N995CF
Registered owner: SKYBUS JET CARGO INC, NV (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| EMERY WORLDWIDE AIRLINES | Operator | on 1999-12-17 | Operator named in NTSB report |
Accident & incident history
Operated by EMERY WORLDWIDE AIRLINES (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.
505 reports on file, 1995-12-21 – 2000-08-04.
Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 64,088 hrs · 20,516 cycles
AUTO PRESSURIZATION FAILED SHORTLY AFTER TAKEOFF, DURING MANUAL CONTROL THROUGH FL 290 CABIN CLIMBED UNCONTROLLABLY AT 2000 FPM. DEFERRED PER MEL 21-10 CAT C. DMI CNTL NR C9037012-7913 DUE 8-14-00. PLACARD INSTALLED.
Part: WARNING LIGHT — ILLUMINATED (NR 2 ENGINE) · airframe 63,993 hrs · 20,472 cycles
ON CLIMBOUT (APPROX 5,000 FEET) NR 2 ENGINE FIRE WARNING/MASTER CAUTION ILLUMINATION/AURAL WARNING. SHUTDOWN NR 2 ENGINE, DISCHARGED BOTH FIRE BOTTLES.
Part: DOWNLOCK SWITCH — INOPERATIVE (NLG) · airframe 63,989 hrs · 20,468 cycles
NR 2 DURING MANUAL EXTENSION CHECKS 0 HYD PRESS. NO NOSE GEAR GREEN LIGHT AND BOTH GEAR NOT LATCHED LT AND GEAR DOOR (RED) LIGHTS STAYED ON. CYCLED GEAR SEVERAL TIMES, NO HELP. RAN EMERGENCY CHECK LIST. RETURNED TO AIRPORT. REMOVED AND REPLACED NLG DOWNLOCK INDICATING SWITCH IAW DC-8 MM 32-60-0, OPS CHECKS GOOD IAW DC-8 MM 32-60-0, GEAR SWING GOOD IAW DC-8 MM 32-30-0.
Part: SKIN — CRACKED (ENGINE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK IN WELD 3 O CLOCK POSITION INSIDE THRUST REV AFT OF BUCKET, 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 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 6-3-00.
Part: COVER — DAMAGED (CARGO DOOR) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND TEMPORARY REPAIRS DONE TO THE CROSS SLIDE COVER ON B PIT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOOR COVER IAW DC-8 SRM 51-3-0 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 5-3-00.
Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES IN THE FLOOR PLANK NR 2 STA 233 TO 315, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. PLUGGED HOLES IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 5-16-00.
Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES TO THE MAIN CABIN FLOOR PLANK ROW 8 AT STA 1240 - 1460, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: SPOILER PANEL — DELAMINATED (NR 1 SPOILER) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE NR 1 GROUND SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED SPOILER IAW MM 27-61-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SPOILER PANEL — DELAMINATED (NR 3) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE NR 3 GROUND SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NR 3 PANEL IAW DC-8 MM 27-61-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND AN ELONGATED BOLT HOLE ON THE RIGHT O/B FLAP VANE NR 6, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED BUSHING IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 5-5-00.
Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SCREW HOLES ELONGATED AND BUSHINGS MISSING ON THE RIGHT WING RIGHT O/B FLAP VANE NR 5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED BUSHING PER EO NR 00-047 WITH APPROVED 8110-3 DATED 4-28-00.
Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES TO THE FLOOR PANEL AT STA 500 - 660 ROW 1 LT, 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 00-047 WITH APPROVED 8110-3 DATED 4-25-00.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A GOUGED SEAT TRACK AT FUSELAGE STA FS 425 XCW 22.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED DAMAGED AREA IAW DC-8 SRM 53-2-3 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 5-10-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES IN THE SEAT TRACK AT STA 1250 - 1460 AND XCW 47 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIRED SEAT TRACK IAW DC-8 SRM 53-2-3, FIG 12, EA NR 77-995CF, ROSEMBALM DRAWING NR 24300 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 6-1-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES TO THE FLOOR PANEL AT STA 800 - 1000, 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 00-047 WITH APPROVED 8110-3 DATED 4-25-00.
Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED END TO THE FLOOR PLANK AT STA 800 - 1020, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: PIN — CORRODED (LT MLG STRUT) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE MLG RETRACT PIN AND PIN BOSS SO MA-AI-3210-01:03 LT MLG RETRACT PIN AND BOSS PIN INSPECTION NEEDED C/W, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8S RM 51-1-8. FABRICATED AND INSTALLED NEW BUSHING AND RETRACT PIN IAW DO NR 00-047 WITH APPROVED 8110-3 DATED 5-10-00 AND MA-AI-3210-01:03. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SEAT TRACK — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES TO THE SEAT TRACK AT FS 1380 - 1400, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW TRACK IAW ROSENBALM DWG NR 24300 AND EA NR 77-995CF DATED 5-22-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE SEAT TRACK AT FS 1300 - 1380 XCW 59.5 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 5-7-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES TO THE NR 3 FLOOR PLANK AT STA 800 - 1000, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES TO THE FLOOR PLANK RT UPPER SKIN AT STA 1460 - 1606, 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 00-047 WITH APPROVED 8110-3 DATED 4-17-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND GOUGES AND MISDRILLED HOLES IN THE SEAT TRACK AT FS 1220 - 1260, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW TRACK IAW ROSENBALM DWG NR 24300 AND EA NR 77-995CF DATED 5-22-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES IN THE FLOOR PLANK AT STA 1240 TO 1460 ROW 10 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-17-00.
Part: SEAT TRACK — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED AND MISDRILLED HOLES TO THE SEAT TRACK AT FS 1360 - 1430, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW TRACK IAW ROSENBALM DWG NR 24300 AND EA NR 77-995CF DATED 5-22-00.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED SEAT TRACK AT FS 1540 - 1560 XCW 22 LT, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW TRACK IAW ROSENBALM DWG NR 24300 AND EA NR 77-995CF DATED 5-22-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE SEAT TRACK AT FS 440-XCW 0, 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 EA NR 77-995CF, ROSENBALM DRAWING NR 24300 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 5-7-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES IN THE SEAT TRACK AT FS 980 - XCW O, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED PART IAW ROSENBALM DWG NR 24300 AND EA NR 77-995CF DATED 5-22-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE SEAT TRACK AT FS 960 - 980 AND XCW 47 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW TRACK IAW DC-8 SRM 53-2-3, FIG 12, 51-1-3, ROSENBALM DWG NR 24300 AND EA NR 77-995CF DATED 5-22-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE SEAT TRACK AT FS 1400 - 1440 XCW 0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW TRACK IAW ROSENBALM DWG NR 24300 AND EA NR 77-995CF DATED 5-22-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES ON THE SEAT TRACK AT FS 1060-XCW 47 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW TRACK IAW EA NR 77-995CF DATED 5-22-00 AND ROSENBALM DWG NR 24300.
Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND HOLES ELONGATED AND CHAFED UNDERSIDE ON NR 5 FLOOR PANEL 320 - 620 ROW 4, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES IN THE SEAT TRACK AT FS 690 - 702, 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 EA NR 77-995CF, ROSENBALM DWG NR 24300 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 5-8-00.
Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND HOLES AND CRACKS TO THE FLOORBOARD AT FS 860 - 1000, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE SEAT TRACK AT FS 980 - 1125 XCW 57 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW TRACK IAW ROSENBALM DWG NR 24300 AND EA NR 77-995CF DATED 5-22-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE SEAT TRACK AT FS 1260 - 1380 XCW 22 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-3, FIG 12 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 5-7-00.
Part: SKIN — DENTED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND 2 DENTS BEHIND THE JACK PAD AT STA 280 BETWEEN L36L - L35L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED DENTED AREAS IAW DC-8 EO NR 00-047 WITH APPROVED 8110-3 DATED 5-23-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES IN THE SEAT TRACK AT FS 460-XCW 47 LT, 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 EO NR 77-995CF DATED 5-22-00 AND ROSENBALM DWG NR 24300.
Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CRACKED OUT FASTENER HOLES TO THE NR 7 FLOOR PANEL 320 - 620 FLOORBEAM ATTACH POINT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES IN THE SEAT TRACK AT FS 525 - XCW 22.5 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED TRACK IAW ROSEMBALM DWG NR 24300 AND EO NR 77-995CF DATED 5-22-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND GOUGED AND ELONGATED HOLES TO THE SEAT TRACK AT FS 925 - 962 XCW 47 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED NEW PART AND INSTALLED IAW DC-8 SRM 53-2-3, FIG 12, EA NR 77-995CF AND ROSENBALM DWG NR 24300.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE SEAT TRACK AT FS 1500 - 1560 XCW 0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW TRACK IAW EO NR 77-995CF DATED 5-22-00 AND ROSENBALM DWG NR 24300.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE SEAT TRACK AT FS 883 - XCW 47 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW TRACK IAW DC-8 SRM 51-3-0, ROSENBALM DWG NR 24300, EA NR 77-995CF AND EO NR 00-047 WITH APPROVED 8110-3 DATED 5-8-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE SEAT TRACK AT FS 822-849 XCW 57 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW TRACK IAW ROSENBALM DWG NR 24300 AND EA NR 77-995CF DATED 5-22-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE SEAT TRACK AT FS 1530 - 1560 XCW 22 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW TRACK IAW DC-8 SRM 53-2-0, FIG 12, EA NR 77-995CF, ROSENBALM DWG NR 24300 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 5-9-00.
Part: SCOOP — CRACKED (WHEEL WELL) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LEFT FWD W/W DRAIN SCOOP, 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 51-1-21, 51-3-0, 53-2-0 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-1-00.
Part: SCOOP — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT DRAIN SCOOP FWD OF MAIN W/W, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21, 53-2-0 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-1-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A HOLE DRILLED VERTICALLY FROM FLOORBEAM ON THE DOUBLER ON INTERCOSTAL AT STA 670 X-0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. INSTALLED OVERSIZED FASTENERS AND RETURNED TO SERVICE IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 5-19-00.
Part: SKIN — DAMAGED (LT WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND COUNTER SINKS FOR ATTACHMENT FASTENERS EXCEED SRM LIMITATIONS ON THE LEFT O/B LEADING EDGE I/B SEGMENT AT XFS 560 - 710, DAMAGE EXCEEDS LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED FASTENERS IAW DC-8 SRM 51-1-22 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 5-18-00.
Part: BRACKET — MISINSTALLED (LT WING TE FLAP) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND IMPROPERLY INSTALLED BRACKETS INSTALLED ON THE LEFT I/B FLAP I/B UPPER FLAP VANE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW VANE IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 5-17-00.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED FLOORBEAM SUPPORT ANGLE FR 1320 X+36 Z-8, 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-89 SRM 51-1-4, 51-1-21 AND 51-1-20D.
Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND LONGATED HOLES TO THE FLOOR PANEL AT STA 225 - 320, 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 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED FLOOR PANEL ON UNDERSIDE AT STA 225 - 320, 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 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES TO THE FLOOR PLANK AT STA 600 - 860, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOOR PANEL AT STA 225 - 420, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES TO THE FLOORBEAM TO PLANK ATTACH POINT, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED AND LONGATED HOLES TO THE NR 2 FLOOR PANEL AT STA 1000 - 1240, 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 00-047 WITH APPROVED 8110-3 DATED 4-25-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED AND ELONGATED HOLES IN THE CABIN FLOOR PLANK AT STA 1000 TO 1320 ROW 5 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. WELDED HOLES AND BLENDED IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES TO THE FLOOR PANEL AT STA 230 - 500, 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 00-047 WITH APPROVED 8110-3 DATED 4-25-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES TO THE CABIN FLOOR PANEL AT STA 215 - 320, 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 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND LONGATED HOLES IN THE FLOOR PANEL AT STA 1000 - 1240, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED HOLES IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED AND ELONGATED HOLES TO THE FLOOR PANEL AT STA 320 - 600, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FLOOR PANEL AT STA 1000 - 1240 ROW 12, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACK IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES TO THE FLOOR PANEL AT STA 1000 - 1400, 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 00-047 WITH APPROVED 8110-3 DATED 4-17-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOOR PLANK AT STA 235 - 660, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES IN THE FLOORBEAM AT STA 400 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES IN THE UPPER AND LOWER SIDE AT STA 660 - 880 LT, 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 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES TO THE FLOOR PANEL AT STA 1000 - 1240 ROW 4, 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 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES TO THE FLOOR PANEL NR 4 AT STA 235 - 320, 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 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES AND ELONGATED HOLES IN THE FLOOR PANEL AT STA 660 - 800, 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 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES ON THE FLOOR PANEL AT STA 860 - 1000 ROW 9, 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 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOOR PLANK AT STA 235 - 230, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOOR PLANK AT STA 225 - 320, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — DAMAGED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED AND ELONGATED HOLES TO THE FLOOR PLANK AT STA 800 TO 1000, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES ON THE FLOOR PANEL TO FLOORBEAM ATTACH FASTENER AT STA 1240 - 1460 ROW 12, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM AT THE UPPER CARGO COMPT FS 1480, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR STRAPS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES IN PLANK CHANNEL ON THE NR 4 FLOOR PANEL AT STA 1000 - 1320, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES TO THE FLOOR PLANK AT STA 660 - 860, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES TO THE FLOOR PLANK AT STA 1240 - 1460 ROW 6, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES TO THE NR 3 FLOOR PLANK AT STA 225 - 320, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES TO THE FLOOR PANEL AT STA 1000 - 1320, 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 00-047 WITH APPROVED 8110-3 DATED 4-25-00.
Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND LONGATED HOLES TO THE FLOOR PANEL AT STA 1000 - 1460 ROW 9 RT, 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 00-047 WITH APPROVED 8110-3 DATED 4-25-00.
Part: FLOORBOARD — CORRODED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND ELONGATED ATTACH FASTENER HOLES TO THE FLOOR PLANK TO FLOORBEAM ON NR 2 FLOOR PANEL AT STA 225 - 320, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-30-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOOR PLANKS AT FS 860 - 1000, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — TOOL DAMAGE (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND TOOLING MARKS GOUGED ON FLOOR PANEL AT STA 660 - 860, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-16-00.
Part: FLOORBOARD — GOUGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND DENTS AND GOUGES TO THE CENTER CHANNEL ON THE NR 2 FLOOR PLANK AT STA 800 - 1000 ROW 5, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES TO THE NR 2 FLOOR PANEL AT STA 320 - 620, 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 00-047 WITH APPROVED 8110-3 DATED 4-25-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES TO THE FLOOR PLANK AT STA 660 - 1000 ROW 7, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES TO THE FLOOR PANEL AT STA 1000 - 1460 ROW 3, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES TO THE NR 4 FLOOR PANEL AT STA 1000 - 1240 ROW 1 RT, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES TO THE FLOOR PANEL AT STA 800 - 1000, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES TO THE NR 4 FLOOR PANEL AT STA 1000 - 1460 ROW 7, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOOR PLANK AT FS 225, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — DAMAGED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED ATTACH POINT HOLES ON THE FLOORBEAM AT NR 1 FLOOR PLANK FS 420 TO 600, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-25-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES ON THE FLOOR PLANK AT STA 320 - 600 LT ROW 2, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES TO THE FLOOR PANEL AT STA 600 - 860, 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 00-047 WITH APPROVED 8110-3 DATED 4-17-00.
Part: FLOORBOARD — GOUGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND DENTS AND GOUGES TO THE NR 2 FLOOR PLANK CHANNEL AT STA 1000 - 1240, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — DAMAGED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES TO THE NR 3 FLOOR PANEL AT STA 320 - 660, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOOR PLANK AT STA 520 - 580, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES IN THE CABIN FLOOR PANEL AT STA 255 - 660, 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 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES TO THE FLOOR PANEL AT STA 660 - 860, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS MISDRILLED HOLES TO THE FLOOR PLANK AT STA 660 - 1000 ROW 6 LT, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES IN THE FLOOR PANEL AT STA 320 - 660, 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 00-047 WITH APPROVED 8110-3 DATED 4-25-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM AT STA 340 CUSP TO CUSP, 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 NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: FLOORBOARD — MISDRILLED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES TO THE NR 2 FLOOR PANEL AT STA 1000 - 1040 RT ROW 8, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES IN THE FLOOR PANEL AT STA 1460 - 1480 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. WELDED AND BLENDED HOLES IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES IN THE FLOOR PANEL AT STA 1460 TO 1500 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. WELDED HOLES IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES IN THE FLOORBEAM 1020 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED STRAPS/FILLERS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM AT FS 700, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOORBEAM IN THE UPPER CARGO COMPT AT FS 640, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED STRAPS/FILLERS AND INSTALLED IAW EO NR 00-0047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES IN THE FLOORBEAM AT STA 1420 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND DAMAGE IN 3 PLACES TO THE FLOOR PANEL ROW 7 AT STA 1580 - 1600 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED DAMAGE IAW DC-8 SRM 53-2-0 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES IN THE FLOOR PANEL AT STA 1580 - 1600 LT, 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 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM 1360 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW DC-8 SRM 51-1-4, 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM AT STA 580 CUSP TO CUSP, 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 NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBOARD — DAMAGED (CABIN) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED AND ELONGATED HOLES TO THE NR 2 FLOOR PANEL AT STA 1000 - 1320 RT, 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 00-047 WITH APPROVED 8110-3 DATED 4-25-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES TO THE FLOORBEAM SPLICE AT STA 740 X+20, 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 00-047 WITH APPROVED 8110-3 DATED 5-12-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOOR PLANK AT FS 1460 - 1580, 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 00-047 WITH APPROVED 8110-3 DATED 4-30-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM AT STA 380 CUSP TO CUSP, 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 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM AT STA 320 CUSP TO CUSP, 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 EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND ELONGATED HOLES IN THE FLOOR PANEL AT STA 1460 - 1580 LT, 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 00-047 WITH APPROVED 8110-3 DATED 4-16-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM AT THE UPPER CARGO COMPT FS 1500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED STRAPS AND FILLERS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM AT STA 520 CUSP TO CUSP, 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 EO NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM 1240 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-20D AND EO NR 00-047 WITH APROVED 8110-3 DATED 3-12-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED AND LONGATED HOLES IN THE FLOOR PANEL AT STA 420 - 620, 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 00-047 WITH APPROVED 8110-3 DATED 4-25-00.
Part: FLOORBOARD — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND DAMAGE IN 3 PLACES TO THE FLOOR PANEL AT STA 1580 - 1600 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBOARD — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES IN THE FLOOR PANEL ROW 7 AT STA 1580 - 1600 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. WELDED AND BLENDED HOLES IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-2-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM AT FS 960, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED HOLES IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOORBEAM AT FS 780, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED HOLES IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED AND DELAMINATED SCREW HOLES ON THE RIGHT O/B FLAP VANE NR 3 ON THE L/E OF THE VANE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NR 3 FLAP VANE IAW MM 27-51-14. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: VANE — DAMAGED (LT WING TE FLAP) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED ATTACHMENT HOLES AND T/E OF FLAP SEPARATING AT THE LT FLAP VANE AT STA 98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED PART IAW MM 27-51-14.
Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED AND DELAMINATED HOLES ON THE LEADING OF THE LEFT O/B FLAP VANE NR 6, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW MM 27-51-14. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SKIN — CRACKED (RAM AIR DUCT) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FASTENER HOLE ON THE LT CHIN SCOOP RAM AIR DUCT SKIN, 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 00-047 WITH APPROVED 8110-3 DATED 5-4-00.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT NEED TO COMPLY WITH MA AM-5310-01:00 EWA FRAME REPAIR AT FS 920 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. C/W MA-AM-5310-01:00 AND RECEIVED AND INSTALLED REPAIR IAAW DC-8 SRM 51-1-21 AND 51-1-20D.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK IN THE FLOOR SUPPORT ATTACHED TO FRAME AT STA 380 AND L30R, 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 00-047 WITH APPROVED 8110-3 DATED 5-9-00.
Part: LINK — GOUGED (LT WING TE FLAP) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A PORK CHOP GOUGE TO THE LEFT HAND WING O/B FLAP STA 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RETURNED TO SERVICE IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 5-5-00.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CRACKS IN THE FLOOR SUPPORT AT STA 440 BETWEEN L31R TO L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACKS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 5-9-00.
Part: FITTING — CHAFED (RT WING TE FLAP) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CHAFING AND A GOUGED T/E ON THE RIGHT I/B FLAP CANOE FITTING AT STA 68, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RETURNED TO SERVICE IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 5-1-00.
Part: PANEL — DAMAGED (LT WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND HOLES ELONGATED ON THE LT WING T/E LWR HINGED PANEL 577A MOUNT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. PANEL IS ACCEPTABLE AND RETURNED TO SERVICE IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 5-1-00.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A SEVERED FLOORBEAM AT FS 360-XCW 52.5 LT, 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 DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-13-00.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A SEVERED FLOORBEAM AT FS 340 AND XCW 52.5 LT, 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 NR 00-047 WITH APPROVED 8110-3 DATED 4-13-00.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A SEVERED FLOORBEAM AT FS 380-XCW 52.5 LT, 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 DC-8 SRM 51-1-4, 51-1-20D, 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-13-00.
Part: FLOORBEAM — GOUGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE UPPER CHORD FLOORBEAM AT STA 1400, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED GOUGES SMOOTH IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-26-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A SEVERED FLOORBEAM AT FS 400-XCW 52.5 LT, 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 DC-8 SRM 51-1-20D, 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-13-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM AT STA 500 CUSP TO 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 DC-8 SRM 51-1-21, 51-1-4, 51-1-20E AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: WEB — CORRODED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE, DOUBLE DRILLED HOLES, GOUGES AND MISSING NUT PLATES AT VARIOUS PLACES AT STA 225 TO 330 AND L21L TO L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED SUB-FLOOR PANEL AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-4 AND 51-1-20. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED INTERCOSTAL AT BOTH ENDS AT STA 1300 TO 1320 AND L4L, 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 DC-8 SRM 51-1-21 AND 51-1-4.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE KEEL BEAM AT STA 815 - 781 AND L35L, 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, 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-20-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SPAR — CRACKED (RT WING TE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A 2 INCH CRACK TO THE LWR AUX SPAR ANGLE IN RADIUS OF THE RIGHT T/E REAR AUX SPAR AT XRS 86, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTINGS IAW DC-8 SRM 51-3-0, 57-2-6, FIG 16 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-28-00.
Part: LONGERON — CORRODED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LONGERON 35L BETWEEN STA 1586 - 1568 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, 51-1-21, 51-1-20D AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-25-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SKIN — CRACKED (LT WING LE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CRACKS AT RIVETS ON THE LT WING O/B SLOT LEADING EDGE VANE AT STA XS 472 AND XS 478, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED RIVETS IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 5-5-00.
