What was found
THE BOLT WAS FROZEN TO THE BUSHING SLEEVE. THIS PREVENTED THE BOLT FROM ROTATING INSIDE THE BUSHINGS AND ELONGATED THE BOLT HOLE THROUGH THE MOUNTING BRACKET. (K)
- Difficulty date
- April 4, 2008
- Submitted
- July 7, 2008
- Operation
- Air carrier
- Aircraft
- N9331B
- Make and model
- Cessna 208B
- Aircraft serial
- 208B0055
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Bellcrank
- Part number
- 26220911
- Condition
- Damaged
- Location
- T/E Flap
- 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.