N947QS
Service difficulty reports not matched to an aircraft · 18
They name N947QS, 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 = 'N947QS' 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 = 'N947QS' 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 DXTA2011120504813Control Lever · failedLANDING GEAR FAILED TO RETRACT AFTER TAKEOFF. 3 GREEN INDICATIONS WITH GEAR HANDLE IN THE UP POSITION, WITH NO RED UNLOCK LIGHT. ALL HYD SYS NORMAL. INSTALLED ONE REPAIRED LANDING GEAR CONTROL HANDLE IAW MM 32-30-01. OPS CHECKS NORM IAW MM 52-80-20.SDR DXTA2011091904731Float Valve · stickingIN LEVEL CRUISE FLIGHT AT FL310, AMBER CAS "WING TANK OVER FILL R", CAME ON AND FUEL WAS VENTING OUT OF THE RT WING. THE CAS MESSAGE WENT OUT, FUEL STOPPED VENTING. THIS ISSUE REPEATED IT SELF TWICE DURING THIS FLIGHT. FOUND FUEL PANEL WITH RELIEF VALVE ISDR DXTA2011062204629Brake Sys · malfunctionedON LANDING ROLL OUT RT BRAKE IS GRABBING FOLLOWED BY A LOUD LONG "SQUEAK" AND VIBRATION. ON POST FLIGHT INSPECTION, THE BRAKE IS VERY HOT AND SMOKING. INSPECTED AND VERIFIED METERING VALVE WAS HITTING STOPS. CHECKED BRAKE HYD PRESSURES ON THE LT AND RT BRSDR DXTA2010113004337Flap System · failedFLAPS FAILED ON CLIMB OUT IN UP POSITION. WOULD NOT RESET IN AIR. SLATS WORKED. TROUBLESHOT, FOUND NO BITES ON CONTROLLER. OPERATED FLAPS DOWN, INSPECTED FLAPS, FOUND SAND TYPE MATERIAL ON INBD FLAP TRACKS. CLEANED AREA, OPERATED FLAPS 25 TIMES WHILE INSPECSDR DXTA2009040603581Bellcrank · stiffACFT REQUIRES LARGER THAN NORMAL INPUTS ON ROLL AXIS. PARTICULARLY NOTICEABLE AT SLOW SPEEDS DURING LANDING. DURING LANDING WITH 10 KT CROSSWIND, YOKE WAS AT LT STOP AND COULD NOT STOP ACFT ROLL. FOUND LT ROLL SPOILER PCU BELL CRANK STIFF. LUBRICATED AND CSDR DXTA2008122103429Tire · failedRT INBD MAIN TIRE BLOWN, RT OTBD MAIN TIRE BLOW. REPLACED NR 3 MAIN WHEEL ASSY WITH OVERHAULED UNIT, REPLACED NR 4 MAIN WHEEL ASSY WITH OVERHAULED UNIT FROM MM 32-42-00. WHEEL ASSY, MAIN PN 3-1537-2 SN 0726 HRS 116.9 CYC 93. PN 3-1537-2 SN 0511 HRS 332.2 CYC SDR DXTA2008122303429Tire · failedRIGHT INBOARD MAIN TIRE BLOWN. RIGHT OUTBOARD MAIN TIRE BLOW.SDR DXTA2008102703319Computer · failedFGC 2 FAIL IN FLIGHT. REMOVED AND REPLACED NR 2 AHRS UNIT IAW MM CHAP 34-21-01. OPS CHECK GOOD.SDR DXTA200702575Structure · damagedON TAKEOFF, NOSE WHEEL SHIMMY WAS ENOUGH TO CAUSE GYROS TO GO OFF LINE SO TAKEOFF WAS ABORTED. FOUND UPPER SCISSOR LT SIDE HARDWARE TO BE WORN. R & R HARDWARE WITH NEW IAW MM 32-20-00- NO OTHER DEFECTS NOTED.SDR