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 AU000065Fitting · cracked(AUS) MAIN LANDING GEAR DOOR ACTUATOR LT AFT AND RT FORWARD FITTINGS CRACKED. FOUND DURING ULTRASONIC INSPECTION IAW SB A320-53A1135.LT CONNECTION STRAP PNO D537061220000 ALSO CRACKED.Jan 19, 2000 · Airbus A320211 · Wing, Landing Gear Attach FittingsSDR AU000064Fitting · cracked(AUS) MAIN LANDING GEAR DOOR ACTUATOR LH FORWARD AND RT AFT FITTINGS CRACKED. FOUND DURING ULTRASONIC INSPECTION IAW SB A320-53A1135.LT CONNECTION STRAP PNO D537061220000 ALSO CRACKED.Jan 19, 2000 · Airbus A320211 · Wing, Landing Gear Attach FittingsSDR CA000209035Cable · frozen(CAN) L2 DOOR WOULD NOT ARM AT DEPARTURE. PUSH PULL CABLE FOUND FROZEN. LUBRICATED.Jan 18, 2000 · Airbus A320211 · Service DoorsSDR CA000209032Sensor · failed(CAN) AFTER TAKEOFF NOSE GEAR DOOR REMAINED OPENWITH 31GA DOOR LOCK SENSOR ECAMWARNING. SENSOR REPLACED.Jan 17, 2000 · Airbus A320211 · Landing Gear Position and WarningSDR AU000062Duct · cracked(AUS) APU BLEED AIR SUPPLY DUCT HOLED IN THE AREA LOCATED AFT OF THEREAR CARGO HOLD BETWEEN FRAMES NR 68 AND NO70. THE HOLE WASAPPROXIMATELY 9.525MM (0.375IN) IN DIAMETER AND LOCATED AT THE 6O'CLOCK POSITION AND WAS ASSOCIATED WITH AN AREA OF SEVERECORROSION IJan 14, 2000 · Airbus A320211 · APU Bleed Air SystemSDR CA000209034Case · cracked(CAN) CREW REPORTED FUEL SMELL IN CABIN AND COCKPIT. PMI CONTACTED REQUESTING OPERATOR FOLLOW-UP. SUPPLEMENTAL SDR TO FOLLOW. SUPPLIMENTAL SDR RECEIVED SPECIFYING THE FUEL SMELL WAS CAUSED BY A CRACKED COMBUSTION OUTER COWL WHICH DISTURBED THE H.P. COMPRESSORJan 12, 2000 · Airbus A320211 · Turbine Engine Combustion SectionSDR CA000209031Sensor · failed(CAN) AFTER TAKEOFF NOSE GEAR DOOR REMAINED OPEN WITH 31GA DOOR LOCK SENSOR ECAM WARNING. SENSOR REPLACED.Jan 11, 2000 · Airbus A320211 · Landing Gear Position and WarningSDR 000443206Stringer · corrodedDuring "M" check found corrosion on stringer 41RH. Repaired per EA32-173634.Jan 6, 2000 · N306US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR CA000209030Damper · leaking(CAN) AFTER REACHING CRUISE ALTITUDE GREEN HYD SYS SLOWLY DECREASED UNTIL ECAM WARNING ILLUMINATED. INVESTIGATION FOUND LEFT YAW DAMPENER ACTUATOR LEAKING. YAW DAMPENER REPLACED.Jan 6, 2000 · Airbus A320211 · Autopilot SystemSDR 0000053221Battery · dischargedDURING TEST OF THE EMERGENCY ESCAPE PATH LIGHTING, THE LIGHTS ON SEATS 1, 2, 3, 6, 7, AND 8 DID NOT ILLUMINATE. MAINTENANCE REPLACED THE POWER SUPPLY UNIT 110WL1 AND BATTERIES. OPERATIONAL CHECK OK.Jan 6, 2000 · N321US · Airbus A320211 · Emergency LightingSDR 0000443206Stringer · corrodedDURING M-CHECK, FOUND CORROSION ON STRINGER 41 RT. REPAIRED PER EA32-173634.Jan 6, 2000 · N306US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR CA000110086Engine · surges(CAN) ENGINE