EDGE HAS A STEEL REPAIR DOUBLER INSTALLED AT STA XFS 297-299. INSTALL CONICAL WASHERS, REPAIR DOUBLER FILLER 4EA IAW DC8 SRM 57-2-1 REV 78.

Part: DOUBLER — GOUGED (TE FLAP) · airframe 80,076 hrs · 52,410 cycles

INSPECTION TYPE:SV REPAIR DOUBLER GOUGED. REF SURVEY SEQUENCE 715-W3-28. INSTALLED DOUBLER IAW DC8 SRM 57-02-01-0.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,076 hrs · 52,410 cycles

INSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN 71520041070 ORIG NR 735729 FRAME STA 7 81 AND X20 (CRACK). REPAIR WAS ACCOMPLISHED WITH DC8 SRM 53-02-00 FIG 001B REV 78.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 80,076 hrs · 52,410 cycles

INSPECTION TYPE:SV EVAL AND DISPOSITION REPAIR EFN 71520081041 ORIG NR 198845 MAIN CABIN STA 240 LBL 45 SEAT TRACK PLUG. NO SEAT TRACK PLUG AT STA 240 LBL 45. SEAT TRACK SPLICE IAW DCI SRM 53-02-03-0 FIG 006A REV 78.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 800,765 hrs · 2,410 cycles

INSPECTION TYPE:SV EVALUATE AND DISPOSITION REPAIR EFN 71520081063 ORIGINAL NON-ROUTINE 1 99042, FORWARD CARGO COMPARTMENT RT SUPPORT ANGLE ATTACHED TO FLOOR SUPPORT BEAM FOUND CRACKED. INSTALLED SUPPORT ANGLE IAW DC8 SRM 51-1-21 REV 78.

Part: BATTERY PACK — DISCHARGED (COCKPIT) · airframe 80,076 hrs · 52,410 cycles

INSPECTION TYPE:SV EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK PER DC8 MM 33-50-01-2. OPS CHECKS GOOD.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 2 EA GOUGES IN UPPER SKIN OF RT WING O/B FLAP, ON I/B & O/B SIDE OF FLAP STA 219. FABRICATED AND INSTALLED 2 EA REPAIR DOUBLERS IAW SRM 57-07-01 FIG 004, 57-02-00, AND 51-1-21A.

Part: FLOOR PANEL — GOUGED (FS 660 RBL 24) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 FLOOR PANEL FROM STA 660 TO STA 760 RBL 24 TO 44 HAS 14 INCH GOUGE PENETRATING OUTER SKIN. FABRICATED AND REPLACED FLOOR PANEL IAW EO DC8-5320-9691C.

Part: FITTING — CRACKED · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 NR 4 ALT Z-FITTING CRACKED. REMOVED CRACKED FITTING IAW SRM 51-01-20D. FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 3644046, SRM 51-01-24, AND 51-01-20D.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 FOUND CRACK ON STRINGER 53 AT O/B DRAG ANGLE NR 4 ALT. REMOVED AND REPLACED STRINGER IAW SRM 51-1-8, 57-2-2 FIG 3D, 57-4-0 FIG 11.

Part: FITTING — CRACKED (WING) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 NR 1 ALT Z-FITTING IS CRACKED. REMOVED Z-FITTING IAW SRM 51-01-20D. FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 364046, SRM 51-01-20D.

Part: DOUBLER — CORRODED (SERVICE DOOR) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE-C1, CORROSION ON A DOUBLER INSIDE RT FWD SERVICE DOOR FWD TORQUE BOX JUST BELOW LOWER HINGE. REMOVED AND REPLACED FITTING (DOUBLER) SRM 51-01-20D,51-03-00.

Part: INTERCOSTAL — CRACKED (FWD SERVICE DOOR) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 CRACKED CHANNEL AND GOUGED INTERCOSTAL AT THE SAME LOCATION ON RT FWD SERVICE DOOR LOWER AFT CORNER. REMOVED EDGE CRACK ON CHANNEL BY BLENDING IAW SRM 53-02-00. FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5615762 SRM 51-01-21, AND 51-01-20D.

Part: ATTACH FITTING — CORRODED (FS 520 L21R) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 B-PIT STA 520 LONGERON 21R FLOORBEAM ATTACH FITTING HAS CORROSION. REMOVED FITTING IAW SRM 51-01-20D. INSTALLED REPLACEMENT FITTING IAW SRM 51-01-20D, AND 51-03-00.

Part: INTERCOSTAL — CRACKED (BS 80 L36) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE-C1, FWD LOWER CARGO COMP FLOOR SUPPORT BRACKET CRACKED AT FUS STA 80 LONGERON 36 AS MARKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL (BRACKET) IAW SRM 51-01-20D,DWG 4619078, AND SRM 51-03-01.

Part: FLOORBOARD — CRACKED (MAIN CABIN) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 COURIER AREA FLOORBOARDS 2EA ARE DELAMINATED AND CRACKING. SANDED, CLEANED AND REPAIRED 2EA COURIER AREA FLOORBOARDS AT DELAMINATED AND CRACKED AREAS IAW SRM 51-01-19.

Part: DOUBLER — GOUGED (RT WING TE FLAP) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 RT WING O/B FLAP STA XF 228 HAS A ROUND DOUBLER GOUGED AT UPPER SKIN, NEXT TO L/E AREA. REMOVED EXISTING DOUBLER IAW SRM 51-1-21A. FABRICATED AND INSTALLED REPLACEMENT REPAIR DOUBLER IAW SRM 57-07-01 FIG 004, 57-02-0 FIG 002A, AND SRM 51-1-21A.

Part: FLOOR PANEL — DAMAGED (FS 880-1000) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 MAIN CABIN FLOORBOARD AT STA 880-1000 LBL 44.60 HAS 3EA MISSING & 1 EA DAMAGED INSERT. REPLACED 4EA INSERTS IAW DPS 1.9023 REPAIR 4.3-1 PAGE 4.

Part: FLOORBOARD — DAMAGED (FS 800-1000) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 MAIN CABIN FLOORBOARD AT STA 800-1000 RBL 25.44 HAS 1 EA MISSING & 3EA DAMAGED INSERTS. REMOVED AND REPLACED 4EA INSERTS PER B DPS 1902-3 REPAIR 4.3.1 PG 4.

Part: SKIN — GOUGED (RT WING TE FLAP) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1, RT WING OB FLAP STA XF 228 HAS EXISTING REPAIR DOUBLER GOUGED AT UPPER FLAP SKIN, NEXT TO AFT FIXED PANEL OF FLAP HINGE COVER REMOVED EXISTING DOUBLER FABRICATED AND REPLACED REPAIR DOUBLER IAW SR M 51-1-21A, 57-2-8 FIG 2A,57-7-01 FIG 4, AND 51-3-0.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1, NR 4 ALT THRU 505B, STRINGER 54 CRACKED AT APPROX XRS 490. FABRICATED AND INSTALLED 2 REPAIR SPLICES IAW SAA EA 088-5710-01-1474.

Part: FLOOR PANEL — CRUSHED (FS 680-780 RBL44) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 MAIN CABIN FLOORBOARD AT STA 680-780 RBL 44.60 HAS 2 EA CRUSHED AREAS. FABRICATED REPLACEMENT FLOOR PANEL IAW EO DC8-5320-9691.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 CRACKED FWD JAMB JUST ABOVE UPPER HINGE ON RT FWD SERVICE DOOR. BLENDED EDGE REMOVING CRACK IAW SRM 53-02-00, AND 51-01-08.

Part: FLOOR PANEL — CRUSHED (FS 680-780) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 MAIN CABIN FLOORBOARD AT STA 680-780 LBL 25.44 IS CRUSHED AT FWD & AFT ENDS. FABRICATED REPLACEMENT FLOOR PANEL IAW EO DC8-5320-9691.

Part: SKIN — GOUGED (NR 3 SPOILER) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 RT WING NR 3 SPOILER HAS TWO DEEP GOUGES AT LOWER SKIN AREA. REMOVED DAMAGE IAW SRM 51-01-09A. FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-07-01 AND 51-01-09A.

Part: STRUCTURE — DAMAGED (LT WING TE FLAP) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1, TWO HOLES IN LT FLAP EITHER SIDE OF FLAP STATION 219 BACKSIDE OF FLAP. CUT OUT DAMAGE, FABRICATED AND INSTALLED 2EA REPAIR DOUBLERS IAW SRM 5 7-02-01 FIG 2Q,51-01-09, AND 51-01-21A

Part: SEAT TRACK — DAMAGED (BS 240 LBL 45) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE-C1 MAIN CABIN, SEAT TRACK PLUG DAMAGED AND ATTACH SCREWS (2EA) TOO HIGH-S TA. 240 LBL 45. REMOVED AND REPLACED PLUG AT MAIN CABIN SEAT TRACK STA 240 LBL 45 IAW SRM 51-3-00 PG1.

Part: FITTING — GOUGED (BS 1345 L28L) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE-C1, D PIT STA 1345 LONGERON 28L, LONGERON FITTING GOUGED AT RADIUS. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D,51-3-2.

Part: FLOORBEAM — CRACKED (BS 1360 L31R) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 D PIT STA 1360 LONGERON 31R FLOORBOARD SUPPORT CRACKED. REPAIRED FLOORBOARD SUPPORT AT STA 1360 L31R IAW EO DC8-5320-6176.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE-C1, TWO MOUNT TABS SHEARED THRU ATTACH RIVETS FOR INTERCOSTAL IN COCKPIT SUBFLOOR STA 8 TO -12 BL 0. FABRICATED AND INSTALLED 2EA REPAIR DOUBLER IAW SRM 53-02-00 FIG 1B 51-1-21.

Part: FITTING — CORRODED (FS 1275 L36) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 C PIT STA 1275, LONGERON 36, FITTING HAS CORROSION. CORROSION ON FITTING OUT OF LIMITS IAW SRM 53-2-0 FIG 1F. REMOVED FITTING IAW SRM 51-1020D, REPLACED FITTING IAW 51-01-24, 51-01-20D, AND 51-03-01.

Part: INTERCOSTAL — DAMAGED (SERVICE DOOR) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 A HOLE DRILLED THROUGH INTERCOSTAL ON RT CTR SERVICE DOOR STRUCTURE 10, 10 INCHES BELOW UPPER HINGE. REMOVED DAMAGED INTERCOSTAL, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-01-21, DWG 5615762, AND SRM 51-03-00, 51-1-20.

