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 AU980957Bushing · separated(AUS) R1, R2, AND L2 CABIN DOOR LOWER CONNECTION LINK BUSHINGS MIGRATED. FOUND DURING INSPECTION IAW ER A32-52-10-7C.Jun 24, 1998 · Airbus A320211 · Service DoorsSDR AU980942Bushing · separated(AUS) L1 AND R1 SERVICE DOOR LOWER CONNECTION LINK BUSHES AND R2 SERVICE DOOR UPPER CONNECTION LINK BUSHES MIGRATED. FOUND DURING INSPECTION IAW ER A32-52-10-7C.Jun 23, 1998 · Airbus A320211 · Service DoorsSDR CA990203016Blade · damaged(CAN) ENGINE WAS INDUCTED IN THE SHOP FOR HIGH PRESSURE NOZZLE GUIDE VANE (NGV) BURNS. ON DISASSEMBLY OF ENGINE, TWO VANES WERE FOUND TO HAVE THE COMPLETE LEADING EDGE BURNED AWAY. THE METAL LOSS EXTENDED TO THE MIDSPAN INTERNAL BULKHEAD OF THE VANE. THE PAJun 17, 1998 · Airbus A320211 · Turbine SectionSDR CA980629024Blade · burned(CAN) DURING ENGINE DISASSEMBLY IN THE SHOP FOR BURN HP NGV, TWO VANES WERE FOUND TO HAVE THE COMPLETE LEADING EDGE BURNED AWAY. THE METAL LOSS EXTENDED TO THE MIDSPAN INTERNAL BULKHEAD OF THE VANE. FURTHER EVALUATION BEING CARRIED OUT.Jun 17, 1998 · Airbus A320211 · Turbine SectionSDR AU980935Bushing · separated(AUS) L1 AND R1 SERVICE DOOR LOWER CONNECTION LINK BUSHES AND L2 AND R2 UPPER AND LOWER CONNECTION LINK BUSHES MIGRATED. FOUND DURING INSPECTION IAW ER A32-52-10-7C.Jun 15, 1998 · Airbus A320211 · Service DoorsSDR CA980706025Outflow Valve · failed(CAN) EXCESSIVE CABIN ALTITUDE NOTED AT FLT LEVEL 310. CABIN ALTITUDE CLIMB AT 550, INITIATED EMERGENCY DESCENT, CABIN CONTINUED TO CLIMB TO 1180, AFTER LEVEL OFF CABIN PRESSURE STABILIZED. MAINTENANCE REPLACED OUTFLOW VALVE AND OPERATIONALLY CHECKED IN AUTOJun 13, 1998 · Airbus A320211 · Pressure Regulator/Outflow ValveSDR AU980988Hose · failed(AUS) LEFT MAIN LANDING GEAR DOOR ACTUATOR HOSE FAILED ADJACENT TO THEINBOARD END FITTING. LOSS OF `GREEN' SYSTEM HYDRAULIC FLUID.Jun 6, 1998 · Airbus A320211 · Landing Gear Door ActuatorSDR CA980707016Control Unit · malfunctioned(CAN) ON LANDING, AFTER ROLL OUT, NOSE WHEEL STEERING FAILED. MAINTENANCE REPLACED STEERING SERVO VALVE AND BRAKE/STEERING CONTROL UNIT. VALVE DID NOT RECTIFY THE PROBLEM, HOWEVER, THE BRAKE/STEERING CONTROL UNIT CURED THE PROBLEM. PART TC: 8,276.Jun 4, 1998 · Airbus A320211 · Landing Gear Steering SystemSDR CA980608019Retract Mech · malfunctioned(CAN) FLAP OVERSPEED AT FULL FLAP ON APPROACH. FLAP AND SLAT OVERSPEED INSPECTION AND OPERATION CARRIED OUT. NO FAULT FOUND, A/C SERVICEABLE.May 20, 1998 · Airbus A320211 · Trailing Edge Flap Control SystemSDR AU980956Bushing · separated(AUS) L1 AND L2 SERVICE DOOR LOWER CONNECTION LINK BUSHES MIGRATED. FOUND DURING INSPECTION IAW ER A32-52-10-7C.May 19, 1998 · Airbus A320211 · Service DoorsSDR 9809053219Pump · leakingDURING CRUISE, RECEIVED HYD B RSVR LOW LEVEL MESSAGE. FLIGHT DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING