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 9627373206Battery · dischargedDURING LINE CHECK, EMERGENCY LIGHTS FAILED CIDS PANEL CHECK. REPLACED BATTERIES AND POWER SUPPLY BETWEEN RIGHT OVERWING EXITS, OPERATIONAL CHECK GOOD.Dec 30, 1996 · N306US · Airbus A320211 · Emergency LightingSDR 9627503218Prox Sensor · malfunctionedAFTER LANDING GEAR EXTENSION, THE LANDING GEAR DOOR INDICATED OPEN. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BRAKE STEERING CONTROL UNIT AND TESTED THE NOSE LANDING GEAR PROXIMITYDec 25, 1996 · N318US · Airbus A320211 · Landing Gear Position and WarningSDR CA970109022Sensor Bolt · loose(CAN) AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. GEAR RECYCLED, NO CHANGE. AIRCRAFT RETURNED TO BASE. MAINTENANCE TROUBLESHOOTING FOUND SENSOR TARGET BOLT LOOSE. SENSOR BOLT RETIGHTENED AND GEAR SWING CARRIED OUT AND SYSTEM CHECKED SERVICEABLE.Dec 15, 1996 · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR CA970109021Gear Lock · found installed(CAN) AFTER TAKEOFF, UNABLE TO RETRACT LANDING GEAR. GEAR RECYCLED NO CHANGE. LEFT GEAR NOT UPLOCKED INDICATION ON ECAM COMPUTER. AIRCRAFT RETURNED TO BASE. MAINTENANCE CHECK REVEALED RH GEAR LOCK INSTALLED. LOCK REMOVED, NO FAULT ON CFDS (CENTRALIZED FAULTY DDec 13, 1996 · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR 9627473204Sill · corrodedDURING C-CHECK, CORROSION WAS FOUND ON THE INBOARD FLANGE OF THE RIGHT AFT DOOR SILL. REPAIRED PER EA 32-120550.Dec 13, 1996 · N304US · Airbus A320211 · Fuselage Miscellaneous StructureSDR 9626433213Window · shatteredCAPTAIN'S WINDSHIELD OUTER PANE SHATTERED AT FL350. RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WINDOW, OPERATIONAL CHECK OK.Dec 12, 1996 · N313US · Airbus A320211 · Flight Compartment WindowsSDR 9627483215Sill · corrodedDURING C-CHECK, FOUND CORROSION DAMAGE TO THE UMBRAIL SILL AT FRAME 68, Y+1292. REPAIRED PER EA 32-120561.Dec 6, 1996 · N315US · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA961220004Fan · broken blade(CAN) SMOKE DETECTED IN CABIN, EMERGENCY DECLARED, AIR PACK REGULATOR FAULT ON UPPER ECAM. ON ARRIVAL WHITE SMOKE NOTED ON OPENING PACK DOOR. MAINTENANCE ACTION INVOLVED CHANGING #2 BYPASS VALVE. ACM FOUND SEIZED AND TURBINE THREW BLADE. FURTHER INVESTIGATION Dec 5, 1996 · Airbus A320211 · Air Distribution FanSDR 9625603219Actuator · malfunctionedEXPERIENCED F/CTL SLATS FAULT' ACCOMPANIED BY SLATS LOCKED DURING HEAVY ICING. AIRCRAFT DID NOT SWITCH TO ALTERNATE LAW. