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.

SDR CA030106005Engine · surges(CAN) ENGINE NR 2 SURGED ON CLIMBOUT. ENGINE SHUT DOWN AND AIRCRAFT RETURNED TO DEPARTURE STATION. BLADE DAMAGE FOUND ON SUBSEQUENT BOROSCOPE CHECK. NR 2 ENGINE REPLACED AS PER AMM.Jan 1, 2003 · Airbus A320211 · Turbine Engine Compressor SectionSDR CA021211004Lock Plate · corroded(CAN) DURING ACCOMPLISHMENT OF AN H02 CHECK. FOUND THAT THE LT AFT LOCKING PLATE FOR THE LT WING TIP FENCE AND THE AFT ATTACH HARDWARE(2) BOLTS WERE FOUND BADLY CORRODED. THERE WAS NO CORROSION INDICATION AT THE LT FWD ATTACHMENT AND THE AFT THAT SHOWS EXTREMDec 3, 2002 · Airbus A320211 · Wing Main, Frame StructureSDR AUS20021334Hose · fractured(AUS) STANDBY ALTIMETER STATIC PRESSURE HOSE KINKED AND FRACTURED. PERSONNEL/MAINTENANCE ERROR.Nov 20, 2002 · Airbus A320211 · Altimeter, Barometric/EncoderSDR CA021115012Actuator · failed(CAN) ON APPROACH YVR WHEN FLAP SELECTED 'F/CTL SLAT FAULT' MASSAGE APPEARING AND SLATS FAILED TO OPERATE.LT NR 2 SLAT ACTUATOR TORQUE LIMITER INDICATOR FOUND POPPED. R/H OUTBD. SLAT ACTUATOR 6029 CM REPLACED AS PER AMM 27-84-49 AND SLAT FUNCTION CHECKED SERVINov 14, 2002 · Airbus A320211 · Leading Edge Slat ActuatorSDR 0203843220Seat Track · corrodedDuring "M"check found corrosion on seat track at BS 1292 on frame 54 plus 20" and frame 52 plus 14". Repaired per EA32-192349.Nov 7, 2002 · N320US · Airbus A320211 · Fuselage, Seat/Cargo Attach FittingsSDR 0203823220Skin · corrodedDuring "M" check found corrosion on fuselage skin at frame 65 between Stringers 30R and 31R. Repaired per EA 32-191301.Nov 7, 2002 · N320US · Airbus A320211 · Fuselage Main, Plate/SkinSDR CA021108006Washer · mismanufactured(CAN) ANTI-ROTATION WASHER SHOWN IN IPC 57-26-13 FIG 01B ITEM 60 IS NOT MANUFACTURED INACCORDANCE WITH DRAWING. SHARP EDGE CUTOUT ON WASHER INTERFERES WITH RADIUS LUG ON FITTING-PREVENTS WASHER FROM LAYING FLAT ON THE ACTUATOR FITTING-PREVENTS BEARING FROM BENov 1, 2002 · Airbus A320211 · Wing, Control Surface Attach FittingsSDR 0203623209Engine · failedDURING CRUISE FLIGHT, ENGINE NR 1 FLAMED OUT. FLIGHT CREW DIVERTED AIRCRAFT AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND THE ALTERNATOR/STATOR (PMA) DAMAGED AND METAL ON THE GEARBOX CHIP DETECTOR. ENGINE NR 1 REPLACED.Oct 30, 2002 · N309US · Airbus A320211 · Engine (Turbine/Turboprop)SDR CA021021007Computer · arced(CAN) WINDOW CRACKED, HEAT CIRCUIT BREAKER PULLED, WINDOW CHANGED, SUSPECT HEAT CONTROL COMPUTER WINDOW CHANGED AND COMPUTER. ARCING OCCURED FIRST THEN CIRCUIT BREAKER PULLED, THAT'S WHEN THE WINDOW