N604BX

Part: ENGINE — FAILED (NR 2)

DURING TAKEOFF ROLL NR 2 ENGINE COMPRESSOR STALLED 3 TIMES. ABORTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. FOUND N1 SEIZED. REPLACED NR 2 ENGINE IAW J/C 7004, 7005, 7104, AND 7104. RAN ENGINE IAW ERH 70.01. OPS CHECKED GOOD. REJECTED TAKEOFF WAS PERFORMED, NO DAMAGE NOTED IAW GMM 3.124. ACFT WAS RETURNED TO SERVICE.

Part: LINK — FAILED (MLG DOOR) · airframe 92,107 hrs · 31,463 cycles

AFTER TAKEOFF, THE CREW HEARD A LOUD NOISE FROM NOSE GEAR AREA, THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX FOUND RT NOSE GEAR DOOR OPENED, NO FURTHER DEFECTS NOTED. THEY REPLACED RT FWD NOSE GEAR LINK. OPS CHECK GOOD IAW MM 32-22-1. ACFT WAS RETURNED TO SERVICE.

Part: FUEL CONTROL — OUT OF ADJUST (NR 4 ENGINE) · airframe 92,078 hrs · 31,442 cycles

DURING CRUISE, NR 4 ENGINE FLAMEDOUT. THE CREW ATTEMPTED RESTART, ENGINE WOULD NOT START. THEY LANDED WITHOUT FURTHER INCIDENT. MX ACCOMPLISHED FAULT TREE 51, CHANGED NR 4 FUEL FILTER, RAN ENGINE AND FOUND FLIGHT IDLE LOW, ADJUSTED FLIGHT IDLE. OPS CHECK GOOD IAW MM 77-11-10, ERH 72.06.2, ERH 70.01.1 AND ERH 70.01.14. ACFT WAS RETURNED TO SERVICE.

Part: VANE — DAMAGED (LWS 247)

(SPUY) LT WING - INBD VANE SLOT WITH ELONGATED HOLES AT STA XS 247.000.

Part: FITTING — CRACKED (LT MLG WW)

(SPUY) LT MLG WW, LT 24L, JOINT FITTNG LWR PART CRACKED .5" AT STA 879.000.

Part: CARGO TRACK — BROKEN (BS 140-160)

(SPUY) MAIN CARGO COMPT - NR 4 SEAT TRACK LUG PLUG BROKEN (STA 140.000- 160.000).

Part: SKIN — DENTED (LT ELEVATOR)

(SPUY) LT HORIZ STAB - ELEVATOR UPPER PLATING DENTED 6" AT STA XE 90.000.

Part: SKIN — CRACKED (NLG DOOR)

NLG - LT AFT DOOR EXTERNAL SKIN CRACKED 1" AND WITH INTERIM REPAIR.

Part: ACCESS DOOR — CRACKED (LT WING)

(SPUY) LT WING - NR505F ACCESS DOOR PLATING SURFACE UPPER PART CRACKED 1".

Part: CARGO TRACK — WORN (CARGO BAY)

(SPUY) MAIN CARGO COMPT - NR 2 SEAT TRACK (03 EA) LUGS WORN AT STA 280.000.

Part: SKIN — CORRODED (RUDDER)

(SPUY) RUDDER LT SIDE PLATING CORRODED AT STA ZR 140.000.

Part: SKIN — DENTED (RT WING TE FLAP)

(SPUY) RT OTBD FLAP T/E PANEL UPPER SKIN WITH (02 EA) DENTS AT STA XF 310.000 AND 320.000.

Part: ACCESS DOOR — CRACKED (CENTER WING)

(SPUY) CTR WING AUX TANK RT SIDE - NR 516 ACCESS DOOR FLANGE WITH (02 EA) CRACKS AROUND STA XCW 23000, S57 AND S58.

Part: CARGO TRACK — CORRODED (BS 857-880)

(SPUY) MAIN CARGO COMPT - NR 2 SEAT TRACK LUGS WORN AND CORRODED (STA 857.000- 880.000).

Part: LONGERON — CORRODED (BS 1700 L34L)

(SPUY) AFT ACCY COMPT L-34L CORRODED AT STA 1700.000 (CORRECTING SOURCE DOCUMENT: CPCP 5600-0551).

Part: FITTING — CORRODED (LT MLG WW)

(SPUY) LT MLG WW - L-24L, JOINT FITTING LWR PART CORRODED AT STA 940.000.

Part: LONGERON — CORRODED (BS 1700 L34L) · airframe 90,739 hrs · 30,862 cycles

DURING ROUTINE C-CHECK INSP, FOUND AFT ACCESSORY COMPARTMENT LONGERON 34 LT CORRODED AT STATION 1700.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED LONGERON SEGMENT. FABRICATED STRAPS. CLEANED, TREATED, PRIMED AREA, STRAPS, AND NEW EXTRUSION. INSTALLED REPAIR PARTS IAW SRM CHAPTER 53-2-2 FIGURE 8, SRM 51-1-8, DC8 SRM 53-2-0, SRM 51-1-8B, SRM 51-1-21, SRM 51-1-20D, AND SRM 51-3-1.

Part: FLANGE — CRACKED (ZONE 100) · airframe 90,739 hrs · 30,862 cycles

DURING ROUTINE C-CHECK INSP FOUND CTR WING AUX TANK RT SIDE NR 516 ACCESS DOOR FLANGE WITH CRACKED AROUND STATION XCW 23000, STRINGER 57 AND STRINGER 58. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING ANGLES AND WEB TO GAIN ACCESS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED EXTERNAL, INTERNAL DOUBLERS, FILLER, ANGLES, WEBS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FORM 8110-3 DATED 05/05/10, DWG ED-5123 DATED 04/22/10, NDT SPM PART 06-10-01-001, SRM 51-1-8B, SRM 51-1-20D, AND SRM 51-3-1.

Part: SEAT TRACK — CORRODED (ZONE 100) · airframe 90,739 hrs · 30,862 cycles

DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 2 SEAT TRACK LUGS WORN AND CORRODED AT STA 857.000 - 880.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED SPLICES. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW SEAT TRACK SEGMENT AND REPAIR PARTS IAW SRM CHAPTER 53-2-3 FIGURE 14, SRM 51-1-8, SRM 53-2-0, SRM 51-1-8B, SRM 53-2-3, SRM 51-1-21, SRM 51-3-0, AND SRM 51-3-1.

Part: SLOT — DAMAGED (LT WING) · airframe 90,739 hrs · 30,862 cycles

DURING ROUTINE C-CHECK INSPECTION FOUND LEFT WING INBOARD VANE SLOT WITH ELONGATED HOLES AT STATION XS 247.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED VANE SLOT. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO DISCREPANCY NOTED. FABRICATED REPAIR DOUBLER, FILLER AND INTERNAL DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 DATED 05/07/10, SEMAN DRAWING ED-5122 DATED 04/26/10, DC8 SRM 51-1-21, NDT SPM PART 06-10-0-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D, SRM 51-1-21, SRM 51-3-0 AND SRM 51-3-1.

