N8084U

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON FWD SIDE OF FRAME AT STA 20 AT CUSP LINE RT SIDE OF CABIN, 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 53-2-0 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: NUT PLATE — MISSING (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A BROKEN NUT PLATE ON THE RIGHT O/B SLOT UPPER SIDE SCREW AT STA XS 515, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW EO NR 00-107 WITH APPROVED 8110-3 DATED 6-29-00.

Part: LINK — DAMAGED (TE FLAP) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND THAT THE FLAP LINK SUPPORT (CANOE FITTING) NEEDS TO BE REPLACED AT STA XW 219.498, 339.723 & 97.906 IAW DC-8 MM 27-51-12 RIGHT SIDE PER S/B 27-260, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PARTS AND INSTALLED IAW DC-8 S/B 27-208, 27-260 & DC-8 MM 27-51-12 & EO NR 00-107 WITH APPROVED 8110-3 DATED 5-17-00.

Part: RETAINER — MISINSTALLED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CANOE FITTING BOLT RETAINER INSTALLED ON WRONG SIDE OF FITTING AT STA 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00-107 WITH APPROVED 8110-3 DATED 6-15-00.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND NUMEROUS PATCHES TO THE FWD LWR CARGO COMPT MID BULKHEAD, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW EO NR 00-107 WITH APPROVED 8110-3 DATED 6-1-00.

Part: PRESSURE PANEL — CORRODED (WING BOX) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CENTER WING AFT LT TOP PANEL AT STA 848.00 AND LBL 60 TO 58 INCHES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRS IAW EO NR 00-107 WITH APPROVED 8110-3 DATED 6-5-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: DRAG LINK — BROKEN (RT MLG) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND THE ATTACHMENT LUG BROKEN OFF TOP OF RT MAIN LANDING GEAR DRAG 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 00-107 WITH APPROVED 8110-3 DATED 6-16-00.

Part: SKIN — DENTED (ELEVATOR) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A DENT TO THE RT. ELEVATOR L/E AT STA XE 120, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. ACCEPTABLE TO RETURN TO SERVICE IAW E.O. 00-107 WITH APPROVED 8110-3 DATED 6-19-00.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SUPPORT BRACKET AT STA FS 857 AND LBL 47 LT MAIN W/W, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 6-5-00.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE UPPER CARGO COMPT AT CUSP LINE AT STA 1240 LT XCW 64 INCHES, 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 53-2-5 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES AND SMALL CRACK TO THE RT WING CENTER LEADING EDGE O/B SLOT EDGE, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 6-14-00.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE BULKHEAD AFT SIDE ANGLE AT STA 70 AND L22R TO L25R, 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 00-107 WITH APPROVED 8110-3 DATD 6-2-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: PRESSURE PANEL — CORRODED (WING BOX) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LWR CENTER WING AREA/BOTTOM RT PLATE AND BOTTOM LT PLATE SCREWS AND BOLTS AT STA 700 - 781 AND L35L - L35R, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-23-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — LIGHTNING STRIKE (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND LIGHTENING STRIKE DAMAGE TO THE RT WING TIP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CIRCUMFERENTIAL FRAME AFT SIDE AT STA 1140 AND L36, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-30-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — CRACKED (LT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK 3 INCHES LONG ON THE LT WING CENTER LEADING EDGE T/E DOUBLER AT STA 339.5, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 6-12-00.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A DIMPLED WASHER ON THE RT HORZ STAB I/B LEADING EDGE SCREW AT STA XFS 178.7, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED PART IAW EO NR 00-107 WITH APPROVED 8110-3 DATED 6-9-00.

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER PANEL SPACERS ON THE LOWER CENTER WING AREA EXTERNAL AT STA 680 - 700 AND L33R, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 6-8-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — DAMAGED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND DAMAGE TO THE SURFACE 8 INCHES AFT OF L/E LWR ON THE RT WING L/E AT STA XW 336.5, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 6-12-00.

Part: SKIN — LOOSE (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND ABOUT 75 RIVETS LOOSE AND PULLING ON O/B REVERSER OUTSIDE SKIN, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 6-7-00.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER AND REINFORCEMENT BRACKET AT STA 8 TO -12-X59-Z-10 RT SIDE OF CUSP, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 6-8-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: PANEL — CRACKED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK AND ELONGATED HOLES TO THE CAN''T PRESS WEB PANEL AT STA 508 AND XCW 463, 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 57-2-0 AND EO NR 00-107 WITH APPROVED 8110-3 DATED 5-15-00.

