What was found
ON SHORT FINAL THE CABLE BROKE AND THE LEFT FLAP RETRACTED WHICH CAUSED A SPLIT FLAP CONDITION. REPLACED CABLE . INSPECTED THE OTHER FLAP CABLES, NO DEFECTS NOTED.
- Difficulty date
- August 14, 2001
- Submitted
- September 10, 2001
- Operation
- Air carrier
- Aircraft
- N7947Q
- Make and model
- Cessna 402B
- Aircraft serial
- 402B0397
- Engine
- Cont TSIO520*
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Control Cable
- Part number
- 50000083CR
- Condition
- Broken
- Location
- T/E Flap
- Part time
- 12,101 hours
- Stage of operation
- AP
- How discovered
- O
- Nature of condition
- F, J
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.