What was found
ATB DUE TO ECAM ENG 2 BLEED FAULT. REMOVED AND REPLACED #2 ENGINE FAN AIR VALVE PER AMM 36-11-54. BITE TEST OF LEFT ENGINE BLEED SYSTEM GOOD. PERFORMED IDLE RUN OF #2 ENGINE. ALL CHECKS GOOD. OK TO CONTINUE
- Difficulty date
- May 25, 2025
- Submitted
- May 27, 2025
- Operation
- Air carrier
- Aircraft
- N208HA
- Make and model
- Airbus A321271N
- Aircraft serial
- 08123
- Aircraft time
- 18,826 hours, 4,134 cycles
- Engine
- Iae PW1133GAJM
- Engine time
- 19,214 hours, 4,322 cycles
- System (JASC)
- 7500 · Engine Bleed Air System
- Part
- Valve
- Condition
- Faulted
- Location
- Zone 400
- Stage of operation
- NR
- How discovered
- O
- Nature of condition
- J
- Precautionary procedure
- A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.