Part: PLATE — GOUGED (CARGO DOOR) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A DENTED/GOUGED B PIT KICK PLATE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21, 53-2-0 AND 51-1-20D.

Part: FITTING — CRACKED (RT WING TE FLAP) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT UPPER T/E FLAP WELL FITTING AT STA XW-47, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 6-7-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND SHEARED EXTERIOR FASTENERS AT STA 305 AND L36, 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 00-107 WITH APPROVED 8110-3 DATED 5-3-00.

Part: FITTING — DAMAGED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A BROKEN TAB AND GOUGED FITTING ON THE 508 CAN''T WEB SUPPORT ATTACHMENT FITTING TO FRONT SPAR LOWER ATTACHMENT AT STA XCW 463, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 6-6-00.

Part: PANEL — CRACKED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK AND HOLES ELONGATED ON THE 508 CAN''T PRESSURE WEB PANEL AT STA XCW 463, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-15-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND I/B EDGE SKIN BROKEN OFF WHERE FLIGHT SPOILER RETRACTS DOWN ON THE LT UPPER TRAILING SURFACE O/B AT STA 340 AT XRS 367, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 6-9-00.

Part: DOUBLER — DAMAGED (SEAL AREA) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A PATCH REPAIR THAT IS TORN NEAR SEAL ON THE LT MLG DOOR, 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 51-1-21, 51-1-21A, 53-2-0 AND 51-3-0.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A HOLE IN THE UPPER FLANGE AT STA 1440 ABOVE L34L, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-24-00.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK ABOUT 2 INCHES LONG ON THE O/B REV TOP FAIRING, 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 00-107 WITH APPROVED 8110-3 DATED 6-7-00.

Part: VANE — DAMAGED (NR 2 TE FLAP) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND ENLARGED SCREW HOLES ON THE NR 2 RT FLAP VANE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 51-3-2 AND EO NR 00-107 WITH APPROVED 8110-3 DATED 6-7-00.

Part: PLATE — GOUGED (CARGO DOOR) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND SEVERAL DENTS/GOUGES AROUND D PIT DOOR EXTERNAL, DAMAGE EXCEEDED LIMITATIONS 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 AND 51-1-21.

Part: FITTING — CORRODED (LT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CANOE FITTING AT STA 410 LT WING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8 AND EO NR 00-107 WITH APPROVED 8110-3 DATED 6-6-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CANOE FITTING ON THE RT WING AT STA 410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8 AND EO NR 00-107 WITH APPROVED 8110-3 DATED 6-6-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — CRACKED (LT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SCREW HOLE 33 INCHES FROM LEADING FROM SPAR LWR, ON LT CENTER SECTION L/E AT STA 520, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 6-7-00.

Part: PANEL — BULGED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE T/E UPPER SURFACE AT STA XE 245, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 6-2-00.

Part: SKIN — CUT (NR 4 NACELLE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND SEVERAL CUTS IN NR 4 ENG O/B T/R INTER RING COWL, 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 00-107 WITH APPROVED 8110-3 DATED 6-1-00.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND LOOSE SCREWS ON THE LEFT O/B SLOT L/E AT STA 520 33 INCHES FROM FRONT SPAR, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 6-7-00.

Part: SKIN — DAMAGED (STUB WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND OVERSIZED ATTACH HOLES TO THE STUB WING OVER NR 3 ENG O/B UPPER SURFACE, 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 00-107 WITH APPROVED 8110-3 DATED 6-6-00.

Part: ANGLE — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACKED NR 11 RIB ON THE RT WING NR 3 STUB LWR LT RIB ANGLE AT STA XS 246, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-8-00.

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE TOP OF CIRCUMFERENTIAL FRAME AT STA 1400 AND L36, 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 53-2-0 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: RIB — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK THROUGH UNDER GUSSET ON THE NR 11 LOWER RIB ON THE RT WING L/E MIDDLE SECTION AT STA XFS 350, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-31-00.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD LWR CARGO BILGE AT STA 350 AND L35R LT SIDE, 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 53-2-0, 53-2-2 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: LONGERON — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND CRACK TO LONGERON 31R AT STA 8 TO -67, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PART IAW DC-8 SRM 51-1-0 AND 51-1-21.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE INSIDE LONGERON UNDER CIRCUMFERENTIAL FRAME AT STA 600 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.

