For Sale: 2022 Bombardier Global 7500
US Based & Registered
Entry Into Service Late 2022
170 Hours TT
Full Manufacturer Warranty Transferable
KA Band Wi-Fi
Aft Stateroom with Large Bed
40" HD Monitor on Credenza
Surface Management System
Airframe: (As of April 2023)
170 Hours Since New
GENERAL ELECTRIC PASSPORT
Engine 1 170 SNEW 60 CSN
Engine 2 170 SNEW 60 CSN
APU: SAFRAN SPU300[BA]
PSU handrail upholstered in Ultraleather.
Upholstered Aft Stateroom Bed headboard.
Jump Seat Sheep skin cover.
Crew Area Partition Access Door.
Crew Area Magazine Rack.
Additional Pull-Out Worksurface under microwave oven in the Galley.
Provisions for coffee maker in a Galley compartment with a slide-out tray behind a nesting door.
Interior: 13-passenger plus bed. Forward galley, crew rest and lav. Aft main lav.
Zone 1: Fwd Cabin Bulkhead with LH Door and RH 24" Flush Mounted Bulkhead Monitor. RH & LH Single Lounge Seats. Lounge Seats with Depth Adjustment.
Zone 2: 6-place Angled Conference Grouping.
Zone 3: RH Credenza & LH Divan. Top Mounted 40" HD Monitor on Credenza.
Zone 4: Aft Stateroom - RH Narrow Credenza with LH Large Bed. Flush Mounted 32'' HD Monitor on forward face aft LH Bulkhead.
Baggage: Additional Water Tank Enclosure Baggage Shelves. Additional Baggage Coat Rod.
Cabin Main Cabin Gaspers.
Miscellaneous: Qty 6 "Bed-In-A-Bag" - loose equipment.
The full fly-by-wire (FBW) flight control system features the Bombardier Vision Flight Deck:
Four 14” x 11” AMLCS - LCD Adaptive Flight Displays Three (3) VHF communication radios Two (2) HF transceivers One (1) dual SELCAL system capable of monitoring three (3) VHF and two (2) HF radios One (1) Iridium Satellite Comm. Sys. with two (2) voice channels and one (1) ata Channel One (1) dual channel interphone system Two (2) Integrated Flight Information System (IFIS) 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 four (4) Air Data Smart Probes (ADSP) One (1) 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 and Warning Sys. (TAWS) Three (3) Flight Management Systems (FMS) Electronic Flight Instrument System (EFIS) Electronic Checklist (ECL) Dual synchronized digital GPS clocks Engine Indication and Crew Awareness Sys. (EICAS) Cockpit Voice Recorder (CVR) Flight Data Recorder (FDR) with underwater location Emergency Locator Transmitter (ELT) Automatic Flight Control Systems (AFCS) · Flight guidance; · Autothrottle; · Autopilot; · Yaw damper; · Automatic pitch trim.
Additional Options: Surface Management System – Airport Moving Map, Predictive windshear, Vertical weather
Three (3) portable fire extinguishers
Crew and passenger life vests
Three (3) rafts with an integrated ELT
Three (3) smoke detectors with EICAS annunciation (lavs & Baggage Compartment)