Part: SKIN — GOUGED (SERVICE DOOR) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE-C1 GOUGE ON INNER SKIN OF RT CTR SERVICE DOOR JUST ABOVE BAYONET. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 52-03-00 AND 51-01-21- 0 FIG 033.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 2 WORN AREAS EITHER SIDE OF O/B FLAP STA 340 LT FLAP. FABRICATED AND INSTALLED REPAIR DOUBLER ON O/B SIDE OF STA 340 IAW SRM 57-07-01 AND 51,1-21A.

Part: DOOR FRAME — DAMAGED (SERVICE DOOR) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 A HOLE DRILLED THROUGH AFT DOOR JAMB ON LT CTR SERVICE DOOR. STOP DRILLED DAMAGE AREA, FABRICATED AND INSTALLED REPAIR ANGLE DOUBLER IAW DC-8 SRM 52-03-01-0 FIG 3.

Part: ANGLE — DAMAGED (FS 857 RBL 23) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 MAIN CABIN SUBFLOOR "L" ANGLE CUTOFF THROUGH BOLT HOLE RADIUS BOLT INSTALLED (HALF ON AND HALF OFF CUT) STA 857 RBL 23, AT BOTTOM OF PRESSURE PNL. REMOVED AND REPLACED "L" ANGLE IAW SRM 51-1-24, 51-3-0, 51-1-20D, 51-1-21.

Part: FRAME — DAMAGED (BS 781 L15R) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 MAIN CABIN DOUBLE DRILLED HOLE IN BELTFRAME STA 781L-15R. FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-8, 53-2-0.

Part: FRAME — DAMAGED (BS 781 L15R) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 MAIN CABIN, DOUBLE DRILLED HOLE IN BELTFRAME STA 781 L15R. FABBED AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-8, 53-2-0 FIG 1B.

Part: FITTING — CRACKED (BS 680 L6R) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE-C1, MAIN CABIN, FUSELAGE SPLICE FITTING CRACKED STA 680 L-6R. REMOVED AND REPLACED FITTING IAW SRM 51-03-01.

Part: DOOR FRAME — DAMAGED (BS 220) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE-C1, MAIN CARGO DOOR UPPER FRAME CENTER DOOR JAM HAS A DOUBLE DRILLED HOLE AT STA 220 & 6L. CUTOUT DAMAGE IAW SRM 53-02-00, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-02-00,51-1-20D, AND 51-1-21.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 PRESSURE WEB CRACKED AROUND RIVET HEAD, RT NOSE A/C TUNNEL CEILING STA -54, RBL 35. REPAIRED CRACK PER SAA EA 008-5330-01-A1489.

Part: FLOOR PANEL — CRUSHED (FS 1120 RBL 14) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 MAIN CABIN, FLOOR PNL HAS CRUSHED HONEYCOMB STA 1120 RBL 14. FABRICATED AND REPLACED FLOOR PNL IAW EO DC8-5320-9691C.

Part: LONGERON — CRACKED (BS 1746 L16L) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE-C1, MAIN CABIN, L16L CRACKED AT BS 1746 CANT FRAME, FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION IAW SRM 53-02-02 FIG 10,51-01-20D,51-03-01.

Part: FLOOR PANEL — DAMAGED (FS 1500 LBL 29) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 MAIN CABIN, FLOOR PNL HAS CRUSHED HONEYCOMB STA 1500 LBL 29. REMOVED PNL, FABRICATED AND INSTALLED REPLACEMENT FLOOR PNL IAW MM 53-21-02, EO DC8-5320-9691C.

Part: FLOOR PANEL — PUNCTURED (FS 1220 RBL 58) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 MAIN CABIN, FLOOR PANEL PUNCTURED STA 1220 RBL 58. REMOVED FLOOR PANEL IAW MM 53-21-02, REPAIRED PER SRM 51-01-19, REINSTALLED PANEL IAW 53-21-02.

Part: FLOOR PANEL — CRUSHED (FS 1180 RBL14) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 MAIN CABIN, FLOOR PANEL HAS CRUSHED HONEYCOMB STA 1180 RBL 14. REMOVED FLOOR PANEL IAW MM 53-21-02, FABRICATED AND INSTALLED REPLACEMENT PANEL IAW EO DC8-5320-9691C, AND MM 53-21-02.

Part: FLOOR PANEL — CRUSHED (FS 1490 RBL 36) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 MAIN CABIN, FLOOR PANEL HAS CRUSHED HONEYCOMB STA 1490 RBL 36. REMOVED PANEL, FABRICATED AND INSTALLED REPLACEMENT FLOOR PANEL IAW MM 53-21-02, AND EO DC8-5320-9691C.

Part: FLOOR PANEL — CRUSHED (FS 1490 RBL 57) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 MAIN CABIN FLOOR PANEL HAS CRUSHED HONEYCOMB STA 1490 RBL 57. REMOVED FLOOR PANEL, FABRICATED AND INSTALLED REPLACEMENT PANEL IAW MM 53-21-02, EO DC8-5320-9691.

Part: LONGERON — CRACKED (BS 1754 L14L) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE-C1, L14R CRACKED IN LOWER RADIUS AT BS 1754 APPROX (SEEN IN BACKSIDE OF LONGERON) AT LONGERON SPLICE IN MAIN CABIN. FABRICATED AND INSTALLED REPLACEMENT LONGERON SECTION IAW SRM 53-02-02 FIG10, 53-05-03, 51-01-20D, AND 51-03-01.

Part: TORQUE BOX — CRACKED (EMERGENCY EXIT) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 A FITTING CRACKED IN LEFT FWD EMERGENCY EXIT DOOR FWD JAMB TORQUE BOX STA 380 L19L. FABRICATED AND INSTALLED REPAIR FITTING IAW SAA EA 008-5310-01-A1486-1.

Part: SKIN — PUNCTURED (FS 136 RBL 8) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 NOSE FUSELAGE AT STA 136.0 HAS PUNCTURED SKIN ON TOP OF AFT SIDE RADOME COMP'T BULKHEAD RBL 8. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 51-02-00, AND 51-01-21.

Part: FRAME — CRACKED (FUSELAGE) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1 CRACKED FRAME AT FLIGHT COMP STA -67.000 BETWEEN LONGERON 10 AND 11 AT LT SIDE NEXT TO LT EYEBROW WINDOW. REMOVED CRACKED FRAME IAW SRM 51-1-21, FABRICATED AND INSTALLED REPLACEMENT FRAME IAW DWG 5642814, SRM 51-1-20D, AND 51-03-01.

Part: STIFFENER — CRACKED (NR 4 PYLON) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE:C1, NR 4 PYLON RT INTERIOR STRUCTURE AREA HAS A CRACKED STIFFENER AT STA. YN 326. FABRICATED AND REPLACED STIFFENER IAW DWG 5756791, AND 51-01-24,51-01- 21D.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE-C1, COCKPIT FLOOR PNL 680 HAS 1 FASTENER HOLE WITH IMPROPER E.D. AND 1 FASTENER HOLE CRACKED TO EDGE. CUTOUT CRACKED AREA IAW SRM 53-02-00 FIG 23, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-02-00,51-01-21.

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 80,018 hrs · 52,368 cycles

INSPECTION TYPE-C1, FLOOR PANEL 626D HAS DAMAGE AT 2 CORNERS AS MARKED EDGE DAMAGE OUT OF LIMITS IAW, SRM 53-2-0 FIG 1F, FABRICATED AND REPLACED FLOOR PANEL SKIN IAW DWG 3619130 AND SRM 51-1-21.

Part: STEERING SYS — MALFUNCTIONED (NLG)

INSPECTION TYPE:N/A ON T/O THE A/C BEGAN TO VEER TO THE RIGHT. THE CREW WAS UNABLE TO CONTROL THE A/C AND ABORTED TAKEOFF. A/C IS OOS. *SDR FILED OPEN*.

Part: HYDRAULIC LINE — CRACKED (RT MLG WW)

INSPECTION TYPE:N/A ATB - ON CLIMBOUT STARTED TO LOSE HYD PRESS/QTY. REMOVED AND REPLACED HYD LINE ON RT MLG BUNGEE CYLINDER.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01-2. OPS CHECK GOOD.

Part: WINDOW — STUCK (COCKPIT)

F/O WINDOW WILL NOT OPEN. ADJUSTED F/O SLIDING CLEARVIEW WINDOW IAW AMM 56-10-03-5. OPS CK GOOD.

Part: BULB — INTERMITTENT (EMERGENCY LIGHT)

EMERGENCY LIGHT DISARMED LIGHT IS ON AND OFF INTERMITTENTLY. BULB HAS DOOR CONTACT IN SOCKET. RELAMPED. OPS CK OK.

Part: BATTERY PACK — MALFUNCTIONED (EMERGENCY LIGHT)

EMERGENCY LIGHTING WILL NOT STAY ON WHEN TESTED. EMERGENCY BATT PACK REPLACED IAW AMM 33-50-01-2 AND EMERGENCY LIGHTING SYSTEM CK SERVICEABLE.

Part: WINDOW — STUCK (COCKPIT)

F/O SLIDING WINDOW WILL NOT OPEN. PERFORMED ADJ/TEST OF F/O SLIDING WINDOW IAW MM 56-10-03-5. NO DEFECTS NOTED. OPS CHECK GOOD.

Part: COALESCER BAG — ODOR

STRANGE ODOR IN C/P. REMOVED AND REPLACED WATER SEPARATOR BAG ON LT & RT WATER SEPARATOR IAW DC8 MM 21-55-03-2. LEAK & OPS CHECK LT & RT WATER SEPARATORS IAW 21-00-00. LT CHECKS GOOD. RT WATER SEPARATOR LEAKS. REMOVED AND REPLACED O-RING IAW 21-55-03-2. LEAK CHECKS GOOD. RAN PACKS IAW DC8 MM 21-00-00. NO ODOR NOTED.

