# N618QS: 2004 Cessna 560XL, registration cancelled 2024-12-04 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: December 4, 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: 560-5506 - Year built: 2004 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: August 24, 2004 - Certificate issued: November 19, 2019 - Last registry action: September 15, 2023 - Mode S code: A80DE5 - 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/N618QS - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=618QS - Page: https://openairdocs.org/deregistered/N618QS-2024-12-04 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 (22) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR DXTA2022092771120](https://openairdocs.org/sdr/DXTA2022092771120), Sep 26, 2022: NONE. DEFECTIVE. FLOOR EMERG EXIT LIGHT: LEFT FORWARD EMERGENCY PATH WAY LIGHTING IS INOP // SIGNOFF// REMOVED AND REPLACED THE LEFT FORWARD POSITION 1 AND LEFT FORWARD POSITION - [SDR DXTA2022092671120](https://openairdocs.org/sdr/DXTA2022092671120), Sep 26, 2022: LIGHT. INOPERATIVE. FLOOR EMERG EXIT LIGHT: LEFT FOWARD EMERGENCY PATH WAY LIGHTING IS INOP - [SDR DXTA2022092671040](https://openairdocs.org/sdr/DXTA2022092671040), Sep 23, 2022: BATTERY PACK. INOPERATIVE. CABIN EMERG LIGHT: FORWARD DROPPED AISLE LIGHTS DO NOT WORK // SIGNOFF// ARRIVED AT AIRCRAFT AND PERFORMED OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM AND FU - [SDR DXTA2022070765450](https://openairdocs.org/sdr/DXTA2022070765450), Jul 6, 2022: SUPPORT STRUT. DAMAGED. MAIN CABIN DOOR INERTIAL REEL?S ARE GRINDING AND CAUSING THE DOOR TO GET STOP ABOUT HALF WAY DOWN. // SIGNOFF// ARRIVED AT AIRCRAFT AND FOUND AFT CABIN DOOR SUP - [SDR DXTA2021120853170](https://openairdocs.org/sdr/DXTA2021120853170), Dec 7, 2021: NONE. NONE. MAIN DOOR VISUAL INDICATOR: TOP LEFT CABIN DOOR PIN INDICATOR FLAG IS NOT CENTERED ABOUT 1/4 OF THE WAY OUT OF THIS SITE WINDOW //SIGNOFF// REMOVED MED STEPS AN - [SDR DXTA030220213893](https://openairdocs.org/sdr/DXTA030220213893), Mar 2, 2021: BOLT. BACKED OUT. ENTRANCE STAIR HARDWARE: FORWARD TELESCOPING MAIN DOOR BRACE HAS ATTACHMENT HARDWARE THAT IS BACKING OUT. INSPECTED PIN AND CONFIRMED WRITE-UP. RE-SECURED PIN A - [SDR 2020F00340](https://openairdocs.org/sdr/2020F00340), Jul 15, 2020: STIFFENER. DEBONDED. DISBOND, ENGINE BEAM, STIFFENERS, AFT. FIELD REPAIR FR-560-5506-7762 DATED 03/05/2020, DISBOND, ENGINE BEAM, STIFFENERS, AFT WITH FAA FORM 8100-9 DATED 03/06/20 - [SDR 2020F00339](https://openairdocs.org/sdr/2020F00339), Jul 15, 2020: FRAME. CHAFED. REPAIR OF TAILCONE FRAME(S)CHAFE DAMAGE. ENGINEERING REPAIR LETTER DQ26014M1 DATED 06/11/2020, TAILCONE FRAME(S)CHAFE DAMAGE. - [SDR DXTA2019111983091](https://openairdocs.org/sdr/DXTA2019111983091), Nov 18, 2019: CONDENSER. DIRTY. COCKPIT ODOR - ON DESCENT INTO PBI WITH POWRAN APU AND HAD NO ODOR. RAN RIGHT ENGINE ONLY AND NO ODOR. RAN LEFT ENGINE ONLY AND NO ODOR. REPOSISTION AIRCRAFT AN - [SDR DXTA2019100702925](https://openairdocs.org/sdr/DXTA2019100702925), Oct 7, 2019: ENGINE. CONTAMINATED. COCKPIT ODOR - REPEAT WRITEUP. DURING TAKEOFF WITH THE APU OFF WE GOT A BAD ODOR OF SOME SORT OF CHEMICAL SMELL. POSSIBLY OIL? DEFINITELY NOT EXHAUST OR BAD SOC - [SDR DXTA2019100402917](https://openairdocs.org/sdr/DXTA2019100402917), Oct 