# N611QS: 2005 Cessna 560XL, registration cancelled 2026-08-28 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 28, 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: 560-5548 - Year built: 2005 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: March 21, 2005 - Certificate issued: September 25, 2019 - Last registry action: September 2, 2023 - Mode S code: A7F3E4 - 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/N611QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=611QS - Page: https://openairdocs.org/deregistered/N611QS-2026-08-28 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 (31) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 2026FA0000202](https://openairdocs.org/sdr/2026FA0000202), Mar 20, 2026: SKIN. CORRODED. LOWER TAILCONE SKIN CORROSION. COMPLIED WITH NETJETS AQRD ERO-988732 REV.IR, DATED MAR.19,2026. N611QS LOWER TAILCONE SKIN CORROSION. - [SDR DXTA2026020606796](https://openairdocs.org/sdr/DXTA2026020606796), Feb 5, 2026: GAUGE. OUT OF POSITION. MAIN CABIN DOOR SIGHT GAUGE INDICATOR: WITH THE DOOR FULLY CLOSED, UNABLE TO VERIFY THE GREEN CONFIRMATION FLAG. THIS IS THE SIGHT GUAGE BELOW THE DOOR HANDLE. - [SDR DXTA2025092205004](https://openairdocs.org/sdr/DXTA2025092205004), Sep 18, 2025: SPRING. DEFECTIVE. WHILE CLOSING MED THERE WAS AN AUDIBLE NOISE FROM INSIDE THE DOOR AND IT FELL OPEN ON ITS OWN. NOW THE DOOR CANNOT BE CLOSED IT STARTS TO BIND ALMOST AS SOON AS - [SDR DXTA2025090804844](https://openairdocs.org/sdr/DXTA2025090804844), Sep 5, 2025: SPRING. LOW TENSION. MAIN CABIN DOOR IS DIFFICULT TO OPEN. IT DOES NOT FEEL LIKE IT IS BINDING BUT JUST VERY HEAVY. FROM OUTSIDE REQUIRES TWO HANDS AND EXCESSIVE FORCE TO OPEN. FROM - [SDR DXTA2025011702001](https://openairdocs.org/sdr/DXTA2025011702001), Jan 16, 2025: LIGHT. UNSECURE. FLOOR EMERG EXIT LIGHT: AFT LIGHT ON FLOOR INSIDE CABIN AT TOP OF STAIRS IS NOT SECURED IN MOUNTING. CORRECTIVE ACTION: RESECURED FLOOR EMERGENCY LIGHT. OPS CHE - [SDR DXTA2024042211575](https://openairdocs.org/sdr/DXTA2024042211575), Apr 21, 2024: HANDLE. BINDING. MAIN CABIN DOOR HANDLE ROTATES FREELY UNTIL ENGAGING AND DISENGAGING DOORS PINS. IT REQUIRES EXCESSIVE FORCE TO OPEN AND CLOSE DOOR. MORE NOTICABLE WHEN OPERATI - [SDR 2TJR202403147481](https://openairdocs.org/sdr/2TJR202403147481), Mar 14, 2024: SPAR CAP. CORRODED. DURING INSPECTION FOUND AREA OF CORROSION ON THE LH WING LOWER MAIN SPAR CAP AT W.S.121.57. PERFORMED A BLEND AND DOUBLER REPAIR IN ACCORDANCE WITH APPROVED DAT - [SDR DXTA2023081693230](https://openairdocs.org/sdr/DXTA2023081693230), Aug 16, 2023: UNKNOWN. UNKNOWN. MAIN DOOR: AFTER TAXING IN THE LINE PERSONNEL ADVISED US THE EXTERNAL DOOR HANDLE WAS HANGING DOWN. REMOVED DOOR COVER. INSPECTED DOOR HANDLE AND FOUND HANDLE N - [SDR DXTA2023061288370](https://openairdocs.org/sdr/DXTA2023061288370), Jun 12, 2023: UNKNOWN. UNKNOWN. DURING DESCENT AT FL300, PITCH TRIM FLAG ACTIVATED. TCS'D & TRIED