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 AU000705Frame · cracked(AUS) FUSELAGE FRAME 35 CRACKED IN ALL TWELVE HOLES LOCATED BETWEEN STRINGERS 30 AND 31 ON LT AND RT SIDES. FOUND DURING EDDY CURRENT INSPECTION IAW AD/A320/94.Sep 1, 2000 · Airbus A320211 · Fuselage Main, FrameSDR 0003313226Slide · deployedAFTER PARKING AT THE GATE, THE AFT LEFT DOOR WAS INADVERTENTLY OPENED WITH THE SLIDE ARMED. THE SLIDE FULLY DEPLOYED REACHING THE GROUND BUT DID NOT INFLATE. MAINTENANCE REPLACED THE SLIDE ASSEMBLY AND RESERVICED THE DOOR ASSIST BOTTLE.Aug 29, 2000 · N326US · Airbus A320211 · Escape SlideSDR 0003123203Packing · deterioratedDURING CRUISE RECEIVED HYD B RSVR LO LVL MESSAGE. FOLLOWED COM PROCEDURES, DIVERTED TO MKE, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING PACKING AT THE BLUE HYHDRAULIC SYSTEM PRESSURE SWITCH. OPERATIONAL CHECK OK.Aug 29, 2000 · N303US · Airbus A320211 · Hydraulic Pressure SensorSDR 0003243231B-Nut · looseDURING TAKEOFF ROLL AT 60 KNOTS RECEIVED ''HYD Y RSVR LO LVL'' MESSAGE. ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE SECURED LOOSE PARKING BRAKE PRESSURE RETURN LINE AT MANIFOLD WITH HP TRANSMITTER. LEAD CHECKED OK.Aug 28, 2000 · N331NW · Airbus A320211 · Hydraulic System, MainSDR CA001004018Engine · fire(CAN) HELICOPTER PILOT REPORTING SEEING FIRE IN BACK OF ONE ENGINE AFTER LANDING. A VISUAL INSPECTION OF BOTH ENGINES WAS COMPLETED WITH NO UNUSUAL FINDINGS. ALSO PILOTS DID NOT SEE ANY ABNORMAL INDICATION IN THE COCKPIT. AIRCRAFT CONSIDERED SERVICEABLE.Aug 24, 2000 · Airbus A320211 · Engine (Turbine/Turboprop)SDR CA001004022Computer · failed(CAN) ECAM MESSAGE ''F/CTL SPR FAULT'' CAME ON SHORTLY AFTER REACHING CRUISE ALTITUDE. SPOILER ELEVATOR COMPUTER REPLACED AND CHECKED SERVICEABLE AS PER 767 MAINTENANCE MANUAL.Aug 21, 2000 · Airbus A320211 · Aileron Control SystemSDR AU001068Slide · leaking(AUS) LT OFFWING ESCAPE SLIDE RAMP SEAMS LEAKING IN VARIOUS AREAS. DURING INVESTIGATION A SEAM ON THE UPPER INBOARD RAIL TUBE OPENED UP FOR APPROXIMATELY 406.4MM (16IN).Aug 17, 2000 · Airbus A320211 · Escape SlideSDR AU001067Slide · leaking(AUS) RT OFFWING SLIDE RAMP LEAKING IN VARIOUS LOCATIONS. DURING INVESTIGATION A SEAM OPENED UP FOR APPROXIMATELY 152.4MM (6IN).Aug 17, 2000 · Airbus A320211 · Escape SlideSDR CA000901011Engine · fod(CAN) A/C 415, AUGUST 16/2000, FLT 825, YQR, LOG SEQUENCE 0283316. ON TAKEOFF AT APPROXIMATELY 1800 AGL, A LARGE BIRD WAS INGESTED IN NR 1 ENGINE. SHARP YAW, VIBRATION INDICATION ABOVE 5 UNITS, REDUCED THRUST TO IDLE, RETURNED TO YQR. INITIAL INSPECTION FOUNDAug 16, 2000 · Airbus A320211 · Engine (Turbine/Turboprop)SDR CA000918008Bleed Valve · failed(CAN) RAPID DESCENT DUE TO RECURRING BLEED FAULTY OF NR 2 SYSTEM. REPLACED NR 2 ENGINE FAN VALVE, REPLACED 