N426QS
Service difficulty reports not matched to an aircraft · 21
They name N426QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N426QS' AND registry_match IS NULL 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 = 'N426QS' AND registry_match IS NULL 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 DXTAT2PL6D0059ZEUValve · failedFUEL COCK WOULD NOT GO OFF ON RIGHT ENGINE. SEVERAL ATTEMPTS FAILED. AFTER TROUBLESHOOTING FUEL COCK HANDLE NOT SHUTTING OFF ON RIGHT ENGING. FOUND OPERATING LEVER ON HIGH PRESSURE FUEL SHUT OFF VALVE LOCKING UP. REMOVED RT ENGINE GIGHT PRESSURE FUEL SHUTOFFSDR G02R20170322004Hinge · corrodedLEFT ELEVATOR NR 4 HINGE HAS CORROSION IN BOLT BORE.SDR G02R20170322003Attach Fitting · corrodedNR 4 ELEVATOR ATTACH POINT ON HORIZONTAL STABILIZER HAS CORROSION IN BORE.SDR G02R20170322002Attach Fitting · corrodedNR 4 ELEVATOR ATTACH POINT ON HORIZONTAL STABILIZER HAS CORROSION IN BOLT HOLE.SDR G02R20170322001Structure · corrodedRIGHT ELEVATOR NR 4 HINGE HAS CORROSION IN BOLT HOLE BORE.SDR 2017FA0000116Hinge · corrodedRIGHT HAND ELEVATOR, NUMBER 4 HINGE HAS CORROSION IN BORE.SDR DXTA2016030706203Flap Track · corrodedRIGHT FLAP TRACK SUPPORT FITTING D, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "D" FLAP TRACK UPPER ASSEMBLY FOUND BUSHINGS TO MEASURE BEYOND LIMITS OF .6245 - .6255 PER DRAWING 1159WM20107. RT "D" TRACKSDR DXTA2016030706202Flap Track · corrodedRIGHT FLAP TRACK SUPPORT FITTING C, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "C" FLAP TRACK UPPER ASSEMBLY FOUND BUSHINGS TO MEASURE BEYOND LIMITS OF .7495 - 07505 PER DRAWING 1159WM20105. RT "C" TRACKSDR DXTA2016030706201Flap Track · corrodedRIGHT FLAP TRACK SUPPORT FITTING B, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "B" FLAP TRACK UPPER ASSEMBLY FOUND BUSHINGS TO MEASURE BEYOND LIMITS OF .8760 -.8770 PER DRAWING 1159WM20056. RT "B" TRACK SDR DXTA2016030706200Flap Track · corrodedRIGHT FLAP TRACK SUPPORT FITTING A, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "A" FLAP TRACK UPPER ASSEMBLY FOUND BUSHINGS TO MEASURE BEYOND LIMITS OF .6245-.6255 PER DRAWING 1159VVM20054. NEW UPPER FITSDR DXTA2016030706199Flap Track · corrodedLEFT FLAP TRACK SUPPORT FITTING D, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "D" FLAP TRACK UPPER ASSEMBLY FOUND BUSHINGS TO MEASURE BEYOND LIMITS OF .6245-.6255 PER DRAWING 1159WM20107. REMOVED LT "D" SDR DXTA2016030706198Flap Track · corrodedLEFT FLAP TRACK SUPPORT FITTING C, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "C" FLAP TRACK UPPER ASSEMBLY FOUND BUSHINGS TO MEASURE BEYOND LIMITS OF .7495-.7505 PER DRAWING 1159WM20105. REMOVED LT "C" SDR DXTA2016030706197Flap Track · corrodedLEFT FLAP TRACK SUPPORT FITTING B, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF "B" FLAP TRACK UPPER ASSEMBLY FOUND BUSHINGS TO MEASURE BEYOND LIMITS OF .8760-.8770 PER DRAWING 1159WM20056. LT FLAP TRACK "BSDR DXTA2016030806196Support Fitting · corrodedLEFT FLAP TRACK SUPPORT FITTING A, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE. AFTER CORROSION WAS REMOVED FROM BORE OF A FLAP TRACK UPPER ASSEMBLY FOUND BUSHINGS TO MEASURE BEYOND LIMITS OF .6245-.6255 IAW DWG 1159WM20054. INSTALLED LT A TRACK SDR DXTA2016030706196Support Fitting · corrodedLEFT FLAP TRACK SUPPORT FITTING A, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE.SDR DXTA2015121706139Apu · unserviceableDURING POST FLIGHT, ACFT CABIN FILLED WITH ENVIRONMENTAL SYS SMOKE. SWITCHED OFF THE APU AIR & AFTER 15 MINUTES THE SMOKE DISSIPATED.
REMOVED ACCESS PANELS, REMOVED CANNON PLUGS, DISCONNECTED ALL DRAIN LINES. REMOVED BOLTS FOR APU MOUNTING BRACKET AND REMOVSDR DXTA2013091005497Brake · malfunctionedDURING LANDING, LT PEDAL BRAKE PRESSURE DROPPED AROUND 95KTS, LT BRAKE GRABS AND LT BRAKE TEMP ROSE TO 200 DEGREES C, WHILE THE RT SIDE REMAINS AROUND 80 DEGREES C. CLEANED LEFT BRAKES OF DEBRIS. BLED BRAKES IAW CMP 324265. PERFORMED HYDROMECHANICAL ANALOG SDR N93A08082010Microwave Oven · smokeF/A WAS HEATING PLATES IN THE MICROWAVE OVEN AND SMOKE AND ELECTRICAL SMELL WAS EMITTING FROM THE OVEN. DISCONTINUED USE AND PULLED CIRCUIT BREAKER AND COLLARED. SUSPECT CAUSE WAS METAL ON PLATES.SDR 142604082006Potentiometer · malfunctionedNWS FAIL MESSAGE APPEARS RIGHT BEFORE T/O.SDR 142601012006Windshield · crackedRIGHT WINDSHIELD CRACKED.SDR GAC081601Charger · failedDURING NORMAL MAINTENANCE WHILE ON THE GROUND THE BATTERY CHARGER BEGAN TO SMOKE AND THE CIRCUIT BREAKER POPPED. REMOVED AND REPLACED BATTERY CHARGER WITH REPAIRED UNIT.
Back to N426QS