# SDR UALA2008111306036

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: October 8, 2008
- Submitted: November 21, 2008
- Operation: Air carrier
- Aircraft: [N811UA](https://openairdocs.org/aircraft/N811UA), registered now
- Make and model: Airbus A319-131
- Registry model: [Airbus A319-131](https://openairdocs.org/model/airbus-industrie-a319-131) (OpenAirDocs)
- Aircraft serial: 847
- Aircraft time: 36,428 hours, 13,926 cycles
- Engine: Iae V2522A5
- System (JASC): [7532 · Compressor Bleed Valve](https://openairdocs.org/jasc/7532)
- Part: Bleed Valve
- Condition: Broken
- Location: Nr 1 Engine
- Stage of operation: CL
- How discovered: O
- Nature of condition: W
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/UALA2008111306036

## Discrepancy

ENG 1 BLEED FAULT.  RTFL.  AIR CREW COMMENTS:  ON CLIMBOUT THRU 3K FEET ECAM AIR ENG NR 1 BLEED FAULT; UNABLE TO RETURN NORMAL.  FOUND CONNECTOR FOR VALVE 4001HA ON NR 1 ENGINE BROKEN.  RE-ACTIVATED HPV.  CREATED NEW ITEM FOR BLEED PRESS REG VALVE 4001HA RPL AND CONNECTOR REPAIR.  REPLACED CONNECTOR BACKSHELL ON CONNECTOR THAT CONNECTS TO NR 1 BLEED PRESSURE REGULATOR.  PRESSURE REG BLEED VALVE REMOVED.  UNABLE TO INSTALL NEW VALVE DUE TO BROKEN CONNECTOR.  INSTALLED NEW VALVE.  ACCOMPLISH OP TEST OF BLEED PRESS-REG VALVE WITH ENG IN OPERATION.  OPS CHECK NORMAL.

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