N748UP

Part: ACTUATOR — MALFUNCTIONED (COCKPIT)

CREW LOST NR 2 INS WITH A WARNING LIGHT. SMELLED ELECTRICAL FUMES FROM PEDESTAL AREA. TURNED NR 2 INS OFF. NOTICED PTC WAS NOT FULLY RETRACTED AND HAD 3/8 EXTENSION SHOWING. FOLLOWED PROCEDURES FOR PTC NOT FULLY RETRACTED. CREW DECLARED EMERGENCY W/TULSA. REMOVED AND REPLACED PTC ACTUATOR AND TESTED PER MM 27-30-07. OPS CHECKS GOOD ON GROUND.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C-1, MAIN CABIN SEAT TRACK G & H AT FS 418 HAS EXFOLIATION. SEAT TRACK AREA DAMAGED RMVD LOCATED AND DRILLED NEW SEAT TRACK SPLICE FITTING AND SPLICE CHANNEL IAW EO DC8 5320-8309-D. INSTALLED IAW EO DC 8 5320-8309D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE:C-1 CORROSION AROUND FASTENER HOLE ON L35 RT STA 1040-1060 INTERNAL AFT PIT, REMOVED INTERCOSTAL & CLIP AT STA 1040 - 1060 RT L35 RT IAW DC8 SRM 51-1- 20D. FILLET PANELS 1924 & 191CC IAW DC8 SRM 51-3-1 EVOL LONGERON SPLIC E 51-1-20D, FOUND TO BE CRACK, RECEIVED, LOCATED & DRILLED UP LONGERON SPLICE 3750545-502 IAW 51-1-24. INSTALLED LONGERON SPLICE IAW 51-1-2 0D,51-1-20D FILLET PANELS 1924 & 191CC IAW DC8 SRM 51-3-0

Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C-1, SEAT TRACK C/H STA 1120-1140 GOUGED, REMOVED GOUGES IAW DC8 SRM 53-2-0 & FOUND TO BE OUT OF LIMITS REMOVED FLOOR PANEL F90 & F94 FOR ACCESS. LOCATE NEW SEAT TRACK DRILLED EXISTING FASTENER HOLES ALODINE & PRIME IAW 51-1-8. LOCATE SEAT TRACK SPLICES & DRILLED FASTENERS HOLES IAW UPS EO 5320-8309. INSTALLED SEAT TRACK SPLICES & FLOOR BOARDS IAW 51-3-0 & UPS EO 5320-8309.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C-1, UPPER CARGO PIT BETWEEN STA 822 TO 837 FLOORBEAM AT STA 822 AT SEAT TRACK (E) IS CORRODED. CUT SEAT TRACK REPAIR FLOORBEAM INSTALLED NEW SEAT TRACK AND 4 EACH FITTING SPLICE.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C-1, LEFT HORIZONTAL STAB LEADING EDGE INBD OF CENTER 3 EACH POPPED RIVETS REMOVED & INSTALLED LT HORIZONTAL STAP L/E 331F TO FOM IAW DC8 SRM 51-3 -0. RMVD FASTENERS IAW DC8 SRM 51-1-21A. FOUND SKIN TO BE CRACKED. CUT OUT DAMAGE & FAB REPAIR DOUBLER IAW DC8 SRM 55-2-1 FIG 4. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR DOUBLER IAW DC8 SRM 51-1-2 1 & 51-1-21A.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C1, LONGERON FITTING IS CRACKED. REMOVED FITTING, RECEIVED, LOCATED, AND DRILLED FITTING, INSTALLED FIT TING; ALL IAW DC8 SRM 51-1-20D, 51-1-24.

Part: LONGERON — GOUGED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C1, LT MLG WW L34 BOTTOM SIDE GOUGED FWD STA 980. REMOVED ADF PANEL AND LONGERON IAW DC8 SRM 51-3-0 AND 51-1-20D. FABRIC ATED LONG -503 IAW DAC DWG 3750347. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED -503 LONGERON IAW DC8 SRM 51-1-20D. INSTALLED ADF PANEL IAW DC8 SRM 51-3-0.

Part: FITTING — CRACKED (LONGERON) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C-1, 680 LONGERON 11 LT LOWER AFT FITTING IS CRACKED, REMOVED CRACKED FITTING P/N 4751625-1 IAW DC8 SRM 51-3-0,51-1-20D & 51-1- 21 LOCATED AND DRILLED NEW FITTING IAW DAC DWG 4751625 AND DC8 SRM 51- 1-24 AND INSTALLED IAW DC8 SRM 51-1-20D, 51-1-21, & 51-3-0

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE:C-1 FWD LWR CARGO STA 300 TC 308 L33R TO L34R DOUBLER HAS CORROSION. REMOVED CORR IAW DC8 SRM 51-1-8. ORIG THICKNESS WAS .063 IAW DAC DWG 3754065. MATERIAL RMVD WAS .020 AND IS OUT OF LIMITS IAW DC8 SRM 53-2-0 FAB NEW DOUBLER FROM 7075-T6 .063 IAW DC8 51-1-24 & DAC DWG 3754065. ALODINED & PRIME DOUBLER IAW DC8 SRM 51-1-8. RMVD OLD & INSTALLED NEW D OUBLER IAW DC8 SRM 51-1-20D

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C1, FWD LWR CARGO STA 300 TO 308 L33R DOUBLER WITHIN TORQUE BOX CORRODED. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMITS IAW DC8 SRM 53-2-0 . FABRICATED NEW DOUBLER FROM 7075-T6 .063 IAW DC8 SRM 51-1-24 AND DAC DWG 3254065. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. REMOVED OLD DOUBLER AND INSTALLED NEW DOUBLER IAW DC8 SRM 51-1-20D.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C-1, ENGINEER SEAT TRACKS HAVE ELONGATED HOLES. REMOVED F/E SEAT TRACKS IAW DC8 SRM 51-3-0, LOCATED AND DRILLED FWD AND AFT TRACKS P/N 3657504-1 IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SR M 51-3-1

Part: FRAME — GOUGED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C-1, NLG RT CTR TUNNEL AREA (ACCESS THUR AFT PRESS PAL) FRAME & BRKT GOUGED JUST FWD OF PWR RECP BOX BLEND GOUGE IAW DC8 SRM 53-2-0, FIG 1F ORINGINAL THICKNESS .050 REMAIN ING MATERIAL OF .036 OUT OF LIMITS. ROUNDED GOUGE ON BRAKETT EDGE REPA IR ANGLES, 7075-0-03 PO 441313-2 MATERIAL ID FOR -35 FILLER .125 707 5T6 PO 424554-3 IAW DC8 TR 53-125 HEAT TREATED REPAIR ANGLES FAB AN GLES ALODINES & PRIMED & INSTALLED REPAIR ANGLES 51-1-8 & 51-1-20D

Part: SEAT TRACK — WORN (COCKPIT) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C-1, ENGINEERS SEAT TRACKS HAVE ELONGATED HOLES. REMOVED FWD F/E'S SEAT TRACK IAW DC8 SRM 51-3-0 LOCATED AND DRILLED SE AT TRACK IAW DC8 SRM 51-1-24 AND INSTALLED IAW DC8 SRM 51-3-1

Part: INTERCOSTAL — DENTED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C-1, STA 1240-1260 L35L INTERCOSTAL DENTED. REMOVED INTERCOSTAL IAW DC8 SRM 51-1-21 & 51-1-20D MATERIAL ID & FAB OF NEW PART IAW DAC DWG 49758507, HEAT TREATED PART REF LOAD HT041904 -3. ALODINE & PRIMED INTERCOSTAL IAW DC8 SRM 51-1-8. INSTALLED INTERCOSTAL IAW DC8 SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C-1, CORROSION AROUND NUTPLATES & FASTENER FROM STH 1480 TO 1540 AT CUSP LT SIDE OF AFT CARGO COMPT PUT A7763. REMOVED AIR GRILLS CUSP CLOSEOUT & FLOOR TO FOM REMOVED SEAT TRACK ORIG THICKNESS .090 IAW 51-2-0. REMOVED CORR IAW 51-1-8 AFTER BLEND .040 MATERIAL REMAINING OUT LIMITS IAW 53-2-3. LOCATED & DRILLED UP NEW SEAT TRACK FLOORBOARD CUSP CLOSEOUT & AIR GRILLS IAW DC8 SRM 51-3-0

Part: CHANNEL — CRACKED (T/E FLAP) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE:C-1 RIGHT WING I/B FLAP O/B TRAILING EDGE IS CRACKED. REMOVED CRACKED CHANNEL. FAB NEW CHANNEL IAW DC8 SRM 57-7-1. ALODINED AND PRIMED CHANNEL IAW DC8 SRM 51-1-8. INSTALLED CHANNEL IAW DC8 SRM 51-3-O,51-3-1,51-1-21 AND 51-1-21A

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C-1C, FWD PIT- FWD SIDE OF TORQUE BOX (APPROX STA 275) BETWEEN LONGERONS 33R -34 RT ZEE ANGLE CORRODED. REMOVED OLD FITTING PN 3755824-1 IAW DC8 SRM 51-1-20D. RECIVED NEW FITT ING PN 3755824-1 TAG 00702413 DRILLED UP FITTING IAW DC8 SRM 51-1- 24 INSTALLED FITTING IAW DC8 SRM 51-1-20D

Part: LONGERON — CORRODED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE:C-1 FWD PIT BETWEEN STA 200-300 LONGERON 34R CORRODED RMVD FASTENERS L34R FS 190-300 & FROM SHEARTIES & FRAMES AT FS 200& 220 AT L34R TO FOM. RMVD CORR FROM L34R AT FS 205-217. ORIG THICKNESS IS .092 MAT RMVD .030 MAT REMAINING.062 & IS OUT OF LIMITS. RMVD CORR FROM VER TICAL LEG L34R. ORIG THICNESS .063 MAT RMVD .027 MAT REMAINING .036 OU T OF LIMITS RMVD L STRAP SPLICED 2 EA HEAT TREATED INSTALLED.

Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C1, MAIN DECK FLOOR PANEL CORRODED STA 50 LBL 14. REMOVED CORROSION IAW DC8 SRM 51-1-8. OUT OF LIMITS. FABBED SPLICE PLATES IAW DC8 SRM 53-2-3; LOCATED, DRILLED, AND COUNTERSUNK NEW FLOOR PANEL SECTION IAW DC8 SRM 51-1-24. ALOD & PRIMED IAW DC8 SRM 51-1-8. INSTALLED ROLLER TRAY FITTING IAW DC8 SRM 51-1-21A, INSTALLED FLOOR PANEL SECTION AND CEILING PANELS IN LOWER PIT A IAW DC8 SRM 51-3-0 & 51-3-1.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C1, AFT PIT RT CUSP EXTRUSION CORRODED BETWEEN STA 1000 AND 1020 LONG 21 RT. REMOVED DAMAGED CUSP SECTION IAW TR53-179 STA 990-1030 L21 RT. IAW DC8 SRM 51-1-20D. REC'ED, LOCATED AND DRILLED -3 & -5 REPAIR ANGLES, -7 D OUBLER AND -9 CUSP SECTION IAW DC8 SRM 51-1-24. FAB IAW TR 53-179 & RE PAIR DWG 2060296. ALODINED & PRIMED IAW DC8 SRM 51-1-8. AND INSTALLED -3,-5,-7, &-9 REPAIR MEMBERS IAW TR53-179 AND REPAIR DWG 3060296

Part: SEAT TRACK — BROKEN (FUSLEAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C-1, SEAT TRACK STA 1700 LOBES BROKEN OFF. SEAT TRACK FOUND OUT OF LIMITS IAW DC8 SRM & UPS EO 5340-12053. REMOVED SEAT TRACK IAW 51-1-200 & 51-30 MAT ID SEAT TRACK P/N 3772660 IAW 53-7-1 LACATED & DRILLED HOLE IN SEAT TRACK F STA 1670-1710 IAW 51-1-24. ALODINE & PRIME IAW 51-1-8. INSTALLED SEAT TRACK IAW DC8 SRM 51-3-0

Part: ANGLE — GOUGED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C1, STA 1560-1580 L21L CUSP MEMBRANE GOUGED. REMOVED GOUGE ON CUSP TONGUE IAW DC8 SRM 53-2-0. OUT OF LIMITS. FABRICATED CUSP IAW DAD DWG 9750448. FABRICATED SPLICES IAW REO G09789. ALODINED & PRIMED IAW DC8 SRM 51-1-8. INSTALLED NEW CUSP SECTION AND SPLICE ANGLES IAW DC8 SRM 51-1-20D INSTALLED FITTING IAW DC8 SRM 51-1-20D. INSTALLED DUCT IAW DC8 MM 20-11-00 & 36-11-01.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,820 hrs · 26,005 cycles

INSPECTION TYPE: C1, MAIN CABIN, FRAME FITTING CRACKED ON BOTH SIDES FS 427 L11L (DOT 6603). REMOVED TEE FITTING TO GAIN ACCESS TO CRACKED FITTING, REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. LOCATED & DRILLED NEW FITTING P/N 3755820- 1 IAW DC8 SRM 51-1-24 & DAC DWG 3755820 ALODINED & PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED FITTING IAW DC8 SRM 51-1-20D.

Part: ANGLE — CORRODED (COCKPIT)

WINDOW FRAME ZEE CHANNEL LT LWR CORNER PITTED AND CORRODED. REMOVED AND INSTALLED NEW ZEE ANGLE IAW UPS EO DC8-5330-19614-A. FERRY TO GSO FOR REPAIR REFERENCE GSO NRC 632693

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY LIGHTING SWITCH LEFT IN ARMED POS. BATTERY PACK DEAD. REMOVED AND REPLACED EMERGENCY LIGHTING BATTERY PACK. NOW OPS OK.

Part: HINGE PIN — OUT OF ADJUST (COCKPIT WINDOW)

INSPECTION TYPE: PFLT, F/O'S COCKPIT WINDOW WILL NOT OPEN PROPERLY. *SUPPLEMENTAL MRR* T/S TO AFT WINDOW HINGE PIN OUT OF PLACE. REINSTALLED AFT HINGE PIN. PERFORMED ADJ, TEST ALL CKS GOOD.

Part: SWITCH — INOPERATIVE (MLG DOOR)

DOORS NOT LATCHED LIGHT ILLUMINATED REMAINED ON AFTER GEAR RETRACTION (LEFT GEAR DOOR). RECYCLED GEAR, BROUGHT FLAPS TO 10 DEG, LIGHT EXTINGUISHED. BROUGHT FLAPS UP, RESUMED NORMAL FLIGHT. CHECKS OK ON GROUND. REMOVED AND REPLACED LEFT ALT GEAR DOOR SWITCH. PRECAUTIONARY INSP GEAR AND DOOR UPLATCHES. COULD NOT DUPLICATE SWITCH WAS CHANGED PRECAUTIONARY.

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS INOP WHEN SWITCH PLACED IN ARM POS AND BAT/EXT POWER SWITCH IN BAT FAILS TEST REF PS CHK. REPLACED EMERGENCY LIGHTING BATTERY AND RELAY UNIT, OPS CHK GOOD REF 33-50-02.

Part: MOUNT — BROKEN (NLG)

INSPECTION TYPE:N/A ATB - NLG RETRACT CYLINDER AFT MOUNT ASSY BROKE CAUSING DAMAGE TO FUSELAGE SKIN. A/C FERRIED TO TCO FOR REPAIR 9150. TRIMMED DAMAGE ON BULKHEAD IAW REO G08732 STEP NR 1, DYE PENETRATE INSP IAW MIL-271F, NO CRACK NOTED IN CUTOUT. FABBED, DRILLED FASTENER HOLES IN DOUBLER, TRIPLER & FILLERS IAW REO G08732. OK TO ALODINE. FABBED NEW LOWER STIFFENER IAW DWG 5615530. INSTALLED UPPER & LOWER STIFFENERS FINGER DOUBLER & TRIPLER IAW DC8 SRM 51-1-21 & REOG08732.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 66,099 hrs · 25,438 cycles

INSPECTION TYPE:LNSV NLG BULKHEAD DAMAGED. TRIMMED OUT DAMAGE ON BULKHEAD IAW REO G08732. DYE PENETRANT CHECKED FOR CRACKS, NONE NOTED. FABRICATED NEW STIFFENER, FILLERS, TRIPLER, AND FINGER DOUBLER PER DAC DWG 5615530 & REO G08732. INSTALLED IAW REO G08732, DC8 SRM 51-1-21, & 51-1-20D.

Part: DOUBLER — CRACKED (LT WING) · airframe 65,884 hrs · 25,282 cycles

INSPECTION TYPE:C23 MOULD-LINE DOUBLER AT NR 1 PYLON HAS PREVIOUSLY INSTALLED REPAIR DOUBLER ON THE I/B SIDE THATS CRACKED AT FASTENER HOLE. REMOVED DOUBLER, PERFORMED HFEC AND BOLT HAVE HFEC IAW NDT SPM 06-10.001 AND 06-10.003. CRACKS PRESENT IN 5 EA HOLES, FABBED REPAIR BUSHINGS IAW REO G08542. INSTALLED BUSHINGS IAW REO G08542 & DC8 SRM 51-1-25. FABBED WASHER, INSTALLED RIVET THROUGH BUSHING & WASHER IAW REO G08542 & SRM 51-1-21. PERFORMED HFEC, NO CRACKS NOTED.

Part: WEB — CRACKED (FLAP) · airframe 65,884 hrs · 25,282 cycles

INSPECTION TYPE:C23 RG I/B FLAP CLOSEOUT WEB CRACKED AROUND BEADED AREA. REMOVED AND REPLACED IAW REO G08529.

Part: WEB — CRACKED (T/E FLAP) · airframe 65,884 hrs · 25,282 cycles

INSPECTION TYPE:C23 LT WING I/B FLAP I/B END CLOSEOUT WEB IS CRACKED AND HAS LOOSE FASTENERS. REMOVED AND REPLACED WEB IAW REO G08529.