Part: SEAT TRACK — BROKEN (ZONE 100) · airframe 90,739 hrs · 30,862 cycles

DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 4 SEAT TRACK LUG PLUG BROKEN AT STA 140.000 -160.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SEAT TRACK. REMOVED DAMAGED AREA. FABRICATED NEW SEAT TRACK SEGEMENT, SPLICES. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS. IAW SRM CHAPTER 53-2-3, FIG 14, SHEET 1, SRM 53-2-3, SRM 53-2-3, SRM 51-2-0, FIG 50, SRM 51-1-8B, SRM 51-1-21, SRM 51-3-0, AND SRM 51-3-1.

Part: SKIN — CORRODED (RUDDER) · airframe 90,739 hrs · 30,862 cycles

DURING ROUTINE C-CHECK INSPECTION FOUND RUDDER LEFT SIDE SKIN CORRODED AT STATION ZR 140.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SRM CHAPTER 55-6-1 FIGURE 1, SRM 55-2-0, DC8 SRM 51-1-8, DC8 SRM 55-2-0, DC8 SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 55-6-1 FIGURE 1 ITEM "A", DPS 4.710 REV "L", DC8 SRM 51-1-9 TR 51-142, SRM 51-1-9A TR 51-141, DPS 1.950 REV "AR" R-1, DC8 SRM 51-1-8B, DC8 SRM 51-1-21 AND SRM 51-1-11.

Part: SKIN — DENTED (HORIZ STAB) · airframe 90,739 hrs · 30,862 cycles

DURING ROUTINE C-CHECK INSPECTION FOUND LEFT HORIZONTAL STABILIZER ELEVATOR UPPER SKIN DENTED AT STATION XE 90.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM CHAPTER 55-6-1 FIGURE 1, DC8 SRM 51-1-21, DC8 SRM 55-4-1 FIGURE 1, DC8 SRM 51-1-9 TR 51-142, SRM 51-1-9A TR 51-141, DPS 1.950 REV "AR" R-1, DC8 SRM 51-1-8B, AND DC8 SRM 51-1-21.

Part: SEAT TRACK — WORN (ZONE 100) · airframe 90,739 hrs · 30,862 cycles

DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 2 SEAT TRACK LUGS ARE WORN AT STA 280.000. REMOVED DAMAGED FASTENERS AS NEEDED TO PERFORM RPAIR. REMOVED DAMAGED AREA. FABRICATED SEAT TRACK, SPLICES, SPLICES. CLEANED, TREATED, PRIMED AREA, AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW SRM CHAPTER 53-2-3 FIGURE 14, SRM 51-3-0, SRM 51-1-21, SRM 51-1-8B, SRM 53-2-3, SRM 51-1-11, AND SRM 51-3-1.

Part: DOUBLER — CRACKED (ZONE 500) · airframe 90,739 hrs · 30,862 cycles

DURING ROUTINE C CHECK INSP, FOUND LT WING NR 505F ACCESS DOOR MATING SURFACE UPPER PART CRACKED. REMOVED CHANNEL AND FASTENERS. REMOVE DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED EXTERNAL REPAIR DOUBLER, INTERNAL REPAIR DOUBLER, AND FILLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM CHAPTER 57-2-1, FIG 36, SRM 51-1-21, SRM 57-2-1, SRM 57-2-1, NDT SPM PART 06-10-01-001, SRM 51-1-8B, SRM 51-1-20D AND SRM 51-3-1.

Part: SKIN — CRACKED (NLG DOOR) · airframe 90,739 hrs · 30,862 cycles

DURING ROUTINE C-CHECK INSP, FOUND LT NLG AFT DOOR EXTERNAL SKIN CRACKED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PART IAW SRM CHAPTER 52-5-1 FIG 1, SRM 51-1-21, SRM 52-1-0 PAGE 1, SRM 51-1-8B, SRM 52-5-1 FIGURE 1 ITEM "A", DPS 4.710 REV "L", SRM 51-1-4, DPS 3.69-5 REV "U", SRM 51-1-8B AND SRM 51-1-11.

Part: FITTING — CRACKED (BS 879 L24L) · airframe 90,739 hrs · 30,862 cycles

DURING ROUTINE C-CHECK INSP FOUND LT MLG WHEEL WELL JOINT FITTING LOWER PART CRACKED AT STA 879.000 LONGERON 24 LT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING, SPLICES, DOUBLER, SHIMS. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-8B. INSTALLED NEW FITTING AND REPAIR PARTS IAW SRM CHAPTER 53-2-0 FIGURE O, SRM 51-1-20D, SRM 53-2-0, SRM 53-2-0 PAGES 41/45/46/51/52, AND SRM 51-3-1.

Part: FITTING — CORRODED (LT MLG) · airframe 90,739 hrs · 30,862 cycles

DURING C-CHECK INSP FOUND LT MLG WHEEL WELL JOINT FITTING LOWER PART CORRODED AT STA 940.000 LONGERON 24 LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED SPLICES, DOUBLER AND SHIMS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FITTING AND REPAIR PARTS IAW SRM CHAP 53-2-0 FIG 8, SRM 51-1-8, SRM 53-2-0, SRM 53-2-0 FIG 8 PAGES 43, 44, 49-53, SRM 51-1-8B, SRM 53-2-0, SRM 51-1-20D, SRM 51-1-11, AND SRM 51-3-1.

Part: WARNING LIGHT — ILLUMINATED (ZONE 700) · airframe 90,671 hrs · 30,827 cycles

DURING CRUISE,THE CREW GOT UNSATISFACTORY UPLATCH CHECK, DOOR NOT LATCH LIGHT ILLUMINATED. THEY CYCLED GEAR, THE DOOR NOT LATCH LIGHT ILLUMINATED THEN GOES OUT INTERMITTENTLY DURING FLIGHT. THEY LANDED WITHOUT FURTHER INCIDENT. THE CREW DEFERRED DOOR LIGHT IAW MEL 32-16-02. MX RAISED ACFT AND PERFORMED NUMEROUS GEAR SWINGS WITH NO DEFECTS. OPS CHECK GOOD IAW MM 32-31. ACFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — BROKEN (NR 1 FIRE WARN) · airframe 90,427 hrs · 30,710 cycles

DURING CLIMBOUT, NR 1 ENG SHORT CIRCUIT LIGHT CAME ON. NR ONE ENG FIRE WARNING WOULD NOT TEST. CREW SHUTDOWN NR 1 ENG AND LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND FOUND LT LWR NINTH STAGE BLEED AIR DUCT BROKEN AT ENG CASE FLANGE AND CORE WIRING HARNESS BURNED. MX REPLACED NR 1 ENG CORE WIRING HARNESS AND LT LOWER NINTH STAGE BLEED AIR DUCT. OPS CHECK GOOD IAW MM 70-30-1 AND 26-10-0.

Part: OXYGEN SYSTEM — LOW · airframe 89,987 hrs · 30,518 cycles

DURING CLIMB OUT, CREW NOTICED OXYGEN REGULATOR AT JUMP SEAT HAD FLOW LEVER IN EMERGENCY POSITION, OXYGEN SYS DEPLETED DOWN TO 75 PSI. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX SERVICED OXYGEN SYS, OPS CHECK GOOD IAW MM 35-10-0. ACFT WAS RETURNED TO SERVICE.

Part: PLUG — MISSING (ENGINE OIL SYS) · airframe 89,553 hrs · 30,344 cycles

DURING CLIMB-OUT FROM KLAX ,THE CREW SHUTDOWN NR 4 ENGINE DUE TO LOST OF OIL QUANTITY. THE CREW LANDED IN KPDX WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED NUMBER FOUR ENGINE AND FOUND THE STARTER SERVICE PLUG OFF. MAINTENANCE INSTALLED SERVICE PLUG AND SERVICED ENGINE AND STARTER. OPERATIONAL CHECK GOOD IAW ATI ERH 70.01.1. AIRCRAFT WAS RETURNED TO SERVICE.

