What was found
AFTER TAKEOFF, CREW WAS NOT ABLE TO RETRACT FLAPS TO ZERO. RETURNED TO FIELD AND LANDED SAFELY WITH NO FURTHER INCIDENT. THE CORRECTIVE ACTION WAS THE FLAP LIMIT CAM SWITCH S-4 WAS RIGGED. THEREFORE NO PARTS WERE USED.
- Difficulty date
- July 11, 2005
- Submitted
- July 15, 2005
- Operation
- Air carrier
- Aircraft
- N155YV
- Make and model
- Beech 1900D
- Aircraft serial
- 155YV
- Aircraft time
- 18,769 hours, 28,399 cycles
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Switch
- Condition
- Out Of Rig
- Location
- Te Flaps
- Stage of operation
- TO
- How discovered
- O
- Nature of condition
- F, J
- Precautionary procedure
- C
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.