N71CX

Part: CONTROLLER — INOPERATIVE (WINDSHIELD) · airframe 78,789 hrs · 20,078 cycles

ACFT ENROUTE AND AIR RETURNED BACK TO DEPARTURE DUE TO F/O WINDSHIELD CRACKED AND ARCING. PILOT STATED F/O VISION IMPAIRED. R & R RT SIDE WINDSHIELD IAW MM 56-10-2 AND R & R RT WINDOW HEAT CONTROLLER IAW MM 30-41-0. OPS CHECKED NORMAL.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 78,519 hrs · 20,008 cycles

F/A EMERGENCY FLASHLIGHTS FOUND INOPERATIVE. R & R THE RT EMERGENCY FLASHLIGHT AND BATTERIES IAW MM 16.02. OPS CHECK GOOD.

Part: ENGINE — STALLED (NR 3) · airframe 78,351 hrs · 19,959 cycles

DURING TAKEOFF ROLL, CREW EXPERIENCED A COMPRESSOR STALL ON THE NR 3 ENGINE. TAKEOFF WAS REJECTED AT 85 KIAS AND 1.96 EPR. RETURNED BACK TO GATE. MX PERSONNEL PERFORMED A VISUAL INSPECTION OF NR 3 ENGINE, NO DEFECTS OBSERVED. ACCOMPLISHED ENGINE RUN UP TO TAKEOFF POWER AND ALL PARAMETERS WERE NORMAL.

Part: GROUND WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 77,956 hrs · 19,856 cycles

PASSENGER COMPARTMENT FORWARD BULKHEAD EMERGENCY EXIT IDENTIFIER DOES NOT ILLUMINATE. REPAIRED GROUND WIRE TO IDENTIFIER IAW MM 20-50-1 AND RELAMPED SIGN. OPS CHECKS NORMAL IAW MM 33.01.1.

Part: SLIDE — LOW PRESSURE (ZONE 800) · airframe 77,684 hrs · 19,787 cycles

LEFT HAND PASSENGER DOOR ESCAPE SLIDE PRESSURE LOW AND IN RED RANGE (2600 PSI AT 22 DEGREES CELCIUS) - DISCOVERED DURING POSTFLIGHT INSPECTION. MX R & R EMERGENCY ESCAPE SLIDE IAW MM 25-60-1.

Part: UNKNOWN — UNKNOWN (NLG) · airframe 77,544 hrs · 19,753 cycles

AFTER TAKEOFF, WHEN GEARS WERE BEING RETRACTED THE CREW A HEARD LOUD NOISE IN NOSE GEAR AREA. THEY CYCLED NOSE GEAR AND NOISE CONTINUED. THEY RETURNED TO WITHOUT FURTHER INCIDENT. ON POST FLIGHT INSPECTION BOTH DOORS WERE CLOSED AND LATCHED. MAINTENANCE INSPECTED BOTH LEFT AND RIGHT NOSE GEAR DOORS FOR MECHANICAL DEFECTS, NONE NOTED IAW DACO 32-20-0. AIRCRAFT WAS RETURNED TO SERVICE.

Part: GROUND WIRE — LOOSE (ZONE 100) · airframe 77,496 hrs · 19,743 cycles

AIR TURN BACK, DUE TO AUTO PILOT WILL NOT STAY ENGAGED WITH ELEVATOR SERVO ON. THE ACFT PITCHES UP AND DOWN AND DISENGAGED IN VERTICAL SPEED OR ALT HOLD MODES. MX TROUBLESHOT AND FOUND WEAK SHIELD GROUND AT GROUND STUD 1385, REPAIRED GROUND SHIELD AT STUD 1385 IAW SWPM 21-21-1. REPLACED AUTO PILOT CONTROLLER, OPS CHECK GOOD IAW MM 22-10-2. ACFT WAS RETURNED TO SERVICE.

Part: FAN — FAILED (ZONE 100) · airframe 77,496 hrs · 19,743 cycles

DURING CRUISE, THE LT RECIRCULATION FAN HAS A SMELL OF SMOKE. THE CREW TURNED OFF LT RECIRCULATION FAN AND SMOKE, SMELL WENT AWAY. THEY LANDED WITHOUT FURTHER INCIDENT. MX PERFORMED OPS TEST ON BOTH LT AND RT RECIRCULATION FAN, NO SMOKE ODOR NOTED IAW MM 21-21-1. ACFT WAS RETURNED TO SERVICE.

Part: FAN — ODOR (COCKPIT) · airframe 77,400 hrs · 19,723 cycles

DURING CRUISE, THE OVERHEAD COCKPIT CLIMATE CONTROL UNIT EMITS A BURNING ODOR WHEN TURNED ON. THE CREW LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED AND CLEANED THE OVERHEAD CLIMATE CONTROL UNIT FAN. OPS CHECK GOOD IAW MM 21-02. ACFT WAS RETURNED TO SERVICE.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 77,393 hrs · 19,722 cycles

DURING PREFLIGHT INSPECTUIN, FOUND EMERGENCY FLASHLIGHT INOPERATIVE. MX REPLACED BATTERY IAW MM 33-50-0.

Part: FAN — FAILED (LT RECIRC) · airframe 77,377 hrs · 19,719 cycles

DURING CRUISE, WHEN THE CREW TURNED ON LT RECIRCULATION FAN IT EMITTED A BURNING SMELL. THEY TURNED THE LT RECIRCULATION FAN OFF AND SMELL WENT AWAY. THEY LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE LT RECIRCULATION FAN. OPS CHECKED GOOD IAW MM 21-21-1. ACFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (AUTOPILOT) · airframe 77,272 hrs · 19,701 cycles

DURING CRUISE, 30 MIN INTO FLIGHT, AUTOPILOT DISCONNECTED AND WOULD NOT RECONNECT. THE CREW RETURNED . MX REPLACED AUTOPILOT CONTROLLER. OPS CHECKED GOOD IAW MM 22-10-2. ACFT RETURNED TO SERVICE.

Part: LIGHT — UNSECURE (CABIN) · airframe 77,128 hrs · 19,674 cycles

DURING PREFLIGHT INSP, FOUND GALLEY SERVICE DOOR EMERGENCY EXIT LIGHTING INTERMITTENT. MX RESECURED LIGHTING ASSY. OPERATIONAL CHECK GOOD IAW MM 33-50-0. ACFT RETURNED TO SERVICE.

Part: STRINGER — DELAMINATED (NR 1 NACELLE) · airframe 77,112 hrs · 19,670 cycles

DURING ROUTINE B-CHECK INSPECTION FOUND NR 1 ENGINE LOWER STRINGER DELAMINATED. R & R DAMAGED STRINGER IAW MM 78-10-2.

Part: FAN — DEFECTIVE (CABIN) · airframe 77,076 hrs · 19,662 cycles

DURING CRUISE, THE LT RECIRCULATION FAN EMITTED A BURNED ELECTRICAL ODOR. THE CREW TURNED OFF THE LT RECIRCULATION FAN THE BURNED ODOR WENT AWAY. THEY LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE LT RECIRCULATION FAN. OPS CHECK GOOD IAW MM 21-21-1. ACFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — SHORTED (INSTRUMENT PANEL) · airframe 76,917 hrs · 19,618 cycles

WHILE INCREASING THE INTENSITY OF THE ENGINE INSTRUMENT LIGHTS, THE CREW SMELLED AN ELECTRICAL ODOR COMING FROM THE ENGINE INSTRUMENT LIGHT PANEL. THEY TURNED OFF THE RHEOSTAT TO THE ENGINE INSTRUMENT LIGHTS, THE ODOR WENT AWAY. THEY LANDED WITHOUT FURTHER INCIDENT. MX INSPECTED THE ENG INSTRUMENT LIGHTS AND FOUND THE NR 1 EGT GAGE BACKGROUND LIGHT CONNECTOR SHORTED OUT. THEY DISCONNECTED AND CAPPED WIRES TO CONNECTOR. OPS CHECK GOOD IAW MM 33-13-0. ACFT WAS RETURNED TO SERVICE.

Part: SMOKE DETECTOR — DEFECTIVE (CARGO BAY) · airframe 76,883 hrs · 19,610 cycles

DURING CLIMBOUT, THE NR 2 CARGO SMOKE DETECTOR FLASHED ON MOMENTARLY SEVERAL TIMES WITH ASSOCIATED AUDIBLE WARNING. THE CREW INSPECTED THE CARGO COMPARTMENT FOR SMOKE OR FIRE AND NONE WAS NOTED. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX INSPECTED THE ACFT FOR EVIDENCE OF FIRE, NONE WAS NOTED. THEY TROUBLESHOT THE SYS AND REPLACED THE NR 2 SMOKE DETECTOR. OPS CHECK GOOD IAW MM 26-.03. ACFT WAS RETURNED TO SERVICE

Part: ACTUATOR — DEFECTIVE (OUTFLOW VALVE) · airframe 76,797 hrs · 19,585 cycles

AT FL 320 CABIN PRESSURIZATION CONTROL WAS SET TO 340 FOR FOR A SELECTED CABIN 4,500 FT CABIN CLIMBED TO 8500 FT. CABIN PRESS CONTROL LEVER PHYSICALLY LIMITED TO 2" FROM FULL CLOSED. THE CREW RETURNED BACK TO DEPARTURE WITHOUT FURTHER INCIDENT. MX FOUND THE OUTFLOW VALVE PRESSURE ACTUATOR WAS NOT WORKING AND R & R IAW MM 21-31-0. THE ACFT WAS RETURNED BACK TO SERVICE.

Part: FAN — FAILED (ZONE 200) · airframe 76,771 hrs · 19,577 cycles

DURING CRUISE THE RT RECIRCULATION FAN EMMITTING AN ELECTRICAL ODOR. THE CREW TURNED OFF FAN AND SMELL WENT AWAY. THE CREW LANDED WITHOUT FURTHER INCIDENT.

Part: FAN — FAILED (RECIRCULATION) · airframe 76,597 hrs · 19,529 cycles

DURING CRUISE, WITH THE RT RECIRCULATION FAN ON HAS A STRONG ELECTRICAL ODOR, WHEN TURNED OFF ODOR WENT AWAY. THE CREW LANDED WITHOUT FURTHER INCIDENT. MX DEFERRED THE RT RECIRCULATION FAN IAW MEL 21-16-01. MX REPLACED RECIRCULATION FAN. OPS CHECK GOOD IAW MM 21-21-1.

Part: SKIN — DAMAGED (NR 4 SPOILER) · airframe 76,511 hrs · 19,506 cycles

DURING ROUTINE MAINTENANCE CHECK FOUND LEFT HAND WING NUMBER FOUR SPOILER PANEL DAMAGED. THE SPOILER WAS REPAIRED IAW DACO MAINTENANCE MANUAL 27-61-0.

Part: PRESSURE SWITCH — CRACKED (OIL PRESSURE) · airframe 76,349 hrs · 19,461 cycles

DURING CRUISE, THE CREW SHUTDOWN NR 1 ENGINE DUE TO LOSS OF OIL QTY. THEY LANDED WITHOUT FURTHER INCIDENT. MX INPECTED NR 1 ENGINE AND FOUND OIL DIFFERENTIAL PRESSURE SWITCH HOUSING CRACKED. THEY REPLACED OIL DIFFERENTIAL PRESSURE SWITCH. OPS CHECK GOOD IAW MM 79-33-1, 79-20-7 AND ERH 70.01.1. ACFT WAS RETURNED TO SERVICE.

Part: FAN — ODOR (LT RECIRC) · airframe 75,868 hrs · 19,328 cycles

DURING CRUISE, THE LT RECIRCULATION FAN WHEN TURNED ON EMITTED A ELETRICAL ODOR. THE CREW TURNED OFF THE LT RECIRCULATION FAN AND CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED THE LT RECIRCULATION FAN. OPS CHECK GOOD IAW MM 21-21-1. ACFT WAS RETURNED TO SERVICE.

Part: FAN — DEFECTIVE (ZONE 100) · airframe 75,856 hrs · 19,325 cycles

DURING CRUISE, THE RIGHT HAND RECIRCULATION FAN WHEN TURNED ON EMITTED A ELECTRICAL ODOR. THE CREW TURNED OFF RIGHT RECIRCULATION FAN AND SMELL WENT AWAY. THEY LANDED IN KWRI WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT RECIRCULATION FAN. OPERATIONAL CHECK GOOD IAW MM 21-20-1. AIRCRAFT RETURNED TO SERVICE.

Part: LONGERON — CORRODED (BS 1380-1400)

(SPUY) AFT ACCY COMPT - L-23R INTERIOR CORRODED (STA 1380.000 - 1400.000).

Part: SKIN — CORRODED (LT ELEVATOR)

(SPUY) LT HORZ STAB - ELEVATOR LWR SKIN CORRODED AT STA XE 195.313.149.000 AND 132.750.

Part: STRUCTURE — CORRODED (RT WING)

(SPUY) RT WING INBD L/E OUTER SECTION UPPER PART CORRODED AT STA XW 257.000.

Part: SKIN — CORRODED (LT WING)

(SPUY) LT WING - UPPER PANEL EXTERNAL SKIN CORRODED AT STA XRS 204.000 S-14.

