# N617QS: 2004 Cessna 560XL, registration cancelled 2024-12-31 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 31, 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: 560-5509 - Year built: 2004 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 9, 2004 - Certificate issued: December 19, 2024 - Last registry action: December 19, 2024 - Mode S code: A80A2E - 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/N617QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=617QS - Page: https://openairdocs.org/deregistered/N617QS-2024-12-31 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 DXTA2023092095960](https://openairdocs.org/sdr/DXTA2023092095960), Sep 19, 2023: ACTUATOR. DEFECTIVE. WHILE CLIMBING THROUGH FL 390 WE RECEIVED PIT TRIM ANNUCIATION ON BOTH PFDS. THE TRIM WHEEL WAS TRYING TO TRIM BUT WAS BINDING AND NOT MOVING AND HAD AN AUDIBLE - [SDR DXTA2023070690360](https://openairdocs.org/sdr/DXTA2023070690360), Jul 5, 2023: MOTOR. DAMAGED. POWER BRAKE CB: BRAKE CB TRIPPED, ANTI SKID AND LOW BRAKE PRESSURE ENNUNCIATED DURING TAXI IN. PNEUMATIC BRAKE APPLIED TO STOP AIRCRAFT AT RAMP PARKING. REMOVED - [SDR DXTA2022122676980](https://openairdocs.org/sdr/DXTA2022122676980), Dec 26, 2022: PIN. LACK OF LUBE. MAIN CABIN DOOR HANDLE REQUIRES EXCESSIVE FORCE TO OPEN AND CLOSE DOOR. CLEANED AND LUBED ALL MAIN CABIN DOOR PINS. ADJUSTED UPPER AFT LATCH PLATE INNER ECCENTR - [SDR DXTA2022012455550](https://openairdocs.org/sdr/DXTA2022012455550), Jan 21, 2022: SOCKET. DEFECTIVE. EMERG LIGHT SWITCH: AMBER LIGHT FOR THE EMERGENCY LIGHT SWITCH IS INOP // SIGNOFF// REMOVED AND RELNSTALLED NEW LAMP P/N 6838. REMOVED AND REPLACED SOCKET P/N M - [SDR DXTA2021071945410](https://openairdocs.org/sdr/DXTA2021071945410), Jul 17, 2021: LIGHT. SHORTED. CABIN EMERG LIGHT: CIRCUIT BREAKER HT 043 POPPED ON THE AFT CIRCUIT BREAKER PANEL IN THE APU COMPARTMENT. WE EXPERIENCED HEAVY ELECTRICAL SMELL AND SMOKE IN THE - [SDR DXTA2020071503863](https://openairdocs.org/sdr/DXTA2020071503863), Jul 14, 2020: STRUT. OUT OF ADJUST. CABIN ENTRY DOOR SPRING TORQUE COUNTERBALANCE HANDLE BAR EXCESSIVELY LOOSE. BARELY MAKES OVER CENTER LOCK. ADJUSTED CABIN DOOR SUPPORT STRUT ASSEMBLY REF AMM 52 - [SDR DXTA2019082102781](https://openairdocs.org/sdr/DXTA2019082102781), Aug 20, 2019: CONDENSER. ODOR. CABIN ODOR OIL SMELL - DISTINCT OIL SMELL IN CABIN AND COCKPIT. STRONGER IN LAV AREA AND CABIN, LESS STRONG ON COCKPIT. NOTICEABLE ON GROUND WITH APU AIR ON AND - [SDR DXTA2018060501036](https://openairdocs.org/sdr/DXTA2018060501036), Jun 4, 2018: UNKNOWN. ODOR. CLIMBING THRU 10K, PAX NOTIFIED CREW OF A SMOKE ODOR IN THE CABIN. CREW CONFIRMED AND FO WENT BACK TO CHECK WHILE CAPTAIN SHUT DOWN APU. ODOR IMMEDIATELY DISSIP - [SDR DXTA201711105HQ2T](https://openairdocs.org/sdr/DXTA201711105HQ2T), Nov 11, 2017: MOTOR. FAILED. COMPLETE BRAKE FAILURE DURING TAXI OUT. ANTI-SKID LIGHT AND POWER PRESSURE CIRCUIT BREAKER TRIPPED. THEN LOW BRAKE PRESSURE LIGHTS. HYD FLUID ON NOSE GEAR DURIN - [SDR DXTAT2PL6D005BQW8](https://openairdocs.org/sdr/DXTAT2PL6D005BQW8), Aug 22, 2017: WATER SEPARATOR. ODOR. ODORS IN THE COCKPIT DURING