N939QS
Service difficulty reports not matched to an aircraft · 32
They name N939QS, 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 = 'N939QS' 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 = 'N939QS' 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 2019FA0000361Skin · corrodedLH AND RH WING PANELS EDDY CURRENT INDICATIONS OF CORROSION ON THE UPPER SURFACE. ACCOMPLISHED FLAP PEEN REPAIR IAW TEXTRON AVIATION ENGINEERING REPAIR MEMO DQ19509M1, DATED MAY 10, 2019.SDR DXTA2018041900161Skin · damagedRT WING TIP SKIN DAMAGED. REPAIRED IAW MEMO DQ11936M1.SDR DXTA2015092906093Coffeemaker · odorDURING GROUND OPS, PLASTIC BURNING ODOR OBSERVED IN CABIN. APPEARS TO BE CONCENTRATED IN THE AREA OF THE OVERHEAD LIGHTING VALANCE, DIRECTLY ABOVE THE GALLEY WORK TABLE. POWERED UP ACFT, INSPECTED AREA AROUND GALLEY, INCLUDING OVERHEAD LIGHTING. FOUND BURNISDR DXTA2015021805982Engine · leakingON BREAKING GROUND, PRIOR TO GEAR RETRACTION, FIRST OFFICER CALLED SMOKE IN COCKPIT, SMELLED ELECTRICAL. TURNED PAC'S OFF CHANGED NOTHING. APPEARED TO BE COMING FROM FIRST OFFICER`S SIDE OF COCKPIT. INSPECTED APU NO OIL NOTED. ISOLATED OIL ODOR SOURCE COMSDR DXTA2015012005963Coalescer Bag · odorIMMEDIATELY AFTER TAKEOFF, THE COCKPIT BEGAN TO FILL WITH SMOKE. AFTER TURNING COCKPIT PACK OFF, SMOKE SEEMED TO DISSIPATE. COMPLIED WITH A LIMITED BORESCOPE INSPECTION OF THE APU IMPELLER. NO DEFECTS NOTED. COMPLIED WITH APU OPERATIONAL CHECK IAW MM 49-10-SDR DXTA2014121505948Apu · failedODOR OF BURNING OIL IN COCKPIT ONLY. RAN APU, VERIFIED CREW DISCREPANCY. STRONG OIL ODOR FROM COCKPIT. RAN LT AND RT ENGINES. APU AIR HAS A NOTICEABLELY STRONG ODOR OF BURNING OIL. PERFORMED BOROSCOPE INSPECTION OF APU INLET. FOUND RESIDUE OF OIL ALONG COMSDR DXTA2014120805942A/C Pack · odorTHE AIR CONDITIONING PRESSURIZATION SYS IS EMITTING A STRONG, RANCID, CHEESE LIKE ODOR INTO THE CABIN. REMOVED THE COALESOR SOCKS FROM PACKS & CLEANED THE PACKS & WATER SEPARATOR. CLEANED AIR SUPPLY LINE FROM ACM TO PACKS ON BOTH SIDES. REMOVED ANY WATER FRSDR DXTA2014072905837Acm · odorSTRONG SMOKEY ODOR IN CABIN WHEN AIR IS TURNED ON. REMOVED AND REPLACED FWD ACM. OPS & LEAK CHECKED GOOD.SDR DXTA2014051405772Skin · corrodedREPAIR OF LT & RT LWR WING SKIN CORROSION. REPAIRED IAW CESSNA S-750-0193 13RD.SDR DXTA2014050205758Structure · gougedGOUGED NLG ACTUATOR TUNNEL. REPAIRED IAW S-750-0193 11RD.SDR DXTA2014022405665Power Supply · defectiveSTRONG ODOR ORIGINATING IN CABIN NEAR SEATS 5 & 6. ODOR SMELLS LIKE CHEMICALS OR HYDROCARBONS. REMOVED LT & RT PSU'S & INSPECTED ALL LIGHTS, POWER SUPPLIES & ELEC CONNECTORS. REMOVED LOWER FASCIA’S BY SEATS 5 & 6, INSPECTED ALL WIRING & ELEC CONNECTORS. FOSDR DXTA2013120205588Light · contaminatedTHE ODOR OF HOT PLASTIC OR HOT VINYL WAS NOTICED BY 4 CREW MEMBERS. THE ODOR IS MUCH STRONGER TOWARDS THE CEILING OF THE CABIN. THE STRONGEST ODOR COMING