# N657QS: 2006 Cessna 560XL, registration cancelled 2024-12-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 26, 2024 - 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: 560-5636 - Year built: 2006 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: May 31, 2006 - Certificate issued: July 23, 2020 - Last registry action: March 4, 2023 - Mode S code: A8A82A - 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/N657QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=657QS - Page: https://openairdocs.org/deregistered/N657QS-2024-12-26 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 (34) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR EBVR202306130001](https://openairdocs.org/sdr/EBVR202306130001), Jun 13, 2023: TORQUE TUBE. CORRODED. AFTER EVALUATION FOUND R/H ELEVATOR TORQUE TUBE TO BE CORRODED BEYOND LIMITS. REMOVED CORRODED RH ELEVATOR TORQUE TUBE AND REPLACED WITH NEW 6634002-20 TORQUE T - [SDR DXTA2023040783850](https://openairdocs.org/sdr/DXTA2023040783850), Apr 7, 2023: PCB. DEFECTIVE. ON TAKEOFF, RETRACTED THE MLG. MLG DID NOT RETRACT. 1-3 MINUTES LATER STAB MISCOMPARE ILLUM. ACFT STILL AT 160 KNOTS. ON APPROACH FLAPS WOULD NOT EXTEND. AFTER - [SDR DXTA2022110873510](https://openairdocs.org/sdr/DXTA2022110873510), Nov 7, 2022: BRAKE. MALFUNCTIONED. DURING REPOSITION TAXI BRAKES FELT LIKE THEY WERE GRABBING. IT WAS HARD TO TELL WHICH SIDE. LANDING APPROX 20MIN PRIOR WAS NORMAL WITH NO CONTROL ISSUES. WHEN W - [SDR DXTA2023092896690](https://openairdocs.org/sdr/DXTA2023092896690), Sep 27, 2022: HOOK. BROKEN. DOOR HANDLE WILL NOT MOVE PAST CENTER POSITION TOWARDS LOCK & SECURE DOOR, EITHER FROM INSIDE OR OUTSIDE. HAD TO USE MANUAL PRE-CATCH OVERRIDE BUTTON TO OPEN DO - [SDR DXTA2022092070760](https://openairdocs.org/sdr/DXTA2022092070760), Sep 19, 2022: NONE. NONE. MAIN DOOR: UNABLE TO LOCK THE MAIN CABIN DOOR FROM THE INSIDE. WE WERE ABLE TO LOCK THE DOOR ONCE BUT HAD A VENT DOOR AND LOCKING HANDLE LIGHT INLLIMINATED ON T - [SDR DXTA2022091570400](https://openairdocs.org/sdr/DXTA2022091570400), Sep 14, 2022: NONE. NONE. MAIN DOOR HANDLE: WHEN CLOSING DOOR FROM INSIDE THE OUTSIDE HANDLE DOES NOT STOW - [SDR DXTA2022091370290](https://openairdocs.org/sdr/DXTA2022091370290), Sep 12, 2022: NONE. NONE. MAIN DOOR HANDLE: ADVISED UPON LANDING FROM GROUND PERSONNEL THAT MAIN CABIN DOOR HANDLE WAS "OUT AND AT AN ANGLE" WE CONFIRMED WITH CREWMEMBER OUTSIDE THAT HAN - [SDR DXTA2022090769510](https://openairdocs.org/sdr/DXTA2022090769510), Sep 7, 2022: NONE. NONE. MAIN CABIN ENTRY DOOR HANDLE, HARD / STIFF TO MOVE TO THE LOCK AND OPEN POSITION.//CORRECTIVE ACTION// LUBRICATED MAIN DOOR INTERNAL COMPONETS AND MADE MINOR AD - [SDR DXTA2022090669620](https://openairdocs.org/sdr/DXTA2022090669620), Sep 3, 2022: NONE. NONE. MAIN CABIN DOOR INSIDE HANDLE EXTREMELY DIFFICULT TO OPERATE, OPENING AND CLOSING. FROM THE INSIDE WITH DOOR CLOSED.//CORRECTIVE ACTION// INSPECTED AND OPS CHEC - [SDR DXTA2022090669520](https://openairdocs.org/sdr/DXTA2022090669520), Sep 2, 2022: NONE. NONE. MAIN CABIN ENTRY DOOR WHEN OPENING FALLS OPEN WITH LITTLE TO NO RESISTANCE.