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 0102543210Frame · corrodedIn M check, found corrosion in nutplate hole on FR 68 R/H, 1 inch from inboard flange and 1 inch above door threshold. Repaired per EA32-184166.Jul 19, 2001 · N310NW · Airbus A320211 · Fuselage Main, FrameSDR CA010814006Tire · separated(CAN) #3 MAIN WHEEL TIRE CAP SEPARATION ON TAKEOFF. AIR TURN BACK TO AIRPORT. AIRCRAFT SUSTAINED DAMAGE TO #2 ENGINE FAN BLADES, ENGINE INTAKE ACOUSTIC PANELS, R/H INBOARD TRAILING EDGE FLAP. ONE LINE OF THE YELLOW HYDRAULIC SYSTEM BROKE IN AREA OF R/H MAIN LAJul 18, 2001 · Airbus A320211 · TireSDR CA010531004Bearing · seized(CAN) PASSENGER DOOR L1 NOISEY DURING DECENT, WHEN DOOR OPENED ON ARRIVAL, , DOOR JAMMED. FOUND DOOR HINGE BEARING TO FRAM, SEIZING. REPLD UPP ER & LOWER HINGE BEARINGS, OP CHECKED NORMAL.. . . . . .Apr 28, 2001 · Airbus A320211 · Passenger/Crew DoorsSDR 0101533208O-Ring · leakingDURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. PERFORMED COM PROCEDURES AND CONTINUED TO FINAL DESTINATION WITH A NORMAL LANDING. MAINTENANCE REPLACED O-RING AT ENGINE NR 2 PYLON CHECK VALVE. LEAK CHECK OK.Apr 28, 2001 · N308US · Airbus A320211 · Hydraulic System, MainSDR AU010385Radio · failed(AUS) VHF SYSTEM FAULTY.Apr 23, 2001 · Airbus A320211 · VHF Communications SystemSDR CA010510015Oven · smoke(CAN) ONE GALLEY UNIT STARTED SMOKING AFTER TAKEOFF. J CLASS OVEN 5877 TURNED OFF.FOUND FOOD SPILLED ON ELEMENT. OVEN CLEANED, FUNCTIONAL CHECK CARRIED OUT NIL FAULT.Apr 2, 2001 · Airbus A320211 · Buffet/GalleysSDR CA010510014Filter · contaminated(CAN) AFTER TAKEOFF, THE COCKPIT AND CABIN FILLED WITH STRONG FUMES. CREW REQUIRED OXYGEN TO OPERATE AIRCRAFT, LANDED WITHOUT ANY FURTHER INCIDENT. AIRCRAFT WAS DE-ICED 3 TIMES PRIOR FLIGHT, AIR CONDITION PACKS WERE ON WITH APU BLEED. MAINTENANCE ACTION: WITH Apr 2, 2001 · Airbus A320211 · Air Distribution SystemSDR 0101283206Fan · failedDURING DESCENT, AN ELECTRICAL BURNING ODOR WAS NOTICED IN THE COCKPIT FOLLOWED BY VENT BLOWER FAULT MESSAGE. COMPLIED WITH COM PROCEDURES, DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AVIONICS VENTILATION INLET BLOWER FAN AND Mar 31, 2001 · N306US · Airbus A320211 · Air Distribution FanSDR AU010289Bearing · spalled(AUS) NR 2 ENGINE NR 4 BEARING OUTER RACE SEVERELY SPALLED.Mar 12, 2001 · Airbus A320211 · Turbine SectionSDR 0100983203Hydraulic Line · leakingDURING CRUISE, RECEIVED HYD G RSVR LO LVL AND HYD G SYS LO PR MESSAGES. SELECTED THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP AND PTU OFF PER COM PROCEDURES. DURING APPROACH AT FINAL DESTINATION, SELECTED PTU ON RESTORING GREEN SYSTEM PRESSURE TO EXTEND LANDING GEAMar 12, 2001 · N303US · Airbus A320211 · Hydraulic System, MainSDR CA010430009Display · failed(CAN) SLAT ECAM (ELECTRONIC CENTRALIZED MONITORING SYSTEM)WARNING MESSAGE