N602AL

Part: SKIN — DAMAGED (ZONE 500) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP FOUND LT WING T/E LOWER SKIN HAS IMPROPER REPAIR AT STA XW 730.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. 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 57-3-3 FIG 23, DPS 4.710 REV "L", SRM 51-1-9 TR 51-142, SRM 51-1-9A TR 51-141, DPS 1.950 REV "AR", SRM 51-1-8B, AND SRM 51-1-21.

Part: SPAR CAP — CRACKED (ZONE 600) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP, FOUND NR 3 MAIN TANK LOWER CTR SPAR CAP AND WEB CRACKED AT STA XRS 168.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED STRAP, SHIMS, SPLICES, FILLER, ANGLE, TEE, AND FITTING. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 DATED 11/24/10, DWG ED-5291, DATED 11/18/10, SRM 51-1-21, SRM 51-1-20D, NDT SPM PART 06-10-01-001, DWG SR08530005, SRM 51-1-8B, SRM 51-1-20D, SRM 51-1-11, AND SRM 51-3-1.

Part: SKIN — DAMAGED (ZONE 500) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP FOUND LT WING T/E UPPER SKIN DOUBLER WITH IMPROPER REPAIR AT STA XW 736.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND FINGER DOUBLERS. BONDED PARTS AS NEEDED WITH HYSOL. 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 57-3-3 FIG 23, DPS 4.710 REV "L", SRM 51-1-9 TR 51-142, SRM 51-1-9A TR 51-141, DPS 1.950, REV "AR", SRM 51-1-8B, AND SRM 51-1-21.

Part: WEB — CRACKED (FUEL CELL) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP FOUND NR 3 MAIN TANK WEB CRACKED AT STATON XRS 168.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED STRAP, SHIMS, SPLICES, FILLER, ANGLE, TEE, AND FITTING. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8110-3 DATED 11/24/10, DWG ED-5291 DATED 11/18/10, SRM 51-1-21, SRM 51-1-20D, NDT SPM PART 06-10-01-001, DWG SR08530005, SRM 51-1-8B, SRM 51-1-20D, SRM 51-1-11, AND SRM 51-3-1.

Part: FITTING — CRACKED (ZONE 200) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT FWD FITTING CRACKED AT STA 902.000 LONG 19 LT. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AREA. SRM 51-1-8B. INSTALLED NEW FITTING IAW SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D, SRM 51-3-1.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CK INSP FOUND MAIN CARGO COMPARTMENT FLOOR PANEL SKIN CORRODED BETWEEN STA 1060.000 LT BOTTOM LINE10. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED DOUBLERS AND FILLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-1-8, SRM 53-2-0, SRM 53-2-3, SRM 53-2-3, SRM 51-1-8B AND SRM 51-1-21.

Part: LONGERON — CORRODED (ZONE 100) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT AFT SECTION FLOOR LONGERON 36 CORRODED AT STA 1690.000 - 1725.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED LONGERON SEGMENT. FABRICATED LONGERON AND STRAPS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW LONGERON SEGMENT AND STRAPS IAW SRM CHAPTER 53-2-2, FIG 8, SHEET 1, 2, SRM 51-1-8, SRM 53-2-0, SRM 51-1-8B, SRM 53-2-2, SRM 51-1-21, SRM 51-1-20D, AND SRM 51-3-1.

Part: FITTING — CRACKED (ZONE 100) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STA 1160.000, LONGERON 20RT. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRM 53-2-0, SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D, SRM 51-1-21, AND SRM 51-3-1.

Part: FITTING — CRACKED (ZONE 100) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STA 857.000, LONGERON 19 & 20 RT. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRM 53-2-0, SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D, SRM 51-1-21, AND SRM 51-3-1.

Part: FITTING — CRACKED (ZONE 100) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STA 781.000, LONGERON 19 & 20 RT. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRM 53-2-0, SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D, SRM 51-1-21, AND SRM 51-3-1.

Part: FITTING — CRACKED (ZONE 100) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 717.000 LT BOTTOM LINE 22. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CRACKED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRM 53-2-0, SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D, SRM 51-1-21, AND SRM 51-3-1.

Part: SKIN — CRACKED (RT ELEVATOR) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR T/E LOWER SKIN CRACKED AND DELAMINATED AT STA XE 132.750. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE. FOUND WITHIN LIMITS. MOMENT 1441.85 IN-LBS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-1-21, SRM 55-1-0 PAGE 1, SRM 55-4-1 FIG 1 SHEETS 1-2 ITEMS "E" & "F", DPS 4.710 REV "L", SRM 51-1-9 TR 51-142, SRM 51-1-9A TR 51-141, DPS 1.950 REV "L", SRM 51-1-8B, SRM 51-1-21, SRM 51-4-4 PAGES 1-4 AND T/R 51-116 PAGES 2-3.

Part: SKIN — DELAMINATED (RT ELEVATOR) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP FOUND RT ELEVATOR T/E LOWER SKIN CRACKED AND DELAMINATED AT STA XE 77.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE. FOUND WITHIN LIMITS, MOMENT 1441.85 IN-LBS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-1-21, SRM 55-1-0 PAGE 1, SRM 55-4-1 FIG 1 SHEETS 1-2 ITEMS "E" & "F", DPS 4.710 REV "L", SRM 51-1-9 TR 51-142, SRM 51-1-9A TR 51-141, DPS 1.950 REV "L", SRM 51-1-8B, SRM 51-1-21, SRM 51-4-4 PAGES 1-4 AND T/R 51-116 PAGES 2-3.

Part: FITTING — CORRODED (ZONE 100) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP FOUND MAIN CARGO COMPARTMENT FITTING CORRODED AT STATION 960.000 - 980.000 RT BOTTOM LINE 28. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRM 53-2-0, SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D, SRM 51-1-21, AND SRM 51-3-1.

Part: FITTING — CRACKED (ZONE 100) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STA 700.000, LT BOTTOM LINE 23. REMOVED CORROSION AND FOUND OUT OF LIMITS. REMOVED CORRODED FITTING. CLEANED, TREATED, AND PRIMED AERA. INSTALLED NEW FITTING IAW SRM 51-1-8, SRM 53-2-0, SRM 51-1-20D, SRM 51-1-8B, SRM 51-1-20D, SRM 51-1-21, AND SRM 51-3-1.

Part: SKIN — CORRODED (ZONE 500) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP FOUND LT WING L/E LOWER PART CORRODED ST STATION XFS 335.250 - 341.500. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO CRACK OR CORROSION NOTED. FABRICATED DOUBLER AND FILLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED REPAIR PARTS IAW FAA FORM 8110-3 DATED 12/07/10, DWG ED-5292 DATED 11/16/10, SRM 51-1-8, SRM 57-2-0, NDT SPM PART 06-10-01-001, SRM 51-1-8B, SRM 51-1-20D, SRM 51-1-11, SRM 51-1-21, AND SRM 51-3-1.

Part: SKIN — BROKEN (LT WING TE FLAP) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP, FOUND LT INBD FLAP UPPER SKIN BROKEN AT STA XW 107.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. 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 57-7-1 FIG 1 ITEM "D", DPS 4.710 REV "L", SRM 51-1-8B, AND SRM 51-1-21.

Part: SKIN — CORRODED (LT WING TE FLAP) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP, FOUND LT OTBD FLAP LOWER SKIN CORRODED AT STA XF 407.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-1-8, SRM 57-2-0, SRM 51-1-21 AND SRM 57-1-0 PAGE 1, SRM 57-7-1, FIG 4 TR 57-94 ITEMS "U" & "Q" AND DPS 4.710 REV "L", SRM 51-1-9 TR 51-142, SRM 51-1-9A TR 51-141, DPS 1.950 REV "AR" R-1, SRM 51-1-8B, AND SRM 51-1-21.

Part: FITTING — CRACKED (ZONE 100) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP FOUND LT MLG WHEEL WELL FRAME FITTING CRACKED AT STATION 920.000, LONGERON 24 LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED FITTING. FABRICATED NEW FITTING, SPLICES, FILLERS, AND DOUBLERS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM CHAPTER 53-2-0 FIG 8, SHEET 2, 4-6, SRM 51-1-20D, SRM 51-1-8B, SRM 53-2-0, SRM 51-3-0, AND SRM 51-3-1.

Part: FITTING — CORRODED (ZONE 100) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP FOUND LT MLG WHEEL WELL FRAME FITTING CORRODED AT STATION 879.375, LONGERON 24LT. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED FITTING. FABRICATED NEW FITTING, SPLICES, DOUBLER AND SHIMS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED FITTING AND REPAIR PARTS IAW SRM CHAPTER 53-2-0, FIG 8 SHEETS 1/3/6, SRM 51-1-8, SRM 53-2-0, SRM 51-1-20D, SRM 51-1-8B, SRM 53-2-0, AND SRM 51-3-1.

Part: FITTING — CRACKED (ZONE 100) · airframe 102,975 hrs · 33,577 cycles

DURING ROUTINE C-CHECK INSP, FOUND CRACKED FITTING AT STA 857.000 & 879.000 LONGERON 24LT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. PERFORMED STOP DRILL END OF CRACKS. PERFORMED NDT INSP. NO CRACKS OR CORROSION NOTED. FABRICATED INTERNAL AND EXTERNAL DOUBLERS, ANGLES, AND SHIMS. CLEANED, TREATED, PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8100-9 DATED 12/01/10,MESSAGE TIN-TIN-10-0088-08B, DWG ED-5277 DATED 11/04/10, SRM 51-1-20D, NDT SPM PART 06-10-01-001, SRM 53-2-2, SRM 51-1-8B, SRM 51-1-14, AND SRM 51-3-1.

Part: FIRE LOOP — DEFECTIVE (ZONE 400) · airframe 102,776 hrs · 33,490 cycles

DURING CRUISE, NR 2 ENGINE FIRE WARNING CAME ON AT FL270 SAT -52. THE CREW SHUTDOWN THE NR 2 ENGINE, WHILE PASSING THROUGH 14,000 FT THE ACFT WAS EXPERIENCING SOME TURBULANCE AND NR 2 FIRE WARNING AND SHORT CIRCUIT LIGHTS ILLUMINATED. CREW DISCHARGED BOTH FIRE BOTTLES. WHILE PASSING THROUGH 10,000 FT FIRE WARNING LIGHT ILLUMINATED AND STAYED ON THE REMAINDER OF THE FLIGHT. THEY LANDED, WITHOUT FURTHER INCIDENT. MX REPLACED THE LT AND RT FAN FIRE LOOPS, LT AND RT CORE FIRE LOOPS, UPPER HOT SECTION FIRE LOOPS AND BOTH FIRE BOTTLES. OPS CHECK GOOD IAW MM 26-10-1, 26-20-1,ERH 70.01. ACFT WAS RETURNED TO SERVICE.

Part: SENSOR — DEFECTIVE (AIRSPEED) · airframe 102,672 hrs · 33,427 cycles

DURING TAKEOFF, THE MAX AIRSPEED WARNING LIGHT AND CLACKER CAME ON. THE CREW REJECTED TAKEOFF AND RETURNED TO BLOCKS WITHOUT FURTHER INCIDENT. MX REPLACED THE OVERSPEED LIMIT SENSOR. OPS CHECK GOOD IAW MM 34-11-0. ACFT WAS RETURNED TO SERVICE.

Part: INDICATOR — DEFECTIVE (STNDBY ATTITUDE) · airframe 102,591 hrs · 33,384 cycles

DURING CLIMB OUT, STANDBY ATTITUDE INDICATOR INOPERATIVE, THE CREW RETURNED TO DEPARTURE WITHOUT FURTHER INCIDENT. MX REPLACED THE STANDBY ATTITUDE INDICATOR. OPS CHECK GOOD IAW MM34-28-0. ACFT WAS RETURNED TO SERVICE.

Part: SWITCH — INOPERATIVE (MLG DOOR) · airframe 100,218 hrs · 32,355 cycles

FLIGHT ATN 802, DURING CRUISE FROM KTOL, GEAR DOOR NOT LATCHED LIGHT CAME ON INTERMITTENT. THE CREW ACCOMPLISHED ABNORMAL CHECK 3-13-01. THE CREW LANDED IN KLAX WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND BAD MAIN LANDING DOOR SWITCH. MAINTENANCE REPLACED SWITCH. OPERATIONAL CHECK GOOD IAW EO 32-DC8-3730, DC8 MAINTENANCE MANUAL 32-8. ACFT HAS RETURNED TO SERVICE. (S)

Part: CONNECTOR — DAMAGED (FIRE DETECTION) · airframe 100,185 hrs · 32,332 cycles

FLT NR: ATN 842/KTOL TO KPHL. DURING CLIMB FROM KTOL THE NR 4 FIRE WARNING CAME ON. THE CREW ACCOMPLISHED THE APPROPRIATE CHECKLIST AND DISCHARGED BOTH FIRE BOTTLES. THE ACFT LANDED AT KPHL WITHOUT INCIDENT. MAINTENANCE INSPECTED NR 4 ENGINE FIRE DETECTION SYSTEM AND FOUND HIGH RESISTANCE AT PIN F, UPPER PYLON SOCKET PLUGS DISTORTED. MAINTENANCE REPLACED PYLON FIRE DETECTOR ELEMENT, SOCKET PLUG, FIRE DETECTOR CONTROL UNIT AND BOTH FIRE BOTTLES. OPERATIONAL CHECK GOOD IAW MM 26-10-0, 26-10-1 AND 26-10-2. AIRCRAFT WAS RETURNED TO SERVICE. (A)

Part: FIRE WARNING — ILLUMINATED (NR 4)

DURING CLIMB, THE NR 4 FIRE WARNING CAME ON. THE CREW ACCOMPLISHED THE APPROPRIATE CHECKLIST AND DISCHARGED BOTH FIRE BOTTLES. THE AC LANDED WITHOUT INCIDENT. CORRECTIVE ACTION IN WORK. (K)

Part: FIRE DETECTOR — MALFUNCTIONED (NR 3 NACELLE)

DURING CRUISE, NR 3 FIRE WARNING CAME ON, THE CREW DISCHARGED BOTH FIRE BOTTLES AND SHUTDOWN NR 3 ENGINE. THE CREW LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED RT CORE SENSING ELEMENT, LT AND RT FAN FIRE SENSING ELEMENT, AND BOTH FIRE BOTTLES, OPS CHECK GOOD IAW MM 26-10-1, AND 26-20. AIRCRAFT WAS RETURNED TO SERVICE. (K)

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FLOOR PANEL WITH CORROSION AT STATION 1425.000 RIGHT BOTTOM LINE 50. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. FABRICATED DOUBLER AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-21, DC8 SRM 51-1-8 PAGES 17-18, DC8 SRM 53-2-0 PAGE 2P, DC8 SRM 53-2-3 PAGES 39-40, AND DC8 SRM 51-1-8B.

Part: CARGO TRACK — WORN (BS 1580) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 6 TRACK WITH LUG WORN AT STATION 1580.000. REMOVED EXISTING SPLICES (AFT SIDE). REMOVED SEGMENT OF DAMAGED TRACK. FABRICATED NEW SPLICES. CLEANED, TREATED AND PRIMED AREA, AND EXISTING SPLICES AND REPAIR PARTS. INSTALLED NEW TRACK AND SPLICES 53-7-3 FIGURE 3E ITEM "G", 51-2-0 FIGURE 5D SHEET 79, DC8 SRM 53-2-3 FIGURE 14 SHEETS 1 AND 2, DC8 SRM 51-3-0, AND DC8 SRM 51-1-8B.

Part: SKIN — CRACKED (RT WING) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 STUB WING DOUBLER SHOWS CRACK AT STATION XS 515.720. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW EXTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA AND EXTERNAL DOUBLER. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-2-1A FIGURE 2, DC8 SRM 51-1-20D, DC8 SRM 51-1-8B, AND 51-3-1.

Part: CARGO TRACK — WORN (BS 680) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK WITH LUGS WORN AT STATION 680.000. REMOVED EXISTING SPLICES (FWD SIDE) AND REMOVED SEGMENT OF DAMAGED TRACK AFT SIDE. FABRICATED SPLICES. CLEANED, TREATED AND PRIMED AREA AND SPLICES. INSTALLED SEGMENT OF NEW TRACK AND NEW SPLICES AND REINSTALLED EXISTING SPLICES IAW DC8 SRM 53-2-3 FIGURE 14 PAGES 49-50, 51-3-0, DC8 SRM 51-1-8B, 53-7-3 FIGURE 3E SHEET 1 AND 2, 51-2-0 FIGURE 50 SHEET 73, AND 51-3-1.