BLUE ELECTRIC HYDRAULIC PUMP. OPERATIONAL CHECK OK.May 11, 1998 · N319US · Airbus A320211 · Hydraulic Pump (Electric/Engine), MainSDR CA980608029Unknown · smoke(CAN) ECAM WARNING, SMOKE IN LAVATORY. AIRCRAFT RETURNED TO DEPARTURE TERMINAL. MAINTENANCE TECHS OPERATED BOTH AIR CONDITIONERS FOR 30 MINUTES AND WERE UNABLE TO DUPLICATE PROBLEM, NO EVIDENCE OF SMOKE. LAVATORY SMOKE DETECTION SYSTEM CHECKED SERVICEABLE.May 10, 1998 · Airbus A320211 · Smoke DetectionSDR 9808893211Actuator · failedDURING CRUISE, LOST GREEN HYDRAULIC SYSTEM FLUID. FLIGHT DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING SPOILER ACTUATOR, OPERATIONAL CHECK OK.May 9, 1998 · N311US · Airbus A320211 · Drag Control ActuatorSDR CA980608031Linkage Pin · missing(CAN) ON CLIMB, DURING GEAR UP SELECTION, ECAM WARNING LANDING GEAR AND INTERFACE UNIT FAULT AND GEAR DOOR NOT CLOSED AT NOSE LANDING GEAR. A/C RETURNED TO DEPARTURE TERMINAL. MAINTENANCE CHECK REVEALED NOSE GEAR DOOR ACTUATOR EYE AND LINKAGE PIN MISSING. NMay 8, 1998 · Airbus A320211 · Landing Gear Door Retract SectionSDR AU980989Brake · malfunctioned(AUS) RIGHT WING TIP BRAKE UNIT FAULTY. SUSPECT DUE TO MOISTURE INGRESS.May 6, 1998 · Airbus A320211 · Drag Control SystemSDR 9808903201Controller · failedDURING CRUISE, ECAM MESSAGE CAB PR SYS 1+2 FAULT ILLUMINATED AND ESCESSIVE CABIN ALTITUDE WAS NOTICED. CREW INITIATED EMERGENCY DESCENT WHILE USING MANUAL PRESSURIZATION CONTROL AVERTING PASSENGER OXYGEN MASK DEPLOYMENT. FLIGHT DIVERTED TO MSP AND LANDED WITMay 6, 1998 · N301US · Airbus A320211 · Cabin Pressure ControllerSDR 9808613214Power Supply · inoperativeCREW OBSERVED CABIN LIGHTING CIRCUIT BREAKER POPPED. FURTHER INVESTIGATION REVEALED EMERGENCY EXIT LIGHTS AFT OF ROW 9 INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND BATTERY 13WL AND 11WL.May 6, 1998 · N314US · Airbus A320211 · Emergency LightingSDR CA980608032Slat · inoperative(CAN) SLATS DID NOT EXTEND WHEN SELECTED. MAINTENANCE ACTION INVOLVED CHANGING WING TIP BRAKE.May 3, 1998 · Airbus A320211 · Leading Edge Slat Control SystemSDR AU980974Hose · failed(AUS) HYDRAULIC HOSE FAILED. LOSS OF `GREEN' HYDRAULIC SYSTEM. INVESTIGATION FOUND THE RIGHT MAIN LANDING GEAR DOWNLOCK ACTUATOR HOSE HAD FAILED ADJACENT TO THE LOWER SWIVEL FITTING. PART TC: 18,828May 2, 1998 · Airbus A320211 · Hydraulic System, MainSDR CA980602022Stabilizer · damaged(CAN) DURING POST HMV ENGINE RUNS, A LARGE PIECE OF ASPHALT DISLODGED STRIKING THE TRIMMABLE HORIZONTAL STABILIZER LT SIDE CAUSING UNREPAIRABLE DAMAGE. T.H.S. REPLACED AND REPAIR TO FUSELAGE SKIN CARRIED OUT. INSPECTIONS TO SURROUNDING STRUCTURES AND VERTICAMay 1, 1998 · Airbus A320211 · Horizontal Stabilizer StructureSDR 9807753212Power Supply · inoperativeDURING TEST OF EMERGENCY LIGHT SYSTEM, EXIT LIGHT ABOVE DOOR 2L WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY AND BATTERY PACK, OPERATIONAL CHECK OK.Apr 30, 1998 · N312US · Airbus A320211 · Emergency LightingSDR 9807633226Battery Pack · dischargedDURING EMERGENCY LIGHT TEST, INT LOADS EMER R FAULT DISPLAYED. MAINTENANCE REPLACED PSEU BATTERY PACK. OPERATIONAL CHECK OK.Apr 27, 1998 · N326US · Airbus A320211 · Emergency LightingSDR 9807233206Battery Pack · dischargedDURING TEST OF THE EMERGENCY LIGHT SYSTEM, INT LOAD EMERG L FAULT WAS DISPLAYED. MAINTENANCE REPLACED BATTERY PACK AND POWER SUPPLY 11WL. OPERATIONAL CHECK OK.Apr 23, 1998 · N360US · Airbus A320211 · Emergency LightingSDR 9806963202Fuel Tank · leakingDURING CLIMB, A FUEL LEAK FROM THE RIGHT WING WAS REPORTED. FLIGHT CREW DIVERTED TO MSP. DURING DESCENT INTO MSP WHILE FOLLOWING COM FOR A FUEL LEAK, NR 2 ENGINE FLAMED OUT AT 5000 FEET. A SUCCESSFUL RELIGHT WAS ACCOMPLISHED, AN UNEVENTFUL LANDING WAS PERFOApr 17, 1998 · N302US · Airbus A320211 · Aircraft Fuel Distribution SystemSDR 9806943209Oil Line · crackedDURING CRUISE, AFT CARGO SMOKE INDICATION ILLUMINATED. CREW DISCHARGED CARGO FIRE EXTINGUISHER, DECLARED AN EMERGENCY, DIVERTED TO JAX, AND LANDED WITHOUT INCIDENT. NO INDICATION OF FIRE OR SMOKE IN AFT CARGO COMPARTMENT UPON INSPECTION BY FIRE FIGHTING CREWApr 17, 1998 · N309US · Airbus A320211 · Turbine Engine Oil SystemSDR CA980602018Beam · cracked(CAN) DURING SLIDE ASSEMBLY REMOVAL, FOUND O/W SLIDE SUPPORT BEAM RH SIDE CRACKED FROM FORWARD END TO FORWARD END SLIDE MOUNT FASTENER HOLE.Apr 15, 1998 · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA980512021Duct Seal · missing(CAN) ON DEPARTURE, NR 2 ENG FIRE LIGHT ILLUMINATED. WHEN NR 2 ENGINE THRUST LEVER AT IDLE, ENGINE LIGHT WENT OUT. ENGINE WAS NOT SHUT DOWN. MAINTENANCE FOUND SEAL MISSING FROM HIGH PRESSURE DUCT FLANGE AT 7 O'CLOCK POSITION AND FLANGE AT 4 O' CLOCK POSITIOApr 15, 1998 · Airbus A320211 · Pneumatic Distribution SystemSDR 9806663209Oil Syst · leakingSHORTLY AFTER TAKEOFF, FLIGHT CREW NOTICED A BURNING SMELL AND LIGHT SMOKE HAZE THROUGHOUT THE AIRCRAFT. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. MAINTENANCE FOUND INTERNAL OIL LEAK IN NR 1 ENGINE. REPLACED THE NR 1 ENGINE.Apr 15, 1998 · N309US · Airbus A320211 · Turbine Engine Oil SystemSDR 9806543231Anti-Ice Valve · malfunctionedEN ROUTE, POSSIBLE ICING CONDITIONS WERE REPORTED. THE NR 1 ENGINE ANTI-ICE VALVE WOULD NOT OPEN. FLIGHT CREW DIVERTED TO COS. MAINTENANCE REPLACED THE ANTI-ICE VALVE.Apr 14, 1998 · N331NW · Airbus A320211 · Engine Anti-Icing SystemSDR 9806573209Pack · overheatFOLLOWING TAKEOFF, GRAY SMOKE WITH AN OILY SMELL WAS OBSERVED IN THE COCKPIT AND CABIN. CREW PERFORMED THE AIR CONDITIONING SMOKE PROCEDURE PER COCKPIT OPERATING MANUAL AND DECLARED AN EMERGENCY, RETURNED TO DTW, AND LANDED WITHOUT INCIDENT. NR 1 PACK WAS PLApr 10, 1998 · N309US · Airbus A320211 · Cabin Cooling SystemSDR 9806383223Power Supply · inoperativeDURING TEST OF EMERGENCY LIGHT SYSTEM, RECEIVED FAULT RT OVERWING. MAINTENANCE REPLACED RIGHT OVERWING POLWER SUPPLY AND BATTERIES, OPERATIONAL CHECK OK.Apr 10, 1998 · N323US · Airbus A320211 · Emergency LightingSDR 9806373209Connector · looseDURING TEST OF EMERGENCY LIGHTS, FOUND LIGHTS INOPERATIVE AT SEAT ROWS 19 TO 21ABC. MAINTENANCE SECURED CANNON PLUG AT SIDEWALL BELOW SEAT 19ABC, OPERATIONAL CHECK OK.Apr 9, 1998 · N309US · Airbus A320211 · Emergency LightingSDR CA980415006Actuator · leaking(CAN) FOUND NR 2 ENGINE LEAKING FUEL WHEN DOING WALKAROUND. TRACED LEAK TO VBV ACTUATOR MOTOR. REPLACED MOTOR, ENGINE RUN CARRIED OUT AND FUNCTIONALLY AND LEAK CHECKED SERVICEABLE. AIRCRAFT RETURNED TO SERVICE.Apr 8, 1998 · Airbus A320211 · Fuel Controlling SystemSDR CA980417008Control Unit · failed(CAN) FLAPS LOCKED OUT DURING EXTENSION ON APPROACH. SLAT/FLAP CONTROL COMPUTER RESET CARRIED OUT AND SYSTEM CHECKED NORMAL.Apr 5, 1998 · Airbus A320211 · Trailing Edge Flap Control SystemSDR CA980417007Sensor · failed(CAN) TWO ATTEMPTS WERE MADE BEFORE ALL THREE LANDING GEAR EXTENDED. CHANGED SENSOR 37G NOSE GEAR DOOR OPEN, RETRACTIONS CARRIED OUT, CHECKED SERVICEABLE.Apr 5, 1998 · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR CA980417006Outflow Valve · failed(CAN) AFTER TAKEOFF, A/C OVERPRESSURIZED DUE TO FAULTY NR SYSTEM AND NR SYSTEM DID NOT TAKE CONTROL. ALSO, DIFFICULTY ENCOUNTERED WITH MANUAL CONTROL. CLIMB-OUT OF FLIGHT LEVEL 320 LOST CONTROL OF CABIN, FIRST DESCENDED, THEN FULL CLIMB AT 3,700 FEET PER MIApr 2, 1998 · Airbus A320211 · Pressure Regulator/Outflow ValveSDR CA980417005Control Unit · failed(CAN) FLAPS STOPPED FROM ZERO AND 1 UNIT. FLAP CONTROL COMPUTER RESET, CLEARED WARNING, PRESSURIZED HYDRAULIC SYSTEMS, CYCLED FLAPS, AND SLATS, OPERATION NORMAL.Apr 2, 1998 · Airbus A320211 · Trailing Edge Flap Control SystemSDR CA980415005Uplock · warning(CAN) UNSAFE LANDING INDICATION. A/C RETURNED TO BASE. MAINTENANCE CHECK REVEALED LANDING UPLOCK HOUSING FILLED WITH GREASE. UPLOCK CLEANED AND LANDING RETRACTION TESTS CARRIED OUT, SERVICEABLE.Apr 2, 1998 · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR CA980417013Line · chafed(CAN) ON CLIMBOUT, NR 2 ENGINE OIL QUANTITY NOTICED DECREASING. PRESSURE AND TEMPERATURE NORMAL. JUST AFTER QUANTITY WENT TO ZERO, OIL PRESSURE STARTED TO DROP. ENGINE SHUT DOWN. AIRCRAFT GROUND RUN AND FOUND OIL PRESSURE LINE TO NR 5 BEARING CHAFED. LINEApr 1, 1998 · Airbus A320211 · Turbine Engine Oil SystemSDR 9805313214T12 Sensor · malfunctionedDURING CLIMB, NR 2 ENGINE N1, FUEL FLOW, AND EGT BEGAN TO FLUCTUATE. FLUCTUATION CONTINUED DESPITE VARIOUS POWER SETTINGS OR IN A CONSTANT POWER SETTING. FLIGHT CREW RETURNED TO DEPARTURE AIRPORT. MAINTENANCE REPLACED THE FUEL FILTER, FUEL PUMP, HMU, AND T1Mar 30, 1998 · N314US · Airbus A320211 · Fuel Controlling SystemSDR