# SDR 07FDEA05109

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: December 20, 2007
- Submitted: December 26, 2007
- Operation: Air carrier
- Aircraft: N448FE
- Make and model: Airbus A310-222
- Registry model: [Airbus A310-222](https://openairdocs.org/model/airbus-industrie-a310-222) (OpenAirDocs)
- Aircraft serial: 260
- Aircraft time: 39,477 hours, 27,798 cycles
- Engine: Pwa JT9D*
- Engine time: 29,103 hours, 11,951 cycles
- System (JASC): [7532 · Compressor Bleed Valve](https://openairdocs.org/jasc/7532)
- Part: Bleed Valve
- Part number: 9788422
- Part serial: 821
- Condition: Cracked
- Location: Nr 1 Engine
- Part time: 3,576 hours, 2,124 cycles
- Stage of operation: CL
- 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/07FDEA05109

## Discrepancy

DURING CLIMB TO CRUISE ALTITUDE, ECAM PRESENTED AN  ADVISORY PAGE FOR NR 1 ENG NAC TEMP AT 200.  SELECTED NR 1 BLEED VALVE OFF AND REDUCED POWER ON  NR 1 WITH NO CHANGE IN NR 1 NAC TEMP.  AFTER THROTTLE WAS REDUCED TO ALMOST IDLE SETTING, NR 1 NAC TEMP FELL TO 190  DEGREES.  THROTTLE REMAINED AT IDLE UNTIL SHORT FINAL APPROACH.  DURING DESCENT WITH NR 1 AT IDLE, ADVISORY INDICATION WENT AWAY AFTER 10-15 MINUTES.  FOUND A SMALL CRACK ON FAN AIR VALVE, FOUND A COUPLE OF SENSE LINES TO BE BAD.  REMOVED AND REPLACED FAN AIR VALVE, REMOVED AND REPLACED SENSE LINES AND NACELLE TEMP SENSOR.

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