# Service difficulty reports: N600QS, cancelled Feb 18, 2026 A list on [N600QS, cancelled Feb 18, 2026](https://openairdocs.org/deregistered/N600QS-2026-02-18.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DXTA2025101705326](https://openairdocs.org/sdr/DXTA2025101705326.md): Windshield · faulted · Oct 15, 2025 · N600QS · Cessna 560XL · Flight Compartment Windows > LEFT 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 POWE - [SDR DXTA2025012002009](https://openairdocs.org/sdr/DXTA2025012002009.md): Wire · unsecure · Jan 17, 2025 · N600QS · Cessna 560XL · Light System Wiring > CABIN 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.33-20-02 - [SDR DXTA2024112601259](https://openairdocs.org/sdr/DXTA2024112601259.md): Pressure Switch · failed · Nov 23, 2024 · N600QS · Cessna 560XL · Brake Anti-Skid Section > AFTER 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 DXTA2023110199480](https://openairdocs.org/sdr/DXTA2023110199480.md): Unknown · unknown · Oct 31, 2023 · N600QS · Cessna 560XL · Fire Detection > RT 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 CLAMP - [SDR DXTA2023092196030](https://openairdocs.org/sdr/DXTA2023092196030.md): Actuator · faulted · Sep 20, 2023 · N600QS · Cessna 560XL · Elevator Control System > LEVELING 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 NO - [SDR DXTA2022121576210](https://openairdocs.org/sdr/DXTA2022121576210.md): Connector · disconnected · Dec 14, 2022 · N600QS · Cessna 560XL · Light System Wiring > LAV 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 DXTA2022052762830](https://openairdocs.org/sdr/DXTA2022052762830.md): Door · lack of lube · May 26, 2022 · N600QS · Cessna 560XL · Passenger/Crew Doors > MAIN 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 -INSTALLED - [SDR DXTA2021110151170](https://openairdocs.org/sdr/DXTA2021110151170.md): None · none · Oct 29, 2021 · N600QS · Cessna 560XL · Passenger/Crew Doors > MAIN 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 DXTA2020100404164](https://openairdocs.org/sdr/DXTA2020100404164.md): Door · binding · Oct 4, 2020 · N600QS · Cessna 560XL · Passenger/Crew Doors > MAIN 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 DXTA2019061742502](https://openairdocs.org/sdr/DXTA2019061742502.md): Coalescer Bag · dirty · Jun 14, 2019 · N600QS · Cessna 560XL · Humidity Control System > COCKPIT 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 21-51-00 - [SDR DXTA2018093001484](https://openairdocs.org/sdr/DXTA2018093001484.md): Apu · smoke · Sep 30, 2018 · N600QS · Cessna 560XL · APU Core Engine > APU FILLED INTERIOR OF AIRCRAFT WITH SMOKE JUST WE TOOK THE RUNWAY FOR DEPARTURE. - [SDR DXTA2018041200830](https://openairdocs.org/sdr/DXTA2018041200830.md): Condenser · odor · Apr 11, 2018 · N600QS · Cessna 560XL · Air Distribution System > THERE 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 JGVR20170627005](https://openairdocs.org/sdr/JGVR20170627005.md): Skin · delaminated · Jun 27, 2017 · N600QS · Cessna 560XL · Trailing Edge Flaps > RIGHT OTBD FLAP LOWER SIDE HAS AN AREA OF DELAMINATION. REPAIRED IAW ERO AND 8110-3. - [SDR JGVR20170605001](https://openairdocs.org/sdr/JGVR20170605001.md): Skin · delaminated · Jun 3, 2017 · N600QS · Cessna 560XL · Trailing Edge Flaps > RIGHT OTBD FLAP DELAMINATED ON LOWER SKIN. REPAIRED. - [SDR DXTR2014102002](https://openairdocs.org/sdr/DXTR2014102002.md): Link Pin · galled · Oct 20, 2014 · N600QS · Cessna 560XL · Main Landing Gear > WHILE 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 DXTR2014102001](https://openairdocs.org/sdr/DXTR2014102001.md): Lock Pin · galled · Oct 20, 2014 · N600QS · Cessna 560XL · Main Landing Gear > WHILE 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 DXTA2014081205855](https://openairdocs.org/sdr/DXTA2014081205855.md): Engine · leaking · Aug 11, 2014 · N600QS · Cessna 560XL · Engine (Turbine/Turboprop) > AT 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 BURNT - [SDR DXTA2014081105854](https://openairdocs.org/sdr/DXTA2014081105854.md): Unknown · odor · Aug 10, 2014 · N600QS · Cessna 560XL · Air Distribution System > VERY 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 65 - [SDR DXTA2014052805783](https://openairdocs.org/sdr/DXTA2014052805783.md): Display · odor · May 27, 2014 · N600QS · Cessna 560XL · Central Display > AFTER 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. FI - [SDR CWQR20121221055](https://openairdocs.org/sdr/CWQR20121221055.md): Tube · cracked · Dec 21, 2012 · N600QS · Cessna 560XL · Pneumatic Distribution System > DURING 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 DXTA2012043004962](https://openairdocs.org/sdr/DXTA2012043004962.md): Anti-Skid Sys · malfunctioned · Apr 29, 2012 · N600QS · Cessna 560XL · Brake Anti-Skid Section > BRAKES 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 DXTA2009032703565](https://openairdocs.org/sdr/DXTA2009032703565.md): Angle · bent · Mar 26, 2009 · N600QS · Cessna 560XL · Rudder Control System > ON 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. FOUND - [SDR DXTA200702502](https://openairdocs.org/sdr/DXTA200702502.md): Warning Light · false activation · Sep 27, 2007 · N600QS · Cessna 560XL · Flight Control System > DURING 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 STABILIZ - [SDR DXTA200702154](https://openairdocs.org/sdr/DXTA200702154.md): Unknown · malfunctioned · Apr 27, 2007 · N600QS · Cessna 560XL · Stabilizer Position Indicating > PILOTS 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. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 ``` This list as a web page: https://openairdocs.org/deregistered/N600QS-2026-02-18/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.