Part: CARGO TRACK — BROKEN (FUSELAGE) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 2 TRACK WITH LUGS, BROKEN AT STATION 55.000. REMOVED SEGMENT OF DAMAGED TRACK AND EXITING SPLICES. CLEANED, TREATED AND PRIMED AREA AND EXITING SPLICES. INSTALLED NEW TRACK AND REINSTALLED SPLICES IAW DC8 SRM 53-2-3 FIGURE 14 SHEETS 1-2, 51-3-0, DC8 SRM 51-1-8B, DC8 SRM 53-2-3 FIGURE 14, 53-7-3 FIGURE 3E SHEETS 1 AND 2 ITEM "K", 51-2-0 FIGURE 50 SHEET 79, 51-1-21, 51-3-0, AND 51-3-1.

Part: SKIN — MISREPAIRED (LT WING TE FLAP) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER PART WITH IMPROPER REPAIR AT STATION XW -2.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PART. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 57-7-1 FIGURE 1 ITEM "E", DC8 SRM 57-1-0 PAGE 1, 51-1-21, DC8 SRM 51-1-8B, AND DC8 SRM 51-1-11.

Part: CARGO TRACK — WORN (BS 310-425) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK WITH LUGS WORN AT STATION 310.000 - 425.000. REMOVED DAMAGED SEGMENT OF TRACK AND EXISTING SPLICES. CLEANED, TREATED AND PRIMED AREA AND EXISTING SPLICES. INSTALLED SEGMENT OF NEW TRACK AND REINSTALLED SPLICES IAW DC8 SRM 53-2-3 FIGURE 14 PAGES 49-50, 53-7-3 FIGURE 3E SHEETS 1 AND 2, 51-2-0 FIGURE 50 SHEET 73, 51-3-0, 51-3-1, DC8 SRM 53-2-3 FIGURE 14 PAGES 49-56, DC8 SRM 53-1-0 PAGE 1, 51-3-0, AND DC8 SRM 51-1-8B.

Part: CARGO TRACK — CORRODED (FUSELAGE) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 3 TRACK WITH CORROSION AT STATION 590.000. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED EXINTING SPLICES (FWD SIDE) AND REMOVED SEGMENT OF DAMAGED TRACK. FABRICATED SPLICES. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW SEGMENT OF TRACK AND SPLICES IAW DC8 SRM 53-2-3 FIGURE 14 PAGES 49-50, DC8 SRM 51-1-8 PAGES 17-18,DC8 SRM 53-2-3 FIGURE 12, DC8 SRM 51-1-8B, 53-7-3 FIGURE 3E ITEM "H", 51-2-0 FIGURE 50 SHEET 73, 51-3-0, AND 51-3-1.

Part: CARGO TRACK — WORN (BS 685) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT NUMBER 4 TRACK WITH LUGS WORN AT STATION 685.000. REMOVED EXISTING SPLICES (FWD SIDE) AND REMOVED SEGMENT OF DAMAGED TRACK AFT SIDE. FABRICATED SPLICES. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED SEGMENT OF NEW TRACK AND REPAIR PARTS AND REINSTALLED EXISTING SPLICES IAW DC8 SRM 53-2-3 FIGURE 14 PAGES 49-50, 51-3-0, DC8 SRM 51-1-8B, 53-7-3 FIGURE 3E SHEET 1, 2, 51-2-0 FIGURE 50 SHEET 73, 51-3-0, AND 51-3-1.

Part: SKIN — DELAMINATED (FLAP VANE) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 6 VANE FLAP DELAMINATED SKIN BETWEEN STATION XF 415.000 TO STA XF 434.000. REMOVED AND REPLACED RIGHT WING NUMBER 6 VANE FLAP. PERFORMED OPS CHECK GOOD TO FLAP SYSTEM IAW DC8 MM 27-51-14 PAGES 201-202, AND DC8 MM 27-50-0 PAGES 506-507.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR UPPER SKIN DENTED AT STATION XE 200.2379. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE FOUND MOMENT WITHIN TOLERANCE, MOMENT 1448-2. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XE 132.000 TO XE 246.000 IAW DC8 SRM 51-1-11, DC8 SRM 55-4-1 FIGURE 1 SHEET 1 AND 2 ITEM "E" AND "F", DC8 SRM 55-1-0 PAGE 1, 51-1-21, DC8 SRM 51-1-9 TR NUMBER 51-142, 51-1-9A TR NUMBER 51-141, AND DC8 SRM 51-1-8B.

Part: SKIN — DAMAGED (LT WING TE FLAP) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP SKIN UPPER PLATING NICKED AT STATION XW 112.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE PLATING. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 57-7-1 FIGURE 1 ITEM "D", AND DC8 SRM 51-1-8B.

Part: SKIN — DENTED (LT ELEVATOR) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT ELEVATOR UPPER SKIN DENTED AT STATION XE 137.531 TO STATION XE 142.062. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE SKIN. FABRICATED NEW SKIN AND FINGER DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. PERFORMED BALANCE FOUND MOMENT WITHIN TOLERANCE, MOMENT 1448-2. INSTALLED NEW FASTENERS AND REPAIR PARTS AT STATION XE 132.000 TO XE 246.000 IAW SRM 51-1-11, SRM 55-4-1 FIGURE 1 SHEET 1 AND 2 ITEM "E" AND "F", SRM 55-1-0 PAGE 1, 51-1-21, SRM 51-1-9 TR NUMBER 51-142, 51-1-9A TR NUMBER 51-141, AND SRM 51-1-8B.

Part: SKIN PANEL — DELAMINATED (NR 4 SPOILER) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 SPOILER PANEL DELAMINATED BETWEEN STATION XRS 247.000 TO XRS 351.000. ADJUSTED LEFT AND RIGHT WING GROUND FLIGHT SPOILER CABLES. PERFORMED OPS CHECK, GOOD TO SPOILER SYSTEM IAW DC8 MM 27-60-0 PAGE 507 ITEMS 15-16 PAGE 509 ITEM 4, AND DC8 MM 27-60-0 PAGE 1.

Part: SKIN — DELAMINATED (NR 4 TE FLAP) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 4 VANE FLAP DELAMINATED SKIN BETWEEN STATION XF 225.000 TO STA XF 335.000. REMOVED AND REPLACED RIGHT WING NUMBER 4 VANE FLAP. PERFORMED OPS CHECK GOOD TO FLAP SYSTEM IAW DC8 MM 27-51-14 PAGES 201-202, AND DC8 MM 27-50-0 PAGES 506-507.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING NUMBER 5 VANE FLAP DELAMINATED SKIN BETWEEN STATION XF 345.000 TO STA XF 404.000. REMOVED AND REPLACED RIGHT WING NUMBER 5 VANE FLAP. PERFORMED OPS CHECK GOOD TO FLAP SYSTEM IAW DC8 MM 27-51-14 PAGES 201-202, AND DC8 MM 27-50-0 PAGES 506-507.

Part: FITTING — CRACKED (BS 902 L19R) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT INTERCOSTAL SUPPORT FITTING CRACKED AT STATION 902.000 LONGERON19 RIGHT. REMOVED CRACKED INTERCOSTAL SUPPORT. FABRICATED NEW INTERCOSTAL SUPPORTS. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED AREA AND INTERCOSTAL SUPPORT IAW DC8 SRM 51-1-20D, 51-3-1, ATI REPAIR SPECIFICATIONS NUMBER 2003-05, DOUGLAS DRAWING 3779498, AND DPS 4.707.

Part: FITTING — CRACKED (ZONE 700) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RT MAIN LANDING GEAR WHEEL WELL FORWARD UPPER PART FITTING CRACKED AT STATION 857.125 AND STATION XCW 23.000. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK FOUND. CLEANED, TREATED AND PRIMED AREA AND FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2003-05, DOUGLAS DRAWING 3646326, DPS 4.707, DC8 SRM 51-1-8B, AND 51-3-1.

Part: SKIN — CORRODED (BS 850 L24L) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND EXTERIOR FUSELAGE SKIN LEFT SIDE WITH CORROSION AT STATION FS 850.000 LONGERON 24. REMOVED FASTENERS FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED INNER TAPERED SPLICE REPAIR, FILLER SKIN. PERFORMED HEAT TREATMENT. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-3-1, FAA FORM 8110-3 NUMBER 08205 DATED 04/29/08, DRAWING NUMBER ED-4752 DATED 03/29/08, DC8 SRM 51-1-20D, 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 51-1-1 PAGES 1, 13 AND 17, AND DC8 SRM 51-1-8B.

Part: FITTING — CRACKED (BS 822) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT BS 822.000 LEFT BOTTOM LINE 22". REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, 51-3-1, SRM 51-1-8B, ATI REPAIR SPECIFICATION 2003-05, DRAWING 3755222, AND DPS 4.707.

Part: SKIN — MISREPAIRED (BS 1150 L21R) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND DOUBLER REPAIR RIGHT AFT FUSELAGE ABOVE AND FWD OF C-PIT DOOR RIVET SPACING EXCEEDED AT FS 1150 LONGERON 21.5 RIGHT. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXITING REPAIR. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW FAA FORM 8100-9 DATED 04-25-08, AD 2005-18-07, S/B DC8 53-078, DRAWING DOUGLAS NUMBER SR08530019, 5750776, BOEING MESSAGE 1-792473913-9 DATED 04/25/08, BOEING SKETCH 1-792473913, SEMAN DRAWING ED-4736, DC8 SRM 51-1-21, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 53-2-0 FIGURE 22, DC8 SRM 51-1-8B, 51-1-21, 51-1-20D, AND 51-3-1.

Part: SKIN — MISREPAIRED (BS 1660 L19L) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT AFT FUSELAGE L-2 DOOR AFT EDGE HAS IMPROPER REPAIR AT FS-1660 LONGERON 19.5. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLER. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, AND FILLER. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW AD 2000-20-08, S/B DC8-53-075, DRAWING DOUGLAS SR08530021, 5750776, BOEING MESSAGE 1-792473688-12 DATED 04/23/08, BOEING SKETCH 1-792473688-9, SEMAN DRAWING ED-4737 DATED 04/18/08, DC8 SRM 51-1-21, DC8 NDT SPM PART 06-10-01-001, DC8 SRM 53-2-0 FIGURE 18, DC8 SRM 51-1-8B, 51-1-11, 51-1-21, AND 51-3-1.

Part: FITTING — CRACKED (BS 759) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STATION 759.000 LBL 22. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING IAW SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2003-05, DRAWING 3755222, DPS 4.707, SRM 51-1-8B, AND 51-3-1.

Part: SKIN — DEFORMED (T/E FLAP) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND LEFT INBOARD FLAP UPPER PANEL DEFORMED AT STATION XW 104.000 TO STATION XW 115.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED SKIN. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, DC8 SRM 57-7-1 FIGURE 1 ITEM "A" AND "L", DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-21, DC8 SRM 51-1-9 TR NUMBER 51-142, DC8 SRM 51-1-9A TR NUMBER 51-141, AND DC8 SRM 51-1-8B.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP SKIN UPPER PART HAS IMPROPER REPAIR AT STATION XW 114.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN, BONDED DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-1-21, DC8 SRM 57-7-1 FIGURE 1 ITEM "A" AND "L", DC8 SRM 57-1-0 PAGE 1, DC8 SRM 51-1-9 T/R 51-142, 51-1-9A T/R 51-141, AND DC8 SRM 51-1-8B.

Part: FITTING — CRACKED (CARGO BAY) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STATION 759.000 RIGHT BOTTOM LINE 22". REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, AND DC8 SRM 51-1-8B.

Part: FITTING — CRACKED (CARGO BAY) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FORWARD FITTING CRACKED AT STATION 717.000 LEFT BOTTOM LINE 22". REMOVED CRACKED FITTING. CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-3-1, AND DC8 SRM 51-1-8B.

Part: FITTING — CRACKED (BS 717) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FORWARD FITTING CRACKED AT STATION 717.000 RIGHT BOTTOM LINE 22". REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2003-05, DRAWING DOUGLAS 3755222, DPS 4.707, DC8 SRM 51-1-8B, AND 51-3-1.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP SKIN UPPER PART DENTED AT STATION XW 114.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGE AREA. FABRICATED NEW SKIN. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-1-21, DC8 SRM 57-1-0 PAGE 1, DC8 SRM 57-7-1 FIGURE 1 ITEM "D", AND DC8 SRM 51-1-8B.

Part: FITTING — CRACKED (FUSELAGE) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT BATH TUB FITTING CRACKED AT STATION 680.000. REMOVED CRACKED FITTING. INSTALLED NEW BATH TUB FITTING IAW DC8 SRM 51-1-20D, AND 51-3-1.

Part: FITTING — CRACKED (CARGO BAY) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STATION 781.000 RIGHT BOTTOM LINE 22". REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC8 SRM 51-1-8B, 51-3-1, ATI REPAIR SPECIFICATION 2003-05, DRAWING DOUGLAS 3755222, AND DPS 4.707.

Part: FITTING — CRACKED (BS 700) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT AFT FITTING CRACKED AT STATION 700.000 LBL 22. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2003-05, DRAWING DOUGLAS 3755222, DPS 4.707, DC8 SRM 51-1-8B, AND 51-3-1.

Part: FITTING — CRACKED (BS 55 L7L) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND MAIN CARGO COMPARTMENT FITTING CRACKED AT STATION 55.000 LONGERON 7LEFT. REMOVED CRACKED FITTING. FABRICATED NEW FITTING. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND AFTER INSPECTION. CLEANED, TREATED AND PRIMED AREA AND NEW FITTING. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, ATI REPAIR SPECIFICATION NUMBER 2003-05, DPS 4.707, DC8 SRM 51-1-8B, AND 51-3-1.

Part: SKIN — MISREPAIRED (RT WING TE FLAP) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND RIGHT WING INBOARD FLAP LOWER PANEL SKIN HAS IMPROPER REPAIR AT STATION XW 18.000. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. FABRICATED NEW SKIN AND BONDED DOUBLER. BONDED PARTS AS NEEDED WITH HYSOL. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-1-21, DC8 SRM 57-7-1 FIGURE 1 ITEM "B" AND "L", DC8 SRM 57-1-0 PAGE 1, 51-1-21, DC8 SRM 51-1-9 TR NUMBER 51-142, 51-1-9A TR NUMBER 51-141, AND DC8 SRM 51-1-8B.

Part: SKIN — MISREPAIRED (BS 1395 L36) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND DOUBLER AFT LOWER FUSELAGE BELLY SKIN BELOW AND FWD D-PIT DOOR ALUMINUM RIVETS IN FRAMES AT FS 1395, LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, FILLER SKIN, INTERNAL FINGER DOUBLER, AND FILLER INTERNAL DOUBLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-1-12, 51-3-1, FAA FORM 8110-3 NUMBER 08205 DATED 04/29/08, SEMAN DRAWING NUMBER ED-4735 DATED 03/24/08, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B.

Part: SKIN — MISREPAIRED (ZONE 500) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT LEFT WING UPPER AFT SKIN PANEL. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-1-11, 51-1-20D, 51-3-1, AD 90-16-05, DC8 S/B 57-86, DOUGLAS DRAWING J060104, SERVICE SKETCH NUMBER 3313, BOEING MESSAGE 1-780888417-2 DATED 03-03-08, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B.

Part: SKIN — MISREPAIRED (ZONE 600`) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT RIGHT WING UPPER AFT SKIN PANEL. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW SRM 51-1-11, 51-1-20D, 51-3-1, AD 90-16-05, DC8 S/B 57-86, DOUGLAS DRAWING J060104, SERVICE SKETCH NUMBER 3313, BOEING MESSAGE 1-780888417-2 DATED 03-03-08, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B.

Part: SKIN — MISREPAIRED (BS 1446 L36) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND DOUBLER AFT LOWER FUSELAGE BELLY BELOW AND AFT OF D-PIT DOOR RIVET SPACING EXCEEDED ON SIDE FOUR, ALSO ALUMINUM FASTENERS IN FRAMES AT FS 1446 LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, FILLER SKIN, INTERNAL FINGER DOUBLER, FILLER INTERNAL DOUBLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-1-12, 51-3-1,FAA FORM 8110-3 NUMBER 08205 DATED 04/29/08M, SEMAN DRAWING NUMBER ED-4735 DATED 03/24/08, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND IMPROPER REPAIR AT FUSELAGE SKIN FORWARD OF FLAT AFT PRESSURE BULKHEAD AT LONGERON 28. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED EXISTING REPAIR DOUBLERS. REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION. NO CRACK AND CORROSION FOUND. FABRICATED EXTERNAL REPAIR DOUBLERS, FILLERS, FINGER DOUBLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW S/B 53A-080 DATED 06-22-04, AD 2007-02-02, ASB DC8-53-080 DATED JUNE 22 2004, FAA FORM 8100-9 DATED 04-02-08, DOUGLAS DRAWING SR08530032, BOEING MESSAGE 1-791406133-7 DATED 04-02-08, SEMAN DRAWING ED-4734 DATED 04-22-08, DC8 SRM 51-1-21, 51-3-0, 51-1-20D, DC8 NDT SPM PART 06-10-01-001, DC-8 SRM 51-1-8B, DC-8 SRM 51-1-11,AND DC-8 SRM 51-3-1.

