What was found
(CAN) ENGINE DID NOT PRODUCE TAKEOFF POWER AND WAS DIFFICULT TO START. INVESTIGATION FOUND THE TWO STAGE FUEL PUMP WAS NOT DELIVERING THE VOLUME OF FUEL REQUIRED, DUE TO A SHEARED DRIVE.
- Difficulty date
- December 26, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Airbus A320231
- Engine
- Iae V2500A1
- System (JASC)
- 7314 · Engine Fuel Pump
- Part
- Fuel Pump
- Part number
- 50087350
- Condition
- Sheared Shaft
- Location
- Low Stage
- Part time
- 7,358 hours
- Component
- Sundstrand
- Stage of operation
- TO
- Nature of condition
- R
- Precautionary procedure
- C, D
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.