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.
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 9512813246B-Nut · looseDURING TAKEOFF ROLL, RECEIVED HYD YELLOW RESERVOIR LOW LEVEL MESSAGE. TAKEOFF WAS ABORTED AT APPROXIMATELY 50 KNOTS. MAINTENANCE TIGHTENED LOOSE B-NUT ON THE YELLOW SYSTEM ACCUMULATOR. SERVICED YELLOW HYDRAULIC SYSTEM TO FULL. LEAK AND OPERATIONAL CHECK OKSDR 9512823242Eiu · malfunctionedDURING CRUISE AT FL 390, RECEIVED ENG 1 EIU FAULT WITH ACCOMPANIED LOSS OF AUTO THRUST. ALSO, RECEIVED AIR PACK 1 AND 2 FAULT. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND DESCENDED TO 10,000 FEET MSL. AIRCRAFT DIVERTED TO DEN AND LANDED WITHOUT INCIDENSDR 9512163204Vbv · malfunctionedDURING CLIMB, NR 2 ENGINE EGT REACHED 890 DEGREES AND NEVER COOLED BELOW 850 DEGREES. THE AIRCRAFT RETURNED TO MSP WHERE AN UNEVENTFUL LANDING TOOK PLACE. THE VBV AND A SHEARED FLEX SHAFT WERE REPLACED. GROUND RUNUP CONFIRMED PROPER ENGINE OPERATION.SDR 9511663223Panel · vibrationWHILE CLIMBING THROUGH FL 300 AT A SPEED OF MACH 0.78, EXPERIENCED AIRFRAME VIBRATION. SLOWED SPEED TO APPROXIMATELY 0.74 MACH AND VIBRATION WENT AWAY. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE TIGHTENED THE FASTENERS ON A BELLY PANESDR 9511423225Engine · failedDURING CLIMB, THE NR 1 ENGINE EGT REACHED TEMPERATURE OF 935 DEGREES CELSIUS AND STAYED THERE FOR 2 TO 4 SECONDS. THRUST WAS REDUCED AND EGT DROPPED TO YELLOW ZONE BEFORE AGAIN CLIMBING TO RED ZONE FOR 5 SECONDS. THRUST LEVER WAS THEN REDUCED TO IDLE AND THESDR 9512133220Computer · malfunctionedWHILE PASSING THROUGH 20,000 FEET IN DESCENT INTO SEA, RECEIVED 'F/CTL ELAC 1 FAULT', ACCOMPANIED BY A 5 TO 10 DEGREE ROLL LEFT AND RIGHT. ATTEMPTED RESET, NO HELP. AIRCRAFT LANDED WITHOUT INCIDENT IN SEA. MAINTENANCE RESET ELEVATOR AILERON COMPUTER NR 1. SDR 9511183214Transmitter · malfunctionedAFTER TAKEOFF, THRUST WAS APPLIED, THE AIRCRAFT DRIFTED SLIGHTLY TO THE RIGHT, FULL LEFT RUDDER WAS APPLIED WITH NO RESPONSE. FULL LEFT TILLER WAS APPLIED WITH NO RESPONSE. THE TAKEOFF WAS ABORTED AT 40 KNOTS. AIRCRAFT RETURNED SAFELY TO THE GATE. MAINTENASDR 9510863211Hyd Pump · leakingDURING CRUISE AT FL 370 APPROXIMATELY ONE HOUR INTO FLIGHT, THE GREEN HYDRAULIC SYSTEM QUANTITY DROPPED TO ZERO. THE POWER TRANSFER UNIT AND THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP WERE DISCONNECTED. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND CONTINUED TSDR 9510853245Eel Power Supply · malfunctionedDURING PREFLIGHT CHECK, THE EMERGENCY PATH LIGHTS ON SEATS ROW 14 TO THE REAR OF THE AIRCRAFT REMAIN ILLUMINATED. REPLACED POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK OK.SDR 9510373224Hyd Syst · reqd serviceDURING APPROACH INTO SAN, THE GREEN HYDRAULIC SYSTEM PRESSURE AND QUANTITY DECREASED TO ZERO. ACCOMPLISHED MANUAL EXTENSION OF THE LANDING GEAR. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO LEAKSDR 9510363224Hose · brokenDURING CLIMBOUT FROM SAN, THE GREEN HYDRAULIC SYSTEM INDICATED ZERO AFTER GEAR RETRACTION. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT IN LAX WHERE MAINTENANCE FOUND THE RIGHT MLG LOCK STAY ACTUATOR OUTBOARD HOSE, LOWER COLLAR, BROKEN. SDR 9509903222Flap Indication · malfunctionedDURING APPROACH INTO LAS, RECEIVED 'F/CTL FLAPS LOCKED' ALIGNMENT FAULT, WHEN SELECTING FLAPS 2 POSITION. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DISCREPANCIES. AIRCRAFT OK FOR SERVICSDR 9509803238Engine · malfunctionedDURING ROTATION, AIRCRAFT YAWED TO THE LEFT ACCOMPANIED BY A LOUD AIR NOISE AND VIBRATION FELT IN THE COCKPIT. NO MESSAGES WERE INDICATED ON ECAM OR STATUS PAGE. OPERATING PROCEDURE WAS FOLLOWED AND THE AIRCRAFT RETURNED TO SEA WHERE AN UNEVENTFUL LANDING TOSDR 9509723237Valve · malfunctionedDURING TAKEOFF ROLL, RECEIVED AIR ENG 2 BLEED FAULT. TAKEOFF WAS ABORTED AT LESS THAN 80 KNOTS. ALSO, RECEIVED AIR LT WING LEAK AND RIGHT PACK OVERHEAT MESSAGES. MAINTENANCE REPLACED THE NR 1 ENGINE OVER PRESSURE VALVE. LEAK AND OPERATIONAL CHECK OK.SDR 9509653216Bushing · wornDURING CLIMBOUT AT 22,000 FEET AND 315 KNOTS, AIRCRAFT BEGAN VIBRATING. VIBRATION WAS FELT THROUGHOUT THE CABIN. ENGINE VIBRATION MONITORS WERE NORMAL. AIRCRAFT RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT FORWARD END RAM AIR SDR 9509353250Servo Unit · malfunctionedEN ROUTE LGA TO MSP, NOSE WHEEL STEERING FAULT APPEARED, RESETS WERE UNSATISFACTORY. A NORMAL LANDING WAS MADE AND THE AIRCRAFT TAXIED CLEAR OF THE RUNWAY. AIRCRAFT WAS TOWED TO THE GATE. REPLACED THE NOSE WHEEL STEERING SERVO CONTROL. OPERATIONAL CHECK WASSDR 9508873205O-Ring · leakingDURING CLIMBOUT AT FL280, RECEIVED HYD Y RSVR LO LVL MESSAGE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO MCO AND LANDED WITHOUT INCIDENT WITH EMERGENCY EQUIPMENT STANDING BY. MAINTENANCE REPLACED AN 'O' RING ON THE HYDRAULIC POWER TRANSFER UNIT HSDR 9509233240Seat Track · corrodedDURING C-CHECK, FOUND CORROSION IN THE SEAT TRACKS FR 20 TO 24 AT Y=-765 AND -1292. REPAIRED TRACK PER EA 32-098322.SDR 9508863226Hyd Fluid · low levelAFTER APPLYING T/O THRUST FOR TAKEOFF ROLL, RECEIVED HYD B RSVR LO LVL MESSAGE. THE TAKEOFF WAS ABORTED AT 60 KNOTS. MAINTENANCE SERVICED THE BLUE HYDRAULIC SYSTEM. LEAK AND OPERATIONAL CHECK OK.SDR 9508643218Computers · failedDURING CLIMBOUT FROM ORD, AIRCRAFT EXPERIENCED APPROXIMATELY 45 SECONDS OF APPROXIMATELY 10 VERY SMALL QUICK AILERON MOVEMENTS ACCOMPANIED BY ELEC 1 FAULT. DURING APPROACH INTO