# N619QS: 2005 Cessna 560XL, registration cancelled 2026-08-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 31, 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: 560-5562 - Year built: 2005 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 1, 2005 - Certificate issued: August 3, 2020 - Last registry action: June 13, 2024 - Mode S code: A8119C - 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/N619QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=619QS - Page: https://openairdocs.org/deregistered/N619QS-2026-08-31 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 (35) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2025110705596](https://openairdocs.org/sdr/DXTA2025110705596), Nov 6, 2025: WIRE. DISCONNECTED. THE LAV EMERGENCY SIGN BELOW LAV SEST ( FWD FACING PANEL) DOES NOT ILLUMINTATE. RECONNECTED WIRES. OPS CHECK GOOD. IAW AMM 33-50-02 - [SDR DXTA2025050903377](https://openairdocs.org/sdr/DXTA2025050903377), May 6, 2025: BELLCRANK. DEFECTIVE. MAIN DOOR: MAIN CABIN DOOR EXTREMELY DIFFICULT TO OPEN. REQUIRED BOTH CREW MEMBERS PUSHING WITH THEIR FEET. IT DOES NOT APPEAR THAT EITHER SEAL WAS INFLATED. CO - [SDR DXTA2025050603377](https://openairdocs.org/sdr/DXTA2025050603377), May 6, 2025: DOOR. BINDING. MAIN DOOR: MAIN CABIN DOOR EXTREMELY DIFFICULT TO OPEN. REQUIRED BOTH CREW MEMBERS PUSHING WITH THEIR FEET. IT DOES NOT APPEAR THAT EITHER SEAL WAS INFLATED. - [SDR DXTA2025032102744](https://openairdocs.org/sdr/DXTA2025032102744), Mar 18, 2025: SOLENOID VALVE. DEFECTIVE. MAIN DOOR SECONDARY SEAL: WITH APU ON AND BLEED AIR OFF THE ACOUSTIC SEAL IN DOOR FRAME INTERFERES WITH OPENING AND CLOSING MAIN CABIN DOOR. BINDING BETWEEN THE - [SDR DXTA2024112001186](https://openairdocs.org/sdr/DXTA2024112001186), Nov 17, 2024: PRECATCH. LOOSE. MAIN DOOR PRECATCH: INSIDE HANDLE OF PRECATCH SPINS FREELY AND CATCHES ON SIDE WALL. GAINED ACCESS TO MAIN ENTRY DOOR TRIM PANELS AND FOUND JAM NUT LOOSE TIGHTE - [SDR DXTA2024110401007](https://openairdocs.org/sdr/DXTA2024110401007), Oct 30, 2024: CIRCUIT BREAKER. DEFECTIVE. DURING TAXING OUT TO THE ACTIVE RUNWAY, WHILE ON A TAXIWAY, WE HAD A MASTER CAUTION, RESET ILLUMINATE ALONG WITH A LOW PRESSURE/ANTISKID INOP ILLUMINATE. THE BR - [SDR DXTA2024102300913](https://openairdocs.org/sdr/DXTA2024102300913), Oct 20, 2024: MOTOR. FAULTED. POWER BRAKE CB: ABOUT 5 MINUTES INTO OUR TAXI FROM SIGNATURE TO RUNWAY 30 AT DULLES, JUST AS WE TURNED ON TAXIWAY ZULU GOT AN ANTI SKID ANNUNCIATOR ALONG