Part: FRAME — BROKEN (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A BROKEN FRAME AND SEAT TRACK AT STA 240 3RD SEAT TRACK FROM LT SIDE OF CABIN, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-2-00.

Part: RIB — DAMAGED (PAX DOOR) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND DAMAGE TO THE LT SIDE L2 DOOR LWR RIB FWD NUT PLATE, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-24-00.

Part: BRACKET — CRACKED (LT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BRACKET AT BOTTOM ON THE L/E SECTION ABOVE NR 1 PYLON I/B AT STA 526, 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 57-2-0 AND 51-3-0.

Part: INTERCOSTAL — TORN (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A TORN SIDEWALL ATTACH FRAME IN CARGO PIT (INTERCOSTAL) AT FS 500 - 520 RT, 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 53-2-0, 51-1-4 AND 51-1-21.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A HOLE IN FLANGE AT STA 1400 AND L35R, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-24-00.

Part: SKIN — DAMAGED (L/E SLOT) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND TOO LONG OF SCREWS AND SCREWS PULLING THROUGH SKIN ON THE LEFT I/B SLOT L/E AT STA XS 250 46.5 INCHES FROM FRONT SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE. FABRICATED AND INSTALLED REPAIR IAW EO 00-107 WITH APPROVED 8110-3 DATED 5-18-00.

Part: SKIN — DAMAGED (LT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND TOO LONG OF SCREWS AND SCREWS PULLING THROUGH SKIN ON THE LEFT I/B SLOT L/E AT STA XS 250 46 .5 INCHES FROM FRONT SPAR, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-18-00.

Part: SKIN — CORRODED (COCKPIT) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER FINGER DOUBLER COCKPIT FLOOR FRAME AT STA -67 + X -17 -Z -11, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-24-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD SIDE OF FRAME AT STA 20 AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-20D AND 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: LONGERON — DAMAGED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND THAT THE PREVIOUS BLEND OUT NEEDS THICKNESS CHECKED AT STA 1690 TO 1700 AND L10L, 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 53-2-0 AND EO NR 00-107 WITH APPROVED 8110-3 DATED 5-24-00.

Part: ANGLE — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACKED RT SIDE ON THE RT WING NR 3 STUB WING NR 11 RIB LOWER ANGLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-21.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER AT STA 1514 BETWEEN L27L AND L28L, 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 00-107 WITH APPROVED 8110-3 DATED 5-23-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — DENTED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND 2 DENTS BEHIND JACK PAD AT STA 280 AND BETWEEN L36 - L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER FROM STA -57 TO -70, -X 59, -Z-10 RT SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. ORIGINAL MATERIAL REMAINING IS WITHIN ALLOWABLE LIMITS IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: RIB — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK ABOUT 9 INCHES LONG ON THE UPPER RIB ON THE L/E SECTION ABOVE NR 2 PYLON AT STA 250, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-8-00.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT AFT ENTRY DOOR/PLATE ABOUT 1.5 INCH AT LWR DOOR HINGE INSIDE LIGHTENING HOLE, 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 52-2-0.

Part: SKIN — CRACKED (LT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK LEADING FROM SCREW HOLE ON THE LEFT I/B LEADING EDGE AT STA XS 515, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-18-00.

Part: SKIN — BULGED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND BULGED AND SCRATCHED SKIN ON THE RT WING O/B LEADING EDGE EXTERIOR AT STA XFS 724, 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 00-107 WITH APPROVED 8110-3 DATED 5-16-00.

Part: SKIN — CRACKED (LT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK EXTENDING FROM SCREW HOLE ON THE LEFT L/E AT STA X OLDI 6.225, 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 57-2-0 AND 57-2-1.

Part: SKIN — DAMAGED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CREASED AND BILGED SKIN ON THE RT WING O/B LEADING EDGE EXTERIOR SKIN AT STA 714, 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 00-107 WITH APPROVED 8110-3 DATED 5-16-00.

