N600QS, cancelled Feb 18, 2026
Service difficulty reports · 24
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 = 'N600QS' AND deregistration_id = 'N600QS-2026-02-18' 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 = 'N600QS' AND deregistration_id = 'N600QS-2026-02-18' 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 DXTA2025101705326Windshield · faultedLEFT WINDSHIELD FAULT APPEARED DURING CLIMB OUT WITH FLASHING MASTER CAUTION. BEGAN RUNNING THE QRH AND THE FAULT CLEARED. UPON ARRIVAL, FAULT REAPPEARED TWICE WITH FLASHING MASTER CAUTION. SWAPPED LT POWER CONTROL UNIT TO THE RT ENGINE & SWAPPED THE RT POWESDR DXTA2025012002009Wire · unsecureCABIN EMERG LIGHT: LIGHT OVER SEAT 7 IS INOP. LIGHT IS ASSOCIATED WITH EMER LIGHTS. CORRECTIVE ACTION: RESECURED LOOSE WIRE CONNECTION. OPS CHECK GOOD. IAW CESSNA 560XL AMM CH.33-20-02SDR DXTA2024112601259Pressure Switch · failedAFTER CLEARING THE RUNWAY AND STARTING TAXIING TO RAMP HEARD A CB POP AND THE ANTI SKID ANNUNCIATOR LIGHT ILLUMINATED THEN SHORTLY AFTER THE LOW BRAKE PRESSURE ANNUNCIATOR ILLUMINATED. AIRCRAFT WAS STOPPED AND TOWED INTO RAMP. THE CB THAT POPPED WAS THE POWER SDR DXTA2023110199480Unknown · unknownRT ENGINE FIRE WARNING CAME ON DURING CLIMB OUT THROUGH 18,000. FOLLOWING QRC REDUCED POWER ON RT & LIGHT WENT OUT. NO OTHER INDS. RESUMED NORMAL POWER & RETURNED TO AIRPORT. INSPECTED RH ENGINE, FOUND FIRE DETECTION LOOP IMPINGING HARD AGAINST A METAL CLAMPSDR DXTA2023092196030Actuator · faultedLEVELING OFF AT FL400, GOT PITCH TRIM ANNUNCIATOR ON PFD. RAN QRH. FOUND BEING TRIGGER BY SPEED. TOO FAST TOO SLOW WITHIN 10KTS. LIGHT COMES ON. DISCONNECTED AUTOPILOT & FOUND TRIM TO BE JAMMED. JAMMED ALL THE WAY IN DECENT TILL APPROX 10,000'. FUNCTIONED NOSDR DXTA2022121576210Connector · disconnectedLAV EXIT SIGN/LIGHT: LOWER EMERGENCY EXIT SIGN AT THE BASE OF THE LAV IS INOP. REMOVED EMERGENCY EXIT LIGHT FROM BASE OF LAV AND RESEATED MOLEX CONNECTOR IAW CESSNA 560XL SPM 20-30-00. OPERATIONAL CHECK GOOD AT THIS TIME.SDR DXTA2022052762830Door · lack of lubeMAIN DOOR: UNABLE TO FULLY ENGAGE THE LATCH TO LOCK THE MAIN CABIN DOOR FROM EITHER THE INSIDE OR THE OUTSIDE. REMOVED MED STEPS AND CLEANED AND LUBED ALL MOVING COMPENANTS AFTER WORKING LUBE IN THE LOCK LOSSENED UP AND IS MUCH EASIER TO LOCK. RE -INSTALLEDSDR DXTA2021110151170None · noneMAIN DOOR: REPEAT WRITE UP. AT ALTITUDE THERE IS A HIGH PITCHED SQUEAL COMING FROM THE MAIN CABIN DOOR. IT CAN BE HEARD IN THE COCKPIT WITH HEADSET ON AND IN THE CABIN. IF YOU ARE FACING THE MAIN DOOR FROM THE CABIN, IT SEEMS TO BE COMING FROM THE LEFT SIDE SDR DXTA2020100404164Door · bindingMAIN CABIN DOOR WILL NOT OPEN FROM THE OUTSIDE USING THE CABIN DOOR HANDLE, DURING PREFLIGHT. SIGN OFF. PERFORMED VISUAL AND OPERATIONAL CHECK OF DOOR AND NO DEFECTS NOTED AT THIS TIME. NO DEFECTS NOTED AT THIS TIME OF PRECATCH. WORK DONE IAW 560XL AMM CH SDR DXTA2019061742502Coalescer Bag · dirtyCOCKPIT ODOR OIL SMELL - WHEN SELECTING HEAT ON DURING CRUISE FLIGHT, THERE WAS AN OIL SMELL IN THE COCKPIT. WHEN SELECTING HEAT OFF THE OIL SMELL DISAPPEARED. REPLACED COALESCOR SOAK RAN APU AND ENGINES. OPERTION CHECK GOOD REF CESZOKMM 21-51-00SDR DXTA2018093001484Apu · smokeAPU FILLED INTERIOR