Airbus A320-211

Service difficulty reports · 5,271

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Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = 'A320211'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR 9607303249Retract Mech · lack of lubeDURING CLIMBOUT UPON LANDING GEAR RETRACTION, LDG GEAR SHOCK ABSORBER FAULT ILLUMINATED AND GEAR WOULD NOT RETRACT. FAULT CLEARED APPROXIMATELY 45 SECONDS LATER AND GEAR RETRACTED NORMALLY. FLIGHT CONTINUED TO MSP AND LANDED WITHOUT FURTHER INCIDENT. MAINTEMar 31, 1996 · N349NW · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR CA960417515Flaps · locked(CAN)FLAP LOCKED, FLAPLESS LANDING CARRIED OUT. MAINTENANCE ACTION INVOLVED CARRYING OUT RMA 27-50-529 AND RESETING BOTH S.F.C.C.'S. OPERATIONAL CHECK CARRIED OUT.Mar 30, 1996 · Airbus A320211 · Trailing Edge Flap Control SystemSDR CA960417514Actuator · inoperative(CAN)ON APPROACH WHEN FLAP 2 SELECTED ECAM MESSAGE "F\CTL FLAPS LOCKED ALIGNMENT FAULT". FLAPLESS LANDING. RMA 27-50-520 CARRIED OUT AND WING TIP BRAKES RESET. ALSO LEFT FLAP ROTARY ACTUATOR CHANGED.Mar 29, 1996 · Airbus A320211 · Trailing Edge Flap ActuatorSDR CA960417511Thrust Lever · fault indication(CAN)ON APPROACH FOLLOWING ECAM MESSAGE "ENGINE #1 THRUST LEVER FAULT" AND "ENGINE #1 FADEC B FAULT", ENGINE SHUT DOWN. FADEC RESET, TEST AND GROUND RUN CARRIED OUT.Mar 24, 1996 · Airbus A320211 · Power LeverSDR CA960417509Prox.Sensor · out of rig(CAN)ON APPROACH WHEN FLAP 2 SELECTED ECAM MESSAGE "F/CTL FLAPS LOCKED ALIGNMENT FAULT". ECAM ACTIONS COMPLETED, LANDING NORMAL. MAINTENANCE FOUND RIGHT FLAP INTERCONNECTING STRUT WITH BOTH SENSORS OUT OF RIG. BOTH PROXIMITY SENSORS RIGGED AS PER M.M. 27-51-4Mar 24, 1996 · Airbus A320211 · Trailing Edge Flap Control SystemSDR CA960321008Concentrator · failed(CAN)DURING FLIGHT, ALL ECAM WARNINGS, MASTER CAUTION, MASTER WARNING BELLS BEGAN CYCLING. PRESSURIZATION CLIMBED, EMERGENCY DESCENT INITIATED, COULD NOT STOP CYCLING OF WARNINGS OR FAULTS. MAINTENANCE TRO UBLESHOOTING LED TO SDAC #1 FAULT. SDAC REPLACED. SUBSMar 21, 1996 · Airbus A320211 · Cabin Pressure Control SystemSDR CA960417508Blower Fan · seized(CAN)BURNING SMELL DETECTED IN COCKPIT, BLOWER AND VENT FANS SHUT OFF. MAINTENANCE FOUND BLOWER FAN SEIZED. DEFECTIVE BLOWER FAN REPLACED.Mar 20, 1996 · Airbus A320211 · Air Distribution FanSDR 9606203222Flush Contl Unit · malfunctionedDURING CRUISE, THE FORWARD LAVATORY TOILET OVERFLOWED SPILLING FLUID INTO THE FIRST CLASS CABIN. AIRCRAFT DIVERTED TO DFW AND LANDED WITHOUT INCIDENT. THE FORWARD LAV WAS PLACED ON MEL AND THE FLUSH CONTROL UNIT LATER WAS REPLACED, OPERATIONAL CHECK OK.Mar 16, 1996 · N322US · Airbus A320211 · Waste Disposal SystemSDR CA960417502Flaps · locked(CAN)ON FINAL APPROACH, FLAPS LOCKED AT ZERO DEGREES. FLAPLESS LANDING CARRIED OUT. MAINTENANCE CARRIED OUT R.M.A. 27-50-435 AND 27-50-431. ALL TORQUE LIMITERS INSPECTED AND SYSTEM TESTED. FLAP SYSTEM CHEC K CARRIED OUT.Mar 12, 1996 · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9605873201Mechanism · frozenDURING GROUND OPERATIONS, THE DOOR 1R WOULD NOT DISARM DUE TO