Part: DOUBLER — LOOSE (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND PREVIOUS REPAIR DOUBLER SEPARATING, FASTENER HOLES ELONGATED AND SEALANT DETERIORATED ON THE RT WING MIDDLE L/E AT STA XW 408, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-17-00.

Part: SKIN — CRACKED (LT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND ABOUT A 1.5 INCH CRACK IN SKIN AND 9 FASTENERS BAD ON THE LEFT L/E AT STA XFS 422, 9 INCHES FROM FRONT SPAR, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-10-00.

Part: SKIN — WORN (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND THE SKIN WORN THROUGH ON THE AFT O/B END ON THE O/B WING L/E AT STA XRS 878, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-16-00.

Part: SKIN — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING BOTTOM OF LEADING EDGE O/B NR 3 PYLON O/B OF PANEL 523 AT STA XFS 291.500, 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 EO NR 00-107 WITH APPROVED 8110-3 DATED 5-10-00.

Part: RETAINER — CRACKED (CARGO DOOR) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK IN SEAL RETAINER OUTBOARD CENTER ''C'' PIT DOOR, 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 53-2-0, 52-2-0 AND 51-1-21.

Part: SKIN — GOUGED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND GOUGED SKIN ON THE RT WING NR 4 STUB LOWER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, ALODINED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-107 WITH APPROVED 8110-3 DATED 5-10-00.

Part: FRAME — CRACKED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA XFS 442, 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 57-2-0 AND 51-1-21.

Part: FRAME — CRACKED (HORIZONTAL STAB) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACKED UPPER LEFT I/B HORIZONTAL STAB L/E FR AT STA XFS 53.7, 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 51-1-4, 51-1-0, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VSIIT FOUND A CRACK TO THE UPPER RIB AT TRAILING EDGE I/B AT XFS 477, 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 51-1-21 AND 57-2-0.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A 9 INCH LONG CRACK TO THE STIFFENER AT X=-20 Y=960 TO 980 AND Z=-6, 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 53-2-0 AND 51-1-21.

Part: NUT PLATE — MISSING (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER RIB AT TRAILING EDGE I/B AT XFS 483, 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, 57-2-0 AND 51-1-21.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A BENT AND CRACKED DOOR FRAME AT A PIT DOOR LOWER DOOR FRAME, 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 51-1-24 AND 52-2-3.

Part: RIB — CRACKED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LOWER RIB AT TRAILING EDGE I/B AT CENTER L/E AT STA XFS 467, 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 57-2-0 AND 51-1-21.

Part: FRAME — CRACKED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA 435, 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 57-2-0 AND 51-1-21.

Part: FRAME — CRACKED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA XFS 360, 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 57-2-0 AND 51-1-21.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER BETWEEN FRAME -52 TO -70, -X20 INCHES TO 25 INCHES, 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 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: ATTACH ANGLE — CRACKED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/E ABOVE NR 2 PYLON UPPER FORWARD FORMER ATTACH ANGLE AT STA XFS 256, 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 51-1-4M 57-2-0 AND 51-1-21.

Part: FRAME — CRACKED (HORIZONTAL STAB) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACKED LOWER LEFT I/B HORIZONTAL STAB L/E FRAME AT XFS 53.7, 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 55-2-0, 51-1-4, 51-1-21 AND 51-1-20D.

Part: WEB — CRACKED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK WITH POPPED RIVETS TO THE AFT DOOR JAMB WEB AT STA 560, 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 53-2-0 AND 5-1-21.

Part: DOUBLER — DAMAGED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND AN IMPROPER REPAIR TO THE CENTER L/E LOWER FORMER AT STA XFS 335, 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 57-2-0 AND 51-1-21.

Part: FRAME — DAMAGED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND AN IMPROPER REPAIR TO THE CENTER L/E LOWER FORMER AT STA XFS 360, 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 57-2-0 AND 51-1-21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK 1 INCH AND 4 INCH LONG ON THE LOWER CENTER WING AREA EXTERNAL/INTERCOSTAL AT STA 781 AND L33R, 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 51-1-21, 51-1-4, 53-3-0 AND 51-1-21.

