N8091U
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNITED AIRLINES, INC. (CALA) | Operator | on 1971-05-15 | Operator named in NTSB report |
Accident & incident history
Operated by UNITED AIR LINES INC (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
257 reports on file, 1995-09-26 – 2001-05-02.
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 84,424 hrs · 32,385 cycles
COMPLY WITH FCD A53-4R1 INSPECTION FOR LOWER FUSELAGE CORROSION. INSPECTED LOWER FUSELAGE FOR CORROSION. FOUND CORROSION AT STA 100 L36 LEVEL 2 CORROSION. BLENDED CORROSION, BEYOND LIMITS. AIRCRAFT FERRIED TO TENNESSEE TECHNICAL SERVICES, LLC. INSPECTED THIS AIRCRAFT AND FOUND IT SAFE FOR THE FLIGHT INTENDED. REMOVED CORROSION IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER, TREATED, PRIMED AND INSTALLED REPAIR PER EO 01-131 WITH APPROVED 8110-3 DATED 05/03/01.
Part: SWITCH — FAILED (MLG) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND UNSAFE LIGHT DAMAGE TO LT MLG UNSAFE LIGHT (RED) STAYS ON & NO L/H MLG GREEN LIGHT AFTER SEVERAL GEAR CYLES, GOT GREEN LIGHT ONLY AFTER STEEP BANKS AT LT. SIDE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 MM 32-60-0 AND DC-8 MM 32-20-00.
Part: FLOOR PANEL — CORRODED (#676 CENTER FWD.) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CENTER FWD. FLOOR PANEL AT COCKPIT PANEL #676, 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 AND DC-8 SRM51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FITTING — GOUGED (WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND GOUGE DAMAGE TO LT. WING CANOE FITTING AT STA.340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 8110-3 DATED 03/23/01.
Part: STRINGER — CRACKED (STR.53 STA.495) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING STR.53 AT STA. 495 AND AFT HORZ. LEG, 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 E.O. #01-024 WITH APPROVED 8110-3 DATED 03/15/01.
Part: PANEL — CORRODED (STA. 46-66) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO LAV. FLOOR PANEL AT STA. 46-66, 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 51-1-4 AND DC-8 SRM 51-3-0 AND DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENCE VISIT FOUND HOLE DAMAGE TO HORZ STAB RT. ELEVATOR AT STA. XE 228.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 8110-3 DATED 02/25/01.
Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT. MLG BODY DOOR AT AFT O/B CORNER FRAME, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. #01-024 WITH APPROVED 8110-3 DATED 03/13/01.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND HOLE DAMAGE TO TAIL CONE SKIN AT STA.1902 AND RT 14 INCHES O/B AND 8 INCHES AFT OF ACCESS DOOR NR 62, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED NEW PART AND INSTALLED IAW DC-8 SRM 51-1-5, DC-8 SRM 53-2-0, AND DC-8 SRM 51-1-21.
Part: BUSHING — ELONGATED (2ND O/B VANE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED BUSHING DAMAGE TO #3 LT. FLAP 2ND FROM O/B VANE AT 2ND O/B VANE, 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 E.O.#01-024 WITH APPROVED 8110-3 DATED 02/01/01.
Part: SPAR — CORRODED (STA 781) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BOTTOM OF SPAR AT STA. 781 AND INSIDE L/H CENTER TANK THUR MID-SPAR ACCESS HOLE560E, 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 E.O.#01-024 WITH APPROVED 8110-3 DATED 01/31/01.
Part: BRACKET — WORN (CARGO DOOR SEAL) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND WORN DAMAGE TO A-PIT DOOR SEAL FRAME AT A-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O 01-024 WITH APPROVED 8110-3 DATED 03/13/01.
Part: SKIN — CRACKED (DOOR FRAME) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CRACK DAMAGED TO A-PIT DOOR SEAL FRAME WORN/CRACKED OUT INCLUDING SKIN--LOC CENTER SECTION OF DOOR AT A-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 8110-3 DATED 03/13/01.
Part: SKIN — GOUGED (CARGO DOOR) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND GOUGED DAMAGE TO A-PIT DOOR SEAL FRAME & DOOR SKIN AT THE A-PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 8110-3 DATED 03/13/01.
Part: SKIN — TOOL DAMAGE (LT WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND TOOLING MARK DAMAGE TO LWR. WING SKIN UPPER SURFACE AT STA. XRS 507.625 AND STR. 54, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 8110-3 DATED 03/09/01.
Part: FRAME — CORRODED (SAT 1140-1160) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BRACKET AT STA. 1140-1160 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 & 51-1-4 & 53-2-0 FIG1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SKIN — CORRODED (L35L STA.705) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO OUTER SKIN L35L AT STA.705, DAMAGE EXCEEDED LIMITATIONS IAW DC-8SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: PANEL — CORRODED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO L/H STRESS PANEL AT KEEL BEAM, AT STA 740, 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 51-1-4.
Part: FITTING — GOUGED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND GOUGING DAMAGE TO RT. CANOE FITTING TOP FWD 3 INCHES AT RT. STA 340, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. #01-024 WITH APPROVED 8110-3 DATED 02/26/01.
Part: SKIN — CORRODED (STA640-610) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FILLET ATTACH HOLES AT STA. 640-610 AND L31L TO L28L, 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 53-2-0 AND E.O.#01-024 WITH APPROVED 8110-3 DATED 03/08/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SKIN — CORRODED (STA772-721) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO SKIN AT STA. 772-721 AND L35L-L36R, 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 EO#01-024 WITH APPROVED 8110-3 DATED 03/02/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: BULKHEAD — CRACKED (C & D PIT) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE INSPECTION FOUND CRACK DAMAGE TO C & D PIT R/H BULKHEAD AT C & D PIT, DAMAGE EXCEEDS LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/23/01.
Part: BRACE — CRACKED (STA. 1916) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENACE VISIT FOUND CRACK DAMAGE TO HORZ. BRACE AT STA. 1916 AND DOOR 62, 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 51-1-4 AND DC-8 SRM 51-1-0.
Part: SKIN — GOUGED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND GOUGED AND DENTED DAMAGE TO SKIN AT STA.1890 AND TAIL POST SUPPORT, DAMAGE EXCEEDED LIMITAIONS IAW DC-8 SRM. REMOVED DAMAGE AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-2-1 AND DC-8 SRM 53-2-0.
Part: SKIN — DAMAGED (RUDDER) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND HOLE DAMAGE TO SKIN AT HOLE 62 AND RUDDER POWER PACK LEDGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND ISTALLED IAW SRM 51-1-4 AND DC-8 SRM 51-1-21.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VIST FOUND ELONGATED HOLE DAMAGE TO SKIN AT FWD OF MLG DOORS, DAMAGE ECXEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 51-3-0.
Part: ANGLE — BROKEN ("C-PIT" R/H AFT) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND THE "C-PIT" ANGLE BROKEN IN HALF (AFT R/H), 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 51-1-4 AND DC-8 SRM 51-1-21.
Part: PANEL — CRACKED (L/H STA1540-1620) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CUSP LINE PANEL AT STA 1540-1620 L/H, 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.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CUSP RAIL AT STA 210-380 RT, 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.