Part: SKIN — DAMAGED (LT WING LE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH SKIN ON THE LT WING O/B SLOT L/E VANE AT STA XFS 428 34 TO 48 INCHES FWD OF SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 57-20-5, 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-21-00.
Part: DUCT — CRACKED (RAM AIR) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED AND BLOWN OUT DE-ICE DUCT ON THE RT CHIN SCOOP, 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, 51-1-7 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-21-00.
Part: FITTING — CHAFED (RT WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CHAFING AT THE RT WING FLAP PORK CHOP FITTING AT STA 219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. ACCEPTABLE TO RETURN TO SERVICE PER EO NR 00-047 WITH APPROVED 8110-3 DATED 5-1-00.
Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISALIGNED HOLES ON THE NR 5 FLAP VANE, 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 00-047 WITH APPROVED 8110-3 DATED 4-28-00.
Part: VANE — MISALIGNED (TE FLAP) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A MISALIGNED HOLE FROM OVERHAUL ON THE NR4 MAIN FLAP VANE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SHIMS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-28-00.
Part: LONGERON — DENTED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A SMALL DENT AT FS 850 AND L9R, 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 DC-8 SRM 51-1-20D, 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-24-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM AT STA 270 CUSP TO CUSP, 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 NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOORBEAM IN THE UPPER CARGO COMPT AT FS 1460, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED STRAPS AND FILLERS AND INSTALLED IAW EO NR 00-0047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOORBEAM IN THE UPPER CARGO COMPT AT FS 1000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED HOLES IAW EO NR 00-0047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOORBEAM IN THE UPPER CARGO COMPT AT FS 660, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED STRAPS/FILLERS AND INSTALLED IAW DC-8 SRM 53-2-0 AND EO NR 00-0047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM 1180 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-20D AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES IN THE FLOORBEAM 1120 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SUPPORT IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES IN THE SEAT TRACK AT FS 520-XCW 0, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. WITHIN ALLOWABLE LIMITS IAW DC-8 SRM 53-2-3, FIG 12 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 5-7-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM AT STA 300 CUSP TO CUSP, 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 EO NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK ON LWR AFT LOBE OF FLOORBEAM AT FS 900 AND XCW 47 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 53-2-0, 51-1-20D AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-2-00.
Part: FRAME — GOUGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A GOUGE TO THE INTERIOR ANGULAR FRAME AT STA 1586 BETWEEN L19R AND L24R, 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 EO NR 00-047 WITH APPROVED 8110-3 DATED 4-27-00.
Part: PLATE — DAMAGED (FUEL TANK) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND AN ELONGATED SCREW HOLE ON THE NR 4 MAIN FUEL TANK LAND PANEL 505D, DAMAGE HAS EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. IT IS ACCEPTABLE TO RETURN TO SERVICE PER EO NR 00-047 WITH APPROVED 8110-3 DATED 4-24-00.
Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED FLOOR CHANNEL AT STA 580 XCW 60 INCHES LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW DC-8 SRM 51-1-20D AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-27-00.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED INTERCOSTAL AT STA 255 RT AND RBL 52.5 INCHES, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-4 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-25-00.
Part: SKIN — DAMAGED (LT WING LE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ATTACH SCREWS PULLING THROUGH SKIN AT LT WING O/B SLOT L/E VANE AT STA XFS 508.000 34 INCHES TO 48 INCHES FWD OF SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-21-00.
Part: SKIN — CRACKED (LT WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A POSSIBLE CRACK EMANATING FROM RIVET HOLE ON THE LT WING UPPER SURFACE AT STA 22.250 AT CENTER SPAR, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-14-00.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A HOLE DRILLED IN THE FRAME AT STA 1570 AND L16L TO L17L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-26-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A HOLE DRILLED THROUGH RADIUS IN WEB ON THE LONGITUDINAL FLOORBEAM AT STA 230 RT AND RBL 45.5, 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 00-047 WITH APPROVED 8110-3 DATED 4-24-00.
Part: FRAME — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND DRILLED HOLES IN THE FRAME AT STA 1400 LT AND L21L TO L19L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-24-00.
Part: VANE — DAMAGED (TE FLAP) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SCREW HOLE ELONGATED ON LEFT I/B FLAP NR 1, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-26-00.
Part: FRAME — TOOL DAMAGE (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND TOOLING MARK AT STA 1280 LT AND L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED TOOLING MARKS SMOOTH IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-24-00.
Part: SUPPORT FITTING — CRACKED (CARGO DOOR) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A WORN AND CRACKED MAIN CARGO DOOR CUTOUT UPPER SUPPORT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-24-00.
Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CENTER KEEL BEAM PANEL SUPPORT CLIP AT STA 880 AND L36L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SUPPORT CLIP IAW DC-8 SRM 51-1-20D AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CENTER KEEL BEAM CENTER PANEL SUPPORT CLIP AT STA 890 AND L36L, 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, 51-1-20D AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOORBEAM IN THE UPPER CARGO COMPT AT FS 600, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED STRAPS/FILLERS AND INSTALLED IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: PANEL — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CRACKED WELDS ON THE CUSP PANEL 1380 TO 1420, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. STOP DRILLED CRACKS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-1-00.
Part: WEB — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES IN THE MEMBRANE AT THE L1 DOOR AREA STA 270 - 225 LT AND L21L DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW MEMBRANE IAW DC-8 SRM 51-1-21 AND 51-1-4.
Part: FRAME — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND DRILLED HOLES IN THE FRAME AT STA 1380 AND L21L TO L19L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-27-00.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A HOLE IN THE FRAME AT FS 620 AND L7L, 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 51-1-20 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-24-00.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED FLOORBEAM ON LWR CUSP AT STA 225 AND L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW GUSSET IAW DC-8 SRM 51-1-21 AND 51-1-4.
Part: CHANNEL — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED FLOOR CHANNEL AT STA 225 RT AND RBL 55.5 - 62 INCH, 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 51-2-0 AND 51-1-21.
Part: SKIN — CORRODED (LT WING LE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LEADING EDGE LT WING AT XFS 566, 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 NR 00-047 WITH APPROVED 8110-3 DATED 4-20-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND GOUGED/CRACKED OUT HOLES ON INTERCOSTAL BETWEEN STA 1420 - 1400 RT AND BETWEEN L2R-L3R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-24, 53-2-0, 51-1-4 AND 51-1-21.
Part: WEB — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A 4 INCH CRACK LT WING I/B FLAP FILLER WEB AT FUSELAGE AT STA 980, 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 NR 00-047 WITH APPROVED 8110-3 DATED 3-13-00.
Part: SKIN — DAMAGED (CENTER WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SCREWS PULLING BELOW SKIN ON THE RIGHT L/E CENTER SECTION O/B NR 3 STUB WING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-18-00.
Part: FRAME — CORRODED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FRAME AT STA 1739 BETWEEN L32R AND L28R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-7-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM INTERCOSTALS AT FS 270 - 280, 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 51-1-2, 51-1-4 AND 51-1-20D.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED ATTACH ANGLE ON THE CIRCUMFERENTIAL FRAME GILLINER AT STA 1140 AND L35R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-10-00.
Part: THRESHOLD — CRACKED (PAX DOOR) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK, DISTORTED EDGES AND ELONGATED HOLES TO A FASTENER AT L2 DOOR INNER THRESHOLD PANEL, 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 00-047 WITH APPROVED 8110-3 DATED 3-1-00.
Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE INTERCOSTAL AT FS 1320 - 1340 AND L5L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DC-8 SRM 51-1-21 AND 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SKIN — DAMAGED (WING LE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH THE SKIN I/B SLOT LEADING EDGE VANE AT STA XS 250.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-4, MM 27-80-1 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-11-00.
Part: SKIN — CRACKED (RT STUB WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK ON THE RIGHT I/B STUB WING LWR SURFACE BETWEEN LWR RIB AT XFS 233 AND XFS 240, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-4, 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-13-00.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED INTERCOSTAL AT FS 1280 TO 1300 AND L9R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DC-8 SRM 51-1-21 AND 51-1-4.
Part: WEB — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MULTIPLE HOLE ELONGATION WITH DISTORTION AND CRACKS IN 4 PLACES TO THE CABIN FLOOR CUSP WEB AT STA 270 TO 235 RT 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 WEB IAW DC-8 SRM 51-1-4 AND 51-1-21.
Part: WEB — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CRACKS IN 5 PLACES AND MULTIPLE DISTORTIONS TO THE CABIN FLOOR CUSP LINE WEB AT STA 320 TO 270 RT CUSP 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 NEW WEB IAW DC-8 SRM 51-1-4 AND 51-1-21.
Part: PLATE — CRACKED (SPAR CAP) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED LWR FRONT SPAR CAP ON THE NR 4 STUB WING I/B MOUNT SHIM, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED EDGES SMOOTH AND RETURNED TO SERVICE IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 4-17-00.
Part: SKIN — CRACKED (STUB WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK ON THE NR 1 STUB WING MOUNTING SHIM AT LWR FRONT SPAR CAP AT STA XW 454, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED SHIM IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-17-00.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SCREWS LOOSE AND PULLING BELOW SKIN ON THE RIGHT I/B SLOT DOOR LEADING EDGE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-3-0, 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-17-00.
Part: SKIN — CHAFED (DOOR HANDLE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CHAFING TO THE L1 DOOR SKIN AT EXTERIOR DOOR HANDLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RETURNED TO SERVICE IAW EO NR 00-0047 WITH APPROVED 8110-3 DATED 4-17-00.
Part: SKIN — DAMAGED (LT WING LE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SCREWS PULLING THROUGH SKIN LT WING I/B SLOT LEADING EDGE VANE AT STA XS 220.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21, MM 27-80-1 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-17-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM AT FS 680, 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 51-1-20D AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM AT STA 540 CUSP TO CUSP, 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 NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES IN THE FLOORBEAM 1380 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW DC-8 SRM 51-1-21, 51-1-4 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: LONGERON — CORRODED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE LONGERON AT STA 1545 AND L8L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21, 53-2-0 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 4-11-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM 1260 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED STRAPS/FILLERS IAW DC-8 SRM 51-1-21, 51-1-20D AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: THRESHOLD — CRACKED (PAX DOOR) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CRACKED AND DRILLED OFF SCREWS ON THE R1 DOOR SILL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 51-3-0, 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-1-00.
