What was found
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.