What was found
(CAN) UNABLE TO RETRACT FLAPS TO LESS THAN 15 DEGREES DUE TO FLAP LEVER JAMMING. TROUBLESHOOTING REVEALED FLAP CONTROL LEVER INTERFERENCE CAUSED BY LOOSE BOLT. BOLT TIGHTENED AND LEVER MECHANISM OPERATED NORMALLY CHECKED SERVICEABLE.
- Difficulty date
- January 31, 1997
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Doug DC932
- Engine
- Pwa JT8D7
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Bolt
- Condition
- Loose
- Location
- Flap Control
- Stage of operation
- AP
- Nature of condition
- F
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.