# N648QS: 2005 Cessna 560XL, registration cancelled 2026-01-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 23, 2026 - Status when cancelled: Valid registration - Airframe: [Cessna 560XL](https://openairdocs.org/model/cessna-560xl) (registry code 2076702) - Engine: [Pratt & Whitney Canada PW545 series](https://openairdocs.org/engine/pratt-whitney-canada-pw545-series) (registry code 52154) - Data sheets: [TCDS A22CE](https://openairdocs.org/tcds/A22CE), [TCDS E00059EN](https://openairdocs.org/tcds/E00059EN) (OpenAirDocs) - Serial number: 560-5574 - Year built: 2005 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 8, 2005 - Certificate issued: December 8, 2020 - Last registry action: November 16, 2023 - Mode S code: A88462 - 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/N648QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=648QS - Page: https://openairdocs.org/deregistered/N648QS-2026-01-23 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 DXTA2025031902720](https://openairdocs.org/sdr/DXTA2025031902720), Mar 16, 2025: BATTERY PACK. DEFECTIVE. FORWARD HALF OF EMERG LIGHTS/FWD EMER BATT (3 MED EXIT SIGNS, 2 FWD OVERHEAD LIGHTS @ SEATS 3&10, FWD AISLE STRIP LIGHT) REMAIN ON WHEN THE EMER LIGHT SWITCH IS - [SDR DXTA2025031402651](https://openairdocs.org/sdr/DXTA2025031402651), Mar 12, 2025: BATTERY PACK. INOPERATIVE. MAIN EXIT SIGN/LIGHT: FWD EMERGENCY LIGHT BATTERY PACK INOP. FWD MAIN CABIN DOOR EMER LIGHT AND FWD FLOOR EMER LIGHTS INOP DURING TEST. REPLACED BATTERY PACK. O - [SDR DXTA2025021302337](https://openairdocs.org/sdr/DXTA2025021302337), Feb 12, 2025: PRECATCH. OUT OF ADJUST. MAIN DOOR PRECATCH: MAIN CABIN DOOR WILL NOT OPEN. STUCK ON PRECATCH. CORRECTIVE ACTION: ADJUSTED PRECATCH CABLE. OPS CHECK GOOD. IAW CE560XL MM 52-10-00. - [SDR 2024FA0000670](https://openairdocs.org/sdr/2024FA0000670), Aug 29, 2024: SKIN. CORRODED. REPAIRED THE LH UPPER WING SKINS BY BLENDING CORRODED AREAS, PERFORMING NDT, AND REPORTING FOR REPAIR DISPOSITION. CLEANED, TREATED, AND PRIMED AREAS FOUND ACCE - [SDR 2024FA0000669](https://openairdocs.org/sdr/2024FA0000669), Aug 29, 2024: SKIN. CORRODED. MECHANICALLY REMOVED 3 AREAS OF CORROSION FOUND AROUND E-EXIT DOOR SKIN AROUND EXTERIOR HANDLE. FOUND 1 CORROSION BLEND TO BE BEYOND LIMITS IAW C560XL SRM 51-70 - [SDR 2024FA0000668](https://openairdocs.org/sdr/2024FA0000668), Aug 29, 2024: SKIN. CORRODED. REPAIRED 54 AREAS OF CORROSION ON THE DROP AISLE FUSELAGE SKIN AND STRINGERS BETWEEN FUSELAGE STATION 175 THRU 355. PERFORMED AN EDDY CURRENT AND ULTRASONIC THI - [SDR 2024FA0000666](https://openairdocs.org/sdr/2024FA0000666), Aug 29, 2024: SKIN. CORRODED. MECHANICALLY BLENDED LH FUSELAGE PSE SKIN CORROSION LOCATED AROUND LH FWD CABIN WINDOW WITH 1 AREA OF CORROSION, 2ND CABIN WINDOW WITH 1 AREA OF CORROSION, 3RD - [SDR JGVR20231003001](https://openairdocs.org/sdr/JGVR20231003001), Oct 3, 2023: UNKNOWN. UNKNOWN. BLENDED CORRODED AREAS ON THE EXTERIOR FUSELAGE SKIN, LOCATED JUST UNDER THE RH #4 CABIN WINDOW, PERFORMED NDT AND REPORTED FOR REPAIR DISPOSITION. CLEANED, TRE - [SDR DXTA2023090194330](https://openairdocs.org/sdr/DXTA2023090194330), Sep 1, 2023: LIGHT. INOPERATIVE. FLOOR EMERG EXIT LIGHT: FWD LEFT AISLE DROPDOWN LED STRIP HAS AN APPROXIMATELY 3 TO 4 FOOT INOPERATIVE SECTION WHEN EMER LTS ARE SELECTED TO ON. REMOVED DAMAGED - [SDR DXTA2023050885530](https://openairdocs.org/sdr/DXTA2023050885530), May 5, 2023: DOOR. DAMAGED. MAIN DOOR: TAKING OFF WE HAD A DOOR OPEN AND DOOR