Part: HOOK — CRACKED (AFT PAX DOOR)

(SPUY) AFT PAX DOOR- HOLD OPEN HOOKS (02EA) CRACKED 1", APPROX AT STA FS 1440.000L TO L-15L.

Part: FRAME — CORRODED (BS 879 L24L)

(SPUY) LT MLG WW - FRAME FITTING CORRODED AT STA FS 879.000 L-24.

Part: SKIN — CRACKED (RT WING)

(SPUY) RT WING NR 4 STUB WING LWR SKIN CRACKED APPROX 1.5" (CORRECTING SOURCE DOCUMENT: INS-100R-5700).

Part: SKIN — CORRODED (BS 1558 L10L)

(SPUY) FUSELAGE SKIN CORRODED AT STA FS 1558.000 L-10L.

Part: ANGLE — CORRODED (VERT TO FUSE)

(SPUY) EMPENAGE - VERTICAL STAB TO FUSELAGE LT JOINT ANGLE CORRODED AT STA 1640.382.

Part: BEAM — CRACKED (BS 1606 L19R)

(SPUY) NR80 ACCESS DOOR - BULKHEAD BEAM CRACKED 4" AT STA 1606.000 L-19 ON RBL-2: TO LBL 2".

Part: SKIN — DENTED (LT WING TE FLAP)

(SPUY) LT WING OTBD FLAP UPPER SKIN DENTED (STA XF 238.00 - 304.000).

Part: CARGO TRACK — CORRODED (BS 372)

(SPUY) MAIN CARGO COMPT NR 6 TRACK CORRODED AT STA 372.000.

Part: SKIN — CORRODED (BS 1480 L11L)

(SPUY) EXTERNAL FUSELAGE - LOWER SKIN PANEL BUTT SPLICE CORRODED AT STA 1480.000 L-11L.

Part: SKIN — CORRODED (RT WING)

(SPUY) RT WING UPPER SKIN CORRODED AT AROUND STA XRS 74.889.

Part: SKIN — CORRODED (RWS 710-760)

(SPUY) RT WING OTBD L/E OUTER SECTION LWR SKIN CORRODED (XFS 710.000-760.000).

Part: SKIN — CORRODED (ZONE 200) · airframe 75,787 hrs · 19,305 cycles

DURING ROUTINE C-CHECK INSP FOUND EXTERNAL FUSELAGE SKIN CORRODED AT STA FS 1556.000 LONGERON 10 LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, REPAIR DOUBLER, FILLER, AND FINGER DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW SKIN AND REPAIR PARTS IAW SRM 51-1-8, SRM 53-2-0, SRM 53-2-1 FIGURE 7 TR 53-203, SRM 53-2-1, FIG 7 TR 53-203, SRM 53-5-2 FIGURE 1 ITEM "A", DPS 4.710 REV "L", SRM 51-1-8B, SRM 51-1-21, SRM 51-1-14, SRM 51-1-20D, AND SRM 51-3-1.

Part: SKIN — CRACKED (RT WING) · airframe 75,787 hrs · 19,305 cycles

DURING ROUTINE C-CHECK INSP FOUND RT WING NR 4 STUB WING LOWER SKIN CRACKED. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, EXTERNAL DOUBLERS AND INTERNAL DOUBLERS. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FORM 8110-3, DWG ED-5190, SRM 51-1-20D, NDT SPM PART 06-10-01-001, SRM 51-1-1, SRM 51-1-8B, SRM 51-1-21, SRM 51-1-20D, AND SRM 51-3-1.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 75,787 hrs · 19,305 cycles

DURING ROUTINE C-CHECK INSP FOUND THE LT WING OTBD FLAP UPPER SKIN DENTED AT STA XF 238.000 - 304.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-1-21, SRM 57-1-0 PAGE 1, SRM 51-1-8B, SRM 57-7-1 FIGURE 4 TR 57-94 ITEM "C", DPS 4.710 REV "L", AND SRM 51-1-21.

Part: SKIN — CORRODED (RWS 710-760) · airframe 75,787 hrs · 19,305 cycles

DURING ROUTINE C-CHECK INSP FOUND RT WING OTBD L/E OUTER SECTION LOWER SKIN CORRODED AT STA XFS 710.000 - 760.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, INTERNAL DOUBLERS, EXTERNAL DOUBLERS AND FILLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 DATED 07/22/10, DWG ED-5189 DATED 06/28/10, SRM 51-1-8, SRM 57-2-0, NDT SPM PART 06-10-01-001, SRM 51-1-8B, SRM 51-1-21, SRM 51-1-14, SRM 51-1-20D, AND SRM 51-3-1.

Part: LONGERON — CORRODED (BS 1380-1400) · airframe 75,787 hrs · 19,305 cycles

DURING ROUTINE C-CHECK INSP FOUND AFT ACCESSORY COMPARTMENT LONGERON L-23 RT INTERIOR CORRODED AT STA 1380-1400. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABERCATED SPLICES. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW LONGERON SEGMENT AND SPLICES IAW SRM CHAP 53-2-2 FIG 10, SRM 51-1-8, SRM 53-2-0, SRM 51-1-8B, SRM 51-1-21, SRM 51-1-20D, AND SRM 51-3-1.

Part: SKIN — CORRODED (ZONE 600) · airframe 75,787 hrs · 19,305 cycles

DURING ROUTINE C-CHECK INSP, FOUND RT WING UPPER SKIN CORRODED AT STA XRS 38.000 -112.000. REMOVED CORROSION. FOUND OUT OF LIMITS. PERFORMED NDT INSP. NO DISCREPANCY FOUND. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED NEW SKIN, REPAIR DOUBLER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FORM 8110-3, DWG ED-5186,SRM 51-1-8, SRM 57-2-0, FIG 7, NDT SPM PART 06-10-01-100, SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-14, SRM 51-1-20D, AND SRM 51-3-1.

Part: CARGO TRACK — CORRODED (BS 372) · airframe 75,787 hrs · 19,305 cycles

DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT NR 6 TRACK CORRODED AT STA 372.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED SPLICES. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW TRACK SEGMENT AND REPAIR PARTS IAW SRM CHAPTER 53-2-3 FIG 14 SHEETS 1-2, SRM 51-1-8, SRM 53-2-0, SRM 53-2-2 PAGE 13, SRM 53-2-3 FIGURE 14 SHEETS 1/53/7-2 FIGURE 3B SHEET 1 ITEM H, SRM 51-2-0 FIGURE 50 SHEET 79, DPS 4.710 REV "L", SRM 51-1-8B, SRM 51-3-0, SRM 51-1-21, AND SRM 51-3-1.

Part: SKIN — CORRODED (LT ELEVATOR) · airframe 75,787 hrs · 19,305 cycles

DURING ROUTINE C-CHECK INSP, FOUND LT HORIZ STABILIZER ELEVATOR LOWER SKIN CORRODED AT STA XE 195.313, 149.000, AND 132.750. REMOVED CORROSION. FOUND OUT OF LIMITS. 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. PERFORMED BALANCE. FOUND WITHIN LIMITS MOMENT: 1461.402 IN-LB. INSTALLED NEW FASTENERS AND REPAIR PART IAW SRM CHAPTER 55-4-1 FIG 1, SRM 51-1-8, SRM 55-2-0, SRM 51-1-21, SRM 55-1-0 PAGE 1, SRM 51-1-9 TR 51-142, SRM 51-19A TR 51-141, DPS 1.950 REV "AR" R-1, SRM 51-1-8B, SRM 51-1-21, SRM 51-4-4, PAGES 2-3.

Part: SKIN — CORRODED (ZONE 200) · airframe 75,787 hrs · 19,305 cycles

DURING ROUTINE C, CHECK INSP FOUND EXTERNAL FUSELAGE LOWER SKIN PANEL BUTT SPLICE CORRODED AT STA 1460.000, LONGERON 11LT. REMOVED FASTENERS AS NEED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER AND TRIPPLER CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 DATED 07/05/10, DWG ED-5183 DATED 06/23/10, SRM 51-1-8, SRM 53-2-0, NDT SPM PART 06-10-01-100, SRM 51-1-8B, SRM 51-1-21, SRM 51-1-20B, SRM 51-1-20D, AND SRM 51-3-1.

Part: SKIN — CORRODED (ZONE 600) · airframe 75,787 hrs · 19,305 cycles

DURING ROUTINE C-CHECK INSP, FOUND RT WING INBD L/E OUTER SECTION UPPER PART CORRODED AT STA XW 257.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED NEW SKIN, REPAIR DOUBLER, AND FILLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 DATED 07/22/10, SEMAN DWG ED-5187 DATED 06/30/10, SRM 51-1-8, SRM 57-2-0, NDT SPM PART 06-10-01-001, SRM 51-1-8B, SRM 51-1-21, SRM 51-1-14, SRM 51-1-20D, AND SRM 51-3-1.

Part: ANGLE — CORRODED (BS 1640) · airframe 75,787 hrs · 19,305 cycles

DURING ROUTINE C-CHECK INSP, FOUND EMPENNAGE VERTICAL STABILIZER TO FUSELAGE LT JOINT ANGLE CORRODED AT STA 1640.382. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED ANGLE, FILLER AND TAPERED SHIMS. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW SRM 51-1-8, SRM 53-2-0, SRM 53-2-2 FIGURE 16A, SHEETS 1-2, DPS 4.710 REV "L", SRM 53-2-5, SRM 51-1-6, SRM 51-1-8B, SRM 51-1-14, SRM 51-1-20D, AND SRM 51-3-1.

Part: SKIN — CORRODED (ZONE 500) · airframe 75,787 hrs · 19,305 cycles

DURING ROUTINE C-CHECK INSP FOUND LT WING UPPER PANEL EXTERNAL SKIN CORRODED AT STA XRS 204.000 STR 14. REMOVED CORROSION. FOUND OUT OF LIMITS. PERFORMED NDT INSP. NO DISCREPANCY FOUND. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED NEW SKIN AND REPAIR DOUBLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FORM 8110-3 DATED 07/23/10, DWG ED-5185 SRM 51-1-8, SRM 57-2-0 FIGURE 7, NDT SPM PART 06-10-01-100, SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-14, SRM 51-1-20D, AND SRM 51-3-1.

Part: FITTING — CORRODED (BS 879 L24L) · airframe 75,787 hrs · 19,305 cycles

DURING ROUTINE C-CHECK, INSP FOUND LT MLG WHEEL WELL FRAME FITTING CORRODED AT FS 879.000 LONGERON 24. REMOVED CORRODED FITTING. FABRICATED NEW FITTING, SPLICES AND DOUBLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FITTING AND REPAIR PARTS IAW SRM CHAPTER 53-2-0 FIG 8, SRM 51-1-8, SRM 53-2-0, SRM 51-1-20D, SRM 51-3-0, SRM 51-1-8B, SRM 51-1-20D, SRM 51-3-0, AND SRM 51-3-1.

Part: HOOK — CRACKED (PAX DOOR) · airframe 75,787 hrs · 19,305 cycles

DURING ROUTINE C-CHECK INSP, FOUND AFT PAX DOOR HOLD OPEN HOOKS CRACKED AT STA FS 1440.000 LONGERON 14 LT LONGERON 15 LT. REMOVED FASTENERS AS NEED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER, FILLER, FINGER DOUBLERS. PERFORMED NDT INSP. NO DISCREPANCY FOUND. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FORM 8110-3 DATED 07/20/10, DWG ED-5182 DATED 06/19/10, SRM 51-1-21, SRM 51-3-0, NDT SPM PART 06-10-0-001, SRM 51-1-8B, SRM 51-1-21, SRM 51-1-14, SRM 51-1-20D, AND SRM 51-3-1.

Part: SKIN — MISREPAIRED (VERTICAL STAB) · airframe 75,787 hrs · 19,305 cycles

DURING ROUTINE C-CHECK INSP, FOUND IMPROPER REPAIR ON THE VERTICAL STABILIZER L/E AT STA ZFS 292. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND REPAIR SPLICE. PERFORMED NDT INSP. NO DISCREPANCY FOUND. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3, DATED 07/06/10 AND DWG ED-5184 DATED 06/26/10, SRM 51-1-21 AND SRM 51-1-21A, NDT SPM PART 06-10-0-001, SRM 51-1-8B, SRM 51-1-21, SRM 51-1-14, SRM 51-1-20D, AND SRM 51-3-1.

Part: CONTROLLER — DEFECTIVE (CABIN PRESSURE) · airframe 75,756 hrs · 19,299 cycles

DURING CRUISE, CABIN RATE OF CLIMB RAISED QUICKLY TO 10,000 FT, FLIGHT ENGINEER RAN PNEUMATIC TO HIGH AND OPERATED THE PRESSURE CONTROL VALVE. THE CREW WAS PERMITTED PARTIAL CONTROL OF CABIN PRESSURE UNTIL ACFT DESCENDED BLOW FL200. THEY RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED CABIN RATE CONTROLLER. OPS CHECK GOOD IAW MM 21-31-2 AND 21-21-0. ACFT WAS RETURNED TO SERVICE.

Part: FAN — FAILED (ZONE 100) · airframe 75,680 hrs · 19,285 cycles

DURING CRUISE THE LT RECIRCULATION FAN STOPPED WORKING AFTER 40 MIN AND EMITTED A SMOKE ODOR. THE CREW PULLED CURCUIT BRAKERS AND LANDED IN PHIK WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT RECIRCULATION FAN. OPERATIONAL CHECK GOOD IAW MM 21-21-1 AND 21-21-0. AIRCRAFT RETURNED TO SERVICE.

