# N673QS: 2006 Cessna 560XL, registration cancelled 2025-12-15 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 15, 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: 560-5651 - Year built: 2006 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 22, 2006 - Certificate issued: September 10, 2025 - Last registry action: September 10, 2025 - Mode S code: A8E84C - 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/N673QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=673QS - Page: https://openairdocs.org/deregistered/N673QS-2025-12-15 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 (23) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2025050703357](https://openairdocs.org/sdr/DXTA2025050703357), May 4, 2025: COUNTERBALANCE. FAULTED. MAIN DOOR: MAIN ENTRANCE DOOR IS VERY HARD/HEAVY TO CLOSE THE LAST 2 FEET OF MOVEMENT. WHEN OPENING DOOR, IT POPS OPEN ABOUT 2 FEET AND PULLED CREWMEMBER INTO D - [SDR DXTA2025050403357](https://openairdocs.org/sdr/DXTA2025050403357), May 4, 2025: DOOR. MALFUNCTIONED. MAIN DOOR: MAIN ENTRANCE DOOR IS VERY HARD/HEAVY TO CLOSE THE LAST 2 FEET OF MOVEMENT. WHEN OPENING DOOR, IT POPS OPEN ABOUT 2 FEET AND PULLED CREWMEMBER INTO D - [SDR DXTA2025032802812](https://openairdocs.org/sdr/DXTA2025032802812), Mar 24, 2025: SOLENOID. FAULTY. DURING DOOR CLOSURE, BOTH LIGHTS GO OUT BRIEFLY. WITHIN A FEW SECONDS THE "CABIN DOOR" LIGHT COMES BACK ON. IT BAS BEEN INTERMITTENT ALL WEEK. IT WOULD GO OUT A - [SDR DXTA2024052011818](https://openairdocs.org/sdr/DXTA2024052011818), May 19, 2024: SOCKET. OUT OF ADJUST. MAIN DOOR: AFTER LANDING, WE HAD TO CYCLE THE DOOR LOCK TO OPEN THREE TIMES TO GET THE DOOR TO OPEN. PRECATCH HANDLE WAS PULLED AND DID NOT HELP THE SITUATION. - [SDR DXTA2024030811140](https://openairdocs.org/sdr/DXTA2024030811140), Mar 8, 2024: SUPPORT STRUT. BINDING. CREW CAN NOT CLOSE CABIN DOOR FROM INSIDE. EVIDENCE OF SCARRING WHERE TOP FWD ROUND PIN ENGAGES LATCH PIN PLATE IN FRAME. INSPECTED DOOR LOCK PINS & BEARING PLA - [SDR DXTA2023012479030](https://openairdocs.org/sdr/DXTA2023012479030), Jan 23, 2023: G SWITCH. TRIPPED. FORWARD CABIN EMERGENCY LIGHT SYSTEM WILL NOT EXTINGUISH UNLESS TURNED OFF WITH THE SWITCH. SUSPECT INERTIA SWITCH. GAINED ACCESS TO FWD EMER BAN AND FOUND THAT - [SDR DXTA2023011978840](https://openairdocs.org/sdr/DXTA2023011978840), Jan 19, 2023: BATTERY PACK. DEFECTIVE. WITH THE EMERGENCY LIGHT SWITCH ON AND BATTERY SWITCH OFF, THE EXIT SIGN OVER SEAT 7 AND EXIT SIGN OVER LAV IS VERY DIM. TURNING BATTERY SWITCH ON BOTH LIGHTS I - [SDR DXTA2021071245000](https://openairdocs.org/sdr/DXTA2021071245000), Jul 9, 2021: ENGINE. FAILED. NR 2 ENGINE FAILED ON TAKEOFF AT GEAR RETRACTION. HEARD LOUD BANGS AND THE ITT SPIKED AT THE TOP OF RED. ENGINE WAS NOT PRODUCING POWER AT THIS POINT. FOLLOWED - [SDR JGVR20180703001](https://openairdocs.org/sdr/JGVR20180703001), Jul 3, 2018: STRUT. CORRODED. AFTER RE-SERVICING OF THE NLG STRUT PRESSURE HELD BUT THE FLUID BYPASSED SEAL. DURING RE-SEAL OF NLG, FOUND CORROSION IN UPPER BARREL. DISASSEMBLED, CLEANED AND - [SDR DXTA2012022204883](https://openairdocs.org/sdr/DXTA2012022204883), Feb 20, 2012: HANDLE. MALFUNCTIONED. AT 220 KTS, 1500 FT, MOVED THE GEAR HANDLE TO THE DOWN POSITION. HANDLE MOVED NORMALLY AND LOCKED INTO PLACE BUT ONLY THE RED GEAR UNSAFE LIGHT CAME ON AND NO S - [SDR CWQR20120207002](https://openairdocs.org/sdr/CWQR20120207002), Feb 6, 2012: HINGE