global_8000_factsheet

Bombardier Aerospace, Business Aircraft, 400 Côte-Vertu Road West, Dorval, Québec, Canada H4S 1Y9 In North America call 800-268-0030 • Elsewhere call 514-855-7698 • www.businessaircraft.bombardier.com All data in this document is approximate, currently under development and remains to be finalized and certified. The representations made and the images shown in this document are solely based on projections and forecasts and may change or be withdrawn without notice and without prejudice. This document does not constitute an offer, commitment, representation or warranty of any kind. The actual configuration and performance of the aircraft shall be determined in a final purchase agreement. ©2011 Bombardier Inc. All rights reserved. *Registered Trademark(s) or Trademark(s) of Bombardier Inc. or its subsidiaries. **Under certain operating conditions. Printed in Canada (01/11). The new Bombardier* Global* 8000 business jet is at the forefront of business aviation with an unparalleled combination of cabin comfort and an unprece- dented range capability. Achieving a remarkable 7,900 nm range at Mach 0.85 with 8 passengers**, the Global 8000 promises faster connections and opens key routes such as LA-Sydney, Hong Kong-New York, and Mumbai-New York. Next-generation GE engines developed for this aircraft set the new standard for efficiency, with the lowest fuel burn and lowest emissions in its class. • 7,900 nm range at Mach 0.85 with 8 passengers** and an unsurpassed Mach 0.90 high-speed cruise capability • Largest and most comfortable cabin in its class • Next-generation GE engines deliver more efficiency with low fuel burn and low emissions. General Capacity Crew: 2-4 Passengers: 8-19 engines Next-generation GE engines Thrust: 16,500 lb (73.4 kN) Flat rated to: ISA + 20°C (95°F) avionics and Cabin Communication • Global Vision Flight Deck • Four Large Liquid Crystal Display (LCD) Screens • Head-Up Display System (HUD), Enhanced Vision System (EVS) and Synthetic Vision System (SVS) • Graphical Flight Planning • Weather Radar with enhanced functionality like windshear detection • Latest Performance Based Navigation: - Wide Area Augmentation System (WAAS) - LPV Approach - RNAV, En-route RNP & RNP AR Approaches • Controller Pilot Data Link Communication (CPDLC) • Onboard Maintenance System (OMS) • Datalink, High Speed SATCOM • Next Generation Cabin Management System (CMS) PerFOrManCe range At M 0.85: 7,900 NM 9,098 SM 14,631 km At M 0.90: 5,650 NM 6,507 SM 10,464 km (Theoretical range with NBAA IFR Reserves, ISA, 8 pax/4 crew. Actual range will be affected by speed, weather, selected options and other factors.) Speed Mach kt mph km/h High-speed 0.90 517 594 957 Typical cruise speed 0.85 488 564 907 airfield Performance Takeoff distance (SL, ISA, MTOW): 5,800 ft (1,768 m) Landing distance (SL, ISA, MLW): 2,810 ft (856 m) Operating altitude Maximum operating altitude: 51,000 ft (15,545 m) Initial cruise altitude after MTOW departure: 43,000 ft (13,106 m) DIMenSIOnS exterior Length: 101.6 ft (30.97 m) Wingspan: 104.3 ft (31.79 m) Height overall: 26.7 ft (8.14 m) Interior Cabin length: 50.6 ft (15.42 m) (from cockpit divider to end of presurized compartment) Cabin maximum width: 8.17 ft (2.49 m) (centerline) Cabin width: 6.92 ft (2.11 m) (floorline) Cabin height: 6.25 ft (1.91 m) (vary with interior selection) Cabin volume: 2,236 ft3 (63.32 m3) Weights A. Maximum ramp weight: 105,050 lb (47,650 kg) B. Maximum take off weight: 104,800 lb (47,536 kg) C. Maximum landing weight: 85,800 lb (38,918 kg) D. Maximum zero fuel weight: 60,000 lb (27,216 kg) E. Standard basic operating weight: 54,300 lb (24,630 kg) (vary with interior selection) F. Maximum fuel weight: 48,950 lb (22,203 kg) Maximum payload (D-E): 5,700 lb (2,585 kg) Payload - maximum fuel (A-E-F): 1,800 lb (817 kg)