Part: FAN — BURNED (ZONE 100) · airframe 75,664 hrs · 19,277 cycles

DURING CRUISE, THE LT RECIRCULATION FAN EMITTED A BURNED ELECTRICAL ODOR. THE CREW SHUTOFF LT RECIRCULATION FAN, ODOR WENT AWAY. THEY LANDED IN WITHOUT FURTHER INCIDENT. MX REPLACED LT RECIRCULATION FAN. OPS CHECK GOOD IAW MM 21-21-1. ACFT WAS RETURNED TO SERVICE.

Part: SKIN — CRACKED (VERTICAL STAB) · airframe 75,615 hrs · 19,265 cycles

DURING PREFLIGHT, FOUND VERTICAL STABILIZER L/E CRACKED AT STA ZFS 292 CTR LINE. REPLACED CRACKED L/E WITH INTERIM REPAIR IAW FVCI DWG NR 55-10165-1.

Part: FAN — ODOR (RECIRCULATION) · airframe 75,470 hrs · 19,231 cycles

AFTER 10 MINUTES OF RUNNING THE RT RECIRCULATION FAN , THE CREW SENSED AN ELECTRICAL/ OZONE SMELL. THE RT RECIRCULATION FAN WAS TURNED OFF, CIRCUIT BREAKER WAS PULLED AND SMELL WENT AWAY. MX REPLACED THE RT RECIRCULATION FAN. OPS CHECK GOOD IAW MM 21-21-1 AND 21-21-0. ACFT WAS RETURNED TO SERVICE.

Part: FAN — ODOR (RECIRCULATION) · airframe 75,470 hrs · 19,231 cycles

AFTER 10 MINUTES OF RUNNING THE RT RECIRCULATION FAN, CREW SENSED AN ELECTRICAL/OZONE SMELL. THE RT RECIRCULATION FAN WAS SWITCHED OFF, CIRCUIT BREAKER WAS PULLED AND SMELL DISSIPATED. OPEN

Part: CONTROL BOX — DEFECTIVE (ATC) · airframe 75,229 hrs · 19,176 cycles

DURING CLIMB OUT, BOTH ATC TRANSPONDERS INOP. THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED TCAS/ATC CONTROL PANEL AND TIGHTENED CONNECTOR ON TRANSPONDER ANTENNA SWITCHING RELAY. OPS CHECK GOOD IAW MM 34-53-0. ACFT WAS RETURNED TO SERVICE.

Part: BLEED VALVE — STUCK (ENGINE) · airframe 75,164 hrs · 19,157 cycles

DURING TAKEOFF ROLL AT APPROX 90 PERCENT N2 RPM THE ENG COMPRESSOR STALLED, EPR, N2 AND EGT ROLLED BACK. THE CREW ABORTED THE TAKEOFF AND RETURNED TO PARKING. MX INSPECTED THE ENG AND FOUND THE PRESSURE RATIO BLEED CONTROL VALVE, (PRBC) STICKING. PRBC WAS LUBED AND THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE IAW ERH 70-01-01.

Part: WARNING LIGHT — FALSE ACTIVATION (PAX DOOR) · airframe 75,011 hrs · 19,113 cycles

DURING TAKEOFF ROLL CABIN DOOR WARNING LIGHT BEGAN TO BLINK. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX INSPECTED ALL CABIN DOORS. OPS CHECK GOOD IAW MM 52-70-1. ACFT WAS RETURNED TO SERVICE.

Part: REGULATOR — DEFECTIVE (ZONE 400) · airframe 74,736 hrs · 19,035 cycles

DURING CLIMB OUT FROM NR 2 ENG COMPRESSOR STALLED WITH GEAR UP, EPR 1.86 AND ANTI-ICE VALVE ON. THE CREW RETURNED TO WITHOUT FURTHER INCIDENT. MX REPLACED BOTH ANTI-ICE VALVE REGULATOR'S. OPS CHECK GOOD IAW MX MM 75-10-2. ACFT WAS RETURNED TO SERVICE.

Part: ANTENNA — DEFECTIVE (WX RADAR SYS) · airframe 74,307 hrs · 18,936 cycles

DURING CRUISE, WEATHER RADAR WILL NOT PAINT AND STABILIZATION INOP. THE CREW RETURNED TO DEPARTURE AND LANDED WITHOUT FURTHER INCIDENT. MX REPLACED WEATHER RADAR TRANSCEIVER AND RADAR ANTENNA. OPS CHECK GOOD IAW MM 34-41-1. ACFT WAS RETURNED TO SERVICE.

Part: CONNECTOR — MISWIRED (WX RADAR SYS) · airframe 74,306 hrs · 18,935 cycles

DURING CRUISE FROM WSAP WEATHER RADAR WILL NOT PAINT KNOWN WEATHER. THE CREW RETURNED TO WSAP WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND PINS 6 AND 9 REVERSED ON INDICATOR AND SHIELDS BROKEN. MAINTENANCE REPAIRED BROKEN SHIELDS AND CORRECTED PINS 6 AND 9 ON INDICATOR. OPERATIONAL CHECK GOOD IAW DACO DC8 MAINTENANCE MANUAL 20-50-1, 34-11-1, WD 34-10-10-2. AIRCRAFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — MALFUNCTIONED (WX RADAR SYS) · airframe 74,306 hrs · 18,934 cycles

DURING CLIMB OUT FROM WSAP WEATHER RADAR STABILIZATION INOP AND WILL NOT PAINT. THE CREW RETURNED TO WSAP WITHOUT FURTHER INCIDENT. MAINTENANCE SWAPPED FOG GYROS AND BLEW OUT WAVE GUIDES WITH NITROGEN, CLEANED ALL ELECTRICAL CONNECTIONS ON WAVE GUIDES AND ANTENNA. OPERATIONAL CHECK GOOD IAW MM 34-41-0, AND 34-21-1. AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — CHAFED (GALLEY)

DURING CRUISE FROM FJDG, THE CIRCUIT BREAKER PANEL ABOVE R2 DOOR AT RIGHT GALLEY BEGAN TO ARC AND HAD MOMENTARY FIRE. FOUND 20 AMP CURRENT LIMITER TRIPPED AND BURNT BUT NO CIRCUIT BREAKER TRIPPED. THE CREW REMOVED POWER FROM GALLEY AND LANDED IN WSAP WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND GALLEY POWER WIRE’S RUBBING TOGETHER CAUSING ARCING. MAINTENANCE REPAIRED AND REPOSITION WIRE'S. OPERATIONAL CHECK GOOD IAW DC8 MAINTENANCE MANUAL TEMP REVISION 20-17 PAGE 2 OF 3, DC8 20-50-1 CODE 1. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — ODOR · airframe 73,406 hrs · 18,772 cycles

DURING CRUISE FROM PKWA, THE LEFT RECIRCULATION FAN EMITTED A SMOKE ODOR. THE CREW TURNED OFF LEFT RECIRCULATION FAN. THE CREW LANDED IN PHIK WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT RECIRCULATION FAN. OPERATIONAL CHECK GOOD IAW DACO DC-8 MAINTENANCE MANUAL 21-21-1. AIRCRAFT WAS RETURNED TO SERVICE.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 73,372 hrs · 18,765 cycles

AT START OF DESCENT INTO PKWA PRESSURIZATION CONTROL LEVER AND OUTFLOW VALVE FROZE UP. THE CREW HAD TO DO AN EMERGENCY DESCENT, THE O2 MASK IN CABIN DROPPED WHEN ALT INCREASED TO 15000 FT. THE CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE IN PKWA DEFERRED PRESSURIZATION TO PHIK IAW MEL 21-10-01. MAINTENANCE IN PHIK REPLACED CABIN RATE CONTROLLER, OUTFLOW ACTUATOR. OPERATIONAL CHECK GOOD IAW MM 21-31-2, 21-31-0, 21-31-4, AND 21-31-4. ACFT WAS RETURNED TO SERVICE.

Part: FAN — SMOKE · airframe 73,266 hrs · 18,744 cycles

DURING CRUISE FROM PKWA LEFT RECIRC FAN SMOKE'S WHEN RUNNING. THE CREW TURNED OFF LEFT RECIRC FAN AND LANDED IN PHIK WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LEFT RECIRC FAN. OPERATIONAL CHECK GOOD IAW DACO DC8 MAINTENANCE MANUAL 21-21-01. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — DEFECTIVE (RECIRC) · airframe 73,065 hrs · 18,698 cycles

DURING CRUISE FROM PKWA RIGHT RECIRCULATION FAN OVERHEATED CAUSING BURNING ODOR. THE CREW TURNED OFF RIGHT RECIRCULATION FAN, THE ODOR DISSIPATED. THE CREW LANDED IN PHIK WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED RIGHT RECIRCULATION FAN. OPERATIONAL CHECK GOOD IAW DACO DC8 MAINTENANCE MANUAL 21-21-1. AIRCRAFT WAS RETURNED TO SERVICE.

Part: FAN — BURNED OUT (CABIN) · airframe 72,936 hrs · 18,670 cycles

ON TOP OF DESCENT FLIGHT ATTENDANT'S DETECTED SMOKE IN CABIN. AFTER TURNING OFF THE RT RECIRCULATION FAN THE ODOR DISSIPATED. THE CREW LANDED IN PHIK WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND FOUND LT RECIRCULATION FAN EMMITTING BURNING ODOR. MAINTENANCE REPLACED LT RECIRCULATION FAN. OPERATIONAL CHECK GOOD IAW MM 21-21-1. ACFT RETURNED TO SERVICE.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 1040.000 LONGERON 19-20 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED ANGLE DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08549, SEMAN DRAWING ED-4877, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-1 PAGES 1, 13, AND 17, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D, AND SRM 51-3-1.

Part: FRAME — DAMAGED (BS 420 L19R) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 420.000 LONGERON 19 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED ANGLE DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NR 08549, DRAWING ED-4877, DC8 NDT SPM PART 06-10-01-001, SRM 51-1-1 PAGES 1, 13, AND 17, SRM 51-1-8B, SRM 51-1-20D, AND SRM 51-3-1.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 1080.000 LONGERON 19-20 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED ANGLE DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08549, SEMAN DRAWING ED-4877, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-1 PAGES 1, 13, AND 17, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D, AND SRM 51-3-1.

Part: SKIN — CRACKED (LT WING) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD CENTER LEADING EDGE LOWER SKIN CRACKED AT STATION XS 520.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP HOLE. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED EXTERNAL DOUBLER, INTERNAL DOUBLER, AND SPACER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08543 DATED 11-18-08, SEMAN DRAWING ED-4876 DATED 11-08-08, DC8 SRM 51-1-21, SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, SRM 51-1-11, SRM 51-1-20D, AND SRM 51-3-1.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 420.000 LONGERON 17-18 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED ANGLE DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08549, SEMAN DRAWING ED-4877, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-1 PAGES 1, 13, AND 17, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D, AND SRM 51-3-1.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 280.000 LONGERON 19-20 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED ANGLE DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08549, SEMAN DRAWING ED-4877, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-1 PAGES 1, 13, AND 17, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D, AND SRM 51-3-1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT SPLICE FITTING CRACKED AT STATION 600.000-620.000 LONGERON 31 LEFT. REMOVED CRACKED SPLICE FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-1, AND DC8 SRM 51-1-8B.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME SHOWS MISDRILLED HOLE AT STATION 1400.000 LONGERON 16 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED INTERNAL DOUBLER ANGLE, AND FILLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FAA FORM 81103 NUMBER 08549 DATED 11/24/08, SEMAN DRAWING ED-4877 DATED 11/10/08, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-1 PAGE 1, 13, AND 17, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D, AND SRM 51-3-1.

Part: SKIN — CRACKED (RUDDER) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND EMPENNAGE RUDDER RIGHT SKIN CRACKED AT STATION ZR 253.00. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. PERFORMED BALANCE. FOUND WITHIN LIMITS WITH A MOMENT: 2532.0 IN-POUND. INSTALLED REPAIR PARTS IAW DC8 SRM 55-6-1 FIGURE 1 ITEM "A", DC8 SRM 55-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-9 TR 51-142, SRM 51-1-9A TR 51-141, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-4-6 PAGES 1-5,

Part: FITTING — CRACKED (FUSELAGE) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 834.000 LONGERON 22 RIGHT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, SRM 51-3-1, AND DC8 SRM 51-1-8B.

Part: FITTING — CRACKED (FUSELAGE) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT SPLICE FITTING CRACKED AT STATION 600.000 - 620.000 LONGERON 31 RIGHT. REMOVED CRACKED FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, AND SRM 51-3-1.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT RIGHT FLANGE FRAME HAS MISDRILLED HOLE AT STATION 1320.000 LONGERON 16 RIGHT. BLENDED OUT MISDRILLED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED ANGLE DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08549, SEMAN DRAWING ED-4877, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-1 PAGES 1, 13, AND 17, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D, AND SRM 51-3-1.

