What was found
FUEL PRESSURE INDICATION WAS 75 PSI WITH THE ENGINE SHUT DOWN AND THE FUEL BOOST PUMP SHUT OFF. REMOVED TRANSDUCER AND INSTALLED NEW FUEL PRESSURE TRANSDUCER. GROUND OPERATION OF FUEL SYSTEM CHECKED NORMAL.
- Difficulty date
- June 15, 2002
- Submitted
- June 25, 2002
- Operation
- General aviation
- Aircraft
- N865AF
- Make and model
- Grob G120A
- Aircraft serial
- 85005
- Engine
- Lyc AEIO540D4D5
- System (JASC)
- 7333 · Fuel Flow Sensor
- Part
- Transducer
- Part number
- P16575GB4A
- Condition
- Failed
- Location
- Fuel System
- Stage of operation
- NR
- How discovered
- O
- Nature of condition
- O
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.