Part: FITTING — CORRODED (FUSELAGE) · airframe 65,884 hrs · 25,282 cycles

INSPECTION TYPE:C23 AFT PIT FS 1200 ZEE FITTING AT L34R - L33R IS CORRODED. REMOVED CORRODED ANGLE LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED ZEE FITTING REPAIR ANGLE IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,884 hrs · 25,282 cycles

INSPECTION TYPE:C23 AFT PIT BILGE Z-FITTING CRACKED I/B OF L34R AT STA 1200. INSTALLED NEW FITTING AND SPLICES IAW DC8 SRM 53-2-0.

Part: SKIN PANEL — CRACKED (HORIZ STAB) · airframe 65,884 hrs · 25,282 cycles

INSPECTION TYPE:C23 LT HORIZONTAL STAB UPPER O/B FWD SKIN PANEL CRACKED AT 2ND BOLT IN AFT DIRECTION. REMOVED AND REPLACED HORIZ STAB PLANK IAW DAC SB55-16 AND DAC DWG SRO 8 550001.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,884 hrs · 25,282 cycles

INSPECTION TYPE:C23 L2 DOOR CORNER UPPER AFT SHOWS CRACK INDICATION IN REPAIR AREA GOING TO FASTENER HOLE. REMOVED EXISTING DOUBLERS, ROUTED OUT CRACK, FABBED AND INSTALLED REPAIR DOUBLERS IAW DC8 SRM 53-2-0 FIG 18.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,884 hrs · 25,282 cycles

INSPECTION TYPE:C23 AFT PIT BILGE Z-FITTING CRACKED O/B OF L35R STA 1180. REMOVED CRACKED FITTING, FABBED SPLICES FOR FITTING REPAIR AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, 53-2-0 NOTE 17.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,884 hrs · 25,282 cycles

INSPECTION TYPE:C23 AFT PIT BILGE Z-FITTING CRACKED O/B OF L34R AT STA 1180. REMOVED CRACK Z-FITTING, LOCATED AND DRILLED NEW FITTING AND SPLICES IAW DC8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC8 SRM 53-2-0 AND 51-120D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 65,884 hrs · 25,282 cycles

INSPECTION TYPE:C23 AFT PIT BILGE Z-FITTING CRACKED O/B AT L28L STA 1180. REMOVED CRACKED Z-FITTING. INSTALLED FITTING AND SPLICES IAW DC8 SRM 53-2-0.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 65,884 hrs · 25,282 cycles

INSPECTION TYPE:C23 AFT PIT LT TUNNEL CORR ON BOTTOM OF CABIN FLOORBEAM UPPER FWD FLANGE AT STA 1240 LBL 62. REMOVED CORROSION IAW DC8 SRM 51-1-8, OUT OF LIMITS IAW DC8 SRM 53-2-0. FABBED AND INSTALLED IAW DC8 SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 65,884 hrs · 25,282 cycles

INSPECTION TYPE:C23 L1 DOOR CORNER UPPER FWD DOUBLER CONDUCTIVITY TEST SHOWS NOT TO BE ALUMINUM. REMOVED EXISTING DOUBLER, ROUTED OUT DAMAGED AREA, FABRICATED AND INSTALLED DOUBLERS IAW DC8 SRM 53-2-0 FIG 15.

Part: CYLINDER — LACK OF LUBE (T/E FLAP)

INSPECTION TYPE:N/A AIRCRAFT TURNS HARD LEFT DURING TAXI AND T/O. WHEN FLAPS ARE LOWERED ACFT BANKS LEFT 10 DEGREES. VISUALLY INSPECTED FLAP MECHANISM, NO DEFECTS NOTED T/S PER MM 27-50-00. FOUND OUTBOARD LOCK CYLINDER LOW, SERVICED AND BLED PER MM 27-51-10. FLAPS OPS CKD OK.

Part: AILERON — LACK OF LUBE (WINGS)

AILERONS STIFF. INSPECTED AILERON CONTROL SYSTEM AND FOUND AILERONS IN NEED OF LUBE. LUBRICATED AILERONS IAW 27-10-06 AND PERFORMED AILERON SYS ADJ/TEST IA W MM 27-10-00. AILERONS CHECKED NORMAL OK FOR SERVICE

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK PER MM 33-50-00, CKS NORMAL.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:P/F, EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS DO NOT TEST. REMOVED AND REPLACED BATTERY PACK PER MM 33-50-02.

Part: UNKNOWN — ODOR (COCKPIT)

INSPECTION TYPE:N/A, COCKPIT ODOR - MX VERIFIED WHAT APPEARED TO BE AN ELECTRICAL PROBLEM ODOR. COULD NOT ISOLATE SOURCE.

Part: TRANSFORMER — OVERHEATED (COCKPIT)

INSPECTION TYPE:N/A, SMOKE IN COCKPIT. DIVERTED INTO KJAX. DECLARED EMERGENCY, OVER-WEIGHT LANDING. *S/D* REFERENCE UPS00833396, PERFORMED OVERWEIGHT/HARD LANDING INSPECTION. REMOVED AND REPLACED TRANSFORMER BALLAST FOR SUSPECTED OVERHEATING. REMOVED AND REPLACED BOTH WATER SEPARATOR BAGS TO REMOVED RESIDUE ODOR, RAN ALL ENGINES AND PACKS, INSPECTED CABIN AND ENTRY WAY ELECTRICAL PANELS, CHECK LIGHTING, INSTRUMENTS AND SYSTEM FOR FAILURES. CHECKS TURN UP NO FURTHER PROBLEMS.

Part: BATTERY PACK — INOPERATIVE (CABIN)

EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECK NORMAL.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, STA. 1767 AT LONGERON 18 RT, THE LONGERON END FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 47723397AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, STA. 1160 AT STR. 19 RT, INTERCOSTAL ATTACH FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING I.A.W . DWG.4750419 AND SRM 51-1-20D.

Part: PANEL — CORRODED (KEELBEAM) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, LOWER RT KEEL STRESS PANEL HAS LARGE AREA OF CORROSION. REMOVED, FABRICATED AND REPLACED PANEL I.A.W. DWG.5754992 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, STA. 1300 - 1310 AT STR. 13 LT, TORQUE BOX FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING I.A.W.DWG.5755936 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, LONGERON TO FRAME ATTACH FITTING IS CRACKED AT STA. 1160 STR. 19 LT. REMOVED, FABRICATED AND REPLACED FITTING I.A.W. DWG.4750418 AND SRM 511--20D.

Part: FINGER DOUBLER — CORRODED (BS 120)

INSPECTION TYPE:C1 STA 120 AT STR 31R, THE FINGER DOUBLER IS CORRODED OUT OF LIMITS. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5779934 AND SRM 51-1-20D.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE:C1 RT L/E UPPER RIBS ARE CRACKED AT THE FOLLOWING LOCATIONS, XFS797.5, XFS766.25, XFS753.75 AND XFS785.0. STOP DRILLED CRACKS AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE:C1 RT WING L/E UPPER RIB IS CRACKED AT STA XFS828.75. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, RT WING LE UPPER RIB IS CRACKED AT STA. XS240.126. STOP DRILLED CRACK AND REPAIRED I.A.W. SRM 57-2-0 FIG.2.

Part: FITTING — CRACKED (BS 1040 - 1060)

INSPECTION TYPE:C1 STA 1040-1060, STR 36 SPLICE FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3750299 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 410 - 416)

INSPECTION TYPE:C1, LT WING L/E UPPER RIBS ARE CRACKED AT STA XFS 410.25 AND XFS 416.5. STOP DRILLED CRACKS AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE:C1 RT WING L/E LOWER RIB IS CRACKED AT STA XFS635.0. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: DOUBLER — CRACKED (WS 297)

INSPECTION TYPE:C1, LEFT WING INTERNAL DOUBLER IS CRACKED AT STA XFS 297.5. REMOVED, FABRICATED AND REPLACED DOUBLER IAW DWG 5769589 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 781)

INSPECTION TYPE:C1 STA 781 LONGERON 13R END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779970, AND SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1340 - 1360)

INSPECTION TYPE:C1 STA 1340-1360 LONGERON 29L SPLICE FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW DWG 4646163 AND SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C 1 STA. 450 RBL. 48 SEAT TRACK HAS EXFOLIATION CORROSION. REPAIRED I.A.W. SRM.53-2-3 FIG. 14

Part: PANEL — CORRODED (NOSE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, RT NOSE TUNNEL AT STA. 80 RBL45, CEILING PRESSURE PANEL HAS MODERATE CORROSION. REPAIRED AREA I.A.W DWG. SR0530026.

Part: FITTING — CRACKED (BS 902)

INSPECTION TYPE:C1 STA 902 AT STR 8L, THE LONGERON END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779659 AND SRM M51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE:C1 STA. 1160 AT STR. 20 - 19 RT, LONGERON TO FRAME ATTACH FITTINGS ARE CRACKED, (2 TOTAL). REMOVED, FABRICATED AND REPLACED FITTINGS I.A.W. DWG.4750418.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, STA. 444 AT RBL 60, SEAT TRACK HAS HEAVY CORROSION. REPAIRED AREA BY SPLICING SECTION OF TRACK I.A.W. EO DC8-5320-5167-C

Part: FITTING — CRACKED (BS 1180)

INSPECTION TYPE:C1 LONGERON TO FRAME FITTING IS CRACKED AT STA 1180, STR 20R. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, STA. 510 AT RBL 60, SEAT TRACK HAS HEAVY CORROSION. REPAIRED AREA I.A.W. SRM 53--2-3.

