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 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.SDR 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 LASDR 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.. . . . . .SDR 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.SDR AU010385Radio · failed(AUS) VHF SYSTEM FAULTY.SDR 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.SDR 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 SDR 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 SDR AU010289Bearing · spalled(AUS) NR 2 ENGINE NR 4 BEARING OUTER RACE SEVERELY SPALLED.SDR 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 GEASDR 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.SDR 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.SDR 010093232Fitting · crackedDURING L-CHECK FOUND CRACK ON RIGHT HAND MAIN LANDING GEAR DOOR ACTUATOR FITTING. REPAIRED PER EA 32-181770.SDR 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 OSDR 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.SDR 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.SDR 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 NSDR 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.SDR 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 NSDR 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, ANDSDR 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. REPSDR 0100113208Frame · corrodedDURING H-CHECK, FOUND CORROSION ON LT FRAME 68 SURROUNDING THE NUT PLATE HOLE AT FLOOR SILL AREA. REPAIRED PER EA 32-181432.SDR CA010201002Windshield · failed(CAN) ON APPROACH, FIRST OFFICER WINDSHIELD SHATTERED.WINDSHIELD CHANGED.SDR 0100023212Floorbeam · corrodedDURING "L" CHECK FOUND CORROSION ON FLOORBEAMS IN AFT GALLEY AREA AT Y765 AND Y1162.5/Y1292. REPAIRED PER EA 32-181716.SDR 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 OPENINGSDR AU001281Oxygen Mask · leaking(AUS) FIRST OFFICERS OXYGEN MASK LEAKING.SDR 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.SDR 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 OPESDR 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.SDR 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 SDR 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, SELECTSDR 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 THESDR 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 THSDR 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.SDR 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.SDR 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.SDR 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 RESDR 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.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 SERVOSDR 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 TSDR 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 ANSDR AU001064Stiffener · cracked(AUS) WING CENTRE SECTION VERTICAL STIFFENERS CRACKED IN HOLES. FOUND DURING INSPECTION IAW SB A320-57-1017.SDR CA001019023Windshield · failed(CAN) CAPTAINS L-1 FORWARD WINDSHIELD SHATTERED IN FLIGHT. WINDSHIELD CHANGED.SDR AU001176Frame · cracked(AUS) FUSELAGE FRAME 35 CRACKED IN AREA BETWEEN STRINGER NO30 AND STRINGER NO31.SDR 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 WASSDR 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).SDR AU000733Skin · cracked(AUS) FUSELAGE SKIN CRACKED IN RIVET HOLES (16OFF). FOUND DURINGINSPECTION IAW SB A320-53-1031.SDR AU000709Frame · cracked(AUS) FUSELAGE FRAME 53 CRACKED. CRACK LENGTH APPROXIMATELY 2MM (0.078IN). FOUND DURING ULTRASONIC INSPECTION IAW SBA320-52-1032.SDR 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.SDR AU000707Stringer · cracked(AUS) FRONT VERTICAL STRINGER CRACKED AT FRAME 36. FOUND DURING EDDY CURRENT INSPECTION IAW SB A320-57-1017.
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