# N689QS: 2006 Cessna 560XL, registration cancelled 2026-07-21

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 21, 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: 560-5659
- Year built: 2006
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 2, 2006
- Certificate issued: March 16, 2026
- Last registry action: March 16, 2026
- Mode S code: A92615
- 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/N689QS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=689QS
- Page: https://openairdocs.org/deregistered/N689QS-2026-07-21

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 (33)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DXTA2026021606905](https://openairdocs.org/sdr/DXTA2026021606905), Feb 14, 2026: SIGN. INOPERATIVE. EMERGENCY EXIT SIGN LIGHT ON FRONT OF LAV IS INOP CORRECTIVE ACTION: REMOVED OLD LAV EXIT LIGHT AND INSTALLED A NEW EXIT LIGHT. FUNCTION TEST IS GOOD AT THIS TI
- [SDR DXTA2026011306507](https://openairdocs.org/sdr/DXTA2026011306507), Jan 11, 2026: OUTFLOW VALVE. FAULTY. ON DEPARTURE CABIN WAS NOT PRESSURIZING AND THE RATE OF CLIMB INDICATOR WAS MIRRORING THE AIRCRAFTS VERTICAL SPEED. WE TRIED MANUAL PRESS AND THE CHERRY PICKER 
- [SDR DXTA2025102105356](https://openairdocs.org/sdr/DXTA2025102105356), Oct 18, 2025: WHEEL. DEFECTIVE. NEW NOSE TIRE INSTALLED BEFORE FLIGHT. UPON TAKEOFF AND SELECTING GEAR UP HEARD LOUD NOSE WHEEL SPINDOWN AND FELT ASSOCIATED VIBRATION. NOISE CONTINUED FOR SEVE
- [SDR DXTA2025100205141](https://openairdocs.org/sdr/DXTA2025100205141), Sep 29, 2025: LIGHT. INOPERATIVE. LEFT FLOOR EMERGENCY EXIT LIGHT STRIP OUT WITH BOTH CABIN AND EMER LIGHTS. REPEAT WRITEUP. POWERED ON THE EMER LIGHTS AND FOUND THE DROP AISLE LIGHTS TO BE WORK
- [SDR DXTA2025093005125](https://openairdocs.org/sdr/DXTA2025093005125), Sep 28, 2025: ELEC CONNECTOR. NOT SEATED. LEFT FRONT FLOOR AISLE EMERGENCY LIGHTS INOPERATIVE. GAINED ACCESS TO FORWARD AISLE EMERGENCY LIGHT, AND LOCATED CONNECTOR. FOUND CONNECTOR PIN NOT SEATED IN CO
- [SDR DXTA2025092405035](https://openairdocs.org/sdr/DXTA2025092405035), Sep 20, 2025: PIN. FOD. AFTER LANDING, MAIN CABIN DOOR WAS VERY DIFFICULT TO OPEN AND CREW WAS UNABLE TO LOCK THE DOOR FROM THE INSIDE. TECHS CLEANED ALL DIRT AND DEBRIS FROM THE LOCKI
- [SDR DXTA2025081504610](https://openairdocs.org/sdr/DXTA2025081504610), Aug 14, 2025: FLOAT. INOPERATIVE. ON CLIMB OUT WE RECEIVED A LO FUEL LEVEL L LIGHT. WE RAN THE QRH WHICH SAID TO TURN ON THE BOOST PUMP AND LAND AS SOON AS POSSIBLE. BOTH FUEL LEVELS APPEARED CO
- [SDR 2025FA0000359](https://openairdocs.org/sdr/2025FA0000359), May 16, 2025: DECK PLATE. CORRODED. FOUND CORROSION ON POTTY DECK LOWER SURFACE DURING 24MO INSPECTION. MEASURED, MAPPED, AND SUBMITTED POTTY DECK LOWER SURFACE CORROSION TO ENGINEERING FOR REPAIR
- [SDR DXTA2025012001995](https://openairdocs.org/sdr/DXTA2025012001995), Jan 16, 2025: LANDING GEAR. COLLAPSED. MLG: AIRCRAFT WAS BEING TOWED INTO A HANGAR BY THE PORT OF EPHRATA AIRPORT. WHILE THE AIRCRAFT WAS BEING PUSHED BACK THE RIGHT MAIN LANDING GEAR WAS ROLLED BACK
