Airbus A320-211
Service difficulty reports · 5,271
Newest first. General aviation reporting is voluntary.
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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.SDR 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.SDR CA000209035Cable · frozen(CAN) L2 DOOR WOULD NOT ARM AT DEPARTURE. PUSH PULL CABLE FOUND FROZEN. LUBRICATED.SDR CA000209032Sensor · failed(CAN) AFTER TAKEOFF NOSE GEAR DOOR REMAINED OPENWITH 31GA DOOR LOCK SENSOR ECAMWARNING. SENSOR REPLACED.SDR 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 ISDR 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. COMPRESSORSDR CA000209031Sensor · failed(CAN) AFTER TAKEOFF NOSE GEAR DOOR REMAINED OPEN WITH 31GA DOOR LOCK SENSOR ECAM WARNING. SENSOR REPLACED.SDR 000443206Stringer · corrodedDuring "M" check found corrosion on stringer 41RH. Repaired per EA32-173634.SDR 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.SDR 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.SDR 0000443206Stringer · corrodedDURING M-CHECK, FOUND CORROSION ON STRINGER 41 RT. REPAIRED PER EA32-173634.SDR CA000110086Engine · surges(CAN) ENGINE SURGES EXPERIENCED, N1 FLUCTUATIONS THEN ENGINE STALLED ON APPROACH. EGT HIT 700C, FIRE SURPRESSION INITIATED.SDR CA000110085Coffeemaker · shorted(CAN) FLIGHT ATTENDANT REPORTED RECIEVING AN ELECTRICAL SHOCK FROM COFFEEMAKER. COFFEEMAKER REPLACED.SDR CA000110084Motor · failed(CAN) COMPRESSOR FAULT MESSAGE DISPLAYED.VARIABLE BLEED VANE GEAR MOTOR ASSY REPLACED.SDR CA000209028Computer · failed(CAN) SLAT LOCKED ON APPROACH ACCOMPANIED WITH NR 1 SLAT/FLAP COMPUTER FAIL (SFCC) ECAM WARN ILLUMINATED. SFCC REPLACED.SDR 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.SDR CA991231026Apu · odor(CAN) PUNGENT SMELL EVIDENT WITH AIR CONDITIONING PACKS ON AND SOURCE SELECTED TOAPU AIR.OIL CONTAMINATION FOUND IN APU COMPARTMENT, APU REPLACED.SDR CA991231025Apu · failed(CAN) OILY SMELL IN AIRCRAFT DURING FLIGHT. INVESTIGATION REVEALED APU INTERNAL FAILSDR CA991231024Controller · smoke(CAN) BOTH WINDSCREENS ARCING AND STRONG SMELL OF SMOKE IN COCKPIT ON APPROACH. AIRCRAFT LANDED BOTH WINDSCREENS AND WINDSHIELD HEAT CONTROLLER REPLACED.SDR CA991208052Fmgc1 Data · faulty(CAN) ECAM REPORTED FMGC 1 FAULT. NR 1 FMGC RESET.SDR CA991231022Computer · failed(CAN) ECAM MESSAGE SLAT WARN ILLUMUINATED. AIRCRAFT LANDED SLAT COMPUTER RESET.SDR CA991231021Valve · failed(CAN) UNABLE TO MAINTAIN CABIN PRESSURISATION IN AUTO OR MANUAL MODE. NR 1 HIGH PRESSURE VALVE REEPLACED.SDR CA991208051Fan · failed(CAN) STRONG SMELL BURNING PLASTIC, VIBRATION AND SMOKE IN COCKPIT AND ECAM MASSAGE VENT EXTRACT FAN. AIRCRAFT LANDED, VENT FAN REPLACED.SDR 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.SDR CA991231019Seal · missing(CAN) LEADING EDGE CUSHON SEAL FOUND MISSING ON INBOARD TRAILING FLAP.SDR CA991208050Tru · faulty(CAN) ELECTRICAL BURNING SMELL REPORTED APPARENTLY COMING FROM AIR CONDITIONING PACKS. INVESTIGATION REVEALED NR 2 TRU FAILED. UNIT REPLACED.SDR CA991210056Flap · failed(CAN) FLAPS FAILED AT O DEGREES ON APPROACH. AIRCRAFT LANDED FLAP BRAKES RESET.SDR CA991210039Acm · failed(CAN) BURNT SMELL IN CABIN, NR2 ACU PACK TURNED OFF, SMELL DISSIPATED. NR2 ACM REPLACED.SDR 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. SDR CA991103086Sensor · failed(CAN) RT GEAR DOOR REMAINED OPEN ON LANDING. PROX SENSOR REPLACED.SDR AU991103086Prox Sensor · failed(AU) RIGHT GEAR DOOR REMAINED OPEN ON LANDING. PROXIMITY SENSOR REPLACED.SDR 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)SDR 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).SDR CA991103084Stop · out of adj(CAN) L1 CABIN DOOR VERY HARD TO OPEN. INNER HANDLE STOP ADJUSTED.SDR 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. MAINTENANCSDR 9904283202Floorbeam · corrodedDURING M-CHECK, FOUND CORROSION ON FLOORBEAM 254R AND 765R BETWEEN FRAMES 16-24R. REPAIRED PER EA 163484 AND SRM 51-72-11.SDR CA991028044Fadec · failed(CAN) NR 2 FADEC B FAULT, ENGINE REMOVED, TEAR DOWN TO FOLLOW.SDR 9904273202Floorbeam · corrodedDURING M-CHECK, FOUND CORROSION ON FLOORBEAM 1292L BETWEEN FRAME 16 AND 18. REPAIRED PER EA 32-163484.SDR CA991008017Carbon Seal · failed(CAN) INTEGRATED DRIVE GENERATOR CARBON SEAL FAILED CAUSING LOSS OF ENGINE OIL.SDR CA991008016Sensor · faulty(CAN) AFTER TAKEOFF, LANDING GEAR ABSORBER FAULT ILLUMINATED.SDR 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.SDR CA990927001Windshield · cracked(CAN) PILOT'S WINDSHIELD OUTER PLY CRACKED.....REPLACED.SDR 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 SDR CA990927089Smoke Detector · malfunctioned(CAN) AVIONIC BAY SMOKE INDICATION WITH NO OBSERVED SMOKE. NO FAULT FOUND.SDR CA990927090Pump · failed(CAN) BLUE SYSTEM HYDRAULIC FAILURE DUE TO LOSS OF PRESSURE. BLUE HYDRAULIC SYSTEM PUMP REPLACED.SDR 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 CORSDR CA990916006Valve · leaking(CAN) AFTER TAKEOFF, FUEL OBSERVED LEAKING FROM RIGHT WING. AIRCRAFT LANDED. RIGHT AIR RELEASE VALVE FOUND TO BE UNSERVICEABLE, UNIT REPLACED.SDR CA990907058Windshield · cracked(CAN) IN CRUISE, LEFT PILOT'S WINDSHIELD OUTER PLY CRACKED. AIRCRAFT LANDED AND WINDSHIELD REPLACED.SDR CA990812035Sensor · failed(CAN) NR 2 COMPRESSOR VANE ECAM STAYED ON FOR 20 MINUTES AFTER TAKEOFF. REPLACED VARIABLE BLEED VANE POSITION SENSOR.SDR 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.
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