# N698QS: 2006 Cessna 560XL, registration cancelled 2025-07-07

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 7, 2025
- 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: 560-5653
- Year built: 2006
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 29, 2006
- Certificate issued: November 17, 2020
- Last registry action: August 2, 2023
- Mode S code: A949DD
- 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/N698QS
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=698QS
- Page: https://openairdocs.org/deregistered/N698QS-2025-07-07

From the FAA registry file of November 3, 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 (44)

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

- [SDR DXTA2025030302554](https://openairdocs.org/sdr/DXTA2025030302554), Mar 2, 2025: DOOR. DAMAGED. MAIN DOOR: WHEN OPENING MAIN CABIN DOOR , ONCE THE DOOR PINS RELEASE THE DOOR WILL FALL OPEN RAPIDLY TO ABOUT 1 FOOT FROM FULLY OPEN POSITION. WHEN CLOSING CABI
- [SDR DXTA2025022402449](https://openairdocs.org/sdr/DXTA2025022402449), Feb 20, 2025: RUB STRIP. WORN. MAIN CABIN DOOR DOES NOT OPEN WHEN MOVING THE HANDLE TO THE OPEN POSITION UNLESS YOU PULL THE PRE-CATCH THEN THE DOOR WILL OPEN. THIS HAPPENS FROM THE OUTSIDE A
- [SDR DXTA2025022002400](https://openairdocs.org/sdr/DXTA2025022002400), Feb 16, 2025: LATCH. OUT OF ADJUST. MAIN DOOR: REPEAT WRITE UP. MAIN ENTRY DOOR HANDLE IS DIFFICULT TO LOCK AND UNLOCK AND VERY DIFFICULT TO UNLOCK OR LOCK AFTER COLD SOAK FLIGHT. VIDEO ATTACHED. 
- [SDR DXTA2024122001555](https://openairdocs.org/sdr/DXTA2024122001555), Dec 16, 2024: DOOR. OUT OF ADJUST. MAIN DOOR: MAIN CABIN DOOR WILL NOT OPEN WITHOUT USING PRECATCH BOTH FROM OUTSIDE AND INSIDE. ADJUSTED DOOR IAW AMM 52-10-00
- [SDR DXTA2024120201301](https://openairdocs.org/sdr/DXTA2024120201301), Nov 26, 2024: PRECATCH. OUT OF ADJUST. MAIN DOOR HANDLE: THE AMOUNT OF FORCE REQUIRED TO LOCK OR OPEN THE MAIN CABIN DOOR IS EXCESSIVE. CORRECTIVE ACTION; ADJUSTED MAIN DOOR PRE-CATCH MECHANISM IAW C
- [SDR DXTA2024112601235](https://openairdocs.org/sdr/DXTA2024112601235), Nov 11, 2024: HANDLE. BINDING. MAIN CABIN DOOR HANDLE REQUIRES EXCESSIVE FORCE TO OPEN AND CLOSE FROM INSIDE OF CABIN. MAIN DOOR: MAIN CABIN DOOR HANDLE REQUIRED TRIED ADJUSTING AFT LOWER SOC
- [SDR DXTA2024111401124](https://openairdocs.org/sdr/DXTA2024111401124), Nov 11, 2024: DOOR. BINDING. MAIN CABIN DOOR HANDLE REQUIRES EXCESSIVE FORCE TO OPEN AND CLOSE FROM INSIDE OF CABIN. OPS CHECK DOOR AND VERIFIED DOOR STRUGGLES TO CLOSE AND OPEN. SEEMS TO B
- [SDR DXTA2024090300393](https://openairdocs.org/sdr/DXTA2024090300393), Aug 30, 2024: SWITCH. DEFECTIVE. STAB MISCOMPARE LIGHT: ON 5 MILE FINAL PRIOR TO LANDING, WE GOT THE STAB MISCOMPARE ANNUNCIATOR LIGHT AND ALSO THE HYD PRESS LIGHT ( FLASHING ). TOOK A LOT OF C