FLIGHT WITH APU RUNNING. SMELLS LIKE BURNED OIL. INSPECTED THE APU INLET AND EXHAUST, APU BLEED AIR DUCT AND HEAT EXCHANGER DUCT, WA - [SDR DXTA2016012406172](https://openairdocs.org/sdr/DXTA2016012406172), Jan 28, 2016: STEERING SYS. CORRODED. AFTER DEPARTURE THE LG UNLOCK LIGHT REMAINED ON. DURING CLIMB OUT THE HYD PRESS LIGHT REMAINED ILLUMINATED. COMPLETED THE LG WILL NOT RETRACT CHECKLIST. LG EXTE - [SDR DXTA2015110706119](https://openairdocs.org/sdr/DXTA2015110706119), Nov 7, 2015: SELECTOR. MALFUNCTIONED. DURING TAKEOFF, A LOUD SOUND OF RUSHING AIR & CABIN PRESSURIZING RAPIDLY. ACCOMPANIED BY A STRONG BURNING ODOR. ANNUNCIATOR WITH FLASHING MASTER CAUTION ILLUMIN - [SDR DXTA2015031105992](https://openairdocs.org/sdr/DXTA2015031105992), Mar 10, 2015: PRESSURE SWITCH. FAILED. DURING LANDING, LOWERING THE LANDING GEAR THE LOW BRAKE PRESSURE & ANTI-SKID INOPERATIVE ANNUNCIATOR LIGHTS CAME ON. RAN THE CHECKLIST & USED THE EMERGENCY BRAK - [SDR DXTA2015021705978](https://openairdocs.org/sdr/DXTA2015021705978), Feb 16, 2015: UNKNOWN. UNKNOWN. DURING LANDING ROLL OUT AT SPEEDS ABOVE NORMAL TAXI SPEED, THE LT BRAKE GRABS EXCESSIVELY & PULLS THE ACFT TO THE LEFT. THE RT BRAKE APPEARED TO RELEASE & REAPP - [SDR DXTA2013111205563](https://openairdocs.org/sdr/DXTA2013111205563), Nov 11, 2013: BRAKE ASSY. MALFUNCTIONED. LT BRAKE GRABS. R & R LT BRAKE ASSY IAW MM 32-42-01. BLED SYS AND PERFORMED OPS CHECKS. OPS CHECKS SATISFACTORY AT THIS TIME. TAXI, OPS, & LEAK CHECKED GOOD. - [SDR DXTA2013103105553](https://openairdocs.org/sdr/DXTA2013103105553), Oct 30, 2013: UNKNOWN. ODOR. DURING CRUISE FLIGHT, A LOUD CLICK OR POP WAS HEARD. CREW NOTICED A STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT THAT QUICKLY WENT AWAY. NO SMOKE WAS NOTED. NO - [SDR DXTA2013070105426](https://openairdocs.org/sdr/DXTA2013070105426), Jun 30, 2013: BEARING. FAILED. DURING DESCENT AT 35000 FT, ELEVATOR PITCH TRIM FROZE. PITCH TRIM LIGHT ILLUMINATED ON THE PFD. THE ELEVATOR PITCH TRIM WAS IMMOVABLE USING BOTH MANUAL AND ELEC - [SDR DXTA2013050605373](https://openairdocs.org/sdr/DXTA2013050605373), May 5, 2013: APU. FOD. AFTER STARTING APU, A BURNING ODOR CAME FROM APU. WENT OUTSIDE AND FOUND FLAMES COMING FROM EXHAUST ALONG WITH DEBRIS FROM A BIRDS NEST. SOME OF THE STICKS AND - [SDR 2013F00002](https://openairdocs.org/sdr/2013F00002), Dec 12, 2012: BOLT. WORN. ON PERFORMING AN INSPECTION-B, FOUND LT ENGINE FORWARD COWLING STRUT UPPER ATTACH BOLT SEVERELY WORN. SUSPECT VIBRATION CAUSING EXCESSIVE WEAR. THIS CONDITION H - [SDR DXTA2011091504727](https://openairdocs.org/sdr/DXTA2011091504727), Sep 15, 2011: MOTOR. FAILED. ACFT WAS TAXIING TO THE RUNWAY, WHEN THE POWER BRAKES AND ANTI SKID SYSTEMS FAILED. THE CREW STOPPED THE ACFT ON THE TAXIWAY. REMOVED FAULTY MOTOR PN MP50B-1, S - [SDR DXTA2010100604257](https://openairdocs.org/sdr/DXTA2010100604257), Oct 4, 2010: BRAKE ASSY. MALFUNCTIONED. BRAKES NOT FUNCTIONING PROPERLY. GRINDING AND GRABBING. TAXIED ACFT & VERIFIED PROBLEM, BUT WENT AWAY DURING TAXI. LET BRAKES COOL DOWN & RETAXIED & BRAKE FUNCT - [SDR DXTA2009111003857](https://openairdocs.org/sdr/DXTA2009111003857), Nov 