N114AX
Service difficulty reports · 24
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 = 'N114AX' AND registry_match = 'registration' 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 n_number = 'N114AX' AND registry_match = 'registration' 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 TIMA2023081131005Unknown · unknownTHE LEFT BLEED AIR FAILURE WARNING LIGHT CAME ON IN CRUISE. THE SMELL OF SMOKE, POSSIBLY FROM ELECTRICAL INSULATION, WAS ALSO PRESENT IN THE COCKPIT. WE MOVED THE LEFT BLEED AIR SWITCH TO INSTRUMENT AND ENVIRO OFF. AFTER CONSULTING 21-1-3 IN THE MEL WE DETERMSDR TIMA2019090600000Fire Loop · out of toleranceON TAKE OFF ROLL, L ENG FIRE WARNING ANNUNCIATOR ILLUMINATED. FOUND INTERNAL RESISTANCE OUT OF SPEC.SDR TIMA2018071900001Bearing · failedNR 1 WHEEL SEPARATED FROM AIRCRAFT AFTER TAKEOFF. THE INVESTIGATION FOUND WHEEL BEARING FAILURE AS THE CAUSE FOR SEPARATION.SDR TIMA20170628010Skin Panel · corrodedDURING A MAINTENANCE INSPECTION OF THE FUSELAGE EXTENSIVE CORROSION WAS DISCOVERED IN THE LOWER FUSELAGE SKIN ASSEMBLY. THE CONDITION WAS CORRECTED BY THE INSTALLATION OF NEW FUSELAGE SKIN PANELS.SDR TIMA20160923015Unknown · fumesDURING CLIMB OUT, PILOT DETECTED FUMES COMING FROM THE CARGO AREA. THERE WAS NO VISIBLE SMOKE, ONLY A BURNING ODOR. THE FUMES CONTINUED UNTIL CABIN WAS DEPRESSURIZED. WHEN THE CABIN WAS RE-PRESSURIZED THE FUMES DID NOT RETURN. AIRCRAFT LANDED UNEVENTFULLY.SDR TIMA20130818008Fcu · faultyRT ENGINE SLOWLY LOST TORQUE DURING CRUISE AT FL 200. ENGINE TORQUE EVENTUALLY FELL TO 0 AND ENGINE WAS SHUTDOWN. ACFT DIVERTED AND LANDED UNEVENTFULLY. PROBLEM WAS DETERMINED TO BE A FAULTY ENGINE FUEL CONTROL UNIT.SDR TIMA20120331005Cap · crackedAIRCRAFT WAS ON JACKS. WHILE CYCLING GEAR A LOUD POP WAS HEARD FROM THE NOSE LANDING GEAR ACTUATOR. EXAMINATION SHOWED A CRACK IN THE ACTUATOR END CAP AND HYDRAULIC FLUID LEAKAGE.SDR ACE030906Flange · corrodedMAINTENANCE FOUND CORROSION ON FORWARD SPAR LOWER CAP FORWARD FLANGE, IN THE CENTER FUSELAGE BAY, UNDER PREVIOUSLY REPLACED SEALANT. REPAIR REQUIRED REMOVAL OF CORROSION AND STRAP DOUBLER PER FR-CO FACTORY REPAIR DESIGN.SDR ACE112805Bearing · failedPILOT REPORTED RT GEN OFF LINE AND NO ENGINE STARTER AFTER LANDING - REPLACED STARTER/GENERATOR DUE FRONT BEARING FAILURESDR ACE101005Pump · leakingNR 2 ENGINE LEAKING FUEL FROM NACELLE. MAINTENANCE REPLACED LOW PSI FUEL PUMP DUE EXTRUDED VALVE BODY GASKET. FUEL WAS NOT DUMPED OVERBOARD AS THE VALVE BODY WAS LEAKING EXTERNALLY.SDR ACE091905Diaphragm · rupturedPIREP - FUEL OBSERVED DRIPPING FROM NR 1 ENGINE DRAIN MAST. VERIFIED LOW