# N609QS: 2004 Cessna 560XL, registration cancelled 2024-12-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 6, 2024 - 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: 560-5522 - Year built: 2004 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 28, 2004 - Certificate issued: December 21, 2020 - Last registry action: April 7, 2023 - Mode S code: A7EA1D - 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/N609QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=609QS - Page: https://openairdocs.org/deregistered/N609QS-2024-12-06 From the FAA registry file of November 4, 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 DXTA2024051011731](https://openairdocs.org/sdr/DXTA2024051011731), May 10, 2024: HANDLE. BINDING. INTERIOR DOOR HANDLE WILL NOT EXTEND OR RETRACT BAYONET PINS. EXTERIOR DOOR HANDLE EXTENDS AND RETRACTS PINS NORMALLY. (PRE-FLIGHT) REMOVED DOOR STEPS TO GAIN A - [SDR DXTA2024040511404](https://openairdocs.org/sdr/DXTA2024040511404), Apr 4, 2024: ENGINE. DAMAGED. JUST AFTER TAKEOFF AROUND 200 FEET AGL WE NOTICED A BURNING SMELL AND FOUND THAT THE ITT ON THE RIGHT ENGINE WAS UP NEAR 800 DEGREES. WHEN WE REDUCED POWER TO L - [SDR DXTA2024040211376](https://openairdocs.org/sdr/DXTA2024040211376), Apr 1, 2024: SOLENOID. MALFUNCTIONED. AIRCRAFT WILL NOT CROSSFEED AT ALTITUDE. AT FL320 WHEN SELECTING CROSSFEED LEFT TO RIGHT, LEFT BOOST PUMP ANNUNCIATOR ILLUMINATED FOLLOWED BY RIGHT BOOST PUMP A - [SDR DXTA2023121910373](https://openairdocs.org/sdr/DXTA2023121910373), Dec 18, 2023: UNKNOWN. UNKNOWN. AISLE EMERGENCY LIGHTS, A SECTION OF THE FLOOR AISLE EMERGENCY LIGHTS ARE INOPERATIVE, LEFT SIDE, AFT HALF. (AFT OF SEAT 3) //SIGNOFF//ADJUSTED CARPET FOR BETTE - [SDR DXTA2023110199470](https://openairdocs.org/sdr/DXTA2023110199470), Oct 31, 2023: UNKNOWN. UNKNOWN. WITH THE EMER LIGHT SWITCH IN ARM AND THE BATT SWITCH ON AND THE PASS SAFETY SWITCH OFF, THE FORWARD EMERGENCY LIGHTS REMAIN ON (FORWARD EXIT SIGNS, FORWARD DRO - [SDR DXTA2023103099180](https://openairdocs.org/sdr/DXTA2023103099180), Oct 28, 2023: CHARGER. INOPERATIVE. REPEAT WRITE-UP. POST FLIGHT, FOUND CIRCUIT BREAKER NUMBER HT043, CORRESPONDING TO EMER LIGHTS-FWD, TRIPPED. REMOVED PILOT SIDE EMERG UGHT P/N 9913-1 S/N 1994.I - [SDR DXTA2023100697300](https://openairdocs.org/sdr/DXTA2023100697300), Oct 5, 2023: PCB. FAILED. DURING CROSSFEED AT FL300 FROM LEFT TANK TO RIGHT GOT XFEED FEED ANNUNCIATOR ALONG WITH STEADY LEFT BOOST PUMP AND FLASHING RIGHT BOOST PUMP AND CAUTION LIGHT. - [SDR DXTA2023092696440](https://openairdocs.org/sdr/DXTA2023092696440), Sep 26, 2023: UNKNOWN. UNKNOWN. MAIN CABIN DOOR WOULD NOT OPEN FROM THE INSIDE. HAD A GROUND CREW OPEN IT WITH THE EXTERIOR HANDLE. MAIN CABIN DOOR FOUND TO BE DIFFICULT TO OPEN AND CLOSE FROM - [SDR DXTA2023032082750](https://openairdocs.org/sdr/DXTA2023032082750), Mar 17, 2023: LIGHT. DEFECTIVE. FLOOR EMERG EXIT LIGHT: FLOOR EMERGENCY LIGHTING FROM BETWEEN SEATS 3 & 5 TO THE MAIN CABIN DOOR DO NOT ILLUMINATE (APPROXIMATEY 4'). LIGHTS DO NOT ILLUMINATE W - [SDR DXTA2023022781420](https://openairdocs.org/sdr/DXTA2023022781420), Feb 27, 2023: MONITOR. INOPERATIVE. DURING CRUISE, OWNER PLUGGED IN AIRSHOW MONITOR AT SEAT 8. WHILE PUSHING