Airframe: |
The most accomplished and luxurious business jet ever brought to market, the Bombardier* Global 6000* aircraft was created to accommodate the needs of the most sophisticated and discerning travelers. Uncompromising throughout, from the superiority of its leading edge flight deck environment, to the sheer tranquility of its aft stateroom, the Global 6000 is the ultimate all-around performance business jet, designed to keep the world in the palm of your hand.
• Leading the world in sheer space, luxury and peace of mind
• Technology at the cutting edge of corporate aviation
• A spacious cabin with a well-appointed aft stateroom and its own adjoining amenities,
accords optimal relaxation and privacy
ENGINES:
Rolls-Royce Deutschland
BR710A2-20 turbofans
Thrust: 14,750 lb (65.6 kN)
Flat rated to: ISA + 20°C (95°F)
AVIONICS:
• Rockwell Collins Pro Line Fusion avionics suite
• Four 15.1-inch (38.4 cm) Liquid Crystal Display (LCD) screens
• Head-Up Display System (HUD), 3rd generation Enhanced Vision System (EVS) and Synthetic
Vision System (SVS)
• Onboard Maintenance System (OMS)
- Advanced diagnostic and troubleshooting tool integrated with most aircraft systems:
available on MultiFunctionDisplay orfor download onto a portable computer
- Available both on the ground and in flight, OMS minimizes troubleshooting workload and
reduces aircraft downtime
• Datalink, SATCOM: Inmarsat, Iridium
• Ethernet-based Cabin Electronic System with on-board Local Area Network (LAN) and wireless LAN
• Dual channel high-speed data, printer
PERFORMANCE:
Range:
At M 0,85:
6,000 NM 6,905 SM 11,112 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 0.89 513 590 950
Typical cruise speed 0.85 488 564 907
Airfield Performance
Takeoff distance (SL, ISA, MTOW): 6,476 ft (1,974 m)
Landing distance (SL, ISA, MLW): 2,670 ft (814 m)
Operating Altitude
Maximum operating altitude: 51,000 ft (15,545 m)
Initial cruise altitude after MTOW departure: 41,000 ft (12,497 m)
Relative cabin pressure altitude at 45,000 ft (13,716 m): 4,500 ft (1,371 m)
Noise Level (EPNdB)
Flyover: 83.5
Approach: 89.7
Lateral: 88.7
DIMENSIONS:
Exterior:
Length: 99.4 ft (30.3 m)
Wingspan: 94 ft (28.7 m)
Height overall: 25.5 ft (7.8 m)
Interior
Crew: 2-4
Passengers: 8-19
Cabin length: 48.35 ft (14.7 m) (from start of forward lavatory to end of pressurized compartment)
Cabin 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)
Floor area: 335 ft2 (31.1 m2) (excluding cockpit)
Cabin volume: 2,140 ft3 (60.6 m3) (from start of forward lavatory to end of pressurized compartment)
Weights
A. Maximum ramp weight: 99,750 lb (45,246 kg)
B. Maximum takeoff weight: 99,500 lb (45,132 kg)
C. Maximum landing weight: 78,600 lb (35,652 kg)
D. Maximum zero fuel weight: 56,000 lb (25,401 kg)
E. Typical basic operating weight: 52,230 lb (23,691 kg)
F. Maximum fuel weight: 45,050 lb (20,434 kg)
Maximum payload (D-E): 3,770 lb (1,710 kg)
Payload - maximum fuel (A-E-F): 2,470 lb (1,120 kg)
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