//CORRECTIVE ACTION// ADJUSTED COUNTER BALANCE OF THE MAIN DOOR IAW 560XLS MM 52-10-0 - [SDR DXTA2022082668910](https://openairdocs.org/sdr/DXTA2022082668910), Aug 25, 2022: NONE. NONE. MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE WITH BOTH APU ON AND OFF. DURING THE LAST THIRD OF HANDLE MOVEMENT BOTH OPENING AND CLOSING DOOR YOU CAN FEEL AND HE - [SDR DXTA2022053162950](https://openairdocs.org/sdr/DXTA2022053162950), May 31, 2022: CABLE. DEFECTIVE. PRIMARY TRIM: BOTH MANUAL AND ELECTRIC ELEVATOR TRIM INOP. TRIM WHEEL MOVES EASILY BUT DOES NOT AFFECT THE TRIM TAB ON THE HORIZONTAL STABILIZER. LARGE NOSE DOW - [SDR DXTA2022052062280](https://openairdocs.org/sdr/DXTA2022052062280), May 20, 2022: FLAG. MISSING. MAIN DOOR: DURING PREFLIGHT, FLAG ON MAIN CABIN DOOR STEP MISSING/OUT OF VIEW. REMOVED CABIN STEPS AND CENTERED ALL GREEN "LOCKED" FLAGS IN OBSERVATION WINDOWS - [SDR DXTA2022051661860](https://openairdocs.org/sdr/DXTA2022051661860), May 15, 2022: SEAL. TORN. MAIN DOOR PRIMARY SEAL: DURING CLIMB THRU 32000 DOOR SEAL LIGHT ILLUMINATED 5 MINUTES LATER HEARD LOAD RUSH OF AIR FOR 1 MINUTE WITH CABIN CLIMB THEN CABIN STAB - [SDR DXTA2022033159360](https://openairdocs.org/sdr/DXTA2022033159360), Mar 31, 2022: SEAL. UNKNOWN. MAIN DOOR PRIMARY SEAL: WHEN EXITING AIRCRAFT AND MOVING MAIN DOOR LEVER TO THE OPEN POSITION DOOR TAKES AROUND 20 SECONDS TO BE ABLE TO OPEN BECAUSE THE DOOR S - [SDR 2022F00137](https://openairdocs.org/sdr/2022F00137), Mar 19, 2022: ATTACH FITTING. GOUGED. RMLG ACTUATOR GOUGED ACTUATOR FITTING. MINOR REPAIR ACCOMPLISHED IAW TEXTRON AVIATION ENGINEERING MEMO DQ34007 DATED MARCH 18, 2022; 560-5636, N657QS, REPAIR RE - [SDR 2022F00136](https://openairdocs.org/sdr/2022F00136), Mar 19, 2022: FLAP. DELAMINATED. L/H IB FLAP HAS MULTIPLE AREAS OF DELAMINATION ON BOTTOM SIDE OF FLAPS. PN: 6525130-37 SN: 733. R/H IB FLAP HAS MULTIPLE AREAS OF DELAMINATION ON BOTTOM SIDE OF - [SDR 2022FA0000148](https://openairdocs.org/sdr/2022FA0000148), Mar 9, 2022: WARNING HORN. FALSE INDICATION. LANDING GEAR WARNING HORN: REPEAT. ON PRE FLIGHT WARNING HON WORKED WITH SEVERAL CHECKS USING ROTORY TEST. IN FLIGHT WARNING HORN INOP AT ALL ALTITUDES ON POST - [SDR 2022F00057](https://openairdocs.org/sdr/2022F00057), Feb 27, 2022: RUDDER. CRACKED. RUDDER SKIN IS CRACKED NEAR THE LOWER END OF THE HINGE HALF. TEXTRON AVIATION ENGINEERING DEEMED THE DAMAGE AS MINOR IN SCOPE. ACCOMPLISHED TEXTRON AVIATION ENG - [SDR DXTA2022010554770](https://openairdocs.org/sdr/DXTA2022010554770), Jan 4, 2022: NONE. NONE. MAIN DOOR: HANDLE BOTH INSIDE AND OUTSIDE VERY DIFFICULT TO TURN. TOOK ABOUT 3 MIN TO GET IT OPEN. THIS WOULD BE A IMPEDANCE TO EGRESS. SIX PACK AND GREEN INDIC - [SDR DXTA2021090748250](https://openairdocs.org/sdr/DXTA2021090748250), Sep 3, 2021: PIN. LACK OF LUBE. MAIN DOOR: MAIN CABIN DOOR IS BECOMING MORE DIFFICULT TO LATCH AND UNLATCH WITH EACH LEG. ONE OF THE TWO TOP PINS EXTENDS FURTHER THAN THE OTHER AND THERE IS EV - [SDR DXTA2019031102140](https://openairdocs.org/sdr/DXTA2019031102140), Mar 9, 2019: SQUAT SWITCH. OUT OF RIG. ALL LANDING GEAR RETRACTION DID NOT RETRACT - AFTER TAKEOFF LANDING GEAR WOULD NOT RETRACT. **SUPPLEMENTAL INFORMATION - JACKED AIRCRAFT AND TRIED TO ACTUATE TH - [SDR