OF AIRCRAFT WITH SMOKE JUST WE TOOK THE RUNWAY FOR DEPARTURE.SDR DXTA2018041200830Condenser · odorTHERE WAS A VERY STRONG DIRTY SOCK ODOR IN THE COCKPIT AND CABIN, WHEN THE CABIN AIR CONDITIONING WAS OPERATING. REMOVED AND REPLACED CONDENSER SOCK WITH NEW CONDENSER SOCK IAW AMM 21-21-00. CHECKED GOOD.SDR JGVR20170627005Skin · delaminatedRIGHT OTBD FLAP LOWER SIDE HAS AN AREA OF DELAMINATION. REPAIRED IAW ERO AND 8110-3.SDR JGVR20170605001Skin · delaminatedRIGHT OTBD FLAP DELAMINATED ON LOWER SKIN. REPAIRED.SDR DXTR2014102002Link Pin · galledWHILE ATTEMPTING TO DISASSEMBLE THE RT MLG TO REPLACE THE TRUNNION ASSY. THE PIVOT LINK PIN WAS BADLY GULLED FROM NO LUBRICATION. THE PIN HAD TO BE FORCIBLY DRIVEN OUT.SDR DXTR2014102001Lock Pin · galledWHILE ATTEMPTING TO R & R THE RT MLG ACTUATOR BECAUSE OF LEAKING FLUID, IT WAS DISCOVERED THAT THE SIDEBRACE ATTACH PIN AND THE LOCKING BOLT WERE SO BADLY GALLED AND FROZEN IN PLACE FROM LACK OF GREASE THEY HAD TO BE DRILLED & DRIVEN OFF TO FREE ACTUATOR END.SDR DXTA2014081205855Engine · leakingAT TAKEOFF POWER JUST AFTER V1 HAD A STRONG OILY ODOR IN CABIN. THE ODOR APPEARED TO DISSIPATE AT REDUCED POWER. ALL ENG INDICATIONS WERE NORMAL, APU WAS OFF. GND RAN AC AT TAKEOFF POWER & ISOLATED ENGS. APU & THEIR BLEED SELECTIONS. TROUBLE SHOT TO BURNTSDR DXTA2014081105854Unknown · odorVERY STRONG SMELL, NOT BURNING, MORE OF AN OILY SMELL. THE ODOR STAYED FOR THE ENTIRE FLIGHT. INSPECTED LT & RT ENGS FOR EVIDENCE OF OIL LEAKS, NONE FOUND. RAN LT & RT ENGS INDEPENDENTLY FOR APPROXIMATELY 5 MINUTES, EACH AT DIFFERENT POWER SETTINGS UP TO 65SDR DXTA2014052805783Display · odorAFTER TAKEOFF AROUND 200 FT AGL, A STRONG ODOR OF BURNING ELECTRIAL WAS NOTICED BY CREW MEMBERS. THE MFD WHICH HAD JUST BEEN ON MEL & HAD A BLACK SCREEN, STARTED FLASHING OFF & ON. CREW CONTINUED WITH NORMAL DEPARTURE UNTIL THROUGH APPROXIMATELY 5000 FT. FISDR CWQR20121221055Tube · crackedDURING AN APU CHANGE, FOUND A 2.5" CRACK IN THE BLEED AIR TUBE ATTACHMENT FLANGE. DISCOVERED VISUALLY AND THE CRACK DID NOT EXTEND INTO THE TUBE, NO BLEED AIR LEAK.SDR DXTA2012043004962Anti-Skid Sys · malfunctionedBRAKES GRAB AND PULL SHARPLY LEFT ON LANDING ROLL WHEN EVENLY APPLIED RELEASING BRAKE APPLICATION DISCONTINUES THE PULL TO LEFT. CHECKED WHEELS AND BRAKES FOR CONDITION, CHECKED GOOD. ACCUMULATOR PRESSURE GOOD. PERFORMED ANTI SKID BRAKE SYS BLEED ON RT AND SDR DXTA2009032703565Angle · bentON TAKEOFF ROLL, THE RUDDER PEDALS FELT VERY STIFF. AFTER TAKEOFF WITH THE YAW DAMPER OFF, IT WAS VERY DIFFICULT TO DEPRESS THE RT RUDDER. ON FINAL APPROACH WITH THE YAW DAMPER OFF, THE RUDDER PEDALS FELT LIKE THEY WERE RUBBING SOMETHING WHEN DEPRESSED. FOUNDSDR DXTA200702502Warning Light · false activationDURING APPROACH, THE FLAPS WERE SELECTED TO 15. THE STAB MISCOMPARE LIGHT ILLUMINATED. EMER CHECKLIST ACCOMPLISHED. ONCE FLAP HANDLE WAS SELECTED TO 35 DEGREES THE STAB MISCOMPARE LIGHT WENT OUT AFTER 5 SECONDS. PERFORMED THE TWO POSITION HORIZONTAL STABILIZSDR DXTA200702154Unknown · malfunctionedPILOTS AUTO PILOT TRIM DISCONNECT BUTTON POPPED OUT OF YOKE IN FLIGHT. [SUP 05-03-07] SECURED PILOT A/P TRIM DISCONNECT SWITCH PER STANDARD PRACTICE.
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