Part: SKIN — CRACKED (PAX DOOR) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND BENT METAL AND JAGGED EDGES (CRACKED) ON THE FORWARD ENTRY DOOR BOTTOM FWD CORNER, 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 51-2-0 AND 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE NR 11 UPPER RIB ON THE RT WING LEADING EDGE MIDDLE SECTION AT STA XFS 408, 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 57-2-0, 51-1-4 AND 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER RIB ON THE RT WING O/B LEADING EDGE AT STA XFS 748, 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 57-2-0, 51-1-4 AND 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE 3RD LOWER RIB ON THE RT WING MIDDLE L/E AT STA XFS 304, 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 57-2-0, 51-1-4 AND 51-1-21.

Part: STIFFENER — CRACKED (RT STUB WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING NR 4 STUB WING RT SIDE VERTICAL STIFFENER, 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 51-1-4 AND 51-1-21.

Part: FRAME — CRACKED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT XFS 328, 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 57-2-0 AND 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER RIB ON THE RT WING O/B LEADING EDGE AT STA XFS 752, 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 57-2-0, 51-1-4 AND 51-1-21.

Part: FRAME — TORN (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A TEAR TO THE FWD FRAME FOR CARGO DOOR UPPER CORNER, 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 53-2-0 AND 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE NR 7 UPPER RIB ON THE RT WING MIDDLE L/E AT STA XFS 407, 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-7 SRM 57-2-0 AND 51-1-21.

Part: FRAME — CRACKED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA XFS 372, 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 57-2-0 AND 51-1-21.

Part: FRAME — CRACKED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA XFS 366, 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 57-2-0 AND 51-1-21.

Part: FRAME — CRACKED (VERTICAL STAB) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE VERT STAB CENTER L/E FRAME AT ZFS 1797, 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 55-2-0 AND 51-1-21.

Part: RETAINER — CRACKED (PAX DOOR) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A BENT FWD DOOR SEAT RETAINER, 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 51-1-4, 51-1-24 AND 51-1-21.

Part: RIB — CRACKED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER RIB AT TRAILING EDGE I/B ON CENTER L/E AT XFS 477, 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 57-2-0 AND 51-1-21.

Part: SKIN — CRACKED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CRACKS TO THE DE-ICER BLEED HOLES ON THE LEADING EDGE O/B OF NR 1 PYLON, 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, 57-2-0 AND 51-1-21A.

Part: BRACE — CRACKED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK IN THE FIRST OVERHEAD BRACE LT SIDE AT STA 1916, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 5-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 53-2-0 AND 51-1-21.

Part: FRAME — CRACKED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA XFS 354, 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 57-2-0 AND 51-1-21.

Part: SKIN — CRACKED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE NOSE WHEEL WELL AFT RT CORNER OF CUTOUT, 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 53-2-1 AND 51-1-21.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE INTERCOSTAL AT STA 1100 TO 1120 AND L27R, 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 53-2-0 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: RIB — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE NR 5 UPPER RIB ON RT WING LEADING EDGE MID SECTION AT STA XFS 408, 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 57-2-0, 51-1-4 AND 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE NR 8 UPPER RIB ON THE RT WING LEADING EDGE MIDDLE SECTION AT STA XFS 408, 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 57-2-0, 51-1-4 AND 51-1-21.

Part: GUSSET — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LOWER RIB INTERCOSTAL GUSSET ON THE RT WING L/E MIDDLE SECTION AT STA XFS 350, 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 51-1-21 AND 51-1-4.

Part: RIB — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK AT END OF UPPER RIB ON RT WING OUTBOARD L/E AT STA XFS 741, 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 57-2-0, 51-1-4 AND 51-1-21.

Part: RIB — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE 4TH RIB LOWER SURFACE ON THE RT WING MIDDLE L/E AT STA XFS 310, 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 57-2-0, 51-1-4 AND 51-1-21.

Part: BAFFLE — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LOWER SURFACE OF THE RT WING O/B LEADING EDGE DUCTED SKIN BAFFLE AT STA 678, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1.

Part: RIB — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACKED NR 12 UPPER RIB ON THE RT WING L/E MIDDLE SECTION AT STA XFS 408, 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 57-2-0, 51-1-4 AND 51-1-21.

Part: WEB — CRACKED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CUSP WEB AT STA 980 TO 1000 LT SIDE AND L24L, 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 53-2-0, 51-1-4 AND 51-1-21.