Part: LANDING GEAR — MALFUNCTIONED

DURING TAKEOFF, FLIGHT CREW WAS UNABLE TO RAISE GEAR HANDLE. FLIGHT CREW ACCOMPLISHED CHAPTER 3 PROCEDURES IN COCKPIT OPERATING MANUAL AND RAISED GEAR. GROUND CONTROL RELAY CIRCUIT BREAKER RELAYS WERE OPEN FOR FLIGHT AND RESET AFTER LANDING. AC LANDED UNEVENTFUL. OPEN (K)

Part: STRUT — CONTAMINATED (NLG)

DURING TAKEOFF, FLIGHT CREW WAS UNABLE TO RAISE GEAR HANDLE. FLIGHT CREW ACCOMPLISHED CHAPTER 3 PORCEDURE IN COCKPIT OPERATING MANUAL AND RAISED GEAR. GROUND CONTROL RELAY CIRCUIT BREAKER RELAYS WERE OPEN FOR FLIGHT AND RESET AFTER LANDING. AC LANDED UNEVENTFUL. MAINTENANCE REMOVED NOSE STRUT, FOUND TRASH IN FLUID RETURN REBOUND CHECK VALVE, FLUSHED OUT TRASH, REPACKED, AND REINSTALLED CHECK VALVE. OPS CHECK GOOD IAW MM 32-21-2. AC WAS RETURNED TO SERVICE. (K)

Part: LANDING GEAR — MALFUNCTIONED (ZONE 700) · airframe 88,355 hrs · 29,813 cycles

DURING TAKEOFF FROM GOOY, THE NOSE LANDING GEAR WOULD NOT RETRACT. THE CREW WAS ABLE TO RETRACT NOSE GEAR WITH HANDLE LATCH FLIGHT RELEASE. WHEN NOSE GEAR RETRACTED THE TAKEOFF WARNING HORN SOUNDED, THE CREW PULLED GROUND SHIFT BREAKERS, WHEN THE LEFT BREAKER WAS PULLED THE HORN SOUNDED, PULLED THE RIGHT BREAKER PER PROCEDURE. THE CREW RETURNED TO GOOY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LANDING GEAR LEVER AND ALL SYSTEM CABLES, PULLY, BEARINGS FOR BINDING, LUBRICATED SYSTEM, ISSUED FERRY PERMIT FROM GOOY TO KTOL PER ATI GMM 3.107. FLIGHT LATCH RELEASE MECHANISM WAS USED IAW ATI DC8 COM PROCEDURES FOR GEAR RETRACTION. MAINTENANCE IN KTOL RERIGGED LANDING GEAR LEVER ANTI-RETRACT SYSTEM, OPERATIONAL CHECK GOOD IAW DACO DC-8 MAINTENANCE MANUAL 32-31-0. AIRCRAFT WAS RETURNED TO SERVICE.

Part: LANDING GEAR — MALFUNCTIONED (ZONE 700) · airframe 88,333 hrs · 29,805 cycles

DURING CLIMB-OUT FROM KTOL LANDING GEAR WOULD NOT RETRACT. THE CREW GOT A INFLIGHT INDICATION OF MECHANICAL AND ELECTRICAL GROUND SHIFT FAILURE. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE RAISED THE AIRCRAFT OFF THE GROUND AND PERFORMED NUMEROUS EXTENSION AND RETRACTION OF THE LANDING GEAR. OPERATIONAL CHECK GOOD IAW DACO DC-8 MAINTENANCE MANUAL 32-30 AND DACO 7-10-0. AIRCRAFT WAS RETURNED TO SERVICE.

Part: MECHANISM — OUT OF ADJUST (MLG) · airframe 88,332 hrs · 29,804 cycles

DURING CLIMB-OUT FROM KTOL, THE CREW WAS UNABLE TO RAISE NOSE LANDING GEAR NORMALLY AFTER TAKEOFF. THE CREW ACCOMPLISHED COM PROCEDURE'S, USING THE HANDLE LATCH FLIGHT RELEASE THE NOSE GEAR CAME UP AND LOCKED. WHEN THE GEAR WAS BEING RAISED THE CREW HEARD A GRINDING NOISE, UPLATCH CHECK WAS OK, THE DOOR NOT LATCHED LIGHT CAME ON AT APPROXIMATELY 300KTS. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NOSE GEAR DOOR AND FOUND GROUND SHIFT OUT OF ADJUSTMENT. MAINTENANCE ADJUSTED THE NOSE GEAR GROUND SHIFT AND SPOILER CONTROL. OPERATIONAL CHECK GOOD IAW DACO DC-8 MAINTENANCE MANUAL 32-23-1, DACO DC-8 MAINTENANCE MANUAL 27-60-0, DACO DC-8 MAINTENANCE MANUAL 32-30-0, AND DACO DC-8 MAINTENANCE MANUAL 32-60-0. AIRCRAFT WAS RETURNED TO SERVICE.

Part: DRIVE LINK — BENT (TE FLAPS) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING LINK AT FLAP DRIVE LINK BENT AT STATION 3.000. REMOVED AND REPLACED LEFT WING FLAP DRIVE LINK IAW DC8 MAINTENANCE MANUAL 20-16-0 PAGE 202. PERFORMED OPS CHECK TO ALL FLIGHT CONTROLS. OPERATIONAL CHECK GOOD IAW DC8 MAINTENANCE MANUAL 27-11-0 PAGE 10-14, DC8 27-21-0 PAGE 5-9. DC8 27-30-0 PAGE 4-7, DC8 27-40-0 PAGE 1-2. DC8 27-41-0 PAGE 10-13, DC8 27-51-0 PAGE 11-12, DC8 27-61-0 PAGE 5-7, DC8 27-70-0 PAGE 1-2 DC8 27-80-0 PAGE 4.

Part: LINK — CRACKED (TE FLAPS) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND FLAP MECHANISM OF INNER WING FORWARD LINK CRACKED AT STATION 3.000 RIGHT. REMOVED REPLACED INNER WING FORWARD LINK OF FLAP MECHANISM IAW OHM 27-27-1 PAGE 4. PERFORMED OPS CHECK TO ALL FLIGHT CONTROLS. GOOD IAW DC8 MAINTENANCE MANUAL 27-11-0 PAGE 10-14, DC8 27-21-0 PAGE 5-9. DC8 27-30-0 PAGE 4-7, DC8 27-40-0 PAGE 1-2 DC8 27-41-0 PAGE 10-13, DC8 27-51-0 PAGE 11-12, DC8 27-61-0 PAGE 5-7, DC8 27-70-0 PAGE 1-2 DC8 27-80-0 PAGE 4.