PITCH WHEEL MANUAL DOWN, JAMMED. TRIED ELECT TRIM & DID NOT WORK. RELEASED TCS & REENGAGED AUT - [SDR DXTAT2PL6D005K07H](https://openairdocs.org/sdr/DXTAT2PL6D005K07H), Nov 28, 2017: UNKNOWN. MALFUNCTIONED. ON TAKE OFF, AFTER GEAR HANDLE WAS RAISED, THE NOSE WHEEL BANGED 4-5 TIMES ATTEMPTING TO STOW. EACH BANG FELT IN AIRFRAME AND HEARD. WITH EACH BANG, THE RED NOS - [SDR DXTA201711125HUED](https://openairdocs.org/sdr/DXTA201711125HUED), Nov 12, 2017: LIMIT SWITCH. UNSERVICEABLE. DURING TAKE OFF WITH BOTH ENGINES IN THE TAKEOFF DETENT, THE RIGHT ENGINE ONLY PRODUCED 82 PERCENT N1. THE CORRECT NUMBER FOR TEMPERATURE AND ALTITUDE SHOULD HA - [SDR DXTR2016081701](https://openairdocs.org/sdr/DXTR2016081701), Aug 16, 2016: DOOR FRAME. CRACKED. FRONT FRAME CRACKED ON MAIN CABIN DOOR. REPAIRED IAW AQRD-ENG-014, REV B ERO-853215. NO DEFECTS NOTED AT THIS TIME. - [SDR DXTA2016061406257](https://openairdocs.org/sdr/DXTA2016061406257), Jun 14, 2016: BRAKE SYS. CONTAMINATED. LEFT BRAKE PEDAL DEFLECTED 2-3" MORE THAN THE RIGHT, UPON LANDING. LEFT BRAKE PEDAL REQUIRES MORE DEFLECTION AND FEELS SPONGY COMPARED TO THE RIGHT. PERFORMED M - [SDR DXTA2015021705979](https://openairdocs.org/sdr/DXTA2015021705979), Feb 16, 2015: SWITCH. OUT OF ADJUST. LOW HYDRAULIC FLUID LEVEL LIGHT CAME ON & WOULDN'T GO OFF ALONG WITH THE CAUTION LIGHT. NO EMERGENCY EXTENSION WAS NECESSARY, DECLARED AN EMERGENCY. DID NOT OBS - [SDR DXTA2015012005964](https://openairdocs.org/sdr/DXTA2015012005964), Jan 19, 2015: TRANSMITTER. FAILED. SHORTLY AFTER LEVEL OFF AT FL350, LT ENGINE OIL PRESSURE DROPPED RAPIDLY TO THE 25 - 30 PSI RANGE. INDICATOR BAR TURNED AMBER. OIL PRESSURE REMAINED IN THIS RAN - [SDR DXTA2014082705868](https://openairdocs.org/sdr/DXTA2014082705868), Aug 22, 2014: SPAR CAP. CORRODED. LEFT & RIGHT WING UPPER SPAR CAP TOP SURFACE HAS CORROSION. ACCOMPLISHED REPAIR TO THE LT AND RT WING UPPER SPAR CAP TOP SURFACE CORROSION AREAS IAW S-560XL-554 - [SDR DXTA2014021305652](https://openairdocs.org/sdr/DXTA2014021305652), Feb 12, 2014: METERING VALVE. LEAKING. AFTER LANDING, ON TAXI INTO THE FBO THE PIC'S LT TOE BRAKE WENT ALL THE WAY TO THE FLOOR WITH NO PRESS. PRESS SEEMED TO RETURN TO THE BRAKE PEDALS AFTER I PUMPE - [SDR CWQR20100308014](https://openairdocs.org/sdr/CWQR20100308014), Mar 8, 2012: HINGE. CORRODED. DURING A SCHEDULED INSPECTION, FOUND CORROSION ON THE FWD CABIN DOOR HINGE FROM THE CORNER EDGE OF THE PART TO BEYOND THE FIRST FASTENER ATTACH HOLE, BEYOND ALL - [SDR CWQR20120306015](https://openairdocs.org/sdr/CWQR20120306015), Mar 6, 2012: HINGE. CORRODED. DURING A SCHEDULED INSPECTION, FOUND CORROSION ON THE AFT CABIN DOOR HINGE FROM THE CORNER EDGE OF THE PART TO BEYOND THE FIRST FASTENER ATTACH HOLE. BEYOND ALL - [SDR DXTR20120302001](https://openairdocs.org/sdr/DXTR20120302001), Mar 2, 2012: HINGE FITTING. CORRODED. CABIN DOOR AFT LOWER HINGE AIRFRAME SIDE, UPPER FORWARD CORNER CORRODED. - [SDR