N662QS
Service difficulty reports not matched to an aircraft · 21
They name N662QS, 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 = 'N662QS' 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 = 'N662QS' 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 DXTA2018090401375Shutoff Valve · faultyDURING TAKE OFF 10KTS BEEFIER V1 AIRCRAFT PULLED HARD RIGHT, CORRECTED WITH FULL LEFT RUDDER MAINTAINED CONTROL, ROTATED MADE NORMAL CLIMB, CRUISE, DESCENT, LANDING OK. REMOVED AND REPLACED RUDDER BIAS ACTUATOR AND RUDDER BIAS CONTROL VALVE OPS AND LEAK CHECKSSDR JGVR201806132003Fitting · corrodedMECHANICALLY BLENDED FOUR AREAS OF CORROSION ON THE LT WING OTBD FLAP PUSHROD ATTACH FITTINGS, PERFORMED AN EDDY CURRENT INSPECTION AND AN ULTRASONIC THICKNESS INSPECTION. FOUND INBOARD FITTING BEYOND LIMITS. PROTECTED BARE METAL IAW SRM 51-10-02 TO AREAS WITSDR JGVR20180613002Axle · corrodedFOUND THE LEFT MAIN LANDING GEAR AXLE CORRODED OUT OF LIMITS, REPLACED THE AXLE.SDR JGVR20180612001Access Panel · corrodedCORROSION FOUND UNDERNEATH THE ACCESS PANEL 340CR, LOWER AFT ON THE RT SIDE OF THE VERTICAL STAB. BLENDED THE CORROSION, CLEANED, CHEMICALLY TREATED, AND PRIMED AREAS IAW ENGINEERING MEMO.SDR DXTA2015042006010Apu · smokeSMOKE IN THE COCKPIT. APU WAS STARTED ABOUT FIVE MINUTES PRIOR TO LANDING & WAS OPERATING NORMALLY. UPON LANDING & TAXI IN APU QUIT DURING ENG SHUTDOWN. WE THOUGHT WE HAD BUMPED A SWITCH. AFTER THE PAXS DEPARTED ABOUT FIVE MINUTES WE TESTED, GOOD TEST & RESDR DXTA2013072205452Bolt · wornWITH SPEED SLOWLY ACCELERATING PAST 265 KIAS AND IN CLIMB THROUGH FL235, A DEFINITE RUMBLING VIBRATION WAS FELT IN THE ACFT. NO SIGNIFICANT VIBRATION IN YOKE, BUT COULD CLEARLY SEE THE LT AILERON VIBRATING UP AND DOWN .2500". IMMEDIATELY SLOWED DOWN AND THESDR DXTA2013011805249Pulley · damagedDURING CLIMB OUT, ACFT SUDDENLY PITCHED NOSE DOWN. ON DETECTING THE PITCH CHANGE, AUTOPILOT WAS DISENGAGED. CONTROLS WERE DIFFICULT TO MOVE ALONG VERTICAL AXIS AND EACH CONTROL INPUT REQUIRED EXCESSIVE FORCE TO PITCH THE ACFT IN A CLIMB OR DESCENT. CONTROL SDR CWQR20110901018Control Cable · frayedFRAYED ELEVATOR TRIM CABLE WAS FOUND DURING A SCHEDULED INSP CABLE WAS FRAYED A HALF OF THE CABLE'S DIAMETER. AND CABLE TENSION WAS WITHIN MM LIMITS.SDR DXTA2011042504557Brake Assy · malfunctionedWHILE TAXIING THE BRAKES WERE APPLIED ON THE RT (CO-PILOTS) SIDE, THEY GRABBED ABRUPTLY & PULLED TO ONE SIDE & WOULDN'T RELEASE RIGHT A SECOND TRY PRODUCED SIMILAR RESULTS PULLING TO THE OPPOSITE SIDE. PILOTS SIDE WORKED NORMALLY. INSPECTED TIRE PRESSURES, SDR DXTA2011010504395Wheel · separatedNOSE WHEEL RIM ASSY SEPARATED WHILE BEING SERVICED. TECH USED HIGH PRESSURE TO SERVICE TIRE WITH NO REGULATOR. WHEEL & ATTACHING HARDWARE ARE UNSERVICEABLE. INSTALLED WHEEL , PERFORMED GEAR SWINGS. LEAK & OPS CHECKED GOOD IAW MM 12-14-00.SDR DXTA2010102804277Display · malfunctionedON