# SDR ANCF2012040800119

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: April 8, 2012
- Submitted: April 9, 2012
- Operation: Air carrier
- Aircraft: N592EL
- Make and model: Airbus A318-111
- Registry model: [Airbus A318-111](https://openairdocs.org/model/airbus-a318-111) (OpenAirDocs)
- Aircraft serial: 2358
- Aircraft time: 2,328,393 hours, 13,739 cycles
- System (JASC): [7700 · Engine Indicating System](https://openairdocs.org/jasc/7700)
- Part: Warning Light
- Condition: False Activation
- Location: Nr 1 Engine
- Part time: 2,328,393 hours, 13,739 cycles
- Stage of operation: CL
- How discovered: O
- Nature of condition: N
- Precautionary procedure: A
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/ANCF2012040800119

## Discrepancy

DURING FLIGHT,  NR 1 ENGINE COMPRESSOR VANE FAULT ECAM ILLUMINATED.  IAW AMM 73-29-00-710-040B OPS TEST OF THE FADEC ON GROUND PERFORMED WITH ENGINE MOTORING & MCDU SHOW NO FAULT RECORDED. IAW AMM 75-31-20-820-001, VBV SYSTEM WAS CLOSED DIMENSION A AND B WERE MEASURED.  FOUND IN LIMITS & CHECK OF VBU POSITION (ONLY WITH AIDS OPTION) IAW SUB TASK 75-31-00- -010-081-A RVDT SHOW N 0.2 ALL TEST SATISFACTORY SATISFACTORY.  IAW AMM 75-31-10-000-002- A/400-002-A THE LEFT BLEED VALVE FUEL GEAR MOTOR ASSEMBLY AND AMM 75-31-70-000-002- A/400-002-A THE LT VARIABLE BLEED VALVE POSITION SENSOR REPLACED.  IAW AMM 73-29-00-710-040 FADEC GROUND TEST WAS PERFORMED AND IAW AMM 71-00-00-710-006 MINIMUM IDLE CHECK WAS PERFORMED THE RESULTS WERE SATISFACTORY.

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.