# N566QS: 2008 Cessna 560XL, registration cancelled 2026-05-16 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: May 16, 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: 560-5825 - Year built: 2008 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 22, 2008 - Certificate issued: January 30, 2026 - Last registry action: January 30, 2026 - Mode S code: A73EA3 - 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/N566QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=566QS - Page: https://openairdocs.org/deregistered/N566QS-2026-05-16 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 (17) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2025091704958](https://openairdocs.org/sdr/DXTA2025091704958), Sep 14, 2025: BATTERY PACK. NO TEST. ALL FORWARD EMERGENCY EXIT LIGHTS INOP IN ARM OR ON POSITION WITH BATTERY OFF. BATTERY PACK #1 RESET INERTIAL SWITCH VERIFIED CONNECTIONS TO BATTERY PACK #1 ARE - [SDR DXTA2025080704462](https://openairdocs.org/sdr/DXTA2025080704462), Aug 4, 2025: HYDRAULIC LINE. LEAKING. ON TAKEOFF, THE MLG WOULD NOT RETRACT AND STAB MIS COMP ANNUNCIATOR ILLUMD. EXECUTED MLG WOULD NOT RETRACT RED GEAR UNLOCKED LIGHT REMAINS ON QRH & STAB MIS COM - [SDR JGVR202407290001](https://openairdocs.org/sdr/JGVR202407290001), Jul 29, 2024: DOOR FRAME. CHAFED. EMERGENCY EXIT CUT OUT, HAS A CHAFE LOCATION ON AN EXISTING REPAIR ON INNER WEB BETWEEN F.S. 123.46 AND 131.04. RE COMPLIED WITH EXISTING AQRD ERO-868105 REV IR - [SDR 2TJR202306207481](https://openairdocs.org/sdr/2TJR202306207481), Jun 20, 2023: HINGE. CRACKED. DURING 600HR DOOR INSPECTION PER TASK CARD TC-5XL-52-121102, FOUND THE AFT MAIN CABIN DOOR HINGE LOWER HALF IS CRACKED. REMOVED AND REPLACED THE AFT MAIN CABIN - [SDR 2TJR202306197481](https://openairdocs.org/sdr/2TJR202306197481), Jun 19, 2023: HINGE. CORRODED. DURING 600HR DOOR INSPECTION PER TASK CARD TC-5XL-52-121102, NOTED SEVERE CORROSION ON THE FWD MAIN CABIN DOOR, FUSELAGE HINGE HALF ASSEMBLY. REMOVED AND REPLAC - [SDR DXTA2023030381720](https://openairdocs.org/sdr/DXTA2023030381720), Mar 2, 2023: METERING VALVE. DEFECTIVE. DURING TAXI WHILE BRAKING THE RIGHT BRAKE PEDAL WENT COMPLETELY SOFT FOR A COUPLE SECONDS AND THEN STARTED WORKING AGAIN. REMOVED AND REPLACED THE BRAKE METERIN - [SDR DXTA2021112252250](https://openairdocs.org/sdr/DXTA2021112252250), Nov 20, 2021: FIRE DETECTOR. DEFECTIVE. LEFT ENGINE FIRE DETECTION LIGHT: THE LEFT ENG FIRE PUSH LIGHT INTERMITTENTLY AND DIMLY FLASHED DURING FLIGHT MULTIPLE TIMES DURING THE SHORT 15 MIN FLIGHT. CLE - [SDR DXTA2021062143980](https://openairdocs.org/sdr/DXTA2021062143980), Jun 19, 2021: VALVE. STICKING. UPON LANDING THE MAIN CABIN DOOR WAS EXTREMELY DIFFICULT TO OPEN. // SIGN OFF // FOUND THE ACCOUSTIC DOOR SEAL VALVE TO BE STICKING. CLEANED ACCOUSTIC DOOR SEAL - [SDR DXTA2018113001738](https://openairdocs.org/sdr/DXTA2018113001738), Nov 30, 2018: STRUT. NOT EXTENDED. ALL LANDING GEAR RETRACTION - GEAR WOULD NOT COME UP, GEAR UNSAFE WITH HYD PRESS LIGHT ILLUMINATED, RAN THE APPROPRIATE CHECKLIST CAME BACK AND LANDED WITHOUT E - [SDR DXTA2018072501228](https://openairdocs.org/sdr/DXTA2018072501228), Jul 25, 2018: ENGINE. MALFUNCTIONED. CABIN ODOR BURNING SMELL, COPILOT COMPLAINED ABOUT SOMETHING BOTHERING HIS EYES WHILE CLIMBING OUT WITH APU OFF AND I DIDN'T NOTICE ANYTHING AT THAT TIME. WHILE - [SDR DXTA2018072302013](https://openairdocs.org/sdr/DXTA2018072302013), Jul 20, 2018: CONVERTER. DIRTY. COCKPIT ODOR BURNING SMELL - AFTER TAXI OUT, WE SMELLED A SMOKY ODOR COMING FROM OVERHEAD GASPER VENTS. OPENED COCKPIT WINDOW TO VERIFY IT WAS NOT AN OUTSIDE SO - [SDR DXTA2014112405934](https://openairdocs.org/sdr/DXTA2014112405934), Nov 23, 2014: VALVE. FAILED. DURING PERFORMANCE A STATIC TAKE OFF, THE LT SEAT BRAKES WOULD NOT HOLD THE AIRPLANE. PERFORMED ENGINE RUNS AND VERIFIED DISCREPANCY. CHECKED FOR CORRECT BRAKE - [SDR DXTA2013120205586](https://openairdocs.org/sdr/DXTA2013120205586), Nov 30, 2013: CONTROLLER. FAULTY. DURING DECENT TO LANDING, THE RT ENG FIRE LIGHT WAS DIMLY FLICKERING ON & OFF, 1 SECOND ON THEN ABOUT 3 SECONDS OFF, UNTIL LANDING. PLACING THE RT THROTTLE TO I - [SDR DXTA2012091705125](https://openairdocs.org/sdr/DXTA2012091705125), Sep 16, 2012: BUNGEE. DAMAGED. DURING LANDING ROLLOUT UNEVEN PRESSURE ON BRAKE APPLICATION. THE LT BRAKE PEDAL TRAVELED SIGNIFICANTLY FURTHER THAN THE RT PEDAL CAUSING A JERKING MOTION. AFTER - [SDR DXTA2011102004754](https://openairdocs.org/sdr/DXTA2011102004754), Oct 19, 2011: MASTER CYLINDER. READS LOW. BRAKES ARE VERY SOFT UPON LANDING. ANTI-SKID NEVER ENGAGED ON WET RUNWAY. UPON INSPECTION OF THE BRAKE PRESSURE CYLINDER, NOTICED IT READ LOW. AT 55 DEGREES, SH - [SDR DXTA2010072204170](https://openairdocs.org/sdr/DXTA2010072204170), Jul 21, 2010: DISPLAY. ERRATIC. STANDBY HSI INDICATIONS ERRACTIC ON BOTH HEADING AND CLIMB AND DESCENT INFORMATION. TESTED AND CONFIRMED ON INITIAL POWER-UP SYS OPERATED NORMALLY. TAXI CHECKED - [SDR DXTA2009031303542](https://openairdocs.org/sdr/DXTA2009031303542), Mar 12, 2009: MONOPOLE. FAILED. SHORTLY AFTER TAKEOFF, LT EEC FAILED WITH BOTH EEC'S IN MANUAL. LT ENGINE WOULD COMPRESSOR STALL WHEN N1 REDUCED BELOW 70 PERCENT AND N2 BELOW 85 PERCENT. NO NO --- 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.