N755UP

Part: BATTERY PACK — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A EMERGENCY LIGHTS DO NOT TEST. REPLACED EMERGENCY BATTERY PACK. OPS CHECK GOOD PER MM 33-50-01-2.

Part: BUSS — FAILED (NR 1)

LOST NUMBER ONE ELECTRICAL BUS. CREW REQUESTED SPECIAL PRIORITY TO REMAIN IN RVSM AIRSPACE AND A LONG DESCENT INTO IAH. CREW DID NOT DECLARE EMERGENCY, BUT TOWER REQUESTED CFR TO STANDBY. R&R NR 1 GEN. PER MM 24-20-01-4, R&R NR 1 VOLT REG & GEN CONT PANEL PER MM 24-20-06-2. R&R GEN FEEDER WIRE T3-T6 & TRANSFORMER. RAN ALL ENGINES. A/C SYSTEM OPS CHECK GOOD.

Part: HYDRAULIC SYSTEM — FAILED

INSPECTION TYPE:N/A ATB - HYDRAULIC SYSTEM FAILURE, LEAK IN RT MLG WHEEL WELL. INSTALL SERVICE HOSE/FTG PER MM 32-32-03-2 & AMM 20-13-00-2. REMOVED AND REPLACED LT & RT ENG HYD PUMP CASE DRAIN FILTER ELEMENTS PER AMM 29-10-15-2-2. INSPECT PER MM 29-10-16-2. NO FOREIGN MATERIAL OR LEAKS NOTED. OPS CHECK ON EA EDP PER AMM 29-10-12-4, OPS NORMAL SERVICED HYD RESERVOIR PER AMM 12-30- 01-3. OK FOR SERVICE.

Part: NUT PLATE — DEFECTIVE (GIRT BAR FITTING)

INSPECTION TYPE:N/A FWD GIRT BAR FITTING IS LOOSE, (NUT PLATE IS BAD). REMOVED AND REPLACED NUT PLATE AND SECURED GIRT BAR FITTING. REF SRM 51-01-21-0.

Part: ESCAPE ROPE — OUT OF POSITION (COCKPIT)

INSPECTION TYPE:N/A CAPTAIN'S ESCAPE ROPE HAS FALLEN FROM ITS STORAGE AREA. REPACKED CAPTAIN'S ESCAPE ROPE PER AMM 25-60-2-2-2.

Part: ESCAPE ROPE — DEPLOYED (COCKPIT)

INSPECTION TYPE:N/A CAPTAINS ESCAPE ROPE AND COVER CAME OUT DURING T/O IN PHL. RESTOWED ROPE. OPS NORMAL.

Part: SLIDE — OUT OF POSITION (COCKPIT)

INSPECTION TYPE:N/A F/E DUMPED SLIDE ON DOOR OPEN. RE-INSTALLED SLIDE PER DC8 MM 25-60-01-2.

Part: SLIDE — OUT OF POSITION (CREW ENTRY DOOR)

INSPECTION TYPE:N/A CREW REPORTED TO MX THAT EMERGENCY SLIDE PACK ON CREW ENTRY DOOR FELL OUT OF COMPARTMENT. RE-INSTALLED EMERGENCY SLIDE ON THE CREW ENTRY DOOR, OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY EXIT LIGHTS INOP. REPLACED EMERGENCY LIGHTING BATTERY UNIT PER DC8 MM 33-50-01-2. OPS CHECK NORMAL.

Part: DOOR — OUT OF ADJUST (CREW ENTRY)

INSPECTION TYPE:N/A CREW ENTRY DOOR COULD NOT BE OPENED FROM THE INSIDE UPON ARRIVAL AT CLE. PERFORMED VERTICAL ADJUSTMENT ON CREW ENTRY DOOR IAW AMM 52-11-01-5. OPS CHECK GOOD.

Part: WINDSHIELD — MALFUNCTIONED (COCKPIT)

INSPECTION TYPE: N/A WITH WINDSHIELD IN -WARM UP- THE CENTER W/S STARTED BUBBLING AND IT WAS VERY HOT TO THE TOUCH. THIS SEVERELY DECREASES COCKPIT VISIBILITY. REMOVED AND REPLACED CTR W/S IAW MM 56-10-01-2, STEPS 1-3. B(12). COMPLETED INSTALLATION BY SEALING AND PRESSURIZING WINDOW. NO LEAKS NOTED.

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE:N/A DURING BITE CHECK EMERGENCY LIGHT WOULD NOT WORK. CHARGED BATTERIES WITH POWER ON, OPERATED SYSTEM & FOUND TO OPERATE NORMAL. OK FOR SERVICE.

Part: SKIN — CRACKED (WING) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 PANEL LANDING FOR ACCESS PNL 505F IS CRACKED. REPAIRED PNL LANDING FOR ACCESS PNL 505F IAW SAA EA NR 008-5710-01- A0505, UPS RAA NR DC8-57-20194, BAC MSG NR 1-237786953, AND FAA FORM 8100-9

Part: PANEL — CRACKED (WING) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 PANEL LANDING FOR ACCESS PANEL 505F IS CRACKED REPAIRED PANEL 505F ACCESS HOLE LANDING IAW SAA EA NR 008-5710-01- A0511, UPS RAA NR DC8-57-20196, AND FAA FORM 8100-9.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 69,055 hrs · 45,885 cycles

CRACK FOUND ON ACCESS PANEL LANDING L/CENTER TANK ACCESS HOLE 516 REPAIRED DAMAGED AT LT CENTER TANK ACCESS HOLE 516 IAW SAA EA NR 008-5730-01-A0493, UPS EO DC8-5730-25433-A, BAC MSG NR 1-237497515-1, BAC MSG 1-237497515-2, AND FAA FORM 8100-9

Part: STRINGER CLIP — CRACKED (RWS 463-428) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 CRACK ON STRINGER TO FRONT SPAR CAP FITTING BETWEEN XRS 463 AND 428. REPAIRED STRINGER TO FRONT SPAR SPAR CAP FITTING AT STA XRS 463 AND XRS 428 IAW SRM 51-1-20D, AND DWG 3644046.

Part: LONGERON — CRACKED (FS 1734 L15R) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 LONGERON CRACKED AT STA 1734 L15R. REMOVED LONGERON SECTION 15R AT STA 1734 IAW SRM 53-02-02 FIG 10. FABRICATED AND INSTALLED LONGERON SECTION AT STA 1734 L15R IAW SRM 53-2-2 FIG 10, AND SRM 53-02-02-0 FIG 10

Part: FITTING — CRACKED (FS 1760 L10L) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 LONGERON END FITTING CRACKED AT STA 1760 L10L. REMOVED, AND REPLACED LONGERON END FITTING AT STA 1760 L10L IAW SRM 51-1-24, 51-1-21, AND SRM 51-1-20D.

Part: FITTING — CRACKED (FS 8 L33R) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 CRACKED LONGERON END FITTING AT L33R FS 8. REMOVED AND REPLACED LONGERON END FITTING AT STA 8 L33R IAW SRM 51-1-20D, AND SRM 51-03-01-0, 51-01-20D-0.

Part: FITTING — CRACKED (FS 781) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 MAIN CABIN BOOT FITTING CRACKED AT STA 781.500 RT SIDE REPAIRED CRACKED BOOT FITTING AT STA 781.5, RT CENTER SPAR FRAME FITTING IAW SAA EANR 008-5310-01-A0489, UPS RAA NR DC8-53-20598-A BAC SERV MSG 1-236203861, AND FAA FORM 8100-9.

Part: LONGERON SPLICE — CRACKED (FS 1260 L36R) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 STA 1260 L36 SPLICE FITTING CRACKED ON RT SIDE FACING FWD REMOVED AND REPLACED LONGERON SPLICE SECTION AND END FITTINGS FROM STA 1270-1350 L36 IAW SRM 51-1-20D, 51-3-2 AND SRM 51-3-0.

Part: FITTING — CORRODED (FS 280 L35L) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 L35L AT STA 280-300 HAS CORROSION. FOUND CORROSION TO BE OUT OF LIMITS AT L35L FS 280-300 IAW SRM 53-02-00 FIG 0001F. REMOVED AND REPLACED BATHTUB FITTING, AND LONGERON SPLICE AT FS 280-300 L34L-L36L IAW SRM 53-02-02-0 FIG 010 AND DWG 9754913.

