What was found
(CAN) THE PILOT REPORTED A FLAP SPLIT ASYMMETRY OCCURRED DURING FLIGHT. MAINTENANCE FOUND THAT THE RT INBD FLAP FLEX SHAFT WAS BROKEN. A HEAVY AMOUNT OF CORROSION WAS NOTICED AT THE BREAK LOCATION.
- Difficulty date
- October 15, 2014
- Submitted
- March 12, 2015
- Operation
- General aviation
- Make and model
- Beech 1900D
- Aircraft time
- 11,304 hours
- Engine
- Pwa PT6A67D
- Propeller
- Hartzl HCE4A3I
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Shaft
- Part number
- 1013800002
- Condition
- Broken
- Location
- Rt Wing Te Flaps
- Stage of operation
- NR
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.