What was found
FLAP CABLE ATTACH BOLTS AT WING BELLCRANK FOUND TO BE INSTALLED UPSIDE DOWN. IPC SHOWS BOLTS INSTALLED HEAD UP. NUT STRIKES ADJACENT RIB AT FLAPS DOWN POSITION. NO RECORD OF FLAP MAINTENANCE IN A/C RECORDS.
- Difficulty date
- December 26, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Aircraft
- N9622V
- Make and model
- Chris A1
- Aircraft serial
- 1154
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Flap Arm
- Condition
- Bolts Incorrect
- Location
- Wing Bellcrank
- Part time
- 595 hours
- Stage of operation
- IN
- Nature of condition
- W
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.