Part: HAND RAIL — CRACKED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SIDE RAIL AT STA 90-220 RT, 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 AND DC-8 SRM 51-1-4.
Part: SKIN — CORRODED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FUEL TANK PANEL LAND 506B AT STA XRS 110 TO 125 S-69 TO S-71, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. #01-024 WITH APPROVED 8110-3 DATED 01/29/01 AND DC-8 SRM 57-2-1 FIG.36.
Part: SKIN — CORRODED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO INTERNAL SKIN LT WW AT STA. 857-879 AND LBL 0-68.5, 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 51-3-0 & 53-2-0 FIG.1F.
Part: PANEL — CORRODED (PANEL #329) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE GALLEY FLOOR PANEL AT TOP SURFACE PANEL #329, DAMAGE EXCEEDED LIMITATIONS IAAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FITTING — CRACKED (RBL -24" STA 300) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FLOOR BEAM SUPPORT FITTING AT STA 300 AND RBL -24", 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.
Part: FITTING — CRACKED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A 2.5 INCH CRACK INSIDE BATH TUB FITTING LWR HORIZ. SURFACE TO LT LONGERON 24 STA 860, 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 & 53-2-2 FIG.5.
Part: FITTING — CORRODED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CENTER WING SKIN AT STA 960-980 X+45", 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 & 53-2-0 FIG. 1F.
Part: FRAME — GOUGED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A GOUGE TO THE FWD SIDE OF FRAME ON THE R/H FWD TYPE I DOOR FRAME SEAL AT STA 370, 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 & 53-2-0.
Part: DOUBLER — BENT (A-PIT FS320-333) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A BENT TO THE UPPER FWD CORNER ON THE DOUBLER FOR "A-PIT" CUTOUT AT STA 320-333, 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 51-1-7 & 51-1-21.
Part: FLANGE — CRACKED (DOOR SEAL) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT FWD TYPE I DOOR FRAME SEAL FLANGE LWR END, DAMAGE EXCEEDED LIMITATIONS IAAW 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 DC-8 SRM 53-2-0.
Part: FLOOR PANEL — MISREPAIRED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND AN IMPROPER REPAIR TO THE MAIN CARGO FLOOR PANEL AT STA 80 TO 340E, 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 DC-9 SRM 53-2-3.
Part: GUARD — CRACKED (PAX DOOR) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK IN 2 PLACES TO THE R-1 DOOR SILL GUARD, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/15/01.
Part: DOUBLER — BENT ("A-PIT" STA 292) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A BENT UPPER FWD CORNER TO THE DOUBLER FOR "A-PIT" CUTOUT AT STA 292, 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 51-1-7 AND DC-8 SRM 51-1-21.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER WING FLOOR BEAM AT STA 857 X+60, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/26/01.
Part: FITTING — CORRODED (STA1690 L30R) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION TO BATH TUBE FITTING AT STA. 1690 AND L30R, 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 & 51-1-24 & 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: PANEL — CORRODED (#681) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE COCKPIT FLOOR PANEL #661 AND CRACKED SCREW HOLES, 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 AND 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SKIN — CORRODED (LT WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND DISCOLORATION TO THE SKIN ON INSIDE TANK AT LT LWR WING FUEL VENT BOX UPPER SKIN BETWEEN STRINGERS NR 1 & 2, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 01/31/01.
Part: PANEL — CORRODED (#677) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND PERIMETER TOP & BOTTOM EDGES OF CENTER COCKPIT FLOOR PANEL #677 CHAFF STRIP BROKEN, ELONGATED HOLES, 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 51-1-4 AND 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED LOCK HOLES ON THE FE'S FWD SEAT TRACK, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREAIAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-3-0.
Part: PANEL — CRACKED (#676D) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE EDGES OF THE FLOOR PANEL CAPT'S SIDE PANEL #676D, 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 51-1-4.
Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO ACCESS HOLE 60 DOOR FRAME AT STA. 1793-1766 AND L34L-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 51-1-21 & 51-1-24 & 51-1-4.
Part: SKIN — BROKEN (NR 2 SPOILER) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A BROKEN CORNER OF NR 2 GROUND SPOILER BAY ON LT WING NOT SPOILER, 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 57-2-0 FIG.4.
Part: PANEL — CRACKED (STA 960-980) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H I/B FLAP TRACK COVER PANEL BETWEEN STA 960-980, 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 53-2-0 FIG.1B.
Part: PLATE — CRACKED (NR 4 STUB WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO NR 4 STUB WING I/B LWR. FRONT SPAR L/E SHIM PLATE AT I/B LWR. FRONT SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.01-024 WITH APPROVED 8110-3 DATED 02/15/01.
Part: PANEL — CORRODED (STRESS PANEL) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE STRESS PANEL ON SHELF (F), 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 FIG.1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: DOUBLER — CRACKED (STA XFS 435.789) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM CENTER DOUBLER AT STA XFS 435.789, 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 51-1-4 & 51-1-21.
Part: SHIM — CRACKED (IB LWR FRNT SPAR) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO #1 STUB WING I/B LWR. FRONT SPAR L/E SHIM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, AND TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-24 WITH APPROVED 8110-3 DATED 02/15/01.
Part: PANEL — CRACKED (L/H WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H #1 ALT INSIDE TANK FWD OF MIDSPAR 485 CAN'T WEB PANEL, 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 57-2-0 FIG.2A & 51-1-21.
Part: PANEL — DELAMINATED (STA XW 106) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE R/H WING LWR SURFACE FWD OF I/B FLAP STOP PANEL AT STA XW 106, 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 51-3-0.
Part: PANEL — CRACKED (STA 485) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H #4 ALT 505B CAN'T WEB PANEL AT STA 485, 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 &57-2-0 FIG.2A.
Part: PANEL — CORRODED (RT WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RT WING UPPER WING T/E PANEL BETWEEN STA XRS 693 TO XRS 624, 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 51-3-0.
Part: FORMER — CRACKED (XFS 227.335) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO T/E FORMER AT STA. XFS 227.335, 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 57-2-0.
Part: BRACKET — CRACKED (XFS 248) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO BRACKET AT STA. XFS248, 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 51-1-4 AND DC-8 SRM 51-3-0.
Part: FRAME — CORRODED (STA1170 L36-L35R) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FUSELAGE FRAME AT STA. 1170 AND LONGERON 36 TO 35R, 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 E.O. #01-024 WITH APPROVED 8110-3 DATED 03/08/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: PANEL — CRACKED (STA 80) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK AT SCREW HOLE TO THE UPPER WING PANEL AT STA 80, 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 AND DC-8 SRM 57-2-0 FIG. 2A.
Part: PANEL — CORRODED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AROUND PARAMETER OF THE BOTTOM PANEL BELOW LT STRESS PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED SCREW HOLES ON THE LWR I/B T/E AT STA XFS 7.500, 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 51-1-26 AND DC-8 SRM 51-1-14 AND DC-8 SRM 51-1-21.
Part: DOUBLER — CRACKED (STA XFS 435.789) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK BETWEEN THE SKIN ON THE BOTTOM DOUBLER AT STA XFS 435.789, 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 57-1-14 & 51-1-21.