Part: SPOILER PANEL — DELAMINATED (NR 1) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND A HOLE IN THE RT WING NR 1 GROUND SPOILER, 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 57-2-3, PARA 22, FIG 4K AND 51-1-9 PARA 3. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND HOLES IN THE INTERCOSTAL AT FS 798 - 822 AND L5L, 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: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOORBEAM IN THE UPPER CARGO COMPT AT FS 650, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED STRAPS/FILLERS AND INSTALLED IAW EO NR 00-0047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM 1080 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PLUGS/STRAPS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES IN THE FLOORBEAM 1400 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM 1300 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM 1100 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED PLUGS/STRAPS IAW DC-8 SRM 51-1-20D AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: STIFFENER — CRACKED (RT WING TE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A 5 TO 6 INCH CRACK ON I/B SIDE VERTICAL STIFFENER RT TRAILING EDGE AT STA XRS 107, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED STIFFENER IAW DC-8 SRM 51-1-20D AND 51-3-0.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES IN THE FLOORBEAM AT STA 1440 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOORBEAM AT FS 940, 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 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM AT FS 857, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM AT FS 900, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM AT FS 940, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM AT FS 980, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: SKIN — CRACKED (RT WING LE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK EMANATING FROM SCREW HOLE ON THE RIGHT I/B SLOT LEADING EDGE BOTTOM SIDE, 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 51-1-7, 57-2-0 AND 51-1-21.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES IN THE FLOORBEAM 1140 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM 1320 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM AT STA 460 CUSP TO CUSP, 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 EO NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM AT FS 878, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: FLOORBEAM — MISDRILLED (FS 1520) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOORBEAM IN THE UPPER CARGO COMPT FS 1520, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IN FLOORBEAM IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM AT STA 560 CUSP TO CUSP, 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 NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOORBEAM INTERCOSTALS AT FS 660 - 680, 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 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES IN THE FLOORBEAM 1340 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED DISCREPANT HOLES IAW DC-8 SRM 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM AT FS 798, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-20D AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES IN THE INTERCOSTALS AT FS 1800 - 1200, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. HOLES WITHIN ALLOWABLE LIMITS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 5-26-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE INTERCOSTALS AT FS 980 - 1000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. HOLES WITHIN ACCEPTABLE LIMITATIONS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: FLOORBEAM — MISDRILLED (STA 1160) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM 1160 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW DC-8 SRM 51-1-21, 51-1-20D AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE INTERCOSTALS AT FS 1360 - 1380, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. HOLES WITHIN ALLOWABLE LIMITS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM INTERCOSTALS AT FS 300 - 320, 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 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE INTERCOSTALS AT FS 1100 - 1120, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. HOLES WITHIN ALLOWABLE LIMITS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM INTERCOSTAL AT FS 500 - 520, 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 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE INTERCOSTALS AT FS 1120 - 1140, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. HOLES WITHIN ALLOWABLE LIMITS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM INTERCOSTALS AT FS 480 - 500, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE INTERCOSTALS AT FS 1280 - 1300, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. HOLES WITHIN ALLOWABLE LIMITS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE INTERCOSTALS AT FS 1220 - 1240, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. HOLES WITHIN ACCEPTABLE LIMITATIONS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: THRESHOLD — CRACKED (PAX DOOR) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CRACKED AND DRILLED OFF SCREWS ON THE L1 DOOR SILL, 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 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-1-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM AT STA 360 CUSP TO CUSP, 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 NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: INTERCOSTAL — TOOL DAMAGE (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND DRILL MARKS BETWEEN STA 620 - 640 XCW 0 CENTER LINE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED CHANNEL IAW DC-8 SRM 51-1-24, 53-2-0 AND 51-1-21.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE INTERCOSTALS AT FS 1400 - 1420, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM 51-1-8. HOLES WITHIN ALLOWABLE LIMITS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE INTERCOSTALS AT FS 1160-1180, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. HOLES WITHIN ALLOWABLE LIMITS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES TO THE FLOORBEAM INTERCOSTALS AT FS 280 - 300, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. HOLES WITHIN ACCEPTABLE LIMITATIONS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL DRILLED HOLES IN FLOORBEAM AT FS 740, 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 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED FLOORBEAM SUPPORT AT STA 520 XCW 6 INCHES LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-21, 53-2-0 AND 51-1-4.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM INTERCOSTALS AT FS 320 - 340, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM INTERCOSTALS AT FS 380 - 400, 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 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM INTERCOSTALS AT FS 360 - 380, 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 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: FRAME — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A MISDRILLED HOLE IN THE FRAME RADIUS AT STA 920 AND L12R, 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 51-1-20D, 51-1-4 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-13-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM INTERCOSTALS AT FS 400 - 420, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. HOLES WITHIN ACCEPTABLE LIMITATIONS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM INTERCOSTALS AT FS 460 - 480, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. HOLES WITHIN ALLOWABLE LIMITS IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL DRILLED HOLES IN THE FLOORBEAM AT FS 760, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21, 51-1-4, 51-1-20D AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM INTERCOSTALS AT FS 340 - 360, 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 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM INTERCOSTALS AT FS 440 - 460, 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 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM INTERCOSTALS AT FS 420 - 440, 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 00-047 WITH APPROVED 8110-3 DATED 3-26-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM 1280 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-4, 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM 1200 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW DC-8 SRM 51-1-21, 51-1-4, 51-1-20D AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM AT FS 840, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED HOLES PER EO NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: ANGLE — CRACKED (LT WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A 6 INCH CRACK TO THE LT WING I/B SLOT UPPER O/B CUTOUT ANGLE AT STA XFS 250.000, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED PART IAW DC-8 SRM 51-1-21.
Part: RIB — CRACKED (STUB WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A 2.5 INCH CRACK TO THE UPPER RIB ON THE NR 2 STUB WING AT STA XFS 250.000, 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 53-28-0, 57-3-2, 57-3-0 AND 51-1-20D.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND SEVERAL MISDRILLED HOLES IN THE FLOORBEAM AT FS 830, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-4, 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM AT STA 480 CUSP TO CUSP, 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, 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-19-00.
Part: WEB — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE WEB ON BOX AREA ON L2 DOOR AREA STA 1460 LT BETWEEN L21L AND L22L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 53-2-0, 51-1-4 AND 51-1-21.
Part: SKIN — DENTED (CARGO DOOR) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND THE D PIT DOOR DENTED, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-4, 52-2-0, 52-2-3 AND 51-1-21.
Part: WEB — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE MEMBRANE IN THE MAIN CABIN INTERIOR UPPER CUSP LINE AT STA 1080 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 REPAIR IAW DC-8 SRM 53-2-0, 51-1-4 AND 51-1-21.
Part: RIB — CRACKED (LT STUB WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING NR 2 STUB WING UPPER RIB, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED ANGLE IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-10-00.
Part: LONGERON — CORRODED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TOP OF LONGERON AND A WEAR SPOT ON THE LIGHT HOLE IN THE FWD LWR CARGO BILGE AT STA 544 AND L33R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. BLENDED GOUGES IAW DC-8 SRM 53-2-0 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-7-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SKIN — CORRODED (STUB WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AND CRACKS AT SCREW HOLES ON NR 2 STUB WING UPPER SURFACE AT STA XS 233 TO 220, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 53-28-0 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-13-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED ATTACH ANGLE FRAME AT STA 1480 RT AT L2R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-21 AND 51-1-4.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED INTERCOSTAL AND MISSING FASTENERS AT FS 1300 TO 1320 AND L4R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 AND 51-1-24.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES IN THE LONGITUDINAL FLOORBEAM BETWEEN STA 270 - 225 AND RBL 28.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 AND 53-2-0.
Part: WEB — CRACKED (PAX DOOR) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED INTERIOR WEB ON THE R-1 DOOR AT STA 395 RT AND L18R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 52-2-0, 51-1-4 AND 51-1-21.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES IN THE LONGITUDINAL FLOORBEAM BETWEEN STA 270 - 225 AND RBL 45.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21 AND 53-2-0.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES IN THE LONGITUDINAL FLOORBEAM AT STA 270 - 225 RT AND RBL 45.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-21.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE LONGITUDINAL FLOORBEAM AT RBL 28 1/2 10 BETWEEN STA 270 - 225 LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED MISDRILLED HOLES IAW DC-8 SRM 53-2-0 AND 51-1-21.
Part: ATTACH FITTING — GOUGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A GOUGED FLOORBEAM ATTACH FITTING AT FS 798 AND XCW 23 RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW DC-8 SRM 51-3-0 AND 51-1-20D.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM 1060 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED L ANGLE IAW EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: PANEL — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND MULTIPLE DRILLED HOLES AND CRACKS TO THE L2 CUSP PANEL AT STA 1480 TO 1520, 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 51-1-21 AND 51-1-4.
Part: ATTACH FITTING — GOUGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A GOUGE TO THE RT TANK EXTERIOR TO FLOORBEAM ATTACH FITTING AT FS 760=XCW 46, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-20D AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-07-00.
Part: ATTACH ANGLE — BROKEN (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A BROKEN ATTACH ANGLE AT STA 1568 AND L24R, 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 AND 51-3-0.
Part: ATTACH ANGLE — BROKEN (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A BROKEN ATTACH ANGLE AT STA 1568 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 51-1-21, 51-1-4 AND 51-3-0.
Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE FRAME ATTACH ANGLE TO FWD RT OVERWING EXIT DOOR AT FS 717 - 740 AND L19R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0 AND 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SKIN — TORN (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND FUSELAGE SKIN TORN AWAY BY GROUND PNEUMATIC CONNECTOR DOOR CUTOUT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21 AND 51-1-4. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FLOOR SUPPORT — GOUGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE AFT FLOORBEAM SUPPORT AROUND BOLT HEADS AND A DEEP GOUGE AT FS 960 XCW 0, 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 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 5-10-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: PANEL — DAMAGED (CARGO BAY) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND DAMAGE TO THE C PIT DOOR FILLET PANEL, 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: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES IN THE LONGITUDINAL FLOORBEAM AT STA 270 - 225 AND RBL 10, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 53-2-0 AND 51-1-21.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED ATTACH ANGLE IN THE MAIN CABIN INTERIOR AT STA 1586 AND L31L, 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 51-3-0 AND 51-1-4.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND HOLES IN THE INTERCOSTAL AT FS 900 - 920 AND L21R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. PLUGGED HOLES IAW DC-8 SRM 53-2-0 AND 51-1-21.
Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED INTERCOSTAL FRAME TIE AT FS 760 AND L3R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED GUSSET IAW DC-8 SRM 51-1-21 AND 51-1-4.
Part: STRUCTURE — CORRODED (HORIZONTAL STAB) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE AT SCREW HOLES ON THE RT O/B HORIZONTAL STAB LEADING EDGE I/B AT STA XFS 185 TO 187, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 55-2-0, 51-1-21 AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-7-00. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED ATTACH ANGLE AT STA 1420 LEFT ABOVE L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-8.
Part: WEB — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A JAGGED METAL PIECE OF MEMBRANE AT STA 1000 - 1020 AT L21L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED WEB IAW DC-8 SRM 51-1-21, 51-1-4 AND 53-2-0.
Part: ATTACH ANGLE — CRACKED (SCUFF PLATE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED DOOR SCUFF PLATE ATTACH ANGLE AT STA 1140 AND L34R, 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: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A HOLE IN THE INTERCOSTAL AT FS 560 - 580 AND L24R, 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: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CUTOUT WITH NO REPAIR ON THE INTERCOSTAL BETWEEN STA 320 - 340 RT AND RBL 10 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 53-2-0, 51-1-4 AND 51-1-21D.
Part: FINGER DOUBLER — CORRODED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON THE FINGER DOUBLER COCKPIT SUBFLOOR AT STA 148 TO 144 AND L20L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-20D, 51-1-4, 51-1-21 AND 53-2-0.
Part: SKIN — CORRODED (LT WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE ON SKIN LEFT WING O/B LEADING EDGE O/B SECTION AT STA XW 761.695 24 INCHES FWD OF 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 DOUBLER IAW DC-8 SRM 57-2-1, 57-2-0 AND 57-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SKIN — CORRODED (RT WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE RIGHT WING RIGHT O/B LEADING EDGE O/B EDGE UPPER AND LWR SKIN INTERIOR AT XFS 710, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 57-2-0, 57-2-1, 57-2-1, FIG 2H AND 51-1-21. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: WEB — TORN (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND HOLES TORN OUT BETWEEN STA 560 - 580 XCW 12 INCHES LEFT AT CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW WEB IAW DC-8 SRM 51-1-21 AND 51-1-4.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND HOLES TO THE INTERCOSTAL AT FS 640 - 660 AND L14R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-21, 53-2-0, 51-1-4 AND 51-1-20D.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE FLOORBEAM TO FRAME ATTACH ANGLE AT STA 1586 AND L24R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-3-0 AND 51-1-4.
