N933QS
Service difficulty reports not matched to an aircraft · 29
They name N933QS, 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 = 'N933QS' 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 = 'N933QS' 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 DXTA2014071405816Line · brokenWHEN GEAR HANDLE WAS SELECTED TO UP POSITION, AMBER HYD QTY LOW MESSAGE ILLUMINATED FOLLOWED BY THE A PUMP FAIL & PTU FAIL MESSAGES. FOLLOWED EMERGENCY CHECKLIST & RETURNED TO DEPARTURE. GEAR DID NOT RETRACT & THREE GREEN & UNSAFE LIGHTS REMAINED ON. ON PSDR DXTA2014021705658Skin · corrodedCORROSION FOUND ON RT UPPER WING SKIN AT THE WING TO FUSELAGE FAIRING SEAM. CORROSION ON RT WING UPPER AFT SKIN FOUND TO BE OUT OF LIMITS. REPAIRED CORROSION ON RT UPPER WING SKIN AT THE WING TO FUSELAGE FAIRING SEAM BY INSTALLING A REINFORCING DOUBLER FABRISDR DXTA2013031805319Acm · failedBURNING ODOR COMING FROM COCKPIT. TURNED COCKPIT PACK OFF AND ODOR DISSIPATED. R & R AFT ACM IAW MM 21-51-00. ACM OPS & LEAK CHECKS GOOD.SDR DXTA2013021505289Downlock Switch · intermittentWHEN GEAR HANDLE WAS SELECTED TO THE DOWN POSITION FOR LANDING, MAIN GEAR INDICATIONS WERE GREEN, NOSE GEAR DID NOT INDICATE GREEN. UNLOCK LIGHT WAS NOT ILLUMINATED. FOLLOWED THE CHECKLIST PROCEDURE WHICH DIRECTED US TO BLOW THE GEAR DOWN AND PULL THE NOSE GEASDR DXTA2012062805020Spar Cap · damagedON DISASSEMBLY UPPER SPAR CAP PANEL, DOUBLE DRILLED HOLE IN INBD SIDE OF EHS 66.5 HINGES SUPPORT ASSY .SDR DXTA2012062805019Skin · corrodedCORROSION REMOVED FROM PANEL LAND AT ACCESS HOLE 521 FB TO MAX DEPTH OF .080 EXCEEDS SPEC COMPLETED EDDY CURRENT NDI IAW 20-00-02. NO CRACKS DETECTED. ACCOMPLISHED REPAIR IAW ENGINEERING REPAIR DEFINITION S-750-0133-13RD REF TO FAA 8100-9 DATED 5-25-12. LEASDR DXTA2012062905018Access Panel · corrodedCORROSION REMOVED FORM PANEL LAND AT ACCESS HOLE 512 TO MAR DEPTH OF .123 EXCEEDS SPEC. COMPLETED EDDY CURRENT NDI IAW NDT MAIN 20-00-00 NO CRACKS DETECTECED. FLAP OPENED DONE IAW PO 2/21 TREATED AND PRIMED FILLED WITH 9394 SANDED ALODINED AND PRIMED, ACCOMSDR DXTA2011052704593Wheel · wornDURING TAKEOFF ROLL, AT APPROX 50 KNOTS, A SEVERE VIBRATION DEVELOPED IN THE NOSE GEAR AND THE TAKEOFF WAS ABORTED. R & R NOSE WHEELS IAW MM 32-41-01. TORQUED, SERVICED AND SAFTIED AS REQUIRED.SDR DXTA2010061004119Uplock Switch · out of adjust5 TIMES IN OUR 1.3 HR FLIGHT, WE HAD THE NOSE GEAR BUMP. 3 TIMES DURING CLIMB OUT & 2 TIMES DURING CRUISE. PERFORMED LANDING GEAR BUMP TROUBLESHOOTING PROCEDURE. FOUND BOTH MAIN GEAR UPLOCK SWITCHES OUT OF ADJUSTMENT. ADJUSTED SWITCHES. OPS CHECK NORMAL. WORSDR DXTA2009102103820Acm · seizedON THE GROUND AND APU RUNNING, SEVERAL SECONDS AFTER ISOLATION VALVE OPENED SMOKE APPEARED