Bombardier Global Express

ENGINES
Rolls Royce BR710A2-20 on Corporate Care Program
Time Since New: 1203.34 / 1203.34
Cycles: 553 / 553

APU – Allied Signal RE-220 (GX) 0n MSP
Time Since New: 511
Cycles: 963
Avionics
Honeywell Primus 2000 XP Integrated Avionics System
6-Tube Electronic Flight Instrument System (EFIS) / Engine Instrument and
Crew Advisory System (EICAS) using DU-870 8 by 7-inch color displays
Dual fail-operational (automatic switching) auto-pilot
Triple integrated Flight Management Systems
Triple long-range NAV source (3 FMS’s)
Navigation Data Base Data Loader
Global Positioning System (GPS)
Dual full flight regime auto-throttle
Triple IC-800 Integrated Avionics Computers (IAC); built in EFIS reversionary capability and fault warning redundancy - combines the functions of five major subsystems
Triple IC-800 Integrated Avionics Computers (IAC); built in EFIS reversionary capability and fault warning redundancy - combines the functions of five major subsystems
Triple Micro Air Data Computers (MADC)
Triple LASEREF Inertial Reference Systems (IRS)
Quad DA-810 Data Acquisition Units (DAU)
Color Weather Radar - Dual control heads
Honeywell LSZ-860 Lightning Sensor System (LSS)
Dual Integrated Nav./Com/Ident. Radios - VOR/ILS/MKR, ADF,nDME, VHF Comm, Mode 'S' Diversity Transponder. Compliance with European 8.33 kHz channel spacing requirements
Honeywell RCZ-833 3rd VHF Transceiver
Honeywell Additional Global Positioning System (GPS)
Central Aircraft Information Maintenance System (CAIMS)
Miltope PrinterTP-4840
TCAS RT-950 Traffic Alert and Collision Avoidance System
Dual HF Comm
Selective Calling (SELCAL) System
Dual Radar Altimeter
Cockpit Voice Recorder (CVR)
Digital Flight Data Recorder (DFDR)
Enhanced Ground Proximity Warning System (EGPWS)
406MHz Emergency Locator Transmitter (ELT)
Sextant Head-up Display
Teledine Telelink
SATCOM
Features & Additional Equipment
NAT-MNPS; B-RNAV; RVSM; JAR-OPS1 Approval
Smart Part Enrolled
CAMP Maint. Tracking System Enrolled
Illuminated Ordinance Signs
Cabin/Lavatory Call System
Manual storage - cockpit - side consoles
Baker Cabin Management System (CMS):
Function control switch panels at every passenger location
IR Receiver/Transmitter c/w two (2) hand-held remotes
Entertainment System:
High quality cabin speaker arrangement
Passenger headphone distribution
Two (2) 21.3” LCD video monitors
Four (4) 10.4” plug-in video monitors
One (1) 6.5” plug-in video monitors
Compact Disc (CD) and Digital Video Disc (DVD) Player
Video Cassette Player (multi-standard)
Airshow 400
One (1) power converter (3500 VA/115V/60Hz)
Ten (10) clear leather seat with electric inflatable lumbar support
Tree (3) places16G divan, approved for taxi, take-off and landing, with armrest end cabinet. Two (2) slipping places when deployed. (RHS).
Conference Hi-Lo Table
Exterior service panel lights
Common panel keyed locks
Aft equipment bay ladder
Aft equipment bay storage box
Cockpit and Jump-seat flashlights
Footrests
Additional cockpit lights
Approach chart holders
Entry area heated
400 Hz Service Bus – ground power
Securaplane CAM-11 incorporating four (4) video cameras and CMX-01 vertical fin camera.
Interior
Thirteen passenger configuration with four place club chairs forward and 21.3” monitor on the forward bulkhead, a four place conference group opposite a credenza midcabin, and a three place berthable divan opposite two executive chairs and a 21.3” bulkhead monitor aft. Other features include a crew rest area with single executive seat, forward and aft lavs with vacuum flush toilets.
Weights
Gross Weight (Ramp): 96,250 lbs.
Max Take Off Weight: 96,000 lbs.
Fuel Capacity: 43,350 lbs.
Max Landing Weight: 78,600 lbs.
Max Zero Fuel Weight: 56,000 lbs.
Disclaimer
Not for sale in the United States or to any US Residents.