Part: BULKHEAD — CRACKED (FS 1766 LBL30) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 AFT PRESS BULKHEAD CRACKED 2 PLACES AT STA 1766 LBL 30, L15L. REPAIRED CRACKS AT AFT PRESS BULKHEAD STA 1766 LBL 30, L15L IAW SAA EA NR 008-5305-01-A0484, UPS EO DC8-5330-25392-A, BAC MSG NR 1-2366446 534-1 AND -2, FAA FORM 8100-9

Part: SHEAR WEB — CORRODED (FS 857 LBL25) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 HEAVY CORROSION ON PRESSURE WEB DOUBLER, STA 857, LT W/W, LBL 25. REPAIRED SHEAR WEB AT STA 857, XW=23, LBL 25 IAW SAA EA NR 008-5320-01 A0492, UPS RAA NR DC8-53-20600, BAC MSG NR 1-237059319, AND FAA FORM 8100-9.

Part: FITTING — CRACKED (FS 1690 L34R) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 L34R AT STA 1690 HAS BULGE UNDER SPLICE END. REMOVED FASTENERS AT L34R STA 1690 UNDER SPLICE, NO CORROSION NOTED IAW SRM 51-1-21. FOUND SPLICE END CRACKED AT STA 1690 L34R. REMOVED AND REPLACED LONGERON SPLICE END AT STA 1690, L34R IAW SRM 51-20-00 51-1-20D.

Part: ATTACH FITTING — CRACKED (FS 1766 L6R) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 AFT PRESS BULKHD TO LONGERON ATTACH FITTING CRACKED AT STA 1766 L6R. REMOVED, FABRICATED, AND INSTALLED REPAIR ATTACH FITTING IAW DWG 5773844, AND SRM 51-1-20D AT STA 1766 L6R.

Part: SKIN — BULGED (FUSELAGE) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 BULGING SKIN FS 465 L32L EXTERNAL FUSELAGE. CUT OUT DAMAGE. FABRICATED AND INSTALLED FILLER, DOUBLER AND FINGER DOUBLER IAW SRM 53-02-01 FIG 007, 53-04-01-0 FIG 002, 51-10-00-0 FIG 002, 51-1-21 AND 51-1-20D.

Part: ANGLE — CRACKED (HORIZ STAB) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 RT HORIZ STAB 2 CRACKS INBD END ON T-ANGLE, FWD OF FRONT SPAR, 9PNL 64J. REMOVED AND REPLACED T-ANGLE IAW SRM 51-01-21, 51-03-00 AND 51-1-20D.

Part: ANGLE — CRACKED (HORIZONTAL STAB) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 RT HORIZ STAB UPPER BULLNOSE "L" ANGLE IS CRACKED, INBD END OF STAB NEXT TO FUSELAGE FWD OF FRONT SPAR. REMOVED AND REPLACED "L" ANGLE AND CAP ON RT HORIZ STAB UPPER BULL NOSE FWD OF FRONT SPAR IAW DWG 5654549, AND SRM 51-01-21, 51-03-00, 51-1-20D.

Part: ATTACH ANGLE — CRACKED (HORIZONTAL STAB) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 LT HORIZ STAB LWR AFT H-ANGLE HAS 6" CRACK FOR BANANA FAIRING ATTACHMENT. REMOVED H-ANGLE FROM LT HORIZ STAB LWR AFT BANANA FAIRING ATTACHMENT BEAM IAW SRM 51-03-00. FABRICATED AND INSTALLED BEAM ASSY AT LWR AFT LT HORIZ STAB BANANA FAIRING ATTACH BEAM IAW DWG 3702464, AND SRM 51-1-24, 51-3-0.

Part: INTERCOSTAL — CRACKED (HORIZONTAL STAB) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 LT HORIZ STAB 2 CRACKS INBD END ON TEE ANGLE, FWD OF FRONT SPAR (PNL 64J). REMOVED AND REPLACED T-ANGLE FITTING, LWR HORIZ STAB L/E INTERCOSTAL FWD OF FRONT SPAR INSIDE PNL 64J IAW SRM 51-03-02-0, 51-1-21, AND SRM 51-1-20D.

Part: ATTACH ANGLE — CRACKED (WING) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 UPPER SURFACE CLIP IS CRACKED AT XRS 139 STRINGER 1 AND 2 NR 2 ALT TANK. REMOVED AND REPLACED UPPER SURFACE CLIP AT XRS 139 STRINGER 1 AND 2 NR 2 ALT TANK IAW SRM 51-1-20D, AND SRM 51-3-2.

Part: SKIN — DENTED (FUSELAGE) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 TRANSFERRED FROM LP 325899/2: REF D-308181, FUSELAGE SKIN DENT FWD OF PIT 32 DOOR CUT OUT. REPAIRED FUSELAGE SKIN DENT FWD OF PIT 32 DOOR CUT OUT LWR FWD DOOR CORNER IAW SAA EA# 008-5320-01-A0477, UPS EO DC8-5330-25373-A, AND FAA FORM 8100-9.

Part: SLIDE — UNSECURE (PAX DOOR)

ESCAPE SLIDE NOT SECURED TO DOOR ON ONE SIDE. RESECURED ESCAPE SLIDE TO MAIN ENTRY DOOR AS REQUIRED.

Part: WINDOW — INOPERATIVE (COCKPIT)

CAPTAIN'S SLIDING WINDOW WOULD NOT OPEN. COMPLIED W/ALERT K 134429 REGARDING CAPTAIN & F/O'S CLEARVIEW WINDOW IAW WAN 1166862 & ALERT REPORT PGS. 1 & 2. NRC'S 962085 & 962041 GENERATED.

Part: SKIN — CORRODED (FS 660 L35L) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C2 CORROSION ON EXTERNAL SKIN MARKER BEACON ANTENNA MATING SURFACE STA 660 L35L. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-2-0 AT STA 660 L35L. REPAIRED FUSELAGE SKIN AT STA 660 L35L IAW SAA EA NR 008-5320-01-A0461, UPS RAA DC8-53-20593, BAC SRID 1-233406465, AND FAA FORM 8100-9.

Part: CAM FOLLOWER — OUT OF ADJUST (COCKPIT WINDOW)

F/O SLIDING WINDOW WILL NOT OPEN, C/W CAM FOLLOWER EXTENSION ADJUSTMENT TO F/O SLIDING WINDOW PER MM 56-10-03-5. OPS CK GOOD, OK FOR SERVICE.

Part: SKIN — CORRODED (E/E BAY DOOR) · airframe 69,055 hrs · 45,885 cycles

INSPECTION TYPE:C3 REPLACE FUSELAGE SKIN AT E/E DOOR STA 35 (P/N 5613862-61). REMOVED AND REPLACED FUSELAGE SKIN IAW UPS EO DC8-5330-22128-A AND DWG 5613862.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT)

INSPECTION TYPE:N/A CAPT OXYGEN MASK INOP. REMOVED AND REPLACED CAPT'S 02 MASK PER MEL 35-10-00. OPS CK GOOD.

Part: STRUCTURE — DAMAGED (FUSELAGE)

INSPECTION TYPE:N/A LOAD CREW REPORTED HOLE IN NR 3 BELLY COMPARTMENT FLOOR APPROX 4 FT FWD OF DOOR LEFT OF CENTER. COMPLIED WITH EO DC8-5320-8724 APPROX A. PERMANENT REPAIR WITHIN 30 DAYS. REPAIRED DAMAGED FLOOR PANEL IAW DC8 SRM 53-2-5, FIG 8A. THIS CLEARS D327390

Part: ESCAPE ROPE — DISLODGED (COCKPIT)

INSPECTION TYPE:N/A LEFT ESCAPE ROPE CAME UNSTOWED. RESTOWED LEFT ESCAPE TAPE AS PER DC8 MM 25-60-02-2.

Part: SMOKE GOGGLES — UNSANITARY (COCKPIT)

F/O'S SMOKE GOGGLES UNSANITARY. REMOVED AND REPLACED F/O'S SMOKE GOGGLES.

Part: WINDOW — LEAKING (COCKPIT)

ATB - PRESSURIZATION LEAK, STARTED AT 15,000'. LOCATED PRESS LEAKS AT CAPTAINS AND FO'S L1 AND R1 WINDOWS. SEALED WINDOWS IAW MM 56-10-02.

Part: WINDOW — CRACKED (COCKPIT)

CONSIDERABLE ARCING ON OUTER LAYERS OF CAPTAIN'S SIDE WINDSHILED. ACROSS ENTIRE TOP EDGE BUT CONCENTRATED AT TOP. REMOVED CAPTAIN'S WINDSHIELD PER MM 56-10-02-2. INSTALLED CAPTAIN'S WINDSHIELD IAW DC8 MM 56-10-022 THRU STEP 12.

