What was found
(CAN) AFTER TAKEOFF, WHEN FLAPS SELECTED FROM 17 DEGREES TO ZERO DEGREES, THE FLAPS DID NOT RETRACT. AIRCRAFT RETURNED TO BASE AND LANDED SAFELY. MAINTENANCE CHECK FOUND FLAP ASYMMETRY SWITCH WAS DEFECTIVE.
- Difficulty date
- April 6, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Beech 1900D
- Engine
- Pwa PT6A67D
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Switch
- Part number
- BZ7RW82255518T
- Condition
- Failed
- Location
- Te Flap
- Stage of operation
- CL
- Nature of condition
- F
- Precautionary procedure
- A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.