What was found
ENLARGED HOLES IN FUSELAGE SKIN AT BEAM 10 BETWEEN FRAME 68-69 AND AT FRAME 67 BETWEEN STRINGER 43-44 RT, BULK CARGO DOOR CUT OUT. REPLACEMENT OF BEAM 10 IAW SRM 51-72-10.
- Difficulty date
- September 24, 2007
- Submitted
- September 24, 2007
- Operation
- Air carrier
- Aircraft
- N803FD
- Make and model
- Airbus A310324
- Aircraft serial
- 378
- Aircraft time
- 36,313 hours, 12,040 cycles
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin
- Condition
- Damaged
- Location
- Zone 100
- 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.