Part: WINDOW FRAME — CORRODED (COCKPIT)

CAPTAIN'S WINDOW FRAME RUSTED PITTED ALONG LOWER I/B CORNER OF WINDOW FRAME. REMOVED CORROSION FROM WINDOW FRAME AND PRIMED AREA AS REQ. REMOVED Z ANGLE FROM CAPT LWR I/B CORNER OF WINDOW FRAME IAW 51-01-21A & 51-01-200. ORIG THICKNESS .090. MAT LOSS .013 TO BE W/IN LIMITS. TREATED & PRIMED IAW SRM 51-01-08-0. CORR REMOVED. INSTALL CAPTS EADT & EHSI ON INSTR PANEL IAW MM 34-23-00. OPS CHECK GOOD IAW MM 30-42-00 LK CHECK GOOD IAW 21-30-00.

Part: A/C PACK — FAILED (CABIN COOLING)

PACK TRIP OVERHEAT LIGHT ON LANDING ALTHOUGH WE HAD SECURED PACK WITH NORMAL CONFIGURATION. SMOKE IN COCKPIT. PACK TRIP DUE TO LOSS OF NR 4 GEN BUSS. RESET BATTERY POWER SWITCH. PERFORMED ADJ/TEST IAW MM 21-55-00-5. RAN ENGS SYSTEM OPS CK GOOD.

Part: WARNING LIGHT — ILLUMINATED (NR 4 GEN)

NR 4 GENERATOR "BUSS POWER FAIL" LIGHT ON CLIMB-OUT. V/F BECAME ERRATIC. ACCOMPLISHED CHECKLIST AND REGAINED POWER FOR 3 MINUTES WITHOUT TRYING PARALLELING. TRIPPED TWICE. MEGGED T1, T2, T3 FEED LINES ALL MORE THAN 20 MEGA OHMS. PLACED NR 2 GCU IN POS NR 4. PERFORMED ADJ/TEST IAW 24-20-01-5. NO FAULTS NOTED.

Part: OXYGEN MASK — LEAKING (COCKPIT)

INSPECTION TYPE:N/A F/O'S OXYGEN MASK LEAKS. REMOVED AND REPLACED F/O'S REGULATOR AND MASK PER MM CHAPT 35-10-08-2 AND CHAPT 35-10-07-4. OPS LEAK CHECK GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY EXIT LIGHT INOP. REPLACED EMERG LIGHT BATTERY PACK PER WDM 33-50-01. OPS CK OK.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK, CHECKS OK MM 33-50-01-2.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT)

INSPECTION TYPE:N/A EMERGENCY EXIT INDICATOR LIGHT BULB INOP. RELAMPED INTERIOR EMERGENCY EXIT LIGHT. OPS CK GOOD PER MM 33-11-0.

Part: RIB — CRACKED (RT WING) · airframe 68,304 hrs · 45,310 cycles

INSPECTION TYPE: C3, RIGHT CENTER L/E RIB (LOWER) CRACKED AT XFS 335. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 57-3-0 AND 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 68,304 hrs · 45,310 cycles

INSPECTION TYPE:C3, RIGHT WING O/B LEADING EDGE UPPER RIB IS CRACKED AT XFS 753.750. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-21 & 51-20D.

Part: RIB — CRACKED (RT WING) · airframe 68,304 hrs · 45,310 cycles

INSPECTION TYPE: C3, RIGHT WING O/B L/E RIB IS CRACKED WITH CORROSION AT XFS 772.500. REMOVED FASTENERS AND CORROSION IAW DD-8 SRM 51-1-21 & 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-3-0 FIG 19 & 57-2-0 FIG 2.

Part: INTERCOSTAL — CRACKED (RT WING) · airframe 68,304 hrs · 45,310 cycles

INSPECTION TYPE: C3, RT WING CENTER L/E INTERCOSTAL IS CRACKED AT XFS 387.750. STOP DRILLED CRACK AT STA XFS 387.750 IAW SRM 57-02-00-0 FIG 002. FABRICATED & INSTALLED REPAIR ANGLES IAW SRM 57-02-00-0 FIG 2 & DC-8 SRM 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 68,304 hrs · 45,310 cycles

INSPECTION TYPE:C3, RIGHT WING CENTER L/E INTERNAL DOUBLER AND L/E SKIN IS CRACKED AT DRAIN HOLE XFS 335.250. REMOVED INTERNAL DOUBLER AND STOP DRILLED 2 CRACKS IAW DC-8 SRM 51-1-21 & 57-2-0 FIG 6. REMOVED, FABRICATED AND INSTALLED EXTERNAL IAW 51-1-20D, 51-1-21, DC8-5720-4087-B, SRM 57-2-0 & 51-1-20D. FABRICATED AND INSTALLED INTERNAL DOUBLER IAW DWG 5769589, SRM 51-1-21, 51-1-8, 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 68,304 hrs · 45,310 cycles

INSPECTION TYPE:C3 RIGHT WING CENTER L/E UPPER RIB IS CHAFED THROUGHT AT XS 515-720. BLENDED CHAFED AREA IAW DC-8 SRM 57-2-0 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0 FIG 2, 57-3-1 & 51-1-20D.

Part: RIB — CRACKED (XFS) · airframe 68,304 hrs · 45,310 cycles

INSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE TWO LOWER RIBS CRACKED AT XFS 622.500 AND XSF 616.250. INSTALLED REPAIR DOUBLERS ON TWO RIBS AT XFS 622.500 AND XSF 616.250 IAW SRM 57-3-2 FIG 6 SHEET 2.

Part: FRAME — CRACKED (LT WING LE) · airframe 68,304 hrs · 45,310 cycles

INSPECTION TYPE: C3, LT WING LEADING EDGE OUTER SECTION STA XFS-759 UPPER FORMER HAS A CRACK AT AFT FASTENER. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-3-0 FIG19, 51-1-20D &51-1-21.

Part: CHANNEL — CRACKED (STA. XFS) · airframe 68,304 hrs · 45,310 cycles

INSPECTION TYPE: C3, LT WING LEADING CENTER SECTION LOWER SUPPORT U-CHANNEL HAS A CRACK AT AFT 2 FASTENERS 2 INCHES LONG STA XFS 510. STOPPED DRILLED CRACK IAW SRM 57-02-00-0. FABRICATED AND INSTALLED REPAIR ANGLE IAW DWG 5770375 AND DC-8 SRM 51-1-21 & 51-1-20D.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

CREW PREFLIGHT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IAW 33-50-01-2.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK. OPS CHECKS OK AT THIS TIME.

Part: WINDOW — LEAKING (COCKPIT)

INSPECTION TYPE:N/A, F/O CLEAR VIEW WINDOW STILL SQUEALING AT CRUISE AIR SPEEDS AND THE WINDOW IS VERY DIFFICULT TO OPEN. PRESSURIZED A/C TO 8 PSI DIFF, NO SQUEAL NOTED. SEALED EYEBROW WINDOW WITH AERODYNAMIC SEALENT. LUBED F/O CLEARVIEW WINDOW & WINDOW OPERATES SMOOTHLY.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 MAIN CABIN FS 1726-1746 INTERCOSTAL ABOVE L26L IS CRACKED. INSTALLED NEW INTERCOSTAL CLIPS IAW DC8 SRM 51-1-20D.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 FLOORBEAM STA 50 IS CRACKED ON UPPER FLANGE AT LT O/B END. REPAIRED IAW DC8 SRM 53-2-0 & TR 53-124.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 STA 1755 LONG 15L CRACKED AT I/B FLANGES. REMOVED DAMAGED SECTION OF LONGERON PER DC8 SRM 53-2-2 FIG 11. FABRICATED REPAIR PER DC8 SRM 53-2-2 FIG 11. INSTALLED PER DC8 SRM 51-1-20D

Part: FITTING — CRACKED (LT WING) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 LT WING NR 2 MAIN XRS 74.000 STRINGER END FITTING CRACKED AFT FITTING. REMOVED AND REPLACED END FITTING IAW DC8 SRM 51-1-20D AND 51-1-23

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 AFT FUSELAGE ACCESS THROUGH DOOR 60 AT FS 1766-1790 LONGERON 17R IS CRACKED. REMOVED LONG & ASSOCIATED PARTS IAW DC8 SRM 51-1-20D & 51-1-21. INSTALLED NEW LONG AND ASSOCIATED PARTS IAW DC8 SRM 51-1-20D & 51-1-21.

Part: FITTING — CRACKED (LT WING) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 S-51 STRINGER END FITTING CRACKED FWD SIDE AT XRS 74.000 2 MAIN. REMOVED AND REPLACED END FITTING IAW DC8 SRM 51-1-20D AND 51-1-23.

Part: FITTING — CRACKED (RT WING) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 S-51 STRINGER END FITTING CRACKED AFT SIDE AT XRS74.000 NR 3 ALT. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20D AND 51-1-23.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 AFT FUSELAGE ACCESS THROUGH DOOR 60 AT FS 1766-1790 LONGERON 17L IS CRACKED. REMOVED AND REPLACED LONG 17L FS 1766-1790 IAW DC8 SRM 51-1-20D AND 51-1-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 LONGERON 17R AT STA 1770 HAS CRACKED FITTING. REMOVED OLD FITTING, LOCATED, DRILLED, DEBURRED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D.