CA980406014Line · leaking(CAN) ECAM LOW YELLOW HYDRAULIC QUANTITY INDICATION. ACTION ECAM PROCEDURE LEVEL STABILIZED ABOVE MINIMUM WARNING LEVEL. T/R YELLOW SYSTEM LINE TO T/R IN NR 2 PYLON FOUND DAMAGED CAUSED BY SHEARED RIVET ATTACH BRACKET WEARING INTO LINE. REPLACED LINE.Mar 27, 1998 · Airbus A320211 · Hydraulic System, MainSDR CA980325011Concentrator · failed(CAN) AIRCRAFT RETURNED TO DEPARTURE TERMINAL DUE TO LOSS OF 6 PRIMARY FLIGHT DISPLAYS (CDU'S). SYSTEM DATA ACQUISITON CONCENTRATOR (SDCU) REPLACED. LOSS OF CDU'S WAS DUE TO MEL APPLIED THAT ALLOWED ALL CDU'S TO BE POWERED FROM NR 1 BUS. MEL WAS APPLIED BECMar 24, 1998 · Airbus A320211 · Flight Management Computing Hardware SystemSDR CA980424012Sensor · failed(CAN) FLAPS LOCKED AND ALIGNMENT FAULT APPEARED ON ELECTRONIC CENTRALIZED A/C MONITORING AT SELECTION OF FLAPS. TWO ECM PROCEDURES CARRIED OUT AND NORMAL LANDING COMPLETED. FLAP WING TIP BRAKE RESET. ON WALK AROUND, FOUND RIME ICE NEAR SENSORS ON FLAPS, SUSMar 19, 1998 · Airbus A320211 · Trailing Edge Flap Control SystemSDR AU980937Bushing · separated(AUS) L1 SERVICE DOOR LOWER CONNECTION LINK BUSH AND L2 SERVICE DOORUPPER CONNECTION LINK BUSH MIGRATED. FOUND DURING INSPECTION IAWER A32-52-10-7C.Mar 16, 1998 · Airbus A320211 · Service DoorsSDR 9804473231Battery Pack · dischargedDURING TEST OF EMERGENCY FLOOR PATH LIGHTING, FOUND LIGHTS INOPERATIVE AT SEAT ROWS 19-21 AND 25-27. MAINTENANCE REPLACED THE BATTERY PACK, OPERATIONAL CHECK OK.Mar 16, 1998 · N331NW · Airbus A320211 · Emergency LightingSDR 9805373225Power Pack · inoperativeDURING TEST OF EMERGENCY LIGHTS VIA CIDS, THE LEFT CENTER EMERGENCY POWER PACK FAILED. MAINTENANCE REPLACED POWER SUPPLY PACK, OPERATIONAL CHECK OK.Mar 14, 1998 · N325US · Airbus A320211 · Emergency LightingSDR 9805393227Battery · dischargedDURING TEST OF EMERGENCY LIGHT SYSTEM, FORWARD LEFT EMERGENCY LIGHT BATTERY FAILED. MAINTENANCE REPLACED BATTERY, OPERATIONAL CHECK OK.Mar 10, 1998 · N327NW · Airbus A320211 · Emergency LightingSDR CA980317032Fuselage · loud bang(CAN) A/C EXPERIENCED A LOUD BANG AND SHUDDER DURING CLIMB IN CLEAN AIR AND CLEAN CONFIGURATION. AFTER RETURN TO BLOCKS, A/C INSPECTED FOR BIRD STRIKE AND INSPECTION OF AIR CONDITIONING PACKS AND BORESCOPE CHECK OF ENGINES CARRIED OUT. NO DEFECTS FOUND. AIRMar 9, 1998 · Airbus A320211 · Aircraft StructuresSDR CA980317031Door · out of rigging(CAN) LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. FOUND RT MAIN LANDING GEAR DOOR OUT OF RIG. MAIN LANDING GEAR DOOR RIGGED.Mar 9, 1998 · Airbus A320211 · Landing Gear Door Retract SectionSDR AU980938Bushing · separated(AUS) L1 SERVICE DOOR UPPER AND LOWER CONNECTION LINK BUSHES AND R1 DOOR LOWER CONNECTION LINK BUSH MIGRATED. FOUN D DURING INSPECTION IAW ER A32-52-10-7C.Mar 4, 1998 · Airbus A320211 · Service Doors
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