Service difficulty report · Bleed Valve · Airbus A320232

Difficulty date
March 27, 2006
Submitted
March 31, 2006
Operation
Air carrier
Aircraft
N664AW
Make and model
Airbus A320232
Aircraft serial
1621
Aircraft time
16,430 hours, 6,284 cycles
Engine
Iae V2527A5
Part
Bleed Valve
Part number
AC69924
Part serial
EGM294
Condition
Malfunctioned
Location
Nr 1 Engine
Part time
16,430 hours, 6,284 cycles
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

DURING CLIMB-OUT, APPROX 8500' REPORTED NR 1 ENG COMPRESSOR STALL WITH A LOUD BANG, FIREBALL, & EPR DROP TO NEARLY "0" THEN RECOVERY. REPORTED ECAM ANNUNCIATED "COMPRESSOR STALL" THEN CLEARED AS ENG RESUMED NORMAL OPS. RETURNED TO ATL. MX T/S IAW AIRBUS 320 TSM. COMPLIED WITH VSV ACT LINKAGE LUBE IAW AIRBUS 320 MM. PERFORMED BOROSCOPE OF NR 1 ENG IAW AMM, NO DEFECTS NOTED. REPLACED 7TH STAGE BLEED VLE IAW MM. PWR ASSURANCE TESTS WERE GOOD ON NR 1 ENG IAW AWA TASK CARD F5M71312. DURING POWER ASSURANCE RUNS, THE NR 2 ENG EXPERIENCED COMPRESSOR STALL. VSV ACT ON NR 2 ENG LUBED & BORESCOPED NR 2 ENG IAW AMM. NO DEFECTS NOTED. ANOTHER PWR ASSURANCE RUN ACCOMP AND ALL SYSTEMS OPS NORMAL ON BOTH ENG.

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