MEM AIRCRAFT EXPERIENCED ONE AILERON JERK. AIRCRAFT LANDED WITHOUT INCIDENT IN MESDR 9508203214Connector · looseDURING CRUISE, THE NR 1 OIL QUANTITY INDICATION DROPPED TO 1.5. THE CIRCUIT BREAKER WAS RESET, BUT INDICATION STAYED THE SAME. THE PRESSURE PROCEEDED TO FLUCTUATE AND THE ENGINE WAS SHUTDOWN. THE AIRCRAFT DIVERTED TO ORD WHERE AN UNEVENTFUL LANDING WAS MADESDR 9507493204Throttle Contl · malfunctionedDURING CLIMBOUT FROM MSP, RECEIVED ENG 2 THR LEVER FAULT MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND RETURNED TO MSP WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE REPLACED THE NR 2 ENGINE THROTTLE CONTROL UNIT. OPERATIONAL CHECK OK.SDR 9507483248Eel Power Supply · inoperativeDURING APPROACH INTO MSP, THE EMERGENCY EXIT SIGNS ABOVE THE AFT GALLEY DOORS DID NOT ILLUMINATE AFTER LANDING GEAR EXTENSION. MAINTENANCE REPLACED THE EMERGENCY LIGHTS POWER SUPPLY AND BATTERY PACK. OPERATIONAL CHECK OK.SDR 9507433228Valve · malfunctionedDURING CLIMBOUT FROM SEA, RECEIVED VENT SKIN VALVE FAULT MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND THEN RECEIVED VENT BLOWER FAULT MESSAGE. UNABLE TO PRESSURIZE AIRCRAFT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO SEA AND LANDED SDR 9507433204Vent Valve · malfunctionedDURING CLIMBOUT FROM SEA, RECEIVED VENT SKIN VALVE FAULT MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND THEN RECEIVED VENT BLOWER FAULT MESSAGE. UNABLE TO PRESSURIZE AIRCRAFT. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO SEA AND LANDED SDR 9507123202Actuator · malfunctionedDURING CRUISE WHILE AT FL 390, THE NR 2 PACK OVERHEATED TO 245 DEGREES CELSIUS, FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES. PACK OVERHEATED AGAIN TO 260 DEGREES CELSIUS, THE PACK WAS SHUTDOWN. LIGHT SMOKE WAS VISIBLE IN THE CABIN. RECEIVED 'SMOKE AFT CARGSDR 9507093208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON STR 41L AND 43L. CORROSION IS LOCALIZED AROUND FASTENERS COMMON TO FUSELAGE SKIN. CORROSION ON STR 41L EXISTS BETWEEN FRAMES 25 AND 35. CORROSION ON STR 43L IS LOCATED BETWEEN FRAMES 29 AND 34. REPAIREDSDR 9507603208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON LONGERON 44 OUTER FLANGE BETWEEN FR 33 TO 34. REPLACED LONGERON 44 PER EA 32-97859.SDR 9507313208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON THE RIVETS COMMON TO STR 44 BETWEEN FRAMES 33 AND 34. AFTER REMOVING THE RIVETS, THE STRINGER REVEALED CORROSION ON THE UPPER SURFACE OF THE STRINGER FLANGE COMMON TO THE FUSELAGE SKIN. REPAIRED PER NWA ESDR 9507103208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON RIVETS COMMON TO STR 40L BETWEEN FRAMES 29 AND 30. AFTER REMOVAL OF THE RIVETS, THE STRINGER REVEALED CORROSION ON THE UPPER