- [SDR DXTA2025010201760](https://openairdocs.org/sdr/DXTA2025010201760), Dec 28, 2024: METERING VALVE. DEFECTIVE. FIRST OFFICER MLG BRAKE PEDAL: WHEN APPLYING EQUAL PRESSURE TO BOTH BRAKE PEDALS THE RIGHT BRAKE APPLIES HEAVIER BRAKING THAN THE LEFT BRAKE CAUSING AIRCRAFT TO
- [SDR DXTA2023080492270](https://openairdocs.org/sdr/DXTA2023080492270), Aug 4, 2023: UNKNOWN. UNKNOWN. RIGHT EXTERIOR EMERG LIGHT: RIGHT WING AFT CIRCULAR EXTERIOR EMERGENCY LIGHT IS VERY DIM COMPARED TO THE TWO FORWARD WING EMERGENCY LIGHTS. ALL WING EMERGENCY L
- [SDR DXTA2023060187470](https://openairdocs.org/sdr/DXTA2023060187470), Jun 1, 2023: LIGHT. DEFECTIVE. DC GENERATION AND CONTROL: WHEN BATTERY POWER TURNED ON THERE IS SMOKE COMING FROM TOP OF ENTRANCE STAIRS WHERE THE EMERGENCY EGRESS LIGHTS ARE WHERE THE CARPET
- [SDR DXTA2023053087320](https://openairdocs.org/sdr/DXTA2023053087320), May 30, 2023: UNKNOWN. UNKNOWN. AFTER CLEARED FOR TAKEOFF, POWERED UP SLIGHTLY TO TAXI ONTO RUNWAY & IMMEDIATELY HAD A STRONG BURNING ODOR IN COCKPIT. CLEARED RUNWAY & SHUTDOWN APU & ODOR ABAT
- [SDR DXTA2023032082780](https://openairdocs.org/sdr/DXTA2023032082780), Mar 17, 2023: WINDSHIELD. DAMAGED. LEFT HAND SIDE HEATED WINDOW APPEARS TO BE CRACKED. DURING FLIGHT IT ARCED FROM THE BOTTOM AND WE TURNED THE WINDSHIELD HEAT OFF. REMOVED FAILED L/H SIDE WINDOW
- [SDR DXTA2023021380410](https://openairdocs.org/sdr/DXTA2023021380410), Feb 11, 2023: UNKNOWN. UNKNOWN. MAIN DOOR PRECATCH: MAIN CABIN DOOR PRE-CATCH HANDLE IS LOOSE. PERFORMED OPERATIONAL CHECK ON MED PRECATCH. ALL OPERATIONAL CHECKS ARE GOOD. TECH VERIFIED HANDL
- [SDR DXTA2023021080330](https://openairdocs.org/sdr/DXTA2023021080330), Feb 10, 2023: BRAKE. DEFECTIVE. LEFT MLG BRAKE HARDWARE: LEFT MAIN LANDING GEAR BRAKE IS LEAKING HYDRAULIC FLUID. AFTER LANDING HYDRAULIC FLUID WAS LEAKING ON THE LEFT BRAKE CAUSING IT TO SMOK
- [SDR DXTA2022091970590](https://openairdocs.org/sdr/DXTA2022091970590), Sep 16, 2022: NONE. NONE. MAIN DOOR PRECATCH: WILL NOT RELEASE WHEN AIR ON. // SIGNOFF// CONDUCTED OPS CHECK ON MAIN DOOR IAW CE-560XL AMM 52-10-00. NO DISCREPANCIES FOUND. MCC APPROVED 
- [SDR DXTA2022020156020](https://openairdocs.org/sdr/DXTA2022020156020), Jan 31, 2022: NOT REPORTED. NOT REPORTED. MAIN DOOR PRECATCH: MAIN CABIN DOOR IS HANGING ON THE PRE CATCH. WITH BLEED AIR ON IT ALWAYS CATCHES. WITH BLEED AIR OFF IT IS INTERMITTENT. // SIGNOFF//ACCESSE
- [SDR DXTA2019081902767](https://openairdocs.org/sdr/DXTA2019081902767), Aug 16, 2019: FUEL CONTROL. LEAKING. FUEL VENT - HEAVY FUEL FUMES IN CABIN AND COCKPIT DURING FLIGHT. REMOVED AND REPLACED APU FUEL CONTROL AND APU FUEL MANIFOLD.
- [SDR JGVR20190723001](https://openairdocs.org/sdr/JGVR20190723001), Jul 23, 2019: ACCESS PANEL. CRACKED. FOUND VERTICAL STABILIZER ACCESS PANELS 340ER AND 340FR TO HAVE CRACKS IN THE FASTENER HOLES, REPLACED CRACKED PANELS WITH TWO NEW P/N 5531005-3.
- [SDR DXTA2018090501382](https://openairdocs.org/sdr/DXTA2018090501382), Sep 3, 2018: MANIFOLD. LEAKING. GAS SMELL COMING FROM GASPERS IN COCKPIT ENTIRE FLIGHT. FOUND FUEL MANIFOLD LEAKING. INSTALLED NEW FUEL MANIFOLD ASSY SECONDARY TUBE P/N: 3883899-1.