POWER BUTTON ON MONITOR, SMOKE CAME OUT OF THE PLUG AREA. THE SMOKE STOPPED WHEN THE MO - [SDR DXTA2023010377610](https://openairdocs.org/sdr/DXTA2023010377610), Dec 31, 2022: SIGN. INOPERATIVE. MAIN CABIN DOOR EMERGENCY EXIT LIGHT INOP. APPLIED POWER TO AIRCRAFT TO CHARGE EMERGENCY BATTERY PACK FOR 30MIN. EXIT LIGHT STILL FAILS TO ILLUMINATE. REPLACED - [SDR EBVR20220927](https://openairdocs.org/sdr/EBVR20220927), Sep 27, 2022: NONE. NONE. A) REPAIRED THREE CHAFED AREAS ON CABIN INTERIOR STRUCTURE, TWO ON THE RIGHT SIDE AT FS 280.45, FS 337.66 AND ON THE LEFT SIDE FS 280.15 IAW AQRD ERO-106971 REV - [SDR DXTA2022071165660](https://openairdocs.org/sdr/DXTA2022071165660), Jul 10, 2022: DIODE. FAILED. CABIN EMERG LIGHT: FORWARD CABIN EMERGENCY LIGHTING BATTERY IS INOPERATIVE. (LIGHTS TESTED WITH PASSENGER ADVISORY SYSTEM OK). *** CORRECTIVE ACTION *** TROUBLE - [SDR DXTA2022032959240](https://openairdocs.org/sdr/DXTA2022032959240), Mar 29, 2022: NONE. DEFECTIVE. FUEL PRESSURE INDICATION: REPEAT WRITEUP. DURING CROSSFEED FROM LEFT TANK TO RIGHT ENGINE, CROSSFEED WORKED NORMALLY. AFTER MOVING CROSSFEED TO OFF POSITION, TH - [SDR DXTA2022032558980](https://openairdocs.org/sdr/DXTA2022032558980), Mar 24, 2022: SHADE. DEFECTIVE. CABIN WINDOW SHADE: CABIN WINDOW SHADE ON THE EMERGENCY EXIT DOOR AND OVER THE LAV IS INOP//CORRECTIVE ACTION//REMOVED WINDOW SHADE ASSY PN.6619325-27 SN.N/A AN - [SDR DXTA2021121353410](https://openairdocs.org/sdr/DXTA2021121353410), Dec 11, 2021: NONE. NONE. CABIN EMERG LIGHT: ONE SECTION OF THE DROP ISLE EMERGENCY LIGHTING STRIP APPEARS INOP OR NOT IN CORRECT POSITION UNDER THE MAIN CABIN ENTRY DOOR // SIGNOFF// VE - [SDR DXTA2021070944950](https://openairdocs.org/sdr/DXTA2021070944950), Jul 8, 2021: PUMP. DEFECTIVE. MLG BRAKE PRESSURE: TAXIING OUT TO RUNWAY, "ANTISKID" ANNUNCIATOR CAME ON AND SIMULTANEOUSLY THE "PWR BRKS" CIRCUIT BREAKER POPPED. TURNED AIRCRAFT AROUND AND H - [SDR DXTA2021020304672](https://openairdocs.org/sdr/DXTA2021020304672), Feb 2, 2021: BATTERY PACK. INOPERATIVE. REPEAT WRITE: THE WHITE EMER EXIT LIGHT OVER THE MAIN ENTRANCE DOOR AND THE TWO RED EXIT LIGHTS FWD AND AFT OF THE MAIN ENTRANCE DOOR ARE ALL INOP. ALSO, THE FW - [SDR DXTA2020081183950](https://openairdocs.org/sdr/DXTA2020081183950), Aug 8, 2020: CIRCUIT CARD. DEFECTIVE. MAIN CABIN DOOR ANNUNCIATIOR DID NOT EXTINGUISH AFTER CLOSING DOOR. OTHER INDICATION OF DOOR CLOSING WERE NORMAL. REMOVED SUSPECTED FAULTY CABIN DOOR MONITOR PC - [SDR JGVR20190207001](https://openairdocs.org/sdr/JGVR20190207001), Feb 7, 2019: SKIN. CORRODED. FOUND CORROSION AROUND THE RH FORWARD NOSE DOOR (AVIONICS ACCESS DOOR) ON THE FUSELAGE SKIN, REPAIRED BY BLENDING, NDT AND INSTALLING REPAIR DOUBLERS. - [SDR DXTA2016071006264](https://openairdocs.org/sdr/DXTA2016071006264), Jul 10, 2016: HINGE. CRACKED. DURING DESCENT FROM 35, 000 FT, RECEIVED A NOTICEABLE SHUDDER IN THE AIRFRAME. SUBSIDED ONCE BELOW 250KTS. GEAR AND FLAPS WERE UP AND SPEEDBRAKE WAS RETRACTED. - [SDR CWQR20160616017](https://openairdocs.org/sdr/CWQR20160616017), Jun 16, 2016: ATTACH BRACKET. CRACKED. DURING SCHEDULED MAINTENANCE, WE FOUND THIS RT AVIONICS ATTACH BRACKET CRACKED .7500", HALF OF THE BRACKETS LENGTH. REPLACED ATTACH