IN THE COCKPIT WITH AN OILY SMELL.SDR DXTA2009050403631A/C Pack · odorSMOKE IN COCKPIT. WHEN PAC'S TURNED ON A BURNED MILDEW ODOR AND HAZE STARTED TO BUILD UP IN COCKPIT. PAC'S SWITCHED OFF AND ODOR / HAZE DISSIPATED. FOUND COCKPIT ACM SIEZED. REMOVED AND REPLACED COCKPIT ACM WITH SERVICEABLE UNIT.SDR DXTA200803116Actuator · faultyDURING CLIMB OUT PASSING THROUGH FL180 AND 250 KIAS THE UPPER RUDDER BEGAN TO OSCILLATE, THIS WAS PHYSICALLY NOTICABLE IN THE AIRFRAME. TROUBLESHOT AND FOUND UPPER RUDDER ACTUATOR TO BE FAULTY. REPLACED UPPER RUDDER ACTAUTOR PERFORMED UPPER RUDDER SYS ADJUSTMSDR DXTA200803058Actuator · inoperativeDURING CLIMB AND CRUISE, RUDDER OSCILLATES INTERMITTENTLY WITH UPPER RUDDER (A) SELECTED. REMOVED UPPER RUDDER ACTUATOR- INSTALLED A REPAIRED ACTUATOR. PERFORMED OPERATIONAL AND LEAK CHECK WITH SATISFACTORY RESULT. TRAVEL CHECKS NORMAL, MAINTENANCE PERFORMED SDR DXTA200802965Actuator · inoperativeAFTER TAKEOFF, WHILE ACCELERATING THROUGH 240 KIAS AT5000 FT, PITCH FEEL FAIL CAS MESSAGE ILLUMINATED. REMOVED RT PITCH FEEL ACTUATOR AND REPLACED IAW MM 27-33-00. ALL OPS CHECKS IAW MM 27-30-00. ALL CHECKS GOOD.SDR DXTA20082965Actuator · malfunctionedAFTER TAKEOFF, WHILE ACCELERATING THROUGH 240 KIAS AT5000 FT, PITCH FEEL FAIL CAS MESSAGE ILLUMINATED. REMOVED RT PITCH FEEL ACTUATOR AND REPLACED IAW MM 27-33-00. ALL OPS CHECKS IAW MM 27-30-00. ALL CHECKS GOOD.SDR DXTA200702735Controller · malfunctionedAFTER TAKEOFF, FLAP FAIL CAS MESSAGE DISPLAYED WITH THE FLAPS AT 0*. FOUND BITS 2 TRIPPED ON FLAP CONTROLLER. RESET FLAP FAIL BUTTON ON SECOND ATTEMPT. THE FLAPS FULLY RETRACTED EXTENDED FLAPS TO 35* POSITION. INSPECTED FLAP TRACKS AND FOUND ICE WAS KEEPING FSDR DXTA200702642Acm · smokeAFTER LANDING DURING TAXI IN, A SLIGHT BURNING RUBBER ODOR WAS NOTICEABLE. ( BOTH ENGINES AND APU RUNNING) AFTER ENGINE SHUTDOWN, APU STILL ON, THE ODOR GOT VERY STRONG AND CABIN STARTED TO FILL WITH SMOKE. ODOR AND SMOKE CLEARED AFTER COMPLETE SHUTDOWN. RESDR DXTA200702438Resolver · failedDURING DESCENT THROUGH 15,000 AT 340 KIAS, THE FLAP FAIL CAS, AMBER FLAP SYNOPTIC AND FLAPS RESET LIGHT CAME ON. AFM PROCDURES WERE FOLLOWED. SLATS EXTENDED, BUT FLAPS DID NOT. VERIFIED FLAPS INOP ON INITIAL OPS CHECK. CONNECTED FLAP SYSTEM BREAKOUT BOX. FOUSDR DXTA200702287Unknown · unknownMASTER WARNING ILLUMINATED DURING TAKEOFF ROLL JUST ABOVE 80 KTS. [07-12-07] REPLACED LOWER YAW DAMP "B" ACTUATOR AND OPS CHECKED IAW 750 M/M 27-24-00.SDR DXTA200702082A/C Pack · odorGETTING A BURNING ODOR IN THE CABIN AND COCKPIT, POSSIBLE PACK IS FAILING. REMOVED AND INSTALLED NEW COALESCER IN BOTH THE COCKPIT & CABIN WATER SEPERATORS. RAN APU AND OPS CHECKED AND LEAK CHECKED GOOD. WORK DONE I.A.W. CE 