Part: SKIN — MISREPAIRED (ZONE 200) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT FORWARD FUSELAGE FORWARD GALLEY VENT ABOVE R-1 DOOR, RIVET SPACING TOO SMALL AT STATION FS 183.000, LONGERON-10.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACK, NO CORROSION NOTED. FABRICATED INTERNAL, AND EXTERNAL DOUBLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8100-9 DATED 12-10-07, BOEING MESSAGE NUMBER 704498313-4 DATED 10-12-07 AND 1-689890784-4 DATED 11-21-07 AD-2000-20-08, S/B DC8-53-075, DRAWING DOUGLAS SR08530021 AND 5750776, DC8 SRM 51-1-21, 51-1-20D, DC8 SRM 51-1-8B, BOEING MESSAGE NUMBER 1-689890784-4, SEMAN DRAWING ED-4662-1, SRM 53-2-0 FIGURE 14 T/R 53-195 DATED 03-26-04, DC8 NDT SPM PART 08-00-02 TO 07, FORM 242-4, DC-8 SRM 51-1-11, DC-8 SRM AND SRM 51-3-1.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT FORWARD FUSELAGE BELOW AND AFT OF ACM, SPACING TOO LARGE AT STATION FS 8.000 LONGERON-30 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK NO CORROSION NOTED. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLERS. CLEANED, TREATED AND PRIMED AREA REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07569 DATED 11-27-07, SEMAN DRAWING NUMBER ED-4663 DATED 11-24-07, DC8 SRM 51-1-21, 51-1-20D, DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242-4, AND DC8 SRM 51-1-8B.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT FORWARD FUSELAGE ACM AFT LOWER CORNER, SPACING TOO LARGE, AT STATION FS 8.000 LONGERON-30 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK NO CORROSION NOTED. FABRICATED NEW SKIN, INTERNAL, AND EXTENAL DOUBLERS. CLEANED, TREATED AND PRIMED AREA REPAIR PARTS. INSTALLED NEW FASTENERS, AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07578 DATED 12-06-07, SEMAN DRAWING NUMBER ED-4660 DATED 11-22-07, DC8 SRM 51-1-21, 51-1-20D, DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242-4, AND DC8 SRM 51-1-8B.

Part: BULKHEAD — MISREPAIRED (ZONE 100) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND BULKHEAD CAP ANGLES HAS IMPROPER REPAIR AT STATION 70.000 LONGERON-32.5LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED FORWARD FRAME SEGMENT. FABRICATED FRAME SEGMENT, AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07578 DATED 12-06-07, SEMAN DRAWING NUMBER ED-4659 DATED 12-01-07, DC8 SRM 51-3-0, 51-1-21, DRAWING DOUGLAS SR08538006 SRM 53-2-5 FIGURE 2 8C-2 SHEETS 1-2, T/R 53-176 FIG 8C-2 SHEET 2,3,4,5 DATED 09-30-03, DC8 SRM 51-1-8B, AND 51-3-1.

Part: BULKHEAD — MISREPAIRED (ZONE 100) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND BULKHEAD CAP ANGLES HAS IMPROPER REPAIR AT STATION 70.000 LONGERON-32.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED FORWARD FRAME SEGMENT. FABRICATED FRAME SEGMENT, AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07578 DATED 12-06-07, SEMAN DRAWING NUMBER ED-4659 DATED 12-01-07, DC8 SRM 51-3-0, 51-1-21, DRAWING DOUGLAS SR08538006 SRM 53-2-5 FIGURE 2 8C-2 SHEETS 1-2, T/R 53-176 FIG 8C-2 SHEET 2,3,4,5 DATED 09-30-03, DC8 SRM 51-1-8B, AND 51.

Part: SKIN — MISREPAIRED (RUDDER) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT SKIN AT STATION ZR 253.000 TO STATION ZR 271.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLER, BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE TO RUDDER FOUND MOMENT WITHIN TOLERANCE. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-1-21, DC8 SRM 51-4-6 PAGES 1-6, IAW DC8 SRM 55-6-1 FIGURE 1, DC8 SRM 55-1-0 PAGE 1 AND SRM 51-1-21, DC8 SRM 55-6-1 FIGURE 1, ITEM "A", DC8 SRM 51-1-9, T/R NUMBER 51-142 DATED 04-05-06, SRM 51-1-9A T/R 51-141 DATED 04-03-06, AND DC8 SRM 51-1-8B.

Part: SUPPORT — CRACKED (ZONE 500) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE INTERNAL PART SUPPORT HAS A CRACK AT STATION XFS 430.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SUPPORT. CLEANED, TREATED AND PRIMED AREA INSTALLED NEW SUPPORT IAW BOEING MESSAGE NUMBER1-680003043-2 DATED 11-12-07, DRAWING NUMBER 5770409, DC8 SRM 57-1-0 PAGE 1, SRM 51-3-0, 51-1-20D, DC8 SRM 51-1-8B, DC8 SRM 57-2-1 FIGURE 12 SHEET 1,2,3, 51-3-0, 51-9-0 T/R NUMBER 51-108, 51-9-0 T/R NUMBER 51-126, AND SRM 51-3-1.

Part: STRUCTURE — CRACKED (ZONE 600) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING. NUMBER 4 STUB WING LEADING EDGE LOWER PART DOUBLER HAS A CRACK AT STATION XFS 529.000. REMOVED FASTENERS AS NEEDED TP PERFORM REPAIR. REMOVED CRACKED DOUBLER. FABRICATED EXTERNAL, INTERNAL REPAIR DOUBLER. PERFORMED HEAT TREATMENT TO REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW 51-1-20D, 51-3-1 DC8 SRM 57-2-1A FIGURE 1, DC8 SRM 51-1-21, DC8 SRM 51-1-1 PAGES 1, 13, 17, AND DC8 SRM 51-1-8B.

Part: ATTACH ANGLE — CORRODED (STAB TO FUSELAGE) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE TO STABILIZER LEFT ATTACH ANGLE SHOWS CORROSION AT STATION 1754.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGES AREA. FABRICATED ANGLE. PERFORMED HEAT TREATMENT TO ANGLE. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PARTS. INSTALLED REPAIR PARTS SRM IAW 51-1-20D, 51-3-1 DC8 SRM 53-2-5 FIGURE 16A SHEET 1-2, DC8 SRM 51-1-8 PAGE 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 53-2-5 FIGURE 16A SHEET 1-2, DC8 SRM 51-1-6, DC8 SRM AND SRM 51-1-8B.

Part: SUPPORT — CRACKED (ZONE 600) · airframe 87,931 hrs · 29,622 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE INTERNAL PART SUPPORT CRACKED AT STATION XFS 430.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED SUPPORT. FABRICATED SUPPORT CLEANED, TREATED AND PRIMED AREA AND NEW SUPPORT. INSTALLED NEW FASTENERS AND NEW SUPPORT IAW BOEING MESSAGE NUMBER 1-680003043-2 DATED 12-11-07, DRAWING NUMBER 5770409, DC8 SRM 57-1-0 PAGE 1, SRM 51-1-20D, DC8 SRM 51-1-8B, DC8 SRM 57-2-1 FIGURE 12 SHEET 1, 2, AND 3, SRM 51-9-0 T/R 51-108, 51-126 DATED 04-03-00 AND 01-08-03, SRM 51-3-0, 51-1-20D, AND SRM 51-3-1.