FITTING. CRACKED. DURING A VISUAL INSPECTION, FOUND CORROSION ON CABIN DOOR HINGE FITTING, LIMITED TO THE INWARD EDGE OF THE HINGE FITTING, ON CLOSER INSPECTION, FOUND A CRACK TH - [SDR CWQR20120207001](https://openairdocs.org/sdr/CWQR20120207001), Feb 6, 2012: HINGE FITTING. CRACKED. DURING A VISUAL INSPECTION OF THE FORWARD CABIN DOOR HINGE FITTING, FOUND CRACK. CRACK .35 INCHES LONG AND WAS IN THE RADIUS AREA BETWEEN THE FLANGE AREA THAT A - [SDR DXTA2010111704308](https://openairdocs.org/sdr/DXTA2010111704308), Nov 17, 2010: TRANSCEIVER. INOPERATIVE. DESCENDING THROUGH 11,500 FT WITH AN AIRSPEED OF 250 KTS. HAD GEAR WARNING AURAL INDICATION. IN CRUISE CONFIGURATION 11,000 AGL. HAD AN ADDITIONAL 4 AURAL WARNI - [SDR DXTA2010110804296](https://openairdocs.org/sdr/DXTA2010110804296), Nov 5, 2010: WARNING HORN. FALSE ACTIVATION. GEAR WARNING HORN SOUNDED ON 3 SEPARATE OCCASIONS. FIRST, FOR 30 SECONDS AT IAS OF 210 KTS & FL220, FLAPS 0. INCREASE OR DECREASE OF THROTTLE SETTING WOULD NOT - [SDR DXTA2010011303944](https://openairdocs.org/sdr/DXTA2010011303944), Jan 13, 2010: CONTROL HANDLE. FAULTY. REMOVED GEAR CONTROL HANDLE ASSY AND REPLACED WITH REPAIRED UNIT. OPS CHECKED CYCLED LANDING GEAR OPS CHECK GOOD. WORK DONE IAW MM 32-30-01. - [SDR DXTA2009110203841](https://openairdocs.org/sdr/DXTA2009110203841), Oct 30, 2009: CONTROLLER. INOPERATIVE. LANDING GEAR SELECTOR HANDLE MOVED TO DOWN. RED UNLOCK LIGHT ILLUMINATED BUT GEAR DID NOT COME DOWN. THREE SECONDS LATER GEAR CAME DOWN. REMOVED DEFECTIVE LANDI - [SDR DXTA2009032302558](https://openairdocs.org/sdr/DXTA2009032302558), Mar 22, 2009: BRAKE ASSY. WORN. REMOVED RT MAIN GEAR WHEEL BRAKES ASSY. INSTALLED O/H CUSTOMER SUPPLIED MAIN GEAR WHEEL BRAKE ASSY. PERFORMED EMERGENCY BRAKE SYS OPS CHECK AND BLED THE ANTISKI - [SDR DXTA2009032303558](https://openairdocs.org/sdr/DXTA2009032303558), Mar 22, 2009: BRAKE. MALFUNCTIONED. ON LANDING, WHEN BRAKES ARE APPLIED THE AIRPLANE YAWS TOWARDS THE RT. REMOVED RT MAIN GEAR WHEEL BRAKES ASSY. INSTALLED O/H CUSTOMER SUPPLIED MAIN GEAR WHEEL BR - [SDR DXTA2009031603549](https://openairdocs.org/sdr/DXTA2009031603549), Mar 13, 2009: PCB. MALFUNCTIONED. WHEN GEAR HANDLE WAS LOWERED RED GEAR UNLOCK ILLUMINATED; NO GREEN GEAR LIGHTS, NO HYD PRESS LIGHT. AFTER 20 SEC GEAR CAME DOWN NORMALLY. REMOVED AND REPLACED L - [SDR DXTA200702486](https://openairdocs.org/sdr/DXTA200702486), Sep 19, 2007: ENGINE. FAILED. (RT LO OIL PRESS) LIGHT CAME ON DURING T/O, WHICH WAS ABORTED. 09-28-07 REMOVED AND REPLACED NR 2 ENGINE WITH SERVICEABLE UNIT USING NEW SEALS. ALL ACCESSORIES - [SDR DXTA200702463](https://openairdocs.org/sdr/DXTA200702463), Sep 10, 2007: CIRCUIT BOARD. MALFUNCTIONED. AIRCRAFT WILL NOT CROSSFEED IN FLIGHT. HAD NORMAL INDICATIONS OF CROSSFEED BUT NO FUEL TRANSFER FROM LT TO RT. TRANSFER FROM T TO LT HAD BOTH LOW FUEL PRESSURE - [SDR DXTA200601643](https://openairdocs.org/sdr/DXTA200601643), Oct 9, 2006: METERING VALVE. INOPERATIVE. DURING TAXI BRAKES RUMBLE WHEN PRESSURE IS APPLIED. CONDITION REPEATS ON PILOT AND COPILOT SIDES. RUMBLING OCCURED DURING SLOW TAXI (LESS THAN 10 KTS). RUMBLING - [SDR DXTA200601625](https://openairdocs.org/sdr/DXTA200601625), Oct 1, 2006: BRAKE. VIBRATES. EVERY TIME THE BRAKES ARE INITIALLY APPLIED, WILL GET A RUMBLE/VIBRATION FROM BOTH BRAKES FOR 2-3 SECONDS FOLLOWED BY NORMAL BRAKING. IF BRAKE PRESSURE IS RELEA --- 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.