6730B01, NR 1 BLEED PRESSURE REGULATOR VALVE (P/N 6714C01) AND REPLACED TEMPERATURE CONTROL THERMOSTAT (P/N 342D030000).Aug 2, 2000 · Airbus A320211 · Compressor Bleed ValveSDR CA000830008Valve · failed(CAN) BLEED FAULT ON NR 1 & NR 2 AT 5,000 FEET, RESET COMPLETED, NR 1 STILL AT FAULT, NR 2 RETURN ON LINE FOR APPROXIMATELY 10 MINUTES BUT FAILED AGAIN, AIRCRAFT RETURNED TO HALIFAX, THE APU WAS USED TO RUN THE PACKS. AFTER INTERROGATION OF THE CFDS (CENTRALIZAug 2, 2000 · Airbus A320211 · Engine Bleed Air SystemSDR CA000804008Sensor · failed(CAN) ECAM CHIME AND ALERT ON FOR NR 2 ENGINE HIGH OIL TEMPERATURE. PROCEDURES FOLLOWED ON ECAM, NR 2 THRUST BROUGHT TO IDLE, OIL TEMPERATURE WAS 140 DEGREES.CELISUS, ALL OTHER ENGINE PARAMETERS WERE NORMAL. CREW SHUTDOWN NR 2 ENGINE AND DIVERTED. ENGINE OIL Jul 29, 2000 · Airbus A320211 · Engine Oil TemperatureSDR CA000830009Transformer · overheated(CAN) SMOKE IN COCKPIT NOTICED BY MAINTENANCE PERSONNEL WHILE DOING A SERVICE CHECK.AFTER INVESTIGATION FOUND TO BE THE NR2 RECTIFIER TRANSFORMER TO BE AT FAULT (OVERHEATING).RECTIFIER TRANSFORMER REPLACED.Jul 20, 2000 · Airbus A320211 · DC Rectifier/ConverterSDR CA000901010Light · illuminated(CAN) ECAM MESSAGE ILLUMINATED FOR HYD RSVR LO LVL. ON HYDRAULICS PAGE LEVEL APPEARED NORMAL. SELECTED TO RETURN TO YYC. DURING APPROACH, YELLOW ELECTRIC PUMP SELECTED BACK ON. PTU SELECTED BACK ON. PROBLEM WENT AWAY. MAINTENANCE CHECKED BSCU, NO FAULTS FOUND.Jul 19, 2000 · Airbus A320211 · Hydraulic Quantity SensorSDR AU000889Computer · faulty(AUS) FLIGHT AUGMENTATION COMPUTER (FAC) SUSPECT FAULTY. WORKSHOP INSPECTION COULD NOT FAULT ITEM.Jul 14, 2000 · Airbus A320211 · Flight Management Computing Hardware SystemSDR CA000802005Valve · failed(CAN) UNABLE TO PRESSURIZE AIRCRAFT AFTER TAKEOFF, AVIONIC EXTRACT VALVE SHOWED OPENED. EXTRACT VALVE REPLACED, AIRCRAFT CHECK SERVICEABLE.Jul 8, 2000 · Airbus A320211 · Cabin Pressure Control SystemSDR AU000578Controller · blocked(AUS) NO2 CABIN PRESSURE CONTROLLER PC PORT HAD A BLANKING CAP FITTED PREVENTING THE CONTROLLER FROM SENSING CORRECT CABIN PRESSURE.THE BLANKING CAP PNO CD-3 HAD BEEN FITTED TO THE PORT DURINGTROUBLESHOOTING AND HAD NOT BEEN REMOVED. PERSONNEL/MAINTENANCE ERROJun 30, 2000 · Airbus A320211 · Cabin Pressure ControllerSDR CA000721009Air Filter · contaminated(CAN) ON GROUND AFTER ENGINE START, SMELL OF EXHAUST (POSSIBLE FUEL VAPORS) IN REAR CABIN, DISSIPATED BEFORE DEPARTURE. ON FINAL APPROACH A STRONG KEROSENE SMELL EMANATED THROUGHOUT FORWARD GALLEY AND J CLASS CABIN AND SMELL DIDNT DISSPATE UNTIL AFTER ENGINES Jun 27, 2000 · Airbus A320211 · Air Distribution SystemSDR CA000721010Filter · dirty(CAN) BURNT RUBBER SMELL IN REAR GALLEY AFTER TAKEOFF ON CLIMB AT 11,000 FEET.DISSIPATED AFTER GALLEY POWER