SURFACE FLANGE COMMON TO THE FUSELAGE SKIN. REPAIRED PER NWA EA 32-97855. SERISDR 9506963231Computers · malfunctionedAT 25,000 FEET DURING CLIMB, THE AIRCRAFT ROLLED RIGHT AND ELAC NR 1 FAULTED. RESET WAS OK, THREE MINUTES LATER THE AIRCRAFT ROLLED AGAIN WITH FAULT DISPLAY SYSTEM INDICATING ELAC NR 2 MALFUNCTION. AIRCRAFT RETURNED TO MSP AND LANDED WITHOUT INCIDENT. REPLASDR 9507073208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON STR 41R BETWEEN FRAMES 33 AND 34. CORROSION IS LOCALIZED TO THE INNER SURFACE OF THE FLANGE COMMON TO THE FUSELAGE SKIN. MAX DEPTH OF THE CORROSION IS 0.026 INCH. REPAIRED PER NWA EA 32-97847. SERIAL NRSDR 9507053208Longeron · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON STR 41R BETWEEN FRAMES 32 AND 33. CORROSION IN LOCALIZED TO THE INNER SURFACE OF THE FLANGE COMMON TO THE FUSELAGE SKIN. MAX DEPTH OF CORROSION IS 0.026 INCH. REPAIRED PER NWA EA 32-97845. SERIAL NR 32 SDR 9506623201Bolt · looseDURING CLIMB-OUT FROM MKE, THE NOSE LANDING GEAR WOULD NOT RETRACT. BOTH THE GREEN DOWN AND LOCKED AND RED IN TRANSIT INDICATION LIGHTS ILLUMINATED. THE MAIN LANDING GEAR RETRACTED AND THE NOSE LANDING GEAR DOORS INDICATED OPEN. THE LANDING GEAR WAS CYCLED SDR 9507083208Support · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON THE UPPER SURFACES OF THE FLOOR SUPPORTS AT Y EQUALS -1292 BETWEEN FRAMES 68 AND 69 AND AT Y EQUALS -464 BETWEEN FRAMES 66 AND 67. REPAIRED PER NWA EA 32-97984. SERIAL NR 32 CHANGED TO 107.SDR 9507063208Support · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON THE UPPER SURFACE OF THE FLOOR SUPPORT AT Y EQUALS -1292 BETWEEN FRAMES 66 AND 68. REPAIRED PER NWA EA 32-97981. SERIAL NR 32 CHANGED TO 107.SDR 9507113208Floor Support · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON THE UPPER SURFACE OF THE FLOOR SUPPORT AT Y EQUALS -254 BETWEEN FRAMES 12 AND 24. REPAIRED PER NWA EA 32-97979.SDR 9507043208Floorbeam · corrodedDURING INTERMEDIATE LAYOVER VISIT, FOUND CORROSION ON THE AFT GALLEY FLOOR SUPPORT BEAM AT Y EQUALS 1262. CORROSION WAS FOUND ON THE UPPER SURFACE OF THE UPPER FLANGE BETWEEN FRAMES 66 AND 67. CORROSION IS LOCALIZED AROUND FASTENER ATTACH HOLES FOR FLOOR BOASDR 9506323219Pump · making metalDURING CLIMBOUT FROM DTW, RECEIVED 'HYD B SYS LO PR' MESSAGE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND PRESSURE RETURNED TO 1750 PSI. DECISION WAS MADE TO RETURN TO DTW WHERE AN UNEVENTFUL LANDING WAS ACCOMPLISHED. MAINTENANCE FOUND THE BLUE HYDRAULSDR 9505653242Limiter · malfunctionedAFTER TAKEOFF FROM MSP, THE EMERGENCY GENERATOR FAULT LIGHT ILLUMINATED. THE LANDING GEAR WAS CYCLED. THE LIGHT EXTINGUISHED WHEN THE GEAR WAS LOWERED, AND RETURNED WHEN THE GEAR WAS RAISED. FLIGHT