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND BOTH LEFT AND RIGHT WING NR 2 SLAT ACTUATOR TORQUE LIMITERS POPPED. REPLACED BOTH SDec 2, 1996 · N319US · Airbus A320211 · Leading Edge Slat ActuatorSDR 9625503202Retract Syst · locked upDURING APPROACH WHEN SELECTING FLAPS 2, RECEIVED F/CTL FLAPS LOCKED ALIGNMENT FAULT COMPLETED COCKPIT OPERATING MANUAL PROCEDURES AND LANDED WITH FLAPS 0. LANDING WAS ACCOMPLISHED WITHOUT INCIDENT. MAINTENANCE RESET NR 1 AND NR 2 SLAT FLAP CONTROL COMPUTERS,Dec 1, 1996 · N302US · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9627493202Longeron · corrodedDURING C-CHECK, THE FLOOR STRINGER AT FRAME 68, Y 1270 LEFT SIDE WAS FOUND WITH AREAS OF CORROSION. REPAIRED PER EA 32-106173.Nov 26, 1996 · N302US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR 9625383213Power Supply · dischargedDURING LINE MAINTENANCE ALL OF FIRST CLASS EMERGENCY FLOOR PROXIMITY LIGHTS FOUND INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY 110WL-1, OPS CHECKED OK.Nov 26, 1996 · N313US · Airbus A320211 · Emergency LightingSDR CA961205013Fire Warn Sys · warning(CAN) CREW REPORTED SMOKE IN CABIN. AREAS OF AIRCRAFT INSPECTED AND FOUND NO EVIDENCE RELATED TO THE WARNING. AIRCRAFT RETURNED TO DEPARTURE BASE.Nov 25, 1996 · Airbus A320211 · Fire DetectionSDR 9625283204Window · shatteredDURING CLIMBOUT AT 16,000 FEET THE FIRST OFFICER'S NR 3 WINDOW OUTER PANE SHATTERED. AIRCRAFT DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED WINDOW, OPS CHECK OK.Nov 24, 1996 · N304US · Airbus A320211 · Flight Compartment WindowsSDR 9625173210Feel Solenoid · failedDURING FINAL APPROACH IN LIGHT ICING CONDITIONS, THE RUDDER PEDALS WERE RESTRICTED IN THE NEUTRAL POSITION. WING AND ENGINE ANTI-ICE WERE OPERATING AT THE TIME. AUTO PILOT WAS NOT ENGAGED. AIRCRAFT LANDED WITHOUT INCIDENT. RUDDER MOVEMENT RETURNED TO NORMANov 24, 1996 · N310NW · Airbus A320211 · Rudder Control SystemSDR CA970129013Windshield · shattered(CAN) AT FLIGHT LEVEL 390 FIRST OFFICERS WINDSHIELD SHATTERED. THERE WAS NO FORWARD VISIBILITY THROUGH WINDSHIELD. FLIGHT DESCENDED TO FLIGHT LEVEL 230. AIRCRAFT REQUIRED TO LAND AT ALTERNATE BASE. UPON ARRIVAL MAINTENANCE INSTALLED NEW WINDSHIELD.Nov 21, 1996 · Airbus A320211 · Flight Compartment WindowsSDR 9624663225Power Supply · inoperativeCIRCUIT BREAKER FOR EMERGENCY LIGHTS ON OVERHEAD PANEL H-5 TRIPPED. RESET UNSUCCESSFULLY. MAINTENANCE REPLACED AFT LEFT EPSU, OPERATIONAL CHECK OK.Nov 18, 1996 · N325US · Airbus A320211 · Emergency LightingSDR 9624323226Casting · crackedDURING LINE CHECK, FOUND THAT THE FORWARD CARGO DOOR HANDLE ATTACH MECHANISM CASTING WAS BROKEN. REPLACED CASTING.Nov 12, 1996 · N326US · Airbus A320211 · Cargo/Baggage DoorsSDR 9624793222Floorbeam · corrodedDURING 1L CHECK, FOUND CORROSION ON THE FRAME 20 FLOORBEAM AT RBL 1640. REPAIRED BEAM (P/N D53112785201) PER EA 32-106167.Nov 10, 1996 · N322US · Airbus A320211 · Fuselage Main, Floor BeamSDR 9624783205Stringer · corrodedDURING 1C1 CHECK, FOUND CORROSION ON THE LBL 1162 FLOOR STRINGER AT FRAME 68. REPAIRED STRINGER PER EA 32-106179.Nov 9, 1996 · N305US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR 9623933246Power Supply · malfunctionedDURING