Part: VANE — DAMAGED (LT WING TE FLAP) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE OUTBOARD VANE WITH ELONGATED HOLES AT STATION XOLDO 67.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION NOTED. FABRICATED REPAIR DOUBLER. INTERNAL DOUBLER CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07532 DATED 11-08-07, SEMAN DRAWING NUMBER ED-4654 DATED 11-05-07, DC8 SRM 51-1-21, 51-3-0, DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242-4, DC8 SRM 51-1-8B, SRM 51-1-11, 51-1-20D, AND 51-3-1.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT "B" DOOR OUTER SKIN HAS A CRACK, WEAR DAMAGE, AND SEVERAL DENTS AT STATION 480.000 TO STATION 560.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW BOEING MESSAGE NUMBER 1-674365491-2 DATED 11-07-07, DC8 SRM 52-1-0 PAGE 1 AND SRM 51-1-21,SRM 52-4-1 FIGURE 3 ITEM "K", DC8 SRM 51-1-8B, AND DC8 SRM 51-1-21.

Part: FITTING — DAMAGED (BS 879 L21L) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT MISSDRILLED HOLE ON FLANGE OF FRAME FITTING AT STATION 879.000 LONGERON-21 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PLUGGED MISDRILLED HOLE WITH RIVET. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION NOTED. FABRICATED REPAIR ANGLE. CLEANED, TREATED AND PRIMED AREA AND REPAIR ANGLE. INSTALLED NEW FASTENERS AND REPAIR ANGLE IAW FAA FORM 8110-3 NUMBER 07529 DATED 11-09-07, SEMAN DRAWING NUMBER ED-4655 DATED 11-07-07, DC8 SRM 51-1-20D, DC8 SRM 51-1-21,DC8 NDT SPM PART 08-00-02 TO 07, FORM 242-4, DC8 SRM 51-1-8B, AND 51-3-1.

Part: FITTING — CRACKED (ZONE 200) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE A CRACK AT SPLICE FITTING AT STATION 1766.000 LONGERON17 LEFT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-3-0, 51-3-1.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, LEFT HORIZONTAL STABILIZER LEADING EDGE UPPER SKIN SHOWS CORROSION AT STATION XFS 177.750. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION AFTER INSPECTION. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLERS. CLEANED, TREATED AND PRIMED AREA REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FORM FAA 8110-3 NUMBER 07529 DATED 11-09-07 SEMAN DRAWING NUMBER ED-4647 DATED 11-08-07, DC8 SRM 51-1-21, 51-3-0, DC8 SRM 51-1-8 PAGE 17-18, DC8 SRM 55-2-0 PAGE 12, DC8 NDT SPM PART 08-00-0 TO 07, FORM SMN 242-4, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND 51-3-1.

Part: SKIN — CRACKED (ZONE 200) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE FOUND A CRACK AT LONGERON 17 LEFT AT STATION 1769.000. REMOVED CRACKED LONGERON. FABRICATED NEW LONGERON. CLEANED, TREATED AND PRIMED AREA AND NEW LONGERON. INSTALLED NEW LONGERON IAW DC8 SRM 51-1-11, 51-1-21, 51-1-20D, 51-3-1, DC8 SRM 53-5-3 FIGURE 5 SHEET 1, DC8 SRM 53-1-0 PAGE 1,SRM 51-1-21 AND 51-1-20D, DC8 SRM 53-5-3 FIGURE 5 SHEET 1 ITEM "B", AND DC8 SRM 51-1-8B.

Part: FITTING — CRACKED (ZONE 200) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND AFT FUSELAGE SPLICE FITTING CRACKED AT STATION 1766.000 LONGERON 17 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, 51-3-0, 51-3-1.

Part: FRAME — DENTED (ZONE 100) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT FRAME WITH DENT AND MISDRILLED AT STATION 200.000 LONGERON31 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED FRAME SEGMENT. FABRICATED FRAME SEGMENT ANGLE AND SPLICE. PERFORMED HEAT TREATMENT TO REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 53-2-0 FIG 2, SHEET 2 AND 6, 51-1-11, 51-3-1, IAW DC8 SRM 53-2-0 FIGURE 2 SHEET 2 AND 6, DC8 SRM 51-1-20D, DC8 SRM 53-2-0 FIGURE 2 SHEET 1, 51-2-0 FIGURE 50 SHEET 49 T/R NUMBER 51-106 DATED 01-29-99, SRM 53-4-1 FIGURE 40 SHEET 5 AND 6, DC8 SRM 53-2-0 FIGURE 2 SHEET 7 AND 8 T/R NUMBER 53-110 DATED 11-10-2000, DC8 SRM 51-1-1 PAGES 1, 13, 17, DC8 SRM 51-1-8B.

Part: SKIN — CRACKED (ZONE 100) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, NOSE SECTION FUSELAGE FREON EXHAUST SYSTEM FORWARD UPPER CORNER CRACKED AT STATION FS 40.000 LONGERON 28 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED EXTERNAL REPAIR DOUBLER, AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW SRM 51-1-21, 51-3-1, DC8 SRM 53-2-0 FIGURE 13 SHEET 1, SRM 53-2-0 FIGURE 13 SHEET 5 TR NUMBER 53-169 DATED 09-20-03, SRM 53-3-3 FIGURE 1 ITEM "C", DC8 SRM 51-1-20D, AND DC8 SRM 51-1-8B.

Part: FRAME — MISREPAIRED (FUSELAGE) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT HAS A IMPROPER REPAIR AND DENT ON FRAME AT STATION 240.000 LONGERON 20 RIGHT. REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED FRAME SEGMENT, SPLICE AND ANGLE. PERFORMED HEAT TREATMENT TO FRAME SEGMENT, SPLICE AND ANGLE. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW 51-1-11, 51-3-1, DC8 SRM 53-2-0 FIGURE 2 SHEET 2 AND 6, DC8 SRM 51-1-20D, DC8 SRM 53-4-1 FIGURE 40 SHEET 7-9 ITEM "C", SRM 53-2-0 FIGURE 2 SHEET 1, SRM 51-2-0 FIGURE 50 SHEET 49A, DC8 SRM 53-2-0 FIGURE 2 SHEET 8 T/R 53-110 DATED 11-10-2000, SRM 53-2-0 FIGURE 2 SHEET 7 T/R 53-110 DATED 11-10-2000, DC8 SRM 51-1-1 PAGES 1, 13, 17, AND DC8 SRM 51-1-8B.

Part: FRAME — MISREPAIRED (BS 240) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT HAS A IMPROPER REPAIR AND DENT ON FRAME AT STATION 240.000 LONGERON-21 RIGHT. REMOVED FASTNER AS NEEDED TO PERFORM REPAIR.REMOVED EXISTING REPAIR.FABRICATED FRAME SEGMENT, SPLICE AND ANGLE.PERFORMED HEAT TREATMENT TO FRAME SEGMENT, SPLICE AND ANGLE. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS.INSTALLED REPAIR PARTS AND NEW FASTNERS IAW 51-1-11, 51-3-1, DC8 SRM 53-2-0 FIGURE 2 SHEET 2 AND 6, DC8 SRM 51-1-20D, DC8 SRM 53-4-1 FIGURE 40 SHEET 7-9 ITEM "C", SRM 53-2-0 FIGURE 2 SHEET 1, SRM 51-2-0 FIGURE 50 SHEET 49A, DC8 SRM 53-2-0 FIGURE 2 SHEET 8 T/R 53-110 DATED 11-10-2000, SRM 53-2-0 FIGURE 2 SHEET 7 T/R 53-110 DATED 11-10-2000, DC8 SRM 51-1-1 PAGES 1, 13, 17, AND DC8 SRM 51-1-8B.