Part: SKIN — MISREPAIRED (BS 1421 L36) · airframe 99,983 hrs · 32,243 cycles

DURING ROUTINE C CHECK INSPECTION, FOUND DOUBLER, AFT LOWER FUSELAGE BELLY BELOW D-PIT DOOR RIVET SPACING EXCEEDED AT FS 1421 LONGERON 36. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED INSPECTION NDT. NO CRACK, NO CORROSION FOUND. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, FILLER SKIN, INTERNAL FINGER DOUBLER, AND FILLER INTERNAL DOUBLERS. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS. INSTALLED NEW FASTENERS AND REPAIR PARTS IAW DC8 SRM 51-1-11, 51-1-12, 51-3-1, FAA FORM 8110-3 NUMBER 08205 DATED 04/29/08, SEMAN DRAWING NUMBER ED-4735 DATED03/24/08, DC8 SRM 51-1-20D, DC8 NDT SPM PART 06-10-01-001, AND DC8 SRM 51-1-8B.

Part: STRIKER — OBSTRUCTED (ZONE 700) · airframe 91,770 hrs · 37,006 cycles

DURING CLIMB-OUT OF KTOL, THE UPLATCH CHECK FAILED LIGHT AND FLICKERED, THEN REMAINED ON. THE CREW ACCOMPLISHED ALL NECESSARY PROCEDURES, THE LIGHT REMAINED ILLUMINATED. THE CREW CONTINUED FLIGHT AND FELT A MODERATE BUMP. THE CREW RETURNED TO KTOL AND LANDED WITH OUT INCIDENT. MAINTENANCE REPLACED MAIN LANDING GEAR DOORS LIGHT SOCKET, AND INSPECTED MAIN LANDING GEAR DOORS AND FOUND LEFT MAIN LANDING GEAR DOOR SWITCH STRIKER CATCHING ON SEAL RETAINER, TRIMMED SWITCH STRIKER. JACKED AIRCRAFT AND PERFORMED EXTENSION AND RETRACTION SIX TIMES IAW DACO DC8 MAINTENANCE MANUAL 32-30-0. NO OTHER DEFECTS FOUND. MAINTENANCE PERFORMED OPERATIONAL CHECK ON MAIN LANDING GEAR DOOR LIGHT. CHECK WAS GOOD IAW DACO DC8 MA

Part: CONNECTOR — LOOSE (FIRE LOOP) · airframe 988,701 hrs · 31,787 cycles

DURING FLIGHT FROM KTOL NUMBER 3 FIRE WARNING LIGHT AND FIRE WARNING BELL CAME ON. THE CREW ACCOMPLISHED ALL NECESSARY PROCEDURES AND LANDED WITHOUT INCIDENT IN KLAS. MAINTENANCE PERFORMED VISUAL INSPECTION ON THE NUMBER 3 ENGINE FOR FIRE, NO INDICATION OF FIRE FOUND. MAINTENANCE CHECKED THE FIRE LOOP FOR SHORT, ALL LOOPS CHECKED GOOD. INSPECTED PNEUMATIC LINES FOR RUPTURES, OR LOOSE CLAMPS, NONE FOUND. MAINTENANCE FOUND RIGHT FAN FIRE LOOP FORWARD CONNECTOR LOOSE IN BACKSHELL. REPLACED CONNECTOR IAW DACO DC8 MAINTENANCE MANUAL 20-50-1. MAINTENANCE DID OPERATIONAL CHECK ON NUMBER 3 FIRE WARNING SYSTEM, AND CHECK WAS GOOD. MAINTENANCE REPLACED BOTH NUMBER 3 AND 4 HRD FIRE BOTTLE. AIRCRAFT RETURNED TO SE

Part: CONTROL VALVE — LEAKING (HYD SYSTEM) · airframe 98,559 hrs · 31,670 cycles

DURING CLIMB-OUT FROM KBNA, AFTER THE FLAPS WERE RAISED, THE CREW NOTICED THE HYDRAULIC QUANTITY DECREASING. THE CREW PERFORMED LOSS OF HYDRAULIC CHECKLIST AND RETURNED TO KBNA AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE RIGHT WHEEL WELL SOAKED IN HYDRAULIC FLUID. FURTHER INSPECTION FOUND THE WING SLOT CONTROL VALVE LEAKING FROM DETERIORATED PACKINGS AT THE CENTER MOUNT BOLT. MAINTENANCE REMOVED AND REPLACED THE DEFECTIVE PACKINGS AND REINSTALLED THE WING SLOT CONTROL VALVE. MAINTENANCE RESERVICED AUXILIARY HYDRAULIC. SYSTEM AND RAN ENGINES AS REQUIRED TO REFILL THE HYDRAULIC SYSTEM. NO LEAKS NOTED AND THE OPERATIONAL CHECK WAS GOOD IAW ATI DC-8 ERH 70.01 AND DC-8 M/M 2

Part: TIRE — SEPARATED (ZONE 700) · airframe 98,498 hrs · 31,646 cycles

DURING TAKEOFF FROM KHRL AT APPROXIMATELY 80 PERCENT N1 ON ALL FOUR ENGINES, THE AIRCRAFT ENCOUNTERED A NOSE WHEEL CONTROL PROBLEM. THE AIRCRAFT PULLED TO THE LEFT AND WOULD NOT RESPOND TO POSITIVE RUDDER CORRECTION. THE CREW INITIATED THE REJECTED TAKEOFF AT 60 KNOTS. MAINTENANCE INSPECTED THE NOSE STEERING SYSTEM AND NOSE TIRES. THE NOSE TIRE TREAD CAP WAS FOUND TO BE SEPARATING FROM THE WHEEL ASSEMBLIES ON BOTH LEFT AND RIGHT NOSE TIRES. MAINTENANCE REPLACED BOTH NOSE WHEEL AND TIRE ASSEMBLIES, AND THE AIRCRAFT WAS RETURNED TO SERVICE IAW DC8MM 32-50-01 AND DC8MM 32-40-2.

Part: ENGINE — OVERTEMP · airframe 98,107 hrs · 31,508 cycles

DURING TAKEOFF ROLL, NR 1 ENGINE OVER TEMPED TO 916 DEGREES AND CLIMBING, THE CREW ABORTED THE TAKE OFF AT 124 KNOTS AND RETURNED TO PARKING. MAINTENANCE INSPECTED THE ENGINE PER ALL APPLICABLE DATA, PERFORMED A POWER ASSURANCE RUN, ALL TARGETS ACHIEVED WITH NO DEFECTS NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRESSURE SWITCH — FAULTY (OIL SYSTEM) · airframe 98,008 hrs · 31,473 cycles

DURING DESCENT INTO KTOL NUMBER THREE ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN PER ALL APPLICABLE DATA. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A FAULTY LOW OIL PRESSURE WARNING SWITCH. MAINTENANCE REPLACED THE LOW OIL PRESSURE WARNING SWITCH, AND THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DAMAGED (ZONE 600) · airframe 97,813 hrs · 31,421 cycles

DURING PRE-FLIGHT INSPECTION FOUND A HOLE ON THE RT IB FLAP TRAILING EDGE. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS IAW DRAWING NR AB84-57-100 DATED 7/28/06, AND DACO SRM 57-2-1.

Part: SKIN — DAMAGED (ZONE 600) · airframe 97,813 hrs · 31,421 cycles

DURING PRE-FLIGHT INSPECTION FOUND A HOLE ON THE RIGHT HAND INBOARD FLAP TRAILING EDGE. REMOVED DAMAGED AREA. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS PER COTNEY DRAWING NUMBER AB84-57-100 DATED 7/28/06, AND DACO DC8 SRM 57-2-1.

Part: TRANSMITTER — FAILED (OIL PRESSURE) · airframe 97,791 hrs · 31,412 cycles

DURING CRUISE FROM KSJC TO KRFD, THE NR 3 ENGINE LOW OIL PRESSURE LIGHT CAME ON. THE CREW RETARDED THE THROTTLE TO IDLE AND THE LIGHT REMAINED ON. THE ENGINE OIL PRESSURE, QUANTITY, AND TEMPERATURE WERE NORMAL. THE CREW DECIDED TO SHUT DOWN THE ENGINE AS A PRECAUTIONARY MEASURE, AND BYPASS KRFD AND FLY DIRECT TO KTOL WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. WINDMILLING OIL PRESSURE WAS APPROXIMATELY FIVE PSI. MAINTENANCE INSPECTED THE ENGINE AND FOUND THE OIL PRESSURE TRANSMITTER AT FAULT. MAINTENANCE REPLACED THE OIL PRESSURE TRANSMITTER, AND THE OPERATIONAL CHECK WAS SUCCESSFUL. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: ACCESS DOOR — CRACKED (VERTICAL STAB) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C CHECK INSPECTION, LEFT HAND VERTICAL STABILIZER ACCESS DOOR EDGE CRACKED. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06119 DATE 03-07-06, SEMAN DWG ED 4187 DATE 03-06-06, EO SEMAN 2006150 DATE 03-07-06. REMOVED FASTENERS IAW DC-8 SRM 51-1-21. REMOVED DAMAGED IAW SEMAN DWG ED 4187. PERFORMED NDT INSPECTION IAW DC-8 NDT IAW DC-8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER & FILLER IAW SEMAN DWG ED 4187. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 4187, DC-8 SRM 51-1-21, DC-8 SRM 51-1-20D, DC-8, DC-8 SRM 51-3-1.

Part: SKIN — DENTED (XA 662.000) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, LT WING OUTBOARD AILERON L/E DENTED, XA 662.000. PERFORMED MAJOR REPAIR IAW DC-8 SRM 57-8-1 FIG 4. PERFORMED NDT INSPECTION DETECT CRACK IAW DC-8 NDT SPM PART 06-10-01-001. CRACK FOUND 0.250 LENGTH ENCLOSED SMN FORM 242-2. REMOVED DAMAGED PLATING IAW DC-8 SRM 57-1-0, DC-8 SRM 51-1-21. FABRICATED NEW PLATING (ALCLAD 2024 T3 0.032) IAW DC-8 SRM 57-8-1 FIG 4 ITEM H, DOUGLAS DWG 5763133. CLEANED, TREATED AND PRIMED AREA + NEW PLATING INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTALLED NEW PLATING IAW DC-8 SRM 51-1-21.

Part: SKIN — CRACKED (ZONE 500) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, LT WING NR 1 STUB WING CRACKED 2.5 INCH, XILD 42 LWR SKIN. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1A FIG 1. REMOVED EXISTING DOUBLERS IAW DC8 SRM 51-1-20D, DC-8 SRM 51-1-21. PERFORMED STOP HOLE ON CRACK END. FABRICATED EXTERNAL REPAIR DOUBLER (AL 7075 T6 0.080) + INTERNAL DOUBLER (AL 7075 T6 0.063) IAW DC8 SRM 57-2-1A FIG 1, DC-8 SRM 51-1-4 (FORMING). PERFORMED HEAT TREATMENT 7075 O TO 7075 T6 IAW DC-8 SRM 51-1-1 PAGES 1, 13, 17. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-1A FIG 1, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-3-1 (TORQUE).

Part: BULKHEAD — CORRODED (FUSELAGE) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C CHECK, FLT CMPT CORR BETWEEN FINGER DOUBLER AND BULKED, STA 67 RBL 53. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06130 DATE 03-09-06 EO SEMAN 2006174 DATE 03-15-06. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17, 18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PAGE 2P. REMOVED DAMAGED AREA IAW SEMAN DWG ED-4192. REMOVED CORRODED CLIP IAW DC8 SRM 51-3-0. PERFORMED NDT INSP TO AREA IAW DC8 NDT SPM PART 06-10-01-001. NO CRACK. FABBED INTERNAL FINGER DOUBLER AND FILLER AND STRUCTURAL FILLERS AND EXTERNAL TRIPLER DOUBLER IAW SEMAN DWG ED 4192. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW DC8 SRM 51-1-8B . FABBED NEW CLIP IAW ATI REPAIR SPECIFICATION 2003-05, EA SEMAN 2000171. PERFORMED HEAT

Part: REPAIR — MISINSTALLED (XF 16.000) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, RT WING INBOARD FLAP LWR FWD SKIN NON STANDRAD REPAIR, XF 16.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 2, 4) TR 57-91 DATE 09-30-01. REMOVED EXISTING NON STANDARD REPAIR IAW DC8 SRM 51-1-21. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER + FILLER (AL 2024 T3 0.050) IAW DC-8 SRM 57-2-5 FIG 2 (SHEET 2, 4), DC-8 SRM 57-7-1 FIG 1 PAGE 2 ITEM B AND L. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-5 FIG 2 (SHEET 2, 4), DC8 SRM 51-1-9A, DC8 SRM 51-1-21.

Part: FRAME — CORRODED (ZONE 100) · airframe 97,112 hrs · 31,235 cycles

DURING C CHECK, FRAME CORRODED AT STA- 62.000 BETWEEN LONGERON-21 AND LONGERON-22. PERFORMED MAJOR REPAIR IAW DC8 SRM 53-3-3 FIG 3. REMOVED CORROSION IAW DC8 SRM 51-1-8 PAGES 17-18. FOUND OUT OF LIMITS IAW DC-8 SRM 53-2-0 PAGE 2P. REMOVED FRAME SEGMENT AND (02 EA) CORRODED CLIPS IAW DC-8 SRM 53-1-0, DC-8 SRM 51-1-21, DC-8 SRM 51-3-0. FAB`D NEW FRAME SEGMENT (ALCLAD 7075 “O” 0.050”) IAW DC-8 SRM 53-3-3 FIG 3 (SHEET 2, 2A) ITEM “G”, DC-8 SRM 51-1-4 (CORNERS). PERFORMED HEAT TREATMENT (7075 “O” TO 7075 T6) IAW DC-8 SRM 51-1-1 PAGES 1, 13, AND 17. CLEANED, TREATED AND PRIMED NEW FRAME SEGMENT IAW DC-8 SRM 51-1-8B. FAB`D (02 EA) CLIPS (ALCLAD 7075 T6 51), (PN 4643970-1 ATI 03-05), (PN 3643968 ATI 03-05) IAW

Part: SKIN — DENTED (RT WING) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C CHECK, RT WING L/E DENTED (STA XFS 888.000 920.000). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-3-3 FIG 8. REMOVED DAMAGED PLATING IAW DC8 SRM 57-1-0, DC8 SRM 51-1-21. FABRICATED NEW PLATING (AL 7075 T6 0.050) IAW DC8 SRM 57-3-3 FIG 8 ITEM A, DC-8 SRM 51-1-4 (FORMING) BONDED NEW PLATING AND EXISTING INNER DOUBLER WITH HYSOL IAW DC8 SRM 51-1-9, DC8 SRM 51-1-9A. CLEANED, TREATED AND PRIMED AREA AND INNER FACE OF NEW PLATING IAW DC8 SRM 51-1-8B. INSTALLED RIVETS IAW DC8 SRM 51-1-21.

Part: PANEL — CRACKED (ZONE 500) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, NR 1 PYLON LT UPPER PART PANEL CRACKED 2 INCHES, YN 321.000. PERFORMED MAJOR REPAIR IAW DC8-70 SB 54-93 CONDITION V. REMOVED FASTENERS IAW SB 54-93 PAGE 11 FIG 2 DC8 SRM 51-3-0, DC8 SRM 51-1-21. PERFORMED VISUAL INSPECTION TO PYLON ADAPTER PANEL FOR CRACK, BREAKS OR MISALIGNED BOLTS. NEITHER CRACKS, BREAKS, CORROSION NOR MISALIGNED BOLTS. PERFORMED STOP HOLE ON CRACK END AND FABRICATED (04EA) DOUBLERS (AL7075T6 0.090) IAW SB 54-93 PAGES 8, 9, 10. CLEANED, TREATED AND PRIMED AREA + REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS.

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C CHECK INSPECTION, RIGHT WING OUTBOARD INNER LEADING EDGE EXTERNAL UPPER SKIN HAS NON STANDARD REPAIR AT STATION XFS 572.500. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-1 FIG 38 TR # 57-85 DATE 11-27-2000. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. TRIMMED OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER (AL 7075 T6 0.063”) AND FILLER (AL 7075 T6 0.050”) IAW DC-8 SRM 57-2-1FIG 38, DC-8 SRM 57-3-3 FIG 1) ITEM “A”. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-1 FIG 38, DC8 SRM 51-1-21, DC-8 SRM 51-3-0, DC-8 SRM 51-1-20D, DC-8 SRM 51-3-1.