LINE MAINTENANCE, TEST OF THE EMERGENCY LIGHTS FAULTED INT LOADS FWD-L AND COMM FWD-L. REPLACED EPSU, OPERATIONAL CHECK OK.Nov 9, 1996 · N336NW · Airbus A320211 · Emergency LightingSDR CA961118011Fire Detection · erratic(CAN) DURING FLIGHT TWO WARNING LIGHT CAME ON IN FIRE P/B SWITCH AND FIRE WARNING LIGHT CAME ON THE CENTRE CONSOLE. NO MASTER WARNING LIGHTS OR BELL OR ECAM MESSAGE OR FAULT. FLIGHT PROCEEDED TO DESTINATION. MAINTENANCE ACTION INVOLVED CHANGING FIRE DETECTION Nov 8, 1996 · Airbus A320211 · Detection SystemSDR 9623923217Hyd Reservoir · low fluidAS POWER WAS ADVANCED FOR TAKEOFF, RECEIVED HYD-Y RSVR LO LVL MESSAGE. TAKEOFF WAS ABORTED AT 40 KNOTS. AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE SERVICED THE YELLOW HYDRAULIC SYSTEM.Nov 8, 1996 · N317US · Airbus A320211 · Hydraulic System, AuxiliarySDR 9623603235Power Supply · inoperativeDURING LINE MAINTENANCE CHECK, FOUND BOTH AFT DOOR EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED LEFT AFT EPSU. OPERATIONAL CHECK OK.Nov 7, 1996 · N335NW · Airbus A320211 · Emergency LightingSDR 9623473229Battery · dischargedPILOT REPORTED THE EMERGENCY EXIT LIGHTS AT DOORS 1L AND 1R WOULD NOT ILLUMINATE WITH ANY SWITCH CONFIGURATION. MAINTENANCE TEST FAULTED THE FORWARD LEFT EPSU. REPLACED BATTERY PACK. OPERATIONAL CHECK OK.Nov 6, 1996 · N329NW · Airbus A320211 · Emergency LightingSDR 9623303207Power Supply · inoperativeDURING LINE MAINTENANCE, FOUND AFT EMERGENCY EXIT SIGNS INOPERATIVE. REPLACED EPSU, OPERATIONAL CHECK OK.Nov 4, 1996 · N307US · Airbus A320211 · Emergency LightingSDR CA961118008Elect Receptacle · shorted(CAN) FLIGHT ATTENDANT FELT ELECTRICAL SHOCK IN REAR GALLEY POSITION #527. HOT CUP RECEPTACLE REPLACED.Nov 3, 1996 · Airbus A320211 · Buffet/GalleysSDR 9623273202Power Supply · inoperativeDURING LINE MAINTENANCE CHECK OF THE EMERGENCY LIGHTS, THE FORWARD EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED POWER SUPPLY, OPERATIONAL CHECK OK.Nov 3, 1996 · N302US · Airbus A320211 · Emergency LightingSDR CA961112033Sensor · failed(CAN) ON APPROACH FLIGHT CONTROL FLAPS LOCKED ALIGNMENT FAULT APPEARED ON ECAM WHEN FLAP MOVED TO 2 POSITION. LH FLAP ATTACHMENT FAILURE DETECTION SENSOR 37 CV REPLACED. SYSTEM TEST SERVICEABLE.Oct 29, 1996 · Airbus A320211 · Trailing Edge Flap Control SystemSDR CA961104016Computer · alignment fault(CAN) ON APPROACH, FLIGHT CONTROL FLAPS LOCKED ALIGNMENT FAULT APPEARED ON E.C.A.M. WHEN FLAP MOVED TO #2 POSITION. CORRECTIVE ACTION INVOLVED RESETING SLAT/FLAP COMPUTER #1 AND #2. ALSO FLAP WING TIP BRAKE RESET AND TEST CARRIED OUT. FLAP OPERATION AND INDICAOct 28, 1996 · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9622873218Apu · failedSHORTLY AFTER TAKEOFF, STRONG OIL FUMES WERE DETECTED THROUGHOUT THE AIRCRAFT. AIRCRAFT RETURNED TO MSP. GROUND MAINTENANCE FOUND OIL