BEING FROZEN. LUBRICATED GIRT BAR AND MECHANISM. OPERATIONAL CHECK OK.Mar 8, 1996 · N301US · Airbus A320211 · Passenger/Crew DoorsSDR 9605963216Web · crackedDURING PERIODIC CHECK, THE TRIANGLE WEB PANEL AFT OF FRAME 68, NEAR THE FUSELAGE SKIN WAS FOUND CRACKED. STOP DRILLED CRACK AND SEALED PER EA 32-106827.Mar 7, 1996 · N316US · Airbus A320211 · Fuselage Miscellaneous StructureSDR 9605363235Bscu · malfunctionedDURING TAXI IN AT THE GATE, THE BRAKES DID NOT RESPOND. USED ENGINE THRUST REVERSE TO STOP AIRCRAFT SAFELY AT THE GATE. THE BRAKES GRABBED AS THE AIRCRAFT CAME TO A STOP. MAINTENANCE REPLACED THE BRAKE STEERING CONTROL UNIT. OPERATIONAL CHECK OK.Mar 6, 1996 · N335NW · Airbus A320211 · Landing Gear Brake SystemSDR CA960321516Bleed Valve · inoperative(CAN)TAKEOFF REJECTED AT 120 KNOTS BECAUSE OF SEVERE VIBRATION FOLLOWED BY HIGH EGT, UP TO 850 DEGREES CENTIGRADE. MAINTENANCE INVESTIGATION REVEALED VARIABLE BLEED VALVE (V.B.V.) MOTOR DRIVE SHAFT TO ACTU ATOR SHEARED. V.B.V. MOTOR DRIVE REPLACED.Mar 4, 1996 · Airbus A320211 · Compressor Bleed ControlSDR 9605023212Computer · malfunctionedDURING CLIMBOUT, RECEIVED VENT AVIONICS SYS FAULT, FOLLOWED SHORTLY BY VENT EXTRACT FAULT. SEVERAL MINUTES LATER, RECEIVED AVIONICS SMOKE MESSAGE AND GEN 1 LINE SMOKE LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT INCIDENT WITH EMERGENCY EQUIMar 3, 1996 · N312US · Airbus A320211 · Air Distribution SystemSDR 9605033236Prox Sensor · malfunctionedDURING APPROACH, RECEIVED L/G DOORS NOT CLOSED MESSAGE AFTER LOWERING THE LANDING GEAR. ALSO, THE WHEEL PAGE ON ECAM DISPLAYED ONE RED GEAR TRIANGLE. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE Mar 2, 1996 · N336NW · Airbus A320211 · Landing Gear Position and WarningSDR 9605003236Interface Units · malfunctionedON THE WHEEL PAGE OF THE ECAM, THE NOSE LANDING GEAR TRIANGLE INDICATED RED WITH THE GEAR DOWN. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 AND NR 2 LANDING GEAR CONTROL INTMar 1, 1996 · N336NW · Airbus A320211 · Landing Gear Position and WarningSDR 9604913224Epsu · inoperativeDURING LINE MAINTENANCE, THE AFT SECTION OF EMERGENCY FLOOR PATH LIGHTS WERE INOPERATIVE. REPLACED EPSU 11O WL 3, OPERATIONAL CHECK OK.Feb 27, 1996 · N324US · Airbus A320211 · Emergency LightingSDR 9604713237Epsu · failedDURING LINE CHECK, THE EPSU FAILED INT LOAD TEST. REPLACED EPSU AND OPERATIONAL CHECK OK.Feb 26, 1996 · N337NW · Airbus A320211 · Emergency LightingSDR CA960321509Engine Fadec · malfunction(CAN)DURING LANDING ROLL AT 70 KNOTS, LEFT ENGINE SHUT DOWN ON ITS OWN WITH NO ASSOCIATED FAULT. ENGINE STARTED NORMALLY AT THE GATE. MAINTENANCE ACTION INVOLVED TEST MOTORING THE FULL AUTHORITY DIGITAL EN GINE CONTROL (FADEC) AND VISUAL INSPECTION. NO FURTHERFeb 24, 1996 · Airbus A320211 · Fuel Controlling SystemSDR 9604843221Computer · malfunctionedDURING TAKEOFF ROLL, RECEIVED F/CTL ELAC 2 PITCH FAULT MESSAGE. TAKEOFF WAS ABORTED AT APPROXIMATELY 80 KNOTS. AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE REPLACED THE NR 2 ELEVATOR AILERON COMPUTER, OPERATIONAL CHECK OK.Feb 22, 1996 · N321US · Airbus A320211 · Flight