Part: FORMER — CRACKED (STA XFS 434.750) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM T/E FORMER AT STA XFS 434.750, 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 SRM 51-1-21.
Part: LINK — GOUGED (STA 98) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A GOUGE AT UPPER END OF THE AFT FLAP DRIVE LINK AT STA 98, 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 E.O.#01-024 WITH APPROVED 8110-3 DATED 02/09/01.
Part: FITTING — CORRODED (RT WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A PITTED CANOE FITTING UNDER FLAP ROLLER TRACKS ON THE RT WING AT STA 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.01-024 WITH APPROVED 8110-3 DATED 02/09/01.
Part: SKIN — CRACKED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A 1 1/2 INCH CRACK AND (2) DENTS TO THE SKIN TOP I/B AT STA XFS 141.250 TO 147.5, 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 55-2-1.
Part: PRESSURE PANEL — CRACKED (COCKPIT FLOOR) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION AND CRACK DAMAGE TO COCKPIT FLOOR PANEL 682A, 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 51-1-4.
Part: FITTING — CORRODED (LT WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A PITTED CANOE FITTING UNDER FLAP ROLLER TRACKS LT WING AT STA 219, 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 E.O.#01-024 WITH APPROVED 8110-3 DATED 02/09/01.
Part: FITTING — CORRODED (LT WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A PITTED CANOE FITTING UNDER FLAP ROLLER TRACKS LT WING AT STA 410, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.01-024 WITH APPROVED 8110-3 DATED 02/09/01.
Part: FITTING — CORRODED (RT WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A PITTED CANOE FITTING UNDER ROLLER TRACKS ON THE RT WING AT STA 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O. 01-024 WITH APPROVED 8110-3 DATED 02/09/01.
Part: DOUBLER — CRACKED (STA XFS 435.789) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM DOUBLER AT STA XFS 435.789, 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 51-1-14 & 51-1-21.
Part: FITTING — CORRODED (LT WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A PITTED CANOE FITTING UNDER FLAP ROLLER TRACKS LT WING AT STA 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/09/01.
Part: BRACKET — CRACKED (I/B END) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED BRACKET AT I/B END REPAIR NOT PER SRM, 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 AND DC-8 SRM 51-1-4.
Part: FORMER — CRACKED (STA 461.372) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA 461.372, 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 57-2-0.
Part: SHIM — CRACKED (L32R STA 1793) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE SHIM UNDER LONGERON 32R INSIDE ACCESS HOLE #60 AT STA 1793, 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 E.O.#01-024 WITH APPROVED 8110-3 DATED 02/23/01.
Part: FITTING — GOUGED (WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A GOUGE TO THE AFT END OF THE CANOE FITTING AT STA 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
Part: FITTING — CORRODED (STA.1690 L32R) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO BATH TUBE FITTING AT STA. 1690 AND L32R, 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 51-1-24 & 51-1-21 & 51-1-20D &51-1-3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: PANEL — CORRODED (PANEL#678) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO FLOOR PANEL #678 UNDER F/E TABLE, 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 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: PANEL — CORRODED (PANEL #676F) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO COCKPIT FLOOR PANEL #676F, 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 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: PANEL — CORRODED (PANEL #676B) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO CO-PILOTS FLOOR PANEL #676B AROUND PERIMETER, 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 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: PANEL — CORRODED (PANEL #676A) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENACE VISIT FOUND CORROSION DAMAGE TO R/H COCKPIT FLOOR PANEL #676A, 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 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: PANEL — CORRODED (STA55-80 X+32) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO GALLEY FLOOR TOP SURFACE PANEL #328 AT STA. 55-80 AND X+32, 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 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: BOSS — CORRODED (LT & RT MLG) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION TO THE MLG STRUT ASSY. RETRACT PIN BOSS & RETRACK PIN BY DOING MA-AI-3210-01:03, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW MA-A1-3210-01:03 AND E.O#01-024 WITH APPROVED 8110-3 DATED 02/02/01 AND DC-8 S/B 32-102 AND DC-8 MM 32-30-0.
Part: FORMER — CRACKED (STA XS 213.750) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 213.750, 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 SRM 57-2-0.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED SCREW HOLE ON THE O/B TOP, 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 57-2-0.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A SCREW PULLING THROUGH SKIN AND HOLES ELONGATED ON THE SLOT L/E PANEL, 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 57-2-1A AND 51-1-21.
Part: DOUBLER — CRACKED (STA XS 220.190) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP DOUBLER ABOUT 2" AT STA XS 220.190, 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 AND DC-8 SRM 51-1-21 DC-8 DWG. 5769869 AND E.O.#01-024.
Part: FORMER — CRACKED (STA XS 213.750) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 213.750, 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
Part: DOUBLER — CORRODED (STA. 1155-1170) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AFT LWR. CARGO BILGE INTERNAL DOUBLER AT STA. 1155-1170 AND L35L TO 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 E.O. #01-024 WITH APPROVED 8110-3, DATED 02/02/01. SEE N/R'S 5E-026 & 5E-091. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: PANEL — CORRODED (STA55-80 X+16) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO GALLEY FLOOR TOP SURFACE PANEL #327 AT STA. 55-80 AND X+16, 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 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: BRACKET — CRACKED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE ANGLE BRACKET BETWEEN STA XS 250.089 AND XS 252, DAMAGE EXCEEDED LIMITATIONS IAAW 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.
Part: SKIN — CRACKED (XFS 253.150) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A 1" CRACK TO THE BOTTOM SKIN AT CUT-OUT FOR PYLON AT STAY XFS 253.150, 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 57-2-1A.
Part: FORMER — CRACKED (STA XS 227.335) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 227.335, 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 AND DC-8 SRM 51-3-0.
Part: FORMER — CRACKED (STA XS 250.089) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A 2 1/2" CRACK TO THE TOP FORMER AT STA XS 250.089, 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 AND DC-8 SRM 51-1-21.
Part: FORMER — CRACKED (STA XS 255) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 255, 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 57-2-0.
Part: FORMER — CRACKED (XFS 255) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 255, 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 AND DC-8 SRM 51-1-21.
Part: FORMER — CRACKED (STA. XFS 117) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT. SIDE T/E FORMER AT STA. ZFS 117, 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 57-2-0.
Part: GUSSET — CRACKED (STA 195) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED GUSSET AT FORMER AT STA 195, 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.
Part: FORMER — CRACKED (STA XFS 616.250) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA 616.250, 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 & 57-2-0.
Part: FORMER — CRACKED (STA XFS 635) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 635, 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 57-2-0 & 51-1-21.
Part: FORMER — CRACKED (XFS 641.250) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 641.250, 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.
Part: SKIN — CRACKED (XFS 141.250-147.) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A 1 1/2" CRACK IN THE TOP L/E SKIN AND TWO DENTS BETWEEN STA XFS 141.250 TO STA XFS 147.500, 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 AND PRC1422-B-2.
Part: ANGLE — CRACKED (XS 195) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE ANGLE AT FORMER AT STA XS 195, 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.