Part: FITTING — CRACKED (FUSELAGE) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 L17L AT STA 1770, FITTING CRACKED. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D.

Part: SKIN — CRACKED (FUSELAGE) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 L1 UPPER FWD DOOR CORNER HAS 4 EACH CRACKS ON EXTERNAL SKIN. FABRICATED DOUBLERS AND FILLER. INSTALLED REPAIR DOUBLERS, FILLERS, DOOR PAN, PAN SPLICES, DOOR SOPS, TORQUE BOX WEBS, SEAL DEPRESSOR AND CALIFORNIA PNL IAW DC8 SRM 51-1-21, 51-1-21A, 51-1-20D, AND 51-3-0.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 R2 UPPER AFT DOOR JAMB CORNER HAS CRACKED INTERNAL DOUBLER APPROX 3 INCHES LONG FOUND BY RADIOGRAPHY. REPAIRED AREA IAW DC8 SRM 53-2-0 T/R 53-133.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 L2 LWR FWD DOOR JAMB CORNER CRACKED APPROX 1.5 INCHES LONG ABOVE TRIMOUT FOUND BY RADIOGRAPHY. REPAIRED AREA IAW DC8 SRM 53-2-0.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 L1 DOOR LWR FWD DOOR JAMB CORNER HAS A CRACKED CUSP LONGERON FOUND BY RADIOGRAPHY. REMOVED AND REPLACED CRACKED INTERCOSTAL IAW DAC DWG 5797646.

Part: FRAME — CORRODED (FUSELAGE) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 AFT PIT FRAME CORRODED AND CRACKED AT SCREW HOLE STA 1400 STRINGER 36. TRIMMED OUT DAMAGED AREA AND FABRICATED REPAIR DOUBLER IAW SRM STD-5310-002. INSTALLED REPAIR DOUBLER IAW SRM STD-5310-002.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 MAIN CABIN STA 147 LONG 21R ANGLE HAS SHORT FASTENER IN DOUBLER DRILLED HOLE. REMOVED ANGLE, CORROSION FOUND, BLENDED, OUT OF LIMITS IAW DC8 SRM 5 1-1-8, 51-1-20D AND SRM 53-2-0. FABBED ANGLE IAW DC8 SRM 51-1-24, AND DAC DWG 2649940. INSTALLED ANGLE IAW DC8 SRM 51-1-20D.

Part: SKIN — DENTED (FUSELAGE) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 DENT IN FUSELAGE SKIN AFT OF L4 DOOR. COLD WORKED AND BLENDED IAW DC-8 SRM 53-2-0, WITHIN LIMITS. NO CRACK NOTED IAW DAC NDT SRM 06-10-01.001. FABBED IAW DC-8 SRM 53-2-1 FIG 10. REPAIRED DENT IAW DC-8 SRM 53-2-1 FIG 10.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 67,392 hrs · 44,587 cycles

INSPECTION TYPE:C1 R2 DOOR UPPER AFT JAMB LONGERON 11 CRACKED. REMOVED AND REPLACED LONGERON IAW DC8 SRM 51-1-20D.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERY DISCHARGED. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK. CHECKS OK.

Part: COVER — DAMAGED (EVAC SLIDE)

INSPECTION TYPE:IN EVAC SLIDE COVER IS DAMAGED. SLIDE CASE WILL NOT STAY CLOSED. GAPS OPEN AT THE BOTTOM. SLIDE COVER REMOVED AND ROUTED TO SHEETMETAL REPLACED SHEARED RIVETS ON COVER LATCH IAW 51-1-21 DC8 SRM 79657 9-15-01 INSTALLED SLIDE PER 25-60-01.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A EMERGENCY LIGHTS WILL NOT TEST. REMOVED AND REPLACED BATTERY PACK.

Part: SLIDE — LOOSE (PAX DOOR)

INSPECTION TYPE:N/A, ESCAPE SLIDE LOOSE. *S/D* RESECURED ESCAPE SLIDE AS NEEDED PER MM 25-60.

Part: ACTUATOR — OUT OF ADJ (RUDDER)

INSPECTION TYPE:N/A, PILOT REPORT-A/C REQUIRES EXCESSIVE RUDDER TRIM ON TAKEOFF AND LANDING DURING CALM WIND CONDITIONS. IN CRUISE FLIGHT AIRCRAFT REQUIRES 5 DEGREES RUDDER TRIM. ADJUSTED RUDDER POWER PACK IAW MM 27-21-02, SYS OPS CHECKS GOOD.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 66,183 hrs · 43,735 cycles

INSPECTION TYPE:C2, AFT CABIN FLOOR PNL F214 LWR SIDE SEVERAL AREAS OF CORROSION MARKED (RACK 23 SHELF 4) DOT A356. REMOVED CORROSION ON FLOOR PANEL, REPLACED HAT CHANNEL, ALODINED AND PRIMED IAW DC8 SRM 53-2-0, 51-1-21 & 51-1-8.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 66,183 hrs · 43,735 cycles

INSPECTION TYPE:C2 R1 DOOR HAS CRACK IN LOWER AFT CORNER. CLEANED IAW DC8 SRM 51-1-8, PERFORMED HFEC IAW SRM 06-10-01.001 TO VERIFY CRACK FABBED -11 DOUBLER -13 DOUBLER & -23 FILLER IAW DC8 SRM 5 3-2-0 FIG 14. ALODINED AND PRIMED DOUBLERS AND FILLER IAW DC8 SRM 51-1-8. INSTALLED DOUBLERS AND FILLER WITH HI-LOKS IAW DC8 SRM 51-01-20D & 53 -2-0 FIG 14. PAINT TO BE TOUCHED UP ON NR 227999 ITEM 13.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,183 hrs · 43,735 cycles

INSPECTION TYPE:C2, AFT PIT L25 LT STA 1040 - 1060 SPLICE HAS 2'' CRACKED (MKD) DOT J974. REMOVED FILLET PANEL IAW DC8 SRM 51-3-0. REMOVED FITTING IAW DC8 SRM 51-1-21, DRILLED AND LOCATED FITTING IAW DC8 SRM 51-1-24, INSTALLED FITTING IAW DC8 SRM 51-1-20D, INSTALLED FILLET PANEL IAW DC8 SRM 51-3-0.

Part: FITTING — CRACKED (ACCESSORY BAY) · airframe 66,183 hrs · 43,735 cycles

INSPECTION TYPE:C2, LONGERON SPLICE FITTING CRACKED STA 1680. REMOVED FITTING IAW DC8 SRM 51-1-21, LOCATED, DRILLED NEW FITTING IAW DC8 SRM 51-1-24, INSTALLED FITTING IAW DC8 SRM 51-1-20D, TORQUED BOLT IAW DC8 SRM 51-3-0.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 66,183 hrs · 43,735 cycles

INSPECTION TYPE:C2, FUSELAGE AFT RT LOWER FILLET PANEL ATTACH ANGLE CRACKED STA 1080 & L30R. REMOVED PART FROM AIRCRAFT IAW DC8 SRM 53-2-0, BLENDED WITHIN ALLOWABLE LIMITS. ALODINED AND PRIMED ATTACH ANGLE IAW DC8 SRM 51-1-8. INSTALLED ATTACH ANGLE IAW DC8 SRM 51-1-20D & 51-1-21.

Part: ANGLE — CRACKED (TORQUE BOX) · airframe 66,183 hrs · 43,735 cycles

INSPECTION TYPE:C2, AFT PIT DUCT TORQUE BOX ATTACH ANGLE CRACKED AT LWR RADIUS FWD SIDE OF STA 1000 FLOORBEAM 2 INCHES I/B OF STANCHION. REMOVED CRACKED ANGLE, FABBED NEW ANGLE IAW DAC DWG 5644699, ALODINED AND PRIMED IAW DC8 SRM 51-1-8 AND INSTALLED ANGLE IAW DC8 SRM 51-1-21.

Part: FITTING — CRACKED (DOOR FRAME) · airframe 66,183 hrs · 43,735 cycles

INSPECTION TYPE:C2, AFT PIT STA 1288.0 L27-28L FWD DOOR JAMB TORQUE BOX Z FITTING IS CRACKED DOT 969. REMOVED CRACKED Z FITTING RCVD NEW Z FITTING P/N 3755842-2N S/N 836395 PO 335326 MAT ID FOR Z FITTING SPLICE REPAIR ANGLE 7075-T6 511 PO 297 588 EXTRUSION BAC1503-100434. FABBED REPAIR SPLICES, LOCATED DRILLED & DEBURRED NEW Z FITTING. ALODINED, PRIMED AND INSTALLED NEW Z FITTING AND REPAIR SPLICES IAW DC8 SRM 51-1-8 & 53-2-0.

