N924QS
Service difficulty reports not matched to an aircraft · 18
They name N924QS, 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 = 'N924QS' 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 = 'N924QS' 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 DXTA2011102104759Downlock Switch · malfunctionedON DESCENT THROUGH APPROX 13,000' CREW NOTICED THE NOSE GEAR GREEN LIGHT ILLUMINATED WHILE GEAR WAS IN THE RETRACTED POSITION. NO GEAR RED LIGHT OR ANY OTHER INDICATIONS WERE PRESENT INDICATING THE NOSE GEAR WAS DOWN. NOSE GEAR GREEN LIGHT REMAINED ILLUMINATSDR DXTA2010041604068Unknown · unknownACFT DOES NOT TAXI WITHOUT OCCASIONALLY ADDING POWER. EVEN AT LIGHT WEIGHTS. AS THOUGH THE BRAKES ARE DRAGGING SLIGHTLY. INSPECTED BRAKE WEAR INDICATORS & FOUND TO BE WITHIN LIMITS. TAXIED ACFT & APPLIED EQUAL PRESSURE DURING TAXI & A/C BRAKES EVENLY. APPLIEDSDR DXTA2009073003748Pump · leakingLOST HYD B SYS QUANITY IN FLIGHT RAN CHECKLIST AND UNLOADED THE B PUMP. FOUND THAT RT ENG HYD PUMP FAILED. REMOVED HYD PUMP AND INSTALLED REPAIRED UNIT (REF WO 29760 1.15) PRIMED PUMP, BLED HYD SYS B, RAN ENGINES, AND FOUND NO LEAKS AT THIS TIME AND HYD SYS BSDR DXTA2009010103454Servo Drive · inoperativeDURING DESCENT, AUTOPILOT BEGAN TO ASCILLATE (ROLL). DISENGAGED THE AUTOPILOT. AFTER LEVELING AR 15,000, WE ATTEMPTED TO RE-ENGAGE THE AUTOPILOT, BUT WERE UNABLE. CONCURRENTLY, THE "YD FAIL LOWER B" CAS MESSAGE WAS OBSERVED. AUTOPILOT WOULD NOT ENGAGE. ONSDR DXTA200901020345AAutopilot Sys · oscillatesDURING DESCENT, AUTOPILOT BEGAN TO OSCILLATE.SDR DXTA200702516Wheel · out of balanceDURING TAKE OFF ROLL AT APPROXIMATELY 60 KIAS THE NOSE WHEEL SHOOK VIOLENTLY. DUST WAS COMING OUT OF THE HEAD LINER. ABORTED T/O. REMOVED AND REPLACED BOTH NOSE WHEEL ASSY, IAW CESSNA 750 M/M 32-41-01.SDR DXTA200702319Air Data Module · intermittentMACH TRIM AND YAW DAMPER DISENGAGED ON TAKEOFF AT 70-75 KTS. (2) ATTEMPTED TAKEOFFS. (M2B) REPLACED NR 2 MADC DUE TO INTERMITENT SPLITS. IAW MM 34-12-00. IAW FAR 91.411 + 91-413. OLD P/N: 7014700-607, OLD S/N: 0316642. NEW P/N: 701-4700-607. NEW S/N: 9909SDR DXTA200702103Pitot Line · obstructedON TAKEOFF, JUST PRIOR TO 80 KNOTS, GOT AMBER MASTER CAUTION AND AMBER YAW DAMPNER OFF LOWER CASE MESSAGE. [SUP 4-19-07] PULLED FAULT CODES 0300 05: AIRDATA MISCOMPARE. FOUND WATER IN PITOT LINES. PURGED LINES PITOT & STATIC. PERFORMED ALTITUDE CORRELATION SDR DXTA200702047Brake Assy · smokeDURING TAXI THE BRAKES STARTED TO DRAG AND MAKE A GRINDING NOISE. UPON VISUAL INSPECTION, THE RT OB BRAKE WAS SMOKING AND ALSO VERY HOT. REMOVED NR 4 MLG WHEEL ASSY. INSPECTED BRAKE FOR DAMAGE AND FOD. NO DEFECTS FOUND. BRAKE SPUN FREELY. BLED NR 4 BRAKE ASSYSDR