Part: FITTING — CRACKED (BS 1180) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND AFT BELLY PIT INTERNAL STRUCTURE FITTING UNDER CROSS SLIDE DOOR CRACKED AT STATION 1180.000 AROUND LONGERON-33 RIGHT. REMOVED CRACKED INTERNAL STRUCTURE FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, AND 51-3-1.

Part: FITTING — DENTED (BS 1180) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND AFT BELLY PIT INTERNAL STRUCTURE FITTING UNDER CROSS SLIDE DOOR CRACKED AT STATION 1180.000 AROUND LONGERON-34 RIGHT. REMOVED CRACKED INTERNAL STRUCTURE FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, AND 51-3-1.

Part: SKIN — MISREPAIRED (RUDDER) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT HAND SKIN AT STATION ZR 115.000 TO STATION ZR 150.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKINS AND INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE TO RUDDER FOUND MOMENT WITHIN TOLERANCE MOMENT 2455 INCH/LB. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 55-6-1 FIGURE 1, DC8 SRM 55-1-0 PAGE 1 AND SRM 51-1-21, DC8 SRM 55-6-1 FIGURE 1 ITEM "A", DC8 SRM 51-1-9 T/R 51-142 DATED 04-05-06 AND DC8 SRM 51-1-9A T/R 51-141 DATED 04-03-06, DC8 SRM 51-1-8B, DC8 SRM 51-4-6 PAGES 1-6. DC8 SRM 51-1-11, AND 51-1-21.

Part: FITTING — CRACKED (ZONE 100) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND AFT BELLY PIT CRACKED FITTING AT STATION 1230.000 LONGERON-32 RIGHT. REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION NOTED. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2003-05 DRAWING DOUGLAS NUMBER 4758514, DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242-4, DC8 SRM 51-1-8B, AND 51-3-1.

Part: VANE — DAMAGED (LT WING TE FLAP) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE OUTBOARD VANE WITH ELONGATED HOLES AT STATION XOLDI 6.224. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION NOTED. FABRICATED REPAIR DOUBLER INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA, REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW 8110-3, DRAWING ED-4652 DATED 11-05-07, DC8 SRM 51-1-21, 51-3-0, DC8 NDT SPM PART 08-00-02 TO 07, FORM SMN 242-4, 51-1-20D, 51-3-1, AND DC8 SRM 51-1-8B.

Part: FRAME — DENTED (ZONE 200) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT HAS A IMPROPER REPAIR AND DENT ON FRAME AT STATION 1580.000 LONGERON-21RIGHT REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED FRAME SEGMENT WITH EXISTING REPAIR. FABRICATED FRAME SEGMENT, ANGLES. PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS, AND REPAIR PARTS IAW DC8 SRM 53-2-0 FIGURE 2 SHEET 4 AND 6, DC8 SRM 51-1-20D, DC8 SRM 53-4-1 FIGURE 51 SHEET 21 ITEM "A", SRM 53-2-0 FIGURE 2 SHEET 7 AND 8 T/R 53-110 DATED 11-10-2000, DC8 SRM 51-1-1 PAGES 1, 13, 17, DC8 SRM 51-1-8B, AND 51-3-1.

Part: FRAME — MISREPAIRED (ZONE 200) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT HAS A IMPROPER REPAIR AND DENT ON FRAME AT STATION 1580.000 LONGERON-20 RIGHT REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED FRAME SEGMENT WITH EXISTING REPAIR. FABRICATED FRAME SEGMENT, ANGLES. PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS, AND REPAIR PARTS IAW DC8 SRM 53-2-0 FIGURE 2 SHEET 4 AND 6, DC8 SRM 51-1-20D, DC8 SRM 53-4-1 FIGURE 51 SHEET 21 ITEM "A", SRM 53-2-0 FIGURE 2 SHEET 7 AND 8 T/R 53-110 DATED 11-10-2000, DC8 SRM 51-1-1 PAGES 1, 13, 17, DC8 SRM 51-1-8B, AND 51-3-1.

Part: SKIN — CRACKED (ZONE 200) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, AFT FUSELAGE FOUND A CRACK AT LONGERON 17 RIGHT AT STATION 1769.000. REMOVED CRACKED LONGERON. FABRICATED LONGERON. CLEANED, TREATED AND PRIMED AREA AND NEW LONGERON. INSTALLED NEW LONGERON IAW DC8 SRM 51-1-11, 51-3-1, DC8 SRM 53-5-3 FIGURE 5 SHEET 1 ITEM "B", DC8 SRM 53-1-0 PAGE 1, SRM 51-1-21 AND 51-1-20D, AND DC8 SRM 51-1-8B.

Part: SKIN — CRACKED (ZONE 100) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, NOSE SECTION FUSELAGE FREON EXHAUST SYSTEM FORWARD UPPER CORNER CRACKED AT STATION FS 40.000 L27L. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR.REMOVED DAMAGED AREA.FABRICATED EXTERNAL REPAIR DOUBLER , AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AND NEW FASTNERS IAW SRM 51-1-21, 51-3-1, DC8 SRM 53-2-0 FIGURE 13 SHEET 1, SRM 53-2-0 FIGURE 13 SHEET 5 TR NUMBER 53-169 DATED 09-20-03, SRM 53-3-3 FIGURE 1 ITEM "C", DC8 SRM 51-1-20D, AND DC8 SRM 51-1-8B.

Part: SKIN — MISREPAIRED (HORIZONTAL STAB) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE HAS A IMPROPER REPAIR AT STATION XFS 178.750. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION NOTED. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA, REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-1-11, 51-1-20D, 51-3-1, FAA FORM 8110-3 NUMBER 07569 DATED 11-27-07, SEMAN DRAWING NUMBER ED-4653 DATED 11-09-07, DC8 SRM 51-1-21, SRM 51-3-0, DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242-4, AND DC8 SRM 51-1-8B.

Part: FITTING — CRACKED (FUSELAGE) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT A CRACKED FITTING BETWEEN STATION 960.000 AND STATION 980.000 RIGHT BOTTOM LINE 25". REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LEADING EDGE WITH DENT AT STATION XFS 242.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA, REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 52-2-1 FIGURE 4, DC8 SRM 51-1-21, 51-1-21A, DC8 SRM 55-2-1, FIGURE 4, SRM 55-3-1 FIGURE 1 SHEET 1 AND 2 ITEM "A", AND DC8 SRM 51-1-8B.

Part: SKIN — MISREPAIRED (ZONE 300) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT SKIN AT STATION ZR 150.000 TO STATION ZR 178.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKINS AND INTERNAL AND EXTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE TO RUDDER FOUND MOMENT WITHIN TOLERANCE MOMENT 2455 INCH/LB. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 55-6-1 FIGURE 1, DC8 SRM 55-1-0 PAGE 1 AND SRM 51-1-21, DC8 SRM 55-6-1 FIGURE 1 ITEM "A", DC8 SRM 51-1-9 T/R 51-142 DATED 04-05-06 AND DC8 SRM 51-1-9A T/R 51-141 DATED 04-03-06, DC8 SRM 51-1-8B, DC8 SRM 51-4-6 PAGES 1-6. DC8 SRM 51-1-11, AND 51-1-21.

Part: SKIN — DAMAGED (ZONE 500) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE UPPER SKIN WITH MISDRILLED HOLES AT STATION XW 408.343. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-1-21, 51-3-0, 51-3-1, DC8 SRM 57-3-3 FIGURE 4 SHEET 1 ITEM "F", DC8 SRM 57-1-0 PAGE 1 AND SRM 51-1-21, AND DC8 SRM 51-1-8B.