Part: SPLICE — CRACKED (FS 1562 L34R) · airframe 78,939 hrs · 51,612 cycles

INSPECTION TYPE: C3, SPLICE FITTING CRACKED, STA 1562 L34R. REMOVED LONGERON 34R AT STA 1562 IAW SRM 51-1-21, FABRICATED AND INSTALLED 2EA SPLICE ANGLES, ATTACH CLIP AND SPLICE FITTING AT STA 1562 L34R IAW SRM 53-02-00-0 FIG 002, 53-04-01 FIG 051, DWG 5758577, AND SRM 51-1-21D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 78,939 hrs · 51,612 cycles

FOUND C3 LONGERON 15L STA 1734 END FITTING IS CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 1734 L15L IAW SRM 51-3-2 AND SRM 51-1-20D.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 78,939 hrs · 51,612 cycles

INSPECTION TYPE:C3 INTERCOSTAL CRACKED AT STA 620-640 L33L, FOUND DURING FLOOR SUPPORT REPAIR. REPAIRED INTERCOSTAL TRACK SUPPORT FITTING IAW SAA EA NR 008-5340-01- A0234, UPS RAA NR DC8-53-20557, BAC MSG NR 1-198392632-1 DATED 6/6/06 BAC MSG NR 1-198392632-2 DATED 6/8/06, BAC MSG NR 1-198392632-5, AND FAA FORM 8100-9 DATED 6/12/26.

Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 78,939 hrs · 51,612 cycles

HFEC INSP DETECTED A .250" CRACK ON THE LWR AFT CORNER OF THE FWD LT TYPE 1 EMERGENCY EXIT DOOR (FWD OF STA 680.500) SEE ATTACHED DRAWING FOR LOC. REPAIRED LT TYPE 1 EMERGENCY EXIT LWR AFT CORNER IAW SAA EA 008- 5320-01-A0237 AND UPS EO DC8-5320-24507-A.

Part: DOUBLER — CRACKED (LT WING) · airframe 78,939 hrs · 51,612 cycles

INSPECTION TYPE:C3 AFTER REMOVAL OF INTERNAL TRIPLER IN LT CTR L/E FOUND LONG INTERNAL SPLICE DOUBLER CRACKED BETWEEN PNL 522A & XFS 409 AFT END. REMOVED INTERNAL SPLICE DOUBLER AT STA XFS 409 IAW SRM 51-01-20D. FABRICATED AND INSTALLED INTERNAL DOUBLER AT STA XFS 409 IAW SRM 51-01-20D AND DWG 5169891.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 78,939 hrs · 51,612 cycles

INSPECTION TYPE:C3 ATTACH FITTING CRACKED AT STA 822.500 L22R AFT SIDE. REMOVED AND REPLACED FITTING AT STA 822.500 L22R IAW SRM 51-1-20D AND SRM 51-03-02.

Part: ATTACH FITTING — CRACKED (BS 834 L22L) · airframe 78,939 hrs · 51,612 cycles

C3 ATTACH FITTING CRACKED AT STA 834.500 L22L . REMOVED CRACKED FITTING AT STA 834.500 IAW SRM 51-1-20D. FABRICATED AND INSTALLED ATTACH FITTING AT STA 834.500 IAW DWG 4753360, AND SRM 51-1-20D.

Part: TRIPLER — CRACKED (LT WING) · airframe 78,939 hrs · 51,612 cycles

INSPECTION TYPE:C3 INTERNAL TRIPLER BROKEN INSIDE LT CTR L/E LWR SURFACE, BETWEEN PANELS 522A & 520B AT XFS 409. REMOVED, FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW SRM 51-1-20D, 51-03-00, 57-03-00-0 FIG 13 AND DWG 5769589.

Part: FITTING — CRACKED (FUSELAGE) · airframe 78,939 hrs · 51,612 cycles

FOUND CRACKED FITTING L21L LWR CUSP FS 1320 D-PIT. REMOVED CRACKED FITTING AT STA 1320 L21L IAW SRM 51-1-20D. FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 9755584, AND SRM 51-3-0, AND SRM 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 78,939 hrs · 51,612 cycles

INSPECTION TYPE:C3 LONGERON 15R CRACKED AT STA 1734. REMOVED CRACKED LONGERON SPLICE AND END FITTING AT STA 1734 L15R IAW SRM 51-1-21. FABRICATED AND INSTALLED LONGERON SPLICE AND END FITTING AT STA 1734-1770 L15R IAW SRM 53-02-02 FIG 10.

Part: SKIN — CORRODED (FUSELAGE) · airframe 78,939 hrs · 51,612 cycles

AFTER REMOVAL OF D-PIT SCUFF PLATE TO FOM NDT INSPECTION, FOUND CORROSION ON FUSELAGE SKIN. CUT OUT DAMAGED SKIN AT STA 1400-1410 L33R IAW SRM 53-2-0 FIG 21. FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER, AND TRIPLER AT STA 1400-1410 L33R IAW SRM 53-02-00 FIG 21.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 78,939 hrs · 51,612 cycles

INSPECTION TYPE:C3 AFT PRESSURE BULKHEAD ATTACH ANGLE CRACKED AT STA 1766 L6R. REMOVED CRACKED ANGLE AT STA 1766 L6R IAW SRM 51-1-21, FABRICATED AND INSTALLED ATTACH CLIP AT STA 1766 L6R IAW SRM 51-01-20D, AND DWG 5773844.

Part: STIFFENER — CRACKED (LT WING) · airframe 78,939 hrs · 51,612 cycles

INSPECTION TYPE:C3 BROKEN STIFFENING ANGLE INSIDE LEFT CTR L/E, AT INBOARD END OF SLOT DOOR COVE, STA XW 408. REMOVED BROKEN STIFFENER AT STA XW 408 IAW SRM 51-3-0, FABRICATED AND INSTALLED STIFFENER AT STA XW 408 LEFT CTR L/E IAW DWG 3770673 AND SRM 51-01-20D.

Part: SMOKE GOGGLES — DAMAGED (COCKPIT)

CAPT AND FE'S SMOKE GOGGLES ARE SCRATCHED AND HAZING. REMOVED AND REPLACED CAPT AND FE'S SMOKE GOGGLES IAW DC8 MM 25-00-00.

Part: REGULATOR — INOPERATIVE (OXYGEN)

CREW OXYGEN REGULATOR INOP. REPLACED CAPTAIN'S 02 REGULATOR PER 35-10-07. OPS CHECK NORMAL.

Part: BATTERY — MALFUNCTIONED (EMERGENCY LIGHT)

EMERG EXIT LIGHTS ARE SLOW TO DISARM WHEN ACTIVATED. REMOVED AND REPLACED EMERG BATTERY AND RELAY UNIT SYS OPS CHECK NORMAL PER MM 33-50-01-2 PARA 2,4 & 5.

Part: BATTERY — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS INOP. R&R BATTERY AND RELAY UNIT W/REF TO MM 33-50-01-2. OPS CHECK GOOD.

Part: REGULATOR — INOPERATIVE (COCKPIT O2)

CREW O2 LOW, POSSIBLE LEAK. ROBBED KNOWN GOOD O2 REGULATOR FROM FWD COURIER POSITION AND INSTALLED AT F/E'S POSITION, OPS AND LEAK CHECK GOOD.

Part: WEB — CRACKED (SUBFLOOR) · airframe 78,278 hrs · 51,082 cycles

INSPECTION TYPE:C2 AC BAY SUBFLOOR WEB CRACKED BETWEEN STA 8 & STA 16 AT L21L. REPAIRED IAW DC-8 SRM 51-1-21A & UPS EO DC8 5350-7876-A.

Part: ATTACH ANGLE — CRACKED (HORIZONTAL STAB) · airframe 78,278 hrs · 51,082 cycles

INSPECTION TYPE: C2, LEFT HORIZONTAL STAB L/E ATTACH ANGLE CRACKED AT LOWER I/B CORNER. REMOVED HORIZONTAL STAB SIDE ROLLER BEARING, TRACK, AND ANGLE FITTING PER SRM 51-3-0, 51-1-20D, 51-1-21 AND MM 55-10-00-2. INSTALLED NEW ANGLE FITTING PER SRM 51-3-0, 51-1-20D, 51-1-21. REINSTALLED SIDE LOAD ROLLER AND TRACK PER SRM 51-3-0, AND MM 55-10-00-2.

Part: FITTING — CRACKED (CARGO BAY) · airframe 78,278 hrs · 51,082 cycles

INSPECTION TYPE: C2, LONGERON 32R SPLICE FITTING CRACKED FROM STA 620 TO STA 640. REMOVED AND REPLACED SPLICE FITTING PER SRM 51-1-20D.

Part: FITTING — CRACKED (LOWER CARGO) · airframe 78,278 hrs · 51,082 cycles

INSPECTION TYPE:C2 LONGERON 36 END FITTING CRACKED AT STA 203. REMOVED AND REPLACED END FITTING REF DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (LOWER CARGO) · airframe 78,278 hrs · 51,082 cycles

INSPECTION TYPE: C2, BATHTUB FITTING CRACKED AT STA 280 L27L. REMOVED CRACKED FITTING. FABBED REPAIR PARTS FROM BAC1503-100163 PER SRM 53-2-0 FIG 2D. INSTALLED NEW FITTING AND REPAIR PARTS PER SRM 53-2-0 FIG 2D, 51-1-8, 51-1-20D, 51-3-0, 51-1-15.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 78,278 hrs · 51,082 cycles

INSPECTION TYPE:C2 LIGHTNING STRIKES ON FUSE EXTERIOR STA 415 BETWEEN L5R & L6R. BURNISHED DAMAGE AREA PER SRM 53-2-0 FIG 1F. NDT VERIFIED MATERIAL THICKNESS OUT OF LIMITS, .020' TO .053, PER NDT SPM 04-00-06. CUT OUT DAMAGED AREA PER 53-2-1 FIG 7. FABBED AND INSTALLED DOUBLER, FILLER & FINGER DOUBLER PER SRM 53-2-1 FIG 7, 51-1-8, 51-1-21, 51-1-26, 51-1-20D.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP WHILE PERFORMING EMERGENCY LIGHT CHECK. REPLACED EMERGENCY LIGHT BATTERY PACK. LIGHTS OPS CHECKED NORMAL REFERENCE MM 33-50-01-2.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

EMERGENCY LIGHTS BATTERY PACK LOW VOLTAGE. REMOVED AND REPLACED EMERGENCY BATTERY PACK.

Part: BELL ASSY — WEAK (NR 4 FIRE DETCTR)

INSPECTION TYPE: PFLT, WHEN TESTING FIRE WARNING SYSTEM ON ALL 4 ENG FIRE WARNING BELL IS WEAK, BARELY AUDIBLE. REMOVED AND REPLACED BELL ASSY ENG FIRE WARNING SYSTEM, OPS CHECK PER MMNL 26-10-03. SYSTEM NORMAL.

