N302US, cancelled Aug 3, 2006

Service difficulty reports · 25

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

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 n_number = 'N302US' AND deregistration_id = 'N302US-2006-08-03'
  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 9904413202Target · out of adjustDURING CRUISE, RECEIVED L/G LGCIU 1 FAULT AND LGCIU 2 FAULT. ON APPROACH PERFORMED GRAVITY EXTENSION OF LANDING GEAR PER COM PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE ADJUSTED THE NOSE LANDING GEAR STRUT EXTENSION TARGET CLEARANCES 24GA AND 25GA. Oct 28, 1999 · N302US · Airbus A320211 · Landing Gear Position and WarningSDR 9904283202Floorbeam · corrodedDURING M-CHECK, FOUND CORROSION ON FLOORBEAM 254R AND 765R BETWEEN FRAMES 16-24R. REPAIRED PER EA 163484 AND SRM 51-72-11.Oct 8, 1999 · N302US · Airbus A320211 · Fuselage Main, Floor BeamSDR 9904273202Floorbeam · corrodedDURING M-CHECK, FOUND CORROSION ON FLOORBEAM 1292L BETWEEN FRAME 16 AND 18. REPAIRED PER EA 32-163484.Sep 30, 1999 · N302US · Airbus A320211 · Fuselage Main, Floor BeamSDR 9806963202Fuel Tank · leakingDURING CLIMB, A FUEL LEAK FROM THE RIGHT WING WAS REPORTED. FLIGHT CREW DIVERTED TO MSP. DURING DESCENT INTO MSP WHILE FOLLOWING COM FOR A FUEL LEAK, NR 2 ENGINE FLAMED OUT AT 5000 FEET. A SUCCESSFUL RELIGHT WAS ACCOMPLISHED, AN UNEVENTFUL LANDING WAS PERFOApr 17, 1998 · N302US · Airbus A320211 · Aircraft Fuel Distribution SystemSDR 9800373202Retract Mech · out of adjustDURING APPROACH WHEN FLAPS POSITION ONE SELECTED, RECEIVED F/CTL FLAPS LOCKED ALIGNMENT FAULT MESSAGE. DIVERTED TO IAD FOR LONGER RUNWAY AND LANDED WITHOUT INCIDENT. MAINTENANCE RIGGED FLAP SYSTEM. OPERATIONAL CHECK OK.Jan 5, 1998 · N302US · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9715603202Actuator · failedDURING APPROACH, RECEIVED F/CTL FLAPS LOCKED ALIGNMENT FAULT. FLAPS LOCKED BETWEEN POSITION ZERO AND ONE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED NR 1, 2 AND 4 LEFT WING FLAP ACTUATORS, OPERATIONAL CHECK OK.Aug 8, 1997 · N302US · Airbus A320211 · Trailing Edge Flap ActuatorSDR 9715203202Control Mech · out of adjustDURING APPROACH, THE FLAPS LOCKED WHEN SELECTING FLAPS POSITION 2. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE RIGGED FLAPS. OPERATIONAL CHECK OK.Aug 6, 1997 · N302US · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9715193202Interconnect · lockedDURING APPROACH WHEN SELECTING FLAPS POSITION 2, RECEIVED F/CTL FLAPS LOCKED ALIGNMENT FAULT. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLAP INTERCONNECT STRUT. OPERATIONAL CHECK OK.Aug 6, 1997 · N302US · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9714893202Pick Off Unit · malfunctionedDURING APPROACH, RECEIVED F/CTL FLAPS LOCKED ALIGNMENT FAULT, SLATS EXTENDED NORMALLY. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE FLAP POSITION PICK OFF UNIT AND RERIGGED THE FLAP ROTARY ACTUATORS, OPERATIONAAug 2, 1997 · N302US · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9714883202Flap Drive · lockedDURING APPROACH, RECEIVED F/CTL FLAPS LOCKED ALIGNMENT FAULT. SLATS EXTENDED NORMALLY, HOWEVER FLAPS REMAINED LESS THAN ONE. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOOTING REVEALED ADIRU1 INPUT TO SFCC Jul 29, 1997 · N302US · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9708853202Antenna · failedDURING CRUISE, THE WEATHER RADAR BEGAN TO SPOKE ON THE RIGHT SIDE OF THE SCREEN. DUE TO WEATHER INBOUND TO MSP, DECISION MADE TO DIVERT TO DTW WHERE THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WEATHER RADAR TRANSCEIVER, NO HELP. THE RADARMay 2, 1997 · N302US · Airbus A320211 · Weather Radar SystemSDR 9705403202Actuator · failedDURING APPROACH, RECEIVED F/CTL FLAPS LOCKED MESSAGE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT WING NR 2 ROTARY FLAP ACTUATOR, OPERATIONAL CHECK OK.Mar 12, 1997 · N302US · Airbus A320211 · Trailing Edge Flap ActuatorSDR 9705143202Actuator · lockedDURING APPROACH WHEN SELECTING FLAPS POSITION TWO, RECEIVED F/CTL FLAPS LOCKED MESSAGE. SLATS EXTENDED TO POSITION TWO. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURE AND SELECTED FLAPS THREE. SLATS REMAINED IN POSITON TWO. AIRCRAFT LANDED WITHOUT INCIDENT. MAIMar 12, 1997 · N302US · Airbus A320211 · Trailing Edge Flap ActuatorSDR 9705063202Computer · failedDURING APPROACH WHILE SELECTING FLAPS ONE, RECEIVED F/CTL FLAPS LOCKED MESSAGE. THE LEADING EDGE SLATS EXTENDED SATISFACTORILY, HOWEVER, THE FLAPS DID NOT REACH POSITION ONE. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 2 SLAT/FLAP CONTROL CMar 8, 1997 · N302US · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9705053202Computer · failedDURING CONFIGURATION FOR APPROACH, RECEIVED F/CTL FLAPS LOCKED MESSAGE. FLAPS LOCKED IN POSITION THREE OR LESS. FOLLOWED COCKPIT OPERATING MANUAL AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE NR 1 SLAT/FLAP CONTROL COMPUTER. OPERATIONAL CHECK OK.Mar 7, 1997 · N302US · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9702843202Actuator · lockedDURING APPROACH WHILE SELECTING FLAPS 1, RECEIVED F/CTL SLATS LOCKED MESSAGE WITH THE WING TIP BRAKE ACTIVATED. COMPLIED WITH COCKPIT OPERATING PROCEDURES. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT WITH SLATS RETRACTED AND FLAPS 3. MAINTENANCE FOUNDFeb 9, 1997 · N302US · Airbus A320211 · Leading Edge Slat ActuatorSDR 9625503202Retract Syst · locked upDURING APPROACH WHEN SELECTING FLAPS 2, RECEIVED F/CTL FLAPS LOCKED ALIGNMENT FAULT COMPLETED COCKPIT OPERATING MANUAL PROCEDURES AND LANDED WITH FLAPS 0. LANDING WAS ACCOMPLISHED WITHOUT INCIDENT. MAINTENANCE RESET NR 1 AND NR 2 SLAT FLAP CONTROL COMPUTERS,Dec 1, 1996 · N302US · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9627493202Longeron · corrodedDURING C-CHECK, THE FLOOR STRINGER AT FRAME 68, Y 1270 LEFT SIDE WAS FOUND WITH AREAS OF CORROSION. REPAIRED PER EA 32-106173.Nov 26, 1996 · N302US · Airbus A320211 · Fuselage Main, Longeron/StringerSDR 9623273202Power Supply · inoperativeDURING LINE MAINTENANCE CHECK OF THE EMERGENCY LIGHTS, THE FORWARD EMERGENCY LIGHTS WOULD NOT ILLUMINATE. REPLACED POWER SUPPLY, OPERATIONAL CHECK OK.Nov 3, 1996 · N302US · Airbus A320211 · Emergency LightingSDR 9609413202Brake Actuator · malfunctionedDURING APPROACH AFTER SELECTING FLAPS ONE POSITION, RECEIVED F/CTL SLATS LOCKED MESSAGE. THE WING TIP BRAKE ENGAGED. CREW FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, DECLARED AN EMERGENCY, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT WING SLApr 28, 1996 · N302US · Airbus A320211 · Leading Edge Slat Control 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 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 CARGMay 1, 1995 · N302US · Airbus A320211 · Cabin Cooling SystemSDR 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 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 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 Section
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