Part: FITTING — CRACKED (FUSELAGE) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT SPLICE FITTING CRACKED AT STATION 902.000 LONGERON 1. REMOVED CRACKED SPLICE FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW SPLICE FITTING IAW DC8 SRM 51-1-20D AND SRM 51-3-1 TABLE II PAGE 2A, DC8 SRM 51-1-21, AND DC8 SRM 51-1-8B.

Part: FITTING — CRACKED (RT MLG WW) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT MAIN LANDING GEAR WHEEL WELL FITTING CRACKED AT STATION 940.000 LONGERON 24 RIGHT. REMOVED DAMAGED FITTING FRAME. FABRICATED SPLICES, DOUBLER, AND FILLERS. PERFORMED HEAT TREATMENT. INSTALL NEW FITTING AND REPAIR PARTS IAW DC8 SRM 53-2-0 FIGURE 8 SHEETS 2, 5, AND 6, DC8 SRM 53-1-0 PAGE 1, SRM 51-1-20D, DC8 SRM 51-1-1 PAGES 1, 13, AND 17, SRM 51-1-11, AND SRM 51-3-1.

Part: FITTING — CRACKED (RT WING) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 STUB WING INNER FITTING CRACKED AT STATION XS 526.000. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. CLEANED, TREATED, AND PRIMED AREA AND FITTING. INSTALLED FITTING IAW DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2003-05, SEMAN FORM IPI NUMBER 2009017, DOUGLAS DRAWING NUMBER 5754705, DC8 SRM 51-1-8B, AND SRM 51-3-1.

Part: SKIN — CORRODED (TE FLAP) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP LEADING EDGE CORRODED AT STATION XW 2.000-91.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED NEW SKIN, AND FILLER. CLEANED, TREATED, PRIMED AREA, AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08543 DATED 11/18/08, SEMAN DRAWING ED-4878 DATED 11/11/08, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 57-2-0 PAGE 16, DC8 SRM 51-1-21, SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND SRM 51-3-1.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LT FUSELAGE CENTER SECTION FLOORBEAM LOWER HORIZONTAL FLANGES AND FLOOR PRESS PANEL CORRODED AT STATION 902.000 LBL 51. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING DAMAGED SPLICE ANGLE. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED MODIFIED SPLICE ANGLES, FILLERS, PANEL SEGMENT, EXTERNAL REPAIR DOUBLERS, STRAPS, TAPERED STRAPS, INTERNAL FINGER DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED IAW FAA FORM 8110-3 NUMBER 08543 DATED 11/18/08, SEMAN DRAWING ED-4871 DATED 11/06/08, DC8 SRM 51-1-21, SRM 51-1-20D, SRM 51-3-0, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-6,

Part: FITTING — CRACKED (FUSELAGE) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND AFT ACCESSORY COMPARTMENT FITTING CRACKED AT STATION 1530.000 LONGERON 36. REMOVED DAMAGED FITTING. CLEANED, TREATED, AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, DC8 SRM 51-1-8B, SRM 51-1-20D, AND SRM 51-3-1.

Part: SKIN — CORRODED (ZONE 300) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 74.469. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE. FOUND WITHIN LIMITS. MOMENT 1526.000 IN-POUND. INSTALLED REPAIR PARTS IAW SRM 55-4-1 FIGURE 1 SHEETS 1-2 ITEMS "E" AND "F", SRM 51-1-8 PAGES 17-18, SRM 55-2-0 PAGE 12, SRM 55-1-0 PAGE 1, SRM 51-1-21, SRM 51-1-9 TR NUMBER 51-142, SRM 51-1-9A TR NUMBER 51-141, SRM 51-1-8B, SRM 51-1-11, AND SRM 51-4-4 PAGES 1-4 TR NUMBER 51-116.

Part: SKIN — CORRODED (ZONE 300) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C-CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER SKIN CORRODED AT STA XE 29.812 - 52.825. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN, AND STIFFENER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AT STATION XE 29.000 - 77.000 IAW FAA FORM 8110-3 NUMBER 08548 DATED 11/18/08, DRAWING ED-4875 DATED 11/05/08, SRM 51-1-8 PAGES 17-18, SRM 55-2-0 PAGE 12, SRM 55-1-0 PAGE 1, SRM 51-1-21, SRM 51-1-8B, AND SRM 51-1-11.

Part: SKIN — CORRODED (ZONE 300) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 147.188A - XE 156.168. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. PERFORMED BALANCE. FOUND WITHIN LIMITS, MOMENT: 1526.0 IN-POUND. INSTALLED REPAIR PARTS IAW SRM 55-4-1 FIGURE 1 SHEETS 1-2 ITEMS "E" AND "F", SRM 51-1-8 PAGES 17-18, SRM 55-2-0 PAGE 12, SRM 55-1-0 PAGE 1, SRM 51-1-21, SRM 51-1-9 TR 51-142, SRM 51-1-9A TR 51-141, SRM 51-1-8B, SRM 51-1-11, AND SRM 51-4-4 PAGES 1-4.

Part: SKIN — CORRODED (ZONE 300) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 77.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, AND STIFFENER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AT STATION XE 29.000 - 77.000 IAW FAA FORM 8110-3 NUMBER 08548 DATED 11/18/08, SEMAN DRAWING ED-4875 DATED 11/05/08, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 55-2-0 PAGE 12, DC8 SRM 55-1-0 PAGE 1, SRM 51-1-21, DC8 SRM 51-1-8B, AND DC8 SRM 51-1-11.

Part: SKIN — CRACKED (RT WING) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER SKIN CRACKED AT STATION XRS 74.869 STRINGER 9. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN, AND FILLER PLUG. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION. TAPERED EXTERNAL DOUBLER FROM 0.160 INCH TO 0.080 INCH. CLEANED, TREATED, PRIMED AREA AND EXTERNAL DOUBLER. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-2-1 FIGURE 17, DC8 SRM 51-1-20D, SRM 57-3-2 FIGURE 13, DC8 NDT SPM PART 08, DC8 SRM 51-10-0 FIGURE 1 SHEET 20, DC8 SRM 51-1-8B, IAW DC8 SRM 51-1-12, AND SRM 51-3-1.

Part: SKIN — CORRODED (ZONE 300) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 89.719. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED EXISTING REPAIR. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE FOUND WITHIN LIMITS. MOMENT 1526.000 IN-POUND. INSTALLED REPAIR PARTS IAW SRM 55-4-1 FIGURE 1 SHEETS 1-2 ITEMS "E" AND "F", SRM 51-1-8 PAGES 17-18, SRM 55-2-0 PAGE 12, SRM 55-1-0 PAGE 1, SRM 51-1-21, SRM 51-1-9 TR NUMBER 51-142, SRM 51-1-9A TR NUMBER 51-141, SRM 51-1-8B, SRM 51-1-11, AND SRM 51-4-4 PAGES 1-4 TR NUMBER 51-116.

Part: SKIN — MISREPAIRED (RT AILERON) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT OUTBOARD AILERON LOWER HAS IMPROPER REPAIR AT STATION XW 698.000. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. PERFORMED BALANCE. FOUND WITHIN LIMITS WITH A MOMENT: 3322.9 IN-POUNDS. INSTALLED REPAIR PARTS AT STATION XA 724.000 - XW 698.000 IAW DC8 SRM 57-8-1 FIGURE 4 ITEMS "E" AND "L", DC8 SRM 57-1-0 PAGE 1, SRM 51-1-21, DOUGLAS DRAWING NUMBER 5763133, DC8 SRM 51-1-9 TR NUMBER 51-142, SRM 51-1-9A TR 51-141, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, SRM 51-1-21A, AND DC8 SRM 51-4-3 PAGES 1-4.

Part: SPAR CAP — CRACKED (RT WING) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING UPPER REAR SPAR CAP VERTICAL FLANGE CRACKED AT STATION XRS 554.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP HOLE. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND AFTER DRILLING STOP HOLE. FABRICATED REPAIR ANGLE, STIFFENER, SPACERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08543 DATED 11/18/08, SEMAN DRAWING ED-4879 DATED 11/07/08, DC8 SRM 51-1-20D, SRM 51-1-21, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-12, DC8 SRM 51-1-11, AND SRM 51-3-1.

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE UPPER SKIN CORRODED AT STATION XE 29.812. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. CLEANED, TREATED, PRIMED AREA. INSTALLED NEW SKIN IAW SRM 55-3-1 FIGURE 1 SHEETS 1-2, SRM 51-1-8 PAGES 17-18, SRM 55-2-0 PAGE 12, SRM 55-1-0 PAGE 1, SRM 51-1-21, AND SRM 51-1-8B.

Part: SKIN — CORRODED (ZONE 300) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT ELEVATOR TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 55.062. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, FINGER DOUBLER. BONDED PARTS AS NEEDED. CLEANED, TREATED, PRIMED AREA AND REPAIR PART. PERFORMED BALANCE FOUND WITHIN LIMITS MOMENT 1526.000 IN-POUND. INSTALLED REPAIR PARTS IAW SRM 55-4-1 FIGURE 1 SHEETS 1-2 ITEMS "E" AND "F", SRM 51-1-8 PAGES 17-18, SRM 55-2-0 PAGE 12, SRM 55-1-0 PAGE 1, SRM 51-1-21, SRM 51-1-9 TR NUMBER 51-142, SRM 51-1-9A TR NUMBER 51-141, SRM 51-1-8B, SRM 51-1-11, AND SRM 51-4-4 PAGES 1-4 TR NUMBER 51-116.

Part: SKIN — CORRODED (ZONE 300) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER SKIN CORRODED AT STATION XE 52.825-75.672. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN, STIFFENER. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AT STA XE 29.000 - 77. 000 IAW FAA FORM 8110-3 NUMBER 08548 DATED 11/18/08, DRAWING ED-4875 DATED 11/05/08, SRM 51-1-8 PAGES 17-18, SRM 55-2-0 PAGE 12, SRM 55-1-0 PAGE 1, SRM 51-1-21, SRM 51-1-8B, AND SRM 51-1-11.

Part: SKIN — MISREPAIRED (ZONE 100) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND DOUBLER BELOW MAIN CARGO DOOR OPENING HAS IMPROPER REPAIR AT STATION FS 400 LONGERON 25 LEFT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED NEW SKIN, INTERNAL AND EXTERNAL DOUBLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08548 DATED 11/18/08, SEMAN DRAWING ED-4868 DATED 10/23/08, DC8 SRM 51-1-21, SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND SRM 51-3-1.

Part: SKIN — CORRODED (ZONE 500) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LT WING LOWER CENTER OUTER LEADING EDGE SKIN CORRODED AT STATION XFS 280.250.REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED NEW SKIN, FILLER. CLEANED, TREATED, PRIMED AREA, AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08548 DATED 11/18/08, DRAWING ED-4872 DATED 11/03/08, SRM 51-1-21, SRM 51-1-20D, SRM 51-1-8 PAGES 17-18, SRM 57-2-0 PAGE 16, NDT SPM PART 06-10-01-001, SRM 51-1-8B, SRM 51-1-11, SRM 51-3-0, AND SRM 51-3-1.

Part: SKIN — CORRODED (ZONE 500) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING OUTBOARD OUTER LEADING EDGE UPPER EXTERNAL SKIN CORRODED AT STATION XW 762.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, AND FILLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 08548, DRAWING ED-4874 DATED 11/06/08, SRM 51-1-8 PAGES 17-18, SRM 57-2-0 PAGE 16, SRM 51-1-21, SRM 51-1-20D, NDT SPM PARTS 06-10-01-001, SRM 51-1-8B, SRM 51-1-11, SRM 51-3-0, AND SRM 51-3-1.

Part: SKIN — CORRODED (ZONE 500) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C-CHECK INSPECTION, FOUND LT WING INBOARD OUTER L/E UPPER EXTERNAL SKIN CORRODED AT STATION XFS 560.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND NO CORROSION FOUND. FABRICATED DOUBLER, FILLER. CLEANED, TREATED, PRIMED AREA, AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 NR 08549 DATED 11/24/08, DRAWING ED-4873 DATED 11/03/08, SRM 51-1-21, SRM 51-3-0, SRM 51-1-8 PAGES 17-18, SRM 57-2-0 PAGE 16, NDT SPM PART 06-10-01-001, SRM 51-1-8B, SRM 51-1-11, AND SRM 51-3-1.

Part: SKIN — CORRODED (ZONE 100) · airframe 72,846 hrs · 18,649 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND FUSELAGE EXTERNAL SKIN CORRODED AT STATION 1530.000 LONGERON 35 RIGHT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. FABRICATED NEW SKIN SEGMENT, SPLICE, INTERNAL DOUBLERS, INTERNAL DOUBLERS, INTERNAL FINGER DOUBLERS, LONGERON STRAPS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW SRM 53-2-1 FIGURE 8 SHEET 1, SRM 51-1-8B PAGES 17-18, SRM 53-2-0 PAGE 2P, SRM 51-1-21, SRM 51-1-20D, SRM 53-2-1 FIGURE 8 SHEET 3 TR 53-173, SRM 53-5-2 FIGURE 1, SRM 51-1-8B. SRM 51-1-11, AND SRM 51-3-1.