Part: FITTING — CRACKED (BS 902)

INSPECTION TYPE:C1, LONGERON 6L END FITTING IS CRACKED AT STA 902. REMOVED AND REPLACED FITTING IAW DWG 3779657 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, STA. 1040 - 1060 STR. 35 LT SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG.3750454 ANS SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1170)

INSPECTION TYPE:C1 FRAME TO CUSP TIE FITTING AT STA 1170 STR 21R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754918 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1160)

INSPECTION TYPE:C1 INTERCOSTAL END FITTING AT STA 1160 AND LONGERON 17R IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4750419 AND SRM 51-1-20D.

Part: SEAT TRACK — CORRODED (BS 815)

INSPECTION TYPE:C1 STA 815 AT RBL 60, THE SEAT HAS MODERATE CORROSION. REPAIRED AREA IAW SRM 53-2-3 FIG 6D.

Part: FITTING — CORRODED (BS 1210)

INSPECTION TYPE:C1 STA 1210 AFT SIDE FITTING HAS MODERATE CORROSION AT 33R. REMOVED AND REPLACED FITTING IAW DWG 5894282, AND SRM 51-1-20D.

Part: FITTING — CRACKED (S 822)

INSPECTION TYPE:C1 INTERCOSTAL END FITTING AT STA 822 LONG 13R IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4751643 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C 1 STA. 1040 - 1060 LONGERON 31 LT SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3750257,AND SRM. 51-1-20D

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, STA. 683 PRESSURE BULKHEAD (CENTERWING) HAS 3 CRACKS PROTRUDING UNDER VERTICAL STIFFNERS AT LBL 12 & 17. REPAIRED AREA I.A.W. SRM 53-2-5 FIG.13.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, STA. 80 BETWEEN STR. 8 - 12 RT, FRAME IS DAMAGED. REPAIRED FRAME I.A.W. DWG. DC8-53A -010.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, FUSELAGE SKIN IS CRACKED AT ST. 160 STR. 11 RT (FWD SERVICE DOOR). REPAIRED AREA I.A.W. SRM 53-2-0 FIG.14.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE:C1 FUSELAGE SKIN IS CRACKED AT STA. 200 STR. 21 RT. REPAIRED AREA I.A.W. SRM 53-2-0 FIG.14.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C 1 STA. 380 - 400 LONGERON 31 LT SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG. 3754473,AND SRM. 51-1-20D

Part: FITTING — CRACKED (BS 1260 - 1280)

INSPECTION TYPE:C1 STA 1260-1280, STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3754473 AND SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (PAX DOOR)

INSPECTION TYPE:C1, INTERCOSTAL ON FWD ENTRY DOOR AT FWD UPPER FWD CORNER IS CRACKED STA 25 LONGERON 6L. REPAIRED IAW SRM 52-2-0 FIG 2.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, STA. 1830 AT STR 2 RT, REPAIR DOUBLER HAS A SMALL CRACK. REMOVED, FABRICATED AND REPLACED DOUBLER I.A.W. DWG.5651927 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 717)

INSPECTION TYPE:C1 INTERCOSTAL FITTING IS CRACKED AT STA 717, STR 18R. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4751640 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 760)

INSPECTION TYPE:C1, INTERCOSTAL FITTING IS CRACKED AT STA 760 LONGERON 18L. REMOVED AND REPLACED FITTING IAW DWG 4751643 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 781)

INSPECTION TYPE:C1 INTERCOSTAL FITTING AT STA 781, STR 13R IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3779874 AND SRM 51-1-20D.

Part: RIB — CRACKED (LT WING)

INSPECTION TYPE:C1 LEFT WING L/E UPPER RIB AT STA XFS366.5 IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-02-0 FIG 2.

Part: FITTING — CORRODED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, STA. 980 AT LONGERON 24 LT STIFFNER FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING I.A.W. DWG.2647420 AND SRM 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, RT WING LE AT STA. XS250.089, THE UPPER LE RIB HAS A 10 INCH CRACK. REPAIRED AREA I.A.W. SRM 57-2-0 FIG.2.

Part: FITTING — CRACKED (BS 740)

INSPECTION TYPE:C1, INTERCOSTAL FITTING IS CRACKED AT STA 740, LONG 13L. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 4751643 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE:C1 STA 857 LONGERON 19R INTERCOSTAL FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779498, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, STA. 1220 AT STR. 33 RT, SHEAR TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING I.A.W. DWG.3755847 AND SRM 51-1-20D.

Part: SKIN — CRACKED (LE FLAP)

INSPECTION TYPE:C1, LEFT CENTER L/E UPPER SKIN IS CRACKED AT XFS 304. REPAIRED IAW SRM 57-2-1 FIG 38.

Part: FRAME — CRACKED (BS 1766)

INSPECTION TYPE:C1, STA 1766 LBL 23 VERTICLE FRAME IS CRACKED LOWER OUTBOARD END. REPAIRED IAW SRM 53-2-0 FIG 1B.

Part: RIB — CRACKED (LE FLAP)

INSPECTION TYPE:C1, RIGHT WING L/E RIB IS CRACKED AT XFS 341.500. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (RT WING) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, RT WING LE AT STA. XFS397.750, LOWER LE RIB IS CRACKED AT MID SPAN. REPAIRED AREA I.A.W. SRM 57-2-0 FIG.2.

Part: FITTING — CRACKED (CABIN) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, STATION 840 AT LONGERON 18 RT, INTERCOSTAL FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING I.A.W. DWG.3779874 AND SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, FLOORBEAM ATTACH FITTING IS CRACKED AT STA. 160, LBL 60, STR. 21 LT. REMOVED, FABRICATED AND RTEPLACED FITTING I.A.W. DWG.3772916 AND SRM 51-1-20D.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, STA. 400 LONGERON 21 LT, HAS HEAVY INTERGRANULAR CORROSION. REPAIRED I.A.W. SRM.53-2-5 FIG. 15

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE:C,1 RT WING LWR SKIN ABOVE NR 4 PYLON CUT-OUT HAS REPAIR DOUBLER CRACKED, STA XW485.0. REPAIRED AREA IAW SRM 57-2-1A FIG 2.

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE:C1, RT WING UPPER SKIN AT STA XRS172.00 AND FRONT SPAR IS CRACKED. REPAIRED AREA IAW SRM 57-2-1 FIG 39.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE:C1, RT WING L/E LWR RIB FWD OF ACCESS PANEL OPENING IS CRACKED AT STA XFS810.0. REMOVED, FABRICATED AND REPLACED RIB IAW DWG 5769471 AND SRM 51-1 -20D.

Part: RIB — CRACKED (RT WING) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C 1 RT WING LE. UPPER RIB IS CRACKED AT XOLDI 6.225. REPAIRED I.A.W. SRM. 57-2-0 FIG. 2

Part: ACCESS DOOR — CRACKED (RT WING) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, RT INBOARD SLOT, UPPER DOOR IS CRACKED. REMOVED AND REPLACED DOOR I.A.W. MM 27-80-00,OP''S CHECH WAS GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, STA. 55 AT STR. 24 LT, FRAME IS CRACKED. REPAIRED AREA I.A.W. SRM 53-2-0 FIG.2.

Part: SKIN — CRACKED (RT WING)

INSPECTION TYPE:C1, RT WING L/E LWR SKIN IS CRACKED ATB THE DRAIN HOLE STA XFS591.250. REPAIRED AREA IAW SRM 57-2-0 FIG 2A.

Part: SPAR — CORRODED (RT WING) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C 1 RT WING LE. AUX TANK UPPER SPAR HAS HEAVY CORROSION BETWEEN XFS 88.75 AND XFS 167.5 REMOVED AND REPLACED SPAR CAP I.A.W. DWG.5766433 AND SRM. 51-1-20D, 51-1-21

Part: DOUBLER — CORRODED (RT WING) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, RT WING LE AT STA. XFS810.0, THE INTERNAL DOUBLER HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED DOUBLER I.A.W. DWG3641257,

Part: SKIN — CORRODED (RT WING) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C 1 RT WING LE. UPPER SKIN HAS HEAVY CORROSION UNDER THE SURFACE BETWEEN XFS 583 TO XFS 686 ** REPAIRED I.A.W. 8110-3.

Part: RIB — CRACKED (LE FLAP)

INSPECTION TYPE:C1, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS. 653.750. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,540 hrs · 24,344 cycles

INSPECTION TYPE: C1, FUSELAGE SKIN AT STA. 1440 AT STR 28 RT IS CRACKED. REPAIRED AREA I.A.W SRM 53-2-0.

Part: SKIN — CRACKED (BS 295)

INSPECTION TYPE:C1 STA 295 AT LONGERON 28L SKIN IS CRACKED AT SECOND AIR START DOOR UPPER AFT CORNER. REPAIRED IAW SR 08530020, EO DC8-5330-0703I, AND SRM 53-2-0 FIG 1B.

