Service difficulty report · Bleed Valve · Airbus A320214

Difficulty date
January 3, 2005
Submitted
January 6, 2005
Operation
Air carrier
Aircraft
N268AV
Make and model
Airbus A320214
Aircraft serial
2175
Aircraft time
1,959 hours, 810 cycles
Part
Bleed Valve
Part number
2293B010000
Part serial
11380
Condition
Cracked
Location
Nr 2 Engine
Part time
1,959 hours, 810 cycles
Stage of operation
DE
How discovered
O
Nature of condition
R, Y, J
Precautionary procedure
O

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

What was found

NR 2 ENG BEGAN COMPRESSOR STALLING. FLT CREW NOTICED THAT N1 WENT TO 43 PERCENT & FLUCTUATED BETWEEN 43 & 45 PERCENT. DECLARED AN EMERGENCY. AT ABOUT 10,000 FT, NR 2 ENGINE STABILIZED & APPEARED TO OPERATE NORMALLY. A VISUAL APPROACH TO A LANDING ON RUNWAY 6 AT RSW FLOWN. DURING ROLLOUT, AN ECAM WARNING, NR 2 ENG FAIL RECEIVED & ENG SHUTDOWN. LANDING ENDED W/O FURTHER INCIDENT. MX PERFORMED FAULT ISOLATION PROCEDURE PER TSM 73-00-00-810-865 & 72-00-00-810-807. FOUND FAULTY "IP BLEED CHECK VALVE". R&R IP CK VALVE PER AMM 36-11-44-000-040 & OPS & LEAK CK PER AMM 36-11-41-200-001, WITH NO FAULT FOUND. PERFORMED PRECAUTIONARY BOROSCOPE INSPECTION OF NR 2 ENG WITH NO UNSERVICEABLE DEFECTS NOTED. A/C RETURNED TO SER

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