SURGES EXPERIENCED, N1 FLUCTUATIONS THEN ENGINE STALLED ON APPROACH. EGT HIT 700C, FIRE SURPRESSION INITIATED.Dec 24, 1999 · Airbus A320211 · Engine (Turbine/Turboprop)SDR CA000110085Coffeemaker · shorted(CAN) FLIGHT ATTENDANT REPORTED RECIEVING AN ELECTRICAL SHOCK FROM COFFEEMAKER. COFFEEMAKER REPLACED.Dec 22, 1999 · Airbus A320211 · Buffet/GalleysSDR CA000110084Motor · failed(CAN) COMPRESSOR FAULT MESSAGE DISPLAYED.VARIABLE BLEED VANE GEAR MOTOR ASSY REPLACED.Dec 21, 1999 · Airbus A320211 · Compressor Bleed ControlSDR CA000209028Computer · failed(CAN) SLAT LOCKED ON APPROACH ACCOMPANIED WITH NR 1 SLAT/FLAP COMPUTER FAIL (SFCC) ECAM WARN ILLUMINATED. SFCC REPLACED.Dec 21, 1999 · Airbus A320211 · Leading Edge Slat Control SystemSDR 9905413218Yaw Damper · leakingDURING DESCENT, RECEIVED HYD G RSVR LOW LVL ECAM MESSAGE. FOLLOWED COM PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING YAW DAMPER 3CC1. OPERATIONAL CHECK NORMAL.Dec 21, 1999 · N318US · Airbus A320211 · Autopilot SystemSDR CA991231026Apu · odor(CAN) PUNGENT SMELL EVIDENT WITH AIR CONDITIONING PACKS ON AND SOURCE SELECTED TOAPU AIR.OIL CONTAMINATION FOUND IN APU COMPARTMENT, APU REPLACED.Dec 13, 1999 · Airbus A320211 · APU Core EngineSDR CA991231025Apu · failed(CAN) OILY SMELL IN AIRCRAFT DURING FLIGHT. INVESTIGATION REVEALED APU INTERNAL FAILDec 10, 1999 · Airbus A320211 · APU Core EngineSDR CA991231024Controller · smoke(CAN) BOTH WINDSCREENS ARCING AND STRONG SMELL OF SMOKE IN COCKPIT ON APPROACH. AIRCRAFT LANDED BOTH WINDSCREENS AND WINDSHIELD HEAT CONTROLLER REPLACED.Dec 8, 1999 · Airbus A320211 · Flight Compartment WindowsSDR CA991208052Fmgc1 Data · faulty(CAN) ECAM REPORTED FMGC 1 FAULT. NR 1 FMGC RESET.Dec 2, 1999 · Airbus A320211 · Flight Management Computing Hardware SystemSDR CA991231022Computer · failed(CAN) ECAM MESSAGE SLAT WARN ILLUMUINATED. AIRCRAFT LANDED SLAT COMPUTER RESET.Nov 30, 1999 · Airbus A320211 · Drag Control SystemSDR CA991231021Valve · failed(CAN) UNABLE TO MAINTAIN CABIN PRESSURISATION IN AUTO OR MANUAL MODE. NR 1 HIGH PRESSURE VALVE REEPLACED.Nov 30, 1999 · Airbus A320211 · Pneumatic Distribution SystemSDR CA991208051Fan · failed(CAN) STRONG SMELL BURNING PLASTIC, VIBRATION AND SMOKE IN COCKPIT AND ECAM MASSAGE VENT EXTRACT FAN. AIRCRAFT LANDED, VENT FAN REPLACED.Nov 30, 1999 · Airbus A320211 · Air Distribution FanSDR CA991231020Gcu · failed(CAN) AIRCRAFT OPERATING ON MEL WITH FAILED RT IDG. APU SHUTDOWN INFLIGHT CAUSING A LOSS OF ELECTRICAL POWER. AIRARAFT LANDED AND NR 2 ENGINE GCU AND IDG REPLACED.Nov 27, 1999 · Airbus A320211 · AC Generation SystemSDR CA991231019Seal · missing(CAN) LEADING EDGE CUSHON SEAL FOUND MISSING ON INBOARD TRAILING FLAP.Nov 26, 1999 · Airbus A320211 · Trailing Edge FlapsSDR CA991208050Tru · faulty(CAN) ELECTRICAL BURNING