# N600QS: 2006 Cessna 560XL, registration cancelled 2026-02-18

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 18, 2026
- Status when cancelled: Valid registration
- Airframe: [Cessna 560XL](https://openairdocs.org/model/cessna-560xl) (registry code 2076702)
- Engine: [Pratt & Whitney Canada PW545B](https://openairdocs.org/engine/pratt-whitney-canada-pw545b) (registry code 52186)
- Data sheets: [TCDS A22CE](https://openairdocs.org/tcds/A22CE), [TCDS E00059EN](https://openairdocs.org/tcds/E00059EN) (OpenAirDocs)
- Serial number: 560-5664
- Year built: 2006
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 21, 2006
- Certificate issued: October 16, 2020
- Last registry action: March 24, 2023
- Mode S code: A7C8AE
- Owner when cancelled: [Netjets Sales Inc](https://openairdocs.org/faa-owner/NETJETS%20SALES%20INC)
- Location: [Oklahoma City, OK](https://openairdocs.org/faa-place/OK/Oklahoma%20City)
- Owner type: Corporation
- Owner's area on the map: 35.5467° N, 97.5646° W: Placed by OpenAirDocs at the center of ZIP code 73116, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N600QS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=600QS
- Page: https://openairdocs.org/deregistered/N600QS-2026-02-18

From the FAA registry file of November 5, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Cessna 560XL: https://openairdocs.org/model/cessna-560xl.md

## Service difficulty reports (24)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DXTA2025101705326](https://openairdocs.org/sdr/DXTA2025101705326), Oct 15, 2025: WINDSHIELD. FAULTED. LEFT WINDSHIELD FAULT APPEARED DURING CLIMB OUT WITH FLASHING MASTER CAUTION. BEGAN RUNNING THE QRH AND THE FAULT CLEARED. UPON ARRIVAL, FAULT REAPPEARED TWICE 
- [SDR DXTA2025012002009](https://openairdocs.org/sdr/DXTA2025012002009), Jan 17, 2025: WIRE. UNSECURE. 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 CESS
- [SDR DXTA2024112601259](https://openairdocs.org/sdr/DXTA2024112601259), Nov 23, 2024: PRESSURE SWITCH. FAILED. 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 
- [SDR DXTA2023110199480](https://openairdocs.org/sdr/DXTA2023110199480), Oct 31, 2023: UNKNOWN. UNKNOWN. 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 & RETURN
- [SDR DXTA2023092196030](https://openairdocs.org/sdr/DXTA2023092196030), Sep 20, 2023: ACTUATOR. FAULTED. 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 AU
- [SDR DXTA2022121576210](https://openairdocs.org/sdr/DXTA2022121576210), Dec 14, 2022: CONNECTOR. DISCONNECTED. 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 CE
- [SDR DXTA2022052762830](https://openairdocs.org/sdr/DXTA2022052762830), May 26, 2022: DOOR. LACK OF LUBE. 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 MOVIN
- [SDR DXTA2021110151170](https://openairdocs.org/sdr/DXTA2021110151170), Oct 29, 2021: NONE. NONE. 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 TH
- [SDR DXTA2020100404164](https://openairdocs.org/sdr/DXTA2020100404164), Oct 4, 2020: DOOR. BINDING. 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 DE
- [SDR DXTA2019061742502](https://openairdocs.org/sdr/DXTA2019061742502), Jun 14, 2019: COALESCER BAG. DIRTY. 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. 
- [SDR DXTA2018093001484](https://openairdocs.org/sdr/DXTA2018093001484), Sep 30, 2018: APU. SMOKE. APU FILLED INTERIOR OF AIRCRAFT WITH SMOKE JUST WE TOOK THE RUNWAY FOR DEPARTURE.
- [SDR DXTA2018041200830](https://openairdocs.org/sdr/DXTA2018041200830), Apr 11, 2018: CONDENSER. ODOR. 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 CO
- [SDR JGVR20170627005](https://openairdocs.org/sdr/JGVR20170627005), Jun 27, 2017: SKIN. DELAMINATED. RIGHT OTBD FLAP LOWER SIDE HAS AN AREA OF DELAMINATION. REPAIRED IAW ERO AND 8110-3.
- [SDR JGVR20170605001](https://openairdocs.org/sdr/JGVR20170605001), Jun 3, 2017: SKIN. DELAMINATED. RIGHT OTBD FLAP DELAMINATED ON LOWER SKIN. REPAIRED.
- [SDR DXTR2014102002](https://openairdocs.org/sdr/DXTR2014102002), Oct 20, 2014: LINK PIN. GALLED. 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 DRI
- [SDR DXTR2014102001](https://openairdocs.org/sdr/DXTR2014102001), Oct 20, 2014: LOCK PIN. GALLED. 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 GALLE
- [SDR DXTA2014081205855](https://openairdocs.org/sdr/DXTA2014081205855), Aug 11, 2014: ENGINE. LEAKING. 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. G
- [SDR DXTA2014081105854](https://openairdocs.org/sdr/DXTA2014081105854), Aug 10, 2014: UNKNOWN. ODOR. 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 
- [SDR DXTA2014052805783](https://openairdocs.org/sdr/DXTA2014052805783), May 27, 2014: DISPLAY. ODOR. 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, STARTE
- [SDR CWQR20121221055](https://openairdocs.org/sdr/CWQR20121221055), Dec 21, 2012: TUBE. CRACKED. 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 L
- [SDR DXTA2012043004962](https://openairdocs.org/sdr/DXTA2012043004962), Apr 29, 2012: ANTI-SKID SYS. MALFUNCTIONED. 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 C
- [SDR DXTA2009032703565](https://openairdocs.org/sdr/DXTA2009032703565), Mar 26, 2009: ANGLE. BENT. 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 WIT
- [SDR DXTA200702502](https://openairdocs.org/sdr/DXTA200702502), Sep 27, 2007: WARNING LIGHT. FALSE ACTIVATION. DURING APPROACH, THE FLAPS WERE SELECTED TO 15. THE STAB MISCOMPARE LIGHT ILLUMINATED. EMER CHECKLIST ACCOMPLISHED. ONCE FLAP HANDLE WAS SELECTED TO 35 DEGREES 
- [SDR DXTA200702154](https://openairdocs.org/sdr/DXTA200702154), Apr 27, 2007: UNKNOWN. MALFUNCTIONED. 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.

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