SEAL LIGHT WITH MASTER CAUTION AND LOUD WIND NOISE. DID AN EMERGENCY RETURN TO THE FIELD. ON TOUCHDOWN THE DOO - [SDR 2021071945450](https://openairdocs.org/sdr/2021071945450), Jul 17, 2021: BATTERY PACK. FAULTY. EMERGENCY LIGHTING: WITH SHIP POWER OFF PASSENGER SAFETY LIGHTS EMERGENCY EXIT LIGHT OVER MAIN DOOR AND FORWARD HALF OF FLOOR LIGHTS DO NOT WORK, BUT ALL THE LI - [SDR DXTA2021071945450](https://openairdocs.org/sdr/DXTA2021071945450), Jul 17, 2021: BATTERY. INOPERATIVE. EMERGENCY LIGHTING: WITH SHIP POWER OFF PASSENGER SAFETY LIGHTS EMERGENCY EXIT LIGHT OVER MAIN DOOR AND FORWARD HALF OF FLOOR LIGHTS DO NOT WORK, BUT ALL THE LI - [SDR JGVR2016101700001](https://openairdocs.org/sdr/JGVR2016101700001), Oct 14, 2016: FLAP TRACK. WORN. DISCOVERED NINE RIVETS PULLED THROUGH THE SKIN ON THE BOTTOM OF THE OUTBOARD FLAP TRACK OF THE RT WING. - [SDR DXTA2016041306231](https://openairdocs.org/sdr/DXTA2016041306231), Apr 13, 2016: TORQUE TUBE. CORRODED. LEFT ELEVATOR TORQUE TUBE CORRODED OUT OF LIMITS. FOUND DURING COMPLETE PAINT PROCESS. REMOVED TORQUE TUBE, PN UNKNOWN, FROM LT ELEVATOR PN 6634200-9, SN 000010 - [SDR DXTA2016041306230](https://openairdocs.org/sdr/DXTA2016041306230), Apr 13, 2016: TORQUE TUBE. CORRODED. RIGHT ELEVATOR TORQUE TUBE CORRODED OUT OF LIMITS. FOUND DURING COMPLETE PAINT PROCESS. REMOVED TORQUE TUBE DUE TO LEVEL 2 CORROSION. INSTALLED NEW TORQUE TUBE - [SDR DXTA2014112105930](https://openairdocs.org/sdr/DXTA2014112105930), Nov 20, 2014: COMPUTER. FAILED. ENROUTE PICS MFD, PFD, FAILED WITH RED X & ANNUNCIATOR, FMS FAILED AS WELL AS YAW DAMPER, AUTOPILOT, TCAS, GND PROX & FLIGHT DIRECTOR. TROUBLESHOOT SYS TO AN IN - [SDR DXTA2010022203997](https://openairdocs.org/sdr/DXTA2010022203997), Feb 20, 2010: HEATING ELEMENT. FAILED. AT FL230 SAT WAS -30C. NOTICED SPARKS AT THE TOP RT PORTION OF PILOT SIDE WINDSHIELD AND WITHIN 5 SECONDS THE WINDSHIELD COMPLETELY SHATTERED, "WINDSHIELD FAIL - [SDR DXTA2009031603544](https://openairdocs.org/sdr/DXTA2009031603544), Mar 15, 2009: TRANSDUCER. MALFUNCTIONED. DURING TAKEOFF ROLL, THE MASTER CAUTION AND ANTI SKID LIGHT CAME ON. AFTER SHUTDOWN, NOTICED THE RT TRANSDUCER FLAG IN THE LT NOSE COMPARTMENT WAS SHOWING WHITE - [SDR DXTA200803031](https://openairdocs.org/sdr/DXTA200803031), Apr 28, 2008: GASKET. LEAKING. DURING T/O ROLL, RT N1 ROLLED BACK FROM 90.8 (T/O PWR SETTING) TO 80 PERCENT N1. REMOVED AND REPLACED BOU TORQUE MOTOR BASE GASKET IAW MM 75-30-01 C/W RUNS ALL - [SDR DXTA200702529](https://openairdocs.org/sdr/DXTA200702529), Oct 6, 2007: HANDLE. OUT OF ADJUST. THE CABIN DOOR ANNUNCIATOR ILLUMINATED WHILE PASSING FL190. 10-29-07 ADJUSTED DOOR HANDLE SWITCH AND LUBED DOOR PINS. IAW CE-560XL M.M. 52-10-01. OP'S CHECK NUM - [SDR DXTA200601392](https://openairdocs.org/sdr/DXTA200601392), May 14, 2006: UNLOCK SWITCH. OUT OF ADJUST. DURING GEAR RETRACTION THE 3 GREEN LIGHTS EXTINGUISHED WHILE THE RED UNLOCK LIGHT REMAINED ILLUMINATED. - JACKED ACFT, ADJUST UP-LOCK, SWITCH ON NOSE GEAR, SWIN - [SDR CWQR2006004](https://openairdocs.org/sdr/CWQR2006004), Mar 8, 2006: DRAIN VALVE. LOOSE. FOUND THE STATIC SYSTEM DRAIN VALVE POPPET RETAING RING COMING LOOSE FROM VALVE BASE. - [SDR DXTA200501173](https://openairdocs.org/sdr/DXTA200501173), Dec 31, 2005: BRAKE. VIBRATES. LT AND RT BRAKES ARE CATCHING AND GRABBING ON BRAKE APPLICATION. LOUD CHATTERING CAN BE HEARD AND THE GRABBING SHAKES THE PLANE. BRAKE WEAR PINS SHOW AMPLE BRAK --- 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.