Part: SKIN — DENTED (LE FLAP) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, LT WING INBOARD FLAP L/E LWR FWD PART DENTED, XW 40.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 2, 4) TR 57-91 DATE 09-30-01. REMOVED FASTENERS IAW DC8 SRM 51-1-21. TRIMMED OUT DAMAGED AREA. FABRICATED REPAIR DOUBLER (AL 2024 T3 0.050) IAW DC-8 SRM 57-2-5 FIG 2 (SHEET 2, 4) DC-8 SRM 57-7-1 FIG 1 PAGE 2 ITEM -B- AND -N-. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-5 FIG 2 (SHEET 2, 4) DC8 SRM 51-1-9A, DC8 SRM 51-1-21.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C CHECK, RT FUSELAGE NOSE SECTION. HEAT EXCHANGER COMPT LWR AFT JAMB CORNER ACS MODIFICATION DOUBLER REINFORCEMENT DOUBLER CRACKED 1/2 INCH STA 12.000 L-27R. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06130 DATE 03-15-06 SEMAN DWG NR ED 4184 DATE 03-10-06, EO SEMAN 2006142 DATE 03-15-06. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. TRIMMED OUT DAMAGED AREA IAW SEMAN DWG NO ED-4184. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER & REPAIR TRIPLER & FILLER IAW SEMAN DWG ED 4184. CLEANED, TREATED AND PRIMED AREA & REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW DC8 SRM 51-1-21, SE

Part: SKIN — MISREPAIRED (ZONE 600) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C CHECK INSPECTION, RIGHT WING OUTBOARD. FLAP LOWER AFT SKIN NON STANDARD REPAIR, AT STATION XF 350.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4 TR NR 57-94 DATE 10-01-02. REMOVED DAMAGED PANEL PLATING IAW DC8 SRM 57-1-0, DC8 SRM 51-1-21. FABRICATED PLATING (AL 2024T3 0.050”) AND DOUBLER (AL 2024T3 0.040”) IAW DC8 SRM 57-7-1 FIG 4 TR NR 57-94 ITEMS “A” AND “G”. BONDED BOTH PARTS WITH HYSOL IAW DC8 SRM 51-1-9, DC8 SRM 51-1-9A. CLEANED, TREATED AND PRIMED AREA AND NEW PANEL PLATING IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED NEW PANEL PLATING IAW DC8 SRM 51-1-21.

Part: ELEVATOR — IMPROPER (ZONE 500) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, LT ELEVATOR UPPER SURFACE HAS NON - STANDARD REPAIR AT STA XE 99.281. PERFORMED MAJOR REPAIR IAW DC8 SRM 55-4-1 FIG 1. REMOVED PANEL PLATING WITH STANDARD REPAIR IAW DC8 SRM 55-1-0, DC8 SRM 51-1-21. FABRICATED NEW PLATING + BONDED FINGER DOUBLER IAW DC8 SRM 55-4-1 FIG 1. BONDED BOTH PARTS WITH HYSOL IAW DC8 SRM 51-1-9, DC8 SRM 51-1-9A. CLEANED, TREATED AND PRIMED AREA + NEW PANEL PLATING IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED NEW PANEL PLATING IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0, 51-3-1. PERFORMED BALANCE TO LT ELEVATOR IAW DC8 SRM 51-4-4 FOUND WITHIN LIMITS TABLE MOMENT 1.449. 37 IN LBS.

Part: REPAIR — MISINSTALLED (XFS 47.500) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, RT HORZ STAB L/E UPPER SURFACE HAS NON - STANDARD REPAIR, STA XFS 47.500. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, 06130 DATE 03-15-06, SEMAN DWG ED 4188 DATE 03-08-06, EO SEMAN 2006149 DATE 03-15-06. REMOVED NON STANDARD REPAIR IAW DC-8 SRM 51-1-21. REMOVED DAMAGED AREA IAW SEMAN DWG ED 4188. PERFORMED NDT INSPECTION IAW DC-8 NDT IAW DC-8 NDT SPM PART 06-10-01-001. FABRICATED FILLER (ALCLAD 7075 T6 0.050) + REPAIR DOUBLER (ALCLAD 7075 T6 0.063) IAW SEMAN DWG ED 4188. CLEANED, TREATED AND PRIMED AREA + FILLER + REPAIR DOUBLER INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIR PARTS (TORQUE).

Part: SKIN — CRACKED (BS 1766 L28L) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, EMPENNAGE 1 INCH CRACK, STA 1766.000, L-28L. REPAIRED PER ALL APPLICABLE DATA.

Part: FITTING — CRACKED (ZONE 500) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C CHECK INSPECTION, LEFT WING NR 2 MAIN TANK LOWER FORWARD FITTING CRACKED, AT STATION 74.000, STRINGER-50. REMOVED AND REPLACED CRACKED FITTING ON LEFT WING NR 2 MAIN TANK LOWER PART, STATION 74.000 S-50 IAW DC8 SRM 51-1-20D DC8 SRM 51-3-1.

Part: REPAIR — MISINSTALLED (BS 1560) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, LEFT CUSP EXTRUSION UPPER SURFACE FRAME NON STANDARD REPAIR, STA 1560.000 L-20L. PERFORMED MAJOR REPAIR. REMOVED NON STANDARD REPAIR. REMOVED DAMAGED AREA, FABRICATED NEW FRAME SEGMENT P/N 52645791. FABRICATED (02 EA) ANGLES. PERFORMED HEAT TREATMENT TO NEW ANGLES IAW DC-8 SRM 51-1-1 PAGES 1, 13, 17 DPS 7.00.1 REV -BK-. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW DC8 SRM 53-2-0 FIG 2 (SHEET 4, 6) DC8 SRM 53-2-0 FIG 2 (SHEET 5).

Part: PANEL — CRACKED (NR 4 PYLON) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C CHECK, RT WING NR 4 PYLON PANEL CRACKED, YN 321.000. PERFORMED MAJOR REPAIR IAW DC8-70 SB 54-93 CONDITION V. REMOVED FASTENERS IAW SB 54-93 PAGE 11 FIG 2 DC8 SRM 51-3-0, DC8 SRM 51-1-21. PERFORMED VISUAL INSPECTION TO PYLON ADAPTER PANEL FOR CRACKS, BREAKS OR MISALIGNED BOLTS. NEITHER CRACKS, BREAKS, CORROSION NOR MISALIGNED BOLTS. PERFORMED STOP HOLE ON CRACK END AND FABRICATED (04EA) DOUBLERS (AL7075T6 0.090”) IAW SB 54-93 PAGES 8, 9, 10. CLEANED, TREATED AND PRIMED AREA & REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW SB 54-93 PAGES 13, 14, 15, 16, DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-3-1 (TORQUED)

Part: REPAIR — MISINSTALLED (XF 21.000) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, RT WING INBOARD FLAP PANEL LWR SKIN NON STANDARD REPAIR, XF 21.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 3, 4) TR 57-91 DATE 09-30-01. REMOVED EXISTING NON STANDARD REPAIR IAW DC8 SRM 51-1-21. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER (AL 2024 T3 0.063) IAW DC-8 SRM 57-2-5 FIG 2 (SHEET 3, 4), DC-8 SRM 57-7-1 FIG 1 ITEM B AND L. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-5 FIG 2 (SHEET 3, 4), DC8 SRM 51-1-9A, DC8 SRM 51-1-21.

Part: FITTING — CRACKED (ZONE 500) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C CHECK INSPECTION, LEFT WING NR 2 MAIN TANK LOWER FITTING CRACKED, STA 220.00 STRINGER-59. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. FABRICATED NEW FITTING (AL 7075 T6 51) IAW ATI REPAIR SPECIFICATION NR 2003-05 EA SEMAN NR 20061966 DATE 03-13-06. PERFORMED NDT INSPECTION IAW NDT SPM PART 08-00-02 TO 07. NO CRACK FOUND. ENCLOSED SMN FORM 242-4. PERFORMED HEAT TREATMENT 7075 T6 51 TO 7075 T6 IAW DC-8 SRM 51-1-1 PAGES 1,13, AND 17. CLEANED, TREATED AND PRIMED AREA, NEW FITTING IAW DC-8 SRM 51-1-8B. INSTALLED NEW FITTING IAW DC8 SRM 51-1-20D, DC-8 SRM 51-3-1.

Part: REPAIR — MISINSTALLED (XF 346.00) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, LT WING OUTBOARD FLAP L/E UPPER PART HAS NON STANDARD REPAIR WORN 1 INCH, XF 346.00. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 4 TR 57-94 DATE 10-01-02. REMOVED DAMAGED PLATING WITH NON STANDARD REPAIR IAW DC8 SRM 57-1-0, DC-8 SRM 51-1-21. FABRICATED NEW PLATING (AL 2024 T3 0.063) IAW DC-8 SRM 57-7-1 FIG 4 ITEM B. CLEANED, TREATED AND PRIMED AREA + NEW PLATING INTERNAL PARTS IAW DC-8 SRM 51-1-8B. APPLIED NEW SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21.

Part: SKIN — WORN (FUSELAGE) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, EXTERNAL FUS LWR SKIN WORN AT SEVERAL SPOTS; STA 680.000 - STA 720.000. PERFORMED MAJOR REPARI BY REMOVING CORROSION IAW DC8 SRH 51-1-8 PGS 17, 18. FOUND OUT OF LIMITS IAW DC8 SRM 53-2-0 PAGE 2P. REMOVED THE DAMAGED AREA IAW SEMON DWG NO EO-4185. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01. FABRICATED NEW PANEL SEGMENT AND REPAIR DOUBLER STRAP AND TRIPLER STRAP. CLEANED TREATED AND PRIMED AREA AND REPAIR PARTS IAW DC8 SRM 51-1-8B. INSTALLED REPAIR PARTS IAW SEMAN DWG EO-4185 DC8 SRM 51-1-20D, DC8 SRM 51-3-0 DC8 SRM 51-3-1.

Part: STRUCTURE — DENTED (T/E FLAP) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, LT WING FLAP L/E INBOARD PANEL LWR PART DENTED 3 INCHES, STA XW 79.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-7-1 FIG 1. REMOVED DAMAGED PANEL PLATING IAW DC8 SRM 57-1-0, DC8 SRM 51-1-21. FABRICATED PLATING (AL 2024T3 0.032) + BONDED FINGER DOUBLER (AL 2024T3 0.020) IAW DC8 SRM 57-7-1 FIG 1 ITEMS B, L. BONDED BOTH PARTS WITH HYSOL IAW DC8 SRM 51-1-9, DC8 SRM 51-1-9A. CLEANED, TREATED AND PRIMED AREA + NEW PANEL PLATING IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED NEW PANEL PLATING IAW SRM 51-1-21.

Part: REPAIR — MISINSTALLED (XF 415.-XF 418.) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, LT WING OUTBOARD FLAP T/E UPPER PANEL HAS NON STANDARD REPAIR BETWEEN XF 415.000 AND XF 418.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 1 (SHEET 1, 2). REMOVED NON STANDARD REPAIR (EXISTING) IAW DC8 SRM 51-1-21. REMOVED DAMAGED AREA. FABRICATED NEW PLATING SEGMENT (AL 2024 T3 0.050) + SPLICE (ALCLAD 2024 T3 0.063) + FILLER (ALCLAD 2024 T3 0.020) IAW DC-8 SRM 57-2-5 FIG 1 (SHEET 1, 2) DC-8 SRM 57-7-1 FIG 4 TR 57*94 ITEM Q AND U. CLEANED, TREATED AND PRIMED AREA AND REPAIR PARTS IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW DC8 SRM 57-2-5 FIG 1 (SHEET 1, 2) DC8 SRM 51-1-21.

Part: REPAIR — MISINSTALLED (XF 430.000) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, RT WING OUTBOARD FLAP PANEL LWR SKIN NON STANDARD REPAIR, XF 430.000. PERFORMED MAJOR REPAIR IAW DC8 SRM 57-2-5 FIG 2 (SHEET 3, 4) TR 57-91 DATE 09-30-01. REMOVED EXISTING NON STANDARD REPAIR IAW DC8 SRM 51-1-21. REMOVED DAMAGED AREA. FABRICATED REPAIR DOUBLER (AL 2024 T3 0.050) IAW DC-8 SRM 57-2-5 FIG 2 (SHEET 3, 4), DC-8 SRM 57-7-1 FIG 4 TR 57-94 ITEM U AND N. CLEANED, TREATED AND PRIMED AREA AND REPAIR DOUBLER IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR DOUBLER IAW DC8 SRM 57-2-5 FIG 2 (SHEET 3, 4), DC8 SRM 51-1-9A, DC8 SRM 51-1-21.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C CHECK, LT FUSELAGE NOSE SECTION HEAT EXCHANGER COMPT, LWR AFT JAMB CORNER ACS MODIFICATION DOUBLER REINFORCEMENT DOUBLER CRACKED 1/2 INCH STA 12.000 L-27L. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06119 DATE 03-07-06 SEMAN DWG NR ED 4183 DATE 03-02-06, EO SEMAN 2006141 DATE 03-07-06. REMOVED EXISTING REPAIR DOUBLER IAW DC8 SRM 51-1-21. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER, REPAIR TRIPLER, AND FILLER IAW SEMAN DWG NR ED 4183. CLEANED, TREATED AND PRIMED AREA & REPAIR PARTS IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW SEMAN DWG NR EO 4183, DC8 SRM 51-1-21, DC8 SRM 51-1-20D, DC8 SRM 51-

Part: REPAIR — MISINSTALLED (XFS 335.250) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, RIGHT WING - CTR L/E LWR EXTERNAL PART NON STANDARD REPAIR XFS 335.250. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3, 06130 DATE 03-15-06, SEMAN DWG ED 4189 DATE 03-07-06, EO SEMAN 2006154 DATE 03-15-06. REMOVED NON STANDARD REPAIR IAW DC-8 SRM 51-1-21. REMOVED DAMAGED AREA IAW SEMAN DWG ED 4189. PERFORMED NDT INSPECTION IAW DC-8 NDT IAW DC-8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER (ALCLAD 7075 T6 0.071) + FILLER (ALCLAD 7075 T6 0.063) IAW SEMAN DWG ED 4189. CLEANED, TREATED AND PRIMED AREA + FILLER + REPAIR DOUBLER INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTALLED REPAIR PARTS.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C-CHECK INSPECTION, LT ELEVATOR UPPER SKIN 1 INCH CRACK AT STA XE 71.169. PERFORMED MAJOR REPAIR IAW DC8 SRM 55-4-1 FIG 1 (SHEET 1, 2). REMOVED DAMAGED PLATING IAW DC8 SRM 55-1-0 PAGE 1, DC-8 SRM 51-1-21. FABRICATED NEW PLATING (AL 2024 T3 0.040) IAW DC8 SRM 55-4-1 FIG 1 (SHEET 1, 2) ITEM -B-. CLEANED, TREATED AND PRIMED AREA + NEW PLATING INTERNAL PART IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED NEW PLATING IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0, DC8 SRM 51-3-1.

Part: VANE — DAMAGED (L/E SLOT) · airframe 97,112 hrs · 31,235 cycles

DURING ROUTINE C CHECK, LT WING L/E INBD SLOT VANE HOLES ELONGATED, XILD 7095. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3 06119 DATE 03-07-06, SEMAN DWG ED 4186 DATE 03-04-06, EO SEMAN 2006146 DATE 03-07-06. REMOVED FASTENERS IAW DC-8 SRM 51-1-21, DC-8 SRM 51-3-0. TRIMMED OUT DAMAGED AREA IAW SEMAN DWG ED 4186. PERFORMED NDT INSPECTION IAW DC-8 NDT IAW DC-8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER, FILLER, INTERNAL DOUBLER IAW SEMAN DWG ED 4186. CLEANED, TREATED AND PRIMED AREA, FILLER, INTERNAL DOUBLER, REPAIR DOUBLER INTERNAL PART IAW DC-8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC-8 SRM 51-1-11. INSTALLED REPAIR PARTS IAW SEMAN DWG ED 4186, DC-8 SRM 51-1-21, DC-8 SRM 51-1-20D,

Part: SKIN — MISREPAIRED (LT ELEVATOR) · airframe 97,112 hrs · 31,235 cycles

DURING C CHECK, LT ELEVATOR UPPER SURFACE HAS NON STANDARD REPAIR AT STA XE 32.937. PERFORMED MAJOR REPAIR IAW DC8 SRM 55-4-1 FIG 1. REMOVED PANEL PLATING WITH STANDARD REPAIR IAW DC8 SRM 55-1-0, DC8 SRM 51-1-21. FABRICATED NEW PLATING AND BONDED FINGER DOUBLER (AL 2024T3 0.016”) IAW DC8 SRM 55-4-1 FIG 1 (SHEET 1, 2) ITEMS “E”, “F”. BONDED BOTH PARTS WITH HYSOL IAW DC8 SRM 51-1-9, DC8 SRM 51-1-9A. CLEANED, TREATED AND PRIMED AREA AND NEW PANEL PLATING IAW DC8 SRM 51-1-8B. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED NEW PANEL PLATING IAW DC8 SRM 51-1-21, DC8 SRM 51-3-0, 51-3-1. PERFORMED BALANCE TO LT ELEV IAW DC8 SRM 51-4-4, FOUND WITHIN LIMITS. TABLE MOMENT 1.449. 37 IN LBS.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 96,893 hrs · 31,147 cycles

LANDING GEAR FAILED UPLATCH CHECK OUT OF KEWR. "GEAR NOT LATCHED" LIGHT STAYED ON. CREW RECYCLED GEAR AND LIGHT WENT OUT. LANDED IN KTOL WITHOUT INCIDENT. MAINTENANCE TRANSFERRED THIS TO DMI NR 33576 IN ACCORDANCE WITH DC8 MEL 32-16-0A CAT "A" WITH A NO FLY DATE OF 2 FLIGHT DAYS (1/19/06). PROCEDURE 36-16A ACCOMPLISHED AND PLACARD INSTALLED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: SCREW — LOOSE (PROX SENSOR) · airframe 96,757 hrs · 31,077 cycles

ON TAKEOFF FROM KTOL TO KBFI GEAR HANDLE UP GEAR NOT LATCHED LIGHT STAYED ON. LANDING CYCLED DOWN THEN UP LIGHT WENT OUT. MAINTENANCE LUBED GEAR UP LATCHES AND INDICATOR SWITCHES, NO DEFECTS NOTED. MAINTENANCE FOUND A LOOSE SCREW ON RT DOOR UP LATCH PROXIMITY SWITCH. SCREW WAS TIGHTENED AND GEAR SWING WAS PERFORMED PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.

