# N661QS: 2007 Cessna 560XL, registration cancelled 2025-12-14 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 14, 2025 - 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: 560-5677 - Year built: 2007 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 10, 2007 - Certificate issued: October 20, 2025 - Last registry action: October 20, 2025 - Mode S code: A8B95F - 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/N661QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=661QS - Page: https://openairdocs.org/deregistered/N661QS-2025-12-14 From the FAA registry file of November 7, 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 DXTA2025080704476](https://openairdocs.org/sdr/DXTA2025080704476), Aug 4, 2025: DOOR SEAL. DEFECTIVE. SHORTLY AFTER REACHING CRUISE FLIGHT AT FLIGHT LEVEL 350, WE HAD A DOOR SEAL ANNUNCIATOR ILLUMINATE, AND A FLASHING MASTER CAUTION LIGHT. REMOVED AND REPLACED M - [SDR DXTA2025050203319](https://openairdocs.org/sdr/DXTA2025050203319), May 2, 2025: LIGHT. INOPERATIVE. FLOOR EMERG EXIT LIGHT: FORWARD STRIP OF AISLE EMERGENCY LIGHTS ON LEFT SIDE OF AIRCRAFT ARE INOP. ALL OTHER EMERGENCY LIGHTS ARE OPERATING NORMAL. CORRECTIVE A - [SDR DXTA2025022802519](https://openairdocs.org/sdr/DXTA2025022802519), Feb 26, 2025: PRECATCH. UNSECURE. MAIN DOOR PRE-CATCH HANDLE SPINS ON THE STEM. CORRECTIVE ACTION; RESECURED PRECATCH RELEASE HANDLE JAMNUT IAW CE-560XL AMM 52-10-01. NO FURTHER DEFECTS NOTED. - [SDR DXTA2025010801849](https://openairdocs.org/sdr/DXTA2025010801849), Jan 5, 2025: DOOR. OBSTRUCTED. MAIN CABIN DOOR IS HARD TO OPEN AND CLOSE. REPAIRED INSULATION BY BELLCRANK. OPS CHECK GOOD. IAW CE-560XL MM 52-10-00. - [SDR JGVR20231009002](https://openairdocs.org/sdr/JGVR20231009002), Oct 9, 2023: UNKNOWN. UNKNOWN. REPAIRED CORRODED AREA LOCATED AT THE RH SIDE OF THE AFT WALL OF THE NOSE LANDING GEAR WHEEL WELL BY BLENDING, PERFORMING NDT, REPORTING FOR REPAIR DISPOSITION. - [SDR DXTA2023022381030](https://openairdocs.org/sdr/DXTA2023022381030), Feb 22, 2023: TIRE. FAILED. RT MLG HAD A BLOW OUT HALF WAY THROUGH OUR LANDING ROLL. THE ANTISKID FAIL ANNUNCIATOR ILLUMINATED AROUND THE SAME TIME AS THE AIRCRAFT STARTED TO PULL TO THE R - [SDR DXTA2022091270130](https://openairdocs.org/sdr/DXTA2022091270130), Sep 10, 2022: NONE. DEFECTIVE. MAIN HYDRAULICS: DURING A CLIMB GOING THROUGH 11,500 FEET WE HAD A STAB-MIS-COMP ANNUNCIATOR LIGHT COME ON , AFTER ABOUT 30 SECONDS THE AUTO PILOT DISCONNECTED - [SDR EBVR20220830](https://openairdocs.org/sdr/EBVR20220830), Aug 30, 2022: NONE. NONE. DURING 48 MONTH INSPECTION FOUND CRACK IN BOTTOM AFT SECTION OF RUDDER TRIM TAB. REPAIRED RUDDER TRIM TAB CRACK PER AQRD ERO-106811 REVISION IR TITLED N661QS RU - [SDR DXTA2022042560900](https://openairdocs.org/sdr/DXTA2022042560900), Apr 22, 2022: LANDING GEAR. MALFUNCTIONED. GEAR POSITION & WARNING: ON CLIMBOUT, AFTER THE GEAR GEAR AND FLAPS WERE SELECTED UP, THE 3 GREEN GEAR INDICATORS EXTINGUISHED AND THE GEAR UNLOCK LIGHT REMAINE - [SDR DXTA2022041460260](https://openairdocs.org/sdr/DXTA2022041460260), Apr 13, 2022: LAMP. BURNED OUT. RIGHT MLG INDICATOR LIGHT: ON FINAL APPROACH WE SELECTED THE GEAR DOWN AND HAD NO RIGHT MAIN GEAR INDICATOR LIGHT TO ILLUMINATE. WE PERFORMED A GO AROUND, PERFO - [SDR DXTR202204131](https://openairdocs.org/sdr/DXTR202204131), Apr 13, 2022: LIGHT. BURNED OUT. RIGHT MLG INDICATOR LIGHT: ON FINAL APPROACH WE SELECTED THE GEAR DOWN AND HAD NO RIGHT MAIN GEAR INDICATOR LIGHT TO