Part: LINE — LOOSE (PT 2)

DURING TAKEOFF ROLL, NR (1) ENGINE WOULD NOT ACCELERATE PAST 78 PERCENT. NR 2 WITH CORRESPONDING LOW N1, FUEL FLOW AND EGT. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS. MAINT INSPECTED AND FOUND LOOSE PT2 LINE ON PRBC VALVE. MAINT RECONNECTED LINE. OPERATIONAL CHECK GOOD. ACFT WAS RETURNED TO SERVICE. (K)

Part: ENGINE — OIL CONSUMPTION (NR 3)

DURING CRUISE, THE CREW SHUTDOWN NR 3 ENGINE DUE TO OIL QUANTITY DROPPING TO LESS THAN ONE GALLON, OIL PRESSURE GAUGE FLUCTUATING, OIL TEMP WAS ABOVE 115C, OIL PRESSURE LIGHT INTERMITTENT, THE CREW LANDED WITHOUT FURTHER INCIDENT. AC WAS AUTHORIZED FERRY FLIGHT FOR MAINTENANCE. MAINT CONFIRMED OIL RESERVOIR IS FULL AND AIRCRAFT SAFE FOR FLIGHT. ENGINE CHANGE IN WORK. (K)

Part: COMPASS — DEFECTIVE (COCKPIT) · airframe 71,916 hrs · 18,398 cycles

DURING CRUISE FROM KBWI, THE CREW PERFORMED COMPASS RATING CHECK, BOTH COMPASS SYSTEM HAD EXCESSIVE DRIFT (20 DEGREE IN 30 MIN). THE CREW LANDED IN CYYR WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED FOG GYRO COMPASS SYSTEM. OPERATIONAL CHECK GOOD IAW DC8 MAINTENANCE MANUAL 34-11-1. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SPEAKER — ODOR (COCKPIT) · airframe 71,698 hrs · 18,340 cycles

DURING CRUISE FROM PKWA, THE CREW NOTICE A ELECTRICAL ODOR COMING FROM THE RIGHT RECIRC FAN. THE CREW TURNED OFF THE RIGHT RECIRC FAN AND LANDED WITHOUT INCIDENT IN PHIK. MAINTENANCE INSPECTED AND FOUND THAT THE ELECTRICAL ODOR WAS COMING FROM THE FIRST OFFICER'S OVERHEAD PANEL SPEAKER. MAINTENANCE DEFERRED FIRST OFFICERS SPEAKER IAW ATI MEL 23-1 TO KMCC. MAINTENANCE IN KMCC REPLACED FIRST OFFICER'S OVERHEAD SPEAKER OPERATIONAL CHECK GOOD IAW DACO DC8 23-50-0. AIRCRAFT WAS RETURNED TO SERVICE.

Part: PITOT TUBE — DAMAGED · airframe 70,935 hrs · 18,177 cycles

DURING CLIMB-OUT FROM PHIK, THE CREW NOTICED THE PITOT HEATER INOP LIGHT ILLUMINATED, ZERO AMPS INDICATED ON THE FIRST OFFICER'S PITOT TUBE POSITION. THE CREW RETURNED TO PHIK, MADE 50 DEGREES FLAP EMERGENCY OVERWEIGHT LANDING AND LANDED WITH OUT INCIDENT. MAINTENANCE REPLACED FIRST OFFICER'S PITOT TUBE PERFORMED LEAK CHECK WAS GOOD, AND PERFORMED A OVERWEIGHT LANDING INSPECTION IAW DACO DC8 MAINTENANCE MANUAL 34-12-0 AND ATI JOB CARD 13.01-5. AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOOR — UNLOCKED (ZONE 800) · airframe 70,600 hrs · 18,108 cycles

DURING TAKEOFF FROM WSAP AT SIXTY KNOTS, THE DOOR WARNING LIGHT (MASTER WARNING) ILLUMINATED. THE CREW ABORTED TAKEOFF WITHOUT INCIDENT AND RETURNED TO BLOCKS. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND R-2 DOOR UNLOCKED. MAINTENANCE RESECURED THE DOOR AND WARNING LIGHT WENT OUT. MAINTENANCE PERFORMED UNSCHEDULED MAINTENANCE INSPECTION FOR REJECTED TAKEOFF IAW DC8 MAINTENANCE MANUAL 13.01-5. AIRCRAFT WAS RETURNED TO SERVICE.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 70,204 hrs · 18,029 cycles

DURING CLIMB-OUT FROM KTOL, THE CREW NOTICED HYDRAULIC QUANITY STARTED DROPPING RAPIDLY TOWARD EMPTY. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND PRESSURE FLEX LINE LEAKING AT NUMBER TWO ENGINE DRIVEN HYDRAULIC PUMP. MAINTENANCE TIGHTEND THE FLEX LINE, RESERVICED HYDRAULIC SYSTEM, OPERATIONAL AND LEAK CHECK WAS GOOD, IAW DACO DC8 MAINTENANCE MANUAL 29-10-12 AND ATI ERH 70.01. AIRCRAFT RETURNED TO SERVICE.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 70,203 hrs · 18,028 cycles

DURING CLIMB-OUT FROM KTOL, THE CREW NOTICED HYDRAULIC QUANTITY DECREASING. THE CREW RETURNED TO KTOL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THAT THE RUDDER HYDRAULIC PUMP WAS DEFECTIVE. MAINTENANCE REMOVED AND REPLACED THE RUDDER HYDRAULIC PUMP, AND RESERVICED HYDRAULIC SYSTEM. MAINTENANCE PERFORMED OPERATIONAL AND LEAK CHECK. OPERATIONAL CHECK WAS GOOD AND NO LEAKS DETECTED IAW MAINTENANCE MANUAL 27-24-2. AIRCRAFT RETURNED TO SERVICE.

Part: AUDIO PANEL — DEFECTIVE (COCKPIT) · airframe 70,211 hrs · 18,031 cycles

DURING FLIGHT FROM RJTY THE CREW SMELLED SMOKE, THE FIRST OFFICER'S AUDIO CIRCUIT BREAKER OPENED THE SMELL OF SMOKE STOPPED. THE CREW LANDED IN WSAP WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FIRST OFFICER'S AUDIO SELECT PANEL IAW DACO DC8 MAINTENANCE MANUAL 23-50-1. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: SPEAKER — DEFECTIVE (COCKPIT) · airframe 70,211 hrs · 18,031 cycles

DURING TAXI OUT AT WSAP, THE CREW SMELLED SMOKE, THEN THE FIRST OFFICER'S AUDIO CIRCUIT BREAKER OPEN, THE FIRST OFFICER'S OVER HEAD SPEAKER WAS HOT TO TOUCH, THE CREW RETURNED TO BLOCK WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FIRST OFFICER'S OVERHEAD SPEAKER, IAW DACO MAINTENANCE MANUAL 23-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: TRANSCEIVER — DEFECTIVE (HF SYSTEM) · airframe 70,022 hrs · 17,992 cycles

DURING FLIGHT FROM KSUU, THE CREW NOTICE THAT BOTH NR 1 AND NR 2 HF TRANSCEIVER WAS NOT TRANSMITTING OR RECEIVEING. THE CREW RETURNED TO KSUU WITHOUT INCIDENT. MAINTENANCE FOUND BOTH NR 1 AND NR 2 HF TRANSCEIVER WERE INOP. MAINTENANCE REPLACED BOTH HF TRANSCEIVER, OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.

Part: LONGERON — CRACKED (ZONE 100) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT, LONGERON-35 RIGHT CRACKED AT STATION 1100.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED LONGERON SEGMENT. FABRICATED NEW SEGMENT OF LONGERON AND EXTERNAL DOUBLER. INSTALLED NEW REPAIR PARTS NEW FASTENERS IAW FORM 8100-9 DATED 03/15/2007, BOEING MESSAGE NUMBER 1-296019761-5 DATED 03/15/2007, DC8 SRM 53-2-2 FIGURE 13 TR NUMBER 53-191 DATED 10/15/2003, DC8 SRM 51-1-21, DC8 SRM 53-2-2 FIGURE 13 TR NUMBER 53-191, BOEING MESSAGE NUMBER 1-296019761-5 (SKETCH JCTO4049 FIGURE 1AND 2), SEMAN DRAWING ED-4470,DC8 SRM 53-4-1 FIGURE 44B SHEET 1 ITEM "R", AND DC8 SRM 51-2-0 FIGURE 50 SHEET 72B.

Part: LONGERON — CRACKED (ZONE 100) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND AFT CARGO COMPARTMENT, LONGERON-36 CRACKED AT STATION 1100.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED LONGERON SEGMENT. FABRICATED NEW SEGMENT OF LONGERON AND EXTERNAL DOUBLER. INSTALLED NEW REPAIR PARTS IAW FORM 8100-9 DATED 03/15/2007, BOEING MESSAGE NUMBER 1-296019761-5 DATED 03/15/2007, DC8 SRM 53-2-2 FIGURE 13 TR NUMBER 53-191, DATED 10/15/2003, DC8 SRM 51-1-21, BOEING MESSAGE NUMBER 1-296019761-5 (SKETCH JCTO4049 FIGURE 1AND 2), SEMAN DRAWING ED-4470, AND DC8 SRM 53-4-1 FIGURE 44B SHEET 1 ITEM "R", DC8 SRM 51-2-0 FIGURE 50 SHEET 72B.

Part: PANEL — CORRODED (ELEVATOR) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER ELEVATOR UPPER PANEL CORRODED, BETWEEN STATION XE 65.158 AND XE 132.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN. BALANCE ELEVATOR FOUND WITHIN OF TOLERANCE LIMITS, MOMENT:1521.12N-LBS IAW DC8 SRM 51-1-8 PAGES 17AND18, DC8 SRM 55-2-0 PAGE 12,DC8 SRM 55-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 55-4-1 FIGURE 1 SHEET 1AND 2 ITEM "E"AND"F,"DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-1-21.

Part: FITTING — CRACKED (ZONE 100) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT, CRACKED ON FITTING BETWEEN STATION 798.000 AND LEFT BOTTOM LINE 24". REPLACED CRACKED FITTING N/P IAW SRM 51-1-20D, AND SRM 51-3-1.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING, INBOARD FLAP LOWER PANEL HAS A NON STANDARD REPAIR, AT STATION XW 3.000 TO XW 50.000. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIGURE 1 PAGE 2 ITEM "B"AND "L", DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-1-21.

Part: FITTING — CRACKED (ZONE 100) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING FRAME CRACKED AT STATION 759.000, LONGERON 18 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM THE REPAIR. PERFORMED STOP HOLE ON CRACK END. PERFORMED NDT INSPECTION. NO CORROSION OR CRACK PROGRESSION FOUND. FABRICATED (HORIZONTAL FLANGE) (VERTICAL FLANGE). PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW FAA FORM 8110-3 NUMBER 07058 DATED 02-15-07, SEMAN DRAWING NUMBER ED-4462 DATED 02-13-07, AND EO SEMAN NUMBER 2007219 DATED 02-15-07, DC8 SRM 51-1-20D, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, FORM SEMAN 242-2, DC8 SRM 51-1-1 PAGES 1, 13, 17, DC8 SRM 51-1-8

Part: SKIN — CRACKED (ZONE 600) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, RT WING OTBD L/E OUTER SECTION SHOWS 1" CRACKED AT STA XFS 885.000 (NEAR EXISTING REPAIR). PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 NR 07110 DATE 03/14/07, SEMAN DRAWING NR ED-4463. DATE 02-15-07 AND EO SEMAN NR 2007221 DATE 03-14-07. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-3-0 AND DC8 SRM 51-1-21. CUT OUT DAMAGED AREA IAW SEMAN DRAWING NR ED-4463. PERFORMED INSPECTION NDT-IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK, NO CORROSION, AFTER CUT OUT DAMAGED AREA ATTACHED FORM SMN 242-2. FABRICATED REPAIR DOUBLER AL7075-T6 0.063 AND INTERNAL DOUBLER AL7075-T6 0.025 AND FILLER SKIN AL 7075-T6 0.050 AND EXTERNAL FILLER AL 7075 T6 0.063 IAW SEMAN DRAWING NR ED-4463. CL

Part: LONGERON — MISREPAIRED (ZONE 100) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD BELLY PIT LONGERON 30 RIGHT HAS IMPROPER REPAIR AT STATION 460.000. REMOVED FASTENERS AS NEEDED TO PERFORM THE REPAIR. REMOVED DAMAGED LONGERON SEGMENT. FABRICATED LONGERON SEGMENT AND SPLICES. CLEANED,TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 53-2-2 FIGURE 4 PAGE 6, DC8 SRM 51-1-20D, DC8 SRM 53-2-2 FIGURE 4A, DC8 SRM 53-4-1 FIGURE 29B SHEET 1 ITEM "A", DC8 SRM 51-2-0 FIGURE 50 SHEET 51, DC8 SRM 53-2-2 FIGURE 10 SHEET 1 AND 3 TR NUMBER 53-153 DATED 12-10-02, DC8 SRM 53-2-2 FIGURE 10 SHEET 4 TR NUMBER 53-193 DATED 03-15-04, DC8 SRM 51-2-0 FIGURE 50 SHEET 62, DC8 SRM 51-1-8B, DC8 SRM 53-2-2 FIGURE 10 TR NUM

