N304US, cancelled Apr 8, 2009

Service difficulty reports · 26

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 = 'N304US' AND deregistration_id = 'N304US-2009-04-08'
  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 0602583204Battery Pack · inoperativeINOPERATIVE SEAT MOUNTED EMERGENCY ESCAPE LIGHTS, ROWS 8, 9, 10, 11. CORRECTED BY REPLACING 110WL2 BATTERY PACK. CHECKS OK.Dec 2, 2006 · N304US · Airbus A320211 · Emergency LightingSDR 0602383204Wire · brokenDURING EMERGENCY LIGHT CHECK, EXTERNAL LOAD FORWARD FAULTED. REPAIRED BROKEN SLIDE LIGHT POWER WIRE AT DOOR 1 LEFT HINGE AREA, CHECKS OK.Nov 6, 2006 · N304US · Airbus A320211 · Light System WiringSDR 0602373204Socket · corrodedDURING EMERGENCY LIGHT CHECK, LT EXTERNAL LOAD FAULTED. FOUND LT AFT OVERWING LIGHT ASSEMBLY AT FAULT. REMOVED CORROSION AND REPLACED OVERWING LIGHT ASSEMBLY. CHECKS OK.Nov 5, 2006 · N304US · Airbus A320211 · Emergency LightingSDR 0601673204Power Supply · faultyCIRCUIT BREAKER 5H (1WL, LIGHTING/EMERG LT/CABIN), POPPED DURING CLIMBOUT, FLIGHT COMPLETED UNEVENTFULLY. CIRCUIT BREAKER RESET, SYSTEM TEST DISPLAYED INT LOAD AFT LEFT, REPLACED AFT EMERGENCY LIGHT POWER SUPPLY (13WL). CHECKS GOOD.Jul 22, 2006 · N304US · Airbus A320211 · Emergency LightingSDR 0500683204Drive Shaft · brokenDURING TAKEOFF ROLL, THE NR 2 ENGINE EGT EXCEEDED 890C. TAKEOFF ABORTED AT 110 KNOTS. MAINTENANCE FOUND NR 2 ENGINE VBV INTER CONNECTING FLEX DRIVE SHAFT AT 9:00 BROKEN. MAINTENANCE REPOLACED FLEX DRIVE SHAFT.May 7, 2005 · N304US · Airbus A320211 · Compressor Bleed ValveSDR 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 9810843204Actuator · leakingDURING DESCENT, RECEIVED HYD R RSVR LOW LVL MESSAGE. CREW SHUT OFF GREEN HYDRAULIC PUMP, PTU, GRAVITY EXTENDED LANDING GEAR, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED LEAKING LEFT YAW DAMPER ACTUATOR. CHANGED HYD R RSVR LOW LVL TO HYD G RSVR LOW LVLDec 8, 1998 · N304US · Airbus A320211 · Autopilot SystemSDR 9811333204Battery Pack · dischargedMID CABIN AFT EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS. OPERATIONAL CHECK OK.Aug 7, 1998 · N304US · Airbus A320211 · Emergency LightingSDR 9801073204Retract Mech · malfunctionedDURING APPROACH WHEN FLAPS POSITION ONE SELECTED, RECEIVED F/CTL FLAPS LOCKED MESSAGE. DIVERTED TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE RIGGED FLAP SYSTEM, OPERATIONAL CHECK OK.Jan 16, 1998 · N304US · Airbus A320211 · Trailing Edge Flap Control SystemSDR 9711803204B-Nut · looseDURING CRUISE, RECEIVED HYD 'Y' RSVR LO LVL MESSAGE. FOLLOWED ECAM PROCEDURES AND DIVERTED TO ATL AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE YELLOW HYDRAULIC SYSTEM ACCUMULATOR 'B' NUT LOOSE. TIGHTENED 'B' NUT, LEAK AND OPERATIONAL CHECK OK.Jun 16, 1997 · N304US · Airbus A320211 · Hydraulic System, AuxiliarySDR 9711083204Warning · malfunctionedDURING TAKEOFF, RECEIVED FORWARD CARGO DOOR OPEN ECAM INDICATION. TAKEOFF WAS ABORTED WITH NO FURTHER INCIDENT. DOOR WAS CONFIRMED CLOSED AND DOOR INDICAITON WAS PLACED ON MEL.Jun 9, 1997 · N304US · Airbus A320211 · Door Warning SystemSDR 9702643204Battery · dischargedDURING LINE MAINTENANCE, FOUND THE AFT EMERGENCY LIGHT INOPERATIVE. REPLACED THE BATTERY PACK, OPERATIONAL CHECK OK.Feb 7, 1997 · N304US · Airbus A320211 · Emergency