Part: FITTING — CORRODED (FUSELAGE) · airframe 66,183 hrs · 43,735 cycles

INSPECTION TYPE:C2, FUSELAGE EXTERIOR SKIN IS BULGED 2 RIVETS PULLING STA 1640 & L36-34R. REMOVED LONG FITTING AT STA 1640 & L34R FOUND TO BE OUT OF LIMITS. LOCATED AND DRILLED NEW FITTING PN 4647657, INSTALLED NEW FITTING.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 66,183 hrs · 43,735 cycles

INSPECTION TYPE:C2 L24 AT RT WHEEL WELL HAS APP 2 INCH CRACK AT FS 980. VERIFIED CRACK WITH HFEC IAW DC8 SRM 06-10-01-001. STOPPED DRILLED CRACK END IAW DC8 SRM 53-2-3. FABBED REPAIR ANGLE AND SHIM IAW DC8 SRM 53-2-3. ALODINED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED REPAIR PART TO A/C IAW DC8 SRM 53-2-3 AND 51-1-20D, SEALED REPAIR TO A/C IAW DC8 SRM 53-2-3 & 51-1-14.

Part: SEAT TRACK — GOUGED (COCKPIT) · airframe 66,183 hrs · 43,735 cycles

INSPECTION TYPE:C2, 1ST OFFICERS SEAT BOTH LOWER AFT GUIDE RAILS GOUGED. REMOVED WORN GUIDE RAILS, INSTALLED RAILS P/N 4657562-501 AND 4657562- 502 WITH SCREWS AND NUTS IAW DC8 SRM 51-3-0.

Part: SKIN — CORRODED (FUSELAGE) · airframe 66,183 hrs · 43,735 cycles

INSPECTION TYPE:C2, FUSELAGE EXTERIOR STA 1766 L21L-L23L SKIN IS BULGED AND RIVETS PULLING. REMOVED FASTENERS IAW DC8 SRM 51-1-21, CHECKED AREA FOR CORROSION, NONE FOUND AT THIS TIME. LONGERON FITTING FOUND TO BE CORRODED OUT OF LIMITS IAW DC8 SRM 53-2-0. LOCATED AND DRILLED NEW FITTING IAW DC8 SRM 51 -1-24. INSTALLED NEW FITTING AND FASTENERS IN SKIN IAW DC8 SRM 51-1-21.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMER EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT BATT PACK, OPS CK GOOD. (P/N 5708458-503), (S/N FTL070) ON, (S/N 1146) OFF.

Part: FITTING — CRACKED (BS 1140)

INSPECTION TYPE-D, INTERCOSTAL AFT END FITTING FOUND TO BE CRACKED AT FWD SIDE OF FS 1140 FRAME AT LONG 33R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 200)

INSPECTION TYPE:D STA 200 AT STR 27L, THE FLOORBEAM SUPPORT FITTING IS CORRODED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3773077 AND SRM 51-1-20D.

Part: ANGLE — CRACKED (WS 250.089)

INSPECTION TYPE:D LT WING L/E AT STA XS 250.089, THE VERTICAL STIFFNENER ANGLE IS CRACKED AT THE LWR END. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5769859 AND SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1540)

INSPECTION TYPE:D STA 1540, LONG 33L IS CORRODED. REMOVED DAMAGED SECTION OF LONGERON AND REPLACED SECTION IAW SRM 53-5-0.

Part: SPLICE — CRACKED (BS 600-620)

INSPECTION TYPE-D, FS 600 TO 620 STR 31R SPLICE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1228)

INSPECTION TYPE:D STA 1228 AT LONG 19R, THE FRAME TIE FITTING IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: WEB — CORRODED (BS 1180-1200)

INSPECTION TYPE-D, STA 1180-1200 AT LONG 34R, THE TORQUE BOX WEB HAS HEAVY CORROSION. REPAIRED AREA IAW DC8-5350-7876-A.

Part: FITTING — CRACKED (BS 440-460)

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

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE:D STA 680 AT RBL 24, THE FLOORBEAM ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 5773275 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 857)

INSPECTION TYPE:D LONGERON 4L END FITTING CRACKED JUST FWD OF F/S 857. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-20D.

Part: FITTING — CRACKED (BS 759)

INSPECTION TYPE:D INTERCOSTAL END FITTING AT LONG 13L JUST AFT OF STA 759 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 3779978 AND SRM 51-1-20D.

Part: INTERCOSTAL — CRACKED (BS 1520)

INSPECTION TYPE-D, FS 1520 LONGERON 33R INTERCOSTAL HAS CRACK. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-1-20D.

Part: LONGERON — CORRODED (BS 1480-1500)

INSPECTION TYPE:D STA 1480-1500, STR 32L HAS HEAVY CORROSION ON INNER FLANGE. REMOVED AND REPLACED SECTION OF LONGERON IAW SRM 53-2-2 FIG 10.

Part: JAMB — CRACKED (CARGO DOORWAY)

INSPECTION TYPE-D, APPROX .25 INCH CRACK NOTED AT UPPER FORWARD DOOR JAMB CORNER OF AFT CARGO DOOR. REPAIRED IAW SRM 53-2-0 FIG 21.

Part: FITTING — CRACKED (BS 902)

INSPECTION TYPE:D LONG 10L END FITTING CRACKED JUST AFT OF STA 902. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D.

Part: ANGLE — CORRODED (BS 25-70)

INSPECTION TYPE:D STA 25-70 AT RBL 54, THE CUSP WEB HAS HEAVY CORROSION. REMOVED CORRODED AREA AND SPLICED IN NEW AREA IAW SRM 53-2-0 FIG 1B.

Part: FITTING — CRACKED (BS 1325)

INSPECTION TYPE:D LT LWR CUSP FITTING CRACKED AT STA 1325. REMOVED, FABRICATED, AND REPLACED FITTING IAW DAC DWG 9755584 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1240)

INSPECTION TYPE-D, INTERCOSTAL END FITTING CRACKED STA 1240 AT LONG 35L. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.

Part: SPLICE — CRACKED (BS 1260-1280)

INSPECTION TYPE-D, LONG 33L SPLICE FITTING CRACKED FS 1260 TO 1280. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT FITTING IAW SRM 51-1-21 AND DWG 3759220.

Part: SPLICE — CRACKED (BS 1040-1060)

INSPECTION TYPE-D, LONG 31R SPLICE FITTING CRACKED FS 1040 TO 1060. REMOVED AND REPLACED FITTINGS IAW SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1050)

INSPECTION TYPE:D HEAVY CORROSION ON STA 1050 BUTT SPLICE ATTACH FITTING AT LONG 31. REMOVED AND REPLACED FITTING IAW DWG 4779940 AND SRM 51-1-20D.

Part: FITTING — CRACKED (BS 1280)

INSPECTION TYPE:D LT LWR CUSP FITTING CRACKED STA 1280. REMOVED AND REPLACED FITTING IAW SRM 51-3-0.

Part: FITTING — CORRODED (BS 1220)

INSPECTION TYPE:D HEAVY CORROSION ON TORQUE BOX VERTICAL SUPPORT ANGLE STA 1220 AT LONG 27L. REMOVED, FABRICATED, AND REPLACED FITTING IAW DAC DWG 9754002 AND SRM 51-1-20D.

Part: LONGERON — CRACKED (BS 1260-1280)

INSPECTION TYPE:D STA 1260-1280, LONGERON 36 IS CRACKED. REPAIRED AREA IAW DHC SK755-547.

Part: INTERCOSTAL — CRACKED (BS 1480-1500)

INSPECTION TYPE:D STA 1480-1500 AT LONG 2L, THE INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND REPLACED INTERCOSTAL IAW DWG 5704908 AND SRM 51-1-20D.

Part: FITTING — CORRODED (BS 1180)

INSPECTION TYPE:D STA 1180 AT LONG 34R, THE SHEAR TIE FITTING HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3755841 AND SRM 51-1-20D.

Part: SKIN — CRACKED (WS 341.5)

INSPECTION TYPE-D, RT WING L/E SKIN (LWR) AT WS XFS 341.5 HAS NUMEROUS CRACKS. REPAIRED IAW UPS EO DC8-5720-4087-B.

Part: RIB — CRACKED (WS 653.75)

INSPECTION TYPE-D, RT WING L/E AT STA XFS653.750, THE UPPER L/E RIB IS CRACKED AT THE AFT END. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.

Part: RIB — CRACKED (WS 822.5)

INSPECTION TYPE-D, RT WING L/E AT WS XFS 822.500 THE UPPER L/E RIB IS CRACKED AT THE AFT END. REPAIRED IAW SRM 57-3-1.

