# N658QS: 2006 Cessna 560XL, registration cancelled 2026-02-17 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: February 17, 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: 560-5665 - Year built: 2006 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 27, 2006 - Certificate issued: June 9, 2021 - Last registry action: May 19, 2023 - Mode S code: A8ABE1 - 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/N658QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=658QS - Page: https://openairdocs.org/deregistered/N658QS-2026-02-17 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 3J7R2025090400001](https://openairdocs.org/sdr/3J7R2025090400001), Sep 3, 2025: LIGHT. INOPERATIVE. THE DROPPED-AISLE EMERGENCY LIGHTS BETWEEN SEAT 8 AND SEAT 6 ARE INOPERATIVE. - [SDR DXTA2024022210966](https://openairdocs.org/sdr/DXTA2024022210966), Feb 19, 2024: SERVO. FAULTY. DURING CRUISE FLIGHT AT FL390 WITH CLEAR AIR AND SMOOTH RIDE , WE FELT A MOMENTARY UNCOMMANDED BACK AND FORTH YAWING MOTION. SUBSEQUENTLY AT FL350 WE AGAIN FELT - [SDR DXTA2023091395310](https://openairdocs.org/sdr/DXTA2023091395310), Sep 12, 2023: UNKNOWN. UNKNOWN. MAIN EXIT SIGN/LIGHT: FWD EXIT SIGN OF MAIN CABIN DOOR IS INTERMITTENT WITH EMER LIGHTS SWITCHED ON. LOCATED AND FOUND LOWER FORWARD LIGHT EXIT ASSEMBLY AT THE - [SDR DXTA2022121476160](https://openairdocs.org/sdr/DXTA2022121476160), Dec 13, 2022: LIGHT. DEFECTIVE. FLOOR AISLE LIGHTS FROM SEAT 5 TO CABIN DOOR IS VERY DIM AND NOT SUFFICENT FOR EMERGENCY AISLE LIGHTING. REMOVED AND REPLACED FWD CABIN DROPPED AISLE LIGHTING A - [SDR DXTA2022050661340](https://openairdocs.org/sdr/DXTA2022050661340), May 5, 2022: BATTERY PACK. DISCHARGED. EMERGENCY LIGHTING: FORWARD INTERIOR CABIN EMERGENCY LIGHTING BATTERY APPEARS TO BE DEAD. EXIT LIGHT, SEAT 3 AND 10 LIGHTS, FWD FLOOR LIGHTING AND RIGHT SIDE DO - [SDR DXTA2021120352920](https://openairdocs.org/sdr/DXTA2021120352920), Dec 2, 2021: APU. ABNORMAL. CABIN SMOKE: AFTER ENGINE START WITH APU RUNNING THE CABIN FILLED WITH SMOKE. SHUTDOWN BOTH ENGINES AND APU. NO OTHER DECREPENCIES FOUND. // SIGNOFF// TECH REMO - [SDR DXTA2021081146770](https://openairdocs.org/sdr/DXTA2021081146770), Aug 10, 2021: PUMP. DEFECTIVE. BRAKE PRESSURE LIGHT: DURING TAXI OUT OF THE CHOCKS BOTH THE LOW BREAK PRESSURE ANNUNCIATOR AND ANTISKID INOP ANNUNCIATOR ILLUMINATED. WE IMMEDIATELY STOPPED TH - [SDR DXTA2021051241930](https://openairdocs.org/sdr/DXTA2021051241930), May 11, 2021: RISER. FAILED. DURING MX WHEN QA INSPECTOR WAS EXITING THE AIRCRAFT THE STEP FAILED CAUSING DAMAGE TO THE STEP HINGE. REMOVED AND REPLACED RISER ASSY AND RISER COVER WITH NEW - [SDR DXTA0301202138800](https://openairdocs.org/sdr/DXTA0301202138800), Feb 28, 2021: ENGINE. FAILED. RIGHT ENGINE OIL PRESSURE LOW ANNUNCIATOR WITH MASTER WARNING. AT 13,000FT, DURING CLIMB OUT, WITH CLIMB POWER SET AIRSPEED 250 KNOTS OIL PRESSURE INDICATES ZER - [SDR DXTA030120213880](https://openairdocs.org/sdr/DXTA030120213880), Feb 28, 2021: WARNING MESSAGE. ACTIVATED. RIGHT ENGINE OIL PRESSURE LOW ANNUNCIATOR WITH MASTER WARNING. AT 13,000FT, DURING CLIMB OUT, WITH CLIMB POWER SET AIRSPEED 250 KNOTS OIL PRESSURE INDICATES ZER - [SDR DXTA2016101206317](https://openairdocs.org/sdr/DXTA2016101206317), Oct 12, 2016: GASKET. FAILED. DURING TAKEOFF AT 1,500 FT, RIGHT ENGINE EXCEEDED ITT RED LINE PRIOR TO FLAP RETRACT ALTITUDE. COMPLIED WITH EXTENSIVE TROUBLESHOOTING. REF MESA WORK ORDER REV. - [SDR