Part: ANGLE — CRACKED (STA XS 225) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A 1" CRACK TO THE ANGLE AT CAP AT STA XS 225, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED ARE IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-4 AND DC-8 SRM 51-1-21.
Part: FORMER — CRACKED (STA XS 251.089) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A 6" CRACK TO THE TOP FORMER AT STA XS 251.089, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTIVE///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 57-2-0.
Part: GUSSET — CRACKED (XFS 195-201.250) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE GUSSET BETWEEN STA XFS 195 AND STA XFS 201.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SR. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND DC-8 SRM 51-1-4 AND DC-8 SRM 51-1-20D.
Part: FORMER — CRACKED (STA. XFS 175) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT. SIDE T/E FORMER AT STA. ZFS 175, 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 57-2-0.
Part: SKIN — CORRODED (STA. 1140-1170) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO AFT LWR. CARGO BILGE FUSELAGE SKIN AT STA. 1140-1170 AND L35L TO L35R, 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 E.O. #01-024 WITH APPROVED 8110-3 DATED 02/02/01. SEE N/R'S 5E-026 & 5E-090. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: DOUBLER — DAMAGED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND AN AREA OF METAL BROKEN OUT AT THE CORNER ON THE BOTTOM SKIN DOUBLER AT STA XS 250.089, 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 57-2-0 AND DC-8 SRM 51-1-21.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH THE SKIN AT THE I/B SLOT VANE, 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 51-1-9.
Part: FITTING — CRACKED (X+69" STA 879) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER WING FRAME FITTING AT STA 879 X+69", 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.
Part: FORMER — CRACKED (XFS 145) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE O/B BOTTOM T/E FORMER AT STA XFS 145, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21.
Part: FORMER — CRACKED (STA XS 520) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A 1" CRACK TO THE TOP I/B FORMER AT STA XS 520, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. ----------CX---------- (NO CRACK)
Part: FORMER — CRACKED (STA ZFS 98) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT SIDE T/E FORMER AT STA ZFS 98, 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 57-2-0.
Part: PANEL — DAMAGED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE BOTTOM SLOT PANEL, 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 51-1-4.
Part: FORMER — CRACKED (STA ZFS 110) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT SIDE T/E FORMER AT STA ZFS 110, 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 57-2-0.
Part: ANGLE — CRACKED (XFS 188.750) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE O/B TOP GUSSET ANGLE AT STA XFS 188.750, 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
Part: FORMER — CRACKED (STA 448.581) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA 448.581, 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 57-2-0.
Part: SKIN — DAMAGED (WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A BROKEN OUT BOLT HOLE ON THE TOP PLATE, 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 57-2-0.
Part: STRINGER — CRACKED (STR #54) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CAN'T LWR STR #54 ON THE R/H 505B INSIDE TANK AND O/B BETWEEN STA XRS 495 AND 508, 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 E.O.#01-024 WITH APPROVED 8110-3 DATED 03/10/01.
Part: FORMER — CRACKED (XFS 448.581) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP FORMER AT STA XFS 448.581, 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 57-2-0.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED SCREW HOLES ON THE BOTTOM T/E BETWEEN STA XFS 85.000 TO STA XFS 91.250, 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 AND DC-8 SRM 51-1-4.
Part: PANEL — DAMAGED (WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES ON THE BOTTOM SLOT PANEL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW 51-1-22 AND 51-1-4.
Part: FORMER — CRACKED (STA XS 235) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A 8" CRACK TO THE TOP I/B FORMER AT STA XS 253, 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 57-2-0.
Part: FORMER — CRACKED (STA 104.750) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT SIDE T/E FORMER AT STA 104.750, 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 SRM 57-2-0.
Part: FRAME — CORRODED (X+69" STA 860) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CENTER WING FRAME FITTING AT STA 860 X+68", 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 51-1-24 AND DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FINGER DOUBLER — DAMAGED (COCKPIT) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL POPPED RIVETS TO THE COCKPIT SUB-FLOOR BETWEEN FRAMES X-32 & X-52 Y-20 Z-11, 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 AND DC-8 SRM 53-2-0 FIG.1F.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FLOORBEAM CENTER WING STA 879, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW E.O.01-024 WITH APPROVED 8110-3 DATED 01/29/01.
Part: SKIN — DAMAGED (WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH SKIN ON THE SLOT VANE I/B END, 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.
Part: SKIN — DAMAGED (WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES IN REPAIR STRAP ON THE O/B SLOT VANE AT STA XS 520.168, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM.
Part: FITTING — CRACKED (L36L-L35L FS1690) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE AFT ACC SUPPORT FITTING AT STA 1690 BETWEEN L36L TO 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 51-1-21 & 53-2-5 & 51-1-20D.
Part: LONGERON — CRACKED (L24L UPPER MILL) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK IN UPPER MIL STOP APPROX 1/4" LONG AT LONGERON 24L, 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 E.O.#01-024 WITH APPROVED 8110-3 DATED 01/29/01.
Part: FORMER — CRACKED (XS 442.185) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 442.185, 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 57-2-0.
Part: FITTING — GOUGED (STA 5) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A GOUGE ABOVE THE L/H FLAP TRACK FITTING & MILL STOP AT STA 5, 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 AND E.O.#01-024 WITH APPROVED 8110-3 DATED 01/29/01.
Part: SKIN — CORRODED (Y-66 Z-11 X-12) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND POPPED RIVETS BETWEEN FRAMES -12 & -32 R/H O/B EDGE OF COCKPIT FLOOR X-12 TO -32 Y-66" Z-11, 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 E.O.#01-024 WITH APPROVED 8110-3 DATED 01/31/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: DOUBLER — CRACKED (XFS 195) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK ABOUT 3" AT T/E ON THE BOTTOM DOUBLER AT STA XFS 195, 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 AND 51-1-4.
Part: SKIN — DAMAGED (WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED SCREW HOLES TO THE SKIN AT STA 304, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-1.
Part: FITTING — CRACKED (XRS 428) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER I/B ATTACH FITTING ON THE L/H UPPER INSIDE TANK OF 506A O/B AT STA XRS 428, 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 E.O.#01-024 WITH APPROVED 8110-3 DATED 02/06/01 AND DC-8 SRM 51-1-20 & MM27-51-12.
Part: STRINGER — CRACKED (STA XRS 495-508) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CAN'T #55 LOWER STRINGER ON THE L/H UPPER WING INSIDE TANK OF 505B O/B BETWEEN STA XRS 495 & 508, 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 E.O.#01-024 WITH APPROVED 8110-3 DATED 01/31/01.
Part: STRINGER — CRACKED (STR 51 XRS 429) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CLIP ON STR #51 L/H UPPER INSIDE TANK OF 506A O/B BETWEEN STA XRS 428 LWR STRINGER CLIP BETWEEN LWR REAR SPAR, 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 E.O.#01-024 WITH APPROVED 8110-3 DATED 02/06/01.
Part: PANEL — DAMAGED (WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE BOTTOM SLOT PANEL, 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 51-1-4.
Part: FORMER — CRACKED (XFS 366.500) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 366.500, 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 57-2-0.
Part: FORMER — CRACKED (STA 316.500) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA 316.500, 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 57-2-0.