CRACKEDOct 18, 2002 · Airbus A320211 · Windshield/Door Rain/Ice RemovalSDR CA021016022Lock · failed(CAN) DURING DEPLOY TEST OF WING SLIDE ENCLOSURE LT DOOR FAILED TO RELEASE CENTER LOCK. DOOR PARTIALLY OPENED AND TORE CENTER LOCK OFF DOOR AND THEN FULLY DEPLOYED. SLIDE AND ENCLOSURE REPLACED.Oct 9, 2002 · Airbus A320211 · Escape SlideSDR CA021008002Valve · failed(CAN) AFTER T/O LANDING GEAR LEVER TOOK 2-3 ATTEMPS TO MOVE FROM DOWN TO UP.AS PER T.S.M. SAFTY VALVE 49GA FAILED TEST. REPLACED AIRSPEED INTERLOCK VALVE PER AMM 32-31-17 AND OPERATIONAL CHECK CARRIED OUT. PASSED.Oct 5, 2002 · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR CA020927006Acm · overheated(CAN) BURNING ODOR REPORTED IN CABIN. NR 2 PACK FOUND OVERHEATED. NR 2 AIR CYCLE MACHINE REPLACED AS PER AMM.Sep 22, 2002 · Airbus A320211 · Cabin Cooling SystemSDR CA020918005Actuator · failed(CAN) YELLOW HYDRAULIC SYSTEM LOST FLUID AND CABIN FILLED WITH SMOKE. YELLOW SYSTEM YAW DAMPER ACTUATOR FOUND LEAKING. YAW DAMPER CHANGED AS PER AMM. YAW DAMPER OPERATION CHECK CARRIED OUT AS PER AMM.Sep 16, 2002 · Airbus A320211 · Hydraulic System, MainSDR 0202973221Engine · making metalDURING CRUISE FLIGHT, THE NR 2 ENGINE COMPRESSOR STALLED AND FLAMED OUT. NO RELIGHT WAS ATTEMPTED. FLIGHT CREW DIVERTED TO LAS AND PERFORMED AN UNEVENTFUL LANDING. MAINTENANCE FOUND METAL IN THE TAILPIPE. REPLACED THE NR 2 ENGINE.Sep 16, 2002 · N321US · Airbus A320211 · Engine (Turbine/Turboprop)SDR CA020918003Metering Valve · failed(CAN) AFTER LANDING AND JUST TURNING OFF RUNWAY, UNABLE TO STEER AIRCRAFT USING RUDDER PEDDLES OR TILLER. HYDRAULIC PRESSURE NORMAL. SELECTING RESERVE BRAKE AND STEERING ALSO NO HELP. AIRCRAFT TOWED TO GATE. REPLACED NLG STEERING METERING VALVE AS PER AMM Sep 15, 2002 · Airbus A320211 · Steering UnitSDR CA020826006Control Unit · failed(CAN) LDG LGCIU 2 FAULT AFTER GEAR SELECTED UP AND DOORS CLOSED (APPROX 1000 AGL0. TWO LOUD THUMPS HEARED AND FELT ON COCKPIT FLOOR. ECAM CARRIED OUT MESSAGE CLEARED AND LATER RETURNED. CHANGED NR 2 LGCIU PER AMM.Aug 20, 2002 · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR 0202673214Light · defectiveEN ROUTE TO SPOKANE, THE LEAD FLIGHT ATTENDANT NOTICED AN ELECTRICAL ODOR FROM THE AREA OF ROW 10DEF. FLIGHT CONTINUED AND LANDED WITHOUT INCIDENT. RELAMPED AND INSPECTED AREA. NO ODOR PRESENT.Aug 12, 2002 · N314US · Airbus A320211 · Passenger Compartment LightingSDR CA020801006Control Unit · failed(CAN) DURING CRUISE NR 1 ENGINE FADEC A FAULT, FADEC B FAULT. ENGINE CONTINUED TO OPERATE NORMAL EXCEPT IN DESCENT NR 1 ENGINE HAD MOMENTARILY SMALL