Part: SKIN — MISREPAIRED (ZONE 300) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RUDDER RIGHT AT STATION ZR 87.000 TO STA ZR 115.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING PAIR. FABRICATED NEW SKIN, INTERNAL, AND EXTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS PERFORMED BALANCE TO RUDDER. FOUND MOMENT WITHIN TOLERANCE MOMENT 2455 INCH/LB. INSTALLED NEW FASTENERS AND REPAIR PARTS DC8 SRM IAW 51-1-11, 51-1-21, DC8 SRM 51-4-6 PAGES 1-6, DC8 SRM 55-1-0 PAGE 1 AND SRM 51-1-21, DC8 SRM 55-6-1 FIGURE 1, ITEM "A", DC8 SRM 51-1-9, T/R 51-142 DATED 04-05-06 AND DC8 SRM 51-1-9A T/R 51-141 DATED 04-03-06, DC8 AND SRM 51-1-8B.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LOWER FUSELAGE NOSE SECTION HAS IMPROPER REPAIR AT STATION 165.000 TO STATION 70.000 LONGERON 31 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKINS AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 53-3-3 FIGURE 1, DC8 SRM 53-1-0 PAGE 1 AND SRM 51-1-21, DC8 SRM 51-1-8B, 51-1-20D, AND 51-3-1.

Part: SKIN — CRACKED (ZONE 100) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT FUSELAGE NOSE SECTION ACS MODIFICATION DOUBLER HEAT INTERCHARGER COMPARTMENT LOWER AFT JAMB CORNER CRACKED AT STATION FS 12.000 LONGERON 27 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED EXTERNAL AND INTERNAL DOUBLER CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-11, 51-1-20D, 51-3-1, FORM FAA 8110-3 NUMBER 07569 DATED 11-27-07 SEMAN DRAWING NUMBER ED-4644 DATED 11-09-07, DC8 SRM 51-1-21, 51-3-0, DC8 NDT SPM PART 08-00-02 TO 07, FORM SMN 242-4, AND DC8 SRM 51-1-8B.

Part: FITTING — CRACKED (BS 822) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT A CRACKED FITTING AT STATION 822.500 RIGHT BOTTOM LINE 25". REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, 51-3-1,DC8 SRM 51-1-20D, SRM 51-1-8B.

Part: FITTING — CRACKED (BS 702) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT A CRACKED FITTING AT STATION 702.875 RIGHT BOTTOM LINE 25". REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-3-0, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D, AND 51-3-1.

Part: FITTING — CRACKED (BS 781) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT A CRACKED FITTING AT STATION 781.500 LEFT BOTTOM LINE 25". REMOVED CRACKED FITTING.CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-3-0, 51-1-20D, 51-3-1, DC8 SRM 51-3-0, AND DC8 SRM 51-1-8B.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOIND LEFT HAND WING INBOARD FLAP HAS A DENT ON UPPER PANEL PLATING BETWEEN STATION XW 115.000 AND STATION XW 122.000.REMOVED FASTNERS AS NEEDED. REMOVED DAMAGEDAREA. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED REPAIR PARTS WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 1 PAGE 2 ITEM "D", "M" AND "K", DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-9A T/R NUMBER 51-141 DATED 04-05-06, DC8 SRM 51-1-8B.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER PLATING HAS IMPROPER REPAIR AND DENT BETWEEN STATION XW 104.000 AND XW 115.000. REMOVED FASTENER AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. APPLIED SEAL TO FAYING SURFACE. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 1 PAGE 2 ITEM "D",DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, 51-3-0, AND 51-3-1.

Part: LONGERON — MISREPAIRED (ZONE 100) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT STATION FS 97.000 LONGERON 34.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NET INSPECTION. NO CRACK NOR CORROSION FOUND. FABRICATED EXTERNAL AND INTERNAL FINGER DOUBLER. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SEMAN DRAWING NUMBER ED-4642, SRM 51-1-11, 51-3-1, FAA FORM 8110-3 NUMBER 07569 DATED 11-27-07, SEMAN DRAWING NUMBER ED-4642 DATED 11-12-07, DC8 SRM 51-1-21, 51-1-20D, DC8 NDT SPM PART 08-00-02 TO 07, DC8 SRM 51-1-8B, AND ATTACHED FORM SEMAN 242-4.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT FS 1518 LONGERON 32.5 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED EXTERNAL DOUBLER AND INTERNAL FINGER DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACE. INSTALLED NEW FASTENER AND REPAIR PARTS IAW DC8 SRM 53-2-1 FIGURE 7 SHEET 1,4,5, DC8 SRM 51-1-21, 51-1-20D, SRM 53-4-1 FIGURE 17A SHEET 2 ITEM "B", DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND 51-3-1.

Part: VANE — ELONGATED (RT WING TE FLAP) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INTERNAL VANE WITH ELONGATED HOLES AT STATION XS 247.000. REMOVED FASTENERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-1-20D, 51-3-1, FORM FAA 8110-3 NUMBER 07532 DATED 11-08-07 SEMAN DRAWING NUMBER ED-4649 DATED 11-07-07, DC8 SRM 51-1-21, 51-3-0, DC8 NDT SPM PART 08-00-02 TO 07, FORM SMN 242-4, AND DC8 SRM 51-1-8B.

Part: VANE — DAMAGED (ZONE 600) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING EXTERNAL VANE WITH ELONGATED HOLES AT STATION XOLDO 67.000. REMOVED FASTENERS AS NEEDED TP PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED REPAIR DOUBLER AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA, AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-3-1, FORM FAA 8110-3 NUMBER 07532 DATED 11-08-07 SEMAN DRAWING NUMBER ED-4648 DATED 11-07-07, DC8 SRM 51-1-21, 51-3-0, 51-1-20D, DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242-4, AND DC8 SRM 51-1-8B.

Part: SKIN — CRACKED (ZONE 100) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT FUSELAGE NOSE SECTION ACS MODIFICATION DOUBLER HEAT INTERCHARGER COMPARTMENT LOWER AFT JAMB CORNER DAMAGE AT STATION FS 12.000 LONGERON 27 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED EXTERNAL DOUBLER AND EXTERNAL REPAIR TRIPLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FORM FAA 8110-3 NUMBER 07529 DATED 11-09-07 SEMAN DRAWING NUMBERED-4645 DATED 11-08-07, SRM 51-1-21, DC8 51-3-0, DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242-4, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, 51-3-0, 51-1-20D, AND 51-3-1.

Part: FITTING — CRACKED (BS 798) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOIND IN MAIN CARGO COMPARTMENT A CRACKED FITTING AT STATION 798.000 LEFT BOTTOM LINE 25". REMOVED CRACKED FITTING. FABRICATED FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLED FITTING IAW DC8 SRM 51-1-20D, 51-3-1, DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2003-05 DRAWING DOUGLAS NUMBER 3755222, DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242.4, AND SRM 51-1-8B.