Part: RIB — CRACKED (WS 297.5)

INSPECTION TYPE-D, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER AT WS XFS 297.500. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 697.5)

INSPECTION TYPE-D, LT WING L/E RIB LWR ARM CRACKED WS XFS 697.5. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 283.25)

INSPECTION TYPE-D, LT WING L/E RIB LWR ARM CRACKED BY AFT FASTENER AT WS XFS 283.250. REPAIRED IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 576.75)

INSPECTION TYPE-D, LT WING L/E RIB UPPER ARM CRACKED BY AFT FASTENER WS 576.75. REPAIRED IAW SRM 57-2-0.

Part: SKIN — CRACKED (WS 74)

INSPECTION TYPE-D, LT WING UPPER SKIN HAS 2 CRACKS JUST I/B OF WS XRS 74 FWD AND AFT LEG OF STR 11. REPAIRED IAW SRM 57-3-1.

Part: SKIN — CRACKED (WS I6.225)

INSPECTION TYPE-D, LT WING L/E LWR SURFACE CRACKED AT WS XOLDI 6.225 ON SKIN. REPAIRED IAW UPS EO 5720-4087 APPN C.

Part: ANGLE — CRACKED (BS 680)

INSPECTION TYPE:D STA 680 AT LBL24, THE FLOORBEAM SUPPORT ANGLE IS CRACKED. REMOVED, FABRICATED AND REPLACED ANGLE IAW DWG 5773275 AND SRM 51-1-20D.

Part: SKIN — CORROSION (WS 304)

INSPECTION TYPE-D, RT WING L/E TOP SKIN AT WS XFS 304.0 FRONT SPAR HAS HEAVY CORROSION, UNDER THE SURFACE. REPAIRED IAW DHC SK 755-816.

Part: FITTING — CORRODED (BS 1160)

INSPECTION TYPE:D STA 1160 AT STR 35R, THE TORQUE BOX FITTING HAS HEAVY CORROSION. REMOVED, FABRICATED AND REPLACED FITTING IAW SRM 53-2-0 FIG 2D.

Part: SKIN — CRACKED (CARGO DOORWAY)

INSPECTION TYPE-N/A, FOUND SKIN BULGED AND CRACKED 2 INCHES FWD OF NR 4 PIT DOOR LOWER FWD CORNER DOUBLER. ALSO, BULGE IN SKIN WITH RIVET PULLED THROUGH AFT CORNER NR 4 PIT DOOR SCUF GAURD AREAS MARKED. NR OPENED AGAINST THIS ITEM. COMPLETED NON ROUTINE 725601, INSTALLED NEW SKIN AS PER EO DC8-5330-10049A.

Part: SUPPORT FRAME — CRACKED (CARGO DOORWAY)

INSPECTION TYPE-N/A, STEP PLATE SUPPORT FRAME IS CRACKED IN 3 PLACES AT NR 4 PIT DOOR OPENED FOR OTHER MAINT, SEE CONTROL ITEM UPS98826172. TRANS TO N\R CARD 75992. FABRICATED NEW CHANNEL SUPPORT FRAME AND INSTALLED PER SRM 53-1-0 COMPLETED NON-ROUTINE 725592.

Part: LONGERON — CORRODED (BS 70-190)

INSPECTION TYPE-C, LONG 35L CORRODED BEYOND LIMITS, STA 70 TO 188. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SECTION FROM STA 70 TO 190 PER SRM 51-1-20 AND SRM 51-1-21.

Part: FITTING — CRACKED (BS 1756)

INSPECTION TYPE-C, TAIL SKID FWD SUPPORT FITTING IS CRACKED AT STA 1756. REPLACED FITTING IAW SRM 51-1-20 AND 51-3-0.

Part: RIB — CRACKED (WS 424.5)

INSPECTION TYPE-C, LT WING L/E RIB CRACKED AT LOWER AFT END XFS 424.5. REPAIRED IAW SRM 57-2-0 FIG 2.

Part: LONGERON — CORRODED (BS 100-190)

INSPECTION TYPE-C, LONG 36L HAS CORROSION STA 100 TO 190. REMOVED, FABRICATED AND INSTALLED REPLACEMENT LONGERON IAW SRM 51-1-21 AND 53-4-1 FIG 28.

Part: DOUBLER — CORRODED (BS 70-190)

INSPECTION TYPE-C, BELLY SKIN FINGER DOUBLERS 4 EA CORRODED STA 70 TO 190 STR 31R, 31L. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLERS IAW SRM 53-4-1. INSTALLED ON N/R 532668.

Part: SKIN — CORRODED (VERT STAB)

INSPECTION TYPE-C, VERT STAB LE RT CORROSION BLEND OUT IS BEYOND LIMITS, ZFS 140. REMOVED DAMAGE, FABRICATED FILLER, DOUBLER AND INSTALLED IAW SRM 55-2-1, 55-30-01 AND 51-1-11.

Part: LONGERON — CRACKED (BS 1540)

INSPECTION TYPE-C, LONGERON 35R CRACKED AT FASTENER HOLE STA 1540. FABRICATED REPAIR PARTS AND INSTALLED STA 1490 TO 1550 IAW SRM 53-2-2 FIG 10.

Part: ANGLE — CRACKED (LT STUB WING)

INSPECTION TYPE-D, LT STUB WING L/E ABOVE NR 1 ENG PYLON INBD ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW DWG 9753297, SRM 57-3-1 AND 51-1-21.

Part: LONGERON — CRACKED (BS 1626)

INSPECTION TYPE-C, LONGERON 23L CRACKED AT FASTENER HOLE FS 1626. REMOVED, FABRICATED SPLICE SECTION AND INSTALLED IAW SRM 53-2-2 AND 51-1-21.

Part: FITTING — CRACKED (BS 8)

INSPECTION TYPE-C, END FITTING CRACKED AT FS 8 LONG 33R. REMOVED AND REPLACED FITTING IAW SRM 51-1-30 AND 51-1-21.

Part: WEB — CRACKED (FS 759)

INSPECTION TYPE-C, WEB CRACKED AT LBL 60 FS 759 WING TO BODY FAIRING STRUCTURE UNDER SIDE. REPAIRED IAW SRM 53-8-1 AND UPS EO DC8-5350-7876A.

Part: FITTING — CRACKED (BS 1690)

INSPECTION TYPE: C. END FITTING CRACKED AT LONGERON 34R STA 1690. REMOVED AND REPLACED FITTING IAW SRM'S 51-1-21 AND 51-1-20D.

Part: LONGERON — CORRODED (BS 1560)

INSPECTION TYPE: C. LONGERON 33R CRACKED AND CORRODED F.S. STA 1560. REMOVED, FABRICATED AND INSTALLED IAW SRM 53-2-2 FIG 10 AND 53-4-1.

Part: SHEAR TIE — CRACKED (BS 25)

INSPECTION TYPE: C. SHEAR TIE CRACKED IN RADIUS STA 25 BETWEEN STR 34R AND 35R. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IAW SRM'S 51-9-0 FIG 68, 53-2-0, 51-1-21, 51-1-20D, AND 53-3-1 FIG 3.

Part: INTERCOSTAL — CRACKED (BS 1520-1540)

INSPECTION TYPE: C. INTERCOSTAL CRACKED ON UPPER FLANGE NUTPLATE HOLE, STA. 1520 STR 33R. REMOVED DAMAGED AREA, FABRICATED REPAIR PER SRM 53-2-0 AND INSTALLED PER SRM 51-1-21.

Part: FRAME — CORRODED (BS 1360)

INSPECTION TYPE-C, CORROSION ON FWD SIDE OF FRAME AT STA 1360 LONGERON 36 FOUND TO BE OUT OF LIMITS ON N/R 532554. FABRICATED FILLER AND FRAME SECTION REPAIR AND INSTALLED IAW SRM 53-2-0, 51-1-20, AND 51-1-21.

Part: SKIN — CORRODED (BS 70-190)

INSPECTION TYPE-C, BELLY SKIN FS 70 TO 190 LONG 31R TO 31L EXCESSIVE CORROSION. REMOVED AND REPLACED BELLY SKIN IAW SRM 51-1-21.

Part: SHEAR TIE — CRACKED (BS 25)

INSPECTION TYPE-C, STA 25 SHEAR TIE BETWEEN 35L AND 36L HAS CRACK IN RADIUS. REPAIRED IAW SRM 53-2-0 FIG 2B.

Part: SHEAR TIE — CRACKED (BS 25)

INSPECTION TYPE: C. SHEAR TIE CRACKED IN RADIUS STA 25 BETWEEN STR 34R AND 35R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE IAW SRM'S 51-9-0 FIG 68, 53-2-0 FIG 2B, 51-1-21, 51-1-20D, AND 53-3-1 FIG3.