Part: SKIN — DAMAGED (WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED SCREW HOLES AT STA XS 520.166, 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.
Part: FORMER — CRACKED (XS 461.372) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 461.372, 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 57-2-0.
Part: FORMER — CRACKED (XS 448.581) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 448.581, 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 57-2-0.
Part: FORMER — CRACKED (XFS 329) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 329, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PARTS AND INSTALLED IAW DC-8 SRM 57-2-0.
Part: FORMER — CRACKED (XS 478.897) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 478.897, 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 57-2-0.
Part: STRINGER — CRACKED (XRS 495-508) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE CAN'T #54 STRINGER AT L/H UPPER INSIDE TANK OF 505B BETWEEN STA XRS 495-508, 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 E.O.#01-024 WITH APPROVED 8110-3 DATED 01/31/01.
Part: SKIN — CORRODED (XFS 422.720-335.) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON INTERNAL SKIN AT TOP DE-ICER VENT HOLES AT STA 422.750 TO XFS 335.250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. ----------CX----------
Part: FORMER — CRACKED (XFS 653.750) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 653.750, 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 SRM 57-2-0.
Part: FORMER — CRACKED (XFS 826.750) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM T/E FORMER AT STA XFS 828.750, 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 SRM 57-2-0 & 51-1-21.
Part: FORMER — CRACKED (XFS 385.250) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM T/E FORMER AT STA XFS 385.250, 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 57-2-0.
Part: FORMER — CRACKED (STA XFS 772.500) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 772.500, 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 57-2-0 & 51-1-21.
Part: INTERCOSTAL — CRACKED (XFS 335.250) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL AT STA XFS 335.250, 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 57-2-0.
Part: FORMER — CHAFED (WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND THE DE-ICER DUCT CHAFED DEEP INTO FORMER AT STA XFS 416, 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 57-2-0 & 51-1-20D.
Part: ANGLE — CRACKED (XFS 427) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE ANGLE AT FORMER AT STA XFS 427, 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 & 51-3-0.
Part: DOUBLER — CRACKED (WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM DOUBLER ABOUT 20 INCHES INSIDE L/E AT STA XFS 427, 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 51-1-4 &57-2-0 &51-1-20D.
Part: FORMER — CRACKED (STA XFS 304.000) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM T/E FORMER AT STA XFS 304.000, 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 57-2-0.
Part: FORMER — CRACKED (STA XFS 835) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 835, 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.
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 420 X=0, 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 53-2-3 FIG.8A.
Part: FORMER — CRACKED (TOP T/E XFS 735) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 735, 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 57-2-0
Part: FORMER — CRACKED (STA XS 442.185) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 442.185, 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 57-2-0 & 51-1-21 & 51-1-20D.
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 320-340 X=0, 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 53-2-3 FIG.8A.
Part: FORMER — CRACKED (TOP T/E XFS 797.) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 797.500, 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 57-2-0.
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A WORN SEAT TRACK AT STA 857-879 X=0, 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 53-2-3 FIG8A.
Part: FORMER — CRACKED (STA XS 454.976) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 454.976, 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 57-2-0 & 51-1-21 & 51-1-20D.
Part: FORMER — CRACKED (STA XFS 372.750) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 372.750, 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 57-2-0.
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 940-960 X-49, 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 53-2-3 & 53-2-3 FIG.8A.
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 859-879 X-49, 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 53-2-3 FIG.8A.
Part: FORMER — CRACKED (XS 461.372) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 461.372, 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 57-2-0 & 51-1-21 & 51-1-20D.
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 320-340 X=+20, 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 53-2-3 & 53-2-3 FIG.8A.
Part: FORMER — CRACKED (XS 467.323) · airframe 87,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 467.323, 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 57-2-0 & 51-1-21 & 51-1-20D.
Part: FORMER — CRACKED (STA XFS 297.500) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 297.500, 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 57-2-0.
Part: FORMER — CRACKED (XS 478.897) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XS 478.897, 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 57-2-0 & 51-1-21 & 51-1-20D.
Part: FORMER — CRACKED (STA XFS 304.000) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE TOP T/E FORMER AT STA XFS 304.000, 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 57-2-0.
Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED LOCK HOLES TO THE FO'S RT AFT SEAT TRACK, 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 53-2-3 AND DC-8 SRM 51-1-20D.
Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED LOCK HOLES TO THE CAPT'S RT AFT SEAT TRACK, 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.
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 140-160 X+45, 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 53-2-3 FIG. 14.
Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED LOCK HOLES TO THE CAPT'S LT AFT SEAT TRACK, 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.
Part: SKIN — DENTED (O/B END) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A DENT AT O/B END OF THE L/E WITH BODY PUTTY INSTALLED, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. ----------CX---------- (WITHIN LIMITS)
Part: SKIN — CORRODED (STA 23.750) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE I/B END AT STA XFS 23.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. -----------------CX--------------(WITHIN LIMITS)
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 1040 X+46", 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 53-2-3 FIG.8A.
Part: SEAT TRACK — WORN (COCKPIT) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND DEEP WEAR TO THE FO'S RT FWD SEAT TRACK, 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.
Part: SEAT TRACK — DAMAGED (COCKPIT) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE FO'S LT AFT SEAT TRACK, 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 53-2-3 AND DC-8 SRM 51-1-20D.
Part: SEAT TRACK — WORN (COCKPIT) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND DEEP WEAR AREAS TO THE CAPT'S RT FWD SEAT TRACK, 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 AND DC-8 SRM 53-2-3.
Part: SKIN — DAMAGED (WING) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND AN ELONGATED SCREW HOLE TO THE TOP T/E, 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 57-2-1.
Part: SKIN — CORRODED (L31L-L29L FS1080) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN BETWEEN STA 1080-1100 BETWEEN L31L TO L29L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. ---------------CX--------------- (WITHIN LIMITS)
Part: INTERCOSTAL — CRACKED (XFS 163.750) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL AT STA XFS 163.750, 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.
Part: SEAT TRACK — WORN (COCKPIT) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND DEEP WEAR TO THE FO'S LT FWD SEAT TRACK, 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.
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 140-160 X=0, 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 AND DC-8 SRM 53-2-3 FIG. 14.
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 140-160 X-24, 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 51-2-3.
Part: SPOILER PANEL — TORN (I/B END #5 SPOIL) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A TEAR TO THE I/B END OF RT WING O/B FLIGHT SPOILER LWR EDGE TRIM, 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.
Part: SEAT TRACK — CRACKED (X-45" FS 120-140) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 120-140 X-45", 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.
Part: SKIN — CORRODED (L36 FS 1160-1140) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN & DOUBLER AT STA 1160-1140 L36, DAMAGE EXCEEDED LIMITATIONS IAW SC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-024 WITH APPROVED 8110-3 DATED 02/02/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SKIN — CORRODED (L36 FS 1160-1170) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMGE INSIDE LIGHT HOLE TO THE SKIN AND DOUBLER AT STA 11160-1170 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 E.O.#01-024 WITH APPROVED 8110-3 DATED 02/02/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SKIN — CORRODED (L35L FS1160-1170) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN AND DOUBLER AT STA 1160 TO 1170 L35L, 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 E.O.#01-024 WITH APPROVED 8110-3 DATED 02/02/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 140-160 X+-45, 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 53-2-3 FIG. 14.