PSI FUEL PUMP DIAPHRAGM RUPTURE, THIS UNIT WAS IN COMPLIANCE WITH THE LATEST SB FOR DIAPHRAGM DESIGN.SDR ACE052405Diaphragm · rupturedPIREP - FUEL LEAKING FROM NR 1 ENGINE GANG DRAIN. REPLACED LOW PSI DUEL PUMP DUE RUPTURED DIAPHRAGM.SDR ACE050805Skin · crackedFOUND CRACKED BELLY SKIN WHILE PERFORMING TURBULENT AIR INSPECTION. CORROSION POSSIBLY ORIGINATING FROM OEM INSTALLATION OF UNPRIMED SHIM STOCK AT STRINGER JOINTS.SDR ACE020105Uplock Switch · malfunctionedGEAR WARNING REMAINED ON AFTER GEAR INDICATED THREE GREEN. PILOT DID A GO-AROUND AND ON NEXT GEAR EXTENSION, ALL INDICATIONS NORMAL. UNEVENTFUL LANDING. MAINTENANCE REPLACED NOSE GEAR UPLOCK SWITCH.SDR ACE120404Seat Track · corrodedDURING CAMP INSPECTION, MAINTENANCE LOCATED CORROSION ON SEAT TRACK FLOOR PANEL FLANGES. SEAT TRACK AND ADJACENT LOCALIZED CORROSION SUSPECTED TO HAVE BEEN CAUSED BY CARGO SPILLAGE. SEAT TRACK REPLACED, OTHER AREAS REPAIRED.SDR ACE103004Actuator · erraticPILOT REPORTED, AFTER 3 GEAR EXTENSION CYCLES AND THE QRH MANUAL EXTENSION PROCEDURE, NOSE GEAR GREEN LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE COULD NOT DUPLICATE (SUSPECT INTERMITTENT SWITCHES) AND REPLACED NOSE GEAR ACTUATOR.SDR ACE09242004Duct · contaminatedUNUSUAL ODOR EMANATING FROM AIR DUCTS WHEN BLEED AIR SYSTEM TURNED ON. RETURNED TO AIRPORT FOR INVESTIGATION, MAINTENANCE RECONNECTED MAIN HEATER DUCT IN BELLY (BELLY HAD CARGO SPILL RESIDUE IN AREA).SDR ACE09042004Spar · corrodedWHILE REPAIRING A FUEL LEAK IN THE RIGHT WING MAIN FUEL TANK, FOUND CORROSION ON THE MAIN SPAR LOWER CAP FORWARD FLANGE REQUIRING MAJOR REPAIR. THIS AREA WAS IDENTIFIED AS A SUSPECT CORROSION LOCATION IN RAYTHEON COMMUNIQUÉ NR 71.SDR ACE071504Roll Pin · shearedPIREP - COCKPIT DOOR HANDLE DOES NOT WORK FROM OUTSIDE. REPLACED SHEARED DOOR HANDLE ROLL PIN.SDR ACE032304Diaphragm · rupturedFOUND DIAPHRAGM LEAKING (RUPTURED) - THIS PUMP WAS BEING INSPECTED DUE TO AN ABORTED TAKEOFF AFTER ENGINE FLAME OUT. 1384 HOUR & 6 MONTHS AFTER INSTALL.SDR ACE032204Engine · flamed outNR 2 ENGINE FLAMED OUT ON TAKEOFF. ABORTED TAKEOFF. MAINTENANCE COULD NOT DUPLICATE.SDR ACE013104Indicator · failedPILOT REPORTED CAPTAIN'S ALTIMETER FAILED (FLAGGED) AT 600 FT AFTER TAKEOFF. RETURNED TO AIRPORT. MAINTENANCE REPLACED THE FAILED ALTIMETER.SDR ACE012504Diaphragm · rupturedMAINTENANCE NOTICED FUEL DRAINING FROM ENGINE GANG DRAIN - REPLACED LOW PSI FUEL PUMP DUE RUPTURED DIAPHRAGMSDR ACE091103Pump · leakingPILOT NOTICED FUEL LEAKING FROM ENGINE DRAIN ON PRE-FLIGHT. MAINTENANCE REPLACED THE DEFECTIVE PUMP.
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