Part: LONGERON — CRACKED (BS 8-36)

INSPECTION TYPE-C, LONG 36 STA 8-36 IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT PART IAW DWG 5613862, SRM 51-1-20, 51-1-21 AND 51-2-0.

Part: TEE CHORD — CORRODED (COCKPIT)

INSPECTION TYPE-C, FLOOR SUPPORT T-CHORD BEHIND EPC PANEL HAS HEAVY CORROSION. FABRICATED AND INSTALLED REPLACEMENT PART IAW 51-1-20D AND 51-21-1.

Part: DOUBLER — CORRODED (BS 1746-1781)

INSPECTION TYPE-C, AFT BELLY SKIN INTERNAL DOUBLER CORRODED BEYOND LIMITS FS 1746 TO 1781. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-1-0, 51-1-8, 51-1-21 AND DWG 5649329.

Part: TEE CHORD — CORRODED (BS 1756-66)

INSPECTION TYPE: C. TEE CHORD STA 1756-1766 IS CORRODED BL ZERO. REMOVED, FABRICATED REPLACEMENT T-CHORD PER DWG 5755032 AND SRM 51-1-21.

Part: FITTING — CORRODED (BS 1766)

INSPECTION TYPE: C. STR END FITTING CORRODED BEYOND LIMITS LONGERON 32L STA 1766. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: SKIN — CORRODED (BS 1650-1690)

INSPECTION TYPE: C. F.S.1650-1690 STR 28L - 33L. INTERNAL TRIPLER IS CRACKED AND CORRODED. FABRICATED TRIPLER IAW DWG 5615377 AND SRM 53-5-1. INSTALL ON NR 532102.

Part: FITTING — CRACKED (BS 680)

INSPECTION TYPE: C. STA 680 BELOW FLOOR RT SIDE AT RBL 63, FUEL TANK TO FRAME TIE FITTING CRACKED. REMOVED AND REPLACED IAW SRM'S 51-1-20D, 53-1-0 AND 51-1-12.

Part: DOUBLER — CORRODED (BS 1690-1766)

INSPECTION TYPE-C, FINGER DOUBLER CORRODED BEYOND LIMITS AT FS 1690 TO 1766 STR 30R. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-5-1 AND 51-1-21.

Part: SKIN — CRACKED (BS 1720)

INSPECTION TYPE-C, FUSELAGE SKIN CRACKED JUST ABOVE BUTT SPLICE LT SIDE AT STA 1720 LONGERON 17L. REMOVED DAMAGED AREA AND INSTALLED REPAIR DOUBLER IAW SRM 53-2-1 FIG 7 SHT 5.

Part: FITTING — CORRODED (BS 1766)

INSPECTION TYPE: C. STR END FITTING CORRODED BEYOND LIMITS, LONGERON 30R, STA 1766. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: FITTING — CORRODED (BS 1766)

INSPECTION TYPE: C. STR END FITTING CORRODED BEYOND LIMITS LONGERON 32R STA 1766. REMOVED AND REPLACED END FITTING IAW SRM 51-1-21.

Part: DOUBLER — CORRODED (BS 800-900)

INSPECTION TYPE: C. STA 880-900 RBL 59-65 FINGER DOUBLER HAS HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW DWG 5645332, SRM'S 53-7-1 FIG 10, 51-1-21, 51-1-11.

Part: DOUBLER — CORROSION (BS 880-900)

INSPECTION TYPE: C. STA 880-900 RBL 59-65 FINGER DOUBLER HAS HEAVY CORROSION. REMOVED DOUBLER, FABRICATED AND INSTALLED DOUBLER IAW DWG 5645332, SRM 53-7-1 FIG 10, 51-1-21, 51-1-11.

Part: SPLICE — CRACKED (BS 380-400)

INSPECTION TYPE: C. STR SPLICE FITTING CRACKED STA 380-400 STR 31L. REMOVED AND REPLACED FITTING IAW SRM'S 51-1-20D AND 51-1-8.

Part: BRACKET — CRACKED (BS 1614)

INSPECTION TYPE: C. FRAME SUPPORT BRACKET CRACKED STA 1614 STR 21L. REMOVED, FABRICATED AND INSTALLED FITTING IAW SRM'S 51-1-0, 51-1-20 AND 51-1-3.

Part: SHEAR TIE — CORRODED (BS 1020)

INSPECTION TYPE-C, SHEAR TIE AT STA 1020 BETWEEN STR 34 TO 35R IS CORRODED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE IAW SRM 53-4-1 AND SRM 51-1-20D.

Part: SHEAR TIE — CRACKED (BS 1060)

INSPECTION TYPE-C, SHEAR TIE STA 1060 BETWEEN STR 36L TO 35L IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PER SRM 53-2-0.

Part: FITTING — CORRODED (BS 1766)

INSPECTION TYPE: C. LONGERON END FITTING CORRODED BEYOND LIMITS STA 1766 L-30L. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.

Part: SKIN — CORRODED (BS 1692)

INSPECTION TYPE-C, FUSELAGE SKIN AT STA 1692 LONGERON 30L HAS CORROSION. CUT OUT DAMAGED AREA AND INSTALLED REPAIR IAW SRM 53-2-1 FIG 7.

Part: TIE FITTING — CRACKED (BS 922)

INSPECTION TYPE-C, STA 922 LBL 62 PRESSURE PANEL TO FUSELAGE TIE FITTING IS CRACKED AT BOTTOM. REPLACED FITTING PER SRM 51-1-20D, 53-1-0, 51-3-0.

Part: CARGO TRACK — CORROSION (NR 1 CARGO PIT)

INSPECTION TYPE: C. NR 1 CARGO PIT LT FORWARD CARGO TRACK AND SPLICE HAVE HEAVY CORROSION. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK AND SPLICE IAW DWG. 5759223 AND SRM 53-1-0.

Part: SPLICE — CRACKED (BS 200-220)

INSPECTION TYPE: C. STA 200-220 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED SPLICE FITTING IAW 51-1-21.

Part: SPLICE — CRACKED (BS 440-460)

INSPECTION TYPE: C. STA 440-460 STR 31L SPLICE FITTING IS CRACKED. REMOVED AND REPLACED SPLICE FITTING PER SRM'S 51-1-21, 51-3-00, 51-1-11.

Part: SKIN — CORRODED (LT HORIZ STAB)

INSPECTION TYPE-C, THE LT HORIZ STAB L/E SKIN SURFACE AT STA XFS178.75 HAS EXFOLIATED CORROSION AROUND SCREW HEAD. REMOVED DAMAGED SKIN SECTION IAW SRM 55-21-1 FIG 4. FABRICATED FILLER, DOUBLER AND INSTALLED IAW SRM 55-2-1 FIG 4.

Part: FITTING — CRACKED (BS 720)

INSPECTION TYPE: C. STA 720 FRAME RT SIDE BELOW FLOOR, FRAME FITTING CRACKED AT BOTTOM. REMOVED, FABRICATED AND INSTALLED REPLACEMENT FITTING IAW DHC SK-755 -575. REF. (UPS ENRG FILE NR DC8-53-1757) AND DWG 3616947.

Part: RIB — CRACKED (WS 641)

INSPECTION TYPE: C. RIGHT WING L/E RIB CRACKED AT AFT UPPER END STA XFS 641.00. REPAIRED RIB IAW SRM 57-2-0.

Part: RIB — CRACKED (WS 746)

INSPECTION TYPE: C. RIGHT WING L/E AT STA XPS 746.00 L/E RIB IS CRACKED AT AFT UPPER END REPAIRED RIB IAW 57-2-0.

Part: SKIN — CORRODED (BS 1680-1890)

INSPECTION TYPE: C. AFT BELLY SKIN FROM STA 1680-1890 LONGERON 28L-28R. CORRODED OUT OF LIMITS. REMOVED AND REPLACED AFT BELLY SKIN IAW SRM'S 51-1-21, 51-1-20D AND DWG 5649329.

Part: SKIN — CRACKED (WS 343.3)

INSPECTION TYPE: C. LEFT WING L/E LOWER SURFACE, AT STA XFS343.3. SKIN IS CRACKED IN 2 PLACES. REPAIRED PER SRM ADDENDUM DC8-5720-4087-B.

Part: RIB — CRACKED (WS 585)

INSPECTION TYPE: C. LEFT WING OUTBOARD L/E RIB AT STA XFS585.0 IS CRACKED AT THE AFT UPPER END. REPAIRED CRACK IAW SRM 57-2-0.

Part: SKIN — CRACKED (WS 424.5)

INSPECTION TYPE-C, LT WING L/E SKIN AT STA 424.5 IS CRACKED AT FASTENER HOLE. CRACK IS .68 LONG. REPAIRED IAW UPS EO DC8-5720-4087-C.