Part: FRAME — CRACKED (VERTICAL STAB) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE VERT STAB LOWER L/E FRAME, 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 55-2-0, 51-1-4 AND 51-1-21.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CRACKED AND BENT BRACES ON THE FWD LOWER BILGE LEFT SIDE OF BULKHEAD AT STA 70, 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 53-20-0 AND 51-1-21.

Part: FRAME — CRACKED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER L/E UPPER FORMER AT TRAILING EDGE AT STA XFS 348, 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 57-2-0 AND 51-1-21.

Part: FRAME — CRACKED (VERTICAL STAB) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE VERT STAB CENTER L/E FRAME AT ZFS 267, 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 55-2-0 AND 51-1-21.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LONGERON AT THE FWD LWR CARGO BILGE AT STA 560 TO 550 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0.

Part: RIB — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING NR 3 STUB WING NR 12 RIB UPPER T/E, 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, 57-2-0, 51-1-21 AND 51-1-20D.

Part: RIB — CRACKED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING NR 3 STUB WING NR 6 RIB UPPER END, 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 57-2-0, 51-1-21 AND 51-1-20D.

Part: SILL — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE R1 DOOR AFT SILL AT FR 600 AND L21R, 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 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMGE TO THE LAV FLOOR PANEL FWD. CARGO COMPT. AT STA 220-240 AND X-40, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PANEL IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE COCKPIT FLOOR PANEL AT SCREW HOLES AT STA -12, +32 TO -32, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PANEL IAW DC-8 SRM 51-1-4, 51-1-21 AND 53-2-0.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOOR PANEL AT STA 50-70 X-50 Z-0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMMAGE TO THE COCKPIT PANEL 676B ALONG EDGE & SCREW HOLES AT FR -52X-20,Z0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SKIN IAW DC-8 SRM 51-1-4 AND 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FRAME — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT SIDE FRAME AT STA 1140 AND L36, DAMAGE EXCEEDED LIMITATIONS 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. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CABIN FLOOR RT INTERCOSTAL AT STA 660, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PART IAW DC-8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — BULGED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A BULGE TO THE SKIN IN THE FWD LWR CARGO BILGE AT STA 622 AND L36 TO L35L, 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 00-107 WITH APPROVED 8110-3 DATED 5-1-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — DENTED (RT WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A PREVIOUS DENT REPAIR FILLER DETERIORATED AND DEBONDING ON THE RT WING EXTERIOR L/E AT STA XFS 737, 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 00-107 WITH APPROVED 8110-3 DATED 5-16-00.

Part: SKIN — DENTED (NLG DOOR) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND 2 DENTS IN SKIN BELOW GROUND POWER RECPT PLATE AT NOSE GEAR/FWD DOOR, 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 53-2-0, 52-1-0 AND 51-1-21.

Part: SKIN — CRACKED (LT WING LE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A CRACK FROM SCREW HOLE ON THE LEFT L/E LWR SURFACE AT STA XFS 710, 26 INCHES FROM FRONT SPAR, 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.

Part: SKIN — DAMAGED (WING) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND A SCREW PULLING THROUGH SKIN ON THE FWD FRONT SPAR AT STA XFS 710, 26 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.

Part: SKIN — CORRODED (LT WING LE) · airframe 733,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN ON THE LT UPPER SURFACE L/E BETWEEN STA XFS 666 & 672, 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. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE UNDER THE FINGER DOUBLER AND POPPED RIVET HEADS AT STA -32+-52, X-15" TO 21", 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 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE DOUBLER BETWEEN FRAMES -12&8, +X=58 INCHES, -Z=11 INCHES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. REMAINING THICKNESS IS WITHIN LIMITS.

Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FINGER DOUBLER AT STA -32, -X=20 TO 22 INCH RT -Z-11, 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 53-2-0.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LONGERON 33R AT STA 580, 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 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN AT STA 700 TO 781 AND L35L TO L35R, 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 AND E.O. 00-107.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON SEAT TRACK 2ND FROM O/B RT SIDE FRAME AT STA 1120+X-48, Z-0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW PART IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE T/E OF THE RT HORIZONTAL STABILIZER AT STA XE 278, 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 53-2-0 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: PANEL — CORRODED (RT HORIZ STAB) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE UPPER PANEL RT HORIZ STAB AT STA XE 248, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED NEW PANEL. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE T/E RT HORIZ STAB AT STA XE99, 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 53-2-0, 51-1-21 AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: ATTACH ANGLE — CORRODED (CARGO BAY) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LOWER GILLINER ATTACH ANGLE AT STA 1540 AND L27L-L27R, DAMAGE EXCEEDED LIMITATIONS 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 AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: LONGERON — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE DOME NUTS ON L30R & L27R AT STA 35-70, 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 53-2-0 AND 52-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FITTING — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FRAME FITTING AFT SIDE AT STA 1240 LT BELOW LONGERON 1, 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 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 73,187 hrs · 27,600 cycles

DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FWD LOWER CARGO BILGE INTERCOSTAL ANGLE TO CIRCUMFERENTIAL FRAME AT STA 380 AND L29R, DAMAGE EXCEEDED LIMITATION 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 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — DAMAGED (FUSELAGE)

ACFT DAMAGED AFT OF CARGO DOOR BY K-LOADER. REPAIRED DAMAGE WITH EXTERNAL DOUBLER IAW DC-8 SRM CHAPTER 53-2-1 PG 117/118 AND MESSAGE NR EAF-ILM-00-00024 H DATED 08 FEB 00. ACFT FERRIED TO KMDT FOR PERMANENT SHEET METAL REPAIRS.

Part: PIN — FAILED (RT MLG ACTUATOR)

UPON GEAR DOWN SELECTION, LOUD (EXPLOSIVE) BANG CAUSED AIRCRAFT TO SHUTTER VIOLENTLY ALL INDICATIONS NORMAL. FOUND RT MAIN LANDING GEAR ACTUATOR PIN BROKEN SECURED ACTUATOR TO GEAR. INSTALLED 3 GEAR PINS AND SAFTIED. I HAVE INSPECTED THIS ACFT AND FOUND IT SAFE FOR FLIGHT INTENDED. REMOVED AND REPLACED RIGHT MLG RETRACT PIN AND REWORK OF MLG PIN BOSS IAW S/B 32-102 AND APPROVED 8110-3 DATED 04/13/99. GEAR SWING C/W PER DC-8 M/M 32-10-00. OPS CHECKS GOOD PER DC-8 MM 32-10-00.

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 1 INCH EACH SIDE OF THE AIRCRAFT CENTERLINE. 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. SUBMITTER RECOMMENDED THE FOLLOWING: PERFORM PERIODIC INSPECTIONS OF ALL DC-8 ACFT WITH FLAT AFT PRESSURE BULKHEADS, AND, REPAIR CRACKS PER DC-8 SRM 53-2-5 FIG 26.

Part: FITTING — CORRODED (BS 878)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 878 AND LONGERON 24 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER TIE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: ANGLE — CORRODED (BS 1750 - 1790)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO ATTACHMENT ANGLE BETWEEN STA 1750 TO 1790 AND LONGERON 2 LEFT, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER TIE IAW DC-8 SRM 53-2-5 FIG 16A.

Part: LONGERON — CORRODED (BS 902)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 24 LEFT AT STA 902, DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: ANGLE — CORRODED (VERTICAL STAB)

DURING A MAINTENANCE VISIT, FOUND CORROSION, VERTICAL STABILIZER, ATTACHMENT ANGLE BETWEEN STA 1750 AND STA 1790 AND LONGERON 2 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER TIE IAW DC8 SRM 53-2-5 FIGURE 16A. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SKIN — CORRODED (BS 1990-1998)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SKIN PANEL BETWEEN STA 1998 AND STA 1990 AND BETWEEN LONGERONS 35 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 REPAIR DOUBLER TIE IAW DC-8 SRM 53-2-0 FIGURE 1D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FRAME — CORRODED (BS 1020)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME AT STA 1020 BETWEEN LONGERONS 35 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 REPAIR IAW TIMCO DWG DC08-0229 REV. A AND DC-8 SRM 53-2-0 FIGURE 2. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-4-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: SHEAR TIE — CORRODED (BS 1717)

DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SHEAR TIE AT STA 1717 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 SHEAR TIE IAW DC-8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).