- [SDR DXTA2024062412149](https://openairdocs.org/sdr/DXTA2024062412149), Jun 24, 2024: WARNING MESSAGE. FALSE ACTIVATION. DURING TAXI TO ACTIVE RUNWAY THE LO BRK PRESS AND ANTI SKID INOP WARING LIGHTS CAME ON. TRIED STOPPING AIRCRAFT WITH TOE BRAKES BUT THEY WHERE INOP. STOPPED AIR
- [SDR DXTA2024030111052](https://openairdocs.org/sdr/DXTA2024030111052), Feb 29, 2024: PUMP. LEAKING. LEFT MLG LANDING GEAR EXTENSION: PERFORMED EMERGENCY LANDING GEAR EXTENSION DUE TO NO HYDRAULIC FLUID. HYD LOW LVL AND BOTH HYD LOW FLO ANNUCIATORS ILLUMINATED 
- [SDR DXTA202403011105](https://openairdocs.org/sdr/DXTA202403011105), Feb 29, 2024: HYDRAULIC SYSTEM. LEAKING. LEFT MLG LANDING GEAR EXTENSION: PERFORMED EMERGENCY LANDING GEAR EXTENSION DUE TO NO HYDRAULIC FLUID. HYD LOW LVL AND BOTH HYD LOW FLO ANNUCIATORS ILLUMINATED 
- [SDR DXTA2024030111051](https://openairdocs.org/sdr/DXTA2024030111051), Feb 29, 2024: PUMP. FAILED. HYDRAULIC RESERVOIR: DURING FLIGHT AT FLIGHT LEVEL 400 WE RECEIVED A HYD LOW LVL ANNUCIATOR. WE RAN THE QRH AND ANNUCIATOR REMAINED ON. REMOVED UH EDP PN 991206
- [SDR DXTA2024022010939](https://openairdocs.org/sdr/DXTA2024022010939), Feb 20, 2024: WINDSHIELD. FAILED. CAPTAIN COCKPIT WINDOW SHATTERED IN FLIGHT. WE HAD A L W/S FAULT ANNUNCIATOR COME ON WITH ASSOCIATED MASTER CAUTION. WE RAN THE ASSOCIATED QRH AND THE ANNUNCIAT
- [SDR DXTA2023122810455](https://openairdocs.org/sdr/DXTA2023122810455), Dec 27, 2023: UNKNOWN. UNKNOWN. MAIN ENTRANCE DOOR IS HARD TO LATCH AND UNLATCH. ESPECIALLY FROM THE INSIDE. PERFORMED SEVERAL OPS CHECK OF THE MAIN ENTRANCE DOOR WITH NO DISCREPANCIES TO NOTE
- [SDR DXTA2023090594650](https://openairdocs.org/sdr/DXTA2023090594650), Sep 4, 2023: UNKNOWN. UNKNOWN. MAIN DOOR: MAIN DOOR EXTREMELY DIFFICULT TO CLOSE FROM THE INSIDE. THE HANDLE CLOSES FINE THE FIRST 45 DEGREES THEN MEETS VERY STIFF RESISTANCE. THE MAIN DOOR C
- [SDR DXTA2023080492260](https://openairdocs.org/sdr/DXTA2023080492260), Aug 4, 2023: UNKNOWN. UNKNOWN. EMERG EXIT SIGN/LIGHT: EXIT SIGN TO LEFT OF MAIN ENTRY DOOR WILL NOT ILLUMINATE IN ANY SWITCH CONFIGURATION. GAINED ACCESS TO EXIT SIGN TO LEFT OF MAIN ENTRY DO
- [SDR DXTA2023072191430](https://openairdocs.org/sdr/DXTA2023072191430), Jul 21, 2023: UNKNOWN. UNKNOWN. MAIN CABIN DOOR ACOUSTIC SEAL WILL NOT RELEASE AFTER SHORT FLIGHT WITH SERVICE AIR ON. DOOR CANNOT BE OPENED WHILE APU WAS RUNNING. HAD TO SHUT DOWN APU TO REMO
- [SDR EBVR202305160001](https://openairdocs.org/sdr/EBVR202305160001), May 16, 2023: UNKNOWN. UNKNOWN. FOUND CORROSION ON LH/RH WING UPPER SURFACE ALONG FS 335.38 OVER MAIN WING SPAR. DAMAGE SUBMITTED TO TEXTRON AND REPAIRED IAW TEXTRON FIELD REPAIR FR-560-5653-1
- [SDR 3J7R2023021700001](https://openairdocs.org/sdr/3J7R2023021700001), Feb 17, 2023: BATTERY PACK. DEPLETED. REAR CABIN AND EXTERIOR EMERGENCY LIGHTS INOP WHEN MAIN BATTERY IS OFF. LIGHTS WORK NORMALLY WHEN MAIN BATTERY IS ON.
