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 9517923215Idg · failedDURING CLIMBOUT, RECEIVED NR 2 ENGINE IDG FAULT ACCOMPANIED WITH THE GENERATOR DROPPING OFF LINE. CREW DISCONNECTED NR 2 IDG PER COCKPIT OPERATING MANUAL PROCEDURE. DUE TO THE APU PREVIOUSLY ON MEL, RETURNED TO SEA AND LANDED WITHOUT INCIDENT. MAINTENANCE RNov 12, 1995 · N315US · Airbus A320211 · Alternator-Generator DriveSDR 9519383211Sill · corrodedDURING IL CHECK, FOUND CORROSION ON THE DOOR 2R LOWER SILL. REPAIRED SILL (P/N D534-80043-205), PER EA 32-104299.Nov 10, 1995 · N311US · Airbus A320211 · Fuselage Miscellaneous StructureSDR 9518623211Sill · corrodedDURING IL CHECK, FOUND CORROSION IN BOTH THE LEFT AND RIGHT AFT SERVICE DOOR LOWER SILLS. REPAIRED SILLS (P/N D534-80043-204, -205), PER EA 32-104298, -104291 RESPECTIVELY.Nov 9, 1995 · N311US · Airbus A320211 · Fuselage Miscellaneous StructureSDR 9517913222Battery Pack · dischargedDURING LINE MAINTENANCE, THE EMERGENCY LIGHTS BATTERY TEST FAILED EMER L AND EMER R POSITIONS. REPLACED THE BATTERY PACKS AT FORWARD LEFT AND MIDDLE LEFT POSITIONS. OPERATIONAL CHECK OK.Nov 9, 1995 · N322US · Airbus A320211 · Emergency LightingSDR CA960103512Sensor · inoperative(CAN)ECAM MESSAGE, "FLAPS LOCKED", FLAPLESS LANDING CARRIED OUT. MAINTENANCE ACTION INVOLVED REPLACING FLAP SELECTOR SENSOR AND RIGHT INBOARD FLAP ACTUATOR P/N 791A000003. FLAP SYSTEM FUNCTIONALLY CHECKED.Nov 8, 1995 · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9517503225Battery Pack · dischargedDURING LINE MAINTENANCE CHECK, THE EMERGENCY LIGHTS TEST FAULTED LEFT. REPLACED THE BATTERY PACK (13WL). OPERATIONAL CHECK OK.Nov 6, 1995 · N325US · Airbus A320211 · Emergency LightingSDR CA960103509Torque Limiters · tripped(CAN)FLIGHT CONTROL PAGE "FLAPS FAULT" INDICATION. PERFORMED ECAM, NO CHANGE, FLAPS LOCKED AT ZERO. MAINTENANCE CHECK FOUND LEFT INBOARD FLAP INBOARD ACTUATOR & LEFT OUTBOARD FLAP OUTBOARD ACTUATOR TORQUE LIMITERS TRIPPED. FLAP TORQUE LIMITERS RESET AND FLAPSNov 5, 1995 · Airbus A320211 · Trailing Edge Flap Control SystemSDR CA960103508Wing Tip Brake · req reset(CAN)ON APPROACH FLIGHT CONTROL PAGE "FLAPS FAULT" INDICATION, FLAPS RECYCLED, NO CHANGE. FLAPLESS LANDING CARRIED OUT. MAINTENANCE ACTION INVOLVED RESETTING WING TIP BRAKE ON S.F.C.C. #1 & #2. OPERATIONALCHECK CARRIED OUT.Nov 4, 1995 · Airbus A320211 · Trailing Edge Flap Control SystemSDR CA960103506Gearbox · water ingress(CAN)ON APPROACH, FLIGHT CONTROL PAGE "FLAPS FAULT" INDICATION. FLAPS RECYCLED, NO CHANGE. FLAPLESS LANDING CARRIED OUT. MAINTENANCE ACTION INVOLVED CHECKING FLAP SYSTEM, REMOVING PLUGS ON EACH ACTUATOR & GEAR BOX. WATER WAS FOUND PRESENT ON EACH GEARBOX 6259Nov 4, 1995 · Airbus A320211 · Trailing Edge Flap ActuatorSDR CA960103505Lgcu · failed(CAN)ON CLIMB OUT THROUGH 15,000 FEET ALL 3 LANDING GEAR DOORS BECAME UNLOCKED. SPEED REDUCED TO 240 KNOTS AND AIRCRAFT RETURNED TO BASE. MAINTENANCE ACTION INVOLVED CHANGING L.G.C.I.U. #1 & #2 (LANDING GE AR CONTROL INTERFACE UNIT).Nov 4, 1995 · Airbus A320211 · Landing Gear Retraction/Extension SystemSDR CA951114003Stop Vbv · seized(CAN)ON