What was found
DURING GROUND RUN, TESTED RUDDER TRIM SWITCH. RUDDER TRIM MOVED TO THE LEFT BUT WOULD NOT MOVE TO THE RIGHT. PROBABLE CAUSE IS INTERNAL FAILURE OF THE SWITCH CIRCUITS.
- Difficulty date
- July 5, 2002
- Submitted
- July 29, 2002
- Operation
- Air carrier
- Aircraft
- N8112T
- Make and model
- Beech F33A
- Aircraft serial
- CE1539
- Engine
- Cont IO520BB
- System (JASC)
- 2721 · Rudder Tab Control System
- Part
- Trim Switch
- Part number
- 972394
- Part serial
- 10
- Condition
- Failed
- Location
- Rudder
- Part time
- 257 hours
- Stage of operation
- IN
- How discovered
- C
- Nature of condition
- L
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.