What was found
(CAN) RAMP CREW REPORT LARGE FUEL SPILL FROM ENGINE NR 2 AFTER START-UP. CFR NOTIFIED. RT TRANSIENT BLEED VALVE, REPLACED IAW AMM 75-26-10. ENGINE START C/O TWICE, NOT LEAK NOTICED, CONSIDER SERVICE WP 07337, CS 35263.
- Difficulty date
- October 12, 2012
- Submitted
- September 14, 2015
- Operation
- General aviation
- Make and model
- Airbus A319112
- Aircraft time
- 36,860 hours
- Engine
- Cfmint CFM565B6
- System (JASC)
- 7310 · Engine Fuel Distribution
- Part
- Valve
- Part number
- 1882M11P01
- Condition
- Leaking
- Location
- Fuel Sys
- Stage of operation
- TX
- How discovered
- 9
- Nature of condition
- K
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.