Part: SKIN — CORRODED (RBL 3 1/2" FS940) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN R/H AFT FILLET AREA BETWEEN STA 1100-1080 L29R TO L31R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. ---------------CX--------------- (WITHIN LIMITS)
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 70 X+45, 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 53-2-3 FIG.14 AND DC-8 SRM 51-3-0.
Part: SEAT TRACK — WORN (FUSELAGE) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND EXCESSIVE WEAR TO THE SEAT TRACK AT STA 240-260 X-59, 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 53-2-3 FIG. 14.
Part: SKIN — CORRODED (L35L FS1160-1170) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE SKIN AND DOUBLER AT STA 1160-1170 L35L, 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 E.O#01-024 WITH APPROVED 8110-3 DATED 02/02/01. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: ANGLE — CRACKED (RBL 3 1/2" FS940) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE R/H RIB ATTACH ANGLE KEEP BEAM BETWEEN MAIN GEAR DOORS AT STA 940 RBL 3 1/2", 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 & 51-1-4.
Earlier reports · 1995–2000 · 49 reports
2000
Part: SKIN — DAMAGED (CARGO DOOR) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND SHEET METAL DAMAGE AFT CENTER OF THE "C" PIT DOOR, DAMAGE EXCEEDED LIMITATIONS IAAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR PER EO 00-306.
Part: STRUCTURE — DAMAGED (RT ELEVATOR) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND DAMAGE TO THE SHEET METAL ON THE O/B T/E OF THE RT ELEVATOR, 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 EO 00-306.
Part: STRUCTURE — DAMAGED (RT ELEVATOR) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND SHEET METAL DAMAGE TO O/B T/E OF THE RT ELEVATOR, 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 51-1-21 AND EO #00-306.
Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 83,975 hrs · 32,127 cycles
MAIN CARGO DECK FLOOR CRACKED AT POSITION NR 7. CUT, FITTED AND INSTALLED NEW FLOOR PANE IAW DC-8 M/M CHAPTER 51-1-21.
Part: ENGINE — FLAMED OUT (NR 4) · airframe 83,674 hrs · 31,957 cycles
NR 4 ENGINE FLAME OUT ON T/O MMMX. ON ENGINFLIGHT START CHECKLIST NR 4 ENG LIT OFF & STAGNATED AT APPROX 320DEG C. THEN FAMED OUT AGAIN. PERFORMED INFLIGHT SHUTDOWN CHECKLIST. NR 4 ENG. R&R'D BY G.E. ON-WING IAW MM 71-00-42. ENG. CHECKED GOOD , OPS. CHECKED IAW FUNCTIONAL TEST RUN MM71-00-00. ALL PARAMETERS NORMAL AT ALL POWER SETTINGS IAW EWA AIRCRAFT MM CHPT. 12. NO DEFECTS NOTED.
Part: STRINGER — CORRODED (XCW +46 TO +69.5) · airframe 84,374 hrs · 32,353 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE INSIDE L/H CENTER TANK THRU MID SPAR ACCESS HOLE 560E STRINGER #76 BETWEEN STA XCW +46 TO XCW +69.5, 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 E.O.#01-024 WITH APPROVED 8110-3 DATED 01-30-01 AND DC-8 SRM 53-2-0 FIG.1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
1999
Part: RELAY — MALFUNCTIONED (E/E BAY)
NO SPOILER PRESSURE WHEN GEAR EXTENDED OR SPOILER SW HELD IN OVERRIDE. WHEN SPOILER PUMP SWITCH WAS PLACED TO OVERRIDE A STRONG ODOR LIKE ELECTRICAL WIRING OVERHEATING WAS NOTICED. REMOVED AND REPLACED RELAY R2-217. SPOILER SYSTEM OP CHECKS NORMAL ON GROUND FUNCTION TEST. NO DEFECT NOTICED.
Part: INTERCOSTAL — CORRODED (WS 129)
DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, INTERCOSTAL TOP CUP BETWEEN LEFT WING NR 2 AND NR 3 SPOILERS AT STA XW 129. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW DC8 SRM 57-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SPAR — CORRODED (WS 485 & 710)
DURING A MAINTENANCE VISIT FOUND CORROSION, LEFT WING, O/B L/E O/B SECTION UPPER SURFACE 17 FWD OF FRONT SPAR BETWEEN STA XFS 710 AND STA XW 485. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. LIMITATIONS EXCEEDED SRM LIMITATIONS, FAA APPROVED TENNESSEE TECHNICAL SERVICES DER ENGINEERING SKETCH NR 99-57-03251 APPROVES ADDITIONAL LIMITATIONS THAT EXCEEDED SRM LIMITS. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FITTING — CORRODED (BS 55)
DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON FITTING AT STA 55, LONGERON 32 RIGHT AT FWD PRODUCTION SPLICE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC8 SRM 51-1-21 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: WEB — CORRODED (BS 860)
DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, RT OUTBOARD PRESSURE BOX RT W/W LOWER L ANGLE AND WEB AT STA 860, LONGERON 24 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED L ANGLE AND WEB IAW DC8 SRM 51-1-4 AND 51-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SKIN — CORRODED (RT WING)
DURING A MAINTENANCE VISIT, FOUND CORROSION, RIGHT WING, AROUND SCREW HOLD RIGHT WING I/B L/E UPPER SURFACE AT XFS 20. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER IAW DC8 SRM 57-2-1 FIG 37 AND INSTALLED IAW DC8 SRM 57-2-1 FIT 37, 51-1-21, 51-1-20D AND 51-1-11. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FITTING — CORRODED (BS 1690 & 1700)
DURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, LONGERON 24 RIGHT BETWEEN STA 1690 AND STA 1700. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW FITTING AND INSTALLED IAW DC8 SRM 51-1-21 AND 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: NUT — CORRODED (BS 35 & 55)
DURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, UNDER DOME NUTS BETWEEN STA 55 AND STA 35, LONGERON 30 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED TENNESSEE TECH DER ENGINEERING SKETCH NR EO- 99-53-0327-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SEAT TRACK — WORN (BS 1580)
DURING A MAINTENANCE VISIT, FOUND WEAR, FUSELAGE, MAIN CARGO COMPARTMENT NR 17 SEAT TRACK ROW NR 2 WORN STA 1580 APPROX. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW AND INSTALLED CHANNEL AND PLUG IAW DC8 SRM 53-2-3 FIG 6D.
Part: SEAT TRACK — WORN (BS 1600)
DURING A MAINTENANCE VISIT, FOUND WEAR, FUSELAGE, MAIN CARGO COMPT NR 17 SEAT TRACK WORN AT STA 1600. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW CHANNEL AND PLUG AND INSTALLED IAW DC8 SRM 53-2-3 FIG 6D.
