What was found
FUSELAGE TAIL SECTION FR84, 1EA CROSS STRUT GOT CORROSION AT STR14 LT 1. REMOVED THE CROSS STRUT IAW SRM 51-40-20 AND 51-40-21. INSTALLED NEW CROSS STRUT WITH FASTEN REF SRM 51-40-21. THE REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100.
- Difficulty date
- July 27, 2011
- Submitted
- July 27, 2011
- Operation
- Air carrier
- Aircraft
- N428FE
- Make and model
- Airbus A310203
- Aircraft serial
- 248
- Aircraft time
- 40,052 hours, 27,074 cycles
- System (JASC)
- 5310 · Fuselage Main, Structure
- Part
- Crossbeam
- Part number
- A5398842420400
- Condition
- Corroded
- 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.