Part: SKIN — CORRODED (BS 21-70)

INSPECTION TYPE-C, FWD SKIN FROM STA 21 TO 70 CORROSION OUT OF LIMITS. REPLACED SKIN PER UPS EO DC8-5330-8942-B.

Part: FITTING — CORRODED (BS 1560)

INSPECTION TYPE: C. LONGERON 33R TIE FITTING AFT OF STA 1560 HEAVILY CORRODED. REMOVED AND REPLACED FITTING IAW SRM'S 53-1-0 AND 51-1-21.

Part: CARGO TRACK — CORRODED (BS 1078-1140)

INSPECTION TYPE: C. C-3 LOWER CARGO PIT LT FORWARD FLOOR TRACK CORRODED 2 EACH PLACES. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK FROM STA 1078 TO 1140 IAW SRM'S 53-2-3 AND 57-3-0.

Part: FITTING — CRACKED (ENTRY DOOR)

INSPECTION TYPE: C. LEFT AFT ENTRY DOOR FORWARD END UPPER SUPPORT FITTING CRACKED. REMOVED, FABRICATED AND INSTALLED SUPPORT FITTING IAW SRM'S 51-1-20, 51-1-8, DAC DWG 9751065-30.

Part: CARGO TRACK — CORRODED (BS 75-165)

INSPECTION TYPE: D. NR 1 PIT FORWARD RT CARGO TRACK HAS HEAVY CORROSION AT FORWARD END. REMOVED AND REPLACED TRACK STA 75 TO 165 PER SRM 53-11-1.

Part: DOUBLER — CORRODED (BS 1620-1640)

INSPECTION TYPE: C. INTERNAL DOUBLER STA 1620-1640 BETWEEN L-29L AND 30L HEAVILY CORRODED. REMOVED, FABRICATED AND INSTALLED DOUBLER PER SRM'S 51-1-8 AND 51-1-21.

Part: CARGO TRACK — CORROSION (NR 4 CARGO PIT)

INSPECTION TYPE-C, C-4 CARGO PIT RT AFT FLOOR TRACK HAS HEAVY CORROSION AND CRACKING. REMOVED, FABRICATED AND INSTALLED REPLACEMENT TRACK IAW SRM 51-3-0, 51-1-20 AND DWG 5759223.

Part: CARGO TRACK — CORROSION (BS 1330-1500)

INSPECTION TYPE: C. C-4 CARGO PIT RT FORWARD CARGO TRACK HAS CORROSION IN TRACK AREA THE ENTIRE LENGTH STA 1330-1500. REMOVED, FABRICATED AND INSTALLED TRACK IAW DWG 5753229 AND SRM 51-3-0.

Part: SPLICE — CRACKED (BS 400-420)

INSPECTION TYPE: C. STA 400-420 STR 31L SPLICE FITTING IS CRACKED ON LOWER LEG. REPLACED SPLICE FITTING IAW SRM'S 53-1-0 AND 51-1-20D.

Part: OUTFLOW NOZZLE — CORRODED (AFT FUSELAGE)

INSPECTION TYPE-C, CABIN AIR DUCT OUTLET DOOR FITTING ASSY HAS HEAVY CORROSION AROUND MOUNT BOLTS. REMOVED AND REPLACED VALVE OUTFLOW NOZZLE IAW M/M 21-31-04.

Part: DOUBLER — CORRODED (BS 8-20)

INSPECTION TYPE-C, STA 8-20 BETWEEN STR 31R TO 32R FINGER DOUBLER IS CORRODED. FABRICATED FINGER DOUBLER IAW DWG 5613862, REF N/R 532214 FOR INST.

Part: DNLOCK SWITCH — INOPERATIVE (LT MLG)

CREW REPORTED, GEAR LOWERED ON APPROACH, MAIN GREEN LIGHT DID NOT ILLUMINATE. GEAR HAD TO BE CYCLED TWO TIMES TO GET ILLUMINATION. REPLACED LEFT MLG DOWNLOCK SWITCH, SWUNG GEAR SEVERAL TIMES, OPERATED NORMAL MM 32-60-00.

Part: DNLOCK SWITCH — DIRTY (LT MLG)

CREW REPORTED, LOWERED LANDING AT BDC AND DID NOT GET GREEN LIGHT FOR LEFT MLG. CYCLED GEAR, NO CHANGE. CHANGED BULBS, NO CHANGE. CYCLED GEAR AGAIN AND GOT NORMAL INDICATION. CLEANED GEAR DOWNLOCK SWITCH, CLEANED TERMINALS.

Part: CONNECTOR — LOOSE (NLG)

ON DEPARTURE FOR CLEVELAND, PILOT REPORTED THAT ON UPLATCH CHECK, NOSE EXTENSION W/GEAR NOT LATCHED LIGHT ILLUMINATED. UPLATCH CHECK PASSED ON THIRD ATTEMPT. MAINTENANCE FOUND THE PLUG NOT LATCHED ON SW LOOSE. RESECURED, LUBED NOSE GEARS AS A PRECAUTION. CHECKED PER MM 32-60-00, PAGE 201.

Part: CONNECTOR — LOOSE (NLG)

WHILE ON DEPARTURE FOR CLEVELAND, PILOT REPORTS ON UPLATCH CHECK, NOSE EXTENDED WITH GEAR NOT LATCHED LIGHT ILLUMINATED. UPLATCH CHECK PASSED ON 3RD ATTEMPT. PLUG NOT LATCHED ON SW. RESECURED, LUBED NOSE GEAR AS A PRECAUTION. CHKED PER MM 32-60-00, PG 201.

Part: FITTING — CORROSION (FS 340)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 6 LOWER T-LOCK FITTING CORROSION REMOVAL OUT OF LIMITS. REPLACED FITTING PER SRM 51-1-20D.

Part: SKIN — CRACKED (WS 304)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING LEADING EDGE INNER SKIN CRACKED .50 INCH LONG AT STA XFS 304. REPAIRED SKIN PER UPS E.O. DC8-57-0593.

Part: SKIN — CORRODED (FS 220-340)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION BULGES ON FUSELAGE SKIN FS 220-340, LONGERONS 34R-36. REPLACED BELLY SKIN PANEL FROM FS 190-450 PER DAC DRAWING 5755271.

Part: LONGERON — CORRODED (FS 240-360)

WHILE IN FOR C-CHECK, MAINTENANCE FOUND HEAVY CORROSION AT 3 EACH LONGERONS. LONGERON 34R, FS 240-360. LONGERON 35R, FS 260-360. LONGERON 36, FS 250-330. REPLACED LONGERON SECTIONS PER SRM 51-1-20D.

Part: FITTING — CORROSION (FS 390)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND LONGERON FITTING HAS HEAVY CORROSION FS 390, LONGERON 36. REPLACED FITTING PER SMR 51-1-20D.

Part: FRAME — CRACKED (FS 380)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND BELT FRAME AT FS 380, LONGERON 33L TO 34L CRACKED 3 INCHES LONG. REPAIRED FRAME PER SRM 53-2-0.

Part: FRAME — CRACK (FS 220-240)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND 2 BELT FRAMES CRACKED AT FS 220 AND 240, BETWEEN LONGERONS 334 TO 34R. REPAIRED FRAMES PER SRM 53-2-0.

Part: VANE — DELAMINATION (LT TE FLAP)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND LT WING TRAILING EDGE INBD FLAP, INBD FLAP VANE DELAMINATED ON LOWER SURFACE. REPLACED VANE ASSY PER MM 27-51-14.

Part: FLOORBEAM — CRACK (FS 340)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND FLOORBEAM END FITTING CRACKED AT FS 340, LONGERON 21 RT. REPLACED FITTING PER SRM 51-1.

Part: DOUBLER — CRACKED (FS 450)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND FS 450 FINGER DOUBLER CRACKED BETWEEN LONGERONS 31L AND 31R. REPLACED DOUBLER PER SRM 51-1-21.

Part: LE RIB — CRACK (RT WING)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND RT WING LEADING EDGE RIBS, 3 EA CRACKED AT WS XFS 346, XFS 397 UPPER, AND XFS 416 UPPER. REPAIRED RIBS PER SRM 57-2-0.

Part: VANE — DELAMINATION (RT TE FLAP)

WHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND RT WING NR 4 FLAP VANE DELAMINATED ON INBD LOWER SURFACE. REPLACED VANE ASSY PER MM 27-51-14.

Part: DOOR JAMB — CRACK (FS 1660)

WHILE IN 'B' CHECK MAINTENANCE REPORTED LT AFT SERVICE DOOR AFT UPPER CORNER OF FUSELAGE CUTOUT STA 1660-6 CRACKS COMING FROM FASTENER HOLES. REPAIRED PER EO DC8-5330-4067-A. DOOR JAMB CORNER DAMAGE - TEMP REPAIR.