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General 
Capacity 
Crew: 2 
Typical seating: 14 to 15 
Engines 
General Electric 
CF34-3B1 turbofans 
Thrust: 8,729 lb (38.84 kN) 
Thrust with APR: 9,220 lb (41.0 kN) 
Flat rated to: ISA + 8°C (73°F) 
Avionics 
• Rockwell Collins Pro Line 4 
six-screen EFIS 
• Two-screen EICAS 
• Dual Flight Management System 
(FMS) 4200 
• Dual Global Positioning System (GPS) 
• Dual Inertial Reference System (IRS) 
• Dual DME / Dual ADF 
• Enhanced Ground Proximity Warning 
System (EGPWS) 
• Traffic Collision Avoidance System 
(TCAS II) 
PER FORMAN CE 
Range 
8 passengers: 
2,770 NM 3,187 SM 5,129 km 
(Theoretical range with NBAA IFR Reserves, ISA, 
8 pax/2crew. Actual range will be affected by speed, 
weather, selected options and other factors.) 
Speed Mach kt mph km/h 
High-speed 0.80 459 528 850 
Typical 
cruise speed 0.77 442 509 819 
Long-range 
speed 0.74 425 489 787 
Airfield Performance 
Takeoff distance (SL, ISA, MTOW): 
6,305 ft (1,922 m) 
Landing distance (SL, ISA, MLW): 
2,910 ft (887 m) 
Operating Altitude 
Maximum operating altitude: 
41,000 ft (12,497 m) 
Noise Level (EPNdB) 
Flyover: 78.8 
Approach: 92.1 
Lateral: 82.4 
DIMEN SIONS 
Exterior 
Length overall: 87.83 ft (26.77 m) 
Wingspan: 69.58 ft (21.21 m) 
Wing area (net): 520.4 ft2 (48.35 m2) 
Height overall: 20.42 ft (6.22 m) 
Interior 
Cabin length: 48.42 ft (14.76 m) 
(from cockpit divider to end 
of pressurized compartment) 
Cabin width: 8.17 ft (2.49 m) 
(centerline) 
Cabin width: 7.17 ft (2.19 m) 
(floorline) 
Cabin height: 6.08 ft (1.85 m) 
Floor area: 346 ft2 (32.14 m2) 
(excluding cockpit) 
Cabin volume: 1,990 ft3 (56.35 m3) 
(excluding cockpit) 
Weights 
A. Maximum ramp weight: 
53,250 lb (24,154 kg) 
B. Maximum takeoff weight: 
53,000 lb (24,040 kg) 
C. Maximum landing weight: 
47,000 lb (21,319 kg) 
D. Maximum zero fuel weight: 
44,000 lb (19,958 kg) 
E. Typical basic operating weight: 
34,790 lb (15,780 kg) 
F. Maximum usable fuel weight: 
18,274 lb (8,289 kg) 
Maximum payload (D-E): 
9,210 lb (4,178 kg) 
Payload - maximum fuel (A-E-F): 
186 lb (85 kg) 
Fuel with maximum payload: 
9,250 lb (4,196 kg) 
Airliner endurance partners with business jet comfort and flexibility, in the 
‘class-capturing’ Bombardier* Challenger* 850 aircraft. With the largest, 
most versatile interior in its class, and a non-stop range that delivers 
transcontinental ease, this powerful and rugged large corporate jet aircraft 
has become the gold standard for reliability, dependability and value. 
• Superior space, flexibility and corporate luxury 
• Airframe proven in over 11 million hours of service 
• Powered by the fuel efficient, reliable General Electric 
CF34-3B1 turbofans 
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 
Performance is based on maximum takeoff/landing weight, sea level, standard day (ISA) conditions, unless otherwise noted. All 
data in this document is approximate, for discussion purposes only and may be subject to certain conditions. This document 
does not constitute an offer, commitment, representation or warranty of any kind. All data is subject to change without prior 
notice. The interior images shown are for information purposes only and may represent some optional configurations. The final 
configuration and performance of the aircraft shall be as per the contractually agreed upon purchase agreement. 
©2008 Bombardier Inc. All rights reserved. * Registered Trademark(s) or Trademark(s) of Bombardier Inc. or its subsidiaries. |   
 
  
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