CONTINUED TO DCA AND LANDED WITHOUT INCIDENT. MAINTENANCE SDR 9505553242Limiter · malfunctionedAFTER TAKEOFF FROM MSP, THE EMERGENCY GENERATOR FAULT LIGHT ILLUMINATED. THE LANDING GEAR WAS CYCLED. THE LIGHT EXTINGUISHED WHEN THE GEAR WAS LOWERED AND RETURNED WHEN THE GEAR WAS RAISED. FLIGHT CONTINUED TO DCA AND LANDED WITHOUT INCIDENT. MAINTENANCE RSDR 9505173248Door Light · illuminatedDURING APPROACH INTO SFO AFTER THE LANDING GEAR WAS EXTENDED, THE LEFT MAIN LANDING GEAR DOOR WARNING LIGHT ILLUMINATED. CYCLED THE LANDING GEAR HANDLE AND ALL INDICATIONS NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TEST OF NR 1 AND NR 2 LANDING GSDR 9505243234Angle · crackedDURING 'C' CHECK, THE LEFT FUSELAGE BELLY FAIRING CONNECTING ANGLE FOR PANEL 193B AND THE LEFT OVERWING SLIDE PACK WAS FOUND CRACKED. THE CRACK EMANATES FROM THE FORWARD MOST EDGE TO THE SECOND FASTENER HOLE APPROXIMATELY 4 INCHES AFT OF THE FORWARD EDGE. RESDR 9504693207Floor Support · corrodedDURING THE INTERMEDIATE LAYOVER VISIT, THE AFT GALLEY FLOOR SUPPORT AT Y=1165 BETWEEN FRAME 68 AND 69 WAS FOUND CORRODED ON THE LOWER SURFACE OF THE UPPER FLANGE. CORROSION IN LOCALIZED AROUND ONE FASTENER ATTACH HOLE FOR FLOOR BOARDS AT APPROXIMATELY X=3942.SDR 9503743214Hyd Door · looseDURING CLIMB-OUT FROM DTW, EXPERIENCED MEDIUM FREQUENCY AIRFRAME VIBRATION AT 310 KNOTS. LEVELED OFF AT FL230 AND REDUCED SPEED TO 290 KNOTS AND VIBRATION STOPPED. AIRCRAFT RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED YESDR 9503753207Seat Track · corrodedDURING INTERMEDIATE LAYOVER CHECK, FOUND CORROSION ON THE UPPER FLANGE OF THE SEAT TRACK AT Y = +765, FRAME 18. CORROSION WAS AT A NUT CLIP LOCATION. REPAIRED PER NWA EA 32-96360.SDR 9503683214Dmc · failedDURING TAKEOFF ROLL, THE CAPTAIN'S PRIMARY FLIGHT DISPLAY, NAVIGATION DISPLAY AND UPPER ENGINE DISPLAY FAILED. THE TAKEOFF WAS ABORTED AT 60 KNOTS. ECAM FAULTED EIS DMC NR 1. PLACED NR 1 DISPLAY MANAGEMENT COMPUTER ON MEL 31-63-01 AND LATER REPLACED. OPS CSDR 9503273226Retract Mech · malfunctionedDURING APPROACH INTO SAN, RECEIVED 'F/CTL FLAPS LOCKED' ALIGNMENT FAULT WHEN FLAP 3 WAS SELECTED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED NO DESCREPANCIES.SDR 9502803213Flt Contl Unit · inoperativeDURING CLIMB-OUT, FLIGHT CONTROL UNITS NR 1 AND NR 2 FAILED. RESET CIRCUIT BREAKERS, NO HELP. DECISION WAS MADE TO RETURN TO MSP. REPLACED FLIGHT CONTROL UNIT. SYSTEM TESTS WERE NORMAL.SDR 9504683207Sill · corrodedDURING INTERMEDIATE LAYOVER VISIT, CORROSION WAS FOUND ON THE INBOARD FLANGE OF THE RIGHT AFT CABIN DOOR LOWER SILL. CORROSION WAS FOUND AROUND EXISTING NUT PLATES. REPAIR ACCOMPLISHED PER NWA EA 32-96362.
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