Part: HYD LINE — LEAKING (BRAKE SYS)

INSPECTION TYPE:N/A, ATB-DISCOVERED HYD QTY LOSS. DECREASED TO AUX WITH ENGINE HYD PUMPS IN BYPASS. AFTER LANDING MX FOUND STAB TRIM HYDRAULIC MOTOR BRAKE RETURN LINE LEAKING. *S/D* INSTALLED INTERIM REPAIR (FLEX LINE) AT THE STAB TRIM HYD BRAKE PER GMM 3-24-1, LEAKS AND OPS CHECK GOOD. TRANSFERRED TO D178926.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW MM 33-50-01 CHKS GOOD.

Part: DOUBLER — CORRODED (BS 920-940)

INSPECTION TYPE-C, FINGER DOUBLER BULGING AND POPPED FASTENER AT RBL 65 AT FS 920 TO 940. REMOVED, FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 57-7-1 FIG 10, 51-1-9, 51-1-20D AND 51-1-21.

Part: DOUBLER — CORRODED (BS 940-960)

INSPECTION TYPE-C, FINGER DOUBLER BLOWN OUT AT RBL 65 AT FS 940 TO 960. REMOVED, FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 53-7-1 FIG 10, 51-1-9, 51-1-20D AND 51-1-21.

Part: LONGERON — CORRODED (BS 1740)

INSPECTION TYPE-C, LONG 34L AT FS 1745 IS CORRODED OUT OF LIMITS. REMOVED, FABRICATED AND REPLACED LONG 34L FROM FS 1720 TO 1766 IAW SRM 53-5-1 FIG 7, 51-1-20D AND 51-1-21.

Part: FITTING — CORRODED (BS 270)

INSPECTION TYPE-C, NR 1 PIT AT STR 32L STA 270, DOOR OPEN STOP/FRAME FITTING HAS HEAVY CORROSION. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERG EXIT LIGHTS ILLUMINATED AT ALL TIMES REGARDLESS OF CONTROL POSITION. REMOVED AND REPLACED EMER BATT PACK. OPS CHECK NORMAL (P/N ON 5708458-503 S/N FTL 010 ), (P/N OFF 60-1223-5 S/N 337).

Part: PACK — FUMES (COCKPIT)

INSPECTION TYPE-N/A, REF LOG PAGE NR 985883 STRONG SMELL OF JET FUEL IN COCKPIT AS SOON AS EITHER PACK IS TURNED ON OR GETS WORSE WITH RECIRC FAN ON. VISUALLY INSPECTED BELLY FOR EVIDENCE OF FUEL, NONE FOUND. REMOVED AND REPLACED L AND R COALESCER BAGS, L AND R PACKS GRD RUN OPS AND LK CK'S OK.

Part: AIR DISTRBUTION — ODOR (COCKPIT)

INSPECTION TYPE-N/A, STRONG ODOR OF JET FUEL IN FLIGHT STATION THE ENTIRE FLIGHT. COULD NOT LOCATE EXACT SOURCE OF ODOR. VENTILATED COCKPIT FOR 12 HRS, SMELLS GOOD.

Part: LIGHT — INOPERATIVE (CABIN)

EMERGENCY LIGHTS INOP. REMOVED AND REPLACED EMERGENCY LIGHT PACK ASSY SYS CKS GOOD PER M/M 33-50-00 OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHT DEAD ON PREFLIGHT. REPLACED EMERGENCY LIGHT BATTERY PACK.

Part: RETRACT MECH — OUT OF ADJUST (NLG)

INSPECTION TYPE-N/A ON TAKEOFF CALLED FOR GEAR UP HANDLE WOULD NOT MOVE AT SAME TIME MAIN GEAR SPOILER INOP CAME ON, COMPLETED MAIN SPOILER INOP CHKLST LIGHT WENT OUT, ELECTED NOT TO RAISE GEAR. DUE TO NOISE PREVIOUSLY NOTED. *S/D* PERFORMED ADJ AND TEST OF LANDING GEAR MECHANICAL CONTROL SYS PER MM 32-31-00, FOUND PUSH RODS ON NOSE GEAR CONTROL U/U OUT OF ADJ PUSH RODS AND OPS CHK SYS, CHKS GOOD. ALSO, PERFORMED VISUAL INSP FOUND NO DEFECTS IN NLG AREA. PERFORMED GEAR SWING ALL SYS CHK GOOD 32-31-00.

Part: DOOR FITTING — CRACKED (BS 1152)

INSPECTION TYPE-C, C-3 CARGO DOOR JAMB BACK UP FITTING CRACKED AT BS 1152 LONGERON 33R. REMOVED AND REPLACED FITTING IAW SRM 51-3-0.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE: D. INTERCOSTAL END FITTING CRACKED AND CORRODED AT AFT SIDE OF STA 1140 LONGERON 33R. REMOVED AND REPLACED FITTING PER SRM 51-1-20.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE: D. INTERCOSTAL END FITTING CRACKED, AFT SIDE OF BS 1140 AT LONGERON 35R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DAC DWG 37 58497 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE: D. INTERCOSTAL END FITTING CRACKED, AFT SIDE OF BS 1140 AT LONGERON 35L. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DAC DWG 3758497 AND SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1240-1268)

INSPECTION TYPE-D, FS 1240 TO 1268 LONGERON 36 CORRODED BEYOND LIMITS. REPAIRED PER DHC SK-748-297, REF UPS ENRG FILE NR DC8-53-1754.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE-D, STA 1690 STR 34L, END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-29D AND 53-1-0 AND 51-1-21.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE-D, STA 1140 STR 33R, END FITTING IS CRACKED. REMOVED AND REPLACED END FITTING IAW DWG 4758514 AND SRM 51-1-20.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE-D, STA 1140 STR 35L, END FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE-D, STA 1140 STR 35R, END FITTING IS CRACKED. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20.

Part: FRAME — CORRODED (BS 1140)

INSPECTION TYPE-C, FRAME BS 1140 CORRODED BETWEEN LONGERONS 32R AND33L. REPAIRED IAW DHC SK-748-706, REF ENRG FILE NR DC8-53-1756.

Part: SPAR CAP — CORRODED (BS 858)

INSPECTION TYPE-D, CENTER TANK UPPER REAR SPAR CAP SEVERELY CORRODED AND CRACKED AT BS 858 RBL 12-24. REMOVED DAMAGED SECTION AND SPLICED IN NEW SECTION IAW SRM 53-2-5 FIG16.

Part: ANGLE — CRACKED (LT WINDSHIELD)

INSPECTION TYPE-D, CRACK IN ANGLE FWD OF CAPTAIN WINDSHEILD LOWER I/B END. STOP DRILLED CRACK, FABRICATED REPAIR ANGLES AND INSTALLED IAW SRM 53-2-0, 51-1-21, 51-1-8, 51-1-11 AND SRM 51-1-29D.

Part: LONGERON — CORRODED (BS 1680-1740)

INSPECTION TYPE:D, LONGERON 36 FROM FS 1680 TO 1740, HAS EXFOLIATED CORROSION. FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-3.

Part: INTERCOSTAL — CORROSION (BS 1715-1725)

INSPECTION TYPE-D, INTERCOSTAL O/B OF STR 30 AT STA 1715-1725 DEFORMED FROM PREVIOUS DAMAGE AND EXFOLIATION. REMOVED INTERCOSTAL, FABRICATED AND INSTALLED REPLACEMENT PER DWG 5649329 AND SRM 51-1-20D.

Part: TEE CHORD — CORRODED (AFT FUSELAGE)

INSPECTION TYPE-D, TEE CHORD AFT OF TAIL SKID FITTING, LONGERON 36 CORRODED. REMOVED, FABRICATED REPLACEMENT TEE CHORD, AND INSTALLED IAW SRM 53-05-1 FIG 3 SHEET 4, SRM 51-1-9, AND 51-1-20D.

Part: DOUBLER — CORRODED (BS 1680-1740)

INSPECTION TYPE:D, FINGER DOUBLER AT STR 28L FS 1680-1740 HAS EXFOLIATED CORROSION. FABRICATED AND INSTALLED FINGER DOUBLER IAW SRM 51-1-21.

Part: DOUBLER — CORRODED (BS 1350-1460)

INSPECTION TYPE:D, STR 31L AT 1350-1460, FINGER DOUBLER IS OUT OF LIMITS AFTER CORROSION REMOVAL. FABRICATED AND INSTALLED REPLACEMENT FINGER DOUBLER IAW SRM 51-1-21, 53-4-1 FIG 17A.

Part: FITTING — CORRODED (BS 1691)

INSPECTION TYPE-D, STA 1691 STR 30R FITTING IS CORRODED AND CRACKED. REMOVED AND REPLACED FITTING PER SRM 51-1-21.

Part: PRESURE WEB — CORRODED (BS 12)

INSPECTION TYPE: D. N/L/G PRESSURE WEB CRACKED AND CORRODED AT LBL 18, STA -12. REPAIRED IAW DHC SK-748-341 REF. UPS ENRG. FILE NR DC8-53-1758.

Part: ANGLE — CORRODED (BS 902)

INSPECTION TYPE: D. CENTER WING UPPER SURFACE DOUBLER AT STA 902 UNDER CUSP ANGLE HAS LIGHT SURFACE CORROSION. FABRICATED REPLACEMENT CUSP ANGLE PER SRM 53-1-0, INSTALLED ANGLE PER SRM 51-1-21D.