Part: UPLOCK — OUT OF RIG (MLG)

INSPECTION TYPE:N/A, MLG DOOR UNSAFE LIGHT. PERFORMED PULL TEST, DOOR FAILED. PERFORMED TEST OF MAIN GEAR DOOR UP PROXIMITY SENSORS, GOOD IAW UPS DC8 MM 32-60-00. R&R PROXIMITY BOX IAW SRM 51-3-0. RIGGED DOOR UPLOCK CABLE RT SIDE CHECKED GOOD IAW UPS DC8 32-31-04. TIGHTENED LOOSE GROUND ON LT DOOR PROX SWITCH. DOOR LATCH SYSTEM FOR MAIN GEAR DOORS OPS CHECK GOOD IAW DC8 MM 32-60-00

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 INT CABIN CRACKED FRAME TO FORMER FITTING STA 12 RT STA 220. REMOVED AND REPLACED CRACKED FITTING.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 NR 1 PYLON O/B SIDE AT PNL 199A UPPER SKIN IS CRACKED. FABBED DOUBLER IAW DC8 SRM 54-2-0, INSTALLED DOUBLER IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (RT WING) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 RT WING STR 51 I/B SIDE AT STA 74 IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-24, INSTALLED FITTING IAW DC8 SRM 51-1-20D, TORQUED BOLT IAW DC8 SRM 51-1-23.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 L1 LWR FWD DOOR JAMB CORNER CRACKED AT FASTENER HOLE. INTERNAL DOUBLER CRACKED PER X-RAY INSP FOUND OX AND DOUBLE DRILLED HOLES, INSTALLED BUSHINGS IAW DAC DWG 47099818, FABBED REPAIR BUSHINGS IAW DAC DWG 4709987B, BLENDED GOUGES WITHIN LIMITS IAW DC8 SRM 553-2-0. ALODINED, PRIMED & INSTALLED DOUBLERS IAW 53-2-0 FIG 15.

Part: FITTING — CRACKED (RT WING) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 RT WING STR 51 I/B SIDE STA 74 IS CRACKED. REMOVED FITTING IAW DC8 SRM 51-1-20D, LOCATED DRILLED AND DEBURRED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED FITTING IAW DC8 SRM 51-1-20D, TORQUED BOLT IAW DC8 SRM 51-1-23.

Part: WEB — CRACKED (FUSELAGE) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 RT MLG DOOR CUTOUT AREA AFT WEB PNL OF UPLATCH CUTOUT IS CRACKED. FABBED NEW WEB IAW DAC DWG 5651021 & NEW ATTACH ANGLE IAW DAC DWG 56 51221. INSTALLED ASSY IAW DC8 SRM 51-1-21 & 51-3-0 AND 51-120D.

Part: WEB — CRACKED (FUSELAGE) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 RT MLG DOOR CUTOUT AREA AFT WEB PNL OF UPLATCH CUTOUT IS CRACKED. FABBED NEW WEB IAW DAC DWG 5651021 & NEW ATTACH ANGLE IAW DAC DWG 56 51221. INSTALLED ASSY IAW DC8 SRM 51-1-21, 51-3-0 & 51-1-20D.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 REPAIR DOUBLER 715-3L-12 STA 1690-1698 AND LONG 28L IS CLASSIFIED AS CAT D ONLY 2 ROWS OF FASTENERS BEYOND CUTOUT AND 3 OF 4 CORNERS OF CUTOUT ARE SQUARE. REMOVED EXISTING REPAIRS AND FITTINGS, FABBED, LOCATED & DRILLED DOUBLER & FILLER IAW DC8 SRM 53-2-0 FIG 7 SHT 5. INSTALLED DOUBLER FILLER & END FITTING IAW DC8 SRM 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB LONGERON 11 CRACKED APPROX 2 INCHES, FOUND BY X-RAY INSPECTION. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB LONGERON 11 CRACKED APPROX 2 INCHES, FOUND BY X-RAY INSPECTION. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 R2 DOOR UPPER AFT DOOR JAMB, LONGERON 11 CRACKED APPROX 2 INCHES, FOUND BY X-RAY INSPECTION. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 FLOOR PANEL STA 759-879 PANEL A DELAMINATED. FABBED NEW PANEL IAW UPS EO DC8 5320-9691C.

Part: FITTING — CORRODED (FUSELAGE) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 FWD PIT STA 278 ABOVE LONGERON 31R LOWER SURFACE OF FITTING CORRODED. REMOVED FITTING FOUND CORROSION OUT OF LIMITS IAW DC8 SRM 51-1-8 AND 51 -1-21 AND INSTALLED IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 CABIN INTERCOSTAL ATTACH FITTING HAS CRACK STA 902 L19L. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-24 AND 51-1-20D.

Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 LT SIDE FWD OVERWING EMERGENCY EXIT DOOR HAS CRACK INDICATION AT LOWER AFT CORNER, FOUND BY NDT INSPECTION. REPAIRED AREA IAW REO G08714.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 FWD CARGO AFT DOOR FRAME FWD LWR INNER SURFACE AT LIGHTENING HOLE MULTIPLE CRACKS, DOUBLER IS UNTREATED METAL AND FASTENERS ARE IMPROPERLY INSTALLED. REPAIRED WEB IAW DAC DWG 5616520.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 FLOORBEAM STA 879 RBL 60 IS CRACKED AT O/B LIGHTENING HOLE. SPLICED IN NEW SECTION OF FLOORBEAM IAW REO G08713.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 FLOORBEAM STA 879 RBL 60 IS CRACKED AT O/B LIGHTENING HOLE. SPLICED IN NEW SECTION OF FLOORBEAM IAW REO G08713.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 LT AFT PRESSURE BULKHEAD CRACKED AT FS 1766 L11L. REPAIRED AREA IAW DC8 SRM 53-2-5 FIG 14A AND DAC DWG SRO8530007.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 77,364 hrs · 50,326 cycles

INSPECTION TYPE:C1 RT APB CRACKED STA 1766 L11R OUTBOARD OF EXISTING DOUBLER. REPAIRED AREA IAW REO-G08719.

Part: LIFE VEST — TORN (COCKPIT)

INSPECTION TYPE:N/A CAPTS LIFE VEST TORN. REPLACED CAPT LIFE VEST.

Part: SLIDING WINDOW — OUT OF ADJ (COCKPIT)

INSPECTION TYPE:PFLT CAPTAIN SLIDING WINDOW WILL NOT OPEN. ADJUSTED PER MM 56-10-00. OPS CHECKS GOOD.

Part: WIRE — LOOSE (ELECTRICAL SYS)

INSPECTION TYPE:N/A NR 1 BUS OFF LIGHT ILLUMINATED AND SMOKE IN COCKPIT. RESECURED WIRE TO TERMINAL X2 OF LMR R2-25 OF NR 1 AC BUS OPS CHECKS NORMAL OF NR 1 AC BUS.

Part: SKIN — CRACKED (CARGO DOOR)

INSPECTION TYPE:IN PIT 33 DOOR LOWER SKIN CRACKED AFT LWR CARGO FWD DOOR BOTTOM EDGE OF SKIN DOUBLER, TORN & CRACKED IN 2 PLACES. FOUND PERVIOUS REPAIR FILLER DAMAGED, NO DAMAGE TO INTERNAL DOUBLER REMOVED AND REPLACED FILLER IAW SRM 51-2-0.

Part: SEAL — FAILED (COCKPIT WINDOW)

CAPTAINS CLEARVIEW SLIDING WINDOW SEAL BLOWN OUT.

Part: ROD END — BROKEN (NLG DOOR)

INSPECTION TYPE:N/A, CLIMBING THRU FL260 AT 320 KIAS A SUDDEN DEAFENING NOISE ACCOMPANIED BY CONSIDERABLE VIBRATION STARTED. SLOWING TO 200 KTS REDUCED THE NOISE AND VIBRATION TO TOLERABLE INTENSITY. NO PRESSURIZATION PROBLEMS WERE NOTED. VISUAL INSP THRU NOSE W/W VIEW PORT SHOWED ONLY MORE LIGHT THAN NORMAL. CONCLUSION WAS AN OPEN NLG DOOR. REMOVED AND REPLACED BROKEN NLG DOOR OPERATING MECHANISM AND UPPER RETRACT ROD ASSY PER M/M 32-22-02. P/N 5640832-5, S/N ON UP16210, S/N OFF NSN P/N 3646504, S/N ON TAG 906792, S/N OFF NSN. CK''''D PER M/M 32-22-01. JACKED AND SWUNG NOSE GEAR, OK.

Part: ACTUATOR — INOPERATIVE (RUDDER)

INSPECTION TYPE:N/A, ABORTED TAKEOFF DUE TO LIMITED RUDDER MOVEMENT. REMOVED RUDDER HYD PACKAGE PER MM 27-21-06. INSTALLED RUDDER HYD PACKAGE STEPS 1-21 MM 27-21-06 LEAK AND OPS CHECKS OK. ACCOMPLISHED RUDDER ADJ TEST IAW 27-20-00, OPS CHECKS GOOD.

Part: FITTING — CRACKED (CARGO BAY) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123. STA 1220, LONG 30 - 32 RT BANANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755847,AND SRM. 51-1-20D

Part: INTERCOSTAL — CRACKED (RT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123 RT WING L/E. LOWER INTERCOSTAL IS CRACKED AT XFS 341 REMOVED, FABRICATED, AND REPLACED INTERCOSTAL I.A.W. DWG. 5769589,AND SRM. 51-1-20D

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123. STA 790 LONGERON 18 LT, INTERCOSTAL IS CRACKED REMOVED, FABRICATED, AND REPLACED INTERCOSTAL I.A.W. DWG. 9779447

Part: DOUBLER — CRACKED (RT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, RIGHT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 628.75. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D, 51-1-21.

Part: DOUBLER — CRACKED (RT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123. RT WING L/E INTERNAL DOUBLER IS CRACKED AT XFS 304. REMOVED, FABRICATED, AND REPLACED DOUBLER I.A.W. DWG. 5769859,AND SRM. 51-1-21,51-1-20D

Part: DOUBLER — CRACKED (LT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 304. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123. UPPER AFT CORNER LEFT AFT SERVICE IS CRACKED STA 1320, LONG 11 LT. REPAIRED SKIN I.A.W. SRM. 53-2-0 FIG. 17

Part: FINGER DOUBLER — CORRODED (COCKPIT) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA -12 TO -32 FINGER DOUBLER IS CORRODED BEYOND LIMITS AT RBL 65. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW SRO 8530026 AND SRM 51-1-20D, 51-1-21.