Part: BEAM — CRACKED (BS 1540) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, MAIN CARGO UPPER FLANGE BEAM WITH CRANK 1" AT STA 1540.000 RBL 39". PERFORMED MAJOR REPAIR IAW SRM 51-2-1 FIG 1 SHEET 8,12 TR NR 51-130 DATE 01/26/04. REMOVED FASTENERS IAW SRM 51-1-21, CUT DAMAGED AREA AND FABRICATED NEW FLANGE SEGMENT (AL 7075-T6 0.125) AND (02EA) REPAIR ANGLES OF (EXTRUSION 7075T6 0.125 P/N S1325214) AND FILLER AL 7075-T6.IAW SRM 51-2-1 FIG 1, SHEET 8,12, TR NR 51-130 SRM 53-5-2 FIG 3, SHEET 2, ITEM "D" SRM 51-2-0 FIG 50, SHEET 61. CLEANED TREATED AND PRIMED AREA AND REPAIR PARTS IAW SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW SRM 51-1-11. INSTALLED REPAIR PARTS IAW SRM 51-2-1, FIG 1, SHEET 8, 12, AND SRM 51-1-20D, 51-3-1. (TORQUE)

Part: SKIN — MISREPAIRED (RT WING) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C-CHECK INSPECTION, FOUND RT WING OUTBOARD SECTION LEADING EDGE HAS A NONE STANDARD REPAIR DOUBLER AT STATION XFS 710. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND AFTER NDT INSPECTION. FABRICATED REPAIR DOUBLER CLEANED,TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS. IAW FAA FORM 8110-3 NUMBER 07110 DATED 03-14-07, SEMAN DRAWING NUMBER ED-4454 DATE 02-19-07, E.O SEMAN NUMBER 2007198 DATE 03-14-07, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, SEMAN 242-2, DC8 SRM 51-1-8B, . DC8 SRM 51-1-11, DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1

Part: SPLICE — CORRODED (ZONE 600) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, NR 4 ALT TANK SPLICES FITTING SHOW CORROSION OUT OF LIMITS AT STA XRS 435 NEAR S60. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PAGE 16. REMOVED CORRODED SPLICE FITTING IAW DC8 SRM 51-1-20D. FABRICATED SPLICE FITTING IAW ATI REPAIR SPECIFICATION NR 2003-05, DWG DOUGLAS NR 3640143. PERFORMED HEAT TREATMENT IAW DC8 SRM 51-1-1 PAGES 1, 13, 17. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 08-00-02 TO 07. CLEANED, TREATED AND PRIMED AREA & SPLICE FITTING. IAW DC8 SRM 51-1-8B. INSTALLED SPLICE FITTING. IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1. L

Part: FITTING — BROKEN (BS 440-460) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND FORWARD BELLY PIT FITTING BROKEN, BETWEEN STATION 440.000 AND STATION 460.000, L-31L. REMOVED DAMAGED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-20D AND DC8 SRM 51-3-1.

Part: FITTING — CRACKED (ZONE 100) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C-CHECK INSPECTION, MAIN CARGO BATHTUB FITTING SHOWS CRACK 2" AT STA 1530, L26R. REMOVED AND REPLACED MAIN CARGO BATHTUB FITTING AT STA. 1530.000 L-26R (P/N 4641324U501) IAW DC8 SRM 51-1-21.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND NUMBER 1 STUB WING SKIN LOWER PART HAS A NON STANDARD REPAIR AT STATION XFS 562.5. REMOVED EXISTING NON STANDARD REPAIR. PERFORMED STOP HOLE ON CRACK END. FABRICATED EXTERNAL DOUBLER AND INTERNAL DOUBLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS. IAW DC8 SRM 57-2-1A FIGURE 1 PAGE 3, DC8 SRM 51-1-21, DC8 SRM 51-1-1 PAGES 1,13,17, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1.

Part: SKIN — CORRODED (ZONE 300) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION FOUND LEFT HAND. ELEVATOR UPPER SKIN CORRODED AT STATION XE65.158. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS FROM STATION XAR0.000 TO XE132.000. BALANCED ELEVATOR. FOUND WITHIN LIMITS, MOMENT:1521.12 IN-LBS. IAW DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 55-2-0 PAGE 12, DC8 SRM 55-1-0 PAGE 1, DC8 SRM 55-4-1 FIGURE 1 SHEET 1-2 ITEM "E" AND "F", DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-21 AND DC8 SRM 51-4-4 PAGES 1-3.

Part: FITTING — CRACKED (ZONE 100) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C-CHECK INSPECTION, FOUND MAIN CARGO BATHTUB FITTING CRACKED AT STATION 1530 L34L. REMOVED AND REPLACED BATHTUB FITTING. IAW DC8 SRM 51-1-21.

Part: FITTING — CRACKED (ZONE 100) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND IN MAIN CARGO COMPARTMENT A CRACKED ON FITTING AT STATION 781.000 LEFT BOTTOM LINE 24". REPLACED CRACKED FITTING IAW DC8 SRM 51-1-21, DC8 SRM 51-1-20D AND DC8 SRM 51-3-1.

Part: SKIN — CORRODED (ELEVATOR) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT HAND HORIZONTAL STABILIZER ELEVATOR UPPER SKIN CORRODED FROM STATION XE 149.000 TO XE 222.875.REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED CORRODED SKIN. FABRICATED NEW SKIN AND INTERNAL DOUBLER BONDED REPAIR PARTS AS NEEDED. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS. PERFORM BALANCE. FOUND WITHIN OF TOLERANCE LIMITS. MOMENT:1521.12 IN-LBS.IAW DC8 SRM 55-4-1 FIGURE 1 SHEET 1 & 2 ITEM E & F DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 55-2-0 PAGE 12,DC8 SRM 55-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06,DC8 SRM 51-1-8B, AND DC8 SRM 51-1-1.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP LOWER SKIN HAS A NON STANDARD REPAIR AT STATION WX 84.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. FABRICATED NW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-5 FIGURE 1 SHEET 1 AND 2, DC8 SRM 51-1-21,DC8 SRM 57-7-1 FIGURE 1 ITEM "B" AND "L", DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06,DC8 SRM 51-1-8B, AND DC8 SRM 51-1-11.

Part: PANEL — CORRODED (HORIZONTAL STAB) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C-CHECK INSPECTION, RT HORIZONTAL STABILIZER, T/E LWR PANEL, CORRODED STA XE 149.906 - STA XE 220.343. PERFORMED MAJOR REPAIR IAW DC8 SRM 55-3-1 FIG 1, SHEET 1 AND 2. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 55-2-0, PAGE 12. REMOVED CORRODED PANEL PLATING IAW DC8 SRM 55-1-0 PAGE 1, DC8 SRM 51-1-21. FABRICATED PANEL PLATING WITH PLATING & DOUBLER, BOTH FROM (AL 7075-T6-0.025") IAW DC8 SRM 55-3-1 FIG 1, SHEET 1 AND 2, ITEM S, T. BONDED BOTH PARTS IAW DC8 SRM 51-1-9, TR 51-142, DATE 04-05-06. CLEANED, TREATED AND PRIMED AREA AND PANEL PLATING INTERNAL PART IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED PANEL PL

Part: FITTING — CRACKED (BS 781) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT, CRACKED ON FITTING BETWEEN STATION 781.000 RIGHT BOTTOM LINE 24". REPLACED FITTING IAW SRM 51-1-21, SRM 51-1-20D, AND SRM 51-3-1, EO NUMBER 53-DC8-2235.

Part: SKIN — CORRODED (ELEVATOR) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C-CHECK INSPECTION, FOUND LT HORIZONTAL STABILIZER ELEVATOR LOWER SKIN CORRODED & UNBONDED, BETWEEN STATION XE 77.000 & XE 132.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED SKIN AND INTERNAL DOUBLER. CLEANED, TREATED & PRIMED AREA & REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS.. PERFORMED BALANCE. FOUND WITHIN OF TOLERANCE LIMITS. MOMENT:1521.12 IN-LBS IAW DC8 SRM 55-4-1 FIGURE 1 SHEET 1 AND 2,DC8 SRM 51-1-8 PAGES 17 & 18, DC8 SRM 55-2-0 PAGE 12, DC8 SRM 55-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 55-4-1 FIGURE 1 SHEET 1 & 2 ITEM E & F, DC8 SRM 51-1-9 TR NR 51-142 DATED 04-05-06, DC8 SRM 51-1

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER PANEL HAS CORROSION, STATION XE 221.000 AND XE 272.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-8 PAGES 17 AND 18, DC8 SRM 55-2-0 PAGE 12, DC8 SRM 55-1-0 PAGE 1, DC8 SRM 51-1-21,DC8 SR 55-3-1 FIGURE 1 SHEET 1 AND 2 ITEM "S"AND "T", DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06, DC8 SRM 51-18B, AND DC8 SRM 51-1-11.

Part: SKIN — CORRODED (TAIL CONE) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND TAIL CONE LOWER SKIN CORRODED STATION XFS 1813.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 53-2-0 FIGURE 1D SHEET 3 PAGE 2K, DC8 SRM 51-1-21, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 53-5-2 FIGURE 2 PAGE 3 ITEM "G", DC8 SRM 51-1-8B, AND DC8 SRM 51-1-11.

Part: FITTING — CRACKED (ZONE 100) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT, CRACKED ON FITTING BETWEEN STATION 759.000, LEFT BOTTOM LINE 24". REPLACED CRACKED FITTING IAW SRM 51-1-21, SRM 51-1-20D, SRM 51-3-1, AND EO NUMBER 53-DC8-2235.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE SLOT VANE UPPER SKIN HAD NON STANDARD REPAIR AT STATION XS 520.000. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS FROM STATION XS 520.000 IAW FAA FORM 8110-3, NUMBER 07042 DATED 02-07-07, SEMAN DRAWING NUMBER ED-4453, DATED 02-02-07, EO SEMAN NUMBER 2007197 DATED 02-07-07, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, FORM SEMAN 242-2, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-20D, AND DC8 SR

Part: SKIN — MISREPAIRED (ZONE 300) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER.- LEADING EDGE OUTER SKIN NON STANDARD REPAIR AND CORROSION AT STATION XFS 178.750. REMOVED SKIN WITH EXISTING NON STANDARD REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACKS OR CORROSION FOUND. FABRICATED NEW SKINS AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS FROM STATION XFS 178.750. IAW FAA FORM 8110-3, NUMBER 07110 DATED 03-14-07,SEMAN DRAWING NUMBER ED-4451, DATED 02-14-07,EO SEMAN NUMBER 2007195 DATED 03-14-07, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 55-2-0 PAGE 12, DC8 NDT SPM PART 06-10-0

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING CENTER LEADING EDGE SLOT VANE UPPER SKIN HAD NON STANDARD REPAIR AT STATION XOLDI 6.225. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACKS OR CORROSION FOUND. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS FROM STATION XOLDI6.225 IAW FAA FORM 8110-3 NUMBER 07042 DATED 02-07-07, SEMAN DRAWING NUMBER ED-4452 DATED 02-06-07, EO SEMAN NUMBER 2007196 DATED 02-07-07, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-0,DC8 NDT SPM PART 06-10-01-001, FORM SEMAN 242-2, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 5

Part: SKIN — MISREPAIRED (ZONE 300) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT HORIZONTAL STABILIZER. LEADING EDGE OUTER SKIN NON STANDARD REPAIR AT STATION XFS 178.750. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA.. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED,TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07058 DATED 02-15-07, SEMAN DRAWING NUMBER ED-4450 DATED 02-14-07 AND EO SMN NUMBER 2007194 DATED 02-15-07, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001,FORM SMN 242-2, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, LEFT OUTBOARD AILERON UPPER SKIN NON STANDARD REPAIR, STATION XA 646.000. REMOVED SKIN WITH EXISTING REPAIR. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIRED PARTS FROM STATION XW 546.000 TO XA 742.000. BALANCED AILERON, FOUND WITHIN TOLERANCE. MOMENT:3345.41 IN-LBS IAW DC8 SRM 51-1-21, DC8 SRM 57-8-1 FIGURE 4, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 57-8-1 FIGURE 4 ITEM "F" AND "G", DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06, DC8 SRM 51-1-8B, DC8 SRM 51-1-11.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP LOWER SKIN HAS A NON STANDARD REPAIR, AT STATION XW 115.000. REMOVED PLATING WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKIN AND REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND PLATING. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN AND REPAIR PARTS IAW DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIGURE 1 PAGE 2 ITEM "D", DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-1-21.

Part: VANE — DAMAGED (ZONE 600) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE SLOT VANE HOLES ELONGATED, BETWEEN STATION XOLDI 6.225 AND XS 435.789. REMOVED EXISTING INTERNAL DOUBLER. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07042 DATED 02-07-07, SEMAN DRAWING NUMBER ED-4458 DATED 02-02-07, EO SEMAN NUMBER 2007209 DATE 02-07-07, DC8 SRM 51-1-21, DC8 SRM 51-3-0, SEMAN DRAWING NUMBER ED-4458,DC8 NDT SPM PART 06-10-01-001, FORM SMN 242-2, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-20D, AND DC8 SRM

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING, OUTBORD FLAP UPPER SKIN NON STANDARD REPAIR, AT STATION XF 210.000. REMOVED PANEL PLATING WITH EXISTING NON STANDARD REPAIR. FABRICATED NEW SKINS AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED PANEL PLATING INTERNAL PART AND AREA. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS FROM STATION XF 210.000 IAW DC8 SRM 57-7-1 FIGURE 4 PAGE 2 TR NUMBER 57-94 DATED 10-01-02, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 4 PAGE 6 ITEM "P"AND "Q, DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06,DC8 SRM 51-18B, DC8 SRM 51-1-11, AND DC8 SRM 51-1-21.

