What was found
DURING A MAINTENANCE VISIT FOUND HOLE DAMAGE TO FLOOR PANEL AT STA. 55 X= -40, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 51-1-4 & 53-2-0.
- Difficulty date
- January 17, 2001
- Submitted
- July 25, 2001
- Operation
- Air carrier
- Aircraft
- N801GP
- Make and model
- Doug DC871F
- Aircraft serial
- 46039
- Aircraft time
- 79,863 hours, 31,419 cycles
- System (JASC)
- 5321 · Fuselage Floor Panel
- Part
- Floor Panel
- Condition
- Damaged
- Location
- Fuselage
- Stage of operation
- IN
- How discovered
- V
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.