What was found
(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.
- Difficulty date
- February 7, 1996
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Make and model
- Airbus A320211
- Engine
- Cfmint CFM565A1
- System (JASC)
- 7532 · Compressor Bleed Valve
- Part
- Bleed Valve
- Part number
- 3017808040
- Condition
- Faulty
- Location
- #1 Engine
- Stage of operation
- CL
- Nature of condition
- O
- Precautionary procedure
- A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.