4, 2019: ENGINE. CONTAMINATED. COCKPIT ODOR - AT FL410 STARTED TO GET A JET EXHAUST ODOR IN THE COCKPIT. BOTH CREWMEMBERS STARTING EXPERIENCE NAUSEOUS SYMPTOMS. CONTINUED BUT STARTED AN EARLY - [SDR JGVR2018102901](https://openairdocs.org/sdr/JGVR2018102901), Oct 29, 2018: SERVICE DOOR. CRACKED. LEVEL 1 CORROSION ON TOILET SERVICE DOOR AROUND LATCHES AND FOUND A CRACK IN DOOR BELOW FWD LATCH. - [SDR JGVR20181027001](https://openairdocs.org/sdr/JGVR20181027001), Oct 27, 2018: LINK. CORRODED. DURING THE REMOVAL OF THE LT MLG TRAILING LINK HINGE PIN FOUND THE ATTACHING CLEVIS POINTS TO BE CORRODED. REMOVED CORRODED LT MLG TRAILING LINK AND INSTALLED A - [SDR JGVR20181026001](https://openairdocs.org/sdr/JGVR20181026001), Oct 26, 2018: ACCESS PANEL. CRACKED. REMOVED CRACKED VERTICAL STABILIZER ACCESS PANEL 340ER AND INSTALLED NEW P/N 5531005-3. - [SDR DXTA2016121406338](https://openairdocs.org/sdr/DXTA2016121406338), Dec 14, 2016: DETECTOR. MALFUNCTIONED. RIGHT ENGINE FIRE LIGHT DIMLY FLICKERED ON AND OFF OVER TEN TIMES ON APPROACH AND LANDING. ANTI-ICE ON OVER OFF MADE NO DIFFERENCE NOT DID MODERATE POWER TO IDL - [SDR JGVR20160808001](https://openairdocs.org/sdr/JGVR20160808001), Jul 28, 2016: ATTACH FITTING. CORRODED. CENTER WING TO FUSELAGE, FWD ATTACH FITTING HAS DEEP CORROSION ON THE BOTTOM. - [SDR DXTA2014040705718](https://openairdocs.org/sdr/DXTA2014040705718), Apr 4, 2014: COMPUTER. MALFUNCTIONED. CLIMBING THRU 20,000 FT AT 220 KTS, THE PITCH ANNUNCIATOR ILLUMINATED ON THE PFD. DISCONNECTED THE AUTOPILOT WHICH RESULTED IN THE ACFT PITCHING UP RAPIDLY. TRI - [SDR EBVR20131024001](https://openairdocs.org/sdr/EBVR20131024001), Oct 24, 2013: BEARING. FROZEN. DURING ELEVATOR REMOVAL, NOTICED THAT A NUMBER OF ELEVATOR ATTACHMENT BEARINGS ARE FROZEN AND REQUIRE REPLACEMENT. - [SDR DXTA2012040204935](https://openairdocs.org/sdr/DXTA2012040204935), Mar 30, 2012: BRAKE. MALFUNCTIONED. DURING A SHARP RT TURN AT TAXI, CO-PILOT`S RT BRAKE PEDAL LOST PRESSURE, & NEEDED TO BE PUMPED TO STOP ACFT FROM A 1 OR 2 MPH. CAPTAIN`S SIDE NEEDED A LOT OF MO - [SDR DXTA200702719](https://openairdocs.org/sdr/DXTA200702719), Dec 27, 2007: ACTUATOR. INOPERATIVE. FAILED TO GET LT MAIN GEAR LIGHT UPON EXTENDING MLG. JACKED A/C, REMOVED NR 2 ENG HYD PUMP TO FACILITATE HYD PWR W/ROBO MULE, REMOVED & REPLACED LT MLG ACTUATOR - [SDR DXTA200500822](https://openairdocs.org/sdr/DXTA200500822), Jul 7, 2005: SWITCH. FAILED. AFTER GEAR RETRACTION, UNLOCK LIGHT REMAINED ILLUMINATED. HYD PRESS AND STAB MISCOMPARE LIGHTS ALSO REMAINED ILLUMINATED. GEAR EXTENDED NORMALLY. UNLOCK LIGHT E - [SDR DXTA200500738](https://openairdocs.org/sdr/DXTA200500738), May 22, 2005: WINDSHIELD. FAILED. RIGHT FRONT WINDSHIELD SHATTERED DURING FLIGHT. REMOVED RT RAIN SHROUD, REMOVED RT HEATED WINDSHIELD, INSTALLED NEW SEAL ON NEW WINDSHILED IAW MM 56-11-00. PERF ## 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 20140728014959I](https://openairdocs.org/incident/20140728014959I), Jul 28, 2014: Cessna 560XL (N618QS), Orlando, FL, Substantial damage. Pilot was on a 6 mile left base for landing runway 25 at an altitude of 1,600 feet and an indicated air speed of 180 knots when the left wing tip leading edge… --- 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.