N436QS
Service difficulty reports not matched to an aircraft · 27
They name N436QS, 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 = 'N436QS' 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 = 'N436QS' 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 G02R20170802004Floorboard · puncturedFLOORBOARD PUNCTURED IN THE TOP SKIN OF FLOOR.SDR G02R20170724011Fitting · corrodedLEFT AND RIGHT HORIZ STAB PIVOT BUSHINGS AND LUGS CORRODED.SDR G02R20170724010Hinge Fitting · corrodedVERTICAL FIN, RUDDER HINGE, UPPER FITTING IS CORRODED.SDR G02R20170724009Hinge Fitting · corrodedVERTICAL FIN, RUDDER HINGE, CENTER FITTING IS PITTEDSDR G02R20170724008Hinge Fitting · corrodedVERTICAL FIN, RUDDER HINGE, LOWER FITTING IS PITTED.SDR G02R2017080100003Torque Tube · corrodedRUDDER TORQUE TUBE IS PITTED BEYOND THE ALLOWABLE DAMAGE LIMITSSDR G02R08012017002Hinge Fitting · corrodedRIGHT NR 4 ELEVATOR HINGE HAS PITTED CORROSION, TOP AND BOTTON CONTACT SURFACES.SDR G02R08012017001Hinge Fitting · corrodedRIGHT ELEVATOR HINGE LINE NR 1 ON HORIZONTAL STAB HAS PITTED CORROSION AND ELONGATION IN BOTTOM FITTING.SDR G02R07242017007Hinge Fitting · corrodedRT ELEVATOR HINGE LINE NR 4 CORRODED.SDR G02R20170724006Hinge · corrodedLEFT ELEVATOR HINGE CORRODED.SDR G02R20170724005Hinge Fitting · corrodedLT ELEVATOR HINGE LINE NR 4 CORRODED.SDR G02R20170724004Hinge Fitting · corrodedRIGHT ELEVATOR HINGE LINE NR 3 CORRODED.SDR G02R20170724003Hinge Fitting · corrodedLEFT ELEVATOR HINGE LINE NR 3 CORRODED.SDR G02R20170724002Hinge Fitting · corrodedRIGHT ELEVATOR HINGE LINE NR 2 HAS CORROSION.SDR G02R20170724001Hinge Fitting · corrodedLEFT ELEVATOR HINGE LINE NR 2 ON HORIZONTAL STAB HAS CORROSION BOTH FITTINGS.SDR GR4220160913001Fitting · gougedLEFT ENGINE AFT MOUNT FITTING HAS GOUGES AND SCRATCHES ON THE AFT VIBRATION ISOLATOR FITTING ON THE FORWARD FACE IN SEVERAL LOCATIONS.SDR DXTA2013110705560Apu · odorAIR CONDITIONING SYSTEM PRODUCED A DIRTY SOCK ODOR. REMOVED LEFT AND RIGHT WATER SEPARATOR COALESCER BAG AND INSTALLED NEW. COMPLIED WITH CMP 215005 AIR CONDITIONING SYSTEM OPS TEST WITH NO DEFECTS NOTED. THERE IS STILL AN ODOR PRESENT ONLY WHEN THE APU IS RSDR DXTA2012110505166Coalescer Bag · odorDURING CLIMB, NOTICED A VERY STRONG EXHAUST ODOR THROUGHOUT THE ENTIRE CABIN. THE ODOR TEMPORARILY FADED BUT REAPPEARED ABOUT 10 MINUTES INTO THE FLIGHT AND REMAINED. DONNED MASKS AND DROPPED PAX MASKS AND RETURNED TO DEPARTURE. AFTER LANDING THE ODOR WAS SSDR DXTA2011012704434Coalescer Bag · odorSTRONG EXHAUST & FUEL ODOR PREVALENT IN CABIN UPON DESCENT. ODOR WAS VERY STRONG AND WAS FIRST NOTICED ON DESCENT THROUGHOUT APPROXIMATELY 10,000FT. R & R WATER SEPARATOR BAGS . PERFORMED OPS AND LEAK CHECKS WITH NO DEFECTS OR ODORS NOTED. ALL WORK DONE IAWSDR N93A07232010Oven · odorABOUT 30 MINUTES INTO FLIGHT, THE F/A TURNED THE OVEN ON TO WARM SOME BREAD. WITHIN A FEW MINUTES SHE NOTICED THE AREA HAD AN ELECTRICAL BURNING ODOR AND AN ODOR OTHER THAN BURNED FOOD. SHE ALSO STATED SHE NOTICED SMOKE INSIDE THE OVEN DOOR WINDOW. THE OVEN SDR N93A04062010Safety Valve · malfunctionedDURING CLIMB, CABIN PRESURIZATION BECAME ERRATIC AND UNCONTROLABLE. CREW DESCENDED IMEDIATELY. CABIN LOW WARNING ILLUMINATED. OPEN.SDR N93A03222010Throttle Cable · brokenCREW REPORTED LT THROTTLE IS LOOSE AND INOPERATIVE. MX FOUND LT THROTTLE CABLE BROKEN UNDER FLOOR IN AFT LAV JUST FWD OF WHERE CABLE TURNS UPWARD AT AFT LAV AFT WALL. CABLE APPARENTLY HAD BEEN FRAYING ON STRUCTURE PRIOR TO BREAKING.SDR 143612282005Wire Harness · failedSTEER BY WIRE FAILURE ON LANDING ROLLOUT.SDR 14361216052Servo Valve · failedNOSE STEERING FAILED ON LANDING.SDR 1436121605Manifold · failedSTEER BY WIRE FAILED ON LANDING.SDR 1436120405Steering Sys · out of adjustSTEERING LAGS WHEN TURNED TO LT WITH TILLER OR RUDDER PEDALS. PERFORMED ADJUSTMENT CHECK IAW GIV MM 32-05-00.SDR 143612042005Steering Sys · malfunctionedSTEERING LAGS WHEN TURNED TO LT WITH TILLER OR RUDDER PEDALS. PERFORMED ADJUSTMENT CHECK IAW MM 32-05-00.
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