BRACKET WITH NEW. - [SDR DXTA2016052006242](https://openairdocs.org/sdr/DXTA2016052006242), May 25, 2016: APU. SMOKE. WHILE STARTING APU, CABIN IMMEDIATELY FILLED UP WITH THICK, ACRID SMOKE. REMOVED APU IAW MM 49-10-00. DRAINED REMOVED APU OF OIL. CLEANED APU CONTAINMENT BOX & - [SDR DXTR2015020501](https://openairdocs.org/sdr/DXTR2015020501), Jan 27, 2015: HINGE FITTING. CORRODED. MCD FORWARD, LOWER HINGE HALF ASSY CORRODED. R & R MCD LOWER HINGE IAW SRM 51-40-03 AND DWG 6611071, DWG 0003.2. CORROSION DAMAGED WAS CONTAINED TO LOWER HINGE - [SDR DXTA2014072805834](https://openairdocs.org/sdr/DXTA2014072805834), Jul 27, 2014: APU. ODOR. SMOKE WAS COMING INTO COCKPIT, WITH APU RUNNING, BLEED AIR ON OR OFF AND WITH ENGINE RUNNING. REMOVED AND REPLACED APU IAW MM 49-10-00. OPS AND LEAK CHECKED GOO - [SDR DXTA2013122702609](https://openairdocs.org/sdr/DXTA2013122702609), Dec 27, 2013: FLAP SYSTEM. MALFUNCTIONED. AFTER TAKEOFF, WHEN FLAPS WERE SELECTED TO 0, FLAPS STUCK AT 7 DEGREES. ON GROUND FLAP HANDLE SELECTED TO 35 DEGREES & STUCK AT 35 DEGREES. REPLACED THE LT FLAP - [SDR DXTA2011110504777](https://openairdocs.org/sdr/DXTA2011110504777), Nov 5, 2011: RUDDER PEDAL. MALFUNCTIONED. WHEN MAKING A TIGHT TURN USING RUDDER AND BRAKES, THE BRAKE PEDALS GO TO THE FLOOR WITHOUT BRAKING. THIS OCCURS BOTH IN RT AND LT TURNS AND IS FELT FROM BOTH PI - [SDR DXTA2011103104772](https://openairdocs.org/sdr/DXTA2011103104772), Oct 30, 2011: WIRE HARNESS. DAMAGED. AFTER TAKEOFF, GEAR HANDLE WOULD NOT MOVE FROM THE EXTENDED POSITION. R & R LT MLG WIRING HARNESS IAW WM 20-10-01. ADJUSTED SQUAT SWITCH IAW MM 32-44-00. OPS CH - [SDR DXTA2011103104774](https://openairdocs.org/sdr/DXTA2011103104774), Oct 28, 2011: SQUAT SWITCH. INOPERATIVE. GEAR WOULD NOT RETRACT AFTER TAKEOFF, GEAR HANDLE WOULD NOT MOVE INTO THE UP POSITION. REPLACED THE LT MLG SQUAT SWITCH WITH A NEW SWITCH IAW MM 32-61-00, OPS C - [SDR DXTA2011102104758](https://openairdocs.org/sdr/DXTA2011102104758), Oct 20, 2011: CONTROL HANDLE. MALFUNCTIONED. AFTER TAKEOFF AND CALLING A POSITIVE RATE AND GEAR UP, THE GEAR HANDLE COULD NOT BE MOVED. REPLACED LANDING GEAR CONTROL HANDLE ASSY IAW AMM CHP 32-30-00. PERFO - [SDR DXTA2009122103906](https://openairdocs.org/sdr/DXTA2009122103906), Dec 18, 2009: CIRCUIT BOARD. INTERMITTENT. UNSAFE NOSE GEAR INDICATION. 2 GREEN 1 RED INDICATION, NO AOA INDEXER. DURING THE VECTORS TO RUN THE CHECKLIST, THE GREEN NOSE INDICATION CAME ON WITH AOA INDEX - [SDR CWQR2006005](https://openairdocs.org/sdr/CWQR2006005), Mar 8, 2006: DRAIN VALVE. LOOSE. FOUND THE STATIC SYSTEM DRAIN VALVE POPPET RETAINING RING COMING LOOSE FROM VALVE BASE. - [SDR DXTA200500899](https://openairdocs.org/sdr/DXTA200500899), Aug 10, 2005: WARNING LIGHT. ILLUMINATED. ON LANDING THE ANTISKID LIGHT ILLUMINATED AND ON TAXI IN THE LOW BRAKE PRESSURE LIGHT ILLUMINATED AND THE PNEUMATIC BRAKES HAD TO BE USED TO STOP THE PLANE. C/W - [SDR CWQR2005005](https://openairdocs.org/sdr/CWQR2005005), Jun 22, 2005: DRAIN. POPPED. FORWARD RT FUSELAGE STATIC DRAIN VALVE NOT FLUSH. NEW UNIT ORDERED AND INSTALLED, LEAK CHECKED. DURING REMOVAL OF SUSPECTED BAD PART, ENTIRE CORE POPPED OUT, CO --- 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.