Part: INTERCOSTAL — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND HOLES TO THE INTERCOSTAL AT FS 700 - 717 AND L5R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW DC-8 SRM 51-1-21, 51-1-4 AND 51-1-20D.
Part: LONGERON — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK APPROX 2.5 INCHES LENGTH AT THE RT W/W LONGERON 24 STA 879, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW DC-8 SRM 53-2-3, 53-2-2 AND 51-1-20D.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE INTERCOSTAL AT FS 798 TO 830 AND L5R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 53-2-0, 51-1-4 AND 51-1-21.
Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A HOLE TO THE INTERCOSTAL AT FS 340 - 360 AND L5R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAAW DC-8 SRM 51-1-4 AND 51-1-21.
Part: SKIN — DENTED (RT WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND THE SKIN DENTED AT RIGHT WING O/B LEADING EDGE AT STA XFS 685, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED RIVETS AND DENT FILLER IAW DC-8 SRM 57-2-1.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK IN RADIUS OF SUPPORT ANGLE ON RT BETWEEN STA 920 AND 902 LONGERON 24, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-21, 51-1-20D AND 51-1-4.
Part: RIVET — LOOSE (DOOR RETAINER) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND LOOSE RIVETS ON LWR DOOR RETAINERS RT FWD EXIT OPENING OVERWING, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED REPAIR IAW DC-8 SRM 51-3-0.
Part: FINGER DOUBLER — DAMAGED (HORIZONTAL STAB) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A RIVET PULLED THROUGH THE FINGER DOUBLER ON THE LT HORIZ STAB REAR SPAR ACCESS AT STA 221, 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 00-047 WITH APPROVED 8110-3 DATED 2-28-00.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,469 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED FLOOR CHANNEL SUPPORT AT STA 600 XCW 6 INCHES LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-21, 51-1-4 AND 51-1-20D.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A HOLE IN THE FRAME AT FS 320 AND L14R, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED GUSSET IAW DC-8 SRM 51-1-21A, 53-2-0, 51-1-4 AND 51-1-21.
Part: RIB — CRACKED (LT WING LE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED LWR RIB ON THE LEFT WING O/B LEADING EDGE I/B SEGMENT AT STA 603.750, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 57-2-0 AND 51-1-21D.
Part: FLOORBEAM — MISDRILLED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND NUMEROUS DRILLED HOLES TO THE FLOORBEAM 1220 CUSP TO CUSP, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW DC-8 SRM 51-1-20D AND EO NR 00-047 WITH APPROVED 8110-3 DATED 3-12-00.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED FLOORBEAM SUPPORT AT STA 500 XCW 6 INCHES RT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-21 AND 51-1-4.
Part: SKIN — DAMAGED (PAX DOOR) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A BROKEN PIECE TOP OF L1 DOOR , DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED, ALODINED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW DOUBLER IAW DC-8 SRM 51-1-21 AND 51-1-4.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED FLOORBEAM SUPPORT AT STA 500 XCW 6 INCHES LT, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-21 AND 51-1-4.
Part: SPOILER PANEL — DELAMINATED (NR 4) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE IN SEVERAL AREAS ON THE NR 4 GROUND SPOILER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED AND INSTALLED NEW PANEL IAW DC-8 SRM 27-61-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE I/B BOTTOM RIB ON THE LEFT I/B STAB LEADING EDGE FRAME AT XFS 172, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER IAW DC-8 SRM 51-1-4, 53-2-0 AND 51-1-20D.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE BOTTOM RIB ON THE LEFT I/B HORIZ STAB I/B LEADING EDGE FRAME AT XFS 166, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLERS IAW DC-8 SRM 55-2-3, 51-1-4, 53-2-3 AND 51-1-20D.
Part: BRACKET — DAMAGED (RT WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND ELONGATED HOLES ON THE ATTACH ANGLE BRACKET ON THE RT LEADING EDGE CENTER SECTION O/B SLOT DOOR PANEL AT STA XFS 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 DC-8 SRM 57-3-0, 51-1-4 AND 51-3-0.
Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACKED ATTACH ANGLE IN THE MAIN CABIN INTERIOR FRAME AT STA 900 AND L11L, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 51-1-20D AND 53-2-0.
Part: ATTACH FITTING — CORRODED (FUSELAGE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE WEB ATTACH FITTING AT FS 1400 AND L21R FRAME TO PRESS, 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 51-1-20D, 51-1-24, 53-2-0 AND 51-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: RIB — CRACKED (LT WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING O/B LEADING EDGE O/B SEGMENT UPPER RIB AT STA XFS 828.750, 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 51-1-21D.
Part: RIB — CRACKED (LT WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING O/B LEADING EDGE O/B SEGMENT UPPER RIB AT STA XFS 822.500, 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 DC-8 SRM 57-2-0 AND 51-1-20D.
Part: RIB — CRACKED (LT WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING O/B LEADING EDGE O/B SEGMENT UPPER RIB AT STA XFS 760.000, 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 51-1-21D.
Part: RIB — CRACKED (LT WING) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT WING O/B LEADING EDGE O/B SEGMENT UPPER RIB AT STA XFS 772.500, 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 DC-8 SRM 57-2-0 AND 51-1-21D.
Part: RIB — CRACKED (LT WING LE) · airframe 63,988 hrs · 20,467 cycles
DURING A MAINTENANCE VISIT FOUND A CRACK TO THE LT O/B LEADING EDGE O/B SEGMENT UPPER RIB AT STA XFS 847.500, 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 DC-8 SRM 57-2-0.
Part: FLOORBEAM — MISDRILLED (BS 1380)
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, FLOORBEAM 1380 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — MISDRILLED (BS 1260)
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, FLOORBEAM AT STA 1260 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — MISDRILLED (BS 1180)
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, FLOORBEAM AT STA 1180 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — MISDRILLED (BS 1340)
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, FLOORBEAM AT STA 1340 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: INTERCOSTAL — CRACKED (BS 1420 - 1400)
DURING A MAINTENANCE VISIT FOUND CRACK, FUSELAGE, INTERCOSTAL GOUGED/CRACKED OUT HOLES BETWEEN STA 1420 AND STA 1400 RT, BETWEEN LONGERON 2 RIGHT AND LONGERON 3 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — MISDRILLED (BS 1240)
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, FLOORBEAM AT STA 1240 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — MISDRILLED (BS 1140)
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, FLOORBEAM, AT STA 1140 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — MISDRILLED (BS 1160)
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, FLOORBEAM AT STA 1160 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — MISDRILLED (BS 1440)
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, FLOORBEAM AT STA 1440 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: ANGLE — CRACKED (BS 1480)
DURING A MAINTENANCE VISIT FOUND CRACK, FUSELAGE, ATTACH ANGLE FRAME AT STA 1480 RT AT LONGERON 2 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — MISDRILLED (BS 1200)
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, FLOORBEAM AT STA 1200 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — MISDRILLED (BS 1320)
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, FLOORBEAM AT STA 1320 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — MISDRILLED (BS 1300)
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, FLOORBEAM AT STA 1300 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — MISDRILLED (BS 1420)
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, MISDRILLED HOLES, FUSELAGE, FLOORBEAM AT STA 1420 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — MISDRILLED (BS 1280)
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, FLOORBEAM AT STA 1280 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — MISDRILLED (BS 1360)
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, FLOORBEAM AT STA 1360 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — MISDRILLED (BS 1220)
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, FLOORBEAM AT STA 1220 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — MISDRILLED (BS 1400)
DURING A MAINTENANCE VISIT FOUND MISDRILLED HOLES, FUSELAGE, FLOORBEAM AT STA 1400 CUSP TO CUSP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8.
Earlier reports · 1995–1999 · 151 reports
1999
Part: FLOOR PANEL — CORRODED (BS 640 & 720)
DURING A MAINTENANCE VISIT FOUND CORROSION, FUSELAGE, CABIN FLOOR PLANK BL 36 LEFT BETWEEN STA 640 AND STA 720. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED DOUBLER REPAIR IAW DC8 SRM 51-1-8 PG 17-20 AND DC8 SRM 53-2-3 FIG 10 PG 39-40. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
1998
Part: O-RING — LEAKING (LT MLG)
LOSS OF HYDRAULIC QUANTITY AND HYDRAULIC PRESSURE. PERFORMED CHECK LISTS TO LOWER FLAPS. FOUND FITTING ON LT GEAR TRIM FITTING LEAKING. REMOVED FITTING, REPLACED O-RING, REINSTALLED FITTING, SERVICED HYD RES. PERFORMED GROUND RUN ON NR 2 AND NR 3 ENGINES, OPS CHECK HYD PUMPS AND LEAK CHECK BOGGIE TRIM FITTINGS, NO LEAKS NOTED. CYCLED FLAPS, SPOILERS, AILERONS, RUDDER AND HORIZONTAL STAB SYSTEMS SERVERAL TIMES.
Part: FRAME — MISDRILLED (FRAME 759)
DURING MAINTENANCE VISIT, FOUND FRAME 759 WITH MISDRILLED HOLE AT LONGERON 15 LEFT. FABRICATED AND INSTALLED REPAIR STRAPS AND CLIPS IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R87, DC-8 SRM 51-1-20D, 51-1-21 AND TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 540)
DURING MAINTENANCE VISIT, FOUND 540 WITH MISDRILLED HOLE AT LT CUSP. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE, FILLER AND SHIM IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R67 AND DC-8 SRM 51-1-1A.
