2019 BOMBARDIER Global 5000 SOLD

Airframe Year of Manufacture: 2019 In-service date: 22 June 2020 Total Time: 1,999 hrs as of Feb. 2024 Total Landings: 595 flights Engine Model: Rolls Royce PEARL 15 Engines on JSSI APU Model: Honeywell RE220 (GX) Hours: 1,202 hrs APU on JSSI Options Installed Quick Access Recorder Datalink Graphical Weather System EU Air OPS Part CAT operations Take-off & Landing Awareness Function (TLAF) Surface Management System Aft Cabin equipped with two (2) 16G 3-Place Divan Provision Installation for KA Band High Speed Connectivity including Software only (Radome not included) Avionics The Aircraft is equipped with the Bombardier Vision Flight Deck Avionics Suite, complete with Four (4) 14”x11” Landscape Active Matrix Liquid Crystal Displays (AMLCD). Options Installed Datalink Graphical Weather System Quick Access Recorder Auto Flight Dual three-axis, Category II Automatic Flight Control Systems (AFCS) is provided with pitch & roll channels & an independent linear actuator for the yaw axis. The AFCS includes computations for: Flight guidance Autothrottle Autopilot Yaw damper Automatic pitch trim The flight director modes include Emergency Descent Mode which will automatically turn and dive the Aircraft down to 15,000 ft when the system senses pressurization issues & pilots do not take action within a specific amount of time. Communications The communication system provides equipment designed to supply communication in the Aircraft, between different aircraft & between the Aircraft & ground stations. The Aircraft communication system includes: Three (3) VHF communication radios Two (2) HF transceivers One (1) dual SELCAL system capable of monitoring three (3) VHF & two (2) HF radios One (1) handset using the cabin satellite airborne telephone system One (1) data communication channel (ACARS), which in conjunction with the VHF meets the requirements of Future Air Navigation System (FANS 1/A+) including Airline Operational Control (AOC), Air Traffic Services (ATS), Facilities Notifications (AFN), Automatic Dependent Surveillance – Contract (ADSC) & Controller Pilot Datalink Communication (CPDLC) One (1) dual channel interphone system with hand-held microphones & individual controls for pilot, co-pilot & flight observer seat Indicating / Recording System Electronic Flight Instrument System (EFIS) Engine Indication & Crew Awareness System (EICAS) Synchronized digital GPS Clock Cockpit Voice Recorder (CVR) Flight Data Recorder (FDR) Emergency Locator Transmitter (ELT) Navigation Two (2) Integrated Flight Information Systems (IFIS)2 with dual File Server Unit One (1) Head-Up Display (HUD) System One (1) Enhanced Vision System (EVS) One (1) Synthetic Vision System (SVS) One (1) Electronic Integrated Standby Instrument (ISI) One (1) Air Data System (ADS) composed of three (3) Air Data Computers (ADC) One (1) Auto-tilt Weather Radar Three (3) Inertial Reference Systems (IRS) Two (2) GPS WAAS receivers Two (2) VHF navigation receivers Two (2) ADF receivers Two (2) DME transceivers One (1) Traffic Surveillance System and One (1) standalone Transponder capable of Dual transponder functionality, TCAS II change 7.1, ADS-B Out Two (2) Radio Altimeter systems One (1) Terrain Awareness & Warning System (TAWS) Three (3) Flight Management Systems (FMS) Interior 14 Passenger configuration – certified for 13 pax during take off & landing Forward Cabin: Four (4) Place Club Seats Mid Cabin: Four (4) Place Conference Group opposite a Credenza Aft Cabin: Two (2) 16G 3- Place Divan Forward & Aft Lavatory The main cabin has a flat floor throughout & includes the following: Manually operated sliding pocket door, with electric release, separating the galley from forward cabin & one pocket door leading into the aft cabin. RH hinged door to close out the aft lavatory Communication System including Passenger Notification Intercoms & Flight Attendant Call Dual Channel Iridium Telephone System Inmarsat Swift Broadband (SBB) Satellite Communication System providing up to 432 Kilobits per second (kbps) Internet Speed Capability & a Voice Channel when not in use by the cockpit Ten (10) Universal GFCI Electrical Universal Outlets at various locations Five (5) Wireless Passenger Control Units (WPCU) to control the Cabin System including Entertainment, Cabin Utilities & Displays Cabin management system featuring a Fiber Optic Network In-Flight Entertainment (IFE) System including worldwide maps & Audio Cabin Briefing One (1) 24” HD monitor port mounted on the aft facing bulkhead in Forward Cabin One (1) 24” HD monitor mounted on the forward facing bulkhead in Aft Cabin Electric accordion type window shades The Passenger Service Unit (PSU) incorporates a handrail, oxygen masks for each seating position, cabin entertainment system speakers, PA speakers, individual adjustable air gaspers & lighting Galley The RH galley includes: Crystal showcase Flat