What was found
(CAN) DURING CLIMB, THE ENGINE EXPERIENCED AN UNCOMMANDED INCREASE IN TORQUE AND FAILED TO RESPOND TO THROTTLE INPUT. THE ENGINE WAS SHUTDOWN IN FLIGHT. SUBSEQUENT INVESTIGATION REVEALED A FRACTURED FUEL CONTROL COUPLING SHAFT.
- Difficulty date
- February 3, 2005
- Submitted
- April 1, 2005
- Operation
- General aviation
- Make and model
- Beech C90A
- Engine
- Pwa PT6A21
- System (JASC)
- 7321 · Fuel Control/Turbine Engines
- Part
- Fcu
- Part number
- 32447452
- Part serial
- B36008
- Condition
- Malfunctioned
- Location
- Engine
- Stage of operation
- CL
- How discovered
- O
- Nature of condition
- E, J
- Precautionary procedure
- E, A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.