N922QS
Service difficulty reports not matched to an aircraft · 25
They name N922QS, 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 = 'N922QS' 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 = 'N922QS' 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 EE4Y2020102111780Frame · corrodedDURING THE MAINTENANCE PROCESS IT WAS FOUND AT THE TAIL CONE 170-50005-423 S/N: 0478001, AREA RT, SILENCER FWD EDGE SKIN WITH BULGED. THE AREA WAS ACCESSED, AND IT WAS FOUND THE INTERNAL FRAME AT RT LOWER PANEL AFT SPLICE AREA CORRODED.
**UNABLE TO VERIFY SDR DXTA2017121806434Display · unserviceableDU CAS MESSAGE AND PFD 2 CIRCUIT BREAKER POPPED. STRONG ELECTRICAL ODOR ALSO. CORRECTIVE ACTION: CONFIRMED PFD 2 BREAKER TRIP IMMEDIATELY WITH AVIONICS SWITCH ON. REMOVED #5 DU SCREEN. APPLIED POWER AND CB IS NO LONGER TRIPPING. INSPECTED WIRING BEHIND RH CB PSDR 2017F00185Skin · corrodedCORROSION ON UPPER WING SKINS (LEFT AND RIGHT SIDE) ENGINEERING LETTER DQ9925M1.SDR 2017F00186Skin · gougedRIGHT WING GOUGE ON UPPER SKIN ENGINEERING LETTER DQ10036M1.SDR 2017FA0000542Door Frame · debondedREPAIR OF DIS-BOND AREA AROUND NOSE DOOR OPENING ENGINEERING LETTER DQ9996M1.SDR DXTA2017042406400Unknown · odorCABIN TEMPERATURE UNABLE TO CONTROL IN AUTO OR MANUAL MODES. CABIN FILLED WITH VISIBLE FUMES. THE FUMES DID NOT SMELL LIKE EITHER PAPER OR ELECTRICAL FIRE.SDR 2016F00222Stiffener · crackedREPAIR OF CRACKED RT WING RIB STIFFENER AT CWS 161.40 DATED NOV 8, 2016 AND FAA FORM 8100-9 DATED 11/9/2016.SDR DXTA2015123006147Unknown · smokeON THE GND WITH APU RUNNING FOR ABOUT 5 MINUTES, TAIL CONE BLD LEAK AMBER CAS MSG CAME ON. WITHIN 30 SECONDS COCKPIT & CABIN FILLED WITH SMOKE. INSPECTED TAIL CONE COMPARTMENT, NO SMOKE DETECTED. POWERED UP APU & RAN ENVIRONMENTAL SYS FOR 30 MINUTES, ALL INSDR DXTA2015102906115Apu · malfunctionedAFTER ENGINE START AND WELL AFTER APU SHUTDOWN CABIN FILLED WITH A LIGHT FOG OF SMOKE. REMOVED APU. INSPECTED FIREWALL, MOUNTS, AND SUPPORT STRUCTURE. NO DEFECTS FOUND. INSTALLED REPAIRED APU IAW CE-750 M/M 49-10-00 AND HONEYWELL GTCP36-150CX MM 49-20-00. SDR DXTA2015090306074Unknown · odorUPON RESTART OF APU, THE FADEC MSGS CAME BACK, ALONG WITH A NEW MESSAGE, TAIL CONE BLEED LEAK. WHEN SELECTED THE APU AIR, THERE WAS A STRONG BURNING ODOR IN THE COCKPIT, SHUTDOWN & INSPECTED. CHECKED APU OIL LEVEL & PERFORMED A GENERAL INSPECTION OF THE APU.SDR DXTA2014060605796Unknown · odorCLIMBING THRU FL 340, DETECTED AN ACRID BURNING ODOR, ONE MINUTE LATER THE FADEC FAULT L A B & R A B CAS MESSAGES CAME ON IN QUICK SUCCESSION. IAW THE CHECKLIST, RESET THE FADEC`S. THE FAULTS CLEARED MOMENTARILY & THEN ALL THE FAULTS REAPPEARED. FADEC`S FSDR DXTA2013112705583Computer · contaminatedABORTED TAKEOFF BELOW 60 KTS DUE TO YD KICKING OFF & NO TAKEOFF MESSAGE. WHEN EXITING RUNWAY WE GOT AMBER CAS FADEC FAULT R B THAT WE COULDN'T CLEAR USING AFM PROCEDURES FOR IMT CODES. WHILE ATTEMPTING TO TROUBLE SHOT EGPWS SYS FOUND THAT IT WOULDN'T TEST INSDR DXTA2013062405423Apu · leakingSMOKE OUT OF WEMACS WITH BLEED AIR ON HIGH. FOUND OIL PRESENT AT APU INLET. REMOVED LEAKING APU AND INSTALLED A REPAIRED APU. ALL WORK PERFORMED IAW AMM 49-00-00. NO FURTHER DECECTS NOTED. OPS AND LEAK CHECKED SATISFACTORY.SDR DXTA2012112605195O-Ring · leakingDURING DECENT, CREW RECEIVED AN AMBER CAS MESSAGE: HYD