DXTA200701839Pitot Tube · contaminated(YD OFF LOWER) AND MACH TRIM OFF OCCURED DURING TAKEOFF, ABORTED TAKEOFF AND COMPLIED WITH CHECKLIST. SECOND ATTEMPT, IDENTIICAL MESSAGES APPEARED. FOUND WATER IN BOTH PITOT TUBES. PURGED SYSTEM AND PERFORMED PITOT LEAK CHECK IAW MM 34-11-08 AND FAR 91-411- SYSDR DXTA200601825Landing Gear · unwanted extendWHILE DESCENDING, AT 8000 FT AND 230 KTS, NOSE GEAR MOMENTARILY EXTENDED AND THEN RETRACTED. NO OBVIOUS DAMAGE NOTED ON POST FLIGHT. COMPLIED WITH GEAR BUMP CHECKLIST. VERIFIED -2 GEAR CONTROL MANIFOLD INSTALLED. INSPECTED NOSE GEAR AREA FOR DEFECTS. NONE NSDR DXTA200601677Windshield · crackedCO-PILOTS WINDSHIELD CRACKED IN FLIGHT AFTER AMBER WSHLD INOP "R" CAS ILLUMINATED. REMOVED CO-PILOTS WINDSHIELD. INSTALLED WINDSHIELD ON AIRCRAFT. RAN AIRCRAFT AND PERFORMED OPS CHECKED CO-PILOTS WINDSHIELD. OPS CHECK GOOD. PRESSURIZED AIRCRAFT AND PERFOMSDR DXTA200601470Actuator · intermittentAMBER "RUD LIMITER FAIL A" CAS MESSAGE, 84 PERCENT INFLIGHT. LOWER RUDDER PERFORMED RUDDER LIMITER OPERATIONAL CHECK. NO DISCREPANCIES NOTED. GAINED ACCESS TO RUDDER LIMITER A ACTUATOR. VISUAL INSPECTION CHECK GOOD. CONTACTED NETJETS WHO ELECTS TO REPLACESDR DXTA200601290Warning Light · illuminatedIN CRUISE, LEFT ENGINE ITT QUICKLY ROSE TO 860 AND SHARPLY DROPPED TO APPROX 820-830 SEVERAL TIMES. APPROX 10-15 BOUNCES IN A 10-15 SEC TIME. FL410, RAT -18, .90M. INSPECTED ALL THERMOCOUPLE CONNECTORS PER A23007C MM 77-21-10. APPLIED STABILANT 22 CONTACT ESDR DXTA200500760Warning Light · illuminatedDURING CLIMB THROUGH FL370 AT MACH .80, GEAR UNLOCK LIGHT ILLUMINATED ACCOMPANIED BY AUDIBLE CLUNK. AIRCRAFT WAS SLOWED AND A DESCENT WAS BEGUN. LIGHT WENT OFF AT FL260 AND 250 KNOTS WITH ANOTHER CLUNK. ITEM IS UNDER INVESTIGATION.SDR DXTA200500745Cable · out of adjust25 MINS INTO THE FLIGHT JUST LEVELING OFF AT FL 410, FELT AND HEARD THE LANDING GEAR UNLOCK AND RETRACT TWICE. THE GEAR "UNLOCK" LIGHT REMAINED ILLUMINATED FOR 42 MINS UNTIL DESCENDING THRU FL310 WHEN FELT AND HEARD THE LANDING GEAR UNLOCK AND RETRACT ONCE ANSDR DXTA200500700Attach Bracket · wornYOKE HAS 1-2" DEAD SPOT IN PITCH IN BOTH MANUAL AND AUTO PILOT MODES. FOUND PITCH FEEL ELEVATOR CONTROL BRACKETS ATTACHING HOLE WORN AND ELONGATED, REPLACED BRACKET AND ACCOMPLISHED REPAIR IAW REPAIR DEFINITION S-750-0124/04RD FROM CESSNA DATED APRIL 29, 2005SDR DXTA200400289Cdu · failedDURING CRUISE AT FL430, NR 1 FMS WENT BLANK WITH RED FMS NR 1 DISPLAYED ON CAPTAIN’S MFD. ABOUT 30 MINUTES LATER A FAINT ODOR OF BURNED INSULATION NOTICED, ODOR STAYED CONSTANT FOR THE REST OF THE FLIGHT. REMOVED AND REPLACED NR 1 FMS CDU, OP-CHECK GOOD PER CE
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