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. ALSO, THE SLEEVE CORRODED TO THE BELLCRANK. (K)
- Difficulty date
- May 8, 2008
- Submitted
- July 7, 2008
- Operation
- Air carrier
- Aircraft
- N9760B
- Make and model
- Cessna 208B
- Aircraft serial
- 208B0102
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Bellcrank
- Part number
- 26220919
- 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.