750 AMM CHAPTER 21-51-00SDR DXTA200601407A/C Pack · failedDURING ENGINE START WE SMELLED A VERY STRONG, PUNGENT ENVIROMENTAL ODOR. SUSPECT COCKPIT PAC FAILURE. VERIFIED COCKPIT PAC FAILED.REMOVED AND REPLACED COCKPIT ACM IAW MM 21-51-00. OPERATIONAL AND LEAK CHECK GOOD.SDR DXTA200601390Pump · failedDURING CLIMB OUT RT HYD PRESSURE INDICATED AMBER AT 3300 LBS. LOW HYD VOLUME AND LOSS OF SYSTEM PRESSURE FOLLOWED. RT HYDRAILIC PUMP HAS FAILED, REMOVED PUMP AND INSTALLED OVERHAULED PUMP. PURIFIED (B) HYDRAULIC SYSTEM AND INSTALLED NEW PRESSURE, RETURN AND CSDR DXTA200601323Strut · malfunctionedAFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. LANDING GEAR HANDLE WOULD NOT MOVE FROM A/C DOWN POSITION. CHECKED AIRCRAFT, FOUND NOSE STRUT NOT FULLY EXTENDED, DISASSEMBLED NOSE STRUT. REMOVED AND REPLACED STRUT ORIFICE WITH NEW. RE-SEALED AND SERVICED STSDR DXTA200601299Position Switch · looseAFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT. LANDING GEAR HANDLE WAS STUCK IN THE DOWN POSITION. FOUND NOSE GEAR TORQUE LINK SQUAT CAM LOOSE. SECURED AND ADJUSTED CAM. CHECKED NOSE GEAR SQUAT SWITCH ADJUSTMENT, FOUND NORMAL. LANDING GEAR EXTENSION AND RSDR DXTA200601267Flap System · failedAT 19,000 MSL AND 220 IAS SELECTED FLAPS TO 5 DEG. FLAPS FAIL CAS MESSAGE APPEARED WITH AMBER FLAP POSTION INDICATOR UNABLE TO RESET FLAPS AND LANDED WITH SLATS EXTENDED FLAPS 0 DEG. TROUBLESHOT FLAPS, FOUND NO FAULT CODES ON CONTROLLER. FLAPS ELECTRICLAL RSDR DXTA200500786Landing Gear · malfunctionedLANDING GEAR BUMP THROUGH 15,000 FT, NO UNLOCK LIGHT INDICATED. COULD NOT DUPLICATE PROBLEM ON GROUND. CARRIED OUT T/S. MADE ADJUSTMENTS TO R/S CLEAR UPLOCK SWITCH. MLG SYSTEM OPS CHECK GOOD. COMPLIED WITH GEAR BUMP TROUBLESHOOTING IAW CE 750 MM. INSTRUCTED SDR DXTA200500580Autopilot Sys · malfunctionedDURING CRUISE, AUTOPILOT INPUTS FOR AILERON & UPPER RUDDER CONTROL OSCILLATES CONTINUOUSLY. TURBULENCE INCREASES THE INTENSITY & FREQUENCY OF OSCILLATIONS. APPLIED PRESSURE ON FLT CONTROLS (AILERON & RUDDER PRESSURE). ON CONTROL PANEL SYNOPTIC AILERON MOVESSDR DXTA200300103Controller · failedDURING DESCENT AT APPROX 13000 FT, (FGC A FAIL) MESSAGE ON EICAS, FOLLOWED SHORTLY AFTER BY SMOKE ODOR AND (TRIM SW FAIL L) ON EICAS. EVENT BUTTON WAS CYCLED. TROUBLESHOT AND FOUND THE F/O’S FLIGHT GUIDANCE CONTROLLER GC-810 FAILED. REMOVED AND REPLACED F/O CSDR DXTA200300069Downlock Switch · inoperativeRIGHT MAIN LANDING GEAR INDICATION REMAINED GREEN AFTER GEAR WAS RETRACTED, USED EMERGENCY BLOW DOWN GEAR. LANDING WAS UNEVENTFUL. DETERMINED THE RIGHT GEAR ACTUATOR DOWNLOCK SWITCH WAS FAULTY, REMOVED AND REPLACED WITH NEW SWITCH, PERFORMED GEAR OPERATION
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