Part: FRAME — MISDRILLED (FRAME 640)
DURING MAINTENANCE VISIT, FOUND FRAME 640 CRACKED BETWEEN LONGERONS 9 AND 10 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW FAA APPROVED ACMI SKETCH SK98500, DC-8 SRM 51-1-20D, 51-1-21 AND TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 822)
DURING MAINTENANCE VISIT, FOUND FRAME 822 WITH MISDRILLED HOLE AT LONGERON 3 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED ACMI SKETCH SK98298, DC-8 SRM 51-1-20D AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — MISDRILLED (BS 660)
DURING MAINTENANCE VISIT, FOUND FLOOR SUPPORT AT FS 660 WITH MISDRILLED HOLES IN THE UPPER FLANGE. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED NEW T-CAP IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R51, DC-8 SRM 51-1-21 AND TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 920)
DURING MAINTENANCE VISIT, FOUND FRAME 920 WITH MISDRILLED HOLES AT LONGERON 16 LEFT. PLUGGED HOLES, FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APPROVED ACMI SKETCH SK98242, DC-8 SRM 51-1-20D AND TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 940)
DURING MAINTENANCE VISIT, FOUND FRAME 940 WITH MISDRILLED HOLE AT LONGERON 14 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE AND STRAPS IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R109, DC-8 SRM 51-1-1, 51-1-20D AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: SKIN — CORRODED (HORIZ STAB)
DURING MAINTENANCE VISIT, FOUND CORROSION ON INTERNAL UPPER SKIN AT STA XE224 TO 260 OF LT HORIZONTAL STABILIZER. REMOVED PANEL, FABRICATED AND INSTALLED NEW SKIN PANEL IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R90, DC-8 SRM 51-1-21 AND TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 960)
DURING MAINTENANCE VISIT, FOUND THE FACE OF FRAME 960 GOUGED AND MISDRILLED HOLE AT LONGERON 9 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE, STRAP AND FILLER IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R94, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 540)
DURING MAINTENANCE VISIT, FOUND FRAME 540 WITH DRILL DAMAGE AT LONGERON 13 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED ACMI SKETCH SK98484, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1380)
DURING MAINTENANCE VISIT, FOUND FRAME 1380 WITH MISDRILLED HOLE AT LONGERON 9 RIGHT. PLUGGED HOLE IN FRAME, FABRICATED AND INSTALLED REPAIR STRAPS IAW FAA APPROVED ACMI SKETCH SK98392, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 640)
DURING MAINTENANCE VISIT, FOUND FRAME 640 WITH MISDRILLED HOLE AT LONGERON 12 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND STRAP IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R40, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1300)
DURING MAINTENANCE VISIT, FOUND FRAME 1300 WITH MISDRILLED HOLES AT LONGERON 13 RIGHT. FABRICATED AND INSTALLED REPAIR STRAPS AND INTERCOSTAL CLIPS IAW FAA APPROVED ACMI SKETCH SK98384, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — DAMAGED (FRAME 255)
DURING MAINTENANCE VISIT, FOUND FRAME 255 NICKED IN RADIUS BETWEEN LONGERONS 12 AND 13 RIGHT. FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APPROVED ACMI SKETCH SK98364. HEAT TREATED IAW DC-8 SRM 51-1-1 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: SKIN — CORRODED (HORIZ STAB)
DURING MAINTENANCE VISIT, FOUND CORROSION ON INTERNAL UPPER SKIN AT STA XE185 OF RT HORIZONTAL STABILIZER. REMOVED PANEL, FABRICATED AND INSTALLED NEW SKIN PANEL IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R91, DC-8 SRM 51-1-21 AND TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1360)
DURING MAINTENANCE VISIT, FOUND FRAME 1360 WITH MISDRILLED HOLES AT LONGERON 9 RIGHT. REMOVED GUSSET, REMOVED DAMAGED AREA, FABRICATED AND INSTALLED NEW SPLICE, STRAPS AND GUSSET IAW FAA APPROVED ACMI SKETCH SK98390, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: SKIN — CORRODED (HORIZ STABS)
DURING MAINTENANCE VISIT, FOUND CORROSION ON INTERNAL UPPER SKIN AT STA XE167 TO 221 OF LT HORIZONTAL STABILIZER. REMOVED PANEL, FABRICATED AND INSTALLED NEW SKIN PANEL IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R91, DC-8 SRM 51-1-21 AND TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1440)
DURING MAINTENANCE VISIT, FOUND FRAME 1440 WITH MISDRILLED HOLE AT LONGERON 12 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R35, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 280)
DURING MAINTENANCE VISIT, FOUND FRAME 280 WITH MISDRILLED HOLE AT LONGERON 5 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLER, TIE CLIPS AND SHIMS IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R31, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 560)
DURING MAINTENANCE VISIT, FOUND FRAME 560 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 8 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIMS IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R93, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 660)
DURING MAINTENANCE VISIT FOUND FRAME 660 WITH MISDRILLED HOLE AT LT CUSP. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R69.
Part: SCUFF PLATE — CORRODED (CARGO DOORWAY)
DURING MAINTENANCE VISIT, FOUND C-PIT DOOR THRESHOLD SCUFF PLATE BULGING AND SEVERAL PULLED FASTENERS. REMOVED DAMAGED SKIN AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH E84-R15, DC-8 SRM 51-1-20D, 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: SKIN — CORRODED (HORIZ STAB)
DURING MAINTENANCE VISIT, FOUND CORROSION ON INTERNAL UPPER SKIN AT STA XE282 TO 291 OF LT HORIZONTAL STABILIZER. REMOVED PANEL, FABRICATED AND INSTALLED NEW SKIN PANEL IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R89, DC-8 SRM 51-1-21 AND TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1260)
DURING MAINTENANCE VISIT, FOUND FRAME 1260 WITH MISDRILLED HOLE AT LONGERON 20 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R21, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1060)
DURING MAINTENANCE VISIT, FOUND FRAME 1060 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 8 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE, STRAPS AND SHIMS IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R98, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1380)
DURING MAINTENANCE VISIT, FOUND FRAME 1380 WITH MISDRILLED HOLE BETWEEN LONGERONS 11 AND 12 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE, STRAPS AND FILLERS IAW FAA APPROVED ACMI SKETCH SK 98393, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1320)
DURING MAINTENANCE VISIT, FOUND FRAME 1320 WITH MISDRILLED HOLE BETWEEN LONGERONS 9 AND 10 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIM IAW FAA APPROVED ACMI SKETCH SK98482, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 600)
DURING MAINTENANCE VISIT, FOUND FRAME 600 WITH MISDRILLED HOLE AT LT CUSP. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLE AND STRAP IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R69, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 920)
DURING MAINTENANCE VISIT, FOUND FRAME 920 WITH MISDRILLED HOLE AT LONGERON 11 LEFT. PLUGGED HOLE, FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APPROVED ACMI SKETCH SK98302, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 880)
DURING MAINTENANCE VISIT, FOUND FRAME 880 WITH MISDRILLED HOLE AT LONGERON 3 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED ACMI SKETCH SK98300, DC-8 SRM 51-1-20D AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 880)
DURING MAINTENANCE VISIT, FOUND FRAME 880 WITH MISDRILLED HOLE AT LONGERON 6 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED ACMI SKETCH SK98301, DC-8 SRM 51-1-1, 51-1-20D AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1120)
DURING MAINTENANCE VISIT, FOUND FRAME 1120 WITH MISDRILLED HOLE AT LONGERON 13 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW FAA APPROVED ACMI SKETCH SK98376, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1180E)
DURING MAINTENANCE VISIT, FOUND FRAME 1180 WITH MISDRILLED HOLE AT LONGERON 13 RIGHT. FABRICATED AND INSTALLED NEW INTERCOSTAL CLIP AND REPAIR STRAPS IAW FAA APPROVED ACMI SKETCH SK98379, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1080)
DURING MAINTENANCE VISIT, FOUND FRAME 1080 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 8 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R97. HEAT TREATED ANGLE IAW DC-8 SRM 51-1-1 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: SKIN — CORRODED (HORIZ STAB)
DURING MAINTENANCE VISIT, FOUND CORROSION ON LOWER SURFACE OF RT HORIZONTAL STABILIZER SKIN PANEL AT STA XE270 TO 310. REMOVED CORROSION AND FOUND TO BE BEYOND LIMITS. FABRICATED AND INSTALLED NEW SKIN PANEL IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R89 AND DC-8 SRM 51-1-21.
Part: FRAME — MISDRILLED (FRAME 700)
DURING MAINTENANCE VISIT, FOUND FRAME 700 WITH MISDRILLED HOLE BETWEEN LONGERONS 11 AND 12 LEFT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R65, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1320)
DURING MAINTENANCE VISIT, FOUND FRAME 1320 WITH MISDRILLED HOLE BETWEEN LONGERONS 19 AND 20 RIGHT. REPAIRED FRAME IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R23, DC-8 SRM 51-1-21 AND TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 560)
DURING MAINTENANCE VISIT, FOUND FRAME 560 WITH MISDRILLED HOLES AT LONGERONS 19 AND 20 RIGHT. PLUGGED MISDRILLED HOLES IAW DC-8 SRM 51-1-21, FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R45 AND TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 798)
DURING MAINTENANCE VISIT, FOUND FRAME 798 WITH MISDRILLED HOLES AT LONGERONS 7, 8, 9, 10, 11, 14, 15 AND 21 RIGHT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R68, DC-8 SRM 51-1-20D AND TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 780)
DURING MAINTENANCE VISIT FOUND FRAME 780 WITH MISDRILLED HOLE AT LONGERON 11 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R49, HEAT TREATED IAW DC-8 SRM 51-1-1, INSTALLED IAW DC-8 SRM 51-1-21 AND TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1420)
DURING MAINTENANCE VISIT, FOUND FRAME 1420 WITH MISDRILLED HOLE AT LONGERON 19 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R26, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 781)
DURING MAINTENANCE VISIT, FOUND FRAME 781 WITH MISDRILLED HOLE BETWEEN LONGERONS 8 AND 9 LEFT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R106.
Part: FLOORBEAM — MISDRILLED (BS 880)
DURING MAINTENANCE VISIT, FOUND FLOORBEAM AT FS 880 WITH MISDRILLED HOLES. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANGLES, FILLER AND STRAP IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R54, DC-8 SRM 51-1-21, 51-1-20D AND TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 760)
DURING MAINTENANCE VISIT, FOUND FRAME 760 WITH MISDRILLED HOLE AT LONGERON 5 RIGHT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R48.
Part: FRAME — MISDRILLED (FUSELAGE)
DURING MAINTENANCE VISIT, FOUND FRAME 1280 WITH MISDRILLED HOLES AT LONGERONS 10, 11 AND 12 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND STRAPS IAW FAA APPROVED ACMI SKETCHES SK98381 AND SK98382, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 798)
DURING MAINTENANCE VISIT, FOUND FRAME 798 WITH MISDRILLED HOLE AT LONGERON 11 LEFT. FABRICATED AND INSTALLED REPAIR STRAPS IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R111, DC-8 SRM 51-1-20D AND TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FUSELAGE)
DURING MAINTENANCE VISIT, FOUND FRAME WITH MISDRILLED HOLES AT LONGERONS 4, 5, 9, 10, 11 AND 13 RIGHT. FABRICATED AND INSTALLED REPAIRS IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R80, DC-8 SRM 51-1-21 AND AREAS TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1320)
DURING MAINTENANCE VISIT, FOUND FRAME 1320 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 8 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND STRAP IAW FAA APPROVED ACMI SKETCH SK98385, DC-8 SRM 51-1-21 AND TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1240)
DURING MAINTENANCE VISIT, FOUND FRAME 1240 WITH MISDRILLED HOLE AT LONGERON 8 LEFT. BLENDED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R44, DC-8 SRM 51-1-21 AND TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 940)
DURING MAINTENANCE VISIT, FOUND FRAME 940 WITH MISDRILLED HOLES BETWEEN LONGERONS 9 AND 12 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLES, SHIMS AND STRAPS IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R86, DC-8 SRM 51-1-21 AND TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1080)
DURING MAINTENANCE VISIT, FOUND FRAME 1080 WITH MISDRILLED HOLES AT LONGERONS 8 AND 10 LEFT. FABRICATED AND INSTALLED REPAIR STRAPS IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R38, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: SKIN — CRACKED (BS 300)
DURING MAINTENANCE VISIT, FOUND FUSELAGE SKIN CRACKED AT FS 300 TO 320 BETWEEN LONGERONS 9 AND 10 LEFT. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E77-R04.
Part: FLOOR — CRACKED (BS 435-445)
DURING MAINTENANCE VISIT, FOUND FLOOR PANEL WITH CRACKS THROUGH BOLT HOLES AT FS 435 TO 445 LBL 60. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH SK98418, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 280)
DURING MAINTENANCE VISIT, FOUND FRAME 280 WITH MISDRILLED HOLE BETWEEN LONGERONS 13-14 RIGHT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R31, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 834)
DURING MAINTENANCE VISIT, FOUND FRAME 834 WITH MISDRILLED HOLE AT LONGERON 15 RIGHT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R79.