Part: PIN — INSTALLED (NLG) · airframe 96,666 hrs · 31,029 cycles

AFTER DEPARTURE FROM EDFH, NLG DID NOT RETRACT. FROM NGL INSPECTION WINDOW FOUND GROUND PIN STILL IN GEAR. RETURNED AIRCRAFT TO EDFH AND CREW LANDED WITHOUT INCIDENT. FOUND GROUND HANDLERS NOSE GEAR PIN INSTALLED. THE HANDLERS NOSE GEAR PIN WAS REMOVED, PER ANY APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: RELAY — DEFECTIVE (FIRE WARNING) · airframe 94,435 hrs · 30,500 cycles

NR 4 ENGINE FIRE WARNING LIGHT AND BELL CAME ON DURING CLIMB AT 36,000 FT. CREW SHUT DOWN ENGINE, HAD NO OTHER INDICATION. ENGINE SHORT CIRCUIT LIGHT WOULD NOT TEST. CREW CONTINUED TO HAVE GOOD OIL PRESSURE ON ENGINE. MAINTENANCE REMOVED AND REPLACED O/B FIRE BOTTLE. CHECKED ALL ENGINE FIRE DETECTOR ELEMENTS AND FIRE WARNING CONNECTORS. REMOVED AND REPLACED NR 4 ENGINE FIRE CONTROL RELAY AND SYSTEMS CHECK IS NORMAL PER ALL APPLICABLE MANUALS AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSING ELEMENT — INTERMITTENT (NR 4 ENGINE) · airframe 94,344 hrs · 30,466 cycles

DURING CRUISE FROM KTOL THE FIRE WARNING LIGHT AND BELL CAME ON FOR THE NR 4 ENGINE. NO OTHER INDICATIONS WERE NOTED. CREW RETURNED AIRCRAFT TO KTOL AND LANDED WITHOUT INCIDENT. AN INSPECTION IS ON GOING. AS SOON AS THE INFORMATION IS AVAILABLE IT WILL BE PROVIDED. MAINTENANCE OHM CHECKED FIRE WARNING SYSTEM, FINDING INTERMITTENT PROBLEM. REMOVED AND REPLACED 5 FIRE SENSING ELEMENTS, CHECKED BLEED LINES FOR LEAKS WITH NONE NOTED. RAN AIRCRAFT TO POWER AND FIRE WARNING CHECKED GOOD PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.

Part: RIB — CRACKED (RT WING) · airframe 94,312 hrs · 30,453 cycles

DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING NR 4 STUB WING INTERNAL RIB CRACKED 3" XS 520.468. MAJOR REPAIR ACCOMPLISHED REMOVAL OF CRACKED RIB IAW DC8 SRM 51-1-20D PAGE 21 DC8 SRM 51-3-0 PG 1. FABRICATED NEW RIB IAW REPAIR SPEC NR 2003-05 DWG 9753297 DC8 SRM 51-1-1 PG 1. PERFORMED HEAT TREATMENT IAW DC8 SRM 51-1-1 PG 1, 13, 17 DPS7.00-1 REV. PERFORMED NDT INSPECTION IAW DC8 NDT SPM PART 00-00-02/07. CLEANED, TREATED AND PRIMED AREA + NEW RIB IAW DC8 SRM 51-1-8B. INSTALLED NEW RIB WITH FASTENERS IAW DC8 SRM 51-3-0 PG 1 DC8 SRM 51-1-21 PG1 DC8 SRM 51-1-20D PG 9.

Part: DOOR — MISREPAIRED (ZONE 200) · airframe 94,312 hrs · 30,453 cycles

DURING A ROUTINE C-CHECK INSPECTION FOUND PASSENGER DOOR FORWARD UPPER CORNER HAS A TEMPORARY REPAIR. MAJOR REPAIR ACCOMPLISHED REMOVAL OF REPAIR. FABRICATED DOUBLER, TRIPLER, & FILLER. CLEANED, TREATED AND PRIMED AREA, REPAIRED PARTS. APPLIED SEALANT TO FAYING SURFACES. INSTALLED REPAIRED PARTS WITH NEW FASTENERS IAW SRM 53-2-0 FIG 15 SHEET 4,5,8, SRM 51-1-20A SRM 51-1-20D PG 9 AND SRM 51-1-21 PG 1, DWG 5750776.

Part: FLOOR PANEL — CORRODED (BS 759) · airframe 94,312 hrs · 30,453 cycles

DURING A ROUTINE C-CHECK INSPECTION FOUND FLOORBEAM CORROSION DAMAGE IN CARGO COMPARTMENT AT STA FS 759.000 LBL 10. REPAIR ACCOMPLISHED BY REMOVING THE CORROSION. FOUND OUT OF LIMITS IAW SRM 53-32-0 PG 2P. FABRICATED REAPRI ANGLE IAW DC8 SRM 53-2-0 FIG 1 SHEET 1, 2. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW SRM 51-1-11 P 9. INSTALLED REPAIR ANGLE IAW SRM 53-2-0 FIG 1G. SHEET 1, 2 SRM 51-1-21 PG 1, SRN 51-1-20D.

Part: FLOORBEAM — CORRODED (BS 640) · airframe 94,312 hrs · 30,453 cycles

DURING A ROUTINE C-CHECK INSPECTION, FOUND FLOORBEAMS IN FUSELAGE CARGO COMPARTMENT WITH CORROSION DAMAGE AT STA FS 640.000 RBL 38. REPAIR ACCOMPLISHED BY REMOVING CORROSION. FOUND OUT OF LIMITS. REMOVED DAMAGE AREA, FABRICATED ANGLE REPAIR AND FILLER. CLEANED, TREATED AND PRIMED AREA, ANGLE REPAIR & FILLER. APPLIED PRC SEALANT AND FAYING SURFACES IAW SRM 51-1-8B, 51-2-1 FIG SHEET 7 AND 12 TR 51-13D, 53-2-0, 51-1-11, AND 51-1-20D.

Part: PLATE — DENTED (WS 726.000) · airframe 94,312 hrs · 30,453 cycles

DURING A ROUTINE C CHECK INSPECTION, LT WING OUTBOARD AILERON UPPER OUTBOARD PLATING DENT DAMAGE AT STA XA 726.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED SKIN IAW DC8 SRM 51-1-21 PG1. FABRICATED NEW SKIN + FINGER DOUBLER IAW DC8 SRM 57-8-1 PG 9 FIG 4. BONDED SKIN AND FINGER DOUBLER IAW DC8 SRM 51-1-9 PGS 1/3. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. INSTALLED SKIN AND FINGER DOUBLERS IAW DC8 SRM 51-1-21 PG 1. INSTALLED NEW SKIN AND FINGER DOUBLER IAW DC8 SRM 51-1-21 PG 1.

Part: PLATE — DAMAGED (RT ELEVATOR) · airframe 94,312 hrs · 30,453 cycles

DURING A ROUTINE C CHECK INSPECTION, RT ELEVATOR UPPER PLATING INBOARD SECTION SEVERAL DAMAGES BETWEEN STA XAR O AND XE 132.00. MAJOR REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED UPPER PLATING IAW DC8 SRM 51-1-11 PG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 5-1-8B. INSTALLED NEW PLATING DC8 SRM 51-1-21 PG 1, DC8 SRM 5-1-21A PGS 1-4.

Part: VANE — DAMAGED (WS 6.224) · airframe 94,312 hrs · 30,453 cycles

DURING A ROUTINE C CHECK INSPECTION, FOUND ELONGATED HOLES ON RT WING EXTENDED LEADING EDGE OUTBOARD VANE FORWARD PLATING A STA XOLDI 6.224. MAJOR REPAIR ACCOMPLISHED REMOVAL FASTENERS IAW DC8 SRM 51-1-21 PGG1, DC8 SRM 51-3-0 PG 1. REMOVED DAMAGED AREA IAW DWG SEMON EO 3780 PERFORMED NDT INSPECTION IAW NOTE NR 3 DWG SEMON EO 3780, NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER, FILLER AND INTERNAL DOUBLER IAW DWG SEMAN EO 3780. CLEANED, TREATED AND PRIMED AREA, REPAIRED PARTS. INTERNAL PORT IAW DC8 SRM 51-1-8B APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIRED PARTS IAW DWG SEMON EO 3780 SR, 51-1-21 PG1 SRM 51-1-20D PG9 DC8 SRM 51-3-0.

Part: SKIN — DAMAGED (ZONE 500) · airframe 94,312 hrs · 30,453 cycles

DURING A C-CHECK INSPECTION, FOUND LT WING INBOARD FLAP UPPER SKIN WITH INTERIM REPAIR. MAJOR REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED PLATING PANEL. FABRICACTED NEW PLATING PANEL. CLEANED, TREATED AND PRIMED AREA AND NEW PLATING PANEL INTERNAL PART. APPLIED PRC SEALANT TO FAYING SERVICES. INSTALLED NEW PLATING PANEL IAW DC8 SRM 51-1-21, 51-3-0, 51-1-8B 51-1-11 AND FAA FORM 8110-3 DWG SEMAN ED 3774.

Part: PLATE — CORRODED (WS 716.000) · airframe 94,312 hrs · 30,453 cycles

DURING A C CHECK INSPECTION, RT OUTER WING OUTBOARD EXTENDED LEADING EDGE OUTER PLAING UPPER SIDE CORROSION DAMAGE AROUND STA XFS 716.000. MAJOR REPAIR ACCOMPLISHED REMOVAL OF CORROSION FROM RT WING OUTBD L/E UPPER SKIN AND IT WAS FOUND OUT OF LIMITS IAW DC8 SRM 57-2-1 PG 11. REMOVED DAMAGE SECTION IAW DC8 SRM 57-2-1 FIG 38. FABRICATED FILLER + DOUBLER IAW DC8 SRM 57-2-1 FG 38. CLEANED, TREATED AND PRIMED INNER FACE OF FILLER + DOUBLER IAW DC8 SRM 51-1-8B. APPLIED (PRC) SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-15 PG 1. INSTALLED FILLER + DOUBLER IAW DC8 SRM 57-2-1FG 38,TR NR 57-85, DC8 SRM 51-1-20D PG 7 DC8 SRM 51-1-21 PG 1.

Part: REPAIR — TEMPORARY (WS 6.224) · airframe 94,312 hrs · 30,453 cycles

DURING A C CHECK INSPECTION, FOUND LT WING EXTENDED L/E OUTBOARD VANE FORWARD OUTER PLATING INTERIM REPAIR AROUND STA XOLDI 6.224. MAJOR REPAIR ACCOMPLISHED REMOVAL OF INTERIM REPAIR IAW DWG SEMON EO 3784, DC8 SRM 51-1-21 PG 1, DC7 SNR 51-1-20D PG 21, AND 51-3-0 PG1. REMOVED DAMAGED AREA IAW DEG SEMON EO 3784. PERFORMED NDT INSPECTION IAW DWG SEMON EO 3784 NOTE 3 DC8 NDT SPM PART 06-10-01-001. FABRICATED REPAIR DOUBLER, INTERNAL DOUBLER AS REQUIRED. FILLER IAW DWG SEMON EO 3784. CLEANED, TREATED AND PRIMED AREA REPAIRED PARTS INTERNAL PARTS IAW DC8 SRM 51-1-8D. APPLIED SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIRED PARTS WITH NEW FASTNERS IAW DC8 SRM 51-3-0 PG 1.

Part: SKIN — DAMAGED (TE FLAP) · airframe 94,312 hrs · 30,453 cycles

DURING A ROUTINE C CHECK INSPECTION, RT WING INBD FLAP UPPER SKIN HAS INTERIM REPAIR BETWEEN STATION XW63.00-XW91.000. MAJOR REPAIR WAS ACCOMPLISHED BY REMOVED THE UPPER PLATING WITH INTERIM REPAIR. FABRICATED NEW PLATING PANEL, CLEANED, TREATED AND PRIMED AREA + NEW PLATING PANEL INTERNAL PART APPLIED SEALANT TO FAYING SURFACES. INSTALLED NEW PLATING PANEL IN ACCORDANCE WITH DC8 SRM 51-1-8B, FAA FORM 8110 NR 04571, DWG SEMAN EO 3375-1, SRM 51-1-11 AND 51-1-21 AND 51-3-0.

Part: SKIN — DAMAGED (LT WING) · airframe 94,312 hrs · 30,453 cycles

DURING A ROUTINE C CHECK INSPECTION FOUND LT L/E WING INBOARD EXTENDED L/E OUTER PLATING INTERIM REPAIR AROUND STA XSF 710.000. MAJOR REPAIR ACCOMP IAW FAA FORM 8110-3 NR 04592, DWG SEMON EO 3787. REMOVED FASTENERS IAW DC8 SRM 51-1-21 AND SRM 51-1-20D. REMOVED DAMAGED AREA IAW DWG SEMON EO 3787. PERFORMED NDT INSPECTION IAW DWG EO 3787, DC8 NDT SRM PART 06-10-01-001. FABRICATED EXTERNAL REPAIR DOUBLER + FILLER IAW DWG SEMON EO 3787. CLEANED, TREATED AND PRIMED AREA + REPAIRED PARTS INTERNAL PART IAW DC9 SRM 51-1-8B APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11. INSTALLED REPAIRED PARTS WITH NEW FASTENERS IAW DWG SEMAN EO 3787 DC8 SRM 51-1-21 AND 51-1-20D

Part: SKIN — DAMAGED (WS 7095) · airframe 94,312 hrs · 30,453 cycles

DURING A C CHECK INSPECTION, FOUND RT WING EXTENDED L/E INBD VANE FWD PLATING ELONGATED HOLES AROUND STA XILD 7095. MAJOR REPAIR ACCOMPLISHED REMOVAL OF FASTENERS IAW DC8 SRM 51-1-21 PG 1,DC8 SRM 51-3-0 PG 1. REMOVED DAMAGED AREA IAW SEMAN DWG EO 3792 DC8 NDT SPM PART 06-10-01 001. FAB`D EXTERNAL DOULBLER, FILLERS AND INTERNAL DOUBLER AS REQUIRED IAW SEMAN DWG EO 3792. CLEANED, TREATED AND PRIMED AREA AND INTERNAL DOUBLER, FILLER AND EXTERNAL DOUBLER AND INTERNAL PART IAW SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED INTERNAL DOUBLER, FILLER, EXTERNAL DOUBLER WITH NEW FASTENERS IAW SEMON DWG EO 3792 IAW DC8 SRM 51-1-21 PG 1 DC8 SRM 51-1-20D PG 9 AND 51-3-0 PG 1.

Part: SKIN — CORRODED (WS74.469-123.187) · airframe 94,312 hrs · 30,453 cycles

DURING A ROUTINE C CHECK INSPECTION, FOUND RT ELEVATOR LOWER PLATING INBOARD SECTION CORROSION DAMAGE BETWEEN STA XE 74.469 AND XE 123.187. MAJOR REPAIR ACCOMPLISHED REMOVAL OF DAMAGED AREA. CORROSION WAS REMOVED IAW DC8 SRM 55-2-1 FIG B PG 17-18. FOUND OUT OF LIMITS IAW DC8 SRM 55-2-0 PG 12. REMOVED THE DAMAGED SECTION IAW DC8 SRM 55-2-1 FIG 8. FABRICATED FILLER & REPAIR SPLICE IAW DC8 SRM 55-2-1 FIG 8 DC8 55-4-1 FIG 1. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B BONDED FILLER + REPAIR SPLICE WITH HYSOL IAW DC8 SRM 51-1-9A. INSTALLED NEW FASTENERS IAW DC8 SRM 51-1-21 PG 1.