ILLUMINATE. WE PERFORMED A GO AROUND, PERFO - [SDR JGVR20210216001](https://openairdocs.org/sdr/JGVR20210216001), Feb 16, 2021: TORQUE TUBE. CORRODED. LH ELEVATOR TORQUE TUBE IS CORRODED. REMOVED CORRODED INBOARD TORQUE TUBE DUE TO LEVEL 2 CORROSION FROM L/H ELEVATOR P/N 6634200-809LH S/N 0000210. INSTALLED NE - [SDR DXTA2020031703589](https://openairdocs.org/sdr/DXTA2020031703589), Mar 16, 2020: UPLOCK SWITCH. OUT OF ADJUST. ALL LANDING GEAR RETRACTION DID NOT RETRACT - UPON RETRACTION RED UNLOCK LIGHT ILLUMINATED PREFORMED CHECKLIST. // SIGNOFF// JACKED AIRCRAFT TO PERFORM GEAR SWI - [SDR DXTA2017070906426](https://openairdocs.org/sdr/DXTA2017070906426), Jul 9, 2017: GENERATOR. FAILED. EVIDENCE OF A RIGHT AC ALTERNATOR FIRE WAS SEEN. THE ENGINE NACELLE PAINT WAS BURNT AFT OF ALTERNATOR VENT AND MOLTEN COPPER COMING OUT OF THE VENT. TROUBLESHOT - [SDR DXTA2017070706425](https://openairdocs.org/sdr/DXTA2017070706425), Jul 7, 2017: CONTROL BOX. FAILED. DURING CLIMB OUT THRU 6500 FEET, RIGHT FIRE LIGHT CAME ON WITH RIGHT FIRE FAULT DET SYSTEM. RAN APPROPRIATE CHECKLIST AND DETERMINED IT WAS A FIRE DETECTION SYS - [SDR DXTA2016123006351](https://openairdocs.org/sdr/DXTA2016123006351), Dec 29, 2016: COALESCER BAG. DIRTY. ACM PRODUCED A SOCK ODOR. REMOVED & REPLACED DIRTY WATER SEPARATOR CONDENSER CLOTH IAW MM 12-19-02. OPS & LEAK CHECKS WERE GOOD. - [SDR DXTA2013050805385](https://openairdocs.org/sdr/DXTA2013050805385), Apr 20, 2013: LOCK NUT. MISSING. DURING A BORESCOPE INSPECTION OF COMBUSTION CHAMBER LINER COOLING RING SEGMENT SELF LOCKING NUTS, IAW MFG SPECIAL INSTRUCTION 35-2013. LINER COOLING RING SELF L - [SDR CWQR20120330023](https://openairdocs.org/sdr/CWQR20120330023), Mar 30, 2012: CONTROL CABLE. FRAYED. DURING A SCHEDULED INSPECTION, THE ELEVATOR TRIM CABLE WAS FOUND TO BE FRAYED BEYOND LIMITS. THIS CABLE ASSY IS LOCATED WHERE THE CABLE TRANSITIONS FROM A VERTI - [SDR CWQR20120327019](https://openairdocs.org/sdr/CWQR20120327019), Mar 27, 2012: HINGE BRACKET. CRACKED. DURING A SCHEDULED INSPECTION, FOUND RT ELEVATOR INBD HINGE CRACKED, VERIFIED WITH NDT, R & R HINGE ASSY. - [SDR DXTA2010120104339](https://openairdocs.org/sdr/DXTA2010120104339), Nov 30, 2010: UNKNOWN. ODOR. JUST PRIOR TO DECENT, TRANSFERRED FUEL FROM LT TANK TO RT. AFTER WHICH NOTICED ODOR OF FUEL. OPENED OVERHEAD FRESH AIR VENTS & DID NOT SMELL ANYTHING. ON POST F - [SDR DXTA2009092303796](https://openairdocs.org/sdr/DXTA2009092303796), Sep 22, 2009: THROTTLE CABLE. BROKEN. WHILE ATTEMPTING TO SET T/O POWER, NR 1 THROTTLE WOULD NOT REMAIN IN T/O DETENT. TAKEOFF ABORTED, NR 2 ENG SHUTDOWN NORMALLY. IN THROTTLE CUTOFF, NR 1 ENG ACCEL - [SDR DXTA2008122003418](https://openairdocs.org/sdr/DXTA2008122003418), Dec 20, 2008: ACTUATOR. LACK OF LUBE. 22-1 AUTO PILOT DISENGAGED 5 SECONDS AFTER SELECTING FLAPS TO 15 DEGREES. AUTO PILOT FAIL AMBER LIGHT SHOWED ON PFD'S. SEEMED LIKE AUTO PILOT TRIM COULD NOT KEE - [SDR DXTA2008122008034](https://openairdocs.org/sdr/DXTA2008122008034), Dec 20, 2008: AUTOPILOT SYS. FAILED. AUTO PILOT DISENGAGED 5 SECONDS AFTER SELECTING FLAPS TO 15 DEGREES. AUTO PILOT FAIL AMBER LIGHT SHOWED ON PFD'S. SEEMED LIKE AUTO PILOT TRIM COULD NOT KEEP UP. - [SDR DXTA2008122303418](https://openairdocs.org/sdr/DXTA2008122303418), Dec 20, 2008: FLAP SYSTEM. MALFUNCTIONED. AUTO PILOT DISENGAGED 5 SECONDS AFTER SELECTING FLAPS TO 15 DEGREES. AUTO PILOT FAIL AMBER LIGHT SHOWED ON PFD'S. --- 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.