- [SDR DXTA201711070001](https://openairdocs.org/sdr/DXTA201711070001), Oct 25, 2017: PUMP. FAILED. DURING TAXI, THE ANTI-SKID LIGHT ILLUMINATED FOLLOWED BY POWER CIRCUIT BREAKER. LOW BRAKE PRESSURE ILLUMINATED. FINALLY EMERGENCY BRAKE HAD TO BE USED TO STOP T
- [SDR DXTA2016082906294](https://openairdocs.org/sdr/DXTA2016082906294), Aug 29, 2016: DISPLAY. MALFUNCTIONED. DURING FERRY FLIGHT WITH INOPERATIVE PRESSURIZATION, ACM, AND TEMPERATURE CONTROL AT FL100 NR 1 PFD STARTED TO DEVELOP A HOT SPOT IN CENTER OF SCREEN AS IF OVER
- [SDR DXTA2014040905723](https://openairdocs.org/sdr/DXTA2014040905723), Apr 5, 2014: STRUCTURE. DAMAGED. LARGE BIRD STRIKE DURING LANDING PHASE. LARGE DENT IN LE OF LT STABILIZER. INSPECTED & FOUND DAMAGE TO LE & RIB ASSEMBLY. REPAIRED AND OPS CHECKED GOOD IAW MM 5
- [SDR DXTA2013120505592](https://openairdocs.org/sdr/DXTA2013120505592), Dec 6, 2013: ACTUATOR. FAULTY. AT FL400 PITCH MISTRIM ANNUNCIATED IN OUR PFDS. UPON DISCONNECTING THE AUTOPILOT, THE ACFT PITCHED DOWN. NEEDED SIGNIFICANT BACK PRESS TO HOLD ALTITUDE. NOTICED
- [SDR DXTA2012110705172](https://openairdocs.org/sdr/DXTA2012110705172), Nov 6, 2012: APU. ODOR. WITH THE APU RUNNING AND THE AVIONICS ON, COCKPIT AND THEN CABIN FILLED WITH SMOKE. SMOKE APPEARED TO BE COMING FROM THE GLARE SHIELD AREA AND FILLED THE COCKPI
- [SDR DXTA2012030904913](https://openairdocs.org/sdr/DXTA2012030904913), Mar 8, 2012: COALESCER BAG. ODOR. PAX DESCRIBED A STRONG ACRID BLEED AIR ODOR IN THE CABIN ON TAKEOFF. CLEANED COALESER SOCK IN WATER SEPERATOR. OPS CHECK OF ECS OK WITH ENGINES AND APU. WORK PE
- [SDR DXTA2011070504642](https://openairdocs.org/sdr/DXTA2011070504642), Jul 2, 2011: BRAKE SYS. MALFUNCTIONED. RT BRAKE GRABS HARD ON HIGH SPEED LANDING ROLLOUT AND TAXIING. RT BRAKE GRABS HARD ON HIGH SPEED LANDING ROLLOUT AND TAXIING. , BLED BRAKES AND CHECK SYS IAW MM
- [SDR DXTA2010042604075](https://openairdocs.org/sdr/DXTA2010042604075), Apr 23, 2010: BRAKE ASSY. WEAK. BRAKE PEDALS FEEL MUSHY. THEY REQUIRE SIGNIFICANTLY MORE PRESSURE THAN NORMAL TO BRAKE THE AIRPLANE. ALL 4 PEDALS FEELS THE SAME. INSPECTED BRAKE SYS FOR LEAKS,
- [SDR DXTA2009100603806](https://openairdocs.org/sdr/DXTA2009100603806), Oct 5, 2009: HMU. INOPERATIVE. DURING CRUISE AT 3000', REDUCED POWER TO APPROX 60% FOR A SPEED REDUCTION IN SMOOTH AIR, NO TURBULENCE, WITH IGNITIONS ON, THE LEFT ENGINE (QUIT WORKING) SPOOLE
- [SDR DXTA2009032703573](https://openairdocs.org/sdr/DXTA2009032703573), Mar 31, 2009: SHIMMY DAMPENER. MALFUNCTIONED. ON TAKEOFF ROLL AT JUST PRIOR TO 40 KTS THE NOSE WHEEL STARTS A VERY EXCESSIVE VIBRATION. FOUND SHIMMY DAMPER LEAKING FLUID, NO FLUID LEFT. REMOVED AND REPLACED
- [SDR DXTA200803255](https://openairdocs.org/sdr/DXTA200803255), Aug 30, 2008: SWITCH. ACTIVATED. DURING APPROACH LOWERED FLAPS TO 15` AND STAB MISCOMPARE CAUTION LT ILLUMINATED. VERIFIED DISCREPANCY. STAB DID NOT MOVE WHEN FLAPS WERE LOWERED AND RAISED. ACC
- [SDR DXTA200702147](https://openairdocs.org/sdr/DXTA200702147), Apr 26, 2007: INDICATION SYS. MALFUNCTIONED. GREEN LT GEAR POSITION INDICATOR LIGHT REMAINED ILLUMINATED AFTER GEAR RETRACTION ON TAKEOFF. [SUP 05-02-07] INSTALLED MLG CONTROLLER (REPAIRED) AND INSPECTED A

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20140405004569I](https://openairdocs.org/incident/20140405004569I), Apr 5, 2014: Cessna 560XL (N689QS), Charlotte, NC, Minor damage. Bird strike to left horizontal stabilizer leading edge which dented the leading edge causing minor damage. Leading edge skin will require repair or…

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