ON APPROACH. FLIGHT LANDED WITH NO SLATS WITH FLAP A THREE POSITION AS PER QRHI.RESET OF THE SYSTEM ON THE GROUND COMPLETED, SYSTEM FOUND SERVICEABLE.Mar 8, 2001 · Airbus A320211 · Leading Edge Slat Control SystemSDR CA010430008Engine · failed(CAN) RT ENGINE HAD A RUMBLE SOUND AND WAS THROWING FLAMES OUT THE EXHAUST. CREW REPORTED COMPRESSOR STALL.ENGINE REMOVED FOR INVESTIGATION. REPLACED ENGINE.Mar 7, 2001 · Airbus A320211 · Engine (Turbine/Turboprop)SDR 010093232Fitting · crackedDURING L-CHECK FOUND CRACK ON RIGHT HAND MAIN LANDING GEAR DOOR ACTUATOR FITTING. REPAIRED PER EA 32-181770.Feb 27, 2001 · N332NW · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR 0100733206Computer · malfunctionedSHORTLY AFTER LIFT-OFF, RECEIVED SMOKE AFT CARGO SMOKE MESSAGE. FOLLOWED ECAM AND COM PROCEDURES AND RETURNED TO DEPARTURE FIELD FOR NORMAL LANDING. MAINTENANCE REPLACED THE SPENT FIRE EXTINGUISHER BOTTLE AND THE FLIGHT WARNING COMPUTER. OPERATIONAL CHECK OFeb 23, 2001 · N306US · Airbus A320211 · Central ComputersSDR 0100523207Hydraulic Line · leakingDURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. FOLLOWED COM PROCEDURES, CONTINUED TO FINAL DESTINATION, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED HYDRAULIC LINE BETWEEN THE AUTO BRAKE SELECTOR AND PARK BRAKE VALVE. NO OTHER LEAK NOTED.Feb 16, 2001 · N307US · Airbus A320211 · Hydraulic System, MainSDR 0100383226Hydraulic System · lowFOLLOWING APPLICATION OF TAKEOFF POWER, RECEIVED HYD Y RSVR LO LVL MESSAGE. ABORTED TAKEOFF AT 60 KNOTS AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE SERVICED THE YELLOW HYDRAULIC SYSTEM BUT NO LEAKS WERE FOUND. OPERATIONAL CHECK OK.Feb 3, 2001 · N326US · Airbus A320211 · Hydraulic Power SystemSDR 0100393207B-Nut · looseDURING CRUISE, RECEIVED HYD Y RSVR LO LVL MESSAGE. FOLLOWED ECAM AND COM PROCEDURES. CONTINUED TO FINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE SECURED A LOOSE B-NUT AT THE YELLOW SYSTEM BRAKE ACCUMULATOR. SERVICED SYSTEM WITH NO OTHER LEAKS NFeb 1, 2001 · N307US · Airbus A320211 · Hydraulic System, MainSDR CA010301026Valve · failed(CAN) ON CLIMBOUT, NR 1 ENGINE ANTI-ICE FAULT INDICATED ON ECAM. VALVE REMAINED CLOSED. DUE TO ICING CONDITIONS FORECAST AT DESTINATION, ELECTED TO RETURN. REPLACED NR 1 ENGINE ANTI-ICE VALVE AS PER MM 30-21-51 PAGE 401.Jan 30, 2001 · Airbus A320211 · Air Intake Anti/De-Ice SystemSDR AU010065Fitting · cracked(AUS) RT MAIN LANDING GEAR DOOR ACTUATOR FITTING AND CONNECTING STRIP CRACKED IN TWO PLACES. CRACK LENGTHS 20MM (0.78IN) IN FORWARD FLANGE AND 28MM (1.102IN) IN AFT FLANGE. CONNECTION STRAP CRACKED FROM FASTENER HOLE. CRACK LENGTH 5MM (0.196IN). FOUND DURING NJan 23, 2001 · Airbus A320211 · Fuselage, Landing Gear Attach FittingsSDR 0100203220Fire Detector · malfunctionedDURING TAKEOFF AT ROTATION, RECEIVED A MOMENTARY NR 2 