What was found
STRUCTURAL DEFECT DISCOVERED DURING SCHEDULED INSPECTION (PHASE 5). METAL FATIGUE, CANTED BULKHEAD, STRUCTURAL REPAIR INITIATED, AND WORK IS IN PROCESS.
- Difficulty date
- September 10, 2002
- Submitted
- November 27, 2002
- Operation
- Air carrier
- Aircraft
- N924FE
- Make and model
- Cessna 208B
- Aircraft serial
- 208B0024
- Engine
- Pwa PT6A11
- System (JASC)
- 5312 · Fuselage Main, Bulkhead
- Part
- Bulkhead
- Part number
- 26120605
- Condition
- Cracked
- Location
- Fuselage
- Part time
- 6,971 hours
- 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.