庞巴迪挑战者605 Bombardier Challenger 605

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General
Capacity
Crew: 2+1
Passengers: Up to 12
engines
General Electric
CF34-3B turbofans
Thrust: 8,729 lb (38.84 kN)
Thrust with APR: 9,220 lb (41.0 kN)
Flat rated to: ISA + 15°C (86°F)
avionics
• Rockwell Collins Pro Line 21 with four
10” x 12” (25.4 cm x 30.5 cm) LCD
screens and integrated menu control
• Dual autopilot with single autothrottle
• EFIS/EICAS system with synoptics
• Dual FMS-6000 with coupled lateral and
vertical nav, performance calculations
• Integrated Flight Information
System (IFIS)
• Dual Honeywell Laseref V Inertial
Reference System
• Integrated Radio Tuning with Rockwell
Collins Pro Line 21 VHF/Nav radios
• Integrated electronic standby instruments
• Optional Head-Up Guidance
System (HGS)/Bombardier Enhanced
Vision System (BEVS)
PerFOrManCe
range
Maximum range at M 0.74:
4,010 NM 4,614 SM 7,427 km
(Theoretical range at M 0.74 with 5 passagers/2 crew,
NBAA IFR reserves, ISA, typical BOW and maximum
allowable fuel. Actual range will be affected by speed,
weather, selected options and other factors.)
Speed Mach kt mph km/h
High-speed 0.82 470 541 870
Typical
cruise speed 0.80 459 528 850
Long-range
speed 0.74 425 489 787
airfield Performance
Takeoff distance (SL, ISA, MTOW):
5,840 ft (1,780 m)
Landing distance (SL, ISA, MLW):
2,777 ft (846 m)
Operating altitude
Maximum operating altitude:
41,000 ft (12,497 m)
Climb to cruise altitude of
37,000 ft (11,278 m): 22 minutes
noise level (ePndB)
Flyover: 81.2
Approach: 90.3
Lateral: 86.2
DIMenSIOnS
exterior
Length: 68.42 ft (20.85 m)
Wingspan: 64.33 ft (19.61 m)
Wing area: 492 ft2 (45.71 m2)
(basic)
Height overall: 20.67 ft (6.30 m)
Interior
Cabin length: 28.42 ft (8.66 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: 202 ft2 (18.77 m2)
(excluding cockpit)
Cabin volume: 1,150 ft3 (32.56 m3)
(from cockpit divider to end
of pressurized compartment)
Weights
A. Maximum ramp weight:
48,300 lb (21,909 kg)
B. Maximum takeoff weight:
48,200 lb (21,863 kg)
C. Maximum landing weight:
38,000 lb (17,237 kg)
D. Maximum zero fuel weight:
32,000 lb (14,515 kg)
E. Typical basic operating weight:
26,915 lb (12,209 kg)
F. Maximum fuel weight:
20,000 lb (9,072 kg)
Maximum payload (D-E):
5,085 lb (2,306 kg)
Payload with maximum fuel (A-E-F):
1,385 lb (628 kg)
Fuel with maximum payload (A-D):
16,300 lb (7,394 kg)
Next-generation by design, the Bombardier* Challenger* 605 widebody
business jet was built in response to the needs and necessities of pilots
and business leaders alike. Now, even more spacious, the aircraft is
designed with more business, relaxation and entertainment flexibility
than any other large business jet. Benefits derived from the 25-year-plus
Bombardier Regional Jet program are felt in every aspect, with increased
payload/range capacity and superior airliner maintainability.
• Evolution of the best-in-class business environment, offering the widest
cabin in its class
• Latest-generation cockpit functionality and simplicity led by the
Rockwell Collins Pro Line 21 avionics suite
• Airliner maintainability, superior aircraft reliability.
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.
Printed in Canada (05/09).