Control SystemSDR CA960321503Fuel Strainer · ice blockage(CAN)LEFT FUEL BOOST PUMPS (#1 & #2) FAULTED ON TAKEOFF, UNABLE TO RESET, NECESSARY TO CROSSFEED. MAINTENANCE ACTION INVOLVED INSTALLING NEW FUEL STRAINERS FOR FUEL PUMPS AS PER PRODUCTION PERMIT #2-28-20/ 351-28-74. MODIFICATION INTRODUCES NEW FUEL PUMP STRAIFeb 21, 1996 · Airbus A320211 · Aircraft Fuel Filter/StrainerSDR 9604333221Sensor · malfunctionedDURING CLIMBOUT, THE LANDING GEAR DID NOT RETRACT, THREE GREEN AND THREE RED GEAR INDICAITON LIGHTS WERE ILLUMINATED. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENAFeb 21, 1996 · N321NW · Airbus A320211 · Landing Gear Position and WarningSDR CA960321502Slats · seized(CAN)PRIOR TO ARRIVAL, UNABLE TO EXTEND LEADING EDGE SLATS, LANDING ACCOMPLISHED WITHOUT SLATS. MAINTENANCE ACTION INVOLVED LUBRICATING SLAT PINIONS AND ROLLERS. SYSTEM CHECK CARRIED OUT.Feb 19, 1996 · Airbus A320211 · Leading Edge Slat Control SystemSDR 9605973213Tr Unit · malfunctionedDURING LANDING, THE NR 1 ENGINE FLAMED OUT AFTER COMING OUT OF SECOND THRUST REVERSER ENGAGEMENT AND ENGINE RESTARTED DURING TAXI INTO GATE. GROUND MAINTENANCE INSPECTED, RAN AND OPERATED NR 1 ENGINE THRUST REVERSER SEVERAL TIMES, NO PROBLEMS FOUND.Feb 17, 1996 · N313US · Airbus A320211 · Engine Thrust ReverserSDR 9604163210Nut · improper configDURING LINE CHECK DIRECTED INSPECTION, FOUND ONE IMPROPER CONFIGURATION NUT ON THE LEFT ENGINE FORWARD ENGINE MOUNT, FORWARD OUTBOARD ATTACH BOLT (P/N LH7461T144D). REPLACED NUT WITH (P/N VN401B144) PER MM 71-00-00 PG 436.Feb 15, 1996 · N310NW · Airbus A320211 · Engine Mount SectionSDR 9604173207Nut · crackedDURING '1C1' CHECK, LEFT ENGINE CHANGE FOUND THE FORWARD ENGINE MOUNT FORWARD ATTACH NUTS CRACKED. FURTHER INVESTIGATION REVEALED THAT IMPROPER CONFIGURATION NUTS WERE PREVIOUSLY INSTALLED (P/N LH7461T144D) PROPER CONFIGURATION IS (VN401B144). REPLACED ENGINFeb 14, 1996 · N307US · Airbus A320211 · Engine Mount SectionSDR 9603893241Battery Pack · dischargedDURING LINE MAINTENANCE, THE EMERGENCY LIGHTS TEST FAULTED THE RIGHT EPSU. REPLACED EPSU AND BATTERY PACK AND OPERATIONAL CHECK OK.Feb 14, 1996 · N341NW · Airbus A320211 · Emergency LightingSDR 9603503204Motor · leakingDURING CLIMBOUT, NOTICED AN ACCUMULATION OF NOXIOUS FUMES IN THE COCKPIT AND CABIN. CREW DONNED THE OXYGEN MASKS AND THE AIRCRAFT RETURNED TO MIA WITH EMERGENCY EQUIPMENT STANDING BY. AN UNEVENTFUL OVERWEIGHT LANDING WAS ACCOMPLISHED. MAINTENANCE FOUND THE Feb 12, 1996 · N304US · Airbus A320211 · Stabilizer Control SystemSDR CA960320541Bleed Valve · faulty(CAN) AIRCRAFT RETURNED TO ORIGIN AFTER TAKEOFF DUE TO #1 ENGINE SURGING. EGT EXCEEDENCE. FOUND ENGINE COMPRESSOR BLEED VALVE AT FAULT. CHANGED #1 ENGINE VARIABLE BLEED VALVE SENSOR. FADEC TEST CARRIED OUT ON BOTH CHANNELS.Feb 7, 1996 · Airbus A320211 · Compressor Bleed ValveSDR 9603583234Battery Pack · dischargedDURING LINE MAINTENANCE, THE FORWARD LEFT EPSU 10 WL FAILED THE EMERGENCY LIGHTS TEST. REPLACED THE BATTERY PACK AND OPERATIONAL CHECK OK.Feb 5, 1996 · N334NW · Airbus A320211 · Emergency LightingSDR 9602903236Idg · malfunctionedDURING CLIMBOUT, THE NR 2 ENGINE INTEGRATED DRIVE GENERATOR LOW OIL PRESSURE LIGHT ILLUMINATED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE INTEGRATED DRIVE GENERATOR, LEAK AND OPERATIONAL CHECK OK.Feb 4, 1996 · N336NW · Airbus A320211 · AC Generator-AlternatorSDR 9602893232Sensor · failedDURING CLIMBOUT AFTER LANDING GEAR RETRACTION, LANDING GEAR DOOR INDICATED UNLOCKED. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN LANDFeb 3, 1996 · N332NW · Airbus A320211 · Landing Gear Position and WarningSDR 9602813221Retract Mech · malfunctionedDURING CLIMBOUT, THE LANDING GEAR DID NOT RETRACT. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. LANDING GEAR EXTENDED NORMALLY AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. REPLACED EXTEND SEFeb 3, 1996 · N321US · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR CA960212004Pump · low press warn(CAN)DURING CRUISE THE LEFT FUEL TANK BOOST PUMPS LOW PRESSURE WARNING ANNUNCIATED (BOTH PUMPS). OPENED FUEL CROSSFEED, UNABLE TO MAINTAIN FUEL BALANCE IN THIS CONFIGURATION WITH #1 AND #2 FUEL PUMPS (TANK1) STILL SELECTED ON. DIVERTED AIRCRAFT TO YXE. MAINTENFeb 2, 1996 · Airbus A320211 · Fuel Boost PumpSDR CA960320536Elect Receptacle · shorted(CAN)HOT CUPS AT REAR GALLEY POSITION 527 AND 528 SPARKED AND POPPED CIRCUIT BREAKER. SHORTED RECEPTACLES REPLACED.Jan 31, 1996 · Airbus A320211 · Buffet/GalleysSDR CA960320534Actuator · inoperative(CAN)ON INITIAL FLAP SELECTION DURING APPROACH, ECAM MESSAGE SLATS INOPERATIVE. MAINTENANCE INVESTIGATION FOUND SLAT ROTARY ACTUATOR 6095CM TRIPPED. SLAT ROTARY ACTUATOR 6095CM REPLACED, S.F.C.C. #1 AND #2TESTED AND FLAP/SLAT OPERATIONALLY CHECKED.Jan 31, 1996 · Airbus A320211 · Leading Edge Slat Control SystemSDR 9602343221Battery Pack · dischargedDURING LINE MAINTENANCE, THE EMERGENCY LIGHTS FAILED TEST. FOUND LEFT BATTERY FAULT LIGHT ILLUMINATED (11WL). REPLACED BATTERY PACK AND RESET FUSES. OPERATIONAL CHECK OK.Jan 30, 1996 · N321US · Airbus A320211 · Emergency LightingSDR CA960215101Fuel Screen · iced(CAN)DURING TAXIING IN TO RAMP,LEFT TANK PUMPS 1 & 2 FAULT ON ECAM & OVERHEAD.CHECK LIST COMPLETED AS PER ECAM.APPROXIMATELY 2 MINUTES LATER #1 ENGINE FLAMED OUT & WAS SHUTDOWN,ACCORDING TO ECAM.FUEL IN LE FT TANK 3020,FUEL IN RIGHT TANK 3180. CHECK POST FLIGHJan 29, 1996 · Airbus A320211 · Aircraft Fuel Distribution SystemSDR CA960320532Door Mechanism · broken(CAN)R-1 DOOR REPORTED INOPERATIVE ON ARRIVAL. MAINTENANCE INVESTIGATION FOUND BROKEN DOOR ARM/DISARM STRIKER PLATE ON GALLEY FLOOR AND BOTTLE BLOWN. COPPER SEAL REPLACED, CLEVIS AND DOOR STRIKER REPLACED.DOOR SLIDE REPLACED.Jan 28, 1996 · Airbus A320211 · Galley DoorsSDR 9602143223Retract Mech · out of rigDURING APPROACH, THE LANDING GEAR DID NOT EXTEND. CYCLED THE LANDING GEAR HANDLE AND GEAR EXTENDED NORMALLY. ACCOMPLISHED A MISSED APPROACH. DURING SECOND APPROACH ATTEMPT, LANDING GEAR FUNCTIONED NORMALLY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE RIJan 28, 1996 · N323US · Airbus A320211 · Landing Gear Door Retract SectionSDR 9602133215Indication · malfunctionedDURING CLIMBOUT AFTER LANDING GEAR RETRACTION, RECEIVED 'L/G GEAR NOT UPLOCKED' AND 'L/G DOORS NOT CLOSED' MESSAGES. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. CORRECTIVE ACJan 28, 1996 · N315US · Airbus A320211 · Landing Gear Position and WarningSDR CA960320531Actuator · inoperative(CAN)FLAP CONTROL ECAM MESSAGE; FLAPS LOCKED AND WING TIP BRAKE. FLAPLESS LANDING. MAINTENANCE ACTION RESET WING TIP BRAKE THROUGH C.F.D.S. AND S.F.C.C. #1 AND #2. REPLACED #3 FLAP ACTUATOR. OPERATION CHEC K CARRIED OUT.Jan 27, 1996 · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9602093245Control Unit · malfunctionedDURING CLIMBOUT, THE LANDING GEAR DID NOT RETRACT. CYCLED THE LANDING GEAR HANDLE AND GEAR RETRACTED NORMALLY. FLIGHT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL INTERFACE UNIT AND SYSTEM TESTJan 27, 1996 · N345NW · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR CA960212005Selector Valve · inoperative(CAN)ON CLIMB LANDING GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO BASE. MAINTENANCE CHECK REVEALED MAIN LANDING DOORS WERE NOT FULLY CLOSED. MAINTENANCE ACTION INVOLVED CHANGING MLG SELECTOR VALVE AS PER AMM 32-31-0. BOTH LGCIU TESTED AND GEAR SWING WAS NORMJan 25, 1996 · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR CA960320528Hydraulic Line · leaking(CAN)CLASS 1 ECAM MESSAGE "FLIGHT CONTROL FAULT" CARRIED OUT ECAM ACTION, LANDED FLAPLESS. MAINTENANCE INVESTIGATION FOUND HYDRAULIC LINE TO LEFT #4 SPOILER LEAKING. NEW LINE FABRICATED & INSTALLED. SYSTEM TOPPED AND OPERATIONALLY CHECKED.Jan 24, 1996 · Airbus A320211 · Hydraulic System, MainSDR CA960320527Press.Controller · failed(CAN)AT FLIGHT LEVEL FL370, CABIN ALTITUDE REACHED 8,500 FT., EMERGENCY DESCENT INITIATED, AIRCRAFT LEVELED AT 19,000 FT. AND CABIN ALTITUDE STABILIZED AT 5,000 FT. MAINTENANCE CHANGED #1 CONTROLLER.Jan 24, 1996 · Airbus A320211 · Cabin Pressure ControllerSDR AU960377Relay · faulty(AUS) NO1 ENGINE FIRE WARNING SYSTEM FAULTY OPERATION - CAUSED BY FIRE DETECTION UNIT RELAY K1 CONTACTS BEING CLOSEDJan 23, 1996 · Airbus A320211 · Detection SystemSDR CA960320524Arming Handle · req adjustiment(CAN)L2 DOOR ARMING HANDLE MOVED TO DISARM DURING FLIGHT. IN FLIGHT THE HANDLE GRADUALLY RAISED AND THE SLIDE ARMED INDICATION SHOWED DISARMED. MAINTENANCE ACTION INVOLVED ADJUSTING TENSION ON ARM/DISARM C ABLE, ADJUSTED PROXIMITY SWITCH TARGET AND OPERATIONALJan 22, 1996 · Airbus A320211 · Passenger/Crew DoorsSDR 9601783223Indication · malfunctionedDURING APPROACH INTO LAS AFTER LANDING GEAR EXTENSION, RECEIVED L/G GEAR NOT DOWN LOCKED MESSAGE. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTION REVEALED NO DISCREPANCIES.Jan 22, 1996 · N323US · Airbus A320211 · Landing Gear Position and WarningSDR CA960320519Computer · inoperative(CAN)ON ENGAGING AUTO PILOT AFTER TAKEOFF, RED WARNING LIGHT AND "GEAR NOT DOWN" MESSAGE WITH A QUICK PITCH UP AND DOWN OF AIRCRAFT. AIRCRAFT RETURNED TO BASE. MAINTENANCE ACCOMPLISHED C.F.D.S. TEST OF A.F .S. AND DETERMINED F.A.C. #2 WAS AT FAULT. REPLACED F.Jan 20, 1996 · Airbus A320211 · Autopilot System
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