Part: ANGLE — CRACKED (RT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, RIGHT WING LEADING EDGE I/B SUPPORT ANGLE IS CRACKED AT XFS -23.75. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5769646 AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (RT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, RIGHT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 341. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D, 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 680 LONG 5R FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779762 AND SRM 51-1-20D.

Part: FITTING — CRACKED (LT MLG WW) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123. LT MLG WW OB STA 879 LONG 24 LT, FITTING IS CRACKED REMOVED, FABRICATED, AND REPLACED FITTING I.A.W. DWG. 3641004,AND SRM. 53-2-0 FIG. 8

Part: ANGLE — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123. STA 500, LONG 33 LT, INTERCOSTAL TO FRAME ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED, AND REPLACED ANGLE I.A.W. DWG. 5753892, AND SRM. 51-1-20D,51-1-21

Part: SKIN — CRACKED (EMERGENCY EXIT) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123, RT AFT EMERGENCY EXIT DOOR SKIN IS CRACKED IN UPPER REAR CORNER AT STA. 822.5 . REPAIRED SKIN IAW SRM. 52-2-0 FIG. 2

Part: RIB — CRACKED (RT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, RIGHT WING AUX TANK HAS A RIB CRACKED AT XFS 188.750. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 445 LONG 36 SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3750330 AND SRM 51-1-20D.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 80 - 100 LBL 12 INTERCOSTAL IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5610326 AND SRM 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 741. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: INTERCOSTAL — CRACKED (LT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, LEFT WING L/E INTERCOSTAL IS CRACKED BETWEEN XFS 195 - 201. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5769859 AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 760. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, RIGHT WING L/E HAS UPPER RIBS CRACKED AT XFS 304, 310.25 AND 329. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (LT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, LEFT WING L/E SKIN IS CRACKED I/B OF XFS 710. REPAIRED SKIN IAW SRM 57-2-1 FIG 2H.

Part: RIB — CRACKED (LT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 360.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (LT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, LEFT WING L/E SKIN IS CRACKED O/B OF XFS 710. REPAIRED SKIN IAW SRM 57-2-1 FIG 2H.

Part: RIB — CRACKED (RT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 835. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123. STA 1314, LONG 21 RT, AFT LOWER CORNER OF RIGHT MID SERVICE DOOR CUTOUT IS CRACKED REPAIRED SKIN I.A.W. 8110-3. APPROVED DH SK 715-737

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123 STA. 1180 LONG. 35R BATH TUB FITTING IS CRACKED REMOVED AND REPLACED FITTING I.A.W. DWG. 3755843,AND SRM. 53-2-0 FIG. 2D

Part: RIB — CRACKED (LT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, LEFT WING L/E UPPER RIB IS CRACKED AT XS 250. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123 RIGHT WING L/E. UPPER RIBS ARE CRACKED AT XFS 347.75, 354, 397.75 REPAIRED RIBS I.A.W. SRM. 57-2-0 FIG. 2

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123. STA 1500, LONG 27 LT, VERTICLE FLOORBEAM SUPPORT IS CRACKED. REPAIRED SUPPORT I.A.W. SRM. 53-2-0 FIG. 1B

Part: DOUBLER — CRACKED (LT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, LEFT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 335.25. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-21, 51-1-20D.

Part: SKIN — CRACKED (RT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, RIGHT WING L/E LOWER SKIN IS CRACKED AT DRAIN HOLE AT XFS 597.5. REPAIRED SKIN IAW DC8-5720-4087-B.

Part: SKIN — CRACKED (LT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, LEFT WING L/E LOWER SKIN IS CRACKED AT XFS 628.75. REPAIRED SKIN IAW EO DC8-5720-4087-B.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123. STA 1520, LONG 27 LT VERTICLE FLOORBEAM SUPPORT IS CRACKED. REMOVED, FABRICATED, AND REPLACED SUPPORT I.A.W. DWG. 3610417,AND SRM. 51-1-20D

Part: RIB — CRACKED (RT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 841.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 1240 LONG 35L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758498 AND SRM 51-1-20D.

Part: DOUBLER — CRACKED (RT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, RIGHT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-21, 51-1-20D.

Part: DOUBLER — CRACKED (LT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, LEFT WING L/E INTERNAL DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, RIGHT WING L/E RIB IS CRACKED AT XOLDI 6.225. REPAIRED RIB IAW SRM 57-2-0 FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123, STA 280, LONG 33 RT, BANNANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG.3755827, AND SRM. 51-1-20D

Part: DOUBLER — CRACKED (LT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123. LT WING L/E LOWER INTERNAL DOUBLER IS CRACKED AT XFS 597.5. REMOVED, FABRICATED, AND REPLACED DOUBLER I.A.W. DWG. 5769600,AND SRM. 51-1-20D,51-1-21

Part: RIB — CRACKED (LT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, LEFT WING L/E HAS CRACKED RIBS AT XFS 797.5 UPPER AND XFS 816.25, AND 822.50 LOWER. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (RT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, RIGHT WING L/E UPPER DOUBLER IS CRACKED AT XFS 572.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769600 AND SRM 51-1-20D, 51-1-21.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 1260 - 1340 LONG 31L FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5750322 AND SRM 51-1-20D, 51-1-21.

Part: SKIN — CRACKED (LT WING) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, LEFT WING L/E LOWER INTERNAL TRIPLER IS CRACKED O/B SIDE OF XOLDI 6.225. REMOVED, FABRICATED AND REPLACED TRIPLER IAW DWG 5769891 AND SRM 51-1-20D.

Part: ANGLE — CRACKED (LT WING SPAR) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, LEFT WING L/E UPPER SUPPORT ANGLE IS CRACKED AT XRS 2 FRONT SPAR. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 4776168 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 1260 LONG 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 1766 LONG 17L AND END FITTING ARE CRACKED AFT OF PRESSURE BULKHEAD. REMOVED, FABRICATED AND REPLACED LONGERON AND FITTING IAW DWG 4772397, DC8-53B-009, AND SRM 53-3-3 FIG 5.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123. STA 1200, LONG 27 LT, AFT STOP BANNANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755854,AND SRM. 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 988 LONG 23R END FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3753306 AND SRM 51-1-20D.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 155 LONG 26R VERTICAL FLOORBEAM SUPPORT IS CRACKED. REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG 5705596 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 1240 LONG 33R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4758514 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 1150 LONG 35R INTERCOSTAL TO TORQUE BOX FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3758570 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 1766 LONG 10L END FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4772397 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 1220 BETWEEN LONG 33-34R BATHTUB IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 3755841 AND SRM 53-2-0 FIG 2G.

Part: BEAM — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123, STA 1766, 2ND J-BEAM FROM BOTTOM IS CRACKED ABOVE TAILSKID FITTING. REPAIRED J-BEAM IAW 8110-3 APPROVED DH SK 715-464

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 980 BULKHEAD VERTICAL SUPPORT FITTING IS CRACKED AT RBL 24. REMOVED AND REPLACED FITTING IAW DWG 3751514 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123, STA 1766, AFT SIDE LONG 10 RT, END FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG. 4772397, AND SRM. 51-1-20D

Part: FRAME — DAMAGED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123, STA 1140, LONG 33 LT HAS A DOUBLE DRILLED HOLE IN RADIUS OF FRAME. REPAIRED FRAME I.A.W. 8110-3 APPROVED DH SK 715-436

Part: LONGERON — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123. STA 1766, LONG 17 RT, AFT SIDE FITTING AND LONGERON ARE CRACKED REMOVED, FABRICATED, AND REPLACED FITTING AND LONGERON I.A.W. DWG. 4772397,AND SRM. 53-2-0 FIG. 10

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 822 LONG 11L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.

Part: LONGERON — CUT (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 1040 - 1060 LONG 35L HAS A CUT. REPAIRED LONGERON IAW 8110-3 APPROVED DH SK 715-515.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123. STA 1150, LONG 33 RT, BANNANA FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3755847, AND SRM. 51-1-20D

Part: BRACKET — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 660 LONG 36 BRACKET ADJUSTMENT SUPPORT IS CRACKED. REMOVED, FABRICATED AND REPLACED SUPPORT IAW DWG 5755360 AND SRM 51-3-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 902 LONG 19L INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779498 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 834 LONG 11B INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 1140 LONG 20R INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4750418 AND SRM 51-1-20D.

Part: FITTING — CRACKED (CABIN) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 857 LONG 18L INTERCOSTAL TO FRAME FITTING IS CRACKED AFT SIDE. REMOVED AND REPLACED FITTING IAW DWG 4750420 AND SRM 51-1-20D.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 759 LONG 18L INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779978 AND SRM 51-1-20D.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123, STA 680, LONG 31 RT, IS CORRODED BEYOND LIMITS. REPAIRED LONGERON IAW 8110-3 APPROVED DH SK 715-208.

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123, STA 1760, LONG 17 LT, END FITTING IS CRACKED. REMOVED, FABRICATED, AND REPLACED FITTING IAW DWG. 4772397, AND SRM. 51-1-20D

Part: FITTING — CRACKED (FUSELAGE) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE: C123, STA 798, LONG 18 LT, INTERCOSTAL TO FRAME FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG.4751639, AND SRM. 51-1-20D

Part: FITTING — CRACKED (MAIN CABIN) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 857 LONG 18L INTERCOSTAL TO FRAME FITTING IS CRACKED FWD SIDE. REMOVED AND REPLACED FITTING IAW DWG 3779498 AND SRM 51-1-20D.

Part: SPLICE — CRACKED (FUSELAGE FRAME) · airframe 76,102 hrs · 49,432 cycles

INSPECTION TYPE:C123, STA 160 BETWEEN LONG 7-8R FRAME SPLICE IS CRACKED. REMOVED, FABRICATED AND REPLACED SPLICE IAW SRM 53-2-0 FIG 2.