Part: FRAME — DAMAGED (BS 1580)
DURING A MAINTENANCE VISIT, FOUND DAMAGE, FUSELAGE, FRAME AT STA 1580 RT DAMAGED AT UPPER CUSP LINE. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED DOUBLER, FILLERS AND SPLICE AND INSTALLED IAW DC8 SRM 53-2-0 FIG 2, 51-1-20D.
Part: FLOOR PANEL — CORRODED (BS 460 - 540)
DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FLOOR PANEL, CARGO COMPARTMENT NR 5 BETWEEN STA 460 AND STA 540 AT BL 20 RIGHT, WL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PANEL IAW DC8 SRM 53-2-3, 51-3-0, 51-1-11. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FASTENER — SHEARED (WS 58)
DURING A MAINTENANCE VISIT, FOUND SHEARED, WING, HI-LOCK SHEARED IN SKATE ANGLE NR 4 ALT TANK 508 CONT AT STA 58. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED IAW FAA APPROVED TENNESSEE TECH DER ENGINEERING SKETCH NR EO-99-060.
Part: ANGLE — CORRODED (BS 1540)
DURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, FRAME TO MEMBRANE ATTACH ANGLE AT STA 1540 LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW AND INSTALLED ATTACH ANGLE IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FLOOR PANEL — CORRODED (BS 55 - 70)
DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LAVATORY FLOOR AND SHROUD CONNECTED AT LOCATION BETWEEN STA 55 AND STA 70 AND BETWEEN BL 60 RIGHT AND BL 40 RIGHT AT WL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOOR SECTION AND SHROUD IAW DC8 SRM 53-2-3 AND M/M 25-40-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SKIN — CORRODED (WS 11.25 - 194)
DURING A MAINTENANCE VISIT FOUND CORROSION, RIGHT WING, I/B LEADING EDGE BETWEEN STA XFS 11.25 AND XFS 194. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC8 SRM 51-1-21, 51-1-20D, 57-2-4 FIG 37 AND 51-1-11. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SKIN — CORRODED (WS 178 - 230.5)
DURING A MAINTENANCE VISIT FOUND CORROSION, WING, AROUND SCREW HOLES RIGHT WING OUTBOARD FLAP INBOARD SEGMENT UPPER SURFACE BETWEEN STA XRS 230.500 AND STA XRS 178.000. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER AND FILLER IAW DC8 SRM 51-1-21 AND 57-2-1 FIG 2Q. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FRAME — CRACKED (FUSELAGE)
DURING A MAINTENANCE VISIT, FOUND CRACK, R-2 DOOR, FWD LOWER CORNER FRAME. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR DOUBLER AND INSTALLED IAW DC8 SRM 51-3-0, 51-1-20, 51-1-21.
Part: FLOOR PANEL — CORRODED (BS 863)
DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, MAIN CARGO COMPT NR 9 FLOOR PANEL AT STA 863, BL 46 LEFT, WL 0. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FLOOR PANEL IAW DC8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: LONGERON — CORRODED (BS 240)
DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, LONGERON 30 RIGHT AT STA 240. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED LONGERON SECTION IAW DC8 SRM 51-1-20D AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FRAME — CORRODED (BS 1340)
DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, AT STA 1340 BETWEEN LONGERONS 35 RIGHT AND LONGERON 36. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FRAME SECTION AND REPAIR PARTS IAW DC8 SRM 53-2-0 FIG 2 AND 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: CHANNEL — CORRODED (BS 1206 - 1380)
DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CTR FLOOR ATTACH CHANNEL BETWEEN STA 1260 AND STA 1380 AT LONGERON 33 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC8 SRM 53-2-0 FIG 2E/2F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: CHANNEL — CORRODED (BS 1260 - 1380)
DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CTR FLOOR ATTACH CHANNEL BETWEEN STA 1260 AND STA 1380 AT LONGERON 33 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED CENTER FLOOR ATTACH CHANNEL IAW DC8 SRM 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FRAME — CORRODED (BS 1110)
DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, FRAME, AT STA 1110, LONGERON 29 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING AND WEB IAW DC8 SRM 51-3-0, 51-1-20D, AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: INTERCOSTAL — CORRODED (BS 1380 - 1400)
DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, INTERCOSTAL BETWEEN STA 1380 AND STA 1400 AT LONGERON 34 LEFT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED INTERCOSTAL IAW DC8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
1998
Part: VERT GYRO — FAILED (NR 2)
F/O'S HORIZON SHOWS INTERMITTENT GYRO AND FLIGHT DIRECTOR FLAGS IN VIEW AND DIFFERS 5-20 DEG NOSE UP. REMOVED AND REPLACED NR 2 VERTICAL GYRO, SYSTEM OPS CHECKS GOOD IAW DC-8 M/M.
Part: SEAL — CUT (NR 3 ENGINE)
DURING CLIMBOUT LOST OIL QUANTITY ON NR 3 WITH OIL PRESSURE FLUCTUATING. PUT NR 3 THROTTLE TO IDLE, AFTER 2 MINUTES LOW OIL PRESSURE LIGHT ILLUMINATED. ACCOMPLISHED INFLIGHT SHUTDOWN CHECKLIST. ON GROUND CHK FOUND STARTER CASE SEAL LEAKS. REMOVED STARTER AND REPLACED CUT CASE SEAL. REPLACED AND SERVICED STARTER, GRD RUN, NO LEAKS. NOTE CHECKED ENG FINGER SCREENS (4) OK. REPLACED SCREEN, NO LEAKS.
Part: SKIN — DAMAGED (WS 3-13)
WHILE AIRCRAFT SAT ON GROUND AT KMCN, JET BLAST FROM OTHER AIRCRAFT BLOW PASSENGERS STAIR INTO LT WING LEADING EDGE. PASSENGERS STAIR DAMAGED LT WING LEADING EDGE AT STA XFS=13 TO 3.0. REMOVED DAMAGED SECTION FROM LEADING EDGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM CHAPTER 57. REPAIRED LT WING LEADING EDGE IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH D76-R01 AND DC-8 SRM 51-1-12 AND 51-1-21.
1997
Part: SKIN — CRACKED (WS 172)
DURING SERVICE CHECK, FOUND FUEL LEAK UNDER LIFT WING. INSPECTED LIFT WING SKIN FOUND 1.75 INCH CRACK AT XWC 172. FERRIED AIRCRAFT TO AEROCORP (KMCN) IAW FAA APPROVED DER (VIA DIRECT) FOR REPAIR.
Part: O-RING — FAILED (LT MLG SWIVEL)
LOSS OF HYDRAULIC FLUID DOWN TO 4.5 GAL IN CRUISE. INSTALLED SERVICEABLE O-RING PACKING ON LT MLG SWIVEL ASSY, LEAK CHECK GOOD. SERVICE HYD RES TO PROPER LIMIT. U/C TAIL NUMBER CHANGE.
Part: HYD LINE — FAILED (LANDING GEAR)
AIR TURNBACK, LOSS OF HYDRAULIC FLUID AND PRESSURE AFTER T/O AND GEAR RETRACTION. RETURNED TO MMGL. REMOVED AND REPLACED BOGIE TRIM FLEXIBLE LINE. REPLENISHED HYD SYSTEM TO PROPER LEVEL, LEAKS CHECK GOOD.
