N920QS
Service difficulty reports not matched to an aircraft · 27
They name N920QS, 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 = 'N920QS' 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 = 'N920QS' 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 DXTA2016050406233Elevator · damagedIN DESCENT AT 15000 FT, ACFT SUFFERED A LT SIDE LIGHTNING STRIKE. BURN MARKS AT VARIOUS RIVETS ALONG FUSELAGE. LT SIDE HORIZONTAL STAB IS MISSING OTBD STATIC WICK. BURN & EXIT MARKS AT PORT SIDE OF HORIZONTAL STAB. COMPLIED WITH LIGHTNING STRIKE INSPECTIONSDR DXTA2015111306123Actuator · failedNOSE GEAR DID NOT CATCH ON UNLOCK AFTER TAKEOFF. PERFORMED GEAR BUMP TROUBLESHOOTING. NLG & LT MLG ARE FUNCTIONING NORMALLY. FOUND THE RT MLG UPLOCK ACTUATOR TO BE CYCLING UNCOMMANDED, FOLLOWING THE RETRACT CYCLE CAUSING RT GEAR TO HAMMER UP & DOWN IN THE SDR DXTA2015022305985Generator · failedON LANDING BELOW A SPEED PF 65 KNOTS THE RT ENG FAILED, DU4, DU5, FMS2 & RM2 WENT BLANK. R&R ENGINE GENERATOR & ACCOMPLISH SB750-24-24 IAW CE-750 AMM 24-30-00 & SB 750-24-24. REMOVED 2 EA PCB CARDS (PN 6918471-6 SN 0163 & 0164 AND REPLACED W/ 2 NEW PCB CARDSSDR DXTA2014100905908Apu · odorTHERE IS A BAD MUSTY ODOR COMING FROM THE A/C PACKS WHEN THE APU BLEED IS OPERATING ON THE GROUND. THE ODOR CLEARS AFTER ENGINE START & THE APU IS SHUTDOWN. PERFORMED A PRE-RUN CHECK & FOUND APU OIL LOW, SERVICED APU OIL. GAINED ACCESS TO THE APU BLEED AIR SDR DXTA2014072205827Connector · burnedDURING DESCENT, SMOKE EMITTED FROM THE GALLEY AREA. HEARD AN ELECTRICAL SIZZLING & SAW SMOKE COMING OUT OF THE GALLEY AREA ABOVE THE LIQUOR CABINET & ABOVE THE ADJACENT INDIRECT OVERHEAD LIGHT PANEL. TURNED OFF THE INTERIOR MASTER SWITCH & THE SMOKE STOPPSDR DXTA2013103105555Acm · odorDURING DESCENT FROM FL430, SMELLED SMOKE DURING POWER REDUCTION. ODOR TOOK PLACE EVERY TIME POWER WAS REDUCED. FOUND OIL RESIDUE TO LT WATER SEPARATOR DOME. CHECKED DUCTING IN BLEED AIR SYSTEM BETWEEN LT ENGINE AND COCKPIT ACM, NO OIL RESIDUE NOTED. REINSTASDR DXTA2012112605196Acm · seizedCABIN ACM IS MAKING A LOUD BEARING NOISE WHEN RUNNING. STRONG OIL ODOR ASSOCIATED IN THE CABIN WITH CABIN PACKS OPERATING. OIL ODOR IS STILL PRESENT AFTER PACKS HAS BEEN SHUTOFF FOR 10 MINUTES. BEARING NOISE STOPS WHEN CABIN PACK IS SHUTOFF. TROUBLESHOT, FOSDR DXTA2012062505012O-Ring · damagedAFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. GEAR HANDLE LOCKED IN THE DOWN POSITION AND WOULD NOT MOVE. NO OTHER ABNORMAL INDICATIONS. OUND NOSE STRUT NOT FULLY EXTENDED. REPACKED