What was found
(CAN) RAPID DESCENT DUE TO RECURRING BLEED FAULTY OF NR 2 SYSTEM. REPLACED NR 2 ENGINE FAN VALVE, REPLACED 6730B01, NR 1 BLEED PRESSURE REGULATOR VALVE (P/N 6714C01) AND REPLACED TEMPERATURE CONTROL THERMOSTAT (P/N 342D030000).
- Difficulty date
- August 2, 2000
- Submitted
- January 19, 2001
- Operation
- Air carrier
- Make and model
- Airbus A320211
- Aircraft time
- 30,253 hours
- Engine
- Cfmint CFM565A1
- System (JASC)
- 7532 · Compressor Bleed Valve
- Part
- Bleed Valve
- Part number
- 6730B01
- Condition
- Failed
- Location
- Nr 2 Engine
- Stage of operation
- CR
- How discovered
- O
- Nature of condition
- J
- Precautionary procedure
- B
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.