What was found
ENGINE DRIVEN MECHANICAL FUEL PUMP WILL ONLY OUTPUT 10.5 GPH AT WIDE OPEN THROTTLE AFTER ADJUSTMENT. OUTPUT SHOULD BE IN THE 17-18 GPH RANGE.
- Difficulty date
- June 27, 2012
- Submitted
- October 19, 2012
- Operation
- General aviation
- Aircraft
- N488DA
- Make and model
- Cirrus SR20
- Aircraft serial
- 201833
- Aircraft time
- 4,027 hours
- Engine
- Cont IO360ES
- Engine time
- 174 hours
- Propeller
- Hartzl PHCJ3YF1
- System (JASC)
- 7314 · Engine Fuel Pump
- Part
- Pump
- Part number
- R64936874A4
- Part serial
- B12BA188R
- Condition
- Out Of Tolerance
- Location
- Fuel System
- Part time
- 174 hours
- Stage of operation
- IN
- How discovered
- V
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.