- [SDR DXTA2022060263150](https://openairdocs.org/sdr/DXTA2022060263150), Jun 2, 2022: FAN. SHORTED. COCKPIT ODOR: JUST PRIOR TO TAKEOFF THE APU WAS SHUTDOWN AND THE COCKPIT RECIRC FAN TURNED TO THE HIGH POSITION. NOTICED AT THE END OF TAKEOFF ROLL A ELECTRICAL
- [SDR DXTA2021081647000](https://openairdocs.org/sdr/DXTA2021081647000), Aug 15, 2021: LOCK BOLT. LOOSE. MAIN CABIN DOOR EXTREMELY HARD TO CLOSE FROM OUTSIDE AS WELL AS INSIDE. INSPECTED DOOR BOLT SYSTEM PINS, FOUND DIRTY AND DRAGGING. CLEANED AS NEEDED, GAINED ACC
- [SDR DXTA2021061443550](https://openairdocs.org/sdr/DXTA2021061443550), Jun 14, 2021: CABLE. DEFECTIVE. LEFT ENGINE FIRE DETECTION LIGHT: IN FLIGHT CLIMBING TO 10000' THE LEFT FIRE RED LIGHT CAME ON. ACCOMPLISHED ENTIRE INFLIGHT ENGINE FIRE QRC & ENGINE INOP APPRO
- [SDR JGVR2020012017004](https://openairdocs.org/sdr/JGVR2020012017004), Jan 17, 2020: AXLE. CORRODED. FOUND CORROSION ON THE LT MAIN LANDING GEAR AXLE. REPLACED CORRODED AXLE WITH NEW P/N 6641646-1.
- [SDR JGVR2020012017003](https://openairdocs.org/sdr/JGVR2020012017003), Jan 17, 2020: HINGE. CORRODED. FOUND CORROSION ON THE MAIN ENTRY DOOR FORWARD HINGE ON THE FUSELAGE SIDE HINGE-HALF. BLENDED CORRODED AREA, PERFORMED NDT AND REPORTED RESULTS FOR DISPOSITION.
- [SDR JGVR202001197002](https://openairdocs.org/sdr/JGVR202001197002), Jan 17, 2020: STIFFENER. CRACKED. FOUND CRACKED STIFFENER NEAR THE AFT COUNTERBALANCE SPRING OF THE MAIN ENTY DOOR. REPAIRED STIFFENER BY CUTTING OUT THE CRACKED AREA AND INSTALLING REPAIR DOUBL
- [SDR JGVR202001197001](https://openairdocs.org/sdr/JGVR202001197001), Jan 17, 2020: TRUNNION. CORRODED. FOUND CORRODED AREAS ON THE RT MAIN LANDING GEAR TRUNNION AT THE UPPER BRAKE LINE BAND CLAMP, REMOVED CLAMP BLENDED AREA AND TREATED IAW REPAIR MEMO.
- [SDR DXTA2019062412525](https://openairdocs.org/sdr/DXTA2019062412525), Jun 21, 2019: THROTTLE. OBSTRUCTED. RIGHT ENGINE POWER LEVER STUCK - ON LANDING ROLLOUT, ATC GAVE CLEARANCE TO MAKE NEXT LEFT TURN. THE RIGHT SEAT PILOT ADVANCED THE RIGHT THROTTLE TO ASSIST THE T
- [SDR DXTA2019FA0000061](https://openairdocs.org/sdr/DXTA2019FA0000061), Mar 11, 2019: FLOORBOARD. CRACKED. REPAIR OF LEFT FORWARD COCKPIT FLOORBOARD DAMAGE (CRACK). ENGINEERING LETTER DQ18712M1 DATED MAR 6, 2019.
- [SDR DXTA2015102606114](https://openairdocs.org/sdr/DXTA2015102606114), Oct 25, 2015: BRAKE SYS. MALFUNCTIONED. UPON INITIAL TAKEOFF ROLL THE ACFT PULLED TO THE RT. AT 30 KNOTS THE TAKEOFF WAS ABORTED. DURING THE ABORT THE ACFT PULLED HARD LT. UPON EXITING THE RUNWAY IT S
- [SDR DXTA2014050205757](https://openairdocs.org/sdr/DXTA2014050205757), Apr 13, 2014: DOOR FRAME. CHAFED. CHAFE ON DOOR FRAME STRUCTURE ABOVE & FWD OF DOOR. REPAIRED IAW RD 5653 04RD.