EXCURSIONS TOWARD IDLE (APROX 21. N1 DROP) AND IDLE WOULD ANNUNCIATE EVEN WHEN IDLE NOT REQUIRED. REPLACE ECU Jul 24, 2002 · Airbus A320211 · Engine ControlsSDR CA020801002Servo · failed(CAN) WHILE DOING OPEN PROCEDURES CALLED FOR MEL 27-93-01 A RB ELEVATOR SERVO FAILED. AIRCRAFT REMOVED FROM SERVICE FOR SERVO CHANGE. REPLACED RT BLUE ELEVATOR SERVO CONTROL AS PER AMM 27-34-51-400. OPERATION CHECKED SERVICEABLE.Jul 15, 2002 · Airbus A320211 · Elevator Control SystemSDR CA020731010Uplock · failed(CAN) LT MLG DOOR NOT CLOSING ON GEAR EXTENSION 200 KTS. GO AROUND AND RE-CYCLED . NO JOY, DOOR NOT CLOSING. LT MLG DOOR UPLOCK ASSY. CHANGED AS PER AMM TASK 21-31-33-400-002.Jul 3, 2002 · Airbus A320211 · Landing Gear Position and WarningSDR USA2002F00058Computer · failedAFTER TAKEOFF, CAPTAIN DETECTED SMOKE IN THE COCKPIT ALONG WITH AN ECAM MESSAGE OF (AVNCS SMOKE). THE FLIGHT RETURNED TO AIRPORT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE AVIONICS EQUIPEMENT VENTILATION COMPUTER DUE TO A FAILED BITE CHECKJun 25, 2002 · N188US · Airbus A320211 · Cabin Cooling SystemSDR CA020731008Oven · overheated(CAN) OVEN NR 1 IN Y CLASS GALLEY, OVERHEATED AND SPARKED THEN STARTED SMOKING.C/B PULLED AND 2 SHOTS OF HALON FIRED IN IT. OVEN COOLED DOWN AND REMAINED DEACTIVATED FOR REMANDER OF FLIGHT. OVEN REPLACED ,WIRING AND CONNECTOR INSPECTED FOR DAMAGE. NO FAULTS FJun 23, 2002 · Airbus A320211 · Buffet/GalleysSDR 0202093215Acm · seizedFLIGHT ATTENDANT REPORTED SMOKE IN AFT CABIN. CAPTAIN NOTICED LIGHT SMOKE IN THE COCKPIT. SMOKE CLEARED WITHIN A FEW MINUTES. AFTER LANDING, RECEIVED PACK 1 OVERHEAT WARNING. FOUND NR 1 AIR CYCLE MACHINE SEIZED. REPLACED THE NR 1 AIR CYCLE MACHINE. LEAK Jun 23, 2002 · N315US · Airbus A320211 · Cabin Cooling SystemSDR CA020530007Seal · failed(CAN) GREEN HYDRAULIC FLUID LEVEL FELL IN YELLOW RANGE. AIRCRAFT DIVERTED TO YYZ RESULTING IN AN OVERWEIGHT LANDING. SEAL FOUND LEAKING ON LANDING GEAR DOOR MANIFOLD ASSY. SEAL REPLACED AND SYSTEM LEAK CHECKED SERVICEABLE. OVERWEIGHT LANDING CHECK COMPLETED, May 27, 2002 · Airbus A320211 · Hydraulic System, MainSDR 0201433224Module · faultyCAPTAIN'S AIRSPEED INDICATION WAS AT 40 KNOTS WHEN THE FIRST OFFICER'S WAS 80 KNOTS. ABORTED TAKEOFF AT 105 KNOTS AND TAXIED TO GATE. CLEARED CAPTAIN'S PITOT LINE. REPLACED NR 1 PITOT PROBE, LEFT AIR DATA MODULE, AND NR 1 AIR DATA INERTIAL REFERENCE UNIT. May 5, 2002 · N324US · Airbus A320211 · Inertial Guidance SystemSDR 0201423204Module · faultyDURING TAKEOFF ROLL, THE FIRST OFFICER'S AIRSPEED INDICATION NEVER EXCEEDED 45 KNOTS. ABORTED TAKEOFF AT 105 