Part: FRAME — DAMAGED (BS 240 S29L) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, AT F/S STATION 240 LEFT FRAME HAS DOUBLE DRILLED HOLE BETWEEN LONGERON 29 LEFT AND LONGERON 30 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PLUGGED MISDRILLED HOLE WITH RIVET. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION. FABRICATED REPAIR ANGLE. CLEANED, TREATED AND PRIMED AREA AND REPAIR ANGLE. INSTALLED NEW FASTENERS AND REPAIR ANGLE IAW SRM 51-1-11, 51-3-1, FAA FORM 8110-3 NUMBER 07529 DATED 11-09-07, SEMAN DRAWING NUMBER ED-4646 DATED 11-08-07, DC8 SRM 51-1-20D, DC8 NDT SPM PART 08-00-02 TO 07, ATTACHED FORM SMN 242-4, AND DC8 SRM 51-1-8B,

Part: SKIN PANEL — MISREPAIRED (ZONE 100) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LOWER FUSELAGE NOSE SECTION HAS IMPROPER REPAIR AT STATION 165.000 TO STATION 70.000 LONGERON 31 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKINS AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 53-3-3 FIGURE 1, DC8 SRM 53-1-0 PAGE 1 AND SRM 51-1-21, DC8 SRM 51-1-8B, 51-1-20D, AND 51-3-1.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT HAND INBOARD FLAP UPPER PLATING HAS A IMPROPER REPAIR AT STATION XW 71.000 AND STATION XW 91.000.REMOVED FASTNER AS NEEDED TO PERFORM REPAIR.REMOVED EXISTING REPAIR.FABRICATED NEW SKIN AND INTERNAL DOUBLRE. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTNERS AND REPAIR PARTS AT STATION XW 2.000 TO STATION XW 91.000 IAW 51-3-1, DC8 SRM 57-7-1 FIGURE 1 PAGE 2, ITEM "D", DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, 51-3-0, AND DC8 SRM 51-1-8B.

Part: SKIN — CRACKED (ZONE 200) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, EXTERNAL SKIN SHOWS CRACK AT STATION FS 1750.000 LONGERON 15 LEFT. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER INTERNAL FINGER DOUBLER. PERFORMED NDT INSPECTION. NO CRACK NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-1 FIGURE 7 SHEET 1 AND 4, SRM 53-5-3 FIGUE 1 ITEM "D", DC8 NDT SPM PART 08-00-02 TO 07, FORM SEMAN 242-4, DC8 SRM 51-1-8B, SRM 51-1-21, 51-1-20D, AND 51-3-1.

Part: SKIN — MISREPAIRED (TE FLAP) · airframe 87,931 hrs · 29,662 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT OUTBOARD FLAP UPPER PLATING HAD IMPROPER REPAIR AT STATION XF 213.000. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 4 T/R 5794 ITEM "C", DATED 10-01-02, DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, AND DC8 SRM 51-1-8B.

Part: DOWNLOCK SWITCH — DEFECTIVE (ZONE 700) · airframe 87,093 hrs · 29,355 cycles

DURING LANDING INTO KTOL WHEN THE GEAR HANDLE WAS PLACED IN DOWN POSITION LEFT GEAR GREEN LIGHT DID NOT ILLUMINATE, RED LIGHT CYCLE ON AND OFF. THE CREW RECYCLED THE GEAR AND GEAR OPERATED NORMALLY. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LEFT GEAR DOOR AND FOUND THE LEFT MAIN LANDING GEAR DOWN LOCK SWITCH DEFECTIVE. MAINTENANCE REPLACED THE SWITCH AND OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,749 hrs · 29,245 cycles

DURING APPROACH TO KTOL, THE LEFT GEAR LIGHT DID NOT ILLUMINATE. THE CREW CYCLED THE GEAR AND THE LIGHT STILL DID NOT ILLUMINATE. AFTER APPROXIMATELY 2 MINUTES THE LIGHT ILLUMINATED. THE CREW LANDED THE AIRCRAFT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND THE GEAR WARNING LIGHT BULBS BAD AND DEBRIS ON THE LEFT GEAR DOOR WARNING SWITCH. MAINTENANCE REPLACED THE LIGHT BULBS AND ALSO CLEANED THE GEAR WARNING SWITCH. THE OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ENGINE — FLUCTUATES (NR 3) · airframe 85,847 hrs · 28,868 cycles

IN FLIGHT NOTICED SLIGHT RUMBLE, NR 3 ENG N1 BEGAN TO FLUCUATE. ENG BEGAN TO ROLL BACK, ENG OIL PRESSURE LIGHT CAME ON. ENG SHUTDOWN, OIL PRESSURE WENT TO NEAR ZERO PSI. INSPECTED ENG INLET & EXHAUST, SPECIFIC GRAVITY, CHECKED MAGNETIC CHIP DETECTORS, FUEL FILTER, CDP TUBES FOR LEAKS AND ALL CHECKS WERE GOOD. MAINTENANCE THEN CHECKED FUEL PUMP LOW PRESSURE IMPELLER ROTATION, CHECKED N1 & N2 FOR ROTATION, ALL CHECKS GOOD. SUMPED TANK AND NO WATER WAS NOTED, INSPECTED FOR FUEL LEAK IN PYLON AND LEADING EDGE WITH NO LEAKS NOTED. RAN ACFT FOR 5 MINS IN IDLE (NOISE CONSTRAINTS IN LAX). TURNED THE BOOST PUMP ON & OFF, ALL ENGINE PARAMETERS CHECKED NORMAL. NR 3 ENGINE CHECKS GOOD ON GROUND.

Part: RUDDER CONTROL — UNKNOWN · airframe 85,699 hrs · 28,822 cycles

AFTER TAKEOFF CREW EXPERIENCED UNCOMMANDED YAW WITH ROLL. TURNED YAW DAMPER OFF AND OPENED C/B. THIS HAD NO EFFECT. CREW RETURNED TO BOEING FIELD AT TIME WITH FULL RUDDER DEFLECTION AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING. WHEN MORE INFORMATION IS AVAILABLE IT WILL BE PROVIDED.

Part: GYRO — INOPERATIVE (VERTICAL) · airframe 85,305 hrs · 28,643 cycles

DURING CLIMB OUT CAPTAINS EHSI FAILED. MULTIPLE FLAGS COMPUTER FLAGS HDG INT. CREW RETURNED AIRCRAFT TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED CAPT'S VG AND DG AND REPLACED WITH LTR-97 UNIT IAW APPLICABLE MM. THE OPERATIONAL CHECK GOOD AND THE AIRCRAFT RETURNED TO SERVICE.

Part: FIBER OPTIC GYRO — INOPERATIVE (ADHI) · airframe 84,995 hrs · 28,507 cycles

DURING CLIMB-OUT FROM KTOL PILOTS HSI/ADHI WAS INOP, INFORMATION WAS LOST. AFTER CREW RESET CIRCUIT BREAKERS ADHI RETURNED THEN WENT BLANK. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 FOG. PERFORMED A SHAKEDOWN OF WIRES BEHIND THE NR 1 EADI NR 1 FOG. ALSO, REPLACED NR 1 INSTRUMENT AMP. THE OPERATIONAL CHECK WAS GOOD PER ALL APPLICABLE MANUALS AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 84,995 hrs · 28,506 cycles

DURING CLIMB-OUT FROM KTOL, PILOT'S HSI/ADHI WAS INOP. LOST ATTITUDE AND HEADING INFORMATION. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET EADI AND EHSI CIRCUIT BREAKERS. THE SYSTEM RETURNED TO NORMAL AND THE OPERATIONAL CHECK WAS GOOD PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.