# SDR CA111205004

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: December 1, 2011
- Submitted: September 14, 2015
- Operation: General aviation
- Make and model: Airbus A319-114
- Registry model: [Airbus A319-114](https://openairdocs.org/model/airbus-a319-114) (OpenAirDocs)
- Aircraft time: 38,603 hours
- Engine: Cfmint CFM565A5
- System (JASC): [7532 · Compressor Bleed Valve](https://openairdocs.org/jasc/7532)
- Part: Bleed Valve
- Part number: 6714D060000
- Condition: Failed
- Location: Nr 2
- Part time: 37,980 hours
- Stage of operation: CR
- How discovered: O
- Nature of condition: J
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/CA111205004

## Discrepancy

(CAN) DISPATCH UNDER ONE ENG BLEED INOP, RECEIVED NR 2 ENG AIR BLEED FAULT & NR 2 PACK OVERHEAT INDICATION, BLEED LOSS DRILL CARRIED OUT, PACK NEVER SHUT DOWN. DIVERSION. NR 2 PACK PRECOOLER TEMP NOTED AT 295DEG C & AMBER X.   NR 2 ENGINE BLEED PRESSURE REGULATOR VALVE REPLACED AS PER AMM 36-11-52 PB 401. BMC NR 2 REPLACED AS PER AMM 36-20-11 GROUND CHECKED SERVICABLE.

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