DXTA200702384Switch · malfunctionedWHILE ENROUTE, AMBER FLAPS FAIL EICAS MSG ILLUMINATED. ALSO AMBER SYNOPTIC FLAP INDICATOR ILLUMINATED SHOWING FLAPS AT 10 DEGREES AND AIRSPEED READOUT WENT RED. FLAPS NEVER EXTENDED, SLATS DID WORK PROPERLY. REMOVED & REPLACED LEFT FLAP POSITION SWITCH WITH SDR DXTA200702329Controller · inoperativeIN CRUISE ALTITUDE OF FL200 MACH NR APPEARED. SELECTED C/O BUTTON ON AUTOPILOT PANEL AND THE BUTTON REMAINED IN THE DEPRESSED POSITION. NO OTHER MODES WERE ALLOWED TO BE SELECTED AND AUTO PILOT WOULD NOT RE ENGAGE. REMOVED AND REPLACED FLIGHT CONTROLLER GC-SDR DXTA200501071Igniter · inoperativeDURING ENGINE START, LEFT ENGINE HUNG AT 33 PERCENT AND DID NOT START. FUEL HAD BLOWN OUT THE BACK. COMPLETED STEPS 1 THRU 8 OF TASK 72-00-00-810 IAW RR AE3007C FIM. REMOVED & REPLACED CHANNEL B IGNITER IAW RR AE3007C MM 74-21-10-000-802.SDR DXTA200500986Pcu · bindingDURING ALL PHASES OF FLIGHT, AIRCRAFT HAD EXTREME RIGHT ROLL REQUIRED ABNORMAL LEFT AILERON TRIM WITH AUTO PILOT ENGAGED RETRIM L WING DOWN CAS MESSAGE ILLUMINATED WHICH REQURED MORE LEFT AILERON TRIM TO EXTINGUISH MESSAGE. TESTED AND FOUND TRIM SYSTEM BINDINSDR DXTA200500926Line · leakingEXCESSIVE BRAKE PEDAL PRESSURE NEEDED ON LANDING ROLL OUT. REQUIRED LARGER THAN NORMAL INPUT TO STOP AIRCRAFT. THIS WAS A DRY RUNWAY NOT CONTAMINATED. PERFORMED VISUAL INSPECTION OF BRAKES AND PLUMBING. PERFORMED POWER BRAKE BLEEDING IAW CITATION 750 MM CHSDR DXTA200500634Light · burned outON APPROACH TO 25L AT LAX, NOTICED NOSE GEAR LIGHT NOT ILLUMINATED. BLEW BOTTLE AND PULLED D-RING. DECLARED AN EMERGENCY AND LANDED UNEVENTFULLY. FOUND NOSE GEAR ANNUNCIATOR BULBS BURNT OUT. RELAMPED ANNUNCIATOR. BLED GEAR SYSTEM. SERVICED RESERVOIRS AS SDR DXTA200400285Odor · detectedAT FL410 STRONG ODOR OF SMOKE IN CABIN AND THE COCKPIT, SMOKE WAS COMING FROM BEHIND THE CAPTAIN’S CIRCUIT BREAKER PANEL AND OUT THE DEFROST HOLES JUST BELOW THE LEFT SIDE WINDOW. DEPLOYED O2 MASKS AND LANDED SAFELY. INSPECTED THE FOLLOWING AREAS FOR SIGNS OFSDR DXTA200300156Float · stuckAFTER TAKEOFF, AMBER CAS MESSAGE WING O FULL RT ILLUMINATED. FUEL CAN BE VISUALLY SEEN DUMPING OUT OF RIGHT WING FROM VICINITY OF SURGE TANK VENT. FUEL IMBALANCE BECAME EVIDENT AT A RATE OF APPROX 100 LBS PER MIN. PRESSURIZED RIGHT WING, FOUND NO LEAKS IN DSDR 20000511SH008Trunnion · looseLEFT NOSE LANDING GEAR TRUNNION LOOSE. THIS IS THE THIRD OCCURRENCE IN A FLEET OF APPROXIMATELY 25 AIRCRAFT. (X)
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