ENGINE FIRE WARNING. ALL ENGINE PARAMETERS WERE NORMAL. RETURNED TO DEPARTURE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES BUT REPLACED NR 1 FDU, CARD 5LP, ANDJan 23, 2001 · N320US · Airbus A320211 · Fire DetectionSDR 0100193220Computer · false indicationDURING TAKEOFF AT ROTATION, RECEIVED A MOMENTARY NR 2 ENGINE FIRE WARNING. ALL ENGINE PARAMETERS WERE NORMAL. RETURNED TO DEPARTURE FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED THE CFDIU AND NR 1 FWC NOT FUNCTIONING PROPERLY. REPJan 23, 2001 · N320US · Airbus A320211 · Fire DetectionSDR 0100113208Frame · corrodedDURING H-CHECK, FOUND CORROSION ON LT FRAME 68 SURROUNDING THE NUT PLATE HOLE AT FLOOR SILL AREA. REPAIRED PER EA 32-181432.Jan 10, 2001 · N308US · Airbus A320211 · Fuselage Main, FrameSDR CA010201002Windshield · failed(CAN) ON APPROACH, FIRST OFFICER WINDSHIELD SHATTERED.WINDSHIELD CHANGED.Jan 6, 2001 · Airbus A320211 · Flight Compartment WindowsSDR 0100023212Floorbeam · corrodedDURING "L" CHECK FOUND CORROSION ON FLOORBEAMS IN AFT GALLEY AREA AT Y765 AND Y1162.5/Y1292. REPAIRED PER EA 32-181716.Jan 5, 2001 · N312US · Airbus A320211 · Fuselage Main, Floor BeamSDR 0100093218Roller · out of adjUPON ARRIVAL AT THE GATE, THE GATE AGENT HAD DIFFICULTY PULLING DOOR 1L OPEN WITHOUT ASSISTANCE BY A FLIGHT ATTENDANT FROM THE AIRCRAFT INTERIOR. MAINTENANCE TROUBLESHOOTING REVEALED THE AFT UPPER DOOR ROLLER WAS NOT CLEARING THE CAM ON THE DOOR FRAME OPENINGJan 4, 2001 · N318US · Airbus A320211 · Passenger/Crew DoorsSDR AU001281Oxygen Mask · leaking(AUS) FIRST OFFICERS OXYGEN MASK LEAKING.Dec 29, 2000 · Airbus A320211 · Crew Oxygen SystemSDR AU001280Cable · damaged(AUS) ESCAPE SLIDE RESERVOIR ASSEMBLY WIRE CONTROL INTERNAL CABLE DAMAGED (KINKED) AT THE END AND AT THE ROD TO CABLE SWAGE. DAMAGE ALSO TO THE END FITTING. FOUND DURING TESTING IAW WR 25-60/119.Dec 28, 2000 · Airbus A320211 · Escape SlideSDR 0004673210Roller · out of adjUPON ARRIVAL AT THE GATE, THE GATE AGENT HAD DIFFICULTY PULLING DOOR 1L OPEN WITHOUT ASSISTANCE BY A FLIGHT ATTENDANT FROM THE AIRCRAFT INTERIOR. MAINTENANCE TROUBLESHOOTING REVEALED THE FORWARD UPPER DOOR ROLLER WAS NOT CLEARING THE CAM ON THE DOOR FRAME OPEDec 18, 2000 · N310NW · Airbus A320211 · Passenger/Crew DoorsSDR CA010105007Line · chafed(CAN) A/C RETURNED TO BASE WITH GREEN HYDRAULIC SYSTEM FLUID LOSS.FOUND SUPPLY LINE IN PYLON CHAFED. REPLACED LINE AND A/C RETURNED TO SERVICE.Dec 15, 2000 · Airbus A320211 · Hydraulic System, MainSDR CA010105008Apu · faulty(CAN) A/C 415, DEC 14/2000, FLT 3598, YEG, LOG SEQUENCE 0291486. ON TAKEOFF FROM YEG, AFT CARGO SMOKE ECAM MESSAGE APPEARED & A BURNING SMELL NOTICED IN CABIN & COCKPIT. EMERGENCY DECLARED & A/C RETURNED TO YEG. CFR DID A VISUAL INSP AFTER LDG, NO EVIDENCE OF Dec 14, 2000 · Airbus A320211 · Airborne Auxiliary Power Unit (APU) SystemSDR 