Part: FIRE LOOP — MALFUNCTIONED (NR 2 ENGINE)

NR 2 ENGINE FIRE WARNING ILLUMINATES INTERMITTENTLY WITH ENGINE RUNNING OR SHUTDOWN. FIRE WARNING TEST NORMAL. REMOVED AND REPLACED RT AND LT FAN COMPARTMENT FIRE LOOPS AND RT AND LT LOWER CORE COMPARTMENT FIRE LOOPS. NR 2 ENGINE FIRE WARNING OPS CHECKS GOOD STATIC AND ON HIGH POWER RUN IAW MM CHAPTER 77-21-20. CLOSED AND SECURED COWLINGS.

Part: SKIN — CRACKED (WS 192)

DURING A JOINT FAA INSPECTION AND EMERY MAINTENANCE PERSONNEL, FOUND .5 INCH CRACK ON RIGHT WING LEADING EDGE AT XFS 192. STOP DRILLED ENDS OF CRACK, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E63-B01 REV 1B.

Part: CONTROLS — MALFUNCTIONED (AILERONS)

IN FLIGHT THERE WAS A LARGE DEAD SPOT IN THE AILERONS IN THE CENTER/NEUTRAL POSITION. IN FLIGHT THE AIRPLANE ROLLS LEFT AND RIGHT. TO STOP OR CONTROL THE ROLL YOU HAVE TO DO A DUTCH ROLL TYPE OF MANUVER TO CONTROL THE ROLL. INSPECTED CONTROL SURFACES, CABLES, PULLEYS, LINKAGES, ALL ATTACH FITTINGS. CHECKED CABLE TENSIONS, RAN AILERONS THROUGH MANY CYCLES. NO DEFECTS FOUND. OPS CK GOOD ON GRND. INSPECTED OPERATION OF FLT SPOILERS, ALLS OPS CK GOOD ON GRND. MAINTENANCE REQUESTED TEST FLIGHT. TEST FLIGHT SATISFACTORY.

Part: LONGERON — CORRODED (BS 990-1010)

DURING A MAINTENANCE VISIT, FOUND LONGERON 31R BETWEEN Y=990 TO Y=1010 CORRODED. CORROSION DAMAGE PAST LIMITATIONS AFTER BLEND-OUT. REPAIRED LONGERON 31R BY FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW REO 01847 AND TREATED AREA IAW DC-8 SRM 51-1-8.

Part: LONGERON — CORRODED (BS 980-990)

DURING A MAINTENANCE VISIT, FOUND LONGERON 36 BETWEEN Y=980 TO Y=990 CORRODED. CORROSION DAMAGE PAST LIMITATIONS. REPAIRED LONGERON 36 BY REMOVING DAMAGE AND FABRICATING REPAIR STRAP AND SHIMS AND INSTALLED, IAW REO 01847 AND TREATED IAW DC-8 SRM 51-1-8.

Part: LONGERON — CORRODED (BS 1220-1240)

DURING A MAINTENANCE VISIT, FOUND LONGERON 27R BETWEEN Y=1220 TO Y=1240 CORRODED. CORROSION DAMAGE PAST LIMITATIONS. REPAIRED LONGERON 27R BY FABRICATING REPAIR STRAP AND INSTALLED IAW REO 01841 AND TREATED AREA IAW DC-8 SRM 51-1-8.

Part: UPLATCH — LACK OF LUBE (MLG DOOR)

KPHX/KDFW - FLT 298 - THE MLG DOOR NOT LATCHED LIGHT REMAINED ON AFTER GEAR RETRACTION. THE FLIGHT CREW RECYCLED THE LANDING GEAR AND THE LIGHT DID NOT EXTINGUISH. MAINTENANCE CLEANED AND LUBED THE RT UPLATCH MECHANISM. AN OPERATIONAL CHECK OF THE LANDING GEAR WARNING SYSTEM WAS GOOD.

Part: FLIGHT LOCK — STICKING (RT MLG)

RIGHT MAIN GEAR DOOR LIGHT ON DURING UPLATCH CHECK. LIGHTS WENT OUT ON 3RD RECYCLE WITH FLAPS UP. MAINTENANCE PERFORMED ELECTRICAL AND MECHANICAL FUNCTIONAL TEST OF LT AND RT GEAR FLIGHT LOCKS. FOUND RT FLIGHT LOCK STICKING. CLEANED AND LUBED FLIGHT LOCKS. OPS CHECK GOOD THROUGH MANY CYCLES PER MM 32-6.