DXTA2015022005984](https://openairdocs.org/sdr/DXTA2015022005984), Feb 19, 2015: DISPLAY. FAILED. APU WAS STARTED & ELECTRICAL POWER WAS APPLIED TO ALL SYSTEMS. AFTER ABOUT 15 MINUTES AN ELECTRICAL BURNING ODOR WAS NOTED FOLLOWED BY SMOKE, A BLANK PFD 2 & IL - [SDR DXTA2014100905907](https://openairdocs.org/sdr/DXTA2014100905907), Oct 8, 2014: CONTROL UNIT. FAILED. AFTER TAKEOFF, SELECTED GEAR UP & IT DID NOT RETRACT. R & R THE LANDING GEAR HANDLE CONTROL UNIT IAW MM 32-30-01. OPS CHECKED GOOD. - [SDR DXTA2014022805668](https://openairdocs.org/sdr/DXTA2014022805668), Feb 27, 2014: APU. DEFECTIVE. APU STARTED NORMALLY ON THE GND BUT SHUT ITSELF OFF AFTER 2 MINUTES OF NORMAL OPERATION. OBSERVED & SMELLED WHITE SMOKE FROM THE WEMACS AS THE UNIT SHUT DOWN. T - [SDR DXTA2013092305512](https://openairdocs.org/sdr/DXTA2013092305512), Sep 22, 2013: DISPLAY. FAILED. DURING CLIMBOUT, A STRONG, BURNING, ELECTRICAL ODOR WAS NOTICED IN THE COCKPIT. ODOR DISSIPATED AFTER ABOUT FIVE MINUTES AND NO SMOKE WAS NOTICED. ODOR WAS NOT - [SDR CWQR20120523032](https://openairdocs.org/sdr/CWQR20120523032), May 23, 2012: CHANNEL. CRACKED. DURING A SCHEDULED INSP WE FOUND THE FWD BAGGAGE DOOR HINGE ASSY CRACKED IN SEVERAL PLACES. 2 CRACKS IN SUPPORT CHANNEL 66120720-2 AND 1 CRACK ON CHANNEL 661206 - [SDR DXTA2010120604351](https://openairdocs.org/sdr/DXTA2010120604351), Dec 5, 2010: LAMP. INOPERATIVE. LT MLG GREEN LIGHT INOPERATIVE. DID A GO AROUND, TESTED THE GEAR LIGHTS. RAN THE BB1 EMERGENCY CHECK LIST. RELAMPED LT MLG GREEN LIGHTS. PERFORMED LANDING GEAR - [SDR DXTA2010072804180](https://openairdocs.org/sdr/DXTA2010072804180), Jul 27, 2010: GARLOCK SEAL. FAILED. RT ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED INFLIGHT AT 25,000'. OIL PRESSURE ON GUAGE AT CRUISE POWER SETTING WAS APPROX 28PSI. RETARDED THROTTLE TO IDLE - [SDR DXTA2010042904078](https://openairdocs.org/sdr/DXTA2010042904078), Apr 28, 2010: ACTUATOR. MALFUNCTIONED. RT LANDING GEAR WOULD NOT INDICATE DOWN AND LOCKED AFTER NORMAL EXTENSION. RAN THE EMERGENCY CHECKLIST, PULLED THE HANDLE AND BLOW DOWN AND STILL NO GREEN INDIC - [SDR DXTA2009033003570](https://openairdocs.org/sdr/DXTA2009033003570), Mar 27, 2009: SWITCH. INOPERATIVE. ON CLIMBOUT AT ABOUT 20,000 FT, WE GOT AN ACM OVERHEAT ANNUNCIATOR FOLLOWED BY A RISE IN CABIN ALTITUDE. WE COMPLETED APPROPRIATE CHECKLISTS AND RETURNED TO DEP - [SDR DXTA20082915](https://openairdocs.org/sdr/DXTA20082915), Mar 5, 2008: METERING UNIT. MALFUNCTIONED. NR1 ENGINE FUEL BOOST PUMP LIGHT FLASHED UPON DESCENT. A FEW SECONDS AFTER THE FLASH THE NR1 ENGINE FAILED. REMOVED/REPLACED FUEL METERING UNIT, FUEL FLOW DIVID - [SDR DXTA200702727](https://openairdocs.org/sdr/DXTA200702727), Dec 28, 2007: CIRCUIT BOARD. INOPERATIVE. CLIMBING TO ALTITUDE THE LEFT GREEN INDICATOR LIGHT STARTED FLICKERING ON AND OFF. NO HYDRAULIC OR GEAR UNSAFE LIGHTS WERE PRESENT. AT FL300 IT CONTINUED TO FLI - [SDR DXTA200702425](https://openairdocs.org/sdr/DXTA200702425), Jul 27, 2007: FIRE LOOP. LOOSE. THE NR 2 ENGINE FIRE LIGHT WOULD FAINTLY GLOW AND FLICKER DURING FLIGHT WHEN WE WERE IN FROZEN PRECIP AND CONTINUOUS CHOP TURBULENCE. THE ENG/WING ANTI ICE WAS - [SDR DXTA200702185](https://openairdocs.org/sdr/DXTA200702185), May 10, 2007: PRESSURE SWITCH. INOPERATIVE. AFTER FLAPS WERE SELECTED UP, HYD PRESS ANNUNCIATOR REMAINED ILLUMINATED. AFTER 40 SECONDS -STAB MISCOMP- ANNUNCIATOR ALSO ILLUMINATED WITH FLASHING MASTER CAUT --- 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.