LightingSDR 9627473204Sill · corrodedDURING C-CHECK, CORROSION WAS FOUND ON THE INBOARD FLANGE OF THE RIGHT AFT DOOR SILL. REPAIRED PER EA 32-120550.Dec 13, 1996 · N304US · Airbus A320211 · Fuselage Miscellaneous StructureSDR 9625283204Window · shatteredDURING CLIMBOUT AT 16,000 FEET THE FIRST OFFICER'S NR 3 WINDOW OUTER PANE SHATTERED. AIRCRAFT DIVERTED TO MSP AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED WINDOW, OPS CHECK OK.Nov 24, 1996 · N304US · Airbus A320211 · Flight Compartment WindowsSDR 9610843204Flex Shaft · wornDURING CLIMB, THE NR 1 ENGINE EGT REACHED 892 DEGREES CELSIUS. RETARDED THRUST, EGT DECREASED, BUT WAS STILL 50 DEGREES CELSIUS GREATER THAN NR 2 ENGINE. RETURNED TO MSP AND LANDED WITHOUT FURTHER EVENT. GROUND MAINTENANCE INSPECTED ENGINE AND FOUND LOWER VMay 16, 1996 · N304US · Airbus A320211 · Compressor Bleed ValveSDR 9610073204Engine · vibrationDURING CLIMB AFTER FLAP RETRACTION, AN AIRCRAFT VIBRATION WHICH SEEMED TO FOLLOW NR 1 ENGINE RPM WAS FELT. AIRCRAFT RETURNED TO MSP. GROUND MAINTENANCE INSPECTION OF AIRFRAME REVEALED NO DISCREPANCIES. NR 1 ENGINE WAS GROUND RUN AND FAN TRIM BALANCE WAS PERMay 4, 1996 · N304US · Airbus A320211 · Engine (Turbine/Turboprop)SDR 9607933204Vbv · failedDURING TAKEOFF ROLL, ENG NR 2 COMPRESSOR VANE FAULT ANNUNCIATED. ABORTED TAKEOFF AT 80 KNOTS, AIRCRAFT RETURNED TO THE GATE. MAINTENANCE REPLACED THE VBV POSITION SENSOR AND RIGGED FOLLOW-UP ROD. FADEC AND TAKEOFF POWER CHECKS WERE ACCOMPLISHED.Apr 9, 1996 · N304US · Airbus A320211 · Compressor Bleed ControlSDR 9603503204Motor · leakingDURING CLIMBOUT, NOTICED AN ACCUMULATION OF NOXIOUS FUMES IN THE COCKPIT AND CABIN. CREW DONNED THE OXYGEN MASKS AND THE AIRCRAFT RETURNED TO MIA WITH EMERGENCY EQUIPMENT STANDING BY. AN UNEVENTFUL OVERWEIGHT LANDING WAS ACCOMPLISHED. MAINTENANCE FOUND THE Feb 12, 1996 · N304US · Airbus A320211 · Stabilizer Control SystemSDR 9521153204Smoke Det · malfunctionedDURING ENGINE START, RECEIVED 'SMOKE AFT CARGO SMOKE' WARNING. FOLLOWED COCKPIT OPERATING MANUAL PROCEDURES, DISCHARGED FIRE BOTTLE, RETURNED TO GATE AND DEPLANED PASSENGERS. MAINTENANCE INSPECTION REVEALED NO EVIDENCE OF FIRE OR SMOKE.Dec 20, 1995 · N304US · Airbus A320211 · Smoke DetectionSDR 9519963204Smoke Light · illuminatedDURING CRUISE, THE SMOKE LIGHT ON THE GEN 1 LINE PUSH BUTTON SWITCH ON THE FLIGHT DECK OVERHEAD PANEL ILLUMINATED ACCOMPANIED BY AN INTERMITTENT VENT EXTRACT FAULT. AIRCRAFT DIVERTED TO PIT AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO SIGN OF SMOKE OR FDec 8, 1995 · N304US · Airbus A320211 · Smoke DetectionSDR 9519953204Eel Power Supply · inoperativeCABIN EMERGENCY LIGHT CIRCUIT BREAKER POPPED ON THE OVERHEAD PANEL. MAINTENANCE REPLACED THE FORWARD EPSU AND BATTERIES. OPERATIONAL CHECK OK.Dec 8, 1995 · N304US · Airbus A320211 · Emergency LightingSDR 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 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 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.Aug 8, 1995 · N304US · Airbus A320211 · Compressor Bleed ControlSDR 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.May 7, 1995 · N304US · Airbus A320211 · Power LeverSDR 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 Engines
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