Part: MECHANISM — BINDING (RUDDER)

RUDDER BINDING DURING TAKEOFF ROLL, NORMAL OPERATION UNTIL AFTER LANDING AND TAXI. RUDDER BINDS LIMITING TRAVEL TO 3 INCH RUDDER PEDAL MOVEMENT PROBLEM WITH RUDDER IS SPORADIC. REF LOG PAGE 138103. REMOVED AND REPLACED LOAD FEEL MECHINISM. SYSTEM OPS CHECKS GOOD IAW DC8MM27-23-01, P/N OFF 3760963-501, S/N OFF UPO4627, P/N ON 3760963-501, S/N ON OA2175.

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A, EMER EXIT LIGHTS FAILED TO DISARM. REMOVED AND REPLACED EMERGENCY BATTERY PACK PER MM 33-50-01. SYSTEM OPS CHECKS NORMAL.

Part: LIGHT — INTERMITTENT (COCKPIT)

EMERGENCY EXIT LIGHT DOES NOT REMAIN ILLUMINATED AFTER DISARM CHECK ON SHUTDOWN CHECKLIST. CYCLED EMERGENCY LIGHT SWITCH. LIGHT OPS CHECK NORMAL.

Part: ACTUATOR — LEAKING (TE FLAP)

INSPECTION TYPE:N/A, AFTER LANDING WHEN PULLING INTO PARKING RES PRESSURE LIGHT ILLUMINATED AND THEN FLIGHT CONTROL MANUAL LIGHTS. ONLY HAD ACCUMULATOR PRESSURE TO STOP AIRCRAFT. FLAPS DID NOT RETRACT. REMOVED AND REPLACED INBOARD LT FLAP ACTUATOR, OPS CK AND FUNCTIONAL CHECK NORMAL. NO LEAKS NOTED IAW MM 27-51-09 PAGE 410.

Part: WINDOW — JAMED (RT COCKPIT)

INSPECTION TYPE:N/A, F/O SLIDING WINDOW WILL NOT OPEN (JAMMED SHUT). ADJUSTED F/O WINDOW PER MM 56-10-03, OPS CHECK GOOD.

Part: LIGHT — INOP (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS WILL NOT DISARM. PERFORMED EMERGENCY LIGHT OPERATIONAL TEST IAW MM REF 33-50-01 PAGE 201, OPS CHECK GOOD.

Part: BRAKE — INOP (MLG)

INSPECTION TYPE:N/A, BTB - NUMBER 8 BRAKE STUCK. REMOVED AND REPLACED MAIN BRAKE ASSY PER MM 32-42-01.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATT PACK OPS GOOD PER 33-50-00.

Part: BATTERY PACK — DISCHARGED (CABIN)

EEL INOP. REPLACED EMERGENCY EXIT LIGHT BATT PACK PER MM 33-50-00. OPS CHK GOOD.

Part: FITTING — CRACKED (BS 8)

INSPECTION TYPE-C, STA 8 STR 22R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4711722 AND SRM 51-1-20D.

Part: WEB — CRACKED (BS 520)

INSPECTION TYPE-C, STA 520 AT STR 32R, THE TORQUE BOX WEB IS CRACKED. REPAIRED AREA IAW SRM 53-2-0 AND DWG 5616520.

Part: DOUBLER — CORRODED (BS 10-20)

INSPECTION TYPE:C COCKPIT SUB-FLOOR FINGER DOUBLER AT STA -10 TO-20 BLB50 HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5612298 AND SRM 51-1-21.

Part: DOUBLER — CORRODED (BS 1541-1590)

INSPECTION TYPE-C, STA 1541 TO 1590 AT STR 31L, THE FINGER DOUBLER IS CRACKED AND CORRODED. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5615674 AND SRM 51-1-21.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE-C, A/C COMP AT STA 70, STR 21R TIE FITTING UNDER CUSP HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D, AND SRM 51-3-0.

Part: LONGERON — CORRODED (BS 35)

INSPECTION TYPE-C, A/S COMP, STA 35, STR 36 IS CRACKED AND CORRODED. REMOVED FABRICATED AND INSTALLED LONGERON IAW DWG 3615532 AND SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (BS 1240-1260)

INSPECTION TYPE-C STA 1240 TO 1260 AT STR 33L, THE INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 9753792 AND SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 8-25)

INSPECTION TYPE-C, STA 8 TO 25, LONG 33L IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED LONGERON IAW DWG 3642838 AND SRM 51-1-21.

Part: ANGLE — CORRODED (BS 380)

INSPECTION TYPE:C STA 380 AT STR 21R, THE CUSP ANGLE IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 9754069 AND SRM 51- 1-21D.

Part: LONGERON — CORRODED (BS 1440-1520)

INSPECTION TYPE-C, STA 1440 TO 1520, LONG 31R IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED SECTION OF LONGERON IAW DWG 3646771 AND SRM 51-1-21.

Part: SKIN — CORRODED (BS 1440-1450)

INSPECTION TYPE-C, STA 1440 TO 1450 AT STR 31R, THE SKIN IS CORRODED BEYOND LIMITS. REPAIRED AREA IAW SRM 53-2-1 FIG 7.

Part: SPLICE — CRACKED (BS 1040-1060)

INSPECTION TYPE-C, LONG 31R SPLICE FITTING CRACKED FS 1040 TO 1060. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: FITTING — CRACKED (WS 1690)

INSPECTION TYPE:C STA 1690, LONG 28 LT END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AND SRM 51-1-20D.

Part: DOUBLER — CORRODED (BS 1440-1520)

INSPECTION TYPE-C, STA 1440 TO 1520 AT LONG 31R, THE FINGER DOUBLER IS CORRODED BEYOND LIMITS. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5615372 AND SRM 51-1-21.

Part: DOUBLER — CRACKED (BS 1541-1580)

INSPECTION TYPE:C STA 1541-1580 AT STR 31R, THE FINGER DOUBLER IS CRACKED AND CORRODED. REMOVED, FABRICATED AND REPLACED FINGER DOUBLER IAW DWG 5779936 AND SRM 51-1-21.

Part: FITTING — CRACKED (BS 8)

INSPECTION TYPE-C, STA 8.00, STR 33L END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 9612650 AND SRM 51-1-20D.

Part: WEB — CRACKED (BS 702)

INSPECTION TYPE-C, STA 702, RBL 45 TO 50 (WING CENTER SECTION) THE FLOORBEAM WEB HAS A 4 INCH CRACK. REPAIRED AREA IAW DHC SK 715-054.

Part: FRAME — CRACKED (BS 55)

INSPECTION TYPE:C STA 55 AT STR 24L, THE FRAME IS CRACKED. REPAIRED AREA IAW SRM 53-2-0 FIG 3.

Part: ANGLE — CORRODED (BS 798)

INSPECTION TYPE:C, WING CENTER SECTION ( UPPER ) AT FS 798 RBL 44, CHORD ANGLE HAS HEAVY CORROSION. REMOVED AND REPLACED CHORD ANGLE IAW SRM 51-1-20D.

Part: FRAME — CRACKED (BS 55)

INSPECTION TYPE:C STA 55 AT STR 24R, THE FRAME IS CRACKED. REPAIRED AREA IAW SRM 53-2-0 FIG 3.

Part: LONGERON — CRACKED (BS 1700)

INSPECTION TYPE:C, LONGERON 36 FS 1700 IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 53-2-2.

Part: FITTING — CRACKED (BS 1280)

INSPECTION TYPE:C STA 1280 ABOVE STR 33R, THE SEAT TRACK SUP[PORT FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 5758571 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1290)

INSPECTION TYPE:C STA 1290 AT STR 21L, THE FRAME TO CUSP TIE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 975584 AND SRM 5 1-1-20D.

Part: LONGERON — CRACKED (BS 1260-1280)

INSPECTION TYPE:C STA 1260-1280, STR 34R IS CRACKED ON UNDERSIDE OF RT FLANGE. REPAIRED AREA IAW DHC SK 715-548.

Part: SPLICE — CRACKED (BS 380-400)

INSPECTION TYPE:C, LONGERON 31L SPLICE FITTING CRACKED FS 380-400. REMOVED AND REPLACED FITTING IAW SRM 51-1-20.

Part: SPLICE — CRACKED (BS 600-620)

INSPECTION TYPE-C, LONG 31R SPLICE FITTING CRACKED FS 600 TO 620. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21D AND DWG 3750257-1N.

Part: LONGERON — CRACKED (BS 1260-1280)

INSPECTION TYPE-D, STA 1260 TO 1280, STR 35L IS CRACKED ON THE UNDERSIDE. REPAIRED AREA IAW DHC SK 715-547.

Part: SPLICE — CRACKED (BS 1040-1060)

INSPECTION TYPE-C, FS 1040 TO 1060 STRINGER 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SPLICE — CRACKED (BS 440-460)

INSPECTION TYPE-C, LONGERON SPLICE FITTING CRACKED FS 440 TO 460 L-31R. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: WEB — CORRODED (BS 1200-1220)

INSPECTION TYPE-C, STA 1200-1220 ABOVE STR 35R, THE TORQUE BOX WEB HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED WEB IAW SRM 53-2-0 FIG1D.

Part: FRAME — CRACKED (BS 1400)

INSPECTION TYPE:C STA 1400 FRAME BTWN STR 35L-36 IS CRACKED ON END. REPAIRED AREA IAW DHC SK 715-883.

Part: BRACKET — CORRODED (BS 1756-1766)

INSPECTION TYPE-C, STA 1756 TO 1766 AT BL O, THE T-BRACKET HAS HEAVY CORROSION OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED REPLACEMENT BRACKET IAW DWG 5753522 AND SRM 51-1-20D.

Part: SPLICE — CRACKED (BS 440-460)

INSPECTION TYPE:C, LONGERON 31L SPLICE FITTING CRACKED FS 440-460. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: FITTING — CORRODED (BS 1690)

INSPECTION TYPE:C STA 1690, STR 30L END FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AND SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1717)

INSPECTION TYPE-C, HEAVY CORROSION ON LONGERON 34R FS 1717. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION IAW SRM 53-5-1.

Part: FITTING — CRACKED (BS 1766)

INSPECTION TYPE:C, TAIL SKID INTERNAL MOUNT FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20.

Part: DOUBLER — CORRODED (BS 1776)

INSPECTION TYPE:C, FS 1776 DOOR 62 DOUBLER SEVERE EXFOLIATED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1- 20 AND DWG 5649329.

Part: LONGERON — CORRODED (BS 1700)

INSPECTION TYPE-C, HEAVY CORROSION ON LONGERON 30L FS 1700. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-20D AND DWG 5649329.