CLIMB AT APPROXIMATELY 1500 FEET THE #1 EGT WAS OBSERVED TO BE IN THE CAUTION RANGE. THE POWER WAS REDUCED MANUALLY ON MAINTENANCE INPUT THEN TRIED AGAIN WITH ANTI-ICE ON, THEN WITH #1 ENGINE BLEEDAIR OFF, PROBLEM REMAINED. SUBSEQUENT MAINTENANCE ACTIONov 4, 1995 · Airbus A320211 · Engine Bleed Air SystemSDR 9517353239Target · looseDEN - DURING CLIMBOUT, THE LEFT MAIN LANDING GEAR DOOR INDICATED IN TRANSIT AFTER LANDING GEAR WAS RETRACTED. CYCLED LANDING GEAR HANDLE AND ALL INDICATIONS WERE NORMAL. AIRCRAFT CONTINUED TO DTW WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE FOUNov 1, 1995 · N339NW · Airbus A320211 · Landing Gear Position and WarningSDR 9517203234Ecu · malfunctionedDURING DESCENT AT 33,000 FEET, NR 2 ENGINE OVERSPEED OCCURRED. AUTO THROTTLE WAS DISENGAGED, POWER LEVER WAS PULLED BACK, AND ENGINE RPM CONTINUED TO ACCELERATE. ENGINE WAS MANUALLY SHUTDOWN. AIRCRAFT DIVERTED TO PHL AND LANDED WITHOUT FURTHER INCIDENT. MANov 1, 1995 · N334NW · Airbus A320211 · Fuel Control/Turbine EnginesSDR 9517183239Door Indication · malfunctionedDURING APPROACH INTO BWI, THE LEFT MAIN LANDING GEAR DOOR DID NOT INDICATE LOCKED AFTER GEAR EXTENSION. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, CYCLED LANDING GEAR AND ACCOMPLISHED A GO-AROUND. ALL INDICATIONS WERE NORMAL AND THE AIRCRAFT LANDED WITHOUNov 1, 1995 · N339NW · Airbus A320211 · Landing Gear Position and WarningSDR 9517173239Prox Sensor · malfunctionedDURING APPROACH INTO DTW, THE LEFT MAIN LANDING GEAR DOOR DID NOT INDICATE LOCKED AFTER LANDING GEAR EXTENSION. PERFORMED COCKPIT OPERATING MANUAL PROCEDURES AND CYCLED LANDING GEAR. ALL INDICATIONS NORMAL AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANNov 1, 1995 · N339NW · Airbus A320211 · Landing Gear Position and WarningSDR 9516543230Iru · failedSHORTLY AFTER LEVEL OFF AT FL 310, AIRCRAFT WENT INTO ALTERNATE YAW. AIRCRAFT RETURNED TO MSP WHERE AN EMERGENCY WAS DECLARED AND AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE NR 1 AIR DATA IRU AND NR 2 SPOILER ELEVATOR COMPUTER, OPERATIONOct 23, 1995 · N330NW · Airbus A320211 · Inertial Guidance SystemSDR CA951129520Heat Exchanger · strong odor(CAN)A VERY NOTICEABLE SMOKE ODOR WAS DETECTED AFTER TAKEOFF. AIRCRAFT RETURNED TO BASE. INVESTIGATION REVEALED PACK #1 PRIMARY HEAT EXCHANGER REPLACED PRIOR TO FLIGHT. SUSPECT PAINT OR SEALANT EMITTING ODOR WHEN FIRST HEATED. BOTH PACKS OPERATED, NO ODOR DETEOct 19, 1995 · Airbus A320211 · Heating SystemSDR 9516173202Pack · overheatedDURING CRUISE, THE RIGHT PACK OVERHEATED FOLLOWED BY SMOKE AFT CARGO SMOKE WARNING, FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES. THE WARNING INDICATION EXTINGUISHED APPROXIMATELY FIVE MINUTES AFTER THE FIRE BOTTLE WAS DISCHARGED. AIRCRAFT DIVERTED TO RNO ANOct 15, 1995 · N302US · Airbus A320211 · Cabin Cooling SystemSDR 9516133226Eel Power Supply · inoperativeDURING CRUISE, THE AFT CABIN EMERGENCY PATH LIGHTS REMAINED ILLUMINATED, RESETTING THE SYSTEM DID NOT HELP. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT, 11WL AND OPERATIONAL CHECK OK.Oct 15, 1995 · N326US · Airbus A320211 · Emergency LightingSDR CA951103103Outlfow Valve · inoperative(CAN)CABIN PRESSURE 1 & 2 FAULT IN CRUISE AT FL350, UNABLE TO CONTROL MANUALLY. FLIGHT CREW REPORTED EAR PAIN FOLLOWED BY ECAM WARNING, CABIN ALTITUDE AT 8500 FEET AND CLIMBING, OUTFLOW VALVE INDICATING FU LL OPEN. NO APPRECIABLE POSITION CHANGE WHEN STANDBY SOct 12, 1995 · Airbus A320211 · Pressure Regulator/Outflow ValveSDR 9516473210Longeron · corrodedDURING IL CHECK, FOUND CORROSION ON STR 44 BETWEEN FRAMES 33 TO 34. REPAIRED STRINGER (P/N D532-31521-200), PER EA 32-104280.Oct 12, 1995 · N310NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR 9516463210Longeron · corrodedDURING IL CHECK, FOUND CORROSION IN STR 43R BETWEEN FRAMES 32 TO 35. REPAIRED STRINGER (P/N D532-31511-201), PER EA 32-104278, -104279.Oct 12, 1995 · N310NW · Airbus A320211 · Fuselage Main, Longeron/StringerSDR 9516113210Fitting · corrodedDURING IL CHECK, FOUND CORROSION ON THE 4L DOOR FRAME CORNER FITTING. REPLACED FITTING.Oct 12, 1995 · N310NW · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA951129511Slide Cable · routing wrong(CAN)DURING INSPECTION OF L2 DOOR ESCAPE SLIDE, MAINTENANCE FOUND ACKBOARD RELEASE MECHANISM INSTALLED INCORRECTLY BY MANUFACTURER. AS A RESULT SLIDE WOULD NOT DEPLOY PROPERLY. UNIT REMOVED TO SAFETY SHOP FOR OVERHAUL.Oct 11, 1995 · Airbus A320211 · Escape SlideSDR CA951129508Limiter · tripped(CAN)PRIOR TO ARRIVAL, WHEN FLAPS INITIALLY SELECTED TO FLAP 1, SLATS DID NOT MOVE & SHOWED ZERO DEGREES RANGE. MAINTENANCE FOUND OUTBOARD TORQUE LIMITER TRIPPED ON #2 RIGHT SLAT ACTUATOR. THE OUTBOARD TOR QUE LIMITER WAS RESET. ACTUATOR CHECKED, WING TIP BRAKOct 9, 1995 · Airbus A320211 · Leading Edge Slat Control SystemSDR 9515133204Line · leakingDURING TAKEOFF ROLL, RECEIVED HYD 'Y' RSVR LO LVL MESSAGE. TAKEOFF WAS ABORTED AT 60 KNOTS AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPAIRED A LEAKING HYDRAULIC LINE IN THE RIGHT MAIN LANDING GEAR WHEEL WELL. LEAK AND OPERATIONAL CHECK OK.Oct 6, 1995 · N304US · Airbus A320211 · Hydraulic System, MainSDR 9515093223Connection · looseDURING DESCENT, RECEIVED HYD 'G' RSVR LO LVL MESSAGE. CREW FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. AIRCRAFT WAS TOWED TO THE GATE WHERE MAINTENANCE FOUND A LOOSE B-NUT AT THE LEFT HAND MAIN LANDING GEAOct 3, 1995 · N323US · Airbus A320211 · Hydraulic System, MainSDR 9515993209Support · corrodedDURING IL CHECK, FOUND CORROSION ON THE FLOOR SUPPORTS AT Y=+- 1929 FRAME 66 TO 68. REPAIRED SUPPORTS PER EA 32-99197.Sep 29, 1995 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR CA951129504Actuator · failed(CAN)DURING APPROACH FLAPS LOCKED OUT AT FLAP 2 SELECTION. MAINTENANCE REPLACED #1 INBOARD LEFT FLAP ACTUATOR.Sep 28, 1995 · Airbus A320211 · Trailing Edge Flap ActuatorSDR 9514933231Engines · malfunctionedDURING TAKEOFF ROLL, THE ENGINES WERE NOT ACCELERATING EVENLY. TAKEOFF WAS ABORTED AT APPROXIMATELY 10 TO 15 KNOTS. MAINTENANCE INSPECTION REVEALED NO DISCREPANCIES. ENGINES OPERATIONAL CHECK OK.Sep 28, 1995 · N331NW · Airbus A320211 · Engine (Turbine/Turboprop)SDR 9515913209Longeron · corrodedDURING IL