Part: SHEAR TIE — CRACKED (BS 1620)

INSPECTION TYPE:D, SHEAR TIE FORMER CRACKED AT FS 1620, BETWEEN LONGERONS 30R AND 31R. INSTALLED REPAIR ANGLE TO SHEAR TIE FORMER PER SRM 53-2-0 FIG 2B.

Part: DOUBLER — CORRODED (BS 1650-1670)

INSPECTION TYPE-D, FUSELAGE SKIN INTERNAL DOUBLER STA 1650 TO 1670 BETWEEN L-31R AND L-33R IS CORRODED BEYOND LIMITS. REMOVED DOUBLER, FABRICATED REPLACEMENT DOUBLER AND INSTALLED PER SRM 53-4-1 FIG 17A AND 51-1-21.

Part: INTERCOSTAL — CORRODED (BS 1660-1680)

INSPECTION TYPE-D, INTERCOSTAL CORRODED FROM STA 1660 TO 1680, BETWEEN LONGERON 28L AND 29L. REMOVED, FABRICATED REPLACEMENT, AND INSTALLED PER SRM 51-1-20D AND 53-4-1 FIG 44.

Part: FITTING — CRACKED (BS 940)

INSPECTION TYPE-D, FLOORBEAM TIE FITTING LT SIDE AT STA 940 CUSP ANGLE IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DHC SK-748 -299 REF UPS ENRG FILE NR DC8-53-1753 AND SRM 51-1-20.

Part: DOUBLER — CORRODED (BS 1636-1680)

INSPECTION TYPE: D. FUSELAGE SKIN INTERNAL DOUBLER CORRODED FS 1636-1680 STR 21R TO 32R. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 51-1-21 AND 51-1-8.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE-D, STA 70 STR 33R END FITTING IS CORRODED AND CRACKED. REMOVED AND REPLACED END FITTING IAW SRM 51-1-29D AND 51-1-21.

Part: SKIN — CORRODED (BS 1680-1890)

INSPECTION TYPE: D. AFT FUSELAGE BELLY SKIN STA 1680-1890 BETWEEN STR 28L AND 28R HAS SEVERAL AREAS OF CORROSION BEYOND LIMITS. REMOVED AND REPLACED SKIN IAW DWG 5649329 AND SRM 51-1-21.

Part: DOUBLER — CORRODED (BS 1650-1670)

INSPECTION TYPE-D, FUSELAGE SKIN INTERNAL DOUBLER FS 1650 TO 1670, AT LONGERON 31L TO 33L IS CORRODED BEYOND LIMITS. FABRICATED REPLACEMENT DOUBLER AND INSTALLED IAW SRM 53-4-1 FIG 17A AND DWG 5615377.

Part: FRAME — CRACKED (BS 99)

INSPECTION TYPE-D, FRAME CRACKED STA 99 LONGERON 25L. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE AT STA 99 STR 25L IAW DHC SK-748-234A REF ENGR FILE NR DC8-53-1749.

Part: SKIN — CRACKED (WS 304)

INSPECTION TYPE:D, RT WING L/E STA XFS304 UPPER SKIN CRACKED BETWEEN THE 4TH AND 5TH INBD HOLES. INSTALLED DOUBLER REPAIR PER SRM 57-2-1 FIG 38.

Part: SKIN — CORRODED (BS 1690)

INSPECTION TYPE-D, FUSELAGE SKIN CORROSION BLEND OUT IS OUT OF LIMITS FS 1690 BETWEEN LONG 27R AND 28R AFT SKIN. CUT OUT DAMAGE AND REPAIRED IAW DHC SK 748-146 REF ENRG FILE NR DC8-53-1745.

Part: ANGLE — CORRODED (BS 1766)

INSPECTION TYPE-D, RT FLOOR SUPPORT ANGLE CORRODED AT AFT BLKD STA 1766 RBL 8. REMOVED FABRICATED AND INSTALLED ANGLE IAW SRM 53-4-1.

Part: FITTING — CRACKED (BS 822)

INSPECTION TYPE:D, STRINGER TIE FITTING CRACKED STA 822 BELOW RT CUSP. REMOVED AND REPLACED FITTING PER SRM 51-1-20.

Part: ANGLE — CRACKED (BS 980)

LT AFT, LT CORNER CENTER WING ANGLE TO FUSELAGE FITTING CRACKED BS 980. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-1-20D AND DWG 4647365.

Part: FITTING — CRACKED (BS 742)

INSPECTION TYPE-D, STA 742 FRAME FITTING LT SIDE IS CRACKED AT THE LWR END. REMOVED AND REPLACED FITTING IAW DHC SK-748-110 AND SRM 51-1-20.

Part: DOUBLER — CORRODED (BS 880-900)

INSPECTION TYPE:D, STA 880-900 FINGER DOUBLER AT BL 0 CORRODED THROUGHOUT. FABRICATED AND INSTALLED REPLACEMENT DOUBLER PER SRM 53-7-1, 51-9-0, AND 51-1-20.

Part: DOUBLER — CORRODED (BS 880-900)

INSPECTION TYPE:D, STA 880-900 LBL 60-66 FINGER DOUBLER HAS WIDE SPREAD CORROSION. FABRICATED REPLACEMENT DOUBLER AND INSTALLED IAW SRM 53-7-1, 51-9-0, AND 51-1-20.

Part: FITTING — CRACKED (BS 717)

INSPECTION TYPE-D, STA 717 FRAME FITTING BELOW FLOOR IS CRACKED AT THE LOWER END LT SIDE O/B. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING PER SRM 51-1-20 DWG 3616947 AND DHC SK-748-110.

Part: DOUBLER — CRACKED (BS 0.0)

INSPECTION TYPE:D, CRACKED INTERNAL DOUBLER AT FS 0 LT SIDE BETWEEN LONG 32L AND 33L. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 53-3-1.

Part: DOUBLER — CORRODED (BS 900-920)

INSPECTION TYPE:D, STA 900-920 FINGER DOUBLER AT BL 0 CORRODED THROUGHOUT. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-7-1, 51-9-0, AND 51-1-20.

Part: ANGLE — CRACKED (BS 180)

INSPECTION TYPE:D, CEILING SUPPORT ANGLE BENT AND CRACKED AT STA 180 BL30L. REMOVED ANGLE, CUT OUT DAMAGED AREA, FABRICATED DOUBLER AND INSTALLED PER SRM 53-2-0 FIG 2A.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:D, STA 680 STR 11R - STR END TIE SIDE IS CRACKED IN TWO. REPLACED FITTING PER SRM 51-1-20.

Part: FITTING — CRACKED (BS 420)

INSPECTION TYPE:D, FRAME TO LONGERON FITTING CRACKED AT FS 420 LONGERON 11L. REPLACED FITTING IAW SRM 51-1-20 AND 51-3-0.

Part: FITTING — CRACKED (BS 1240)

INSPECTION TYPE-D, STA 1240 STR 35R, END FITTING IS CRACKED. REMOVED AND REPLACED END FITTING IAW DWG 3758495 AND SRM 51-1-20.

Part: DOUBLER — CRACKED (RT WING)

INSPECTION TYPE:D, RT WING L/E SECTION, BETWEEN PYLONS, HAS A 17 INCH CRACK AT LWR INTERNAL DOUBLER AT MIDDLE OF SECTION (LWR). REMOVED INTERNAL DOUBLER, FABRICATED REPLACEMENT SPLICE STRAP IAW SRM51-3-1. INSTALLED SPLICE STRAP IAW SRM 51-1-20 AND 51-1-21.

Part: FRAME — CORRODED (BS 1060)

INSPECTION TYPE: D. FRAME CAP CORRODED AT STA 1060, LONGERON 36. REPAIRED IAW SRM 53-2-0 FIG 1D, AND 51-1-21.

Part: RIB — CRACKED (RT WING)

INSPECTION TYPE:D, RT WING L/E SECTION BETWEEN PYLONS ABOVE SLOT ACTUATOR LE RIB IS CRACKED AT UPPER AFT END. STOP DRILLED CRACK AND INSTALLED REPAIR IAW SRM 57-1-11.

Part: STRINGER — CORRODED (BS 70)

INSPECTION TYPE:D, STA 70 STR 32R IS CORRODED AT AFT END. FABRICATED, AND INSTALLED LONGERON 32R FROM STA 8.0 TO 70.0 IAW SRM 53-3-1, 51-1-20, AND 51-1-21.

Part: SHEAR TIE — CORRODED (BS 35)

INSPECTION TYPE-D, STA 35 SHEAR TIE, BETWEEN STR 34L AND 34R, IS CORRODED. REMOVED AND REPLACED SHEAR TIE IAW DWG 5618866 AND SRM 53-10-0 AND SRM 51-1-21.

Part: DOOR JAMB — CORRODED (BS 200)

INSPECTION TYPE:D, MAIN CARGO DOOR JAMB SUPPORT ANGLE CORRODED AT STA 200. FABRICATED REPLACEMENT ANGLE, AND INSTALLED IAW SRM 51-1-21, 51-2-0, 51-1-0 AND 51-1-21.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE-D, STA 70 STR 30R END FITTING IS CORRODED. REMOVED AND REPLACED FITTING IAW SRM 51-1-29D AND 51-1-21.

