What was found
(CAN) ON START, FLAPS WOULD NOT EXTEND FULLY TO 5 DEGREES. AIRCRAFT SYSTEM POWERED DOWN THEN POWERED UP AND FLAPS OPERATED NORMAL. FLAP SLAT ELECTRONIC UNIT FAULT FLAP LEVER ROTARY VARIABLE DISPLACEMENT. TRANSDUCER REPLACED.
- Difficulty date
- June 5, 1998
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Make and model
- Boeing 767233
- Engine
- Pwa JT9D7R4D
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Transducer
- Part number
- 3A1260A
- Condition
- Faulty
- Location
- Te Flaps
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.