FROM THE CEILING BETWEEN SEATS 3 & 5. NO SMOKE IS NOTICED. DUCT SUPPLY TEMP IS 46 DEGREES TO THE CABIN SDR DXTA201307115442Unknown · unknownAFTER TAKEOFF, INTERMITTENT NOSE GEAR THUMPING SOUND FROM THE NOSE GEAR WAS NOTICED. UNLOCK LIGHT BLINKING. AT A LESSER FREQUENCY HAPPENED SEVERAL TIMES DURING FLIGHT. ON DESCENT AT ABOUT FL220 IS STARTED NON STOP. GEAR EXTENDED AT ABOUT 17000FT TO STOP IT.SDR DXTA2012082305103Squat Switch · out of adjustAFTER TAKEOFF, GEAR HANDLE SELECTED UP RED UNLOCK LIGHT ILLUMINATED, NOSE DOWN AND LOCKED LIGHT REMAINED ILLUMINATED, LT AND RT MAIN GEAR DOWN AND LOCKED LIGHTS EXTINGUISHED. WITNESSES ON THE GROUND SAID NONE OF THE GEAR RETRACTED. DURING INSPECTION, CYCLEDSDR DXTA2012081605097Pcb · malfunctionedGEAR FAILED TO RETRACT. UNLOCK LIGHT REMAINED ON. EXTENDED GEAR IAW CHECKLIST NORMALLY. LANDING UNEVENTFUL. JACKED AND PERFORMED SEVERAL GEAR SWINGS WHILE MONITORING NC002 PCB, USING PCB 60 BREAK OUT BOX. FOUND ALL POWER AND GROUND INPUTS CHECKED GOOD. T/S SDR DXTA2012010504840Float Valve · malfunctionedLEFT AND RIGHT WING TANKS DUMPING FUEL "WING TANK O'FULL LT & RT AMBER CAS MESSAGE. OBSERVED FUEL COMING OUT OF WING. FOLLOWED CHECKLIST AND TURNED TRANSFER PUMP OFF. LOST OVER 300 POUNDS OF FUEL. ONCE FUEL HAD BURNED TO 3000 LBS ON RT SIDE, TURNED CENTERSDR DXTA2011120604815Pdu · malfunctionedFLAPS FAIL AMBER EICAS MESSAGE CAME ON WHEN FLAPS SELECTED UP AFTER TAKE OFF. FLAPS VISUALLY APPEARED UP. CHECKLIST ITEMS COMPLETED. NO CHANGE. PERFORMED A STUCK FLAP LANDING. UNABLE TO REACH ERROR CODES IN AFT AVIONICS BAY. R & R POWER DRIVE UNIT WITH O/SDR DXTA2011042604562Fuel Cell · leakingWING TANK OVERFILL LT CAS MESSAGE. FUEL VENTED FROM LT WING TANK AT CRUISE FL 270 & NO TURBULENCE FOR APPROX 15 MINUTES. NORMAL CLIMB IN LIGHT TURBULENCE. YAWED ACFT TO STOP VENTING, NO SUCCESS. VENTING STOPPED AT APPROX 18000 FT. FUEL ABOARD 10000 LBS AT SDR DXTA2009092803801Transfer Valve · inoperativeAMBER CAS MESSAGE "WING OVERFILL-L" KEPT ILLUMINATING (3 TIMES). WITH ILLUMINATION LEFT WING VENTED FUEL. TROUBLE SHOOT TO BAD INBOARD AND OUTBOARD LEFT WING FUEL TRANSFER VALVES. REMOVED INBOARD AND OUTBOARD FUEL TRANSFER VALVES AND INSTALLED NEW FUEL TRANSFSDR DXTA200802808Squat Switch · inoperativeAFTER TAKEOFF, GEAR WOULD NOT RETRACT. REMOVED AND REPLACED NLG SQUAT SWITCH WITH A NEW UNIT ALL WORK PERFORMED IAW MM CH 32-60-00. ALSO REPACKED NLG WHEEL BEARINGS IAW MM CH 32-40-00.SDR DXTA200802754Actuator · failedAMBER CAS MESSAGE (PITCH FEEL FAIL) ILLUMINATES IF SPEED EXCEEDS 250K. TROUBLE SHOT DISCREPANCY TO FAILED RT PITCH FEEL ACTUATOR. REMOVED & REPLACED RT PITCH FEEL ACTUATOR IAW 750 M.M. CH. 27-33-00. OPS AND TRAVEL CHECK GOODSDR DXTA200702269Unknown · vibrationABORTED TAKEOFF, DUE TO VERY BAD NOSE WHEEL VIRBRATION. KNOCKED OFF YAW DAMP AND FGC. [07-09-07] REMOVED AND REPLACED BOTH NOSE WHEEL ASSY'S DUE TO VIBRATION