Part: ANGLE — CORRODED (BS 160)

INSPECTION TYPE-D, FLOORBEAM SUPPORT ANGLE AT STA 160, HAS MODERATE CORROSION ABOUT 4 INCHES ABOVE STR 27R. REMOVED CORROSION AND REPAIRED IAW SRM 53-2-0 FIG 1B, AND 53-7-1 FIG 14.

Part: TEE CHORD — CRACKED (BS 70)

INSPECTION TYPE-D, TEE CHORD CRACKED AT STA 70 FROM LONGERON 28R TO 30R. CUT OUT DAMAGE, FABRICATED REPAIR DOUBLERS AND ANGLE AND INSTALLED IAW SRM 53-2-5 FIG 8C-2, 51-1-20, 51-1-21, AND 51-3-0.

Part: FITTING — CRACKED (BS 8)

INSPECTION TYPE-D, STA 8 STR 23R END FITTING IS CRACKED AND CORRODED. FABRICATED REPLACEMENT FITTING AND INSTALLED IAW SRM51-1-20 AND DWG 4612650.

Part: SHEAR TIE — CORRODED (BS 55)

INSPECTION TYPE-D, STA 55 SHEAR TIE BETWEEN STR 34L AND 34R IS CORRODED. FABRICATED AND INSTALLED SHEAR TIE IAW SRM 51-1-21 AND DWG 6745869.

Part: FRAME — CORROSION (BS 1060)

INSPECTION TYPE-D, FRAME CORROSION OUT OF LIMITS AT STA 1060 LONGERON 36. CUT OUT DAMAGE, FABRICATED DOUBLERS AND FILLERS AND INSTALLED PER SRM 53-2-0.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE:D, FS 1690 LONGERON 26L END FITTING CRACKED. REPLACED FITTING IAW SRM 53-1-0 AND 51-1-20.

Part: STRINGER — CORRODED (BS 8-70)

INSPECTION TYPE:D, STA 8-70 STR 30R IS CORRODED IN SEVERAL PLACES. FABRICATED AND INSTALLED REPLACEMENT DOUBLER DWG 3642838 AND SRM 51-1-21.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE-D, STR END FITTING IS CRACKED STA 1690 STR 32L. REMOVED AND REPLACED FITTING IAW SRM 51-1-29D, 51-1-21, 51-3-0 AND MM 20-16-00.

Part: SKIN — CORRODED (RUDDER)

INSPECTION TYPE-D, RT UPPER RUDDER T/E SKIN PANEL CORROSION BLEND OUT BEYOND LIMITS AT ZU307. REPAIRED RUDDER SKIN IAW SRM 55-2-0, 51-1-9, 51-1-8B. CALCULATED RUDDER BALANCE PER SRM 51-4-6 AND 51-4-8.

Part: FITTING — CORRODED (BS 70)

INSPECTION TYPE-D, STA 70 STR 29R END FITTING IS CORRODED. REMOVED AND REPLACED END FITTING IAW SRM 51-1-29D AND 51-1-21.

Part: LONGERON — CORRODED (BS 8-70)

INSPECTION TYPE:D, LONGERON 27R AT STA 8 TO 70 RT HAS CORROSION BEYOND LIMITS. REMOVED AND INSTALLED REPLACEMENT PART IAW SRM 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (WS 163.75)

INSPECTION TYPE:D, RT WING INBD L/E TANK RIB STA XFS163.75 HAS CRACKED REPAIR DOUBLER AT AFT LWR END. FABRICATED AND INSTALLED REPAIR IAW SRM 57-2-0

Part: FITTING — CRACKED (BS 380-400)

INSPECTION TYPE:D, LONGERON 31L SPLICE FITTING CRACKED FS 380-400. REMOVED AND REPLACED SPLICE FITTING P/N 3754473-501N IAW SRM 51-1-20 AND 53-1-0.

Part: SPLICE — CRACKED (BS 600-620)

INSPECTION TYPE-D, STA 600 TO 620, STR 31L SPLICE FITTING HAS A 9 INCH CRACK. FABRICATED REPLACEMENT SPLICE AND INSTALLED IAW SRM 51-1-21 AND DWG 3750257.

Part: FITTING — CRACKED (BS 600-620)

INSPECTION TYPE-D, STA 600 TO 620 STR 31R SPLICE FITTING HAS MULTIPLE CRACKS ON LWR LEG. FABRICATED REPLACEMENT FITTING AND INSTALLED IAW SRM 51-1-20 AND DWG 3750257.

Part: FITTING — CRACKED (BS 1260-1280)

INSPECTION TYPE:D, STA 1260-1280 STR SPLICE IS CRACKED DUE TO HEAVY CORROSION. REPLACED SPLICE FITTING IAW SRM 51-1-20 AND 51-1-11.

Part: ANGLE — CORRODED (BS 20)

INSPECTION TYPE-D, INTERCOSTAL ANGLE CORRODED AT STA 20, RBL40. REMOVED ANGLE PER SRM 53-7-1, FABRICATED REPLACEMENT ANGLE AND INSTALLED PER SRM 51-1-20, 51-1-21, AND 51-1-8.

Part: DOUBLER — CORRODED (BS 75)

INSPECTION TYPE-D, CONTROL CABIN SUB FLOOR STA 75 LBL 59 FINGER DOUBLER IS CORRODED INTERNALLY WITH 7 CORRODED AND SHEARED RIVETS. REMOVED FINGER DOUBLER. REMOVED CORROSION UNDER DOUBLER (WITHIN LIMITS) FABRICATED AND INSTALLED FINGER DOUBLER PER SRM 53-3-1 FIG 7D AND 51-1-21.

Part: ANGLE — CRACKED (LT WING)

INSPECTION TYPE:D, LT WING INBD L/E INBD UPPER AFT L/E ATTACH ANGLE CRACKED APPROX 4.75. FABRICATED AND INSTALLED REPLACEMENT BRACKET PER DWG 5769646 AND SRM 51-3-0 AND 53-8-1.

Part: SKIN — CORRODED (WS 610-618.5)

INSPECTION TYPE-D, LT WING O/B L/E UPPER SKIN AT STA XFS 610.0 IS CRACKED AND CORRODED AT AFS618.5. REPAIRED AREA IAW SRM 57-2-1 FIG 38.

Part: RIB — CRACKED (WS 360)

INSPECTION D-CHECK, LT WING L/E RIB CRACKED AT STA XFS 360.250 UPPER AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: STIFFENER — CRACKED (BS 940)

INSPECTION TYPE-D, RT UPPER KEEL BEAM VERTICAL STIFFENER BS 940 IS CRACKED. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 53-2-0 FIG 1B PAGE 2E.

Part: RIB — CRACKED (WS 254)

INSPECTION D-CHECK, L/E RIB CRACKED AT STA XRS 254.00 AT UPPER END LT WING. STOP DRILLED AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 10)

INSPECTION TYPE:D, RT WING TE AT FLAP STA 10.00 - THE TE I/B RIB IS CRACKED IN 2 PLACES. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 57-5-0 AND SRM ADDENDUM DC8-5720-7767-A.

Part: RIB — CRACKED (WS 6.225)

INSPECTION D-CHECK, RT WING L/E XOLDI 6.225 LWR L/E RIB CRACKED AT THE AFT END. STOP DRILLED CRACK, REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 679)

INSPECTION D-CHECK, RT WING L/E, STA XFS 679.00, RIB CRACKED AT UPPER AFT END. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE AND INSTALLED PER SRM 57-2-0 FIG 2, SHT 2 AND SRM 51-1-20D, 51-1-21.

Part: RIB — CRACKED (WS 722.5)

INSPECTION D-CHECK, LEFT WING LEADING EDGE RIB AT STA XFS 722.5 IS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 57-2-0.

Part: SKIN — CRACKED (WS 423)

INSPECTION TYPE-D, LT WING CENTER L/E UPPER SKIN AT STA XFS 423.0 IS CRACKED AT 3 FASTENERS. STOP DRILLED CRACKS, FABRICATED AND INSTALLED DOUBLER IAW UPS EO DC8-5720-7767A AND SRM 51-1-26.

Part: RIB — CRACKED (WS 817)

INSPECTION TYPE:D, RT WING L/E AT XFS817.00. THE L/E RIB IS CRACKED AT THE UPPER AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 51-1-20.

Part: STIFFENER — CORRODED (NLG WW)

INSPECTION TYPE:D, NLG CEILING STRUCTURE STIFFENER HAS EXCESSIVE BULDGING AFT LT LOWER SURFACE OF NLG CEILING. FABRICATED AND INSTALLED REPLACEMENT STIFFENER PER DWG 5612298. INSTALLED ON N/R 528341.