Part: SKIN — CRACKED (BS 25)

INSPECTION TYPE:C FUSELAGE SKIN IS CRACKED AROUND FWD ENTRY DOOR HOLD OPEN ROD (STA 25 ). REPAIRED IAW SRM 53-3-3 FIG 1.

Part: FITTING — CORRODED (BS 1690)

INSPECTION TYPE:C STA 1690, LONG 34R END FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW DWG 4641324 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 3)

INSPECTION TYPE:C RT WING T/E RIB AT STA XW 3.00, IS CRACKED IN 4 PLACES. REPAIRED AREA IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 329)

INSPECTION TYPE:C RT WING L/E AT STA XFS 329.000- THE LWR L/E RIB IS CRACKED AT MID SPAN. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 778.750)

INSPECTION TYPE-C, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER WS XFS 778.750. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (WS 347.5)

INSPECTION TYPE:C RT WING L/E LWR SKIN AT STA XFS347.500 IS CRACKED IN 2 PLACES. REPAIRED AREA IAW SRM 57-2-1 FIG 2.

Part: RIB — CRACKED (WS 597.5)

INSPECTION TYPE-C, RT WING L/E AT WS XFS 597.5 THE LWR L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (BS 240-260)

INSPECTION TYPE:C, BETWEEN FS 240-260, L-34L TO L-35L 8 CRACK IN OUTER PLATING FUSELAGE SKIN. REPAIRED IAW DHC SK 715-633.

Part: SKIN — CRACKED (WS 304)

INSPECTION TYPE-C, RT WING L/E SKIN IS CRACKED AT WS XFS 304.00. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 397.75)

INSPECTION TYPE-C, RT WING L/E AT WS XFS 397.75 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 691.25)

INSPECTION TYPE-C, RT WING L/E AT WS 691.250 THE LWR L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 847.5)

INSPECTION TYPE-C, RT WING L/E RIB CRACKED AT WS XFS 847.5 UPPER AFT END. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (WS 616.25)

INSPECTION TYPE-C, LT WING L/E UPPER SKIN CRACKED AT WS XFS 616.25 APPROX 2 INCHES FWD OF T/E. REPAIRED IAW SRM 57-2-1.

Part: RIB — CRACKED (WS 810)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER XFS 810.000. REPAIRED IAW SRM 57-2-0.

Part: DOUBLER — CORRODED (WS 797.5)

INSPECTION TYPE:C, RT WING L/E AT W/S XFS 797.500, THE INTERNAL DOUBLER HAS HEAVY CORROSION AT O/B END OF ACCESS PANEL. REMOVED AND REPLACED DOUBLER IAW SRM 51-1-21.

Part: SKIN — CRACKED (WS 610)

INSPECTION TYPE-C, LT WING L/E UPPER SKIN CRACKED AT XFS 610 APPROX 2 INCHES FWD OF T/E. REPAIRED IAW SRM 57-2-1.

Part: RIB — CRACKED (WS 385.25)

INSPECTION TYPE-C, RT WING L/E AT WS XFS385.25 THE LWR L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW 57-2-0.

Part: RIB — CRACKED (WS 778.75)

INSPECTION TYPE-C, RT WING L/E AT WS 778.750 THE UPPER L/E RIB IS CRACKED AT THE AFT UPPER END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 697.5)

INSPECTION TYPE-C, RT WING L/E AT WS XFS 697.5 THE LWR L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 772.5)

INSPECTION TYPE-C, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER XFS 772.5. REPAIRED IAW SRM 57-2-0.

Part: ACCESS PANEL — CRACKED (LT WING TANK)

INSPECTION TYPE:C, LT WING NR 2 MAIN TANK INBD AFT ACCESS PANEL LAND CRACKED AT OTBD AFT CORNER. REPAIRED IAW SRM 57-2-1.

Part: SKIN — CRACKED (WS 628.75)

INSPECTION TYPE-C, LT WING L/E UPPER SKIN CRACKED AT WS XFS 628.750 APPROX 2 FWD FROM T/E. REPAIRED IAW SRM 57-2-1.

Part: SKIN — CRACKED (WS 597.5)

INSPECTION TYPE-C, LT WING L/E UPPER SKIN CRACKED AT WS 597.500 APPROX 2 INCHES FWD OF T/E. REPAIRED IAW SRM 57-2-1.

Part: DOUBLER — CORRODED (WS 828.75)

INSPECTION TYPE:C, RT WING L/E AT W/S XFS 828.75, THE INTERNAL DOUBLER HAS HEAVY CORROSION AT FWD END OF ACCESS PANEL. REMOVED AND REPLACED DOUBLER IAW SRM 51-1-20.

Part: DOUBLER — CORRODED (WS 728 & 741)

INSPECTION TYPE:C LT WING L/E INTERNAL DOUBLER HAS HEAVY CORROSION AT STA XFS 728. 750 AND XFS741.250. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 3641257 AND SRM 51-1-20D.

Part: SKIN — CRACKED (WS 603.75)

INSPECTION TYPE-C, LT WING L/E UPPER SKIN CRACKED AT WS 603.75 APPROX 2 INCHES FWD OF T/E. REPAIRED IAW SRM 57-2-1.

Part: SKIN — CRACKED (WS 283.25)

INSPECTION TYPE:C RY WING L/E SECTION BTWN PYLONS AT STA XFS283.250, THE L/E SKIN IS CRACKED AT THE L/E. REPAIRED AREA IAW SRM 57-2-1 FIG 2H.

Part: CARGO TRACK — CORRODED (BS 1240-1320)

INSPECTION TYPE:C, FS 1240-1320 ABOVE STR 33R, CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRACK IAW SRM 51-3-0 AND DWG 5751516.

Part: FITTING — CRACKED (BS 320)

INSPECTION TYPE-C, NR 1 PIT, THE LWR AFT T-BOLT FITTING IS CRACKED (STA 320). REMOVED AND REPLACED FITTING IAW SRM 51-3-0.

Part: FITTING — CRACKED (WS 98)

INSPECTION TYPE:C RT WING T/E AT STA 98.00, THE REAR SPAR VERTICAL STIFFNER FITTING WHICH TIES TO THE FLAP CYCLINDER FITTING IS CRACKED AT THE BOTTOM. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3643319 AND SRM 51-1-20D.

Part: FRAME — CRACKED (BS 683)

INSPECTION TYPE:C FWD ACC COMP AT STA 683 AND STR 30R, THE FRAME CHORD IS CRACKED. STOP DRILLED CRACK AND REPAIRED IAW SRM 53-2-5 FIG 14.

Part: CARGO TRACK — CORRODED (BS 1410-1490)

INSPECTION TYPE:C, FS 1410-1490 ABOVE STR 33L, CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRACK IAW SRM 51-3-0 AND DWG 5151516.

Part: CARGO TRACK — CORRODED (BS 1330-1410)

INSPECTION TYPE:C, FS 1330-1410 ABOVE STR 33L, CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT CARGO TRACK IAW SRM 51-3-0 AND DWG 5751516.

Part: CARGO TRACK — CORRODED (BS 980-1070)

INSPECTION TYPE:C, FS 980-1070 ABOVE STR 33L, CARGO TRACK HAS HEAVY CORROSION. REMOVED AND REPLACED CARGO TRACK IAW SRM 51-3-0.

Part: SKIN — CRACKED (WS 603.75)

INSPECTION TYPE-C, RT WING L/E SKIN (UPPER) HAS 4 CRACKS AT STA XFS603.750. REPAIRED AREA IAW SRM 57-2-0 FIG 2A.

Part: FITTING — CRACKED (WS 98)

INSPECTION TYPE:C RT AUX SPAR AREA, THE REAR SPAR TO AUX SPAR LWR TIE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DHC SK 715-421 AND DWG 5642205.

Part: CARGO TRACK — CORRODED (BS 980-1070)

INSPECTION TYPE:C, FS 980-1070 ABOVE STR 33R, CARGO TRACK AND SPLICE HAVE HEAVY CORROSION. REMOVED AND REPLACED CARGO TRACK IAW SRM 51-3-0.

Part: FRAME — CORRODED (BS 8)

INSPECTION TYPE-C, BULGING AT THE CUSP STA 8 AT LONG 21R. REMOVED FASTENERS FOUND STA 8 FRAME CORRODED OUT OF LIMITS. CUT OUT DAMAGED FRAME, FABRICATED AND REPLACED FRAME PER DAC DWG 5641783 AND SRM 51-1-20D.

Part: CARGO TRACK — CORRODED (BS 120)

INSPECTION TYPE-C, STA 120 ABOVE STR 33R, THE CARGO TRACK HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED TRACK IAW DWG 5151516 AND SRM 51-3-0.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMER LTS INOP. REMOVED AND REPLACED EMER BATTERY PACK, GROUND CHECKS NORMAL. ON P/N 5708458-503 S/N FTL 145 OFF P/N 5708458-503 S/N 925.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE-N/A, VISIBLE CORROSION NOTICED LEFT OF CENTER ACCESSORY ACCESS TRANSCRIBED TO SV PACKAGE NON-ROUTINE 724751, TEMPORARY REPAIR INSTALLED IAW UPS EO DC8-5330-9765A. THIS ITEM TO BE MPI'D ON L/P 871216 ITEM NR 3.

Part: SLIDING WINDOW — OUT OF ADJUST (RT COCKPIT)

INSPECTION TYPE-N/A, F/O SLIDING WINDOW WILL NOT OPEN. ADJUSTED F/O'S SLIDING WINDOW, SEE L/P 871217 ITEM 3.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, ON PREFLIGHT EMERGENCY EXIT LIGHTS WOULD NOT TEST, NO LIGHT ILLUMINATION. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECKED OK PER MM 33-50-01.

Part: FITTING — CRACKED (XRS 408)

INSPECTION TYPE:S/V, STRINGER AND FITTING CRACKED NR 62 APPROX XRS408 P/N 3616846-505. REMOVED CRACKED END FITTING AND INSTALLED NEW END FITTING P/N 361684 6-505 IAW DC8 SRM 51-1-23 AND 51-1-20D.

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE-SV, 9.4375 INCH CRACK FOUND ON RT WING JUST I/B OF THE NR 4 PYLON DURING ROUGH AIR INSP. PERMANENT REPAIR INSTALLED AS PER TIMCO REO-03156 ROD SKETCH 97-05-0 1-002 DC8 SRM 57-2-2 AND DAC DWG 5612385 AND 5613420 FINAL FOR FABRICATION OF ALL REPAIR PARTS SEE REO-03156.