Part: DOUBLER — DAMAGED (RT WING) · airframe 94,312 hrs · 30,453 cycles

DURING A ROUTINE C CHECK INSPECTION, FOUND RT WING OUTBOARD L/E INTERIM REPAIR AT STA XFS 710.000. ACCOMPLISHED MAJOR REPAIR BY REMOVING EXISTING REPAIR AND THE DAMAGED AREA. PERFORMED NDT INSPECTION. FABRICATED EXTERNAL DOULBER AND FILLER IN ACCORDANCE WITH FAA FORM 8110-3 NR 04589, SEMAN DWG EO 3788, DC8 SRM 51-1-21, 51-3-0, 51-1-20D. CLEANED, TREATED AND PRIMED AREA + FILLER + DOUBLER INTERNAL PART IN ACCORDANCE WITH DC9 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 INSTALLED FILLER + DOUBLER WITH NEW FASTENERS IAW DWG SEMON EO 3788, DC8 SRM 51-1-20D AND DC8 SRM 51-3-0 DC8 SRM 51-1-21.

Part: VANE — DAMAGED (XOLDO) · airframe 94,312 hrs · 30,453 cycles

DURING A ROUTINE C-CHECK INSPECTION, FOUND LEADING WING EXTENDED LEADING EDGE OUTBOARD VANE FORWARD OUTER PLATING INTERIM REPAIR AROUND STATION XOLDO 67.000. MAJOR REPAIR ACCOMPLISHED. REMOVED INTERIM REPAIR, REMOVED DAMAGED AREA. PERFORMED NDT INSPECTION AND FABRICATED PLATING SEGMENT, REPAIR DOUBLER AND INTERNAL DOUBLER. CLEANED, TREATED AND PRIMED AREA. REPAIRED PARTS INTERNAL PARTS. INSTALLED REPAIRED PARTS WITH NEW FASTENERS IAW DWG SEMAN EO 3785, SRM 51-1-21, 51-1-20D, 51-3-0, DWG SEMON EO NR 3785, SRM 51-1-21A.

Part: FLOORBEAM — CORRODED (BS 560) · airframe 94,312 hrs · 30,453 cycles

DURING A ROUTINE C CHECK INSPECTION, FOUND FOWARD CARGO COMPARTMENT FLOORBEAM CORRODED AT STA 560.000 RBL 60. MAJOR REPAIR ACCOMPLISHED BLEND OUT OF DAMAGED AREA. FOUND OUT OF LIMITS IAW DC8 SRM 53.2.0 FIG 1F. FABRICATED REPAIR ANGLE IAW EC8 SRM 53-2-0 FIG 1G SHEET 1-2. CLEANED, TREATED AND PRIMED AREA, REPAIR ANGLE IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT TO FAYING SURFACES IAW DC8 SRM 51-1-11 PG 9. INSTALLED REPAIR ANGLE IAW DC8 SRM 53-2-0 FIG 16, DC8 SRM 51-1-20 D PG 9 SRM 51-.-0 PG 1.

Part: SKIN PANEL — CORRODED (WS 63.50-107.50) · airframe 94,312 hrs · 30,453 cycles

DURING A ROUTINE C CHECK INSPECTION, FOUND RT INNER WING EXTENDED LEADING EDGE SLANT PANEL UPPER CAP CORROSION DAMAGE BETWEEN STA XFS 63.500 AND XFS 107.500. MAJOR REPAIR ACCOMPLISHED BLEND OUT ON CORRODED AREA REMAINING OUT OF LIMITS IAW DC8 SRM 57-2-1 FIG 37 PGS 135 AND 136. FAB`D EXTERNAL DOUBLER IAW DC8 SRM 57-2-1 FIG 37 PGS 135 AND 136. CLEANED, TREATED, AND PRIMED AREA AND EXTERNAL DOUBLER INTERIOR IAW DC8 SRM 51-1-8 B. PRIMED AREA AND EXTERNAL DOUBLER INTERIOR IAW DC8 SRM 51-1-8B. APPLIED PRC SEALANT ON INDICATED AREA IAW DC8 SRM 51-1-12, INSTALLED EXTERNAL DOUBLER IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 9.

Part: HINGE — CRACKED (LT WING FLAP) · airframe 94,312 hrs · 30,453 cycles

DURING A ROUTINE C-CHECK INSPECTION FOUND LT OB FLAP HINGE CRACKED AT STATION XC 337.000. MAJOR REPAIR ACCOMPLISHED. REMOVED CRACKED SUPPORT FITTING IAW SRM 51-1-21. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. INSTALLED NEW SUPPORT FITTING IAW SRM 51-1-21 SRM 51-20D AND 51-3-0.

Part: UPLOCK — LACK OF LUBE (MLG) · airframe 93,775 hrs · 30,141 cycles

ON DEPATURE FROM KBDL TO KTOL GEAR UPLATCH CHECK FAILED. THE GEAR NOT LATCHED LIGHT CAME ON AND NOSE GEAR CAME OUT OF THE WHEEL WELL. CREW COMPLETED FLIGHT TO KTOL AND LANDED WITH OUT INCIDENT. MAINTENANCE JACKED AIRCRAFT, INSPECTED, CLEANED AND LUBED UPLATCH MECHANISM. NO DEFECTS WERE NOTED. SWUNG GEAR AND PERFORMED UPLATCH CHECK AND OPERATIONAL CHECK WAS GOOD PER ALL APPLICABLE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.

Part: DOWNLOCK SWITCH — FAILED (MLG) · airframe 91,928 hrs · 29,528 cycles

ON FINAL APPROACH FROM TOL TO MCI UPON GEAR EXTENSION, GREEN GEAR DOWN LIGHTS DID NOT ILLUMINATE. CREW PERFORMED ABNORMAL PROCEDURES, INDICATION REMAINED THE SAME. AFTER TOWER VISUALLY CONFIRMED GEAR DOWN CREW MADE UNEVENTFUL LANDING IN MCI. UPON INSPECTION MAINTENANCE FOUND THE DOWNLOCK POSITION SWITCH CONNECTOR DEFECTIVE. SWITCH WAS REPLACED AND SYSTEM OPERATIONALLY CHECKED NORMAL. ALL WORK PERFORMED PER APPLICABLE MANUALS

Part: PROXIMITY SENSOR — FALSE INDICATION (MLG DOOR) · airframe 91,695 hrs · 29,417 cycles

AFTER TAKEOFF FROM KLAX TO KTOL DOOR NOT LATCHED LIGHT REMAIN ILLUMINATED. GEAR WAS RECYCLED TWICE WITH NO CHANGE. UP LATCH CHECK WAS SATISFACTORY. INSPECTION IS ON GOING. ADDITIONAL INFORMATION WILL BE PROVIDED AS IT BECOMES AVAILABLE. AFTER INSPECTION OF AIRCRAFT MAINTENANCE REMOVED AND REPLACED RIGHT MAIN LANDING GEAR DOOR NOT LATCHED PROXIMITY SWITCH AND PROXIMITY SWITCH STRIKER. OPERATIONAL CHECK GOOD IN ACCORDANCE WITH DOUGLAS AIRCRAFT MAINTENANCE MANUAL.

Part: FITTING — CRACKED (FUSELAGE)

PAX CABIN AT STA Y781.500 CRACKED FITTING.

Part: FITTING — CRACKED (AFT PAX DOOR)

AFT ENTRANCE DOOR HAS A CRACKED FITTING.

Part: FITTING — CRACKED (FUSELAGE)

LOWER FUSELAGE STA Y640 CRACKED FITTING.

Part: STIFFENER — CRACKED (LT WING)

LEFT WING TRAILING EDGE AREA AT XRS407.000 CRACKED STIFFENER.

Part: FITTING — CRACKED (FUSELAGE)

LOWER FUSELAGE AT STA Y798 CRACKED FITTING.

Part: CONNECTOR — LOOSE (#4EGT HARN) · airframe 91,314 hrs · 29,257 cycles

ON CLIMB OUT #4 EGT GAUGE FAILED (ANALOG & DIGITAL) ALL ENG INDICTORS NORMAL. AFTER 40 MIN #4 EGT GUAGE STARTED WORKING AGAIN. *** CORRECTIVE ACTION *** FOUND EGT HARNESS CONNECTOR NOT PROPERLY SECURED ON #4 EGT INDICATOR. SECURED CONNECTOR ON #4 EGT INDIC ATOR. INSPECTED EGT PIGTAIL HARNESS ON #4 ENGINE. PERFORMED EGT INDICATOR TEST IAW DC-8MM 77-20-15 &#4 AND #5 EGT INDICATION GOOD.

Part: HOSE · airframe 91,249 hrs · 29,216 cycles

ON LANDING ROLL LOST HYD PRESS AND QTY *** CORRECTIVE ACTION *** FOUND HOSE ON R/H BOGIE TRIM CYL HAD SEPARATED FROM FITTING- R AND R HOSE IAW 20-12-0 LK CK GOOD

Part: SKIN — DENTED (C-PIT DOOR FRAME) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND DENTED DAMAGE TO C-PIT CROSS SLIDE DOOR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 52-1-0, 51-1-21.

Part: SKIN — CORRODED (XFS341-XFS354) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LH WING CENTER LE UPPER SKIN AT STA XFS341 TO XFS354, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-1 FIG38, 51-1-20D. (CORROSION DAMAGE RECORED IN EWA CORROSION PROGRAM).

Part: STRUCTURE — CRACKED (LT MLG DOOR) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CRACKED DAMAGE TO DOOR AT LT OB SLOT UPPER CENTER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 27-80-01.

Part: SKIN — DELAMINATED (LH UPPER TE PANE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LH WING LWR TE PANEL IB OF FLAP HINGE 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 MM 20-15-01, 20-30-01.

Part: SPAR CAP — CORRODED (XFS32.5-XFS1117) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RH AUX TANK UPPER SPAR CAP AT XFS32.5 AND XFS1117, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1 FIG37, DHSK602-004. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: STRUT — BROKEN (LT MLG) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND BROKEN DAMAGE TO LT MLG STRUT ASSY GEAR AT LT WW, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 32-11-1.

Part: FITTING — CRACKED (STA340 L35L-L36L) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO BATHTUB FITTING AT STA 340 AND L35L TO L36L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0, 53-2-0 FIG2D.

Part: PANEL — DELAMINATED (LH WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO PANEL AT LH WING LWR PANEL FWD OF MLG, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-3-1, 51-1-9A.

Part: SEAT TRACK — CORRODED (STA1577-1600) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA 1577-1600 AND RBL45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG8A, 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CRACKED (STA1230 L33R) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FITTING AT L33R AND STA 1230, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, DWG#4758514.

Part: FITTING — CRACKED (N/WW AFT BLKD) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO N/W/W AFT LWR BLKD FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-3-0, DWG#4640111.

Part: TAB — DEBONDED (LT ELEVATOR) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND DEBONDED DAMAGE TO LH ELEVATOR IB CORNER OF GEARED TAB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-9A, DC-8 MM 27-30-3.

Part: PANEL — DELAMINATED (LT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO LH WING LWR TE PANEL AT FLAP HINGE 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0, 51-1-9A.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR BEAM LOWER FLANGE AT STA 902 AND LBL48-53, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK602-708. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (STA960 LBL60) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA. 960 AND LBL60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0FIG8, 51-1-20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (A-PIT#4LATCH) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT A-PIT DOOR FRAME LWR #4 LATCH, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG2D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (STA1160L35L-L34R) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA 1160 AND L35L TO L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-1-20D, DWG#3755843. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — GOUGED (XFS 257-500) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO RT WING UPPER LE AT STA XFS257-500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-20, DHSK602-706-1.

Part: FITTING — CORRODED (STA960 LBL60) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 940 AND LBL60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0, DWG#63646956. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FRAME — DAMAGED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND BLEND OUT DAMAGE TO FRAME AT STA 1280 AND L34L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 FIG2, 51-1-20D.

Part: FITTING — CRACKED (STA XW98) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RH WING INTERCOSTAL FITTING AT STA XW98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 57-1-0, 51-1-20D, 51-1-21, 51-3-0.

Part: WEB — CRACKED (STA70 LBL28) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO BULKHEAD AT STA 70 AND RBL28, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG23.

Part: SEAT TRACK — CORRODED (STA1400 LBL48) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CABIN SEAT TRACK AT STA 1400 AND LBL48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-3 FIG8A.

Part: SEAT TRACK — WORN (STA610-1000LBL24) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 610-1000 AND RBL24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-21-03, 53-2-3 FIG8A.

Part: SKIN — CRACKED (STA X552) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LH WING LE SKIN AT STA X5520, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-1-0, 51-1-21, 51-1-20D.

Part: SKIN — CRACKED (XFS 422-75) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LH LWR WING SKIN AT STA XFS422-75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D, DHSK602-828.

Part: AILERON — BENT (RH OB AILERON) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND BENT DAMAGE TO R/H OUTBOARD AILERON OUTBOARD TRAILING EDGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21A, 51-1-9A, 51-1-11, AND DWG#5763133.

Part: FRAME — CORRODED (STA1120 L36) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FRAME AT SAT 1120 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK 602-260. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: PANEL — CORRODED (STA ZR45-ZR74) · airframe 9,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO R/H VERT STAB SKIN AT STA ZR45 TO ZR74, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0, 51-1-21, 51-1-20D, AND DWG#5773845-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: INTERCOSTAL — CRACKED (STA1300 RBL33) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CRACK DAMGE TO C-PIT FLOOR SUPPORT STRAP AT STA. 1300 AND RBL33, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0, 51-1-21.

Part: SKIN — CORRODED (XOL D16-225) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LH WING LE LWR SKIN AT STA. XOL D16-225, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: ANGLE — CRACKED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO SUPPORT ANGLE AT STA 860 AND LBL55, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D, 53-1-0 AND DWG 5645332.

Part: SEAT TRACK — WORN (STA 150-250) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VIST FOUND WORN DAMAGE TO SEAT TRACK AT STA 150 - 250 AND LBL24 TO LBL30, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-3 FIG.14.

Part: ANGLE — GOUGED (LH WING OB SLOT) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO I/B ATTACH ANGLE AT O/B SLOT VANE L/H WING L/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DWG#5769891.

Part: RETAINER — CORRODED (STA XW743.750) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LH WING TE STATIC WICK BASE AT STA XW743.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SB 23-43. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: PANEL — DEBONDED (XA550 - XA585) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND DEBONDED DAMAGE TO L/H WING UPPER PANEL AT XA550 TO XA585, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-3-0, 51-1-21.

Part: LONGERON — CRACKED (STA605 L35R) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LONGERON AT STA 605 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-2-0 FIG.10.

Part: LONGERON — CORRODED (STA605 L35L) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA 605 AND L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-2 FIG.10, 51-1-20D, DHSK 602-647. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: WEB — CORRODED (RT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RH WING LOWER FALSE SPAR AFT OF MLG TRUNION AT STA XW75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D, DWG 9887427.

Part: FITTING — CRACKED (STA1200 L27L) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO BANNANA FITTING AT STA 1200 AND L27L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D, 51-3-0.

Part: FITTING — CORRODED (STA1180L32L-L33L) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA 1180 AND L32L TO L33L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, DWG#3755842, AND DHSK 602-336. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CRACKED (STA1140 L35R) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO FITTING AT STA 1140 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-1-20D AND DWG#3758496.

Part: LONGERON — CRACKED (STA1766 L17R) · airframe 91,115 hrs · 291,312 cycles

DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LONGERON AT STA 1766 AFT OF BULKHEAD AND HOLE#60 AND L17R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 53-1-0, 51-1-20D.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA 1580-1600 AND LBL45, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-8 AND DHSK 602-497.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO MAIN CABIN FLOOR BEAM AT STA 1640 AND LBL48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 FIG.1B AND DHSK 602-751.

Part: INTERCOSTAL — CORRODED (STA1460 L34R) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LOWER CORD ON INTERCOSTAL AT STA 1460 AND L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (DOOR FRAME) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO C-PIT DOOR FRAME LWR NR 3 LATCH, BACKUP FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0, AND DWG#3754930.