Part: SKIN — CORRODED (ZONE 200) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT UPPER SKIN CORRODED AT STATION XFS1730.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS AND NEW FASTENERS IAW DC8 SRM 53-2-1 FIGURE 7 SHEET 1 AND 5, DC8 SRM 51-1-21, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 53-5-2 FIGURE 1 ITEM "B", DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-20D AND DC8 SRM 51-3-1.

Part: SKIN — CORRODED (ZONE 300) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, RIGHT HORIZONTAL STABILIZER INBOARD LEADING EDGE OUTER SKIN CORRODED, STATION XFS 47.500. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS FROM STATION XFS 47.500 IAW FAA FORM 8110-3 NUMBER 07058 DATED 02-15-07, SEMAN DRAWING NUMBER ED-4459 DATED 02-14-07, EO SEMAN NUMBER 2007211 DATE 02-15-07, SEMAN NUMBER 2007211 DATE 02-15-07, SEMAN DRAWING NUMBER ED-4459 DATED 02-14-07, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, DC8 SRM 51-3-1, DC8 NDT SP

Part: SKIN — CORRODED (ZONE 200) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT UPPER SKIN CORRODED AT STATION 1730.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 53-5-2 FIGURE 1 ITEM "B", DC8 SRM 51-1-8B, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 53-2-1 FIGURE 7 SHEET 1 AND 5, DC8 SRM 51-1-21, DC8 SRM 51-1-20D AND DC8 SRM 51-3-1.

Part: PANEL — MISREPAIRED (ZONE 500) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, LEFT WING OUTBORD AILERON LOWER PANEL NON STANDARD REPAIR, BETWEEN STATION XA 650.000 AND XA 693.000. REMOVED SKIN WITH EXISTING NON STANDAR REPAIR. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED PARTS, FROM STATION XW 546.000 TO XA 724.000. BALANCED AILERON, FOUND WITHIN TOLERANCE. MOMENT: 3345.41 IN-LBS IAW DC8 SRM 57-8-1 FIGURE 4, ITEM "E" AND "L", DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-4-4.

Part: SKIN — BROKEN (ZONE 500) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT WING INBOARD FLAP, UPPER SKIN BROKEN AT STATION XCW 64.000. REMOVED DAMAGED PANEL PLATING. FABRICATED NEW SKIN AND INTERNAL DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND PANEL PLATING INTERNAL PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 1 PAGE 2, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 1 PAGE 2 ITEM "A"AND "L" DC8 SRM 51-1-9 TR NUMBER 51-142 DATED 04-05-06, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-1-21, DC8 SRM 51-1-21A.

Part: SKIN — MISREPAIRED (RT WING) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING OUTBOARD LEADING EDGE OUTER SECTION HAS A NON STANDARD REPAIR, BETWEEN STATION XFS 710.000 AND XFS 716.250. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW SKIN AND REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07110 DATED 03-14-07, SEMAN DRAWING NUMBER ED-4454 DATED 02-19-07 AND EO SEMAN NUMBER 2007198 DATED 03-14-07, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, FORM SEMAN 242-2, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-20D,

Part: FITTING — CRACKED (ZONE 200) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING FRAME, CRACKED AT STATION 759.000, LONGERON 18 LEFT. REMOVED FASTENERS. PERFORMED STOP HOLE ON CRACK END. PERFORMED NDT INSPECTION. NO CORROSION OR CRACK PROGRESSION FOUND. FABRICATED REPAIR ANGLE (HORIZONTAL FLANGE) AND (VERTICAL FLANGE) AND FILLER. PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS FROM STATION 759.000 IAW FAA FORM 8110-3, NUMBER 07058 DATED 02-15-07,SEMAN DRAWING NUMBER ED-4461 DATED 02-13-07,EO SEMAN NUMBER 2007220 DATED 02-15-07, DC8 SRM 51-1-20D, DC8 SRM 51-3-0, SEMAN DRAWING NUMBER ED-4461, DC8 NDT SPM PART 06-10-01-001, FORM SEMAN 242-2, DC8 SRM 51-1-1 PAGE

Part: DOOR FRAME — CRACKED (ZONE 800) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE "A" DOOR AFT LOWER JAMB CORNER CRACKED. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND, AFTER TRIM OUT. FABRICATED REPAIR DOUBLER AND REPAIR TRIPLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW AD-2005-18-07, SB DC8-53-078, DRAWING DOUGLAS SR08530019 AND 5750776, DRAWING DOUGLAS SR08530019, DC8 NDT SPM PART 06-10-01-001, FORM SMN 242-2, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1.

Part: VANE — MISREPAIRED (ZONE 600) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING CENTER LEADING EDGE SLOT VANE HAS A NON STANDARD REPAIR, BETWEEN STATION XS 515.720 AND XS 520.168. REMOVED EXISTING NON STANDARD REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 NUMBER 07042 DATED 02-07-07, SEMAN DRAWING NUMBER ED-4457 DATED 02-02-07, EO SEMAN NUMBER 2007208 DATED 02-07-07, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-0, DC8 NDT SPM PART 06-10-01-001, FORM SMN 242-2, DC8 SRM 51-1-8B, DC8 SRM 51-1-11, AND DC8 SRM 51-3-1.

Part: FITTING — CRACKED (ZONE 300) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT HORIZONTAL STABILIZER LOWER FITTING ANGLE CRACKED AT STATION XFS 60.000. REMOVED DAMAGED FITTING ANGLE. CLEANED, TREATED AND PRIMED. INSTALLED NEW FITTING ANGLE IAW DC8 SRM 51-1-21, DC8 SRM 51-1-8B, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, AND DC8 SRM 51-3-1.

Part: SKIN — CORRODED (ZONE 300) · airframe 70,003 hrs · 17,984 cycles

DURING ROUTINE C CHECK INSPECTION, RIGHT HORIZONTAL STABILIZER. UPPER INBOARD LEADING EDGE OUTER SKIN CORRODED, STATION XFS 178.750. REMOVED EXISTING NON STANDARD REPAIR, AND REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK OR CORROSION FOUND. FABRICATED NEW SKIN AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS FROM STATION XFS 178.750 IAW FAA FORM 8110-3- NUMBER 07110 DATED 03-14-07, SEMAN DRAWING NUMBER ED-4451 DATED 02-14-07, EO SEMAN NUMBER 2007195 DATED 03-14-07, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 55-2-0 PAGE 12, SEMAN DRAWING NUMBER

Part: RELIEF VALVE — MISINSTALLED (NR 1 ENGINE) · airframe 68,033 hrs · 17,581 cycles

AT LEVEL OFF, THROTTLES REDUCED TO CRUISE PWR NR 1 ENG OIL PRESS LIGHT CAME ON. OIL PRESS IND 10 PSI. CREW SHUTDOWN ENG. LANDED W/O INCIDENT. MX VERIFIED NO SIGNIFICANT OIL LOSS. C/W ABNORMAL OIL PRESS INSPECT. INSPECT MAIN FILTER AND SCAV PUMP INLET SCREENS & NO DEBRIS NOTED. FOUND OIL FILTER RELIEF VLV (BYPASS) LEAKS. INSPECT & FOUND VLV SEAT INSTALLATION INCORRECT. CORRECTED. R&R ENG DRIVEN OIL PUMP AND PRESS RELEIF VLV ASSY. R&R OIL PRESS X-MTTER. ENGS RUN & NR 1 OIL PRESS FLUCTUATES BETWEEN 5 & 20 PSI. INSPECT OIL SUPPLY SYS & REMOVED DEBRIS FROM OIL TANK AT PUMP SUPPLY OUTLET. MX FLUSHED TANKS & TUBES, RAN ENGS & ADJUSTED RELIEF VLV. SYS OPS CHK NORM IAW MANUALS AND A/C RTS.

Part: FAN — BROKEN (RECIRCULATION) · airframe 67,734 hrs · 17,524 cycles

DURING CRUISE FROM VTBU, A SLIGHT BURNING SMELL WAS DETECTED DURING CRUISE WHEN USING LEFT RECIRC FAN. FAN WAS TURNED OFF AND SMELL WENT AWAY. MAINTENANCE REMOVED AND REPLACED THE LT RECIRC FAN IAW ALL APPLICABLE MANUALS. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 67,024 hrs · 17,385 cycles

DURING INSPECTION CHECK, SKIN DENT AND SCRATCH DAMAGE WAS FOUND ON THE LEFT HORIZONTAL STABILIZER LEADING EDGE AT UPPER PLATING AROUND L/E STATION XFS 146.00. REMOVED DAMAGE AREA AND DOUBLER WAS INSTALLED IAW EWO ATI 55-05 & EO ATI-071905. EDDY CURRENT INSPECTION WAS PERFORMED IAW SPM TP-MDC-093K393 PROCEDURE 06-10-01.001 AND NO CRACKS WERE FOUND. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: SKIN — CORRODED (1440-1530) · airframe 67,024 hrs · 17,385 cycles

DURING A ROUNTINE C CHECK INSPECTION FOUND CORROSION ON LOWER SKIN STA 1440-1530 LONGERON 31RH- 31LH. SKIN STA 1440-1530 LONGERON 31R-31L WAS REMOVED AND REPLACED IAW DOUGLAS DRAWING 5615374, AND EXTERNAL SPLICE, INTERNAL SPLICE, FINGER DOUBLER AND LONGERON STRAP WERE INSTALLED BETWEEN STA 1420-1440 LONGERON 31RH - 31LH IAW EWO ATI 53-009 & SRM 53-2-1 FIGURE 4.

Part: PLATE — CORRODED (RT WING) · airframe 67,024 hrs · 17,385 cycles

DURING A ROUTINE C CHECK INSPECTION, FOUND CORROSION AT WING OUTER INBD EXTENDED LE PLATING A STA XFS XW 560 TO SPAR RT. CORROSION ON RT WING L/E LOWER SKIN WAS REMOVED AND REPAIR WAS ACCOMPLISHED IAW EWO ATI-57-033 AND SRM 57-2-1 FIGURE 2H.

Part: SKIN — DENTED (LT WING SLAT) · airframe 67,024 hrs · 17,385 cycles

DURING INSPECTION CHECK, FOUND A DENT AT WING OUTER INBOARD EXTENDED LEADING EDGE PLATING STA XFS 610 TO SPAR LT. EXTERNAL DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 57-032 AND SRM 57-2-1 FIGURE 2H.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 67,024 hrs · 17,385 cycles

DURING ROUTINE "C" CHECK, CRACKS 2.023" AND 0.521" LONG WERE FOUND ON THE LEFT WING OUTBOARD FLAP AT FITTING STA XF 409.6675 OUTBOARD. FITTING WAS REPAIRED IAW EWO ATI 57-025 AND EO ATI-071105. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: SUPPORT FITTING — CRACKED (ZONE 600) · airframe 67,024 hrs · 17,385 cycles

DURING ROUTINE "C" CHECK, RT WING OUTBOARD FLAP SUPPORT FITTING STA XF 219.498 WAS FOUND CRACKED (0.177"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-018 & EO ATI-070405. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: SUPPORT FITTING — CRACKED (ZONE 600) · airframe 67,024 hrs · 17,385 cycles

DURING ROUTINE "C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF 339.723 WAS FOUND CRACKED (0.703"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-019 & EO ATI-070505. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: SUPPORT FITTING — CRACKED (XF 409.664) · airframe 67,024 hrs · 17,385 cycles

DURING ROUTINE "0C" CHECK, RT WING OUTBOARD FLAP SUPPORT FITTING STA XF409.664 WAS FOUND CRACKED (LONG 1.570"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-021 & EO ATI-070705. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: SUPPORT FITTING — CRACKED (XF) · airframe 67,024 hrs · 17,385 cycles

DURING ROUTINE "0C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF 97.6090 WAS FOUND CRACKED (0.2740"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-015 & EO ATI-070105. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: SUPPORT FITTING — CRACKED (XF 97.6090) · airframe 67,024 hrs · 17,385 cycles

DURING ROUTINE "C" CHECK, RT WING OUTBOARD FLAP SUPPORT FITTING STA XF 97.6090 WAS FOUND CRACKED (0.2035"). REPAIR ACCOMPLISHED, STOP HOLES WERE DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-016 & EO ATI-070205. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: SUPPORT FITTING — CRACKED (XF 219.498) · airframe 67,024 hrs · 17,385 cycles

DURING ROUTINE "C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF219.498 WAS FOUND CRACKED (1.599"). REPAIR ACCOMPLISHED, STOP HOLES WERE DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-017 & EO ATI-070305. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: SUPPORT FITTING — CRACKED (XF 409.664) · airframe 67,024 hrs · 17,385 cycles

DURING ROUTINE "C" CHECK, RT WING INBOARD FLAP SUPPORT FITTING STA XF 409.664 WAS FOUND CRACKED (LONG: 3.178"). REPAIR ACCOMPLISHED, STOP HOLE WAS DRILLED, ANGLE WAS FABRICATED AND INSTALLED IAW EWO ATI 57-020 & EO ATI-070605. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 67,024 hrs · 17,385 cycles