0004583229Fitting/Strap · crackedAFTER TAKEOFF WHEN GEAR SELECTED UP, RECEIVED "L/G GEAR NOT UPLOCKED' ECAM MESSAGE. WITHIN 90 SECONDS OF SELECTING LANDING GEAR HANDLE UP, LANDING GEAR AND GEAR DOOR IN TRANSITION INDICATION LIGHTS AND ECAM WARNING EXTINGUISHED. FLIGHT CONTINUED TO PHX, SELECTDec 12, 2000 · N329NW · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR 0004493229Sensor, Prox · inoperativeAFTER TAKEOFF WHEN GEAR SELECTED UP, RECEIVED "L/G GEAR NOT UPLOCKED" AND "L/G DOOR NOT CLOSED" MESSAGES. CYCLED GEAR HANDLE TWICE WITH THE SAME RESULTS. DIVERTED TO PDX WITH NORMAL GEAR DOWN INDICATIONS AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THEDec 8, 2000 · N329NW · Airbus A320211 · Landing Gear Position and WarningSDR 0004413224Harness · abradedDURING CRUISE, RECEIVED ECAM MESSAGE "C/B TRIPPED ON OVHD PNL". CABIN EMERGENCY LIGHTS AT SEAT ROW 9 AND AFT ILLUMINATED. CIRCUIT BREAKER WAS LEFT OUT OF REMAINEDER OF THE FLIGHT. MAINTENANCE TROUBLESHOOTING REVEALED A BARE WIRE AT SEAT TRACK 9ABC. REPLACED THDec 3, 2000 · N324US · Airbus A320211 · Emergency LightingSDR CA001212014Sensor · out of adj(CAN) IN CRUISE AFT CARGO DOOR INDICATED OPEN ON ELECTRONIC CENTRALIZED AIRCRAFT MONITORING.NORMAL PRESSURIZATION AND NO VIBRATION. ADJUSTED DOOR PROXIMITY SENSOR 34WV, SYSTEM CHECKED NORMAL.Nov 15, 2000 · Airbus A320211 · Door Warning SystemSDR CA001201003Control Unit · failed(CAN) ON APPROACH, FLAPS 1 SELECTED AT 215 KNOTS, ECAM INDICATED SLAT LOCK. DECLARED AN EMERGENCY, LANDED WITH SLATS RETRACTED. MAINTENANCE TESTED BOTH SFCC,S NR 1 AND NR 2, TESTED OK. RESET WING TIP BRAKES, SYSTEM FUNCTION CHECKED SERVICEABLE.Oct 31, 2000 · Airbus A320211 · Leading Edge Slat Control SystemSDR CA001110008Sensor · failed(CAN) ON CLIMB OUT OF VANCOUVER, C2 CARGO DOOR WARNING MESSAGE APPEARED.AIRCRAFT RETURNED TO VANCOUVER. 32V PROXIMITY SENSOR REPLACED AND SYSTEM CHECKED NORMAL.Oct 21, 2000 · Airbus A320211 · Door Warning SystemSDR 0003803222Hose · rupturedDURING CLIMB AFTER LANDING GEAR AND FLAP RETRACITON, RECEIVED HYD G RSVR LO LVL MESSAGE. PER COM PROCEDURES, SHUT OFF THE GREEN HYDRAULIC SYSTEM PUMPS, GRAVITY EXTENDED LANDING GEAR ON APPROACH TO FINAL DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE REOct 15, 2000 · N322US · Airbus A320211 · Hydraulic System, MainSDR CA001110019Engine · making metal(CAN) ENGINE CREW ALERT SYSTEM MESSAGE NR 1 ENGINE FULL AUTHORITY DIGITAL ENGINE CONTROL LIGHT ON.ENGINE SHUT DOWN. FOUND METAL CONTAMINATION ON SCAVENGE OIL FILTER AND ON CHIP DETECTOR.ENGINE CHANGED. ADDITIONAL INFO WILL FOLLOW AFTER INVESTIGATION.Oct 10, 2000 · Airbus A320211 · Engine (Turbine/Turboprop)SDR CA001110017Servo · worn(CAN) STRONG AIRFRAME VIBRATION IN CRUISE AT 135 KTS, FL230, REDUCED SPEED, IT INITIALLY DISAPPEARED AT 280 KTS GOING THROUGH FL270. ON WALK AROUND FOUND