WITH T - [SDR DXTA2024101400817](https://openairdocs.org/sdr/DXTA2024101400817), Oct 11, 2024: PRESSURE VALVE. DEFECTIVE. MAIN HYDRAULICS: UPON APPROACH INTO CHO WE ATTEMPTED TO BRING THE FLAPS TO 15° AND THEY DID NOT MOVE. WE ATTEMPTED TO LOWER THE LANDING GEAR. THE HANDLE CAME D - [SDR DXTA2024100100718](https://openairdocs.org/sdr/DXTA2024100100718), Sep 30, 2024: INDICATOR. OUT OF ADJUST. CABIN DOOR LOCKED FLAG THAT IS IN THE STEP IS EXACTLY OPPOSITE TO DOOR FUNCTION. WHEN CABIN DOOR IS UNLOCKED FLAG INDICATES DOOR LOCKED. WHEN DOOR IS LOCKED, FL - [SDR 2TJR202405147481](https://openairdocs.org/sdr/2TJR202405147481), May 14, 2024: STRINGER. CRACKED. DURING INSPECTION FOUND FUSELAGE STRINGER 15L IS CRACKED ON THE AFT END OF THE TAIL CONE SECTION AT F.S. 580.00. TRIMMED DAMAGED STRINGER AND PERFORMED A DOUBLE - [SDR DXTA2023103099300](https://openairdocs.org/sdr/DXTA2023103099300), Oct 30, 2023: SWITCH. DEFECTIVE. AFTER SHUTTING MAIN CABIN DOOR, THE CABIN DOOR LIGHT REMAINS ILLUMINATED. INTTERMINTLY THE TOP CENTER AND BOTTOM CENTER LIGHTS ON THE CABIN DOOR INDICATORS REMA - [SDR DXTA2023070590320](https://openairdocs.org/sdr/DXTA2023070590320), Jul 3, 2023: UNKNOWN. UNKNOWN. MAIN ENTRANCE DOOR AFT "EXIT" LIGHT IS INOP. ALL OTHER LIGHTS WORK. ARRIVED AT AC. POWERED ON AC AND CONFIRMED DISCREPANCY. GAINED ACCESS TO LIGHT ASSEMBLY. FOU - [SDR DXTA2023053187420](https://openairdocs.org/sdr/DXTA2023053187420), May 31, 2023: UNKNOWN. UNKNOWN. LAV EXIT SIGN/LIGHT: THE SMALL LIGHTED EXIT SIGN MOUNTED ON THE FRONT FASCIA IS INOP.//CORRECTIVE ACTION//FOUND MOLEX PIN 1 OF CONNECTOR J964V PUSHED OUT.RE-TER - [SDR EBVR202305180002](https://openairdocs.org/sdr/EBVR202305180002), May 18, 2023: FLAP. DEBONDED. ON LH OB FLAP 1.6 INCHES FROM INBOARD EDGE NEAR DATA TAG, THERE WAS A SPOT OF DISBONDING 7.6 INCHES SQUARE. AQRD REPAIRED AND REPAINTED THE FLAP IAW AQRD RS-825 - [SDR EBVR202305090451](https://openairdocs.org/sdr/EBVR202305090451), May 9, 2023: UNKNOWN. UNKNOWN. EMERGENCY EXIT DOOR SURROUND DOUBLER WAS CHAFFED BY SCREWS ON THE INTERIOR OF THE EMERGENCY EXIT INTERIOR REVEAL PANEL. TWO OF THESE CHAFES WERE IN AN AREA WHER - [SDR EBVR20230509450](https://openairdocs.org/sdr/EBVR20230509450), May 9, 2023: RUDDER. CRACKED. ON VISUAL INSPECTION DRIVEN OFF OF AAIP, FOUND CRACK IN LOWER TRAILING EDGE SKIN APPROXIMATELY 0.6 INCHES IN LENGTH. PERFORMED AN EXTERNAL DOUBLER REPAIR OVER T - [SDR DXTA2023041484200](https://openairdocs.org/sdr/DXTA2023041484200), Apr 