# SDR CA960320541

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: February 7, 1996
- Submitted: March 26, 2000
- Operation: Air carrier
- Make and model: Airbus A320-211
- Registry model: [Airbus A320-211](https://openairdocs.org/model/airbus-industrie-a320-211) (OpenAirDocs)
- Engine: Cfmint CFM565A1
- System (JASC): [7532 · Compressor Bleed Valve](https://openairdocs.org/jasc/7532)
- Part: Bleed Valve
- Part number: 3017808040
- Condition: Faulty
- Location: #1 Engine
- Stage of operation: CL
- Nature of condition: O
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/CA960320541

## Discrepancy

(CAN) AIRCRAFT RETURNED TO ORIGIN AFTER TAKEOFF DUE TO #1 ENGINE SURGING. EGT EXCEEDENCE. FOUND ENGINE COMPRESSOR BLEED VALVE AT FAULT. CHANGED #1 ENGINE VARIABLE BLEED VALVE SENSOR. FADEC TEST CARRIED OUT ON BOTH CHANNELS.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
