Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR ANCF201812270401Guard · missingREJECTED TAKE OFF BRAKE RELEASE TWICE FIRST DURING TAXI OUT, SYSTEM RESET PERFORMED THEN DURING TAKE OFF AT 60 KNOTS BRAKE RELEASE APPEAR ON ECAM CAUSING LOW SPEED RTO // ACTION CORRECTIVE: IN ACCORDANCE WITH TSM 32-42-00-810-817-A, AND AMM 32-42-00-720-003-A SDR ANCF2018010601Servo · failedLEFT AND RIGHT AILERON FAULT AFTER LIFT OFF, BOTH ACTUATOR IN BOTH WINGS WERE AMBER. IAW AMM 27-14-51-000-001-A, AND AMM 27-14-51-400-001-A THE AILERON SERVO CONTROL LT 33CE3 WAS REPLACED. .IAW AMM 27-94-34 PB 401,CONF 00 THE SEC N 2 REMOVED AND REPLACED. SDR ANCF2017122901Computer · malfunctionedIMMEDIATELY AFTER TAKE OFF, THE FOLLOWS MSGS APPEARED ON ECAM (WHEN TURNING RIGHT) F/CTL R AIL FAULT F/CTL AIL SERVO FAULT AIRCRAFT TRIMMED THE RUDDER TO L3.6 -AFTER ENGINE 2 SHUTDOWN F/CLT R AIL FAULT AND ELAC 1 FAULT APPEARED. CORRECTIVE ACTION: ACC TSM 27-9SDR ANCF2015081101Engine · bird ingestionBIRD STRIKE ON ENG 2 DURING TAKEOFF. IAW AMM 72-21-00-210-009 GENERAL CONDITION OF THE FAN ROTOR BLADE ITEM 4-A-1-H WAS FOUND ROTOR BLADE NR 5 DEEP 4.54" & LARGE 101 MM BETWEEN LIMITS. IAW AMM 72-21-00-210-009 GENERAL CONDITION OF THE FAN ROTOR BLADE
ITEM 4SDR ANCF2015072601Hmu · malfunctionedDURING ENG 1 START, THE ENG 1 IGNITION B FAULT APPEARS ON ECAM. NEW START PROGRESS WAS PRESENTED WITH ING AB. THE ENG REACHED 50% N2 & REMAINED HUNG START. AT 3RD START APPEARS ENG STALL, THEN WAS PERFORMED ON MANUAL ENG START & APPEAR ENG 1 FAIL ALL PARAMESDR ANCF2015071401Ecu · faultyDURING ENG 1 START THE ENG 1 ING A FAULT APPEAR. THE FADEC MADE A NEW ENG START WITH IGN AB WITHOUT POSITIVE SUCCESS, ENG REMAIN HUNG STAR. IAW AMM 73-21-60-000 400-001-B THE ECU ON ENG 1 WAS R & R. THE FUNCTIONAL TEST OF THE ECU WAS SATISFACTORY PN 2123M56SDR ANCF2015071301Starter · malfunctionedDURING ENG 1 START WHEN MASTER SWITCH TO NR N 2 MOVEMENT, BLEED PRESS NORMAL, START VLV OPEN. IAW AMM 80-11-10 PB 401 THE STARTER WAS REPLACED, O TEST WAS PERFORMED SATISFACTORY PN 3505582-27, SN OFF YG439040-H & SN ON Y6336238-AC.SDR ANCF2015060101Igniter · failedDURING ENG 1 START, ENG 1 IGNITER A FAULT. IAW TSM 74-00-00-810-801A THE OPERATIONAL OF IGNITION SYS WAS ACCOMPLISHED THE RT IGNITER PLUG CANNOT HEARD. IAW AMM 71-21-30 PB401 THE SPARK IGNITER A WAS REPLACED. OPERATIONAL TESTED SATISFACTORY.SDR ANCF2015042001Ignition Sys · malfunctionedDURING ENG START, IGNITION A, ENG 1 FAULT. IAW AMM TASK 74-21-20-000-400-002-A ON ENG NR 1 IGNITION A WAS REPLACED. IAW AMM 74-00- -00-710-043-A OPERATIONAL TEST OF THE IGNITION SYS WAS PERFORMED WITH RESULT SATISFACTORY.SDR ANCF2013042000157Control Unit · malfunctionedDURING LANDING ROLL CROSSING ABOUT 70KTS WHEEL NOSE WHEEL STEERING FAULT AND BRAKES SYSTEM 1 FAULT WAS PRESENTED
NWS REMAINS INOPERATIVE UNTIL FINAL STOP IN THE RWY. ACCORDING TSM 32-51-00-810-818A THE BSCU MUST BE REPLACED FOLLOWING AMM 32-42-34PB401. THE SDR ANCF2012100900132Oven · malfunctionedDURING TAXI BURNING SMELL WAS DETECTED ON AFT GALLEY (4 LEFT). IAW AMM TASK 25-35-00 WAS PERFORMED CHECK IN AFT GALLEY AND FOUND C/B OVEN NR 3 TRIPPED, OVEN NR 3 IS DEFERRED TO DMI /NEF NR 1158 AS PER MEL NEF II-5 CAT D.