THE NLG STRUT AND SERVICED IAW MM 32-20-02. SWUNG GEAR, OPS & LEAK CHECKS SDR DXTA2012010604842Windshield · failed45 MINUTES INTO FLIGHT RECEIVED RT WINDSHIELD HEAT INOPERATIVE, THAN THE RT WINDSHIELD SHATTERED. REMOVED AND REPLACED CO-PILOTS WINDSHIELD IAW MM 56-11-00. COMPLETED CABIN PRESS. FUNCTIONAL CHECK IAW MM 21-00-00 WITH NO DEFECTS NOTED. COMPLIED WITH CO-PILOSDR DXTA2011020104441Acm · malfunctionedSMOKE COMING FROM CABIN REGISTERS AND CABIN PAC WILL NOT DECREASE IN SUPPLY TEMP LESS THAN 215 IN AUTO OR MANUAL. FOUND CABIN ACM SEIZED. REMOVED ACM, INSTALLED REPAIRED ACM. REPLACED CABIN AND COCKPIT COALESCER FILTERS. OPS CHECKED CABIN PAC, CHECKED GOOD.SDR DXTA2010110204285Acm · failedON INITIAL DESCENT, CREW & PAX NOTICED STRONG, PUNGENT ODOR (LIKE A STRUCK MATCH). ON REACHING A LOWER ALTITUDE, ISOLATED EACH PACK AND FOUND THE COCKPIT PACK TEMPERATURE TO BE UNCONTROLABLE IN AUTO & MANUAL. REMOVED AND INSTALLED COCKPIT ACM IAW MM 21-51-00SDR DXTA2008121403400Tube · misinstalledWING OVER FILL CAS MESSAGE ILLUMINATED IN FLIGHT. THE LT WING VENTED FUEL UNTIL SPEED WAS REDUCED FOR LANDING UPON INSP OF VENT SYS. FOUND TUBES 6726220-29 AND 6726220-30 INSTALLED ON WRONG SIDES WITH FLAPPER VALVE HANGING OPEN. REMOVED TUBES AND REINSTALLED SDR DXTA200809073265Bearing · wornAROUND 40 KTS ON T/O ROLL NOSE WHEEL STARTED TO SHIMMY. SHIMMY GOT WORSE THROUGH 60 KTS. ABORTED T/O. THIS WAS SEVERE-KNOCKED LWR YD OFF LINE + SHOOK OPEN DRAWERS IN THE CABIN. 9000 LBS FUEL, 7 PAX NO NOSE WHEEL PRESSURE. WHILE PERFORMING NOSE WHEEL SHIMMY MX SDR DXTA200807213186Wheel · vibrationSEVERE NOSE SHIMMY ON TAKEOFF. STARTED AS WE GAINED SPEED THRU EST 30-40 KTS. BY THE TIME WE ABORTED WE WERE AT APPROX 40-50 KTS. SUB:(M-2B). REMOVED AND REPLACED LT AND RT NLG WHEEL/TIRE ASSY, WITH OVERHAULED/NEW UNITS SERVICED NLG STRUT, REPLACED (2) EACHSDR DXTA200803186Landing Gear · vibrationSEVERE NOSE SHIMMY ON TAKEOFF. STARTED AS ACFT GAINED SPEED THRU EST 30-40 KTS. ABORTED AT APPROX 40-50 KTS. (A)SDR DXTA200702373Apu · smokeWHILE RUNNING APU ON THE GROUND WITH COCKPIT PAC ON HIGH GOT SMOKE IN COCKPIT. COCKPIT PAC SUPPLY TEMP ROSE RAPIDLY. COCKPIT PAC OIL RESEVOIR WAS CLEAR ON PREFLIGHT NOW BLACK. REPLACED COCKPIT PAC ACM & COALESCER SOCK OPS CK GOOD REF CE750 M/M 21-51-00.SDR DXTA200702232Hydraulic System · lowIN CRUISE (HYD VOLUME LOW A (CAS) MESSAGE ILLUMINATED HYDRAULIC QUANTITY OF A SYSTEM INDICATED 5 PERCENT. WE FOLLOWED CHECKLIST AND BLEW DOWN LANDING GEAR AND USED EMERGENCY BRAKES AND STEERING UPON LANDING. [06-15-07] REMOVED