# SDR 05FDEA01967

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: July 15, 2005
- Submitted: July 18, 2005
- Operation: Air carrier
- Aircraft: N417FE
- Make and model: Airbus A310
- Registry model: [Airbus A310](https://openairdocs.org/model/airbus-a310) (OpenAirDocs)
- Aircraft serial: 333
- Aircraft time: 39,030 hours, 19,857 cycles
- Engine: Pwa JT9D7R4E1
- System (JASC): [7532 · Compressor Bleed Valve](https://openairdocs.org/jasc/7532)
- Part: Bleed Valve
- Condition: Malfunctioned
- Location: Nr 2
- Stage of operation: CL
- How discovered: O
- Nature of condition: M, J
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/05FDEA01967

## Discrepancy

AFTER TAKEOFF FROM LISBON HAD NR 2 BLEED VALVE FAULT.  DURING RETURN TO LISBON RESET NR 2 BLEED AND FOUND  FOLLOWING CONDITIONS:   AT 3000 FT NR 1 BLEED TEMP 175  / NR 2 BLEED TEMP 175.  THE OVERHEAT WITHIN 2 MINS AT 210 - 220  WITH  SUBSEQUENT BLEED VALVE NR 2 FAULT.  ON GROUND WITH HP VALVE SELECTED OFF, EVEN AT  INCREASE POWER SETTINGS NO PROBLEM NOTED.   FAN AIR VALVE REPLACED IAW AMM 36-11-16-4. NO FAULD FOUND ON ENGINE RUN-UP,PERFORMED IAW  AMM 71-00-00-5.

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