- [SDR CWQR20131016044](https://openairdocs.org/sdr/CWQR20131016044), Oct 16, 2013: HINGE. CRACKED. DURING A SCHEDULED MAINTENANCE, FOUND THE AFT MAIN CABIN DOOR HINGE HALF VERTICAL ATTACH FLANGE CRACKED FROM THE EDGE OF THE PART 0.60" INWARD. NDT INSPECTION V
- [SDR DXTA2011031704512](https://openairdocs.org/sdr/DXTA2011031704512), Mar 16, 2011: UPLOCK SWITCH. OUT OF ADJUST. NORMAL TAKEOFF ROLL, UPON POSITIVE RATE, GEAR LEVER WAS SELECTED UP, IT APPEARED GEAR CYCLED UP HOWEVER RED "UNLOCK" LIGHT REMAINED ILLUMINATED. FOUND HYD FLUID
- [SDR DXTA2011020104438](https://openairdocs.org/sdr/DXTA2011020104438), Jan 27, 2011: CONTROL HANDLE. MALFUNCTIONED. AFTER T/O, PLACED GEAR LEVER UP, RED LIGHT CAME ON, SOUNDED LIKE DOORS OPENED, BUT 3 GREEN STAYED ON WITH THE RED. WIGGLED THE HANDLE IN THE UP POSITION AND THE
- [SDR DXTA2009110203838](https://openairdocs.org/sdr/DXTA2009110203838), Nov 1, 2009: STRUCTURE. DENTED. BIRD STRIKE ON THE RIGHT SIDE JUST ABOVE THE ROSEMOUNT, IT CONTINUE TO THE RIGHT WING AT THE STALL STRIP DENTING THE WING AND IT HIT THE RT ENGINE JUST BELOW TH
- [SDR DXTA200811143356](https://openairdocs.org/sdr/DXTA200811143356), Nov 14, 2008: CHECK VALVE. UNKNOWN. ABORT, THE LIGHT EXTINGUISHED ( POWER REDUCTION). COMPLIED WITH APPENDIX 29-2, "O" PROCEDURE. DEFERRED IAW MEL 29-2. CAT C. DUE 11-24-08. RAN AC AT T/O POWER IN
- [SDR DXTA20081114](https://openairdocs.org/sdr/DXTA20081114), Nov 14, 2008: SWITCH. MALFUNCTIONED. DURING TAKEOFF AT APPX 60KTS, THE RT HYD LOW FLOW ANNUNCIATOR ILLUMINATED. AFTER ABORT, THE LIGHT EXTINGUISHED( POWER REDUCTION). COMPLIED WITH APPENDIX 29-2, "
- [SDR DXTA2008111703356](https://openairdocs.org/sdr/DXTA2008111703356), Nov 14, 2008: WARNING SYSTEM. ACTIVATED. DURING TAKEOFF AT APPROX 60KTS, THE RIGHT HYD LOW FLOW ANNUNCIATOR ILLUMINATED.
- [SDR DXTA200811093346](https://openairdocs.org/sdr/DXTA200811093346), Nov 9, 2008: RESERVOIR. UNDERSERVICED. LOW HYD FLOW RT ANNUNCIATOR ILLUMINATED WHEN POWER APPLIED FOR T/O TROUBLESHOT HYD SYS. FOUND HYD RESERVOIR UNDERSERVICED. INSPECTED HYD PANEL ASSY. HOOKED UP H
- [SDR DXTA2008111003346](https://openairdocs.org/sdr/DXTA2008111003346), Nov 9, 2008: WARNING SYSTEM. ACTIVATED. LOW HYD FLOW RT ANNUNCIATOR ILLUMINATED WHEN POWER APPLIED FOR T/O. T/O ABORTED.
- [SDR DXTA200810093300](https://openairdocs.org/sdr/DXTA200810093300), Oct 9, 2008: ACTUATOR. FAULTY. WHEN LANDING GEAR WAS SELECTED DOWN. RT GREEN LIGHT ILLUMINATED. THE NO GREEN LIGHT APPEARED TO TAKE LONGER THAN NORMAL TO ILLUMINATE THE LT GREEN LIGHT DID NOT
- [SDR DXTA200803300](https://openairdocs.org/sdr/DXTA200803300), Oct 9, 2008: WARNING SYSTEM. ACTIVATED. WHEN LANDING GEAR WAS SELECTED DOWN, THE "RT" GREEN LIGHT ILLUMINATED. THE "LT" GREEN LIGHT DID NOT ILLUMINATE AND THE RED "UNLOCK" LIGHT REMAINED ILLUMINATED.
- [SDR 2008FA0000360](https://openairdocs.org/sdr/2008FA0000360), May 15, 2008: STIFFENER. MISINSTALLED. FOUND RT STIFFENER (PN 662121126) INADVERTENTLY INSTALLED IN LT POSITION. WITH LANDING GEAR IN THE STOWED POSITION, THE ACTUATOR CONTACTED THE STIFFENER AND CAU
- [SDR CWQR200804](https://openairdocs.org/sdr/CWQR200804), May 12, 2008: STIFFENER. CHAFED. AC WAS IN SCHEDULED MAINTENANCE, AN INSP NOTICED THAT THE LT MAIN GEAR ACTUATOR WAS CHAFING ON THE WING SPAR WHEEL WELL STIFFENER, PN 6621211-26. UPON FURTHER I
- [SDR CWQR200707](https://openairdocs.org/sdr/CWQR200707), Aug 21, 2007: BALANCE WEIGHT. MISINSTALLED. DURING A PHASE 1-4 INSPECTION, FOUND THE RUDDER BALANCE WEIGHT WAS TRIMMED DOWN AND ATTACHED WITH ONLY (2) BOLTS.THE IPC SHOWS (4) BOLTS TO ATTACH THIS WEIGHT. 

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