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.

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 SHUTOFFJul 27, 2017 · N426QS · Gulstm GIV · Aircraft Fuel Distribution SystemSDR G02R20170322004Hinge · corrodedLEFT ELEVATOR NR 4 HINGE HAS CORROSION IN BOLT BORE.Mar 22, 2017 · N426QS · Gulstm GIV · Elevator StructureSDR G02R20170322003Attach Fitting · corrodedNR 4 ELEVATOR ATTACH POINT ON HORIZONTAL STABILIZER HAS CORROSION IN BORE.Mar 22, 2017 · N426QS · Gulstm GIV · Horizontal Stabilizer, Attach FittingsSDR G02R20170322002Attach Fitting · corrodedNR 4 ELEVATOR ATTACH POINT ON HORIZONTAL STABILIZER HAS CORROSION IN BOLT HOLE.Mar 22, 2017 · N426QS · Gulstm GIV · Horizontal Stabilizer, Attach FittingsSDR G02R20170322001Structure · corrodedRIGHT ELEVATOR NR 4 HINGE HAS CORROSION IN BOLT HOLE BORE.Mar 22, 2017 · N426QS · Gulstm GIV · Elevator StructureSDR 2017FA0000116Hinge · corrodedRIGHT HAND ELEVATOR, NUMBER 4 HINGE HAS CORROSION IN BORE.Mar 21, 2017 · N426QS · Gulstm GIV · Elevator StructureSDR 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" TRACKMar 7, 2016 · N426QS · Gulstm GIV · Trailing Edge FlapsSDR 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" TRACKMar 7, 2016 · N426QS · Gulstm GIV · Trailing Edge FlapsSDR 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 Mar 7, 2016 · N426QS · Gulstm GIV · Trailing Edge FlapsSDR 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 FITMar 7, 2016 · N426QS · Gulstm GIV · Trailing Edge FlapsSDR 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" Mar 7, 2016 · N426QS · Gulstm GIV · Trailing Edge FlapsSDR 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" Mar 7, 2016 · N426QS · Gulstm GIV · Trailing Edge FlapsSDR 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 "BMar 7, 2016 · N426QS · Gulstm GIV · Trailing Edge FlapsSDR 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 Mar 7, 2016 · N426QS · Gulstm GIV · Trailing Edge FlapsSDR DXTA2016030706196Support Fitting · corrodedLEFT FLAP TRACK SUPPORT FITTING A, CORROSION FOUND AT FLAP TRACK SUPPORT FITTING BOLT HOLE.Mar 7, 2016 · N426QS · Gulstm GIV · Trailing Edge FlapsSDR 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 REMOVDec 16, 2015 · N426QS · Gulstm GIV · APU Core EngineSDR 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 Sep 9, 2013 · N426QS · Gulstm GIV · Landing Gear Brake SystemSDR 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.Aug 8, 2010 · N426QS · Gulstm GIV · Buffet/GalleysSDR 142604082006Potentiometer · malfunctionedNWS FAIL MESSAGE APPEARS RIGHT BEFORE T/O.Apr 8, 2006 · N426QS · Gulstm GIV · Landing Gear Steering SystemSDR 142601012006Windshield · crackedRIGHT WINDSHIELD CRACKED.Jan 1, 2006 · N426QS · Gulstm GIV · Flight Compartment WindowsSDR 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.Aug 16, 2001 · N426QS · Gulstm GIV · Battery/Charger System
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