DURING ROUTINE "C" CHECK, CRACK 0.2740" LONG WAS FOUND ON THE LEFT WING OUTBOARD FLAP AT FITTING LOCATED AROUND STATION XF 339.7232 INBOARD. LEFT WING INBOARD FLAP SUPPORT FITTING WAS REPAIRED IAW EWO-ATI-57-023 AND EO ATI-070905. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 67,024 hrs · 17,385 cycles

DURING ROUTINE "C" CHECK, CRACK 0.5220" LONG WAS FOUND ON THE LEFT WING OUTBOARD FLAP AT FITTING LOCATED AROUND STATION XF 339.7232 OUTBOARD. LEFT WING OUTBOARD FLAP SUPPORT FITTING WAS REPAIRED IAW EWO ATI 57-024 AND EO ATI-071005. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: SUPPORT FITTING — CRACKED (TE FLAP) · airframe 67,024 hrs · 17,385 cycles

DURING ROUTINE "C" CHECK, CRACK 0.385" LONG WAS FOUND ON THE LEFT WING INBOARD FLAP AT FITTING LOCATED AROUND STATION XF 97-6090 INBOARD. LEFT WING OUTBOARD FLAP SUPPORT FITTING WAS REPAIRED IAW EWO ATI 57-022 AND EO ATI-070805. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: SKIN — CORRODED (XFA 603.750) · airframe 67,024 hrs · 17,385 cycles

DURING A ROUTINE C CHECK INSPECTION FOUND SKIN CORROSION DAMAGE ON THE RT OUTER WING AT INBD EXTENDED L/E AROUND STA XFS 603.750REMOVED CORROSION DAMAGE, FABRICATED REPAIR DOUBLER AND INSTALLED IAW EWO ATI 57-031 & EO ATI-071405. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: SKIN — CORRODED (RT WING) · airframe 67,024 hrs · 17,385 cycles

SKIN CORROSION DAMAGE FOUND ON RIGHT OUTER WING AT UPPER PLATING AROUND WING STATION XRS 727.00 AND STRINGER 3RH DURING A ROUTINE C CHECK INSPECTION. CORRODED AREA WAS BLENDED OUT, DOUBLER WAS FABRICATED AND INSTALLED IAW EWO ATI 57-035 AND EO ATI-071605. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: SKIN PANEL — CORRODED (RT WING) · airframe 67,024 hrs · 17,385 cycles

DURING INSPECTION CHECK CORROSION WAS FOUND ON PANEL AT WING OUTER INBOARD EXTENDED LEADING EDGE PLATING STA XFS 710.0, RT. CORROSION ON RT WING LEADING EDGE UPPER SKIN WAS REMOVED AND REPAIR "DOUBLER" WAS INSTALLED IAW EWO ATI 57-029 AND EO ATI-071505. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: SKIN — CORRODED (RT WING) · airframe 67,024 hrs · 17,385 cycles

DURING A "C" CHECK INSPECTION, FOUND SKIN CORROSION DAMAGE ON THE RIGHT OUTER WING AT THE INBOARD EXTENDED L/E STA XFS 653.750. RT WING L/E UPPER SKIN WAS REPAIRED IAW EWO ATI 57-030 AND EO ATI-071305. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: SKIN — CORRODED (RT WING) · airframe 67,024 hrs · 17,385 cycles

DURING A ROUTINE C CHECK INSPECTION, FOUND CORROSION OVER EXISTING REPAIR ON WING ON INNER OUTBOARD EXTENDED L/E SLAT STA XFS 207-XILD42. CORROSION ON RT WING LEADING EDGE UPPER SKIN WAS REMOVED AND REPAIR "DOUBLER' WAS INSTALLED IAW EWO ATI 57-034 AND SRM 57-2-1 FIG 44.

Part: SKIN — CORRODED (LT WING) · airframe 67,024 hrs · 17,385 cycles

DURING INSPECTION CHECK, SKIN CORROSION DAMAGE WAS FOUND ON THE LEFT INNER WING AT OUTBOARD EXTENDED LEADING EDGE SLOT AROUND L/E STATION XFS 207.00. REMOVED CORROSION AND ACCOMPLISHED REPAIR "DOUBLER" IAW EWO ATI 57-028 AND EO ATI-071205. FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: DOOR — CRACKED (FUEL) · airframe 67,024 hrs · 17,385 cycles

DURING A ROUTINE C CHECK INSPECTION A CRACK WAS FOUND AT FUEL ACCESS DOO 506A LH.CORRECTIVE ACTION: ACCESS DOOR 506A LH WAS REPAIRED IAW EWO ATI-57-027 & SRM 57-2-1 FIGURE 43.

Part: ANGLE — CORRODED (BS 857.000) · airframe 67,024 hrs · 17,385 cycles

CORROSION ON LT WHEEL WELL "DOG HOUSE" AREA LOWER SIDE STA 857.000, ANGLE WAS FOUND CORRODED. ANGLE WAS FABRICATED IAW DOUGLAS DRAWING 5644678 AND ASSEMBLED IAW DC8 SRM 53-7-2 FIGURE 4.

Part: DOOR — CRACKED (FUEL) · airframe 67,024 hrs · 17,385 cycles

DURING A ROUTINE C CHECK INSPECTION A CRACK WAS FOUND AT FUEL ACESS DOOR 506B LH. CORRECTIVE ACTION: ACCESS DOOR # 506B WAS REPAIRED IAW EWO ATI 57-026 & SRM 57-2-1 FIGURE 43.

Part: SKIN — MISDRILLED (XRS 795) · airframe 67,024 hrs · 17,385 cycles

DURING A ROUTINE C CHECK INSPECTION FOUND A MISS DRILL HOLE ON PLATING STA XRS 795 LONGERON 3-RHD. REPAIR WAS MADE AND DOUBLER WAS INSTALLED IAW EWO ATI 57-036 & EO ATI-071705.FAA FORM 8110-3 WAS ISSUED APPROVING THIS REPAIR.

Part: CONNECTOR — LOOSE (HYD SYS) · airframe 66,843 hrs · 17,335 cycles

DURING CRUISE, ACFT STARTING LOSING HYDRAULIC FLUID. CREW ACCOMPLISHED EMERGENCY PROCEDURES AND RETURNED ACFT. LANDED WITHOUT INCIDENT. MX FOUND LOOSE HYDRAULIC CONNECTOR RT SIDE OF NR 2 ENGINE. SECURED LINE. OPS CHECK GOOD PER ALL APPLICABLE MANUALS. ACFT RETURNED TO SERVICE.

Part: TRANSMITTER — BROKEN (OIL PRESSURE) · airframe 66,339 hrs · 17,195 cycles

AFTER TAKEOFF FROM TAPA NR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. CREW PERFORMED ENGINE SHUTDOWN CHECK LIST AND CREW RETURNED AIRCRAFT TO TAPA AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED NR 1 ENGINE DIFFERENTIAL TRANSMITTER PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SEAL — MISSING (NLG DOOR) · airframe 66,167 hrs · 17,149 cycles

UPON CLIMBOUT FROM KBWI EN ROUTE TO KWRI AFTER GEAR RETRACTION CREW NOTED AIR NOISE FROM UNDER COCKPIT FLOOR. AFTER GEAR RECYCLE, UNDER AIR LOAD NOISE DECREASED. CREW PROCEEDED TO KWRI AND MADE AN UNEVENTFUL LANDING. UPON INSPECTION MX NOTED NLG DOOR SEAL ON RT SIDE MISSING AND INSTALLED A SERVICEABLE SEAL. AIRCRAFT RETURNED TO SERVICE.

Part: REGULATOR — FAILED (NR 2 ENGINE) · airframe 65,782 hrs · 17,056 cycles

DURING CRUISE FROM PKWA, TAKEOFF PLUS 45 MINS TURNED ON RECIR FAN AND HEARD LOUD BANG FROM AREA UNDER CAPTAIN SEAT, COULD NOT STOP CABIN FROM CLIMBING. GOT CONTROL OF CABIN AT ABOUT 15,000, ACFT ALTITUDE CABIN WAS AT 10,2000. TURNED BLEED OFF ON LEFT SIDE, PRESSURE WOULD NOT GO DOWN. MANIFOLD PRESS AND TEMP STAYED AT 35 PSI AND 200C. MAINTENANCE TROUBLESHOT AND FOUND A LEAKING BLEED HEAT EXCHANGER ON NR 1 ENGINE PYLON. ALSO FOUND BAD PRESS REGULATOR ON NR 2 ENGINE. MAINTENANCE DEFERRED BOTH PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO FIRE) · airframe 65,224 hrs · 16,945 cycles

DURING CRUISE AT FL 370 LOWER CARGO COMPARTMENT FIRE WARNING ILLUMINATED. DISCHARGED BOTH FIRE EXTINGUISHERS. CREW RETURNED AND LANDED WITHOUT INCIDENT. UPON LANDING MAINTENANCE INSPECTED ALL LOWER CARGO COMPARTMENTS AND FOUND NO EVIDENCE OF FIRE. REF DMI NR 30653, CAT (C) NFD 10/31/04, IAW ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 65,114 hrs · 16,921 cycles

AFTER TAKEOFF LEFT PACK CONTROL VALVE WOULD NOT MAINTAIN CABIN ALTITUDE OF 10000 FEET WITH AIRCRAFT AT FL250 AND RIGHT PACK OFF. RIGHT PACK CONTROL VALVE WILL NOT MAINTAIN CABIN ALTITUDE OF 10000 FEET WITH AIRCRAFT AT FL 250 AND LEFT PACK OFF. CREW RETURNED AIRCRAFT TO PHIK AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING AND INFORMATION WILL BE PROVIDED AS SOON AS IT IS AVAILABLE.

Part: FLOW VALVE — FAILED (LT A/C PACK) · airframe 65,113 hrs · 16,920 cycles

AFTER TAKEOFF, LEFT PACK CONTROL VALVE WOULD NOT MAINTAIN CABIN ALTITUDE OF 1000 FEET WITH AIRCRAFT AT FL 250 AND RIGHT PACK OFF. CREW RETURNED TO PHIK AND LANDED WITHOUT INCIDENT. MAINTENANCE VERIFIED SECURTIY OF LEFT PACK/FLOW CONTROL SYSTEM, DUCTS AND COMPONENTS. NO DEFECTS WERE NOTED. VERIFIED SECURITY AND FREEDOM OF OPERATION OF LEFT CONDITIONED AIR, CHECK VAVLE AND RAM AIR(COLD) CHECK VALVE, NO DEFECTS NOTED. MAINTENANCE REMOVED AND REPLACED LEFT FLOW CONTROL VALVE PER ALL APPLICABLE MANUALS.

Part: ENGINE — FAILED (NR 4) · airframe 64,824 hrs · 16,858 cycles

DURING CRUISE FROM KSUU TO PHIK, NR 4 ENGINE LOSS OF ALL OIL QUANTITY AND OIL PRESSURE OF 12PSI. ENGINE NR 4 OIL LIGHT CAME ON. CREW SHUT DOWN NR 4 ENGINE AND AFTER SHUT DOWN NR 4 ENGINE WINDMILLING OIL PRESSURE AT 5PSI. AIRCRAFT ARRIVED IN PHIK AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING AND INFORMATION WILL BE PROVIDED AS SOON AS IT IS AVAILABLE. MAINTENANCE FOUND EVIDENCE OF OIL IN GAS PATH. MAINTENANCE REMOVED NR 4 ENGINE AND INSTALLED REPLACEMENT. OPERATIONAL CHECK GOOD ON GROUND AND ENGINE RUN GOOD PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.

Part: LINKAGE — LOOSE (OUTFLOW VALVE) · airframe 64,050 hrs · 16,706 cycles

DURING FLIGHT CABIN CLIMBING AT 1000' PER MINUTE- AIRCRAFT ALTITUDE FL200- UNALBE TO CAUSE CABIN TO DESCEND TO NORMAL ALTITUDE- CROSSFEED OPEN. MAINTENANCE INSPECTED PNEUMATIC DUCTING AND PERFORMED LEAKS CHECK. NO DEFECTS NOTED. MAINTENANCE THEN PERFORMED GROUND PRESSURIZATION PER ALL APPLICABLE MANUALS AND NO DEFECTS WERE NOTED. MAINTENANCE INSPECTED CABIN AIR OUTFLOW VALVE FOUND DRIVE ROD LINKAGE LOOSE, CAUSING VALVE TO STICK OPEN. ADJUSTED LINK PER ALL MANUALS,OPERATIONAL CHECK WAS GOOD. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 63,708 hrs · 16,626 cycles

FINGER DOUBLER ON PRESSURE WEB STA 188 TO 208 RBL 28 HAS CORROSION AND RIVET HEADS SHEARED. REMOVED CORROSION, CUT OUT DAMAGED AREA, FABRICATED FILLER, FINGER DOUBLER 2 EACH AND PLATE IAW DC8 SRM 53-2-0. TREATED AND PRIMED IAW DC8 SRM 51-1-8. INSTALLED ALL REPAIR PARTS IAW DC8 SRM 51-1-21.