OFF. ON APPROACH WITH GALLEY POWER OFF SMELL REAPPEARED.FOUND GALLEY VENT FILTERS PLUGGED, DEBRIS FOUND BEHIND AND AROUND OVENS.AREA CLEANED AND NEW FILJun 20, 2000 · Airbus A320211 · Buffet/GalleysSDR AU000586Thermostat · failed(AUS) DURING CLIMB THE NR 2 BLEED OVERHEATED. SUSEQUENTLY, THE NO1 BLEED ALSO OVERHEATED, CABIN COULD NOT BE PRESSURISED. STRIP REPORT HIGH LIGHTED THAT THE NR 1 FAN AIR VALVE AND THE NR 2 TEMPERATURE CONTROL THERMOSTAT WERE BOTH FAULTY.Jun 14, 2000 · Airbus A320211 · Cabin Temperature Control SystemSDR AU000999Wire · damaged(AUS) RT INBOARD ELEVATOR SERVO POSITION FEEDBACK TRANSDUCER WIRE PNO 2793-0288 HAD INSULATION DAMAGE. SUSPECT DAMAGE CAUSED BY FOD.Jun 12, 2000 · Airbus A320211 · Elevator Control SystemSDR CA000714019Switch · seized(CAN) DURING CRUISE NR 2 ENGINE REVERSER FAULT MESSAGE, ENGINE SHUT DOWN ON APPROACH PER QUICK REFERENCE HANDBOOK PROCEDURE.FOUND LEFT HAND UPPER REVERSER DOOR DEPLOY SWITCH ASSEMBLY SEIZED.SWITCH ASSEMBLY RELEASED AND LUBRICATED. OPERATION CHECKED NORMAL.Jun 10, 2000 · Airbus A320211 · Engine Thrust ReverserSDR CA000621038Carriage · failed(CAN) DURING APPROACH WHEN FLAPS SELECTED TO 2 DEGREES FLAPS LOCKED MESSAGE APPEARED. QUICK REFERENCE HANDBOOK PROCEDURE CARRIED OUT, AIRCRAFT LANDED NORMALLY. RIGHT AND LEFT WING FLAPS GEAR BOXES, TORQUE TUBES AND TRANSMISSIONS INSPECTED, NO FAULT. RIGHT AND Jun 4, 2000 · Airbus A320211 · Trailing Edge FlapsSDR CA000614049Fan · failed(CAN) PASSENGER & CREW MENTIONED ELECTRICAL SMELL IN AREA OF ROW 20-23. OCCURRED AFTER 2 HOUR INTO CRUISE. FOUND R/H RECIRULATING FAN CAUSING ODOUR. FAN CHANGED, SYSTEM CHECKED SERVICEABLE.May 26, 2000 · Airbus A320211 · Air Distribution FanSDR CA000614048Wheel · damaged(CAN) RT HAND NOSE WHEEL DAMAGED & PIECE BROKEN OFF. SLIGHT VIBRATION WAS NOTICED ON TAKEOFF AND DETERIORATED ON LANDING. NOSE WHEEL ASSEMBLY CHANGED, NO OTHER DAMAGE FOUND. HIGH SPEED TAXI CARRIED OUT NORMAL.May 25, 2000 · Airbus A320211 · Wheel/Ski/FloatSDR CA000530060Light · failed(CAN) ELECTRICAL BURNING SMELL AND A LITTLE SMOKE IN COCPIT IN VICINITY OF FO SLIDING WINDOW. MAP LIGHT ASSY SHORTING ON LAMP SOCKETAND SMOKING. UNIT REPLACED.May 20, 2000 · Airbus A320211 · Flight Compartment LightingSDR CA000530059Computer · malfunctioned(CAN) ON APPROACH FLAP/SLATS SELECTED WITH NO MOVEMANT. LANDED FLAPLESS. SYSTEM INSPECTED WITH NO FAULT FOUND, COMPUTER RESET, OPERATED NORMAL.May 12, 2000 · Airbus A320211 · Leading Edge Slat Control SystemSDR CA000718004Starter · leaking(CAN) AFT CARGO SMOKE WARNING ON AT FLIGHT LEVEL 270 ON CLIMB. RETURNED TO AIRPORT. AIRCRAFT GROUND RUN BOTH ENGINES FOR 15 MINUTED. AIR CONDITIONING CHECKED AT IDLE, LOW AND MEDIUM POWER. ALL VENTS OPENED AND SYSTEM PURGED TO CLEAR CONTAMINATION CAUSED BY GROMay 6, 2000 · Airbus A320211 · Engine Starting SystemSDR 0001483203Line · rupturedAFTER TAKEOFF WHEN LANDING GEAR SELECTED UP, RECEIVED HYD G RSVR LO LVL AND L/G GEAR NOT UPLOCKED MESSAGES. FOLLOWED COM PROCEDURES, RETURNED TO DEPARTURE FIELD, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED BLOWN FLEX LINE FOR THE LEFT MAIN GEAR INBOARDApr 27, 2000 · N303US · Airbus A320211 · Hydraulic System, AuxiliarySDR 0001663214Frame · crackedDURING 1C-CHECK, FOUND CRACK ON FRAME NR 54 AT AFT CARGO DOOR. REPAIRED PER EA 32-175984.Apr 19, 2000 · N314US · Airbus A320211 · Fuselage Main, FrameSDR CA000505027Fan · overheated(CAN) ECAM AVIONICS SMOKE WARNING AND EVIDENCE OF SMOKE IN CABIN. AIRCRAFT LANDED. SCREEN AND FILTER AT AVIONICS EXTRACT FAN FOUND SOILED AND FAN HOT. FAN AND FILTERS REPLACED.Apr 15, 2000 · Airbus A320211 · Air Distribution FanSDR CA000505025Computer · malfunctioned(CAN) POST NR 2 ENGINE SHUTDOWN, FIRE WARNING ON OVERHEAD PANEL. NO BELL OR ECAM. FLIGHT WARNING COMPUTER RESET, ENGINE STARTED AND SHUTDOWN TO CONFIRM FAULT CLEARED. GROUND RUNS CARRIED OUT. AIRCRAFT RETURNED TO SERVICE.Apr 15, 2000 · Airbus A320211 · Flight Management Computing Hardware SystemSDR CA000410030Proximity Switch · faulty(CAN) UNABLE TO EXTEND LANDING GEAR. EMERGENCY EXTENSION CARRIED OUT. INVESTIGATION REVEALED FAULTY PROXIMITY SENSOR NR 37GA ON THE LEFT NOSE GEAR DOOR. SWITCH REPLACED.Mar 25, 2000 · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR AU000351Fitting · cracked(AUS) LT MAIN LANDING GEAR DOOR ACTUATOR FORWARD AND AFT ATTACHMENT FITTINGS PNO D5337061320300 (FORWARD) AND PNO D5337061320200(AFT) CRACKED IN THE VERTICAL FLANGE. FOUND DURING EDDY CURRENT AND ULTRASONIC INSPECTION IAW AIRBUS SB A320-53A1135. CRACK LENGTHS Mar 23, 2000 · Airbus A320211 · Fuselage, Landing Gear Attach FittingsSDR AU000888Contactor · faulty(AUS) AC ESSENTIAL BUS FEED SWITCH CONTACTOR 3XC FAULTY.Mar 22, 2000 · Airbus A320211 · AC Power Distribution SystemSDR AU000381Frame · corroded(AUS) FUSELAGE FRAME 20 LOCATED IN R1 DOOR CUTOUT SEVERELY CORRODED.AREA OF CORROSION 152.4MM BY 101.6MM (6IN BY 4IN) WITH A MAXIMUMDEPTH OF 2.8MM (0.112IN). EVIDENCE OF PREVIOUS CORROSION REMOVALIN THE SAME AREA.Mar 15, 2000 · Airbus A320211 · Fuselage Main, FrameSDR CA000320010Dampener · leaking(CAN) GREEN HYDRAULIC LOW LEVEL ANNUNCIATOR ON. LEFT YAW DAMP FOUND LEAKING.Mar 15, 2000 · Airbus A320211 · Autopilot SystemSDR 0000813211Turbine Case · puncturedDURING MAIN ENGINE START, APU SHUT DOWN.. MAINTENANCE FOUND A HOLE IN APU COMPRESSOR CASE, NO AC DAMAGE NOTED. REPLACED THE APU. CHECKED OK.Mar 4, 2000 · N311US · Airbus A320211 · APU Core EngineSDR CA000320029Actuator · failed(CAN) HIGH FREQUENCY VIBRATION FELT IN AFT GALLY DURING CLIMB. VIBRATION DISSIPATED DURING CRUISE. YELLOW SYSTEM