DXTA2011102604764](https://openairdocs.org/sdr/DXTA2011102604764), Oct 25, 2011: CONNECTOR. UNSECURE. INTERMITTENT FIRE LIGHT TEST ON LT ENGINE. FOUND LOCKING COLLAR ON LT FIRE DETECTION CONTROL UNIT CONNECTOR WAS UNLOCKED AND UNSECURE. RESECURED AND LOCKED CONN - [SDR DXTA2011080404684](https://openairdocs.org/sdr/DXTA2011080404684), Aug 3, 2011: BEARING. SEIZED. IN FLIGHT WHEN LANDING GEAR EXTENDED, A LOUD CLUNKING NOISE HEARD IN COCKPIT. ON GROUND IF YOU WIGGLE THE RT NLG DOOR, SAME CLUNKING NOISE IN THE GEAR DOOR LINK - [SDR DXTA2010090204216](https://openairdocs.org/sdr/DXTA2010090204216), Sep 1, 2010: CONTROL HANDLE. FAILED. UNABLE TO RETRACT LANDING GEAR AFTER TAKEOFF. GEAR HANDLE STUCK IN THE DOWN POSITION. APPEARS TO BE A SQUAT SWITCH ISSUE. JACKED ACFT AND SWUNG GEAR. NO DEFECTS - [SDR DXTA2010071504155](https://openairdocs.org/sdr/DXTA2010071504155), Jul 14, 2010: CONTROL CABLE. BROKEN. ON DESCENT FOR APPROACH, THE PITCH TRIM LIGHT ON THE PFD CAME ON. AFTER DISCONNECTING AUTOPILOT, THE ELECTRIC TRIM DID NOT MOVE THE TRIM WHEEL. PITCH TRIM CIRCU - [SDR DXTA2009021703508](https://openairdocs.org/sdr/DXTA2009021703508), Feb 16, 2009: ACTUATOR. OUT OF ADJUST. AFTER TAKEOFF, WHEN LANDING GEAR HANDLE SELECTED UP, ALL THREE GREEN LIGHTS WENT OUT, RED UNLOCK LIGHT REMAINED ON. FOUND THE LT MAIN SIDE BRACE ACTUATOR OUT OF - [SDR DXTA20082927](https://openairdocs.org/sdr/DXTA20082927), Mar 9, 2008: APU. SMOKE. APU RUNNING, WITH BLEED ON AND ENGINES RUNNING, SMOKE ENTERED THE CABIN. REMOVED AND REPLACED APU. SERVICED OIL TO FULL. OPERATIONAL AND LEAK CHECK GOOD. WORK P - [SDR DXTA20082913](https://openairdocs.org/sdr/DXTA20082913), Mar 4, 2008: APU. OVERSERVICED. WHILE RUNNING APU, ELECTRICS AND BLEED ON, RT WING O'HEAT ANN ILLUMINATED. RAN BOTH ENGINES W/APU ELECTRICS AND BLEED ON, O`HEAT ANN DID NOT ILLUMINATE, BUT STR - [SDR DXTA200702437](https://openairdocs.org/sdr/DXTA200702437), Aug 31, 2007: OIL SYSTEM. LEAKING. APU AUTOMATICALLY SHUTDOWN IN FLIGHT DUE TO AN OVERHEAT. SMOKE FROM OVER-HEATED APU ENTERED CABIN. UPON VISUAL INSPECTION OF APU FOUND APU OIL TO BE LOW. ADDED - [SDR DXTA200601658](https://openairdocs.org/sdr/DXTA200601658), Oct 14, 2006: ACTUATOR. NO INDICATION. WHEN GEAR SELECTED DOWN, RIGHT MAIN GEAR DOWN LIGHT DID NOT COME ON AND RED UNLOCK LIGHT ILLUMINATED. CHECKLIST ACCOMPLISHED, BOTTLE BLOWN BUT INDICATIONS REMAI - [SDR DXTA200601325](https://openairdocs.org/sdr/DXTA200601325), Mar 30, 2006: ENGINE. LOW PRESSURE. AFTER TAKEOFF AT CLIMB-OUT POWER DETENT, LT LOW OIL PRESSURE ANNUNCIATER ILLUMINATED. LOW PRESSURE WAS VERIFIED ON TAPE, DIGITS WERE RED AND PRESSURE WAS ZERO. - [SDR DXTA200601200](https://openairdocs.org/sdr/DXTA200601200), Jan 16, 2006: INDICATOR. ACTIVATED. PRIOR TO LANDING GEAR INDICATORS SHOWED GEAR UNSAFE LIGHT AND NO LEFT MAIN LIGHT CHECKED OK W/ ROTARY TEST. RAN CHECKLIST CONDITION REMAINED. CONDITION CLEARED --- 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.