What was found
RAMP REPORTS FUEL LEAK ON ENGINE 2 AFTER ENGINE START. ACCOMPLISHED IDLE ENG RUN TWICE, STEADY STREAM FUEL LEAKS FROM CORE DRAIN BEYOND LIMITS OF MM. ISOLATED TO SLAVE LPC BLEED ACTUATOR. REPLACED ACTUATOR PER MM, IDLE LEAK CHECK OK.
- Difficulty date
- April 12, 2012
- Submitted
- April 13, 2012
- Operation
- Air carrier
- Aircraft
- N457UA
- Make and model
- Airbus A320232
- Aircraft serial
- 1146
- Aircraft time
- 40,458 hours, 16,945 cycles
- Engine
- Iae V2527A5
- System (JASC)
- 7530 · Compressor Bleed Control
- Part
- Actuator
- Part number
- 5L0039
- Part serial
- 252
- Condition
- Leaking
- Location
- Nr 2 Engine
- 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.