Part: ANGLE — CORRODED (BS 69)
DURING MAINTENANCE VISIT, FOUND VERTICAL TO HORIZONTAL PRESSURE WEB ATTACH ANGLE CORRODED AT FS 69 RBL 12 TO 16. REMOVED DAMAGED SECTION OF ATTACH ANGLE, FABRICATED AND INSTALLED NEW SECTION OF ATTACH ANGLE AND SPLICE REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R102, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 500)
DURING MAINTENANCE VISIT, FOUND FRAME 500 WITH MISDRILLED HOLE BETWEEN LONGERONS 16 AND 17 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R66, DC-8 SRM 53-2-0 AND 51-1-21.
Part: FRAME — MISDRILLED (FRAME 1100)
DURING MAINTENANCE VISIT, FOUND FRAME 1100 WITH MISDRILLED HOLE AT LONGERON 14 LEFT. FABRICATED AND INSTALLED REPAIR DOUBLED IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R33, DC-8 SRM 51-1-21 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 440)
DURING MAINTENANCE VISIT, FOUND FRAME 440 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 9 RIGHT. FABRICATED AND INSTALLED REPAIR STRAPS IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R36, DC-8 SRM 51-1-21 AND TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 580)
DURING MAINTENANCE VISIT, FOUND FRAME 580 WITH MISDRILLED HOLE AT LONGERON 9 LEFT. FABRICATED AND INSTALLED REPAIR ANGLES, FILLER AND SHIM IAW FAA APPROVED ACMI SKETCH SK 98362, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1300)
DURING MAINTENANCE VISIT, FOUND FRAME 1300 WITH MISDRILLED HOLE AT LONGERON 20 RIGHT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R22, DC-8 SRM 53-2-0 AND 51-1-21.
Part: FRAME — MISDRILLED (FRAME 1420)
DURING MAINTENANCE VISIT, FOUND FRAME 1420 WITH MISDRILLED HOLES AT LONGERONS 5, 7 AND 8 LEFT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R41.
Part: FRAME — MISDRILLED (FRAME 822)
DURING MAINTENANCE VISIT, FOUND FRAME 822 WITH MISDRILLED HOLE BETWEEN LONGERONS 7 AND 8 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R76, DC-8 SRM 51-1-20, 53-2-0 AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 640)
DURING MAINTENANCE VISIT, FOUND FRAME 640 WITH MISDRILLED HOLE ABOVE LONGERON 21 RIGHT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R01, DC-8 SRM 51-1-20D AND TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1280)
DURING MAINTENANCE VISIT, FOUND FRAME 1280 WITH MISDRILLED HOLE AT LONGERON 13 RIGHT. FABRICATED AND INSTALLED REPAIR STRAPS, GUSSET AND FILLER IAW FAA APPROVED ACMI SKETCH SK98383, DC-8 SRM 51-1-21 AND TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 780)
DURING MAINTENANCE VISIT, FOUND FRAME 780 WITH MISDRILLED HOLE BETWEEN LONGERONS 9 AND 10 RIGHT. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R49, DC-8 SRM 53-2-0 AND 51-1-1A.
Part: FLOORBEAM — CRACKED (BS 1480)
DURING MAINTENANCE VISIT, FOUND FLOORBEAM AT FS 1480 LEFT CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA APPROVED ACMI SKETCH SK98463, DC-8 SRM 51-1-20D AND AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FLOORBEAM — CRACKED (BS 1500)
DURING MAINTENANCE VISIT, FOUND FLOORBEAM AT FS 1500 LEFT CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER AND SHIM IAW FAA APPROVED ACMI SKETCH SK98464, DC-8 SRM 51-1-20D AND TREATED AREA IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1400)
DURING MAINTENANCE VISIT, FOUND FRAME 1400 WITH MISDRILLED HOLES AT LONGERONS 18, 20 AND 21 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R27.
Part: FRAME — MISDRILLED (FRAME 1340)
DURING MAINTENANCE VISIT, FOUND FRAME 1340 WITH MISDRILLED HOLES BETWEEN LONGERONS 6 AND 9 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R84, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1520)
DURING MAINTENANCE VISIT, FOUND FRAME 1520 WITH MISDRILLED HOLES AT LONGERONS 8 AND 9 RIGHT. FABRICATED AND INSTALLED REPAIR IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R83.
Part: FRAME — MISDRILLED (FRAME 1140)
DURING MAINTENANCE VISIT, FOUND FRAME 1140 WITH MISDRILLED HOLE IN RADIUS AT LONGERONS 16 AND 19 RIGHT. FABRICATED AND INSTALLED STRAP AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R07, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1220)
DURING MAINTENANCE VISIT, FOUND FRAME 1220 WITH MISDRILLED HOLES IN RADIUS BETWEEN LONGERONS 7 AND 11 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R72, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 717)
DURING MAINTENANCE VISIT, FOUND FRAME 717 WITH MISDRILLED HOLES AT LONGERONS 9 AND 10 LEFT. ALSO LONGERON 11 LEFT INTERCOSTAL MISDRILLED IN THE RADIUS. REMOVED CLIPS AND LOOSENED STRAPS, PLUGGED MISDRILLED HOLES IAW DC-8 SRM 51-1-21, FABRICATED AND INSTALLED REPAIR ANGLE AND STRAPS IAW FAA APPROVED ACMI SKETCH SK98260, HEAT TREATED IAW DC-8 SRM 51-1-1, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1020)
DURING MAINTENANCE VISIT, FOUND FRAME 1020 WITH MISDRILLED HOLES BETWEEN LONGERONS 7 AND 9 RIGHT. FABRICATED AND INSTALLED REPAIR STRAP IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R81, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1040)
DURING MAINTENANCE VISIT, FOUND FRAME 1040 WITH MISDRILLED HOLES AT LONGERONS 7 AND 8 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R73 AND DC-8 SRM 51-1-21, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FUSELAGE)
DURING MAINTENANCE VISIT, FOUND FRAME 1100 WITH MISDRILLED HOLES AT LONGERONS 8 RIGHT AND BETWEEN LONGERONS 12 AND 13 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE, STRAPS AND FILLER IAW FAA APPROVED ACMI SKETCH SK98374 AND DC-8 SRM 51-1-21, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: VANE — CRACKED (LT TE FLAP)
DURING MAINTENANCE VISIT, FOUND LT O/B SLOT LEADING EDGE CRACKED IN TWO PLACES. ROUTED OUT CRACKS ON SLOT VANE AT STA X0LD025.5 AND X0LD014.75, DRILLED AND COUNTERSANK NEW HOLES ON EACH SIDE OF CLEAN UP. INSTALLED NEW FASTENERS IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R104 AND DC-8 SRM 51-1-21.
Part: FRAME — MISDRILLED (FRAME 1240)
DURING MAINTENANCE VISIT, FOUND FRAME 1240 MISDRILLED BETWEEN LONGERONS 7 AND 9 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R46 AND DC-8 SRM 51-1-21.
Part: FRAME — MISDRILLED (FRAME 450)
DURING MAINTENANCE VISIT, FOUND FRAME 450 MISDRILLED AT LONGERON 3 LEFT. REMOVED DAMAGED AREA, FABRICATED NEW RING AND BRACKET IAW ROSEMBALM DRAWING NR 44212, TREATED AND PRIMED IAW DC-8 SRM 51-1-8. INSTALLED RING AND BRACKET IAW DC-8 SRM 51-1-20D AND 53-2-0.
Part: FRAME — MISDRILLED (FRAME 1440)
DURING MAINTENANCE VISIT, FOUND FRAME 1440 WITH MISDRILLED HOLES AT LONGERONS 5A-7 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE AND STRAP IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R47.
Part: FRAME — MISDRILLED (FRAME 1040)
DURING MAINTENANCE VISIT, FOUND FRAME 1040 WITH HOLE IN RADIUS BETWEEN LONGERONS 10 AND 11 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R73, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1340)
DURING MAINTENANCE VISIT, FOUND FRAME 1340 WITH HOLE IN RADIUS BETWEEN LONGERONS 10 AND 11 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND SHIM IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R84, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — CHAFED (FRAME 1586)
DURING MAINTENANCE VISIT, FOUND FRAME 1586 CHAFED AND DRILL MARKS AT LONGERON 27 TO 31 LEFT. REMOVED FASTENERS AND BLENDED FRAME, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R61.
Part: WEDGE — CREASED (RT TE FLAP)
DURING MAINTENANCE VISIT, FOUND RT INBOARD FLAP WEDGE AFT CENTER UPPER SKIN STA XCW26.75 CREASED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R58.
Part: FRAME — MISDRILLED (FRAME 1260)
DURING MAINTENANCE VISIT, FOUND FRAME 1260 WITH MISDRILLED HOLES IN RADIUS AT LONGERONS 8, 9, 11 AND 13 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R71, HEAT TREATED ANGLE IAW DC-8 SRM 51-1-1, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1500)
DURING MAINTENANCE VISIT, FOUND FRAME 1500 WITH MISDRILLED HOLES AT LOWER AFT DOOR FRAME. FABRICATED AND INSTALLED REPAIR ANGLE AND CLIP, INSTALLED NEW CUSP WEB AND FITTING IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R99 AND RFTS 98-420.
Part: FRAME — MISDRILLED (FRAME 1000)
DURING MAINTENANCE VISIT, FOUND FRAME 1000 WITH MISDRILLED HOLES AND GOUGES BETWEEN LONGERONS 7 AND 11 RIGHT. FABRICATED AND INSTALLED REPAIR ANGLES IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R82.
Part: FLOOR — PUNCTURED (BS 1423)
DURING MAINTENANCE VISIT, FOUND FLOOR PANEL AT STA 1423 BL 0 PUNCTURED. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH SK98541 AND DC-8 SRM 51-1-21, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: SWITCH — INOP (NLG)
ON APPROACH, NO GREEN NOSE LIGHT INDICATION, DOORS NOT LATCHED AND GEAR NOT LATCHED LIGHTS ARE ON, CYCLED THE GEAR SEVERAL TIMES, NO HELP. ACCOMPLISHED QRH PROCEDURES, PREFORMED EMERGENCY LANDING. PREFORMED T/S TO LANDING GEAR POSITION AND WARNING SYS. FOUND NOSE GEAR DOWNLOCK LIMIT SWITCH INOP. REMOVED AND REPLACED SAME. PREFORMED TEST TO SYS OPS CHECKS GOOD IAW MM CH 32-60-0.
Part: FRAME — DAMAGED (BS 834)
DURING A MAINTENANCE VISIT, FOUND A HOLE IN RADIUS OF FRAME STA 834 AT LONGERON 11R. REMOVED TIE PLATE, INSTALLED FASTENER IN HOLE, REINSTALLED TIE PLATE IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R78, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: FRAME — MISDRILLED (FRAME 1240)
DURING MAINTENANCE VISIT, FOUND HOLE IN RADIUS OF FRAME 1240 BETWEEN LONGERONS 11 AND 12 RIGHT. PLUGGED HOLE IN FRAME IAW FAA APPROVED DER COTNEY ENGINEERING RFTS 98-351 DATED 7-22-98.
Part: FRAME — MISDRILLED (FRAME 780)
DURING MAINTENANCE VISIT, FOUND FRAME 780 MISDRILLED HOLES BETWEEN LONGERONS 18, 19, 20 RIGHT. FABRICATED AND INSTALLED GUSSETS AND SPLICES IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH E84-R105, AREA TREATED IAW DC-8 SRM 51-1-8.