Part: FITTING — CORRODED (STA1160L32L-L35L) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA 1160 AND L32L TO L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0, AND DWG#3755842. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FINGER DOUBLER — CORRODED (STA610 L32L-L33R) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FINGER DOUBLER AT STA 610 AND L32LTO L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND 53-1-0 AND DWG#5779913. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (L27R STA 70-80) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 27R END FITTING AT STA 70 TO 80, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-1-21 AND DWG 46110671. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: LONGERON — CORRODED (STA35-55 L27R) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA 35-55 AND L27R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW 53-3-3 FIG.2 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: LONGERON · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA 8-70 AND L27R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-1-20D, 51-1-21 AND DWG#5613861. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: WEB — CORRODED (L/H MLG WW) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO TOP WEB AFT OF FLAP BOSS CABLE PULLEY AT L/H MLG WW, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DHSK 602-583. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: CAP — DEBONDED (LTELEVATOR) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND DEBONDING DAMAGE TO REPAIR AT LT ELEVATOR O/B END T/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 AND 51-1-21A AND 51-1-11 AND DC-8 MM 23-60-0.

Part: SKIN — DENTED (RT WING SPOILER) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A DENT TO THE RT WING NR 4 SPOILER UPPER SURFACE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART, TREATED AND PRIMED, INSTALLED PART IAW DC-8 SRM 51-21-00, 57-2-3.

Part: FRAME — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE UPPER FLANGE AT FS 1140 BETWEEN L34L TO L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 1F, 53-2-0 AND DSK 602-652.

Part: PANEL — CHAFED (RT MLG) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A GOUGE TO THE WING PANEL ABOVE RT MLG INBD END, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 51-3-0, MM 20-16-02 AND DH SR#4446.

Part: FRAME — CORRODED (FS1440 L34R) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LOWER FRAME AT FS 1440 AND L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-0, FIG 1B. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FRAME — CRACKED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE STUB FRAME AFT SIDE OF TORQUE BOX AT D-PIT DOOR AT FS 1446 AND L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 1B.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND/UNDER ROLLER TRACKS RECEPTACLE MAIN CABIN FLOORBOARD AT FS 122 RBL 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3, FIG 10 AND 51-1-20.

Part: PANEL — CRACKED (L/H WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H WING LOWER T/E PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-9A.

Part: SKIN — MISDRILLED (RT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND 2 HOLES IN THE R/H WING T/E WEDGE AT STA XW 761, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20, 57-2-0, FIG 2A AND DWG 5644654.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN AT STA 190 AND L36 TO L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D, 53-1-0 AND DWG 5779925.

Part: SKIN — CORRODED (STA 1050-1350) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT BELLY SKIN AT STA 1050 TO 1350 L31R TO L31L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-1-21 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CRACKED (AFT LWR CARGO) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FLOOR PANEL SUPPORT FITTING AT STA 1220 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////OPEN/////

Part: SKIN — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION AND A CRACK TO THE SKIN AT FS 1440 L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 21 AND DH SK 602-601.

Part: CHANNEL — CORRODED (L34R FS1400-1420) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER STRAP ON LONGERON 34R AT STA 1400 TO 1420, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DAC DWG 5616674. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — CORRODED (RH WING UPR SKIN) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE RH WING UPPER SKIN 10" FWD OF REAR SPAR & UNDER EXISTING DOUBLER AT STA XRS -6, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1, FIG 20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1180 BETWEEN L35L & L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-1-01, 51-1-20D AND DWG 3755843.

Part: EXHAUST GATE — WORN (LT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A WORN EXHAUST GATE LT FLAP L/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAAW DC-8 SRM 51-1-21A, 51-1-21 AND DWG 56414111.

Part: SKIN — CRACKED (L/H O/B SLOT) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H O/B SLOT VANE UPPER I/B SECTION, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-8 AND 57-2-0, FIG 2A.

Part: SEAT TRACK — DAMAGED (STA 500 RBL 48) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND ELONGATED SCALLOPS ON THE MAIN CABIN SEAT TRACK AT STA 500 AND RBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3, FIG 8A AND 53-7-2 FIG 2A.

Part: FRAME — PUNCTURED (CABIN) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A LARGE PUNCTURE IN THE RADIUS OF THE MAIN CABIN FRAME 280 AT LONGERON 20L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DH SK 602-459.

Part: STIFFENER — CRACKED (R/T WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING T/E VERT. STIFFENER AT STA XW 75.31, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.

Part: STRUCTURE — CORRODED (LT WING W/W) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT WING W/W TOP OF W/W O/B ABOVE AFT OF FLAP BUSS CABLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D AND DH SK 602-583.

Part: FITTING — CRACKED (AFT LWR CARGO) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK BETWEEN LONBERON 28L AND 29L AT STA 1160, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 2D.

Part: FITTING — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1160 TO 1220 AND L34R TO L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND 53-2-0, FIG 26.

Part: AILERON — DAMAGED (LH I/B AIL O/B) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND BUCKLED SKIN L/H INBD AILERON UPPER LWR SKINS JUST FWD OF TAB O/B L/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND 57-2-0, FIG 1B.

Part: SKIN — CRACKED (R/H WING L/E) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H WING O/B L/E UPPER SKIN AT XFS 703.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1, FIG 38.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO SHEAR TIE AT STA 1420 AND L34R AND L36R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-3-0.

Part: PANEL — CORRODED (RT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT WING LOWER T/E PANEL O/B OF FLAP HINGE 410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. NO DELAMINATION NOTED, NO ACTION REQUIRED.

Part: STRUCTURE — CORRODED (LT WING WW) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE LT WING W/W ABOVE TRUNION FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DH SK 602-583.

Part: CAP — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER SKIN OF C-PIT ON BEAVER TAIL (KEEL CAP) AT STA 1080 L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND DH SK602-633.

Part: SKIN — CORRODED (LH WING #4 SPOIL) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE L/H WING #1 SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-9H AND 57-7-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: RETAINER — CRACKED (C-PIT DOOR LWR) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE C-PIT DOOR LOWER RETAINER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DH SK602-787.

Part: SKIN — CORRODED (LT WING O/B L/E) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LEFT WING O/B L/E SKIN BETWEEN STA'S XFS 578.75 TO 641.25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DH SK 602-379. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: DOUBLER — CRACKED (LT WING L/E) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TEE DOUBLER LOWER LT WING AT STA XW 467, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DH SK 602-746 AND 8110-3.

Part: PANEL — CORRODED (R/H WING UPR T/E) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE R/H WING UPPER T/E PANEL AFT OF REAR SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-9 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SEAT TRACK — WORN (STA146-156 LBL48) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO SEAT TRACK AT STA 146-156 AND LBL48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG14.

Part: SUPPORT — CRACKED (STA 860 LBL 55) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT MLG W/W PRESSURE WEB SUPPORT ANGLE AT STA 860 LBL 55.0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D AND DWG 5645332.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING CENTER L/E VERT. ATTACH ANGLE AT LOWER END AT STA XS 520, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAAW DC-8 SRM 51-1-20D AND DWG 9753297.

Part: TRACK — CRACKED (DOOR #12) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A/C DOOR #12 FWD TRACK MISSING A PIECE OF METAL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-1-21 AND DWG 5613836.

Part: CLIP — CRACKED (LT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H WING CENTER L/E O/B END ATTACH CLIP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0 AND DWG 5769928.

Part: FLOOR PANEL — CORRODED (FS 580-1000) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MAIN CARGO FLOOR PANEL FROM STA 580 TO 867 LBL 24 TO LBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DWG 589041. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: LONGERON — CORRODED (L31L FS 1255) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LOWER FLANGE OF LONGERON AT FS 1255 L31L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-2-21 AND 51-1-8. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FRAME — CRACKED (R/H NOSE STA 58) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FRAME ON THE R/H NOSE TUNNEL AT STA 58, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 23 AND 51-1-21.

Part: FITTING — CORRODED (FS 1160 & 1180) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1160 & 1180 AND L30L TO L31L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 2D AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FINGER DOUBLER — CORRODED (L31R STA 70-80) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER AT STA 70 TO 80 AND L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-21, 51-1-20D AND DWG 5779916. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND BROKEN LUGS ON THE SEAT TRACK AT STA 1590 AND 1640 LBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-3-0 AND 53-2-3, FIG 8A.

Part: FRAME — CRACKED (STA 67 RH TUNNEL) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FRAME ON THE R/H NOSE TUNNEL AT STA 67, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 23 AND 51-1-8.

Part: SKIN — CRACKED (STA XFS 430) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE STRAP ON THE L/H WING LOWER SKIN SIDE JUST INBD OF #1 PYLON AT STA XFS 430, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND 57-2-1, FIG A.

Part: SKIN — CORRODED (B-PIT LWR FUSELA) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER THE FUSELAGE SKIN B-PIT SCUFF PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 20 AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: DOUBLER — CRACKED (L/H L/E XFS 304) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERNAL DOUBLER LOWER SKIN L/H WING L/E AT STA XFS 304, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-21, 51-1-20D AND DWG 5641252.

Part: ANGLE — CRACKED (L/H CTR L/E) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H CENTER L/E SLOT ANGLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-21 .

Part: FITTING — CORRODED (L33L, STA 8) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FITTING AT LONGERON 33L AT STA 8, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FRAME — CRACKED (L10R-L11R FS 190) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND DAMAGE TO THE FRAME ON THE R/H FWD SERVICE DOOR JAMB AFT AT STA 190 BETWEEN L10R-L11R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-0, FIG 2 AND 51-1-21.

Part: FITTING — CORRODED (A-PIT DOOR FRAME) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE A-PIT DOOR FRAME LWR #5 LATCH FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: RIB — CHAFED (LT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A HOLD CHAFFED THROUGH THE RIB ON THE LT L/E AT STA 5510, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.

Part: FITTING — CRACKED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BATHTUB FITTING ON FWD SIDE OF STA 340 BETWEEN L34R-35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0, FIG 2D AND 51-1-20D.

Part: SKIN — CRACKED (XRS 421 L/H WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A 1/2" CRACK ON THE LEFT WING UPPER SKIN AT STA XRS 721 AND STRINGER 3, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 57-2-1, FIG 10 AND 51-1-11.

Part: DOUBLER — CRACKED (AFT LWR MCD) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND 4 CRACKS AT AFT LWR CORNER OF MCD APPROX 3/8" LONG, DAMAGE EXCEEDED LIMITATIONS IAW DC-8S RM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8S RM 51-1-20D, 51-1-21A AND DWG SR08530027.

Part: SKIN — CRACKED (LH WING XRS74) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LH WING UPPER SKIN AT STA XRS74 AND STR #10, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-78 SRM 57-2-1 FIQ10.

Part: INTERCOSTAL — CRACKED (STA 1870 @ 3'OCL) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO INTERCOSTAL #62 HOLE AT 3 O'CLOCK AT STA 1870, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-11 AND DWG 4550170.

Part: FRAME — BENT (FS 1580 L21R) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A BENT FRAME AT FS 1580 L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-8, 53-2-0 AND DWG 5753352.

Part: PANEL — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LT BELLY STRESS PANEL AT STA 687 L33L-L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PANEL AND INSTALLED IAW DC-8 SRM 51-3-0 AND DWG 5750365.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 35R AT STA 120-140, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 53-2-2, FIG 10 AND DWG 3754045.

Part: PANEL — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE EXTERIOR OF R/H BELLY STRESSED PANEL NEAR STA 687 L33R-L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PANEL AND INSTALLED IAW DWG 4750365-9.

Part: DOUBLER — CRACKED (STA 70 RBL 30) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BULKHEAD HORIZ. INTERCOSTAL AT STA 70 RBL 30 ABOVE L30R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND 51-1-20D.

Part: SKIN — GOUGED (RT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND 3 DEEP GOUGES AT RT WING UPPER L/E AT STA XFS 257.500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED DOUBLER AND INSTALLED IAW DHK 602-706-1.

Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND/UNDER ROLLER TRACK RECEPTACLE MAIN CABIN FLOOR BOARD AT STA 122 RBL 36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-3, FIG 10.

Part: SEAT TRACK — CORRODED (FS420-590 RBL60) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SEAT TRACK IN THE MAIN CABIN AT STA 420-585 RBL 60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG 14.

Part: SUPPORT BRACKET — CORRODED (CARGO DOOR) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MCD BRACKET FWD NR 1 LATCH SPOOL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 51-3-0.

Part: SEAT TRACK — WORN (STA 146) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK IN THE MAIN CABIN AT STA 130-510 AT RBL 24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3 FIG 14 AND DWG 5750864.

Part: SKIN — GOUGED (L/H I/B FLAP) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A GOUGE AT FLAP HINGE 98 L/H I/B FLAP UPPER SKIN, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1, FIG 2Q.

Part: SKIN — GOUGED (L/H O/B FLAP) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A GOUGE TO THE L/H O/B FLAP UPPER SKIN O/B OF FLAP HINGE 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1, FIG 2Q.

Part: SUPPORT BRACKET — CORRODED (CARGO DOOR) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MCD SUPPORT BRACKET FWD NR 7 LATCH SPOOL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-0.

Part: SKIN — DAMAGED (LT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH SKIN AT STA XFS 710 ON LT WING OB LE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1 FIG2H.

Part: SEAT TRACK — WORN (FS590-980 LBL48) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND THE SEAT TRACK WORN BEYOND LIMITS AT STA 590 TO 980 LBL 48, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-3, FIG 8A AND 53-7-1, FIG 4.

Part: FITTING — CRACKED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TORQUE BOX BANANA FITTING AT STA 1150 L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D AND 53-1-0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SPLICE FITTING AT LONGERON 35R AT STA 1050, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-3-0, 53-1-0 AND DWG 370545.

Part: FITTING — MISDRILLED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A DRILLED END FITTING AT RADIUS AT STA 1687 L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D AND DWG 4773155.

Part: FITTING — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1160 L29L TO L30L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0 AND DWG 3755842.

Part: FITTING — TOOL DAMAGE (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A DRILL START TO THE BATHTUB FITTING AT STA 1228 AND L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0 AND DWG 3755845.

Part: FITTING — CRACKED (FS 1220 L33L-34L) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A LARGE GAP BETWEEN O/B END FITTING AND BATHTUB FITTING AT FS 1220 AND L33L TO L34L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0 AND DWG 3755845.

Part: DOUBLER — CORRODED (LT WING AUX TANK) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LH AUX TANK UPPER SPAR CAP BETWEEN STA XFS 1.25 TO XFS 113.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DH SK 602-748.

Part: RIB — CRACKED (L/H CTR L/E) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H CENTER L/E AT STA XFS 291-500 AND 304.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2, 51-1-21 AND 51-1-20D.

Part: LONGERON — CORRODED (STA1168-1270) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT L33L AND STA 1168-1270, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-2-2 FIG10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BATHTUB FITTING AT STA 1220 BETWEEN L34R TO L35R AND L35R TO L36R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-1-1, 51-1-20D AND DWG 3755845.

Part: RIB — CRACKED (LEFT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB LEFT WING L/E AT STA XFS 616.25 AND 622.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB ON THE LEFT WING L/E AT STA XFS 578375, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB TIP ON THE LT CENTER L/E AT STA XFS 341.500, 354.800 & 360.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.

Part: FITTING — CORRODED (FUSELAEGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE C-PIT DOOR FRAME NR 2 LATCH BACKUP FITTING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0 AND DWG 3754930-1N.

Part: FITTING — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE C-PIT DOOR FRAME NR 5 LATCH BACKUP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 53-1-0 AND DWG 3754930-1N.

Part: RIB — CRACKED (LT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB TIP LT WING L/E AT STA XFS 385-250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.

Part: RIB — CRACKED (XFS 422.750) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB TIP ON THE L/H L/E WING CENTER AT STA XFS 422.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAAW DC-8 SRM 57-2-0, FIG AND 51-1-20D.

Part: SKIN — CRACKED (LT WING L/E) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FWD DRAIN HOLE ON THE LT WING O/B L/E LWR SKIN AT STA XFS 597.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-21D AND SH SK 602-627.

Part: RIB — CRACKED (LT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LEFT WING L/E UPPER RIB AT STA X5497-401, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.

Part: RIB — CRACKED (LEFT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB ON THE LEFT WING L/E AT STA XFS 641.25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.

Part: RIB — CRACKED (LT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIB ON THE LEFT WING L/E AT STA XF 5660, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.

Part: DOUBLER — CRACKED (FS1350 L32R) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FINGER DOUBLER AT FS 1350 L32R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-21 AND DWG 5779915.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 36 AT STA 140-160, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-4-1, FIG 28 AND DWG 5758874.

Part: FITTING — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE C-PIT DOOR FRAME LOWER NR 4 LATCH BACKUP FITTING , DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-1-20D AND DWG 3754930-1N.

Part: RIB — CRACKED (RT WING) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RIGHT WING L/E RIB (UPPER) AT STA XFS 816.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND DAMAGE TO THE LEFT I/B FLAP T/E OTBD END, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DWG 3652279.

Part: FITTING — CRACKED (STA 300 L34R-35R) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BATHTUB FITTING AT STA 300 BETWEEN L34R TO L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. RECEIVED PART AND INSTALLED IAAW DC-8 SRM 53-2-0, FIG 2B.