CHECKED BALANCE OF NEW WHEEL ASSY. COMPLIED WITH NETJETS NOSE GEAR SHIMMY LIST NO DEFECTS NOTED ALLSDR DXTA200702151Yaw Damper · malfunctionedEICAS MESSAGES, YAW DAMPER OFF LOWER, YAW DAMPER NOT CENTERED. (MACH TRIM OFF) ILLUMINATED DURING THE TAKEOFF ROLL AFTER 40 KTS. [SUP 05-03-07] PERFORMED PITOT/STATIC LEAK CHECK AND FOUND NR 2 MADC PITOT FLEX LINE LEAKING. REPAIRED LINE IN ACCORDANCE WITH SDR DXTA200601647Hinge · bentGEAR "UNLOCK" LIGHT ON AFTER GEAR RETRACTION ON T/O. VISUALLY INSPECTED LANDING GEAR. FOUND RED PAINT STREAK ON L/R NLG DOOR + LARGE PAINT CHIP ALONG STREAK. IT WOULD APPEAR THAT SOMETHING STRUCK THE AIRCRAFT ON THE GROUND PRIOR TO TAKEOFF. FURTHER INSPECTISDR DXTA200601451O-Ring · blownIN LEVEL FLIGHT AT FL400, HYD VOLUME LOW A CAS MESSAGE CAME ON. OBSERVED THE VOLUME AT 14 PERCENT AND THE PRESSURE AT 2800 PSI. RAN THE CHECKLIST AND MADE A LANDING. THE EMERGENCY GEAR BLOW DOWN AND BRAKES WERE APPLIED. TROUBLESHOT TO BLOWN O-RING ON -A- SSDR DXTA200500864Warning Light · illuminatedPRIMARY STAB TRIM FAIL CAS MESSAGE. ITEM IS UNDER INVESTIGATION.SDR DXTA200500805Connector · contaminatedPRI STAB TRIM FAIL CAS MESSAGES IN FLT AT FL380, PRI STAB TRIM FAIL, A/P FAIL AND MACH TRIM OFF. CHECKED SYSTEM FOR PROPER OPERATION. COULD NOT DUPLICATE SQUAWK. REMOVED LT & RT HORIZONTAL STAB ACTUATOR ACCESS PANELS. FOUND WATER ON ALL CONNECTORS. CLEANESDR DXTA200400454Autopilot Sys · malfunctionedDURING GO AROUNDS (AFTER A COUPLE APPROACHES) THE AUTO-PILOT DISENGAGED MULTIPLE TIMES AFTER IT WAS RE-ENGAGED IN STABILIZED CLIMB/LEVEL OFF AND IN LEVEL FLIGHT. ON SECOND MISSED APPROACH BOTH FMS UNITS FAILED FOR ABOUT 30 SECONDS ALONG WITH THE AUTO-PILOT DISDR DXTA200400430Door Seal · leakingAFTER CRUISING AT FL 410 FOR APPROXIMATELY 1 HR, BAGGAGE DOOR SEAL CAS MESSAGE DISPLAYED. 15 MINUTES LATER, CABIN BEGAN TO CLIMB AT A RATE OF 1000' PER MIN WITH IN 1 MINUTE CABIN RATE INCREASED TO APPROX 6000' PER MINUTE. AMBER AND RED CABIN ALTITUDE CAS MESSDR DXTA200400421Solenoid · failedDURING INITIAL DESCENT WITH POWER REDUCTION, THE CABIN BEGAN TO CLIMB AT A RATE OF APPROX 2000 FPM. THE CABIN CONTINUED TO CLIMB AND CONTINUED TO DESCEND, THE CABIN ALT RED CAS ILLUMINATES, INITIATED EMERGENCY DESCENT FOR LOWER ALTITUDE. TROUBLESHOOT TO FAULSDR DXTA200300139O-Ring · leakingLT HYDRAULIC QUANTITY DROPPED TO ZERO 10 MINUTES AFTER TAKE-OFF. (A) SYSTEM UNLOADED, GEAR BLOW DOWN AND EMERGENCY BRAKE SYSTEMS ACTUATED. ACCOMPLISHED AIR TURN BACK TO CMH. - FOUND PLUG O-RING ON HYDRAULIC MANIFOLD LEAKING. REMOVED AND REPLACED O-RING, LEAK SDR DXTA200300040Resolver · inoperativeFLAPS FAIL AMBER CAS MESSAGE ILLUMINATED AND FLAPS INDICATOR JUMPED FROM 0-35 DEGREES IN LEVEL CRUISE FLIGHT ABOVE 250 KIAS ON 3 DIFFERENT OCCASIONS. - INSPECTED AND FOUND RESOLVER GROUND (GT048) LOOSE. TIGHTENED GROUND TERMINAL.
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