DXTA2019030802128](https://openairdocs.org/sdr/DXTA2019030802128), Mar 7, 2019: SWITCH. DIRTY. ALL LANDING GEAR RETRACTION DID NOT RETRACT - LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. GEAR HANDLE WOULD NOT MOVE AND WAS STUCK IN THE DOWN POSITION. WE HA - [SDR DXTA2018112601719](https://openairdocs.org/sdr/DXTA2018112601719), Nov 25, 2018: UNKNOWN. ODOR. AT GEAR RETRACTION THE LO HYD LVL LIGHT ILLUMINATED. GEAR AND FLAPS RETRACTED NORMALLY WITH LIGHT ILLUMINATED. LIGHT WENT OUT WHEN GEAR WAS EXTENDED. GEAR AND F - [SDR IGXR20160921004](https://openairdocs.org/sdr/IGXR20160921004), Sep 7, 2016: TRIM TAB. CRACKED. THE LOWER AFT CORNER OF THE RUDDER TRIM HAS A CRACK MEASURING 0.76 INCHES LONG. PERFORMED PERMANENT REPAIR USING APPROVED ENGINEERING ORDER ERO-859505. - [SDR DXTA2013031505317](https://openairdocs.org/sdr/DXTA2013031505317), Mar 14, 2013: MOTOR. FAILED. AFTER ENGINE START LOW BRAKE PRESSURE ANNUNICATOR CAME ON. I RESET THE "PWR BRKS" CB IAW THE CHECKLIST. WE ATTEMPTED TO TAXI, BRAKE PEDALS WENT TO THE FLOOR. RE - [SDR DXTA2013012305257](https://openairdocs.org/sdr/DXTA2013012305257), Jan 22, 2013: BOLT. SHEARED. NOSE WHEEL WOBBLING AFTER ONLY 100 YARDS OF TAXIING FROM THE BLOCKS. 3 BOLTS HOLDING THE SHIMMY DAMPENER TO THE STEERING ARE SHEARED OFF. INSPECTED NOSE GEAR AN - [SDR DXTR20120322001](https://openairdocs.org/sdr/DXTR20120322001), Mar 22, 2012: WEB. CRACKED. WEB HAS 3 CRACKS AT DOOR HANDLE ATTACH POINT. REMOVED DAMAGE AS REQUIRED AND INSTALLED NEW STIFFENER IAW SRM 51-40-03 AND 51-40-06 AND SB-52-14. - [SDR DXTA2011091204719](https://openairdocs.org/sdr/DXTA2011091204719), Sep 11, 2011: ACTUATOR. BINDING. ELEVATOR TRIM STUCK, BINDING AND DIFFICULT TO MOVE USING ELECTIRIC SWITCH AND MANUAL TRIM WHEEL. AT TIMES IT WAS IMPOSSIBLE TO MOVE. TROUBLESHOT & FOUND LT ELEV - [SDR DXTA2011080504686](https://openairdocs.org/sdr/DXTA2011080504686), Aug 4, 2011: AHRS. INOPERATIVE. DURING DECENT FL260 AT 300KIAS, NOTICED A BACK & FORTH FLUXUATION ON TRIANGLULAR RUDDER TRIM INDICATOR, FOLLOWED BY AUTOPILOT KICKING OFF WITH AUDIBLE ALARM. RE - [SDR DXTA200905213662](https://openairdocs.org/sdr/DXTA200905213662), May 21, 2009: DISPLAY. INOPERATIVE. CLIMBING THROUGH 15,000 FT, THE CO-PILOTS SIDE PFD DISPLAYED AN ATTITUDE AND HEADING FAIL. SWAPPED AHRS REFERENCE UNITS FOR TROUBLESHOOTING. NO FAIL. SWAPPED BA - [SDR DXTA20082914](https://openairdocs.org/sdr/DXTA20082914), Mar 5, 2008: UPLOCK SWITCH. DAMAGED. AFTER TAKEOFF WHEN GEAR HANDLE PLACED IN UP NOSE WHEEL UNLOCK. RED LIGHT STARTED FLASHING AND THUMPING NOISE CAME FROM NOSE AREA. DURING ARRIVAL INSPECTION. RH - [SDR DXTA200701908](https://openairdocs.org/sdr/DXTA200701908), Feb 2, 2007: ANTI-SKID SYS. MALFUNCTIONED. AT FL 320 ANTI-SKID ILLUMINATED STEADY THEN FLASHED RESET TO STEADY. WHEN GEAR WAS LOWERED, LOW BRAKE PRESS ILLUMINATED, FLASHING. CONDUCTED APPRORIATE CHECKLIS - [SDR DXTA200601674](https://openairdocs.org/sdr/DXTA200601674), Oct 20, 2006: CIRCUIT BREAKER. OPEN. BRAKES FAILED, SED AIR BRAKES TO STOP. (M2B). REPLACED SKID CONTROL C/B PER 560XL MM CH 24-50-02. BLED AND PERFORMED OPERATIONAL CHECK AND TAXI CHECK OF BRAKE S --- 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.