What was found
CREW REPORTED ENGINE NR 1 STALL (LARGE BANG) AT ABOUT 1,000 FT AGL. ENGINE OPERATION WAS NORMAL AFTER BUT AIRCRAFT RETURNED TO FIELD. MAINTENANCE REPLACED NR 1 ENGINE STAGE 7C BLEED VALVE IAW AIRBUS MAINTENANCE MANUAL 75-32-52.
- Difficulty date
- October 19, 2011
- Submitted
- October 21, 2011
- Operation
- Air carrier
- Aircraft
- N519UW
- Make and model
- Airbus A321231
- Aircraft serial
- 3881
- Aircraft time
- 10,235 hours, 3,147 cycles
- Engine
- Iae V2533A5
- System (JASC)
- 7532 · Compressor Bleed Valve
- Part
- Bleed Valve
- Part number
- EB101729B
- Part serial
- HAB1040
- Condition
- Defective
- Location
- Nr 1 Engine
- Part time
- 10,235 hours, 3,147 cycles
- Stage of operation
- CL
- How discovered
- O
- Nature of condition
- R
- Precautionary procedure
- A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.