13, 2023: SOLENOID. DEFECTIVE. PRIOR TO DEPARTURE, GOT A CABIN DOOR ANNUNCIATOR & RED 6 PACK LIGHT. BOTTOM ROW MIDDLE LIGHT FOR THE VENT DOOR. COMPLIED WITH MEL O PROCEDURES MEL 52-70-01-06. - [SDR DXTA2023030682070](https://openairdocs.org/sdr/DXTA2023030682070), Mar 8, 2023: NONE. NONE. WITH APU RUNNING WE RECEIVED AN AIR DUCT O'HEAT CAB CAUTION. CABIN TEMP WAS EXCESSIVE AND THE CABIN STARTED TO FILL WITH AN UNKNOWN SMOKE/ODOR THAT WAS EASILY V - [SDR DXTA2022031458440](https://openairdocs.org/sdr/DXTA2022031458440), Mar 13, 2022: ENGINE. DAMAGED. RIGHT ENGINE FUEL FLOW: IN FLIGHT AFTER ACTUATING THE CROSSFEED FROM LEFT TANK TO RIGHT ENGINE THE RIGHT FUEL BOOST PUMP AMBER ANNUNCIATOR ILLUMINATED STEADY AN - [SDR DXTA2021061743820](https://openairdocs.org/sdr/DXTA2021061743820), Jun 17, 2021: BOLT. UNSECURE. MAIN DOOR HARDWARE: BOLT ON THE AFT MAIN CABIN DOOR SUPPORT IS ALMOST UNSECURED. THE END ATTATCHED TO THE DOOR NOT THE AIRCRAFT DOOR FRAME. "CORRECTIVE ACTION" - [SDR DXTA2021051442030](https://openairdocs.org/sdr/DXTA2021051442030), May 14, 2021: BRAKE. WEAK. RIGHT MLG BRAKE: AT SLOW SPEED WITH MINIMUM RIGHT SEAT PILOT BRAKE APPLICATION THE RIGHT LANDING GEAR BRAKE LOCKED UP AND RELEASED TWICE IN RAPID SUCCESSION./// - [SDR DXTA2018061101059](https://openairdocs.org/sdr/DXTA2018061101059), Jun 9, 2018: UNKNOWN. ODOR. DESCENDING OUT OF 23000 FEET, DETECTED A DIRTY SOCK/BURNT OIL ODOR ALL THE WAY DOWN TO LANDING. REMOVED AND REPLACED THE CONDENSER BAG. RAN APU, NR 1 AND 2 ENGI - [SDR DXTR2017050201](https://openairdocs.org/sdr/DXTR2017050201), May 1, 2017: CHANNEL. CRACKED. MAIN CABIN DOOR FRAME STRUCTURE CRACKED BENEATH AFT SUPPORT ROD LOWER FITTING. ACCOMPLISHED MAJOR REPAIR IAW 5562/05RD. - [SDR DXTA2016102506323](https://openairdocs.org/sdr/DXTA2016102506323), Oct 25, 2016: CONTROL UNIT. DEFECTIVE. EXPERIENCED COMPLETE FAILURE OF NORMAL BRAKE SYSTEM WITH ILLUMINATION OF MASTER CAUTION AND ANTI-SKID INOP ANNUNCIATOR. THERE IS NO EVIDENCE OF FLUID LEAK. BRAK - [SDR DXTA2015051506018](https://openairdocs.org/sdr/DXTA2015051506018), May 14, 2015: BRAKE SYS. CONTAMINATED. WHEN DOING STATIC TAKEOFF AROUND 88% N1 WITH FULL APPLICATION OF BRAKES, ACFT MOVES FWD. PERFORMED BRAKE SYS BLEED IAW MM 32-44-00. PERFORMED ACFT POWER RUN, OB - [SDR DXTA212021304871](https://openairdocs.org/sdr/DXTA212021304871), Feb 10, 2012: UNKNOWN. VAPOR. WITH APU RUNNING AND BLEED AIR ON WE NOTICED LIGHT SMOKE OR VAPOR IN CABIN AND A MUSTY ODOR. TURNED BLEED AIR