Part: ACTUATOR — FAILED (LT MLG)
ON GEAR RETRACTION, A LOUD BANG WAS HEARD, GEAR UNSAFE LIGHT ON. MAINTENANCE INSPECTED AND FOUND LEFT MAIN GEAR LOWER RETRACT PIN BROKEN. AIRCRAFT APPROVED FOR FERRY FLIGHT TO MCN FOR REPAIR. MAINTENANCE REMOVED AND REPLACED THE LT MAIN LANDING GEAR RETRACT CYLINDER. OPS AND LEAK CHECK GOOD IAW DC8 MM 32-32-2. PERFORMED GEAR SWING OPS AND LEAK CHECK IAW DC8 MM 32-30-0.
Part: DRAG ANGLE — DAMAGED (NR 4 PYLON)
DURING MAINTENANCE VISIT, FOUND DRAG ANGLE (P/N 5803961-502) WITH SHEARED RIVETS AND DAMAGE, AT NR 4 PYLON XW=467 AND STRINGER 63. FABRICATED AND INSTALLED 7075T-6AL BUSHINGS IN STRINGER, WING SKIN, WING DOUBLER T-DOUBLER AND 17-7PH TH-170 BUSHING IN DRAG ANGLE. ALSO, ADDED 17-7PH TH-170 STRAP ON DRAG ANGLE FOR REINFORCEMENT. ALL WORK PERFORMED IAW APPROVED FAA-DER REO-02621.
Part: BEAM — CORRODED (BS 320)
DURING A-MAINTENANCE VISIT, FOUND CORROSION DAMAGE ON BEAM (P/N 9779445) IN FORWARD CARGO COMPARTMENT, AT Y=320. ALSO, STRAP INSTALLED ON LWR HORIZONAL LEG OF BEAM HAD TO BE CUT OUT TO CLEAN-UP ALL CORROSION ON BEAM. TIMCO REO-02608 INSTALLED REPAIR ANGLE AS REINFORCEMENT FOR THINNER AREA ON BEAM DUE TO CORROSION BLEND-OUT. ALSO, REO-02608 REINSTALLED A NEW STRAP AS REPLACEMENT FOR REMOVED STRAP, SPLICE PLATE WAS USED FOR REATTACHMENT TO EXISTIG STRAP, IAW APPROVED FAA-DER REO-02608.
Part: JAMB FRAME — CORRODED (BS 1170)
DURING C-CHECK, FOUND CORROSION DAMAGE ON JAMB FRAME (P/N 5750195) IN AFT CARGO COMPARTMENT BASKET DOOR AT Y= 1170 AND LONGERON 36. DAMAGE WAS REMOVED AND TRIMMED OUT. FABRICATED FILLER FROM 7075 AND REINFORCEMENT ANGLE FROM .080 7075-0, HEAT-TREATED TO T-6 AND INSTALLED ON FRAME. ALL WORK ACCOMPLISHED IAW TIMCO REO-02576 AND FAA-DER APPROVED IAW 8110-3 FORM (CFG-01233).
Part: FITTING — CORRODED (BS 1445)
DURING A-MAINTENANCE VISIT, FOUND SEPARATOR NET SUPPORT FITTING (P/N 5711283-514) DAMAGED BEYOND ECONOMICAL REPAIR. REPLACEMENT PART UNAVAILABLE, BLANK FORGING UNAVAILABLE. TIMCO REO-02606 PROVIDES AUTHORITY TO FABRICATE NEW FITTING IAW DOUGLAS DRAWING NR 5711283. EXCEPT SUBSTITUTE FORGING (P/N 4710626-2) WITH 7075-T6511 EXTRUDED BAR STOCK GRAIN LGWISE.
Part: DOUBLER — CRACKED (WS 297)
DURING MAINTENANCE VISIT, FOUND LT WING LEADING EDGE INTERNAL DOUBLER (P/N 5641252-1) WITH 2 EACH CRACKS, AT XW= 297. REPAIRED BY FABRICATING AND INSTALLING EXTERNAL REPAIR DOUBLER IAW APPROVED FAA-DER REO-02560.
Part: JAMB FRAME — CORRODED (BS 333)
DURING MAINTENANCE VISIT, FOUND DOOR JAMB (P/N 9779454) CORRODED PAST LIMITATIONS IAW DC-8 SRM, AT Y=333 AND BETWEEN LONGERONS L35L TO L35R. FABRICATED AND INSTALLED FILLER FROM 7075, 2 EACH REINFORCEMENT ANGLES FROM .080 7075T-0 HEAT-TREATED TO T-6. ALL WORK ACCOMPLISHED IAW FAA-DER APPROVED REO-02575.
Part: SKIN — DENTED (RT TE FLAP)
DURING MAINTENANCE VISIT, FOUND DENT PAST LIMITATIONS IAW DC-8 SRM ON RT WING I/B FLAP, AT UPPER SURFACE XW=107. FABRICATED AND INSTALLED DOUBLER REPAIR IAW APPRROVED FAA-DER REO-02591.
Part: SKIN — DENTED (WS 725)
DURING A-MAINTENANCE VISIT, FOUND DENT ON LT WING O/B NOSE SKIN AILERON (P/N 5763133-75), LWR SURFACE, AT XA=725. DAMAGE ROUTED OUT, FABRICATED FILLER AND REINFORCING DOUBLER, INSTALLED ON AILERON NOSE SKIN IAW APPROVED FAA-DER REO-02590.
Part: SKIN — WORN (RT LE FLAP)
DURING A-MAINTENANCE VISIT, FOUND RT WING O/B FLAP LEADING EDGE ASSEMBLY (P/N 5655752-345) WAS CHAFED AND WORN UNDER RIB STRIP, AT XF=244.263. DAMAGE ROUTED OUT IN 2 EACH PLACES, FABRICATED AND INSTALLED FILLERS AND REINFORCING INTERNAL DOUBLER ADDED ON LEADING EDGE, ATTACHED WITH HL 329-6 HI-LOK FASTENERS. ALL WORK ACCOMPLISHED IAW APPROVED FAA-DER REO-02594.
Part: SKIN — DENTED (WS 750)
DURING A-MAINTENANCE VISIT, FOUND LT WING LWR SKIN CREASED AND DENTED PAST LIMITATIONS IAW DC-8 SRM, AT XRS=750 BETWEEN STRINGER 53 AND REAR SPAR. FABRICATED AND INSTALLED DOUBLER REPAIR FROM 7075T-6 IAW APPROVED FAA-DER REO-02582.
1995
Part: ENGINE — MALFUNCTIONED (NR 1)
FLT NR 137 - CYYZ-KDAY - NR 1 ENGINE UNSPOOLED IN FLIGHT. MAINTENANCE THOROUGHLY INSPECTED THE NR 1 ENGINE INLET AND EXHAUST AND FOUND NO DAMAGE. FUEL QUANTITY INDICATIONS MATCHED BETWEEN THE INDICATOR AND DRIPSTICKS. MAINTENANCE PERFORMED A POWER ASSURANCE RUN IAW THE EWA RUN UP HANDBOOK. NO DEFECTS NOTED, AIRCRAFT RETURNED TO SERVICE. (M)