10, 2009: NOSE CONE. DAMAGED. POSSIBLE BIRD STRIKE ON RT ENGINE AT 7 O`CLOCK POSITION. DENT FOUND ON ENGINE LIP AND BLOOD WITH FEATHERS AROUND INTAKE. PERFORMED A BIRD STRIKE INSP ON RT ENG - [SDR DXTA2009111103853](https://openairdocs.org/sdr/DXTA2009111103853), Nov 10, 2009: STRUCTURE. DENTED. POSSIBLE BIRD STRIKE ON RT ENGINE AT 7 OCLOCK POSITION. DENT FOUND ON ENGINE LIP AND BLOOD WITH FEATHERS AROUND INTAKE. - [SDR DXTA2009071703731](https://openairdocs.org/sdr/DXTA2009071703731), Jul 17, 2009: SEAL. LEAKING. DURING TAKEOFF APPROX 500FT, CREW GOT A RT 'LO OIL PRESS' INDICATION LIGHT. CREW FOLLOWED CHECKLIST AND LANDED THE ACFT SAFELY. OIL PRESSURE WAS AT APPROX 30 PS - [SDR DXTA200702508](https://openairdocs.org/sdr/DXTA200702508), Sep 28, 2007: ACTUATOR. INOPERATIVE. RT EEC INOP ON TAKEOFF ROLL AND COULD NOT REACH TAKEOFF POWER SETTING IN MANUAL POSITION. REMOVED & REPLACED R/H BLEED TORQUE MOTOR. RAN A/C FOR LEAK & OPS CHEC - [SDR DXTA200601474](https://openairdocs.org/sdr/DXTA200601474), Jul 1, 2006: ADC. FLUCTUATES. EXPERIENCED PITCH OSCILLATIONS IN CLIMB WITH KP/FD COUPLED TO AUTO PILOT. VIS FLUCTUATED FROM 500FPM TO +5000 FPM. GOT RED X ON VSI AND ALT AND A/S YELLOW FLAGS - [SDR DXTA200601437](https://openairdocs.org/sdr/DXTA200601437), Jun 14, 2006: WINDSHIELD. CRACKED. RIGHT FRONT WINDSHIELD HAS MULTIPLE CRACKS BROKE AT FLIGHT LEVEL 390 AND APPEARS TO BE THE OUTER LAYER ONLY. VERIFIED CO-PILOTS WINDSHIELD SHATTERED. REMOVED & - [SDR DXTA200601367](https://openairdocs.org/sdr/DXTA200601367), Apr 28, 2006: POSITION SWITCH. OUT OF ADJUST. AFTER TAKEOFF, GEAR RAISED WITH NORMAL INDICATIONS. AT 400FT WHEN FLAPS RAISED TO (0) DEGREE, GOT A STEADY HYD PRESS AND STAB MISCOMPARE LIGHT. AFTER RUNNING CH - [SDR DXTA200601359](https://openairdocs.org/sdr/DXTA200601359), Apr 23, 2006: POSITION SWITCH. CONTAMINATED. SHORTLY AFTER TAKEOFF POWER APPLIED NO TAKE OFF LIGHT ILLUMINATES AND AUARAL WARNING. AFTER CLEARING RUNWAY LIGHT GOES OUT. TROUBLESHOT SYSTEM. CLEANED LT AND R - [SDR DXTA200500740](https://openairdocs.org/sdr/DXTA200500740), May 22, 2005: WIRE HARNESS. FAULTY. DURING TAKEOFF ROLL LEFT ENGINE PRODUCED 80% N1. SCHEDULED TAKEOFF POWER WAS 90.1% - REMOVED AND REPLACED ENGINE WIRING HARNESS PER P&WC M/M CH 76-20-02 OPERATI - [SDR DXTA200500626](https://openairdocs.org/sdr/DXTA200500626), Mar 12, 2005: UPLOCK CABLE. OUT OF ADJUST. WHILE IN CRUISE AT FL410, CREW HEARD CLUNK SOUND FROM GEAR AREA, RED GEAR UNSAFE LIGHT ILLUMINATED AND HYD PRESS LIGHT ILLUMINATED STEADY. PULLED HYD CONTROL CB - [SDR DXTA200500603](https://openairdocs.org/sdr/DXTA200500603), Feb 20, 2005: LANDING GEAR. MALFUNCTIONED. AFTER ROTATION, GEAR SELECTED UP, AFTER 3-4 SEC GEAR MADE A CYCLING THUMPING NOISE FOR APPROX 3 SECONDS. RECEIVED A HYD FLOW & A HYD LOW CAUTION LIGHT. CYCLING - [SDR DXTA200400500](https://openairdocs.org/sdr/DXTA200400500), Dec 27, 2004: SWITCH. MALFUNCTIONED. AFTER GEAR UP/FLAPS UP HAD HYD PRESS, STAB MISCOMPARE ANNUNCIATORS AND UNLOCK GEAR LIGHT. PULL HYD C/B, AND LOUD THUMP HEARD AND FELT IN NOSE GEAR AREA. 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