SMELL REPORTED APPARENTLY COMING FROM AIR CONDITIONING PACKS. INVESTIGATION REVEALED NR 2 TRU FAILED. UNIT REPLACED.Nov 26, 1999 · Airbus A320211 · DC Rectifier/ConverterSDR CA991210056Flap · failed(CAN) FLAPS FAILED AT O DEGREES ON APPROACH. AIRCRAFT LANDED FLAP BRAKES RESET.Nov 11, 1999 · Airbus A320211 · Trailing Edge Flap Control SystemSDR CA991210039Acm · failed(CAN) BURNT SMELL IN CABIN, NR2 ACU PACK TURNED OFF, SMELL DISSIPATED. NR2 ACM REPLACED.Nov 2, 1999 · Airbus A320211 · Cabin Cooling SystemSDR 9904413202Target · out of adjustDURING CRUISE, RECEIVED L/G LGCIU 1 FAULT AND LGCIU 2 FAULT. ON APPROACH PERFORMED GRAVITY EXTENSION OF LANDING GEAR PER COM PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE NOSE LANDING GEAR STRUT EXTENSION TARGET CLEARANCES 24GA AND 25GA. Oct 28, 1999 · N302US · Airbus A320211 · Landing Gear Position and WarningSDR CA991103086Sensor · failed(CAN) RT GEAR DOOR REMAINED OPEN ON LANDING. PROX SENSOR REPLACED.Oct 23, 1999 · Airbus A320211 · Door Warning SystemSDR AU991103086Prox Sensor · failed(AU) RIGHT GEAR DOOR REMAINED OPEN ON LANDING. PROXIMITY SENSOR REPLACED.Oct 23, 1999 · Airbus A320211 · Door Warning SystemSDR CA991103085Actuator · failed(CAN) POST TAKE OFF ECAM MESSAGE, FLIGHT CONTROL ELEVAT0OR AILERION COMPUTER FAULTS 1 AND 2. AIRCRAFT DIVERTED AND LANDED. REPLACED HORIZONTAL STAB PITCH TRIM ACTUATOR (HSTA)Oct 21, 1999 · Airbus A320211 · Stabilizer ActuatorSDR AU991103085Hsta · failed(AU) POST TAKEOFF ECAM MESSAGE, FLIGHT CONTROL ELEVAT0OR AILERION COMPUTER FAULTS 1 AND 2. AIRCRAFT DIVERTED AND LANDED. REPLACED HORIZONTAL STABILIZER PITCH TRIM ACTUATOR (HSTA).Oct 21, 1999 · Airbus A320211 · Stabilizer ActuatorSDR CA991103084Stop · out of adj(CAN) L1 CABIN DOOR VERY HARD TO OPEN. INNER HANDLE STOP ADJUSTED.Oct 18, 1999 · Airbus A320211 · Passenger/Crew DoorsSDR 9904353219Outflow Valve · failedDURING CRUISE, RECEIVED CABIN PRESSURE SYS 1 AND 2 FAULT AND CABIN PRESSURE EXCESS CAB ALT MESSAGES WITH AUTOMATIC DROP OF OXYGEN MASKS. INITIATED RAPID DESCENT DUE TO A MODERATELY RAPID DECOMPRESSION. DIVERTED TO MCI AND LANDED WITHOUT INCIDENT. MAINTENANCOct 18, 1999 · N319US · Airbus A320211 · Pressure Regulator/Outflow ValveSDR 9904283202Floorbeam · corrodedDURING M-CHECK, FOUND CORROSION ON FLOORBEAM 254R AND 765R BETWEEN FRAMES 16-24R. REPAIRED PER EA 163484 AND SRM 51-72-11.Oct 8, 1999 · N302US · Airbus A320211 · Fuselage Main, Floor BeamSDR CA991028044Fadec · failed(CAN) NR 2 FADEC B FAULT, ENGINE REMOVED, TEAR DOWN TO FOLLOW.Oct 5, 1999 · Airbus A320211 · Fuel Controlling SystemSDR 9904273202Floorbeam · corrodedDURING M-CHECK, FOUND CORROSION ON FLOORBEAM 1292L BETWEEN FRAME 16 AND 18. REPAIRED PER EA 32-163484.Sep 30, 1999 · N302US · Airbus A320211 · Fuselage Main, Floor BeamSDR CA991008017Carbon