RUDDER ACTUATOR FOUND AT FAULT. REPLACED.Mar 2, 2000 · Airbus A320211 · Rudder ActuatorSDR AU000077Bolt · loose(AUS) LT MAIN LANDING GEAR FORWARD PINTLE PIN LOCK BOLT SHOWED EVIDENCE OF ROTATION. FOUND DURING VISUAL INSPECTION IAW SB A320-32-1187.Feb 22, 2000 · Airbus A320211 · Main Landing Gear Strut/Axle/TruckSDR CA000320022Computer · failed(CAN) SLATS LOCKED AT NR 2 POSITION AFTER FAILURE OF SLAT FLAP COMPUTER (SFCC).Feb 13, 2000 · Airbus A320211 · Leading Edge Slat Control SystemSDR 0000283218Valve · leakingDURING DESCENT RECEIVED HYD G RSVR LO LEVEL MESSAGE. FOLLOWED COM PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING NOSE LANDING GEAR DOOR BYPASS VALVE. RESERVICED SYSTEM. LEAK CHECK OK.Feb 2, 2000 · N318US · Airbus A320211 · Landing Gear Door Retract SectionSDR 0000273221Line · leakingDURING DESCENT RECEIVED HYD Y RSVR LO LEVEL MESSAGE. FOLLOWED COM PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC LINE ON LEFT WING AFT SPAR. RESERVICED SYSTEM. LEAK CHECK OK.Feb 2, 2000 · N321US · Airbus A320211 · Hydraulic System, MainSDR CA000215040Panel · failed(CAN) IN CRUISE, APU FIRE PBA INDICATION ON WITH NO ECAM MESSAGE. CREW RESET AND UNABLE TO CLEAR. APU FIRE PANEL REPLACED.Feb 1, 2000 · Airbus A320211 · Detection SystemSDR AU000075Bolt · loose(AUS) LT MAIN LANDING GEAR STRUT BOLTS (8OFF12) LOOSE. THE TAB WASHERSWERE STILL IN PLACE BUT DISTORTED. DAMAGE WAS FOUND ON THE UPPERDIAPHRAGM TUBE, UPPER BEARING HOUSING AND GLAND HOUSING.Jan 31, 2000 · Airbus A320211 · Main Landing Gear Strut/Axle/TruckSDR CA000215039Receptacle · failed(CAN) WHILE ATTEMPTING TO ESTABLISH GROUND POWER ON AIRCRAFT, A LARGE SPARK WAS EMITTED FROM RECEPTACLE. RECEPTACLE AND BONDING WIRE REPLACED.Jan 30, 2000 · Airbus A320211 · External Power SystemSDR AU000058Fitting · cracked(AUS) MAIN LANDING GEAR DOOR ACTUATOR ATTACHMENT FITTINGS (4OFF) CRACKED. FOUND DURING EDDY CURRENT AND ULTRASONIC INSPECTION IAWSB A320-53A1135.Jan 27, 2000 · Airbus A320211 · Wing, Landing Gear Attach FittingsSDR AU000057Fitting · cracked(AUS) MAIN LANDING GEAR DOOR ACTUATOR ATTACHMENT FITTINGS (4OFF)CRACKED ON INBOARD FLANGES. FOUND DURING EDDY CURRENT AND ULTRASONIC INSPECTION IAW SB A320-53A1135.Jan 27, 2000 · Airbus A320211 · Wing, Landing Gear Attach FittingsSDR 0000183211Valve · leakedAFTER CLIMB, RECEIVED HYD Y RSVR LO LVL MESSAGE. FOLLOWED COM PROCEDURES AND DIVERTED TO MEM WITH AN UNEVENTFUL LANDING. MAINTENANCE REPLACED LEAKING PARK BRAKE VALVE. OPERATIONAL CHECK OK.Jan 24, 2000 · N311US · Airbus A320211 · Hydraulic System, MainSDR AU000067Arm · cracked(AUS) COCKPIT SLIDING WINDOW OPERATING ARMS CRACKED. FOUND DURING INSPECTION IAW ER A32-56-10-9.Jan 19, 2000 · Airbus A320211 · Flight Compartment Windows
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