LEVEL LOW A, HYD SHOWED 16 PERCENT. FOLLOWED EMERGENCY CHECKLIST AND MADE A SAFE LANDING, STOPPING THE ACFT ON THE RUNWAY USING THE EMERGENCY BRAKE. DURING POST FLIGHT INSPECTION, FOUND FRESH HYD FLUIDSDR DXTA2012082105099Apu · odorFUMES IN CABIN AND COCKPIT, ISOLATED PACS FOR 10 MINUTES BUT COULD NOT TELL ANY DIFFERENCE. FOUND APU LEAKING OIL FROM INLET. INSTALLED REPAIRED APU IAW MM 49-10-00. OPS AND LEAK CHECKED GOOD.SDR DXTA2012073005065Landing Gear · failedAFTER TAKEOFF THE NLG FAILED TO RETRACT. RED UNLOCK LIGHT FOR THE NOSE GEAR STAY ON. LOWER THE MAIN GEAR WE GET 3 GREEN DOWN AND LOCK. BUT THE GEAR STAYS STUCK ON THE DOWN POSITION. OPS CHECK NOSE GEAR CENTERING FUNCTION TO INSURE GEAR IS CENTERING AND ALLSDR DXTA2012072705060Bearing · failedAFTER TAKEOFF THE LANDING GEAR FAILED TO RETRACT. THE RED UNLOCK LIGHT REMAINED ON. THE GEAR CONTINUED TO MAKE AIR NOISE. THE GEAR WAS CYCLED ONCE WITH THE SAME INDICATION. THE GEAR WAS SELECTED DOWN WITH A SAFE INDICATION. CHECKED NOSE STRUT FOR FULL EXTENSISDR DXTA2011071004647O-Ring · leakingIN CRUISE FLIGHT AT FL400, DURING CRUISE CHECKLIST, NOTED HYD VOL WAS 20 PERCENT AND DECREASING. ONCE HYD VOL A CAS ILLUMINATED FOLLOWED APPROPRIATE CHECKLIST AND LANDED WITHOUT INCIDENT. DETERMINED HYD LEAK FROM RUDDER PCU UPPER UNIT HAD O-RING CUT ON PRESSUSDR DXTA2011031104503Resolver · inoperativeCLIMBING THROUGH FL200 FLAPS FAIL INDICATOR CAME ON WITH FLAPS INDICATING 0. RAN CHECKLIST AND PUSHED FLAP RESET AT WHICH TIME INDICATOR WENT TO AMBER FLAPS 7 WITH NO SLATS. MATCHING FLAP INDICATION, WENT TO FLAPS 5 WITH SELECTOR AT WHICH TIME SLATS CAME OUT ASDR DXTA2011011804414Actuator · malfunctionedIN FLIGHT, DURING CLIMBOUT FOR ABOUT 1000' FROM 15,000 TO 16,000 AT AN AIRSPEED OF 300KTS THE UPPER RUDDER BEGAN TO FLUTTER/PULSATE RAPIDLY LT AND RT. AFTER THE INITIAL PULSING, IT CALMED DOWN TO A SLOW CONTINUAL PULSATION BEING MORE PRONOUNCED ABOVE 300KTS ASDR DXTA2010112904326Apu · leakingWHEN PULLING POWER BACK FOR DESCENT, AS SOON AS HP VALVES OPENED, GOT VERY STRONG "LIGHTING A MATCH" ODOR IN THE COCKPIT. R & R APU IAW CMM 49-10-10. OPS & LEAK CHECKED GOOD.SDR DXTA2010112904325Line · leakingLEFT BRAKE GRABS HARD WHEN LIGHTLY APPLIED. FOUND LEAKING HYD LINE AT BRAKE FUSE. TIGHTENED & VERIFIED BRAKE HYD PRESSURES AT BRAKE METERING VALVE, RUDDER PEDALS & BRAKES IAW MM 32-42-00. OPS & LEAK CHECKED GOOD. TAXI CHECKED GOOD.SDR DXTA2010112904324Apu · odorVERY STRONG FUEL ODOR IN CABIN WITH APU RUNNING. BURNS EYES. SEEMS TO DISSIPATE AFTER APU SHUTDOWN AND ONLY ENGINES RUNNING. REMOVED CABIN & COCKPIT COALESCER SOCKS & CLEANED IAW MM 12-10-01, REV 40. COMPRESSOR HOUSING IN INLET VERY OILY. PERFORMED GEARBOXSDR DXTA2010042704077Strut · failedLANDING GEAR WOULD NOT RETRACT DURING INITIAL CLIMB OUT. GEAR HANDLE WILL NOT MOVE FROM THE DOWN POSITION. JACKED ACFT. FOUND NOSE STRUT NOT FULLY EXTENDED. HANDLE WILL NOT MOVE FULLY EXTENED STRUT. HANDLE MOVE TO UP POSITION. FOUND NO PRESSURE IN LOWER CSDR DXTA2009021703509Engine · making metalDURING TAKE OFF ROLL GOT "CHIP DETECT -R" AMBER CAS MESSAGE. ABORTED TAKEOFF. EXAMINED ALL RT ENG MAGNETIC PLUGS FOR PARTICLES. FOUND CHIP, REPLACED OIL FILTER AND COMPLIED WITH OIL FILTER AND ANALYZER KIT. OPERATED THE RT ENG, "CHIP DETECTER" CAS MESSAGE DID
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