Seal · failed(CAN) INTEGRATED DRIVE GENERATOR CARBON SEAL FAILED CAUSING LOSS OF ENGINE OIL.Sep 25, 1999 · Airbus A320211 · AC Generation SystemSDR CA991008016Sensor · faulty(CAN) AFTER TAKEOFF, LANDING GEAR ABSORBER FAULT ILLUMINATED.Sep 22, 1999 · Airbus A320211 · Landing Gear Position and WarningSDR 9904473212Floorbeam · corrodedDURING LINE CHECK, FOUND SOFT FLOOR IN FORWARD GALLEY AREA. FOUND CORROSION ON FLOORBEAMS AND SEAT TRACKS FROM FRAMES FS 13 TO 24. REPAIRED PER SRM 51-72-11 AND NW DWG SA 5346-01004-2.Sep 18, 1999 · N312US · Airbus A320211 · Fuselage Main, Floor BeamSDR CA990927001Windshield · cracked(CAN) PILOT'S WINDSHIELD OUTER PLY CRACKED.....REPLACED.Sep 13, 1999 · Airbus A320211 · Flight Compartment WindowsSDR 9903773209Structure · damagedDURING INSPECTION OF DOOR 1R SLIDE GIRT BAR TRIGGER SPRING PER EO 2561-01223, THE SLIDE DROPPED (UNPACKED) FROM THE DOOR PACKBOARD ASSEMBLY AND THE INFLATION BOTTLE HIT THE GROUND BRAKING AT THE NECK ALLOWING THE BOTTLE TO PROPEL ITSELF INTO THE FORWARD RIGHT Sep 7, 1999 · N309US · Airbus A320211 · Fuselage Main, StructureSDR CA990927089Smoke Detector · malfunctioned(CAN) AVIONIC BAY SMOKE INDICATION WITH NO OBSERVED SMOKE. NO FAULT FOUND.Sep 4, 1999 · Airbus A320211 · Smoke DetectionSDR CA990927090Pump · failed(CAN) BLUE SYSTEM HYDRAULIC FAILURE DUE TO LOSS OF PRESSURE. BLUE HYDRAULIC SYSTEM PUMP REPLACED.Aug 29, 1999 · Airbus A320211 · Hydraulic Pump (Electric/Engine), MainSDR CA990817019B-Nut · loose(CAN) NR 1 ENGINE OIL QUANTITY DROPPED TO 3.5 DURING FLIGHT. AIRCRAFT LANDED. INVESTIGATION REVEALED A LOOSE B-NUT ON A LINE ON THE ENGINE. THE NR 1 ENGINE FUEL PUMP HAD BEEN REPLACED PRIOR TO THE FLIGHT AND THE LINE MAY HAVE BEEN DISTURBED THEN AND NOT CORAug 7, 1999 · Airbus A320211 · Turbine Engine Oil SystemSDR CA990916006Valve · leaking(CAN) AFTER TAKEOFF, FUEL OBSERVED LEAKING FROM RIGHT WING. AIRCRAFT LANDED. RIGHT AIR RELEASE VALVE FOUND TO BE UNSERVICEABLE, UNIT REPLACED.Aug 6, 1999 · Airbus A320211 · Fuel StorageSDR CA990907058Windshield · cracked(CAN) IN CRUISE, LEFT PILOT'S WINDSHIELD OUTER PLY CRACKED. AIRCRAFT LANDED AND WINDSHIELD REPLACED.Aug 4, 1999 · Airbus A320211 · Flight Compartment WindowsSDR CA990812035Sensor · failed(CAN) NR 2 COMPRESSOR VANE ECAM STAYED ON FOR 20 MINUTES AFTER TAKEOFF. REPLACED VARIABLE BLEED VANE POSITION SENSOR.Jul 17, 1999 · Airbus A320211 · Turbine Engine Compressor SectionSDR CA990812034Control Unit · failed(CAN) GEAR WOULD NOT EXTEND, EMERGENCY EXTENSION USED. LGCIU NR 1 SWAPPED, BRAKE/STEER UNIT, GEAR SELECTOR LEVER, GEAR SELECTOR VALVE, MANIFOLD VALVE, GEAR CONTROL UNIT, AND INTERFACE UNIT REPLACED. OPERATIONAL CHECKS COMPLETED.Jul 17, 1999 · Airbus A320211 · Landing Gear Retraction/Extension System
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