AND REPLACED NOSE WHEEL STESDR DXTA200701906Wheel · vibrationNOSE WHEEL SHIMMY BETWWEN 60-70 KNOTS. DURING TAKE-OFF ROLL. REMOVED AND REPLACED NR 1 AND 2 NOSE WHEEL ASSEMBLIES WITH AN OVERHAULED UNITS AND SECURED, LUBRICATED NOSE GEAR TORQUE LINKS AS NEEDED IAW CE750 MM CHAPTER 32-41-01.SDR DXTA200701903Wheel · vibrationSEVERE NOSE WHEEL SHIMMY ON TAKE-OFF ROLL UNDER 60 KTS. KICKED OFF LOWER YD. REMOVED AND REPLACED LEFT AND RIGHT NOSE WHEEL ASSEMBLYS IAW CESSBA MODEL 750 MM CHAP 32-41-01 PAGE 1-5.SDR DXTA200601823Wheel · vibratesDURING TAKEOFF A VIBRATION FROM THE NOSE WHEEL AREA WAS OBSERVED AND THE TAKEOFF WAS ABORTED. AMBER YD OFF LOWER CAS MESSAGE WAS DISPLAYED. REMOVED AND REPLACED BOTH NOSE WHEEL ASSEMBLIES IAW MM CH 32-41-01.SDR DXTA200601711Nut · looseSEVERE NOSE WHEEL SHIMMY AT 40 KTS IAS,REPEAT WRITE UP. YAW DAMPER DISCONNECTED. TAKEOFF ABORTED. RETORQUED UPPER BARREL NUT AND RETORQUED / LUBED UPPER AND LOWER TORQUE LINK HARDWARE IAW COMPONENT MM CHAPTER 32-20-02 FUNCTIONAL TEST OF NOSE STEERING SYSTEMSDR DXTA200601699Wheel · vibratesTAKEOFF ABORTED AT APPROX. 65 KTS DUE TO SEVERE NOSE WHEEL SHEEL SHIMMY. LOWER YAW DAMPENER AMBER CAS MESAGE ILLUMINATED, BUT DID RESET. TAKEOFF ROLL WAS NORMAL UNTIL THE ABORT. REPLACED BOTH NOSE WHEEL ASSY'S IAW MM 32-41-07, INSPECTED NOSE STRUT ASSY AND ATSDR DXTA200601607Wheel · vibratesON T/O ROLL AT 50 KTS NOSEWHEEL HAS EXCESSIVE SHIMMY. YAW DAMPNER KICKED OFF. T/O ABORTED. REMOVED AND REPLACED LT./RT. NOSE WHEEL/TIRE ASSY'S IAW M/M 32-41-01. OPS CHECKED GOOD.SDR DXTA200601320Electrical Sys · unknownUNABLE TO EXTEND GEAR NORMALLY DUE TO PREVIOUS ELECTRICAL PROBLEM (ABNORMAL CONDITION WITH THE CROSS TIE CLOSED RIGHT GEN ON APU OFF BATTERY NR 2 OFF EMERGENCY BUS WAS NOT POWERED NR 2 DC BUS SWITCH DID NOT INDICATE NORMAL OR EMERGENCY), EXTENDED GEAR MANUALLYSDR DXTA200500960Acm · failedABOUT 1 HOUR INTO OUR FLIGHT AT FL410, DETECTED AN ODOR IN THE COCKPIT THAT SMELLED ELECTRICAL IN NATURE. SYSTEMS WERE OPERATING NORMALLY AND THE SMELL DISSIPATED AFTER ABOUT 5 MINUTES THEN AFTER LANDING WITH THE APU RUNNING, DETECTED THE SAME SMELL. THE A/CSDR DXTA200500611Isolation Valve · openAFTER STARTING THE LEFT ENGINE, ON FIRST START OF THE DAY, A STRONG ODOR OF RAW FUEL COMES INTO THE COCKPIT. PACK ISOLATION VALVE WAS OPEN. AIR COMING FROM WEMAC SMELLED CLEAN.SDR DXTA200300004Circuit Board · failedUPON LANDING THE LT THRUST REVERSER DEPLOYED, BUT THE HANDLE WOULD NOT LET THRUST GO ABOVE IDLE.
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