What was found
(CAN)IN CLIMB A REPORTED LOSS OF POWER OCCURRED ON #1 ENGINE. POST FLIGHT INSPECTION DETERMINED THE FAULT WAS THE HYDROMECHANICAL FUEL CONTROL UNIT WHICH WAS REPLACED.
- Difficulty date
- October 2, 1995
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Pwa PW126A
- System (JASC)
- 7322 · Fuel Control/Reciprocating Engines
- Part
- Fuel Control
- Condition
- Faulty
- Location
- Nr 1 Engine
- Stage of operation
- CL
- Nature of condition
- R
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.