CHECK, FOUND CORROSION ON STR 43R BETWEEN FRAMES 32 TO 35. REPAIRED STRINGER (P/N D532-31511-200), PER EA 32-99209.Sep 27, 1995 · N309US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR 9515903209Longeron · corrodedDURING IL CHECK, FOUND CORROSION ON STR 42R BETWEEN FRAMES 33 TO 34. REPAIRED STRINGER (P/N D532-31523-200), PER EA 32-99207.Sep 27, 1995 · N309US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR 9515893209Longeron · corrodedDURING IL CHECK, FOUND CORROSION ON STR 41R BETWEEN FRAMES 30 TO 31. REPAIRED STRINGER (P/N D532-31542-200, D532-31543-200), PER EA 32-99208.Sep 27, 1995 · N309US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR 9514913217Ecu · malfunctionedDURING CRUISE AT FL 390, THE AUTO THROTTLE TRIPPED OFF AND THE NR 1 ENGINE N1 SPEED ACCELERATED TO 102 PERCENT FOR 41 MINUTES. CYCLING OF THE THRUST LEVER WAS NO HELP, DESCENDED TO A LOWER ALTITUDE AND SHUT NR 1 ENGINE DOWN. AFTER ALLOWING THE ENGINE TO COOLSep 27, 1995 · N317US · Airbus A320211 · Fuel Control/Turbine EnginesSDR 9514783229Controller · malfunctionedDURING CRUISE, EXPERIENCED SEVERAL UNCOMMANDED AILERON ROLLS. THE RIGHT AILERON APPEARED TO MOVE ON THE ECAM PICTORIAL WHILE THE LEFT WAS STABLE. ALSO, RECEIVED ELAC 1 FAULT. AIRCRAFT CONTINUED TO SAN AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE CSep 27, 1995 · N329NW · Airbus A320211 · Aileron Control SystemSDR 9515823209Supports · corrodedDURING IL CHECK, FOUND CORROSION ON THE RIGHT AND LEFT OUTBOARD FLOOR SUPPORTS BS 1292. REPAIRED SUPPORTS (P/N 534-72172-203, -204) PER EA 32-99197.Sep 22, 1995 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR 9514503214Oil Temp Wire · chafedDURING CLIMB, THE NR 1 ENGINE OIL TEMPERATURE GAUGE INDICATED HIGH. ENGINE WAS SHUTDOWN AND THE AIRCRAFT WAS DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. CHAFED WIRES IN THE PYLON SECTION WERE FOUND AND REPAIRED. ENGINE WAS RUN AND LEAK CHECKED OK. AIRCRAFSep 22, 1995 · N314US · Airbus A320211 · Engine Oil TemperatureSDR 9515753209Sill · corrodedDURING IL CHECK, FOUND CORROSION ON THE LEFT AFT DOOR SILL. REPAIRED SILL PER EA 32-99200.Sep 21, 1995 · N309US · Airbus A320211 · Fuselage Miscellaneous StructureSDR 9514163221Servo · faultedDURING CLIMBOUT, RECEIVED ELAC 1 FAULT AND ATTEMPTED RESET WITH NO HELP. LEFT AILERON INDICATES BOTH B AND G AMBER AND RIGHT AILERON INDICATES G AMBER. WITH LEFT AILERON HYDRAULIC SERVO CONTROL SYSTEM PREVIOUSLY ON MEL, THE DECISION WAS MADE TO RETURN TO MSPSep 11, 1995 · N321US · Airbus A320211 · Aileron Control SystemSDR 9514173206Vbv Sensor · malfunctionedDURING CLIMB AT 10,000 FEET, RECEIVED ECAM MESSAGE ENG 2 COMPRESSOR VANE ACCOMPANIED WITH NO RAPID THROTTLE MOVEMENT. AIRCRAFT RETURNED TO DTW DUE TO LACK OF PARTS IN SJU TO ADDRESS THE PROBLEM. THE AIRCRAFT LANDED WITHOUT INCIDENT AND THE VBV SENSOR WAS REPSep 9, 1995 · N306US · Airbus A320211 · Compressor Bleed ValveSDR 9513763203O-Ring · failedDURING DESCENT, RECEIVED HYD 'G' RSVR LOW LEVEL MESSAGE. AN EMERGENCY WAS DECLARED AND EQUIPMENT CALLED OUT. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE O-RING ON NR 1 ENGINE PRESSURE FITTING. LEAK AND OPERATIONAL CHECK OK.Sep 6, 1995 · N303US · Airbus A320211 · Hydraulic System, MainSDR 9513773217Air Distribution · smokeDURING CLIMBOUT FROM SAN, HEARD A BANG AND FELT A THUMP, VISUAL CHECK REVEALED NO DISCREPANCIES. APPROXIMATELY 1.5 HOURS LATER, FLIGHT ATTENDANT REPORTED SMALL CLOUD OF SMOKE JUST OUTSIDE THE FORWARD LAVATORY, A STRONG ELECTRICAL SMELL WAS NOTED. AN EMERGENCSep 5, 1995 · N317US · Airbus A320211 · Air Distribution SystemSDR 9513553204Hyd Pump · failedDURING CRUISE RECEIVED HYD-B ELEC PUMP LOW PRESSURE MESSAGE. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE BLUE HYDRAULIC SYSTEM ELECTRIC PUMP. OPS AND LEAK CHECKED OK.Aug 31, 1995 · N304US · Airbus A320211 · Hydraulic Pump, AuxiliarySDR 9513353226Generator · malfunctionedDURING TAKEOFF ROLL, RECEIVED ELEC IDG 2 OIL LOW PRESSURE MESSAGE. THE TAKEOFF WAS ABORTED AT APPROXIMATELY 40 KNOTS AND AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE NR 2 IDG, LEAK AND OPERATIONAL CHECK OK.Aug 30, 1995 · N326US · Airbus A320211 · AC Generator-AlternatorSDR 9513363250Hyd Pump · failedDURING DESCENT INTO DTW, RECEIVED HYD B-SYS LOW PRESSURE INDICATION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT IN DTW. MAINTENANCE REPLACED THE BLUE HYDRAULIC SYSTEM ELECTRIC PUMP, CASE DRAIN, AND PRESSURE FILTERS. LEAK AND OPERATIOAug 27, 1995 · N350NA · Airbus A320211 · Hydraulic Pump, AuxiliarySDR 9512893205Spoiler · floatingDURING ROTATION, NOTICED A SLIGHT ROLL MOMENT AT APPROXIMATELY 1,000 FEET. RECEIVED F/CTL GND SPOILER FAULT. AIRCRAFT DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. MAINTENANCE NOTED THAT THE RIGHT GROUND SPOILER INDICATED A FOUR INCH DEFLECTION ON THE LOWER Aug 22, 1995 · N305US · Airbus A320211 · Drag Control SystemSDR 9512803240Idg · overheatDURING CRUISE, THE NR 2 ENGINE IDG TEMPERATURE INCREASED TO 183 DEGREES CELCIUS. DISCONNECTED NR 2 IDG AND RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 IDG AND IDG OIL COOLER. OPERATIONAL CHECK OK.Aug 20, 1995 · N340NW · Airbus A320211 · AC Generator-AlternatorSDR 9512793215Water Line · rupturedDURING CLIMBOUT FROM MIA, THE RIGHT AFT LAVATORY DEVELOPED AN UNCONTROLLABLE WATER LEAK. AIRCRAFT DIVERTED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AFT RIGHT LAV WATER SUPPLY LINE. LEAK AND OPERATIONAL CHECK OK.Aug 20, 1995 · N315US · Airbus A320211 · Waste Disposal SystemSDR 9512853215Fire Loop · malfunctionedDURING TAKEOFF WITH ENG NR 2 FIRE LOOP 'B' FAULT INDICATION ON MEL, RECEIVED NR 2 ENGINE FIRE WARNING. ENGINE WAS SHUT DOWN AND AIRCRAFT RETURNED TO DTW WHERE AN UNEVENTFUL LANDING TOOK PLACE. THE NR 2 PYLON LOOP 'B' AND CORE LOOP SUPPORT WERE REPLACED. THEAug 19, 1995 · N315US · Airbus A320211 · Fire DetectionSDR 9512843212Hmu · malfunctionedDURING CLIMBOUT, VIBRATION FROM NR 1 ENGINE WAS FELT THROUGHOUT THE AIRCRAFT ACCOMPANIED BY FLUCTUATIONS IN FUEL FLOW N1, AND THROTTLE POSITION ON ECAM INDICATION. POWER WAS REDUCED, BUT ENGINE PERFORMANCE WAS STILL ERRATIC. AIRCRAFT RETURNED TO MSP AND LANDAug 19, 1995 · N312US · Airbus A320211 · Fuel Controlling System
Back to Airbus A320-211