What was found
(CAN) FLAP CABLE RT WING INBD FLAP SHEARED APPROX .2500 INCH TO .1250 INCH INSIDE THE SHEATH BODY. THE MM CALLS FOR A REPLACEMENT OF THE CABLE AT 22,500 CYCLES.
- Difficulty date
- July 15, 2009
- Submitted
- August 3, 2009
- Operation
- General aviation
- Make and model
- Beech 1900D
- Aircraft time
- 18,074 hours
- Engine
- Pwa PT6A67D
- Propeller
- Hartzl HCE4A3I
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Shaft
- Part number
- 1013800002
- Condition
- Unserviceable
- Location
- Inbd Rt Flap
- Stage of operation
- AP
- How discovered
- 9
- Nature of condition
- J
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.