General PERFORMANCE DIMENSIONS
Capacity Range Exterior
Crew: 2 Maximum range: Length: 58.69 ft (17.89 m)
2,405 NM 2,768 SM 4,454 km
Passengers: Up to 8 + 1 Wingspan: 41.81 ft (12.74 m)
(NBAA IFR 100 NM reserves, ISA, with 4 pax/2 crew)
Overall Wingspan: 43.79 ft (13.34 m)
Engines
Speed Mach kt mph km/h Wing area: 264.5 ft2 (24.57 m2)
Pratt & Whitney Canada
High-speed 0.81 466 536 863 (basic)
PW305A turbofans
Typical cruise Height overall: 14.56 ft (4.44 m)
Thrust: 4,600 lb (20.46 kN)
speed 0.79 453 521 839
Flat rated to: ISA + 17°C (90°F) Interior
Long-range
speed 0.74 426 491 789 Cabin length: 17.67 ft (5.39 m)
Avionics
(from cockpit divider to end
• A
ll-digital Rockwell Collins of pressurized compartment)
Airfield Performance
Pro Line 21 four LCD EFIS Cabin width: 5.95 ft (1.81 m)
Takeoff distance (SL, ISA, MTOW):
• D
ual automatic Attitude Heading (centerline)
5,450 ft (1,661 m)
Reference System (AHRS) Cabin width: 3.80 ft (1.16 m)
Landing distance (SL, ISA, MLW):
• D
igitized Engine Indication 3,420 ft (1,042 m) (floorline)
System (EIS) Cabin height: 5.71 ft (1.74 m)
• Integrated Flight Instrument Operating Altitude
Floor area: 69 ft2 (6.41 m2)
System (IFIS) with electronic charts Maximum operating altitude: (excluding cockpit)
• Dual nav/comm systems 51,000 ft (15,545 m)
Cabin volume: 453 ft3 (12.83 m3)
• Dual Flight Management System (FMS) Climb to cruise altitude (from cockpit divider to end
of 41,000 ft (12,497 m) of pressurized compartment)
• T
raffic Collision Avoidance System after MTOW departure:
(TCAS II) 18 min, 30 sec Weights
• E
nhanced Ground Proximity A. Maximum ramp weight:
Warning System (EGPWS) with Noise Level (EPNdB) 23,750 lb (10,773 kg)
Windshear alert Flyover (thrust cutback): 70.8 B. Maximum takeoff weight:
True to its thoroughbred form, the Bombardier * Learjet* 60 XR easily
Approach: 87.7 23,500 lb (10,659 kg)
outpaces the competition in time-to-climb performance and operating Entertainment
Lateral: 83.2 C. Maximum landing weight:
altitude without compromising a class-leading low operating cost. With • Bulkhead Monitors (Forward & Aft)
19,500 lb (8,845 kg)
its cutting-edge cockpit technologies and stylishly redefined cabin space, • Moving Map System
D. Maximum zero fuel weight:
the Learjet 60 XR business jet speeds four passengers across distances 17,000 lb (7,711 kg)
of up to 2,405 nautical miles (4,454 km) with ease. E. Typical basic operating weight:
14,896 lb (6,757 kg)
• Class-leading low operating cost F. Maximum fuel weight:
7,910 lb (3,588 kg)
• Rethought, redesigned interior provides passengers with more space
Maximum payload (D-E):
and better cabin functionality
2,104 lb (954 kg)
• ‘Next-generation’ flight deck design and technologies led by the Rockwell Payload – maximum fuel (A-E-F):
Collins Pro Line 21 avionics suite, with paperless chart capability 944 lb (428 kg)
Fuel with maximum payload (A-D):
6,750 lb (3,062 kg)
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. All internal
dimensions are based on an aircraft without a completed interior. 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.
©2011 Bombardier Inc. All rights reserved. *Registered Trademark(s) or Trademark(s) of Bombardier Inc. or its subsidiaries.
Printed in Canada (09/11).
