Service difficulty report · Compressor · Airbus A320232

Difficulty date
October 13, 2006
Submitted
October 24, 2006
Operation
Air carrier
Aircraft
N425UA
Make and model
Airbus A320232
Aircraft serial
508
Aircraft time
40,201 hours, 14,488 cycles
Engine
Iae V2527A5
Engine time
28,321 hours, 10,650 cycles
Part
Compressor
Condition
Stalled
Location
Nr 2 Engine
Stage of operation
CL
How discovered
O
Nature of condition
R, J
Precautionary procedure
A

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

RETURNED TO FIELD DUE TO NR 2 ENGINE COMPRESSOR STALL. NR 2 ENGINE COMPRESSOR STALLED DURING CLIMB FROM LAX. LOST 50% THRUST FOR ABOUT 5 SECONDS. ALL INDICATIONS WERE NORMAL AND AIRCRAFT RETURNED TO FIELD. NO EMERGENCY DECLARED. NO OVER WEIGHT LANDING. THE CREW SUSPECTS PRIOR DEPARTING AIRCRAFT WAKE TURBULENCE AT 1500-2000 FT CAUSED STALL. POST FLIGHT REPORT SHOWS ENGINE 2 STALLED. 7TH STAGE BLEED LOWER LEFT VALVE DID NOT PASS AMM TEST. REPLACED VALVE. ALL OTHERS TESTS GOOD. ENGINEERING STATES WAKE TURBULENCE FROM PRIOR DEPARTING AIRCRAFT IS LIKELY CAUSE. THE 7TH STAGE BLEED VALVE THAT WAS CHANGED IS ONLY USED FOR ENGINE START NOT ENGINE STABILITY.

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