Part: FRAME — CRACKED (BS 433)

INSPECTION TYPE-C/CK, FRAME CRACKED RW CTR LE AT APPROX STA 433 TOP SIDE. FABRICATED REPAIR IAW DC8 SRM 57-2-0, ALODINED AND PRIMED IAW DC8 SRM D 51-1-8. INSTALLED REPAIR IAW DC8 SRM D 51-1-20D AND DC8 SRM 51-1-21.

Part: BRACE — CRACKED (BS 660)

INSPECTION TYPE-C/CK, FRAME BRACE CRACKED AT STA 660 LT FWD OF WING SUPPORT. REMOVED CRACKED FRAME BRACE ANGLE, FABRICATED NEW ANGLE IAW DC8 SRM 53-8-1 FIG 1 SHEET 2, ALODINED AND PRIMED IAW DC8 SRM 51-1-8, INSTALLED ANGLE IAW DC8 SRM 51-30SD AND 51-1-20D.

Part: SLOT BRACE — CRACKED (LT LE SLAT)

INSPECTION TYPE-C/CK, LT CENTER LE SLOT BRACE CRACKED AT FWD END O/B OF PANEL 522A TOP SIDE OF LE. REMOVED CRACKED BRACE IAW DC8 SRM 51-1-24 AND DC8 SRM 51-1-20D MATERIAL ID IAW DC8 SRM 57-30D, FABRICATED DOUBLER IAW DC8 SRM 57-2-0 AND DC8 SRM 51-1-24, ALODINED AND PRIMED DOUBLER IAW DC8 SRM 51-1-8, INSTALLED DOUBLER IAW DC8 SRM 51-1-20D AND DC8 SRM 51-1-21.

Part: HINGE — CRACKED (LT REAR SPAR)

INSPECTION TYPE-C/CK, LOWER REAR SPAR O/B AILERON O/B HINGE CRACKED. REMOVED LT O/B AILERON, REMOVED AND REPLACED SUPPORT ASSY IAW DC8 SRM 51-3-1 AND REINSTALLED LT O/B AILERON IAW DC8 MM 27-11-02.

Part: FUEL FILTER — MALFUNCTIONED (NR 3 ENG)

INSPECTION TYPE N/A, REMOVED AND REPLACED FUEL FILTER ASSY DUE TO ENGINE FLAME-OUT, NR 3. REPLACED FUEL FILTER ASSY, NO CONTAMINATION FOUND REF MM 27-00-00. LEAK CHK'D NR 3 FUEL FILTER AS REQUIRED AND NO LEAKAGE NOTED.

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE 'B', CRACK PROTRUDING FROM RIVET HEAD OUTBOARD AND FWD PANEL 523, FIRE BOTTLE ACCESS MARKED. REMOVED CRACKED AREA OF THE SKIN. INSTALLED FILLER AND DOUBLER PER SRM 57-2-1.

Part: SKIN — CRACKED (FUSELAGE BELLY)

INSPECTION TYPE 'B', 3 CRACKS IN SKIN PROTRUDING FROM RIVETS IN BELLY SKIN 3 INCHES AFT OF LT AFT NOSE WHEEL WELL DOOR. INSTALLED DOUBLER PER SRM 53-2-1.

Part: RETRACT MECH — MALFUNCTIONED (LT MLG DOOR)

CREW REPORTED, AFTER T/O AND GEAR RAISED, DOORS NOT LATCHED LIGHT STAYED ON. RECYCLED GEAR AND COMPLIED WITH CHECK LIST, LIGHT REMAINED ON, CONTINUED TO SDF AT M 0.6. INSTALLED NEW CABLE PULLEY IN LT MLG DOOR FOLLOW-UP SYSTEM. LT MLG DOOR FOLLOW-UP SYS REQUIRES ADJ TEST. ADJUSTED LT MLG DOOR FOLLOW-UP MECHANISM IAW UPLATCH MECHANISM IAW DC8 MM 32-31-04. TEST GOOD, NO GEAR DOOR LIGHT DISCREPANCIES NOTED.

Part: SWITCH — MALFUNCTION (LT MLG DOOR)

CREW REPORTED ON DEPARTURE, ROD GEAR DOOR NOT LATCHED LIGHT ILLUMINATED. CYCLED GEAR AND PERFORMED UPLATCH CHECK. LIGHT WENT OUT. HOWEVER, LT MAIN AMBER ALTERNATE GEAR DOOR LIGHT REMAINED OUT, UNTIL APPROACH IN TURBULANCE, THEN AMBER LIGHT WENT OUT. REMOVED AND REPLACED LT GEAR ALTERERNATE SWITCH. C/W ADJ AND TEST PROCEDURES OF POS. AND WARNING SYS. PER DCE MM 32-60-00, PG 203, SYS OPS NORMAL.

Part: FLOORBEAM WEB — CORRODED (FS 80)

WHILE IN DALFORT FOR C-CHECK, MAINT FOUND HEAVY CORR ON LOWER SIDE OF VERT WEB FS 80 FWD SIDE OF FLOORBEAM, LT SIDE OF COCKPIT SUBFLOOR AREA. REPLACED VERT WEB PER SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 520-540)

WHILE IN DALFORT FOR C-CHECK, HVY. CORR. AT LONGERON 33R, FS 520-540. REPAIRED PER E.O. DC8-5310-7236-A.

Part: SUB FLOOR — CORRODED (FUSELAGE)

WHILE IN DALFORT FOR C-CHECK, HVY. CORR. DAMAGE ON FLT DECK SUB-FLOOR PRESSURE PANEL. REPAIRED PER E.O. DC8-5310-7237-A.

Part: FITTING — CORRODED (BS 300/320)

WHILE IN DALFORT FOR C-CHECK, CORR. AT DOOR FITTING, FS 300 AND 320, BETWEEN LONGERON 33R-A AND 33L. REPLACED PER SRM 51-1-20D AND SRM 51-1-21.

Part: FITTING — CORRODED (BS 280)

WHILE IN DALFORT FOR C-CHECK, MODERATE CORR. ON B/T FITTING, FS 280, BETWEEN LONGERONS 34R-33R (AFT SIDE). REPLACED FITTING PER SRM 51-1-20D.

Part: SHEAR TIE — CORRODED (BS 1020)

WHILE IN DALFORT FOR C-CHECK, SHEAR TIE HAS CORR AT FS 1020, BETWEEN LONGERONS 35L-36. REPLACED PER SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1200/1205)

WHILE IN DALFORT FOR C-CHECK, CORR. ON T-FITTINGS, NR 5, FS 1205 AND FS 1200 AND NR 4 FS 1195, LONGERON 33R. REPLACED PER SRM 53-2-0 AND SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1270-1350)

WHILE IN DALFORT FOR C-CHECK, CORR. AT LONGERSON 31L, FS 1270-1280 AND FS 1350. REPAIRED PER E.O. DC8-5310-7244A AND DC8-5310-7240-A.

Part: SKIN — CORRODED (BS 1050-1350)

WHILE IN DALFORT FOR C-CHECK, HVY. CORR. DAMAGE AND BULGES AT FUSELAGE BELLY SKIN, FS 1050 - 1350. REPLACED PER DAC DRAWING 570322 AND SRM 51-1-20D.

Part: FITTING — CORRODED (BS 160)

WHILE IN DALFORT FOR C-CHECK, T-FITTING HAS CORR. AFT SIDE OF FS 160, LONGERON 21R. REPLACED SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1510-1530)

WHILE IN DALFORT FOR C-CHECK, CORR. AT FINGER DOUBLER FS 1510-1520, LONGERONS 31R-29R. REPLACED PER SRM 51-1-20D.

Part: FRAME — CORRODED (BS 1140)

WHILE IN DALFORT FOR C-CHECK, CORR. ON BELT FRAME LOWER FWD LIP FS 1140, LONGERON 35L-36. REPAIRED PER DC8-5310-7238-A.

Part: VANE — DELAMINATED (NR 2 TE FLAP)

WHILE IN DALFORT FOR C-CK, MAINT FOUND LT WING NR 2 FLAP VANE DELAM. REPLACED PER MM 27-51-14.

Part: SKIN — DELAMINATED (NR 3 SPOILER)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND RT WING SPOILER NR 3 DELAMINATED AT LOWER SURFACE. REPLACED IAW M/M 27-61-01.

Part: SKIN — CRACKED (RT AILERON)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND RT I/B AILERON LOWER SKIN CRACKED O/B OF I/B HINGE CUTOUT. REPAIRED IAW SRM 57-2-0.

Part: FITTING — CRACKED (FS 812)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND BELT FRAME END FITTING CRACKED AT F.S. 812, LONGERON 21R. REPAIRED FITTING PER SRM 51-1-20D.

Part: ANGLE — CRACKED (FS 781-812)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND 3 EACH CRACKED L-ANGLES LOWER SIDE OF CENTER WING BOX, F.S. 781, RBL AND LBL 69 AND F.S. 812, LBL 69. REPAIRED ANGLES PER SRM 53-2-0.

Part: RIB — CRACKED (LT WING)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND LT WING LEADING EDGE 7 EACH RIBS CRACKED AT STA XFS 835, XFS 817, XFS 804 LOWER, XFS 823, XFS 804 UPPER, XFS 720, AND XFS 763. REPAIRED RIBS PER MM 57-00-00, FIG 801.

Part: TAB — DELAMINATED (RT AILERON)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND RT INBOARD AILERON OUTBOARD TAB DELAMINATED. REPLACED TAB ASSY PER T/C CL11R-42.

Part: RIB — CRACKED (RT WING)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND RT WING OUTBOARD LEADING EDGE 4 EACH UPPER RIBS CRACKED AT STA XFS 735, XFS 791, XFS 811, AND XFS 817. REPAIRED RIBS PER MM 57-00-00, FIG. 801.

Part: SWITCH — MALFUNCTIONED (RT MLG)

PILOT REPORTED RT MAIN LANDING GEAR DID NOT INDICATE DOWN AND LOCKED, BOTH GEAR NOT LATCHED AND DOOR NOT LATCHED LIGHTS REMAINED ILLUMINATED, RECYCLED GEAR, ALL INDICATIONS NORMAL. REPLACED RT MAIN GEAR DOWNLOCK SWITCH - PERFORMED GEAR SWING, ALL INDICATIONS NORMAL.