LEFT HAND PACK EXHAUST DOOR FULLY OPENED, AND RIGHT HAND DOOR FULLY CLOSED. FOUND BLUE SYSTEM RUDDER SERVOOct 10, 2000 · Airbus A320211 · Elevator Control SystemSDR CA001129035Wire · faulty(CAN) ELECTRONIC CENTRALIZED AIRCRAFT MONITORING MESSAGE STROBE LIGHT OFF REGARDLESS OF THE SWITCH POSITION. FOUND STROBE LIGHT CIRCUIT BREAKER POPPED, UNABLE TO RESET. FURTHER INVESTIGATION REVEALED A MAJOR FAULT IN THE WIRING RUNNING ALONG THE REAR SPAR OF TOct 2, 2000 · Airbus A320211 · Light System WiringSDR CA001012006Axle · damaged(CAN) DURING TAXI, HEAVY VIBRATION DEVELOPED ABOVE 10 KNOTS, FELT SIMILAR TO A FLAT. FOUND NR 4 MAIN WHEEL LOOSE ON AXLE, UNABLE TO REMOVE MAIN WHEEL NUT ASSEMBLY. RETORQUED NUT FOR TOW PURPOSES TO HANGER. WHEEL AND BRAKE ASSEMBLY REMOVED, AXLE SLEEVE LOOSE ANSep 15, 2000 · Airbus A320211 · Main Landing Gear Strut/Axle/TruckSDR AU001064Stiffener · cracked(AUS) WING CENTRE SECTION VERTICAL STIFFENERS CRACKED IN HOLES. FOUND DURING INSPECTION IAW SB A320-57-1017.Sep 15, 2000 · Airbus A320211 · Wing Miscellaneous StructureSDR CA001019023Windshield · failed(CAN) CAPTAINS L-1 FORWARD WINDSHIELD SHATTERED IN FLIGHT. WINDSHIELD CHANGED.Sep 13, 2000 · Airbus A320211 · Flight Compartment WindowsSDR AU001176Frame · cracked(AUS) FUSELAGE FRAME 35 CRACKED IN AREA BETWEEN STRINGER NO30 AND STRINGER NO31.Sep 8, 2000 · Airbus A320211 · Fuselage Main, FrameSDR 0003323203Servo · leakingDURING DESCENT RECEIVED HYD G RSVR LO LVL MESSAGE. PER COM PROCEDURES TURNED OFF THE GREEN HYDRAULIC SYSTEM. GRAVITY EXTENDED THE LANDING GEAR AND LANDED WITHOUT INCIDENT. MAINTENANCE TOWED THE AIRCRAFT FROM THE RUNWAY TO THE GATE. THE HYDRAULIC SYSTEM WASSep 4, 2000 · N303US · Airbus A320211 · Hydraulic Reservoir, MainSDR CA001019021Window · cracked(CAN) AT TAKEOFF, CAPTAINS SLIDING WINDOW DEVELOPED A CRACK.WINDOW OUTER PANE SHATTERED.CHANGED WINDOW AND WINDOW HEAT COMPUTER (P/N 6664202-4).Sep 3, 2000 · Airbus A320211 · Flight Compartment WindowsSDR AU000733Skin · cracked(AUS) FUSELAGE SKIN CRACKED IN RIVET HOLES (16OFF). FOUND DURINGINSPECTION IAW SB A320-53-1031.Sep 1, 2000 · Airbus A320211 · Fuselage Main, Plate/SkinSDR AU000709Frame · cracked(AUS) FUSELAGE FRAME 53 CRACKED. CRACK LENGTH APPROXIMATELY 2MM (0.078IN). FOUND DURING ULTRASONIC INSPECTION IAW SBA320-52-1032.Sep 1, 2000 · Airbus A320211 · Fuselage Main, FrameSDR AU000708Frame · cracked(AUS) FUSELAGE FRAME CRACKED IN HOLES (2OFF) LOCATED BETWEEN FRAME 38 AND FRAME 41 AND STRINGER 12 AND STRINGER 21. FOUND DURING INSPECTION IAW AD/A320/89.Sep 1, 2000 · Airbus A320211 · Fuselage Main, FrameSDR AU000707Stringer · cracked(AUS) FRONT VERTICAL STRINGER CRACKED AT FRAME 36. FOUND DURING EDDY CURRENT INSPECTION IAW SB A320-57-1017.Sep 1, 2000 · Airbus A320211 · Fuselage Main, Longeron/Stringer
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