CLIMB OUT, CO-PILOT'S PFD NR 2 WENT BLANK FOR 5 - 6 SECONDS, WITH CHECK PFD NR 2 ANNUNCIATOR ILLUMINATED & MASTER CAUTION. SCREEN CAME BACK ON WITH RED X FOR APROX 10 SECONDS, WITH CHECK PFD NR2 ANNUCIATOR ILLUMINATED WITH MASTER CAUTION. THEN SCREEN REBOOSDR DXTA201006014106Door · failedMAIN ENTRY DOOR HISS ON CLIMB OUT, DOOR OPENED IN FLIGHT UPON RETURN TO AIRPORT. NO DEFECTS WERE NOTED WITH THE DOOR LATCHING/WARNING SYS. NTSB INVESTIGATION IN PROGRESS, AWAITING CVR SUMMARY.SDR DXTA2010031504030Oil System · reads highAT CLIMB TO FL370. RT ENGINE OIL PRESSURE EXCEEDED RED LINE TO 190/200PSI. REDUCED THROTTLE & BEGAN TO DESCEND. AT FLT IDLE, OIL PSI STAYED ABOVE RED LINE UNTIL BELOW FL200. KEPT THROTTLE AT FLT IDLE. PSI HIGHER THAN LT ENGINE BUT STAYED IN GREEN AT 120PSI. ASDR DXTA200808043215Indicator · false indicationAFTER BRAKE RELEASE, LT ITT GAUGE WENT OFF SCALE HIGH. TAKEOFF WAS ABORTED AT LESS THAN 20 KNOTS. PRIOR TO BRAKE RELEASE, ALL ENGINE GAUGES RAD NORMAL AT FULL POWER. ENGINE GAUGES ON BOTH ENGINES CONTINUED TO REMAIN NORMAL EXCEPT FOR LT ITT GAUGE WHICH STAYSDR DXTA200807193188Coalescer Bag · contaminatedJUST PRIOR TO LEVEL OFF AT 15,000 FT, WE STARTED SMELLING A STRONG "BURNING" ODOR. AT LEVEL OFF, WITH POWER REDUCED, THE ODOR DISSIPATED. IT RECURRED ON APPROACH WITH POWER INCREASES. REMOVED, CLEANED AND DRIED, INSTALLED WATER SEPARATOR CONDENSER BAG IAW MM SDR DXTA20083188Unknown · odorJUST PRIOR TO LEVEL OFF AT 15,000 FT, STARTED SMELLING A STRONG "BURNING" ODOR. AT LEVEL OFF, WITH POWER REDUCED, THE ODOR DISSIPATED. ODOR RECURRED ON APPROACH WITH POWER INCREASES. (A)SDR DXTA200701865Circuit Breaker · openDURING TAKEOFF PRIOR TO V1, LT SIDE MASTER WARNING LIGHT CAME ON STEADY. RT SIDE MASTER WARNING DID NOT COME ON AT ALL. (WILL NOT RESET) ALL OTHER INDICATIONS NORMAL.SDR DXTA200601598Uplock Switch · out of rigTHE RED 'GEAR UNLOCKED' LIGHT WOULD NOT EXTINGUISH AFTER GEAR RETRACTION. RIGGED NOSE GEAR UPLOCK SWITCH FOR POSITIVE ACTUATION. COMPLETED SATISFACTORY FUNCTIONAL CHECKS IAW C560XL MM 32-30-05.SDR DXTA200501155Fuel Filter · bypassingRIGHT FUEL FILTER BYPASS LIGHT CAME ON WITH APPLICATION OF T/O POWER DURING TAKEOFF ROLL. REMOVED AND REPLACED RIGHT FUEL FILTER IAW P&W 545 M/M CH 73-10-05, OPS AND LEAK CHECKS SATISFACTORY.SDR DXTA200501042Fork · maladjustmentA -GEAR UNLOCK- LIGHT REMAINED ON AFTER TAKEOFF WITH THE GEAR IN THE -UP POSITION-, THE -HYD PRESS- LIGHT REMAINED ON AS WELL. REMOVED NLG STRUT PISTON ASSY. FOUND MEASUREMENT BETWEEN FORK AND BEARING ORIFICE ASSY TO BE AT 16 .0 IN. RETORQUED BEARING AND ORSDR DXTA200500624Support Bracket · damagedNO TAKEOFF LIGHT AND HORN CAME ON AT TAKEOFF POWER AND TAKEOFF ROLL INITIATION. FLAPS 15, SPEED BRAKE RETRACTED, TRIMS SET FOR T/O). FOUND RT SPEED BRAKE SWITCH JAM NUT BEING PUSHED UP BY SPEED BRAKE DOOR SUPPORT BRACKET, CAUSING PLUNGER TO RELAX. ADJUSTED
Back to N662QS