What was found
REAR FUSELAGE FR 86, 5" INCHES INBD OF STR 15L, AFT CROSSBEAM HAS 2 EA PLACES OF EXFOLIATION CORROSION, APPR 2" INCHES SQUARE. R & R CROSSBEAM AT FR 86, STR 15L IAW SRM 51-72-10 PAR 5&6 AND SRM 51-40-21, PAGES 1,2,3.
- Difficulty date
- December 4, 2010
- Submitted
- December 6, 2010
- Operation
- Air carrier
- Aircraft
- N443FE
- Make and model
- Airbus A310203
- Aircraft serial
- 283
- Aircraft time
- 42,386 hours, 21,622 cycles
- Engine
- Ge CF680A3
- System (JASC)
- 5310 · Fuselage Main, Structure
- Part
- Crossbeam
- Part number
- A53988624200
- Condition
- Corroded
- Location
- Zone 200
- 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.