Part: ANGLE — CORRODED (BS 759)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM ATTACHMENT ANGLE AT STA 759 BETWEEN BL 54 LEFT TO BL 64, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED ANGLE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FITTING — CORRODED (BS 900)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 900 AND LONGERON 24 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-2 FIGURE 5. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SHEAR TIE — CORRODED (BS 902)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SHEAR TIE AT STA 902 AND LONGERON 24 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SHEAR TIE IAW DC-8 SRM 51-1-20D. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: ANGLE — CORRODED (BS 1606)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOORBEAM ATTACHMENT ANGLE AT STA 1606 AND LONGERON 32 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 53-2-0 FIGURE 7. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FITTING — CORRODED (BS 920)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 920 AND LONGERON 24 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-2 FIGURE 5. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: LONGERON — CORRODED (BS 1536)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 32 LEFT AT STA 1536, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2 FIGURE 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FITTING — CORRODED (BS 940)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 940 AND LONGERON 24 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: LONGERON — CORRODED (BS 1536)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 34 LEFT AND FITTING AT STA 1536, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2 FIGURE 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FITTING — CORRODED (BS 1557)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 1557 AND LONGERON 31 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: LONGERON — CORRODED (BS 1536)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 30 RIGHT AT STA 1536, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2 FIGURE 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: LONGERON — CORRODED (BS 1530)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 34 RIGHT AT STA 1530, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2 FIGURE 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FITTING — CORRODED (BS 1557)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 1557 AND LONGERON 35 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FRAME — CORRODED (BS 1557)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME AT STA 1557 BETWEEN LONGERONS 33 LEFT TO 34 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 53-2-5 FIGURE 8C-1. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: LONGERON — CORRODED (BS 1538)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 36 BETWEEN STA 1535 TO STA 1538, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2 FIGURE 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FITTING — CORRODED (BS 1557)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 1557 AND LONGERON 35 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: SKIN — CORRODED (HORIZ STAB)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SKIN PANEL AT XE 125 TO XE 146, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SKIN PANEL IAW SK8550002. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FITTING — CORRODED (BS 1557)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 1557 AND LONGERON 34 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FRAME — CORRODED (BS 1440)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME AT STA 1440 BETWEEN LONGERONS 35 RIGHT TO 36, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 53-2-0 FIGURE 2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FLOOR TRACK — CORROSION (BS 980-1380)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FLOOR TRACK BETWEEN STA 980 TO 1380 AND BETWEEN LONGERONS 33 LEFT 33 RIGHT TO 36, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FLOOR TRACKS IAW DC-8 53-3-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FITTING — CORRODED (BS 900)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 900 AND LONGERON 24 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-2 FIGURE 5. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: LONGERON — CORRODED (BS 1460-1480)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 28 RIGHT BETWEEN STA 1460 TO STA 1480, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: LONGERON — CORRODED (BS 980)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 35 LEFT AT STA 980, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-0 FIGURE 1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: LONGERON — CORRODED (BS 880)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 24 RIGHT AT STA 880, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2 FIGURE 10. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FITTING — CORRODED (BS 1420)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 1420 AND LONGERON 21 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW FITTING IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FITTING — CORRODED (BS 1557)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 1557 AND LONGERON 29 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: DOUBLER — CORRODED (BS 1570-1578)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO SKIN DOUBLER AT STA 1570 TO STA 1578 AND BETWEEN LONGERONS 32 LEFT 33 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0 FIGURE 1F. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: INTERCOSTAL — CORRODED (BS 1385)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO INTERCOSTAL AT STA 1385 AND LONGERON 26 LEFT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: LONGERON — CORRODED (BS 1440-1480)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LONGERON 26 LEFT BETWEEN STA 1440 TO STA 1480, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW LONGERON SECTION IAW DC-8 53-2-2. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: DOUBLER — CORRODED (BS 920-940)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LEFT AND RIGHT WHEEL WELL PRESURE PANEL FINGER DOUBLER AT STA 920 TO STA 940 BETWEEN BL 66 LEFT TO BL 66 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED , TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FINGER DOUBLER IAW DC-8 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: ANGLE — CORRODED (BS 1080)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FRAME ATTACHMENT ANGLE AT STA 1080 AND LONGERON 35 RIGHT, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 53-1-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FRAME — MISDRILLED (BS 834)
DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 834 AND LONGERON 15 RIGHT.
Part: FRAME — MISDRILLED (BS 560)
DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 560 BETWEEN LONGERONS 7 LEFT TO 8 LEFT.
Part: FRAME — MISDRILLED (BS 440)
DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 440 AND LONGERON 16 RIGHT.
Part: FRAME — MISDRILLED (BS 280)
DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 280 BETWEEN LONGERONS 13 RIGHT TO 14 RIGHT.
Part: FRAME — MISDRILLED (BS 822)
DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 822 AND LONGERON 3 LEFT.
Part: FRAME — MISDRILLED (BS 580)
DURING A MAINTENANCE VISIT, FOUND FRAME WITH MISDRILLED HOLE, AT STA 580 AND LONGERON 9 LEFT.
Part: FRAME — MISDRILLED (BS 270)
DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 270 BETWEEN LONGERONS 12 RIGHT TO 14 RIGHT.
Part: FRAME — MISDRILLED (BS 640)
DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 640 AND LONGERON 7 LEFT.
Part: FRAME — MISDRILLED (BS 420)
DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 420 BETWEEN LONGERONS 7 RIGHT TO 8 RIGHT.
Part: SKIN — CORRODED (HORIZ STAB)
DURING A MAINTENANCE VISI, FOUND CORROSION DAMAGE TO HORIZONTAL STABILIZER SKIN PANEL AT XE 181, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW SKIN PANEL IAW SK8550002. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: PANEL — CORRODED (BS 940)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO LEFT WHEEL WELL PRESURE PANEL AT STA 940 AND BETWEEN BL 63 LEFT TO BL 66 LEFT, DAMAGE BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW FAA APPROVED COTNEY DER ENGINEERING SKETCH E84-R55. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FITTING — CORRODED (BS 759)
DURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO FITTING AT STA 759 AND BL 66, DAMAGED BEYOND LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED NEW ANGLE IAW DC-8 SRM 53-2-0. (CORROSION DAMAGE RECORDED IN EWA CORROSION PROGRAM).
Part: FRAME — MISDRILLED (BS 640)
DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 640 AND LONGERON 21 LEFT.
Part: FRAME — MISDRILLED (BS 660)
DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 660 AND LONGERON 21 LEFT.
Part: FRAME — MISDRILLED (BS 759)
DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 759 BETWEEN LONGERONS 19 LEFT TO 20 LEFT.
Part: FRAME — MISDRILLED (BS 620)
DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLE, AT STA 620 AND LONGERON 21 LEFT.
Part: FRAME — MISDRILLED (BS 560)
DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 560 AND LONGERON 21 LEFT.
Part: FRAME — MISDRILLED (BS 540)
DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 540 AND LONGERON 21 LEFT.
Part: FRAME — MISDRILLED (BS 520)
DURING A MAINTENANCE VISIT, FOUND FUSELAGE FRAME WITH MISDRILLED HOLES, AT STA 520 AND LONGERON 21 LEFT.
Part: DOOR — NOT LATCHED (CARGO COMPT)
CARGO DOOR OPENED IN FLIGHT. DOOR SECURED PER DER INSTRUCTIONS. ACFT FERRIED TO MACON FOR REPAIRS.
1997
Part: O-RING — CUT (FUEL PRESS LINE)
REPORT FROM TOWER OF FUEL COMING FROM NR 2 ENGINE AFTER TAKEOFF. NR 2 FUEL FLOW 4000 NR HR HIGHER THAN OTHERS. ON REDUCTION OF THROTTLE NR 2 ENGINE STOPPED PRODUCING THRUST/FLAMEOUT, WENT THROUGH PRECAUTIONARY IN FLIGHT ENGINE SHUTDOWN PROCEDURE AT 1615Z AS PER QRH. FOUND NR 2 ENGINE FUEL PRESSURE AND PUMP VALVE IN LINE, NUTS HAD BACKED OF TO THE POINT OF EXPOSING O-RING. ALSO, FOUND O-RING CUT IN HALF. REMOVED AND REPLACED O-RING AND FLANGE NUTS, RESECURED IN LINE TO VALVE, OPS AND LEAK CHECKS GOOD ON GROUND ENGINE RUN-UP IAW DC-8 JET RUN-UP HANDBOOK, NO DEFECTS.
Part: CENTERING ASSY — MALFUNCTIONED (ELEVATOR CONTL)
AIR TURNBACK, ELEVATOR EXTREMELY STIFF IN FLIGHT AND VERY SLOW TO RESPOND TO INPUTS. REMOVED AND REPLACED ELEVATOR LOAD FEEL/CENTERING ASSEMBLY IAW MM 27-30-4. OPS CHECK NORMAL, NO DEFECTS NOTED.
Part: PLATING — CRACKED (NR 1 PYLON)
ON POST-FLIGHT INSPECTION, FOUND 1 EACH .50 INCH CRACK AND 1 EACH 5.50 INCH CRACK IN OTBD SIDE OF NR 1 PYLON AT YN 225.279. STOP DRILLED CRACK ON PYLON PANEL. FABRICATED TWO REPAIR DOUBLERS AND INSTALLED AND SEALED IAW DC-8 SRM TR 54-2-2, FIGURE 6, PAGE 20, PARA. 2 AND SEALED PYLON PANEL IAW DC-8 SRM 51-1-16.
Part: PLATING — CRACKED (NR 1 PYLON)
ON POST-FLIGHT INSPECTION, FOUND 1 EACH .50 INCH CRACK AND 1 EACH 5.50 INCH CRACK IN OUTBOARD SIDE OF NR 1 PLYON AT YN225.279. TEMPORARY REPAIR INSTALLED ON 970125 FOR ONE-TIME FERRY FLIGHT IAW DER APPROVED SKETCH B99-T01 FROM KMEM TO KMCN. STOP DRILLED CRACK ON PYLON PANEL. FABRICATED TWO EACH REPAIR DOUBLERS AND INSTALLED AND SEALED IAW DC-8 SRM TR 54-2-2, FIGURE 6, PAGE 20, PARA 2 AND SEALED PYLON PANEL IAW DC-8 SRM 51-1-16.
1996
Part: O-RING — FAILED (SLOT CONTL VLV)
ON CLIMBOUT, LOST HYDRAULIC SYSTEM PRESSURE, STOPPED QUANTITY LOSS AT 6 GALLONS INDICATED. LOSS OF HYDRAULIC SYSTEM AND PRESSURE EMERGENCY CHECKLIST FOLLOWED. MAINTENANCE REPLACED THE O-RING IN THE SLOT CONTROL VALVE MOUNT, SERVICED THE HYDRAULIC SYSTEM. HYDRAULIC POWERED FLT CONTROLS OPERATED NORMALLY ON GROUND CHECK, NO LEAKS NOTED.
1995
Part: RETRACT MECH — MALFUNCTIONED (NLG)
FLT - NR 651 - KPDX-KDAY - ON GEAR RETRACTION, A LOUD NOISE AND VIBRATION WAS NOTICED IN THE NOSE AREA. THE LANDING GEAR WAS RECYCLED WITH THE SAME RESULTS. RETURNED TO KPDX. MAINTENANCE INSPECTED THE UPLATCH FITTINGS, TRUNNION AND THE NOSE WHEEL WELL. NO DEFECTS WERE NOTED. (M)