Part: RIB — CRACKED (WS 766.25)

INSPECTION TYPE:D, LT WING L/E RIB IS CRACKED AT STA XFS 766.25 AFT UPPER END. STOP DRILLED CRACK , INSTALLED REPAIR IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 714)

INSPECTION TYPE:D, RT WING L/E AT STA XFS714.00 L/E RIB CRACKED AT THE UPPER AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 467.323)

INSPECTION D-CHECK, LT WING L/E RIB AT STA XS467.323, IS CRACKED AT THE AFT UPPER END. STOP DRILLED AND REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 785)

INSPECTION TYPE:D, LT WING L/E RIB CRACKED AT STA XFS785.0 AFT UPPER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 797.5)

INSPECTION TYPE:D, LT WING L/E RIB AT STA 797.5 IS CRACKED AT AFT UPPER END. STOP DRILLED CRACK, AND REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 426)

INSPECTION D-CHECK, RT L/E RIB AT STA XFS 426.00 UPPER L/E RIB IS CRACKED AT AFT END. STOP DRILLED AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 810)

INSPECTION TYPE:D, LT WING L/E RIB CRACKED AT STA 810.00 AFT UPPER END. STOP DRILLED CRACK, INSTALLED REPAIR IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 328.)

INSPECTION D-CHECK, RT WING L/E STA XFS 328.00 UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 635)

INSPECTION D-CHECK, LEFT WING L/E RIB AT STA XFS 635.0, IS CRACKED AT THE AFT LWR END. STOP DRILLED CRACK, FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 57-2-0.

Part: HINGE CASTING — CRACKED (RT AILERON)

INSPECTION TYPE-D, RT O/B AILERON CENTER HINGE CASTING IS CRACKED AT UPPER O/B LEG. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DWG 5718753, SRM 51-1-20, AND DHC SK-748-126 REF UPS ENRG FILE NR DC8-57-0763.

Part: WEB — CORRODED (BS 1740)

INSPECTION TYPE-D, RT FLOOR COLLAR WEB, AFT OF STA 1740, IS CORRODED OUT OF LIMITS. REMOVED, FABRICATED REPLACEMENT WEB AND INSTALLED IAW SRM 53-1-0, SRM 51-1-21.

Part: SKIN — CORROSION (BS 1746)

INSPECTION TYPE-D, THE AFT FUSELAGE SKIN, AT STA 1746 STR 28L, HAS SEVERE CORROSION. REPAIRED SKIN IAW DHC SK-748-159 REF UPS ENRG FILE NR DC8-53-1746.

Part: LONGERON — CORROSION (BS 1680)

INSPECTION TYPE:D, LONGERON 29L HAS EXFOLIATED CORROSION AT STA 1680. FABRICATED AND INSTALLED REPLACEMENT LONGERON FROM STA 1650 TO 1690 IAW SRM 53-1-0, 51-1-21, AND DWG 5757779.

Part: SKIN — CORRODED (BS 1640-1660)

INSPECTION TYPE-C, SKIN AND DOUBLER CORRODED STA 1640 TO 1660 STR 30L TO 32L. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLERS AND SKIN IAW SRM 51-1-21, 51-1-8, 53-2-1 FIG 8 AND DHC SK-748-046 IR, REF ENRG FILE NR DC8-53-1750.

Part: SKIN — CORROSION (BS 4-70)

INSPECTION TYPE-D, FUSELAGE SKIN FROM FS 70 TO FS 4 BETWEEN LONGERONS 31R AND 31L SHOWS SIGNS OF CORROSION BETWEEN SKIN AND INTERNAL DOUBLER. REMOVED SKIN AT STA 21.92 THROUGH 70.0 LONGERON 31L TO 31R. SPLICED SKIN FROM 21.92 TO 79.0 PER UPS EO DC8-5330-8942-B AND INSTALLED IAW SRM 51-1-20 AND 51-1-21.

Part: RIB — CRACKED (WS 201)

INSPECTION TYPE:D LT WING I/B L/E RIB CRACKED AT STA XFS 201.25 UPPER AFT END. STOP DRILLED CRACK AND REPAIRED IAW 57-2-0 FIG 2 .

Part: ANGLE — CRACKED (BS 640)

INSPECTION TYPE:D, LT FWD UPPER WING FILLET PANEL ATTACH ANGLE IS CRACKED IN TWO, BS 640. FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-21.

Part: RIB — CRACKED (WS 6.225)

INSPECTION TYPE:D, LT WING LE RIB AT STA XOLDI 6.225 IS CRACKED. FABRICATED AND INSTALLED REPAIR IAW SRM 57-2-0.

Part: DOUBLER — CRACKED (WS 423)

INSPECTION TYPE:D, LT WING CENTER L/E UPPER DOUBLER AT STA XFS423.0 IS CRACKED. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 57-3-1, 51-1-21.

Part: SKIN — CRACKED (WS 597)

LT WING - 2.50 INCH CRACK IN LOWER SURFACE OF LEADING EDGE SKIN - STA XFS 597.000, OTBD OF NR 1 PYLON. STOP DRILLED CRACKS (26700/QC15650). FABRICATED DOUBLER AND INSTALLED SAME PER EO NR DC8-5720-4087.

Part: LIGHT — INOP (COCKPIT)

MAINTENANCE PRE-DEPARTURE CHECK, EMERGENCY EXIT LIGHT INOP. EMERGENCY LIGHT BATTERY PACK REPLACED.

Part: FITTINGS — CRACKED (FS 940/960)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, 2 FITTINGS ABOVE LONGERON 24 CRACKED FS 940 AND 960. REPLACED FITTINGS PER SRM 51-1-20D.

Part: FLOORBEAM — CORROSION (FS 920)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY CORROSION LT PRESSURE DECK PANEL AND FLOORBEAM FS 920 ABOVE LONGERON 24L. REPAIRED PER UPS EO.

Part: TRAP FITTING — CRACKED (LT/RT WING)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT AND RT TRAP FITTINGS CRACKED AT LOWER ENDS. REPLACED FITTINGS PER SRM 57-2-7.

Part: SKIN — CRACKED (SLIDE DOOR)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, SKIN CRACKED ON A-X-SLIDE DOOR AT FASTENER ON AFT END OF RAMP. REPAIRED SKIN PER SRM 52-2-0.

Part: TAB — DELAMINATED (RUDDER)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RUDDER TRIM TAB DELAMINATION RT SIDE 30 INCHES FROM BOTTOM. REPLACED TAB ASSY FOR MM 27-21-02.

Part: DOOR FRAME — CRACKED (SLIDE DOOR)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, A-X-SLIDE FRAME CRACKED ON BOTTOM SIDE THROUGH LIGHTENING HOLE. REPAIRED PER UPS EO.

Part: GUSSET — CORRODED (FS 156)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, MODERATE CORROSION AT GUSSET ANGLE RBL 35 UNDER COPILOT RUDDER PEDALS AND BULKHEAD. REPLACED GUSSET PER SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (FS 640)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, 1 INCH LONG CRACK ON LOWER SIDE OF SHEAR TIE FS 640 BETWEEN LONGERONS 26L TO 27L. REPLACED SHEAR TIE PER SRM 53-2-0 AND SRM 51-1-20D.

Part: RIB — CRACKED (WS 501)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING L/E UPPER RIBS CRACKED AT STA XFS 501. REPAIRED PER MM 57-00-00 FIG 801.

Part: LONGERON — CORRODED (FS 902)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED HEAVY INTERGRANNULAR CORROSION FS 902, LONGERON 24R NEEDS REPLACEMENT. REPLACED LONGERON PER DOUGLAS DRAWING NR 5750196.

Part: SKIN — DELAMINATED (RT SPOILER)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED RT WING NR 2 SPOILER DELAMINATED ON BOTTOM SIDE. REPLACED SPOILER PER MM 27-61-00.

Part: LONGERON — CRACKED (FS 880)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED LT LONGERON 24 CRACKED IN FISH MOUTH BOTTLE BOLT HOLE FS 880. REPLACED LONGERON PER DOUGLAS DRAWING NR 5750188.

Part: RIB — CRACKED (LT WING LE)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT WING L/E ASSY HAS 8 RIBS CRACKED AT STA XFS 691, 672, 666, 660, 647, 641, 635 AND 629. REPAIRED PER MM 57-00-00 FIG 801.

Part: VANE — DELAMINATED (NR 1 TE FLAP)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT AND RT WING NR 1 FLAP VANES DELAMINATED ON BOTTOM SIDES. REPLACED VANES PER MM 27-51-14.

Part: VANE — DELAMINATED (NR 5 TE FLAP)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT WING O/B NR 5 FLAP VANE DEL ON UPPER SIDE. REPLACED VANE ASSY PER MM 27-51-14.

Part: SKIN — CRACKED (RT WING)

WHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING I/B SLOT CUTOUT AFT O/B CORNER HAS A 1.0625 INCH CRACK. INSTALLED NEW PANEL SECTION PER SRM 51-3-0.

Part: EEL BATTERY PACK — FAILED (CABIN)

CREW REPORTED EMERGENCY LIGHTS CAME ON IN-FLIGHT AND WOULD NOT GO OUT. REPLACED EMERGENCY BATTERY PACK.

Part: EEL BATTERY PACK — DISCHARGED (CABIN)

WHILE ON GROUND, MAINTENANCE FOUND EMERGENCY EXIT LIGHTS WOULD NOT DISARM. REPLACED EMERGENCY BATTERY PACK, SYS CHECKS OK.