Part: LONGERON — CORRODED (STA 1050-1270) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA1050-1270 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, DWG#9758508. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (STA1150 L36) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON FITTIND AT STA 1150 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (STA 1180 L36L) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 1180 AND L36L-L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-1-0, 51-1-20D, DWG#3755845. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (STA1230 L36) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FITTING AT STA 1230 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SEAT TRACK AT STA 590 AND RBL 60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-3FIG8A, 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: ANGLE — CORRODED (STA1766-1780) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RH VERT STAB SKATE ANGLE AT STA 1766-1780 AND L2R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-5, 51-1-26. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (STA 1160-1220) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ALL 6 T-BOLT FITTINGS AT STA 1160-1220 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D, 51-1-11. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (Y=1210,X=24) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO C-PIT DOOR LWR #6 LATCH BACK UP FITTING AT STA Y=1210, X=24R, Z=-30, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (STA300 L33R-L34R) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATHTUB FITTING AT STA 300 AND L33R-L34R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (Y=350 X=24R) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT DOOR FITTING AT STA Y=350, X=24R, Z=-30, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 53-2-0FIG2D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ANTENNA PAD AT STA 87-93 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-11, 51-3-0.

Part: LATCH — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO A-PIT DOOR FRAME LWR NR 1 LATCH AT STA Y=285, X=24R, Z=-30, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D,

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ANTENNA MOUNT PLATE AND SKIN AT STA 367-373, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-3-01.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FINGER DOUBLER AT STA 180-200 AND L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 1F, 51-1-21, 51-1-20D.

Part: DOUBLER — CORRODED (STA 70-80 L31R) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SKIN DOUBLER AT STA 70-80 AND L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DWG#5649028. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM)

Part: DOUBLER — CORRODED (STA180-190 L31R) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BULGING SKIN AT STA 180-190 AND L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D AND DWG#5779916. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SPAR CAP — CORRODED (XFS32.5-XFS142) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RH AUX TANK UPPER SPAR CAP AT STA XFS32.5-XFS142, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-25, DC-8 MM 57-20-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — CORRODED (XOLDI6.225) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LH WING CENTER LE UPPER SKIN AT STA XOLDI 6.225 TO XFS422.75, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1 FIG38, 51-1-21, 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RT WW DOOR FRAME AT STA 883, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 53-2-0 FIG2B, DWG 5616306, DC-8 SRM 53-1-01, 51-1-21.

Part: LONGERON — CORRODED (STA35-55 L26R) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON AT STA 35-55 AND L26R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: TAB — VIBRATION (ELEVATOR) · airframe 90,966 hrs · 29,067 cycles

ELEVATOR CONTROL HAS VIBRATION WHICH INCREASES WITH AIRSPEED ABOVE 250 KTS ANY DOWNWARD PRESSURE ON THE YOKE WILL CAUSE THE YOKE TO KICK BACK (AUTOPILOT OFF) (PTC ON/OFF MADE NO DIFFERENCE). REMOVED AND REPLACED ELEV LOUD FEEL CENTERING MECHANISM IAW DC-8 M/M 27-30-4, OPS CK GOOD ON GROUND. REMOVED AND REPLACED LT ELEVATOR CONTROL TAB IAW DC-8 M/M 27-30-2.

Part: LINE — BROKEN (HYD SYSTEM) · airframe 90,530 hrs · 28,854 cycles

UPON GEAR RETRACTION AFTER T/O GEAR RETRACTED NORMALLY WHEN GEAR HANDLE PLACED IN UPLATCH CHECK POSITION NOSE GEAR SOUNDED LIKE IT FELL OUT OF THE WHEEL WELL AND BOTH RED LIGHTS FOR DOORS NOT LATCHED AND GEAR NOT LATCHED ILLUMINATED. CREW THOUGHT THEY HAD MISSED THE UPLATCH DETENT BY GOING TOO FAR TOWARD DOWN GEAR WAS FULLY LOWERED AND GOT 3 GREEN LIGHTS. WHEN GEAR RETRACTED 2ND TIME RED LIGHTS ILLUMINATED AGAIN AND HYDRAULIC QTY AND PRESS RAPIDLY DECREASED TO STAND PIPE INDICATION. REPLACED BROKEN RUDDER PUMP SUPPLY LINE, PERFORMED GEAR SWING AND UPLATCH CK. OPS CK GOOD IAW DC-8 M/M 32-30-0, NO OTHER DEFECTS NOTED.

Part: STRUT — CRACKED (NLG) · airframe 90,527 hrs · 28,852 cycles

NOSE GEAR STRUT HAS 1 INCH CRACK ON THE OUTER CYLINDER, AT TOP AFT. REMOVED AND REPLACED NOSE LANDING GEAR STRUT IAW DC8 M/M 32-21-1. RIGGED NOSE GEAR GROUND SHIFT MECHANISM IAW DC8 M/M 32-23-1, RIGGED NOSE STEERING IAW DC8 M/M 32-51-0. PERFORMED GEAR SWING IAW DC8 M/M 32-30-0. LEAK AND OPS CHECKED GOOD IAW DC8 M/M 32-21-1, 32-23-1, 32-50-0 AND 32-30-0.

Part: ACTUATOR — CRACKED (TE FLAP CRANK) · airframe 89,880 hrs · 28,582 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING FLAP ACTUATOR CRANK (KNUCKLE) AT STA 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW MM 27-51-9.

Part: SKIN — DENTED (RT TE FLAP) · airframe 89,880 hrs · 28,582 cycles

DURING A MAINTENANCE VISIT FOUND 3 DENTS ON THE RIGHT I/B FLAP UPPER SURFACE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1 AND 51-1-21.

Part: LINK — GOUGED (LT WING) · airframe 89,880 hrs · 28,582 cycles

DURING A MAINTENANCE VISIT FOUND A GOUGE TO THE LEFT O/B FLAP AFT LINK AT STA 410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-186 WITH APPROVED 8110-3 DATED 7-5-00.

Part: BRACE — CORRODED (LT WING TE FLAP) · airframe 89,880 hrs · 28,582 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LEFT WING FLAP CANOE SIDE BRACE AT STA 98 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-186 WITH APPROVED 8110-3 DATED 7-5-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (LT TE FLAP) · airframe 89,880 hrs · 28,582 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE, PITTING AND SMALL AREAS OF GOUGING ON THE LT FLAP LWR MOUNT AT STA 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-186 WITH APPROVED 8110-3 DATED 7-3-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (LT TE FLAP) · airframe 89,880 hrs · 28,582 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE, PITTING AND SMALL AREAS OF GOUGING ON THE LT FLAP LWR MOUNT AT STA 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-186 WITH APPROVED 8110-3 DATED 7-3-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — GOUGED (LT TE FLAP) · airframe 89,880 hrs · 28,582 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE, PITTING AND SMALL AREAS OF GOUGING TO THE LT FLAP LWR MOUNT AT STA 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-186 WITH APPROVED 8110-3 DATED 7-3-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (RT WING TE FLAP) · airframe 89,880 hrs · 28,582 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE, PITTING AND SMALL AREAS OF GOUGING TO THE RT WING FLAP LWR MOUNT AT STA 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-186 WITH APPROVED 8110-3 DATED 7-3-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (RT WING TE FLAP) · airframe 87,880 hrs · 28,582 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE, PITTING AND SMALL AREA OF GOUGING ON THE RT WING FLAP LWR MOUNT AT STA 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-186 WITH APPROVED 8110-3 DATED 7-3-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (RT WING TE FLAP) · airframe 87,880 hrs · 28,582 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE, PITTING AND SMALL AREA OF GOUGING ON THE RT WING FLAP LWR MOUNT AT STA 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-186 WITH APPROVED 8110-3 DATED 7-3-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: LINK — GOUGED (LT TE FLAP) · airframe 89,880 hrs · 28,582 cycles

DURING A MAINTENANCE VISIT FOUND A GOUGE TO THE LT WING O/B FLAP FWD LINK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-186 WITH APPROVED 8110-3 DATED 7-3-00.

Part: FITTING — CORRODED (FUSELAGE) · airframe 91,115 hrs · 29,132 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FITTING AT FS 1230 AND L36, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-20D & 53-1-0.

Part: ANGLE — CORRODED (BS 857)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO ATTACHMENT ANGLE IN RIGHT MAIN LANDING GEAR TOP SECTION AT STA 857 AND BETWEEN WL-6 AND WL-8, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVE TIMCO DER ENGINEERING SKETCH REO-05655 REV A. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — CORRODED (BS 190 - 440)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO EXTERNAL SKIN PANEL BETWEEN STA 190 TO STA 440 AND BETWEEN LONGERONS 31 LEFT TO 31 RIGHT. REMOVED DAMAGED SKIN, TREATED AREA IAW DC-8 SRM 51-1-8.. RECEIVED NEW SKIN PANEL AND INSTALLED IAW 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: BEAM — CRACKED (FUSELAGE)

AT C-CHECK, CRACKS WERE FOUND IN THE J-BEAM WHICH IS ATTACHED TO THE AFT FACE OF THE AFT PRESSURE BULKHEAD. THE CRACKS ORIGINATE IN THE RADII ADJACENT TO ATTACH BOLTS APPROXIMATELY ONE INCH EACH SIDE OF THE AIRCRAFT CENTERLINE. SUBMITTER STATED THE CRACKS APPEAR TO OCCUR UNDER NORMAL OPERATING CONDITIONS AND ARE POSSIBLY CAUSED BY THE COMBINED FORCES OF CABIN PRESSURE AGAINST THE FRONT FACE OF THE BULKHEAD AND TENSION FROM THE 13 FLIGHT CONTROL CABLES WHICH ARE ROUTED THROUGH PULLEYS ATTACHED TO THE J-BEAM AND RECOMMENDED THE FOLLOWING: PERFORM PERIODIC INSPECTION OF ALL DC-8 AIRCRAFT WITH FLAT AFT PRESSURE BULKHEADS, AND, REPAIR CRACKS PER DC-8 SRM 53-2-5 FIG 26.

Part: BULKHEAD WEB — CORRODED (BS 12-32)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO BULKHEAD WEB AND FITTING BETWEEN STA -12 TO STA -32 AND LONGERON 23 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW WEB AND FITTING IAW SRO 8530026. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: PRESSURE PANEL — CORRODED (BS 950-970)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO PRESSURE PANEL BETWEEN STA 950 TO STA 970 AND LONGERON 21 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVE TIMCO DER ENGINEERING SKETCH REO-05655 REV A. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: LONGERON — CORRODED (BS 8-70)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 33 RIGHT BETWEEN STA 8 TO STA 70, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR SPLICE IAW DC-8 SRM 53-2-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (BS 280)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 280 AND LONGERON 29 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0 FIGURE 1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (BS 280)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 280 AND LONGERON 32 LEFT TO 35 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (BS 200-280)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING BETWEEN STA 200 TO STA 280 AND LONGERONS 28 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG 3755822. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (BS 280)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO 2 EACH FITTINGS AT STA 280 AND LONGERON 33 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTINGS IAW DC-8 SRM 53-2-0 FIGURE 1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FLOOR — CORRODED (BS 1664)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOOR PANEL AT STA 1664 AND BL 10 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-3 FIGURE 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FRAME — CORRODED (BS 1660)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME AT STA 1660 BETWEEN LONGERONS 29 LEFT TO 34 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 FIGURE 1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: INTERCOSTAL — CORRODED (BS 1720)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA1720 AND BL 12 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FRAME — CORRODED (BS 1150-1160)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME BETWEEN STA 1150 TO STA 1160 AND BETWEEN LONGERONS 24 LEFT TO 25 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FRAME — CORRODED (DOOR JAMB)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO DOOR JAMB FRAME WEB AT STA 238, BL 78 LEFT AND WL -3, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FRAME WEB IAW DAC DWG 5772786. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: LONGERON — CORRODED (BS 8)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 33 RIGHT AND FITTING AT STA 8, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0 FIGURE 1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (BS 645-669)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO ATTACHMENT ANGLE BETWEEN STA 645 TO STA 669 AND LONGERON 21 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-4-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (BS 822-)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 822 BETWEEN LONGERONS 21 RIGHT AND 22 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: ANGLE — CORRODED (BS 340)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO CROSS SLIDE CARGO DOOR, ATTACHMENT ANGLE AT STA 340 AND LONGERON 34 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DAC DWG 5711283. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (BS 440)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 440 AND LONGERON 21 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG 4597643 AND DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FLOOR — CORRODED (BS 1000)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOOR PANEL AT STA 1000 AND BL 27 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-7-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (BS 270)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 270 AND LONGERON 36, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 51-3-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SEAT TRACK — CORRODED (BS 180-185)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SEAT TRACK BETWEEN STA 180 TO STA 185 AND BL 65 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW SEAT TRACK IAW DC-8 SRM 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FLOORBEAM — CORRODED (BS 1000)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM AT STA 1000 AND BL 23 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (BS 1525-1530)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING BETWEEN STA 1525 TO STA 1530 AND LONGERON 31 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — CORRODED (BS 190-440)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO EXTERNAL SKIN PANEL BETWEEN STA 190 TO STA 440 AND BETWEEN LONGERONS 31 LEFT TO 31 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REMOVED AND INSTALLED NEW SKIN PANEL IAW DC-8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — CORRODED (BS 100-110)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO EXTERNAL SKIN PANEL BETWEEN STA 100 TO STA 110 AND BETWEEN LONGERONS 26 RIGHT TO 27 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SKIN PANEL IAW DAC DWG 5756065. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: HINGE — CORRODED (CARGO DOOR)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO MAIN CARGO DOOR FWD HINGE SEGMENT AT STA 130 AND LONGERON 6 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRO 8530027. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (BS 280)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 280 AND LONGERON 30 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DAC DWG 3755822. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (BS 280)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 280 AND LONGERON 34 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: LONGERON — CORRODED (BS 190-375)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 36 BETWEEN STA 190 TO STA 375, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED LONGERON IAW DC-8 SRM 51-3-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (BS 200)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 200 BETWEEN LONGERONS 34 RIGHT TO 35 RIGHT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (BS 270)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 270 BETWEEN LONGERONS 34 LEFT TO 35 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: LONGERON — CORRODED (BS 857-980)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 24 RIGHT BETWEEN STA 857 TO STA 980, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED NEW LONGERON 24 RIGHT IAW TIMCO WORKCARD 90453100. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: DOUBLER — CORRODED (BS 260-350)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FINGER DOUBLER BETWEEN STA 260 TO STA 350 AND LONGERON 31 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FINGER DOUBLER IAW DAC DWG 5758874. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: RETRACT MECH — LACK OF LUBE (NLG DOORS)

ON GEAR UPLATCH CHECK, GEAR FAILED CHECK IN COMPLIANCE WITH GEAR UPLATCH FAILURE CHECK LIST GEAR CONTINUED TO FAIL UPLATCH CHECK AND SOUNDED AS THOUGH NOSE GEAR DOORS WERE OPEN AND/OR NOSE GEAR EXTENDED WHILE IN THE GEAR UP POSITION. IN COMPLIANCE WITH THE QRH DOMESTIC RESTRICTIONS RETURN WAS MANDATORY. INTERNATIONAL DESTINATION WAS MMGL. LUBED GEAR UPLATCH MECHANISMS ON ALL GEAR. FLIGHT TEST REQUESTED BY MANAGER OF M/C FOR FURTHER EVALUATION PER MR/P CHAP 4 ITEM XX PG 164 AND 165.

Part: BALLAST — FAILED (COCKPIT)

SMOKE COMING FROM UNDER GLARESHIELD FLORS LIGHTS. FOUND GLARESHIELD BALLAST BURNT DEFERRED BALLAST PER MEL 33-1. F/O'S FLUORESCENT LIGHTS INOP. CAT C PLACARD INSTALLED.

Part: FIRE WIRE — BROKEN (NR 2 ENGINE)

SHUTDOWN NR 2 ENGINE AT 0947 DUE TO FIRE WARNING. DISCHARGED BOTH FIRE BOTTLES. CKED AND INSPECTED NR 2 ENGINE WARNING SYSTEM. FOUND BROKEN WIRE ON FIRE BELL CUTOUT RELAY. REPAIRED WIRE. ALL FIRE WARNING SYSTEMS 1, 2, 3, 4 CK GOOD. REMOVED AND REPLACED NR 1 AND 2 FIRE EXT BOTTLES AND SQUIBS, ALL IAW MM 26-1-1.

Part: FIRE LOOP — MALFUNCTIONED (NR 2 ENGINE)

INTERMITTENT FIRE WARNING ON NR 2 ENGINE. REMOVED AND REPLACED NR 2 ENGINE RT SIDE FAN COWL FIRE LOOP DETECTOR IAW DC-8 MM CHAPTER 26-10-1, OPERATIONAL CHECK GOOD.