KNOTS. REPLACED THE LEFT NR 1 AIR DATA MODULE AND NR 2 AIR DATA INERTIAL REFERENCE UNIT. LEAK AND FUNCTIONAL CHECK OF ALTITUDE, AIRSPEED AND AIR DATMay 4, 2002 · N304US · Airbus A320211 · Inertial Guidance SystemSDR CA020507002Fitting · cracked(CAN) CARGO DOOR HANDLE FITTINGS FOUND CRACKED IN RADIUS BELOW THE BUSHING HOUSING. FOUND ON MORE THAN ONE DOOR.AC TIME 35,253HRS, FITTINGS REPLACED. IPC REF 52-32-21 FIG 3 ITEM 140May 3, 2002 · Airbus A320211 · Cargo/Baggage DoorsSDR CA020527008Electrical Box · overheated(CAN) DURING LEVEL FLIGHT AN ELECTRICAL BURNING ODOUR (ACRID SMELL) CAME FROM SEAT ROW 1-3 LEFT.AIRCRAFT DIVERTED AS A PRECAUTION. COMPLETE INSPECTION OF ROW 1-5 LEFT CARRIED OUT WITH NO OBVIOUS FAULTS WITH WIRING. SEB (SEAT ELECTRONIC BOX) FOR SEATS 2ABC FOUApr 19, 2002 · Airbus A320211 · Passenger Compartment EquipmentSDR 0200853217Frame · corrodedDuring "M" check found corrosion on frame 68 above door sill. Repaired per EA 32-18934.Mar 22, 2002 · N317US · Airbus A320211 · Fuselage Main, FrameSDR CA020328002Fitting · failed(CAN) PLAY AT TRIMMABLE HORIZONTAL STABILIZER (THS) REAR ATTACH FITTINGS. THS REAR ATTTACH FITTINGS HAVE PLAY BETWEEN BUSHINGS AND THS LT AND RT AFT ATTACH FITTING BORES.Mar 15, 2002 · Airbus A320211 · Stabilizer ActuatorSDR CA020328003Power Unit · failed(CAN) IN CRUISE AFTER APPROXIMATELY 1.5 HOURS IN FLIGHT, YELLOW HYDRAULIC FLUID LEVEL WENT LOW LEVEL. AIRCRAFT DIVERTED AND LANDED IN WINNIPEG. POWER TRANSFER UNIT (PTU) REPLACED. OPERATION CHECKED SERVICEABLE AS PER AIRCRAFT MAINTENANCE MANUAL REFERENCE 29-Mar 9, 2002 · Airbus A320211 · Hydraulic System, MainSDR CA020315004Line · leaking(CAN) AIRCRAFT HAD A COMPLETE LOSS OF GREEN HYDRAULIC SYSTEM FLUID AND PRESSURE IN FLIGHT OVER WASHINGTON STATE. FLIGHT DIVERTED TO VANCOUVER. PTU GREEN PRESSURE FLEX LINE FOUND LEAKING. FLEX LINE REPLACED AND SYSTEM LEAK CHECKED SERVICEABLE.Feb 25, 2002 · Airbus A320211 · Hydraulic System, MainSDR CA020308007Panel · cracked(CAN) VERTICAL STAB LEADING EDGE PANEL 322AL AND 322BL CRACKED. PANEL 322AL APPEARS CRACKED ON BOTH LT AND RT SIDES APROX 4 INCHES BELOW UPPER EDGE. ALSO APPROX. 4 INCHES UP FROM LOWER EDGE ON LT SIDE APPEARS TO BE A THIRD CRACK. 322BL APPEARS TOBE DELAMINATEDFeb 25, 2002 · Airbus A320211 · Vertical Stabilizer, Plate/SkinSDR CA020308009Engine · faulty(CAN) BIRD INGESTION/STRIKE ON #2 ENGINE AT TOUCHDOWN.NORMAL REVERSE USED. NO ABNORMAL ENGINE INDICATIONS IN COCKPIT. BIRD STRIKE INSPECTION CARRIED OUT NIL FAULTS FOUND.ENGINE RUN COMPLETE NIL FAULTS FOUND. THRUST REVERSER OPERATION CHECK COMPLETED NIL FAULTSFeb 17, 2002 · Airbus A320211 · Engine (Turbine/Turboprop)SDR CA020228004Fitting · failed(CAN) LT AND RT THS REAR ATTACH BEARING FOUND LOOSE IN REAR YOKE FITTINGS.BORES IN THE THS LT AND RT REAR SUPPORT FITTING FOUND BEYOND PRODUCTION TOLERANCES. BUSHINGS WILL BE NICKEL PLATED TO RETURN OD DIAMETER. THIS CONSIDERED A PERMANENT FIX FOR THE RT FITFeb 12, 2002 · Airbus A320211 · Stabilizer Control SystemSDR CA020228003Panel · cracked(CAN) VERTICAL STAB LEADING EDGE PANELS 322AL, 322CL AND 322BL CRACKED. PANEL 322AL CRACKED APPROXIMATELY 4 INCHES FROM LOWER EDGE LT SIDE. PANEL 322CL CRACKED APPROXIMATELY 4 INCHES FROM LOWER EDGE LT SIDE. ALSO 322BL. PRODUCTION PERMIT RAISED FOR REPAIR IF BFeb 12, 2002 · Airbus A320211 · Vertical StabilizerSDR CA020215005Structure · cracked(CAN) VERTICAL STAB LEADING EDGE PANEL 322B1 CRACKED APPROXIMATELY 5 INCHES UP FROM LOWER EDGE. LT SIDE. THE DAMAGE IS WITHIN REPAIR LIMITS WILL BE REPAIRED AS PER SRM 55-30-00, PA 200, OR REPLACED.Jan 29, 2002 · Airbus A320211 · Vertical Stabilizer, Plate/SkinSDR CA020201024Uplock · failed(CAN) CLIMBING THROUGH 16,000 FT AT 265 KTS ECAM L/G DOOR OPEN. SLOWED TO 215 KTS. GEARS RECYCLED AS PER MAINTENANCE REQUEST, NO CHANGE. AMBER DOOR LIGHT INDICATION REMAINS ON UNTIL GEAR SELECTED DOWN. AIRCRAFT RETURNED TO TORONTO. LT MAIN LANDING GEAR DOOR UPJan 24, 2002 · Airbus A320211 · Landing Gear Door Retract SectionSDR CA020201023Selector Valve · failed(CAN) ON FINAL APPROACH TO VANCOUVER AT 1600 AGL "L/G NOT DOWNLOCKED" WARNING CAME ON. GEARS CYCLED. ALL EXTENDED NORMALLY THE SECOND TIME. THE GEAR AT FAULT WAS THE RT MAIN. MAIN LANDING GEAR SELECTOR VALVE REPLACED AS PER AMM TASK 32-31-12-400-001, LEAK Jan 23, 2002 · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR CA020201015Smoke Detector · failed(CAN) AFTER TAKEOFF, AVIONIC VENT SMOKE MESSAGE, NO APPARENT OF SMOKE OR SMELL. RAT DEPLOYED. SMOKE INDICATION DISAPPEARED BEFORE LANDING. FLIGHT RETURNED TO FORT LADERDALE. AVIOINIC COMPARTMENT INSPECTED FOR EVIDENCE OF SMOKE, BLOWN DUCTS OR OVERHEATED EQUJan 19, 2002 · Airbus A320211 · Smoke DetectionSDR 0200063215Fitting · corrodedDuring "M" check found corrosion in three holes of inner rear spar anchorage fitting. Repaired per EA 32-184839.Jan 9, 2002 · N315US · Airbus A320211 · Wing, Attach FittingsSDR CA020121006Sensor · contaminated(CAN) AIR TURN BACK TO MONTREAL DUE TO MAIN LANDING DOOR NOT SHOWING PROPERLY LATCHED. AFTER VERIFICATION, FOUND TO BE THE SENSORS CONTAMINATED WITH GREASE AFTER AN OVERNIGHT CHECK (OVERGREASED).SENSORS CLEANED, GEAR SWING COMPLETED, SYSTEMM FOUND SERVICEABJan 2, 