What was found
(CAN) AFTER NR 1 ENGINE BLEED AIR FAULT ILLUMINATED, AIRCRAFT LANDED DUE TO ICING CONDITION FORECAST. REPLACED PRESSURE REGULATOR VALVE AND TRANSDUCER 7HA1.
- Difficulty date
- October 5, 1999
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Make and model
- Airbus A319114
- Engine
- Ge CFM565A
- System (JASC)
- 7500 · Engine Bleed Air System
- Part
- Valve
- Condition
- Failed
- Location
- Nr 1 Engine
- Component
- CFM565A5
- Stage of operation
- CL
- Nature of condition
- J
- Precautionary procedure
- A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.