IN THE APU DUCTS. THE APU WAS REPLACED.Oct 25, 1996 · N318US · Airbus A320211 · APU Core EngineSDR 9622633203Power Supply · inoperativeDURING LINE MAINTENANCE, THE LEFT AFT EPSU FAULTED THE BATTERY INTERNAL AND EXTERNAL LOADS. REPLACED POWER SUPPLY, OPERATIONAL CHECK OK.Oct 23, 1996 · N303US · Airbus A320211 · Emergency LightingSDR 9622033203Power Supply · inoperativeDURING LINE MAINTENANCE, THE LEFT AFT EPSU FAULTED THE BATTERY INTERNAL AND EXTERNAL LOADS. REPLACED POWER SUPPLY, OPERATIONAL CHECK OK.Oct 23, 1996 · N303US · Airbus A320211 · Emergency LightingSDR CA961104014Hot Cup · elect short(CAN) FLIGHT ATTENDANT RECEIVED ELECTRICAL SHOCK FROM THE HOT CUP IN AFT GALLEY. LARGE SPARK SEEN IN GALLEY AREA. INVESTIGATION REVEALED HOT CUP RECEPTACLE DEFECTIVE. RECEPTACLE REPLACED.Oct 16, 1996 · Airbus A320211 · Buffet/GalleysSDR CA961029010Flap · locked up(CAN) ON APPROACH AFTER SELECTING FLAP 2, ECAM WARNING, FLAP FAULT, GROUND APPROACH INITIATED AND LANDING MADE WITH FLAPS LOCKED UP. WING TIP BRAKE/PRESSURE OFF BRAKE TEST COMPUTER RESELECTED, FLAP/SLAT ALL POSITIOIN CHECKED SERVICEABLE. RED TRIP INDICATOR FOUOct 16, 1996 · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9622053218Computer · malfunctionedAFTER RECEIVING VENT SKIN VALVE FAULT DURING A PREVIOUS TAKEOFF ATTEMPT, RECEIVED THE SAME MESSAGE. TAKEOFF WAS AGAIN ABORTED. THE AIRCRAFT RETURNED TO THE GATE. MAINTENANCE PLACED THE EXTRACT VALVE ON MEL. THE AVIONICS EQUIPMENT VENTILATION COMPUTER WAS LOct 14, 1996 · N318US · Airbus A320211 · Air Distribution SystemSDR 9622043218Skin Valve Ind · malfunctionedDURING TAKEOFF ROLL, RECEIVED VENT SKIN VALVE FAULT. TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES.Oct 14, 1996 · N318US · Airbus A320211 · Central WarningSDR CA961021013Skin Valve · failed(CAN) ENROUTE FLIGHT DIVERTED DUE TO ECAM MESSAGE VENT AVIONICS SYSTEM FAULT. VENT AND EXTRACT VALVES POSITION AMBER ON CABIN PRESSURE PAGE AND UNABLE TO PRESSURIZE CABIN. MAINTENANCE ACTION INVOLVED REPLACING SKIN AIR EXHAUST VALVE. EXTRACT VALVE SEQUENCED ANOct 10, 1996 · Airbus A320211 · Cabin Pressure Control SystemSDR 9621093206Engine · failedDURING TAKEOFF ROLL, THE NR 1 ENGINE EXPERIENCED A CONTAINED FAILURE. TAKEOFF WAS ABORTED AT 75 KNOTS. MAINTENANCE FOUND METAL IN TAILPIPE. REMOVED AND REPLACED THE NR 1 ENGINE.Oct 3, 1996 · N306US · Airbus A320211 · Engine (Turbine/Turboprop)SDR 9621663214Support · corrodedDURING IL CHECK, FOUND CORROSION IN THE FS 68 FLOOR BEAM SUPPORT AT THE LEFT DOOR SILL. REPAIRED SUPPORT (P/N D53480043) PER EA 32-109588.Oct 2, 1996 · N314US · Airbus A320211 · Fuselage Miscellaneous StructureSDR 9621043217Engine · vibrationDURING CLIMB AFTER TAKEOFF, AIRCRAFT DEVELOPED A VIBRATION. CAPTAIN REPORTED THAT NR 2 ENGINE PYLON WAS SHAKING EXCESSIVELY. AIRCRAFT RETURNED TO DEPARTURE AIRPORT.Oct 1, 1996 · N317US · Airbus A320211 · Engine (Turbine/Turboprop)SDR CA961018018Eiu · failed(CAN) IN-FLIGHT SHUTDOWN DUE TO NR 2 ENGINE OIL TEMPERATURE HIGH, UP TO 190 DEGREES. NR 2 ENGINE INTERFACE UNIT AND OIL TEMPERATURE SENSOR P/N 561397 REPLACED. NIL FOUND ON CHIP DETECTOR.Sep 27, 1996 · Airbus A320211 · Central WarningSDR 09620753249Sensor · malfunctionAFTER TAKEOFF, LANDING GEAR DOOR OPEN WAS INDICATED. CREW RETURNED AIRCRAFT TO DEPARTURE AIRPORT. GROUND MAINTENANCE REPLACED GEAR DOOR PROXIMITY SWITCH.Sep 27, 1996 · N349NW · Airbus A320211 · Landing Gear Position and WarningSDR 9620503226Actuator · leakingDURING CLIMBOUT, THE YELLOW HYDRAULIC SYSTEM FLUID DECREASED TO ZERO ACCOMPANIED BY A RIGHT WING NR 2 SPOILER ECAM INDICATION. THE SPOILER WAS DEPLOYED AT APPROXIMATELY 45 DEGREES. AIRCRAFT CONTINUED TO ORIGINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINSep 23, 1996 · N326US · Airbus A320211 · Drag Control ActuatorSDR 9620633213Support · corrodedDURING IL CHECK, FOUND CORROSION ON THE AFT GALLEY FLOOR SUPPORT BETWEEN FRAMES 67 AND 68 AT THE LEFT AFT ENTRY DOOR SILL. REPAIRED SUPPORT PER EA 32-106351.Sep 19, 1996 · N313US · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA961018015Windshield · pitted(CAN) AIRCRAFT FLEW IN VOLCANIC ASH FOR 3 TO 5 MINUTES. SMOKE ENTERED COCKPIT AND CABIN A FEW SECONDS LATER. NO INSTRUMENT INDICATION OR MALFUNCTION. AIRCRAFT LANDED WITHOUT INCIDENT. PRELIMINARY MAINTENANCE CHECK REVEALED WINDSHIELDS PITTED, LH ENGINE STATOR Sep 17, 1996 · Airbus A320211 · Flight Compartment WindowsSDR 9620063228Interface Unit · malfunctionedDURING APPROACH, RECEIVED L/G NOT DOWN LOCKED MESSAGE AFTER LANDING GEAR EXTENSION. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL INTERFACE UNIT AND NOSE LANDING GESep 17, 1996 · N326NW · Airbus A320211 · Landing Gear Position and WarningSDR 9619943220Flt Contl Unit · malfunctionedIMMEDIATELY AFTER LEVEL OFF AT CRUISE FL350, LOST NR 1 AUTO-PILOT. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND RESET NR 1 FLIGHT MANAGEMENT AND GUIDANCE COMPUTER WITH NO HELP. LATER, LOST THE FLIGHT CONTROL UNIT. AIRCRAFT DIVERTED TO MIA AND LANDED WITSep 14, 1996 · N320US · Airbus A320211 · Autopilot SystemSDR CA961018021Flap · locked(CAN) ON APPROACH WITH FLAP SELECTION 2, FLAP CONTROL LOCKED. MAINTENANCE INSPECTED FLAP/SLAT AND UNABLE TO DUPLICATE FAULT. ALL HYDRAULIC SYSTEMS PRESSURIZED AND FLAP SYSTEM RECYCLED SERVICEABLE.Sep 13, 1996 · Airbus A320211 · Trailing Edge Flap Control SystemSDR CA960924013Target · broken(CAN) ON TAKEOFF, LEFT MAIN LANDING GEAR DOOR INDICATED NOT CLOSED ON ECAM. SUBSEQUENT MAINTENANCE CHECK REVEALED SHIM P/N 201061607 WAS MISSING AND TARGET BROKEN. MAIN LANDING GEAR UPLOCK REPLACED.Sep 11, 1996 · Airbus A320211 · Landing Gear Door Retract Section
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