Airbus A320-211

Service difficulty reports · 5,271

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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"

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SDR 950467SHOPCross Beam · wornDURING ENGINE SHOP OVERHAUL, SEVERAL FORWARD ENGINE MOUNT CROSS BEAMS WERE FOUND WITH WEAR MARKS IN THE CRITICAL AREA AS DEFINED BY ROHR CMM 71-21-06, FIG.803. THE DAMAGED AREAS RANGED IN DEPTH FROM 0.002 INCH TO 0.011 INCH. REPAIRS ACCOMPLISHED PER NWA EA 3Feb 17, 1995 · Airbus A320211 · Engine Mount SectionSDR 9501903211Handle · not secureDURING TAKEOFF ROLL, THE AFT CARGO DOOR INDICATED OPEN. THE TAKEOFF WAS ABORTED. MAINTENANCE FOUND THE AFT CARGO DOOR HANDLE POPPED OUT 0.5 INCH. SECURED DOOR HANDLE AND ALL INDICATIONS AND OPERATION NORMAL.Feb 6, 1995 · N311US · Airbus A320211 · Cargo/Baggage DoorsSDR 9501823241Antenna · malfunctionedDURING CRUISE, RECEIVED 'NAV RA 2' FAULT. AIRCRAFT DIVERTED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 RADIO ALTIMETER TRANSMISSION ANTENNA (6SA2). OPERATIONAL CHECK OK.Feb 5, 1995 · N341NW · Airbus A320211 · Ground Proximity SystemSDR 9501833204Ecu · malfunctionedDURING CLIMB, THE NR 1 ENGINE EXPERIENCED TWO OR THREE POWER SURGES. NUMEROUS 'A' AND 'B' FADEC MESSAGES WERE OBSERVED. ENGINE THRUST WAS REDUCED TO IDLE AND ENGINE WAS EVENTUALLY SHUT DOWN DUE TO FAILURE DURING RETURN TO MEM. THE ENGINE CONTROL UNIT AND ENFeb 3, 1995 · N304US · Airbus A320211 · Fuel Control/Turbine EnginesSDR 9503353202Skin · delaminatedDURING C-CHECK, FOUND THE NR 1 AND NR 2 ENGINE FAN COWLS RIGHT SIDE WITH 22 INCH BY 28 INCH AND 20 INCH BY 28 INCH AREA OF DELAMINATION RESPECTIVELY. REPAIRS ACCOMPLISHED PER NWA EA 32-96350 AND EA 32-96349.Jan 31, 1995 · N302US · Airbus A320211 · Engine Cowling SystemSDR 9501323205Adc · malfunctionedDURING APPROACH INTO BOS, RECEIVED 'F/CTL ADR DISAGREE' MESSAGE. DUE TO SEVERE WEATHER IN THE APPROACH PATH INTO BOS, CREW ELECTED TO DIVERT TO PHL. AN EMERGENCY WAS DECLARED, AN UNEVENTFUL LANDING ACCOMPLISHED. MAINTENANCE REPLACED THE NR 1 AIR DATA INERTIJan 20, 1995 · N305US · Airbus A320211 · Air Data ComputerSDR 9501023211Indication · malfunctionDURING CLIMB-OUT FROM MKE AFTER LANDING GEAR RETRACTION, THE LEFT MAIN LANDING GEAR DOOR DID NOT INDICATE FULLY CLOSED. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT CONTINUED AND LANDED IN MSP WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOJan 16, 1995 · N311US · Airbus A320211 · Landing Gear Position and WarningSDR 9501063232Thrust Link · wornDURING C-CHECK, THE NR 1 ENGINE FORWARD ENGINE MOUNT THRUST LINKS WERE FOUND WITH WEAR MARKS IN THE CRITICAL AREA AS DEFINED BY ROHR CMM 71-22-07. THE MAXIMUM DEPTH OF THE DAMAGED AREAS WAS 0.002 INCH. REPAIRED PER NWA EA 32-96336.Jan 13, 1995 · N332NW · Airbus A320211 · Engine Mount SectionSDR 9503313232Thrust Link · wear marksDURING C-CHECK, THE NR 1 ENGINE FORWARD ENGINE MOUNT THRUST LINKS AND THE NR 2 ENGINE FORWARD INBOARD THRUST LINK WERE FOUND WITH WEAR MARKS IN THE CRITICAL AREAS AS DEFINED BY ROHR CMM 71-21-06, FIG 803. THE DAMAGED AREAS RANGED IN DEPTH FROM 0.001 INCH TO 0Jan 12, 1995 · N332NW · Airbus A320211 · Engine Mount SectionSDR 9503623232Angle · crackedDURING 'C' CHECK, FOUND THE LEFT FUSELAGE BELLY FAIRING CONNECTING ANGLE FOR PANEL 193B CRACKED. THE CRACK, EMINATES FROM THE FORWARD MOST EDGE TO THE 3RD FASTENER HOLE APPROXIMATELY 6 INCHES AFT OF THE FORWARD EDGE. THE ANGLE IS ATTACHED TO THE LEFT OVERWINJan 10, 1995 · N332NW · Airbus A320211 · Aerodynamic FairingsSDR 9500383247Handle · not stowedDURING TAKEOFF ROLL, THE AFT CARGO DOOR WARNING LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE FOUND THE AFT CARGO DOOR HANDLE NOT FAIRED. STOWED HANDLE AND ALL INDICATIONS WERE NORMAL.Jan 10, 1995 · N347NW · Airbus A320211 · Door Warning SystemSDR 9500363213Computer · failedDURING CLIMB-OUT FROM DTW, RECEIVED 'VENT SKIN VALVE' FAULT. UNABLE TO PRESSURIZE AIRCRAFT. RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AVIONICS EQUIPMENT VENTILATION COMPUTER. OPERATIONAL CHECK OK.Jan 10, 1995 · N313US · Airbus A320211 · Cabin Pressure Control SystemSDR 9500273242Duct · leakingDURING CLIMBOUT FROM DTW, RECEIVED 'AIR R WING LEAK' MESSAGE. ACCOMPLISHED COCKPIT OPERATING MANUAL PROCEDURES AND RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND PNEUMATIC DUCT LEAKING FORWARD OF RIGHT PACK FLOW CONTROL VALVE. TIGHTENED CLJan 9, 1995 · N342NW · Airbus A320211 · Pneumatic Distribution SystemSDR 9500263214Flap Drive · out of rigDURING APPROACH INTO SNA RECEIVED 'F/CTL FLAPS LOCKED' ALIGNMENT FAULT WHEN SELECTING FLAPS 3. THE FLAPS WERE LOCKED AT ZERO. AN EMERGENCY WAS DECLARED AND AIRCRAFT DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. MAINTENANCE RIGGED THE NR 1, 2, 3, AND 4 LEFT WJan 8, 1995 · N314US · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9500233214Retract Mech · malfunctionedDURING APPROACH INTO PHX RECEIVED 'F/CTL FLAPS LOCKED' ALIGNMENT FAULT. ACCOMPLISHED A FLAPS LESS THAN ONE LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTION OF THE FLAP DRIVE MECHANISM REVEALED NO DISCREPANCY. OPERATIONAL CHECK OK.Jan 7, 1995 · N314US · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9500373202Valve · malfunctionedDURING CLIMB-OUT FROM MSP, THE CREW WAS UNABLE TO PRESSURIZE THE AIRCRAFT. RETURNED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE SKIN AIR EXTRACT VALVE. OPERATIONAL CHECK OK.Jan 6, 1995 · N302US · Airbus A320211 · Cabin Pressure Control SystemSDR 9500413233Thrust Link · wear marksDURING C-CHECK, FOUND THE NR 1 ENGINE FORWARD ENGINE MOUNT THRUST LINKS AND THE INBOARD AFT MOUNT LINK WITH WEAR MARKS IN THE CRITICAL AREA AS DEFINED BY RHOR CMM 71-22-07. THE DAMAGED AREAS RANGED IN DEPTH FROM 0.0005 INCH TO 0.001 INCH. REPAIRS ACCOMPLISHEJan 5, 1995 · N333NW · Airbus A320211 · Engine Mount SectionSDR 9501133220Air Speed Ind · malfunctionedDURING TAKEOFF ROLL, CREW NOTICED NO AIRSPEED INFORMATION ON THE NR 1 PRIMARY FLIGHT DISPLAY. THERE WERE NO ASSOCIATED WARNINGS OR ECAM MESSAGES. THE TAKEOFF WAS ABORTED AT 100 KTS. DURING THE REJECTED TAKEOFF, THE AIRSPEED INDICATION ON THE NR 1 PRIMARY FLJan 4, 1995 · N320US · Airbus A320211 · Airspeed/Mach IndicatorSDR 9503303202Thrust Links · wear marksDURING OVERNIGHT MAINTENANCE, THE NR 1 AND NR 2 ENGINES INBOARD FORWARD ENGINE MOUNT THRUST LINKS WERE FOUND WITH WEAR MARKS IN THE CRITICAL AREA AS DEFINED BY ROHR CMM 71-21-06, FIG 803. THE DAMAGED AREAS DID NOT EXCEED 0.002 INCH DEEP. REPAIRS ACCOMPLISHED Jan 2, 1995 · N302US · Airbus A320211 · Engine Mount SectionSDR 9500013240Hyd Reservoir · low fluidDURING TAKEOFF ROLL, RECEIVED "HYD B RSVR LO AIR PR" MESSAGE. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE SERVICED THE BLUE HYDRAULIC SYSTEM RESERVOIR WITH APPROXIMATELY ONE GALLON OF FLUID.Jan 2, 1995 · N340NW · Airbus A320211 · Hydraulic Reservoir, AuxiliarySDR 9503293227Thrust Links · wear marksDURING OVERNIGHT MAINTENANCE, THE NR 1 ENGINE INBOARD AND OUTBOARD FORWARD ENGINE MOUNT THRUST LINKS AND THE NR 2 ENGINE OUTBOARD FORWARD ENGINE MOUNT THRUST LINKS WERE FOUND WITH WEAR MARKS IN THE CRITICAL AREA AS DEFINED BY ROHR CMM 71-21-06, FIG 803. THE DJan 1, 1995 · N327NW · Airbus A320211 · Engine Mount Section
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