2002 · Airbus A320211 · Landing Gear Position and WarningSDR CA020110003Idg · overheated(CAN) @1 IDG OIL PRESSURE AND OVERHEAT ON ON DESCENT TO YVR. TEMPERATURE GRADUALLY RISING (PULSATING GREEN) ECAM ACTION CARRIED OUT. IDG DISCONNECTED PRIOR LANDING.IDG FOUND OVERSERVICED. MEL 24-20-01 APPLIED. OIL STILL FLUCTUATING.IDG REPLACED AS PER AMM 24-2Dec 23, 2001 · Airbus A320211 · AC Generation SystemSDR CA011121020Control Column · failed(CAN) AFTER TAKEOFF CREW REPORTED ELAC FLT NR 1 MSG.AIRCRAFT RETURNED TO TORONTO. CAPT. SIDE STICK REPLACED. OPERATIONAL TEST PERFORMED AS PER AMM 27-02-41-710-001. AIRCRAFT SERVICEABLE.Nov 3, 2001 · Airbus A320211 · Control Column SectionSDR CA011114005Uplock · overserviced(CAN) AFTER TAKEOFF, THE "LANDING GEAR NOT UPLOCKED" MESSAGE CAME ON ECAM. GEARS RECYCLED AS PER AOM. NO JOY. AIRCRAFT RETURNED TO WINNIPEG.LARGE AMOUNT OF GREASE REMOVED FROM MLG UPLOCK 8GA 10GA R/H AS PER CANADIAN TECHNICAL INFORMATION BULLETIN NO.32-1-98-6 Oct 27, 2001 · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR CA010910005Computer · failed(CAN) REPEAT FLAP FAIL MESSAGE WHEN FLAP 2 SELECTED, CREW ELECTED TO GO AROUND AND CARRY OUT QRH PROCEDURES. AIRCRAFT LANDED IN CALGARY SAFELY WITHOUT FURTHER INCIDENT.FLAPS RECYCLED BACK TO CLEAR CONFIGURATION FLAP MESSAGES, SYSTEM RETURNED TO NORMAL. CYCLED Aug 20, 2001 · Airbus A320211 · Leading Edge Slat Control SystemSDR CA010906018Actuator · failed(CAN) IN ROUTE TO MIAMI THE AIRCRAFT EXPERIENCED AN UNCOMMANDED YAW, SEVERAL ATTEMPTS FROM THE CREW TO ISOLATE THE PROBLEM FAILED, THE AIRCRAFT DIVERTD TO RALEIGH FOR REPAIR. FOUND TO BE THE YAW DAMPER ACTUATOR, ALSO AS A PRECAUTION THEY CHANGED BOTH (FAC)Aug 8, 2001 · Airbus A320211 · Rudder ActuatorSDR CA010906020Actuator · failed(CAN) COMPRESSOR STALL 25 MINUTES BEFORE LANDING IN TORONTO, AIRCRAFT DECLARED AN EMERGENCY LANDING, THE CREW RE-STARTED THE ENGINE AND LANDED SAFELY WITH NO INCIDENT. AIRCRAFT REMOVED FROM SERVICE FOR TROUBLESHOOTING AND RECTIFICATION.FOUND TO BE THE VARIABLEAug 7, 2001 · Airbus A320211 · Turbine Engine Compressor SectionSDR USAASA01039Power Supply · dischargedPHL - THE EMERGENCY LIGHT SYSTEM WILL NOT TEST. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT. (M)Jul 31, 2001 · N174US · Airbus A320211 · Emergency LightingSDR CA010906017Bolt · loose(CAN) DURING H-CHECK AND ACCOMPLISHING AIRCRAFT MAINTENANCE MANUAL TASK 53-51-00-210-009 FOUND THREE BOLTS LOOSE AS WELL AS CORRODED NUT FOR THE TAIL CONE ATTACHMENT.BOLTS RETORQUED AND NUTS REPLACED.Jul 19, 2001 · Airbus A320211 · Vertical Stabilizer
Back to Airbus A320-211