OFF AND SMOKE/VAPOR SEEMED TO GET WORST. SHUTDOWN - [SDR DXTA2010112404319](https://openairdocs.org/sdr/DXTA2010112404319), Nov 23, 2010: CONNECTOR. BURNED. WHEN VIDEO SCREEN AT SEAT NR3 WAS INSTALLED, SMOKE BEGAN COMING FROM SOCKET AND SHORTLY THEREAFTER FROM BEHIND CLUB TABLE. SCREEN WAS REMOVED AND SMOKE DISSIPAT - [SDR DXTA2010082304201](https://openairdocs.org/sdr/DXTA2010082304201), Aug 21, 2010: YOKE. BINDING. FROM THE RT YOKE, IN FLIGHT WITH THE AUTOPILOT ON THERE IS A VIBRATION IN THE RT YOKE AND YOU CAN FEEL A VIBRATION IN THE FLOORBOARDS AT THE BASE OF THE YOKE. Y - [SDR DXTA2009070203713](https://openairdocs.org/sdr/DXTA2009070203713), Jul 1, 2009: SENSOR. INOPERATIVE. ACM OVERHEAT LIGHT ILLUMINATES DURING TAKEOFF ROLL BETWEEN 70KTS AND V1. ALSO EXPERIENCED RUSH OF AIR IN CABIN AND COCKPIT WITH HOT AIR RUBBER ODOR. TROUBLESHOT - [SDR DXTA200702574](https://openairdocs.org/sdr/DXTA200702574), Oct 25, 2007: METERING UNIT. INTERMITTENT. AT TAXI SPEEDS OF 15 MPH AND LESS, BOTH BRAKES GRAB INTERMITTENTLY AND INDEPENDENTLY OF EACH OTHER. THE BRAKES CAUSED THE AIRCRAFT TO LURCH AND SHUDDER. REMOVED - [SDR DXTA200702427](https://openairdocs.org/sdr/DXTA200702427), Jul 29, 2007: O-RING. CUT. WITH AIR COMING OUT OF SIDE VENTS. UPPER DUCTS A BURNED ACRID SMELL AND BLUE-ISH SMOKE LIKE HAZE WAS OBSERVED IN CABIN (APU RUNNING, ENGINES OFF) FOUND HYD RESE - [SDR DXTA200601700](https://openairdocs.org/sdr/DXTA200601700), Oct 30, 2006: SWITCH. STUCK. LT GEAR INDICATED UNSAFE W/ASSOC UNLOCKED LIGHT AND NO AOA INDEXERS. ROTARY TEST LIGHTS CHECK 4.0 FOLLOWED ALL EMERGENCY PROCEDURES INCLUDING BLOW DOWN, UNSAFE - [SDR DXTA200601416](https://openairdocs.org/sdr/DXTA200601416), Jun 1, 2006: ENGINE. OIL CONSUMPTION. LT ENGINE OIL PRESSURE ANNUNCIATOR ILLUMINATED, MASTER WARNING ILLUMINATED. OIL PRESSURE FELL BELOW 20 PSI THEN CAME BACK UP AND HOVERED AT 40 PSI, SHUT ENGINE - [SDR DXTA200601295](https://openairdocs.org/sdr/DXTA200601295), Mar 13, 2006: ACTUATOR. MALFUNCTIONED. ON APPROACH WITH FLAPS AT 15 (DEG) AND 175 KTS, GEAR DOWN WAS SELECTED. LEFT MAIN AND NOSE GEAR INDICATED GREEN LIGHTS. RIGHT MAIN DID NOT LIGHT UP. NO RED UNLO - [SDR DXTA200601289](https://openairdocs.org/sdr/DXTA200601289), Mar 10, 2006: WARNING LIGHT. NO INDICATION. RIGHT MAIN LANDING GEAR LIGHT DID NOT ILLUMINATE WITH GEAR EXTENSION. CONDITION REPEATS AFTER CYCLING. BULBS CHECKED GOOD WITH ROTORY TEST. COMPLETED EMERGENCY --- 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.