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Learjet 60 Specification

The document provides specifications for the Bombardier Learjet 60 aircraft, including its performance capabilities, dimensions, and operating costs. It can carry 6-8 passengers up to a maximum range of 2,496 nautical miles, has a maximum operating altitude of 51,000 feet, and cruises at speeds between 457-486 mph. Key specifications include its length of 58.69 feet, wingspan of 43.79 feet, and maximum takeoff weight of 23,500 pounds.

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0% found this document useful (0 votes)
1K views2 pages

Learjet 60 Specification

The document provides specifications for the Bombardier Learjet 60 aircraft, including its performance capabilities, dimensions, and operating costs. It can carry 6-8 passengers up to a maximum range of 2,496 nautical miles, has a maximum operating altitude of 51,000 feet, and cruises at speeds between 457-486 mph. Key specifications include its length of 58.69 feet, wingspan of 43.79 feet, and maximum takeoff weight of 23,500 pounds.

Uploaded by

shabashakkim
Copyright
© Attribution Non-Commercial (BY-NC)
We take content rights seriously. If you suspect this is your content, claim it here.
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Download as PDF, TXT or read online on Scribd
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GENERAL SPECIFICATIONS. PERFORMANCE. DIMENSIONS.

GENERAL

Noise Level
EPNdB 2 Takeoff: Approach: Sideline: 78.9 87.7 83.2

Capacity
Crew: Passengers: Up to 8

Engines
Pratt & Whitney Canada PW305A turbofans Thrust: 4,600 pounds (20.46 kN) thrust at takeoff Flat-rating: ISA + 17C (90 F)
DIMENSIONS

External
Length: Wingspan: Wing area:
(basic)

58.69 ft (17.89 m) 43.79 ft (13.35 m) 264.5 ft2 (24.57 m2) 14.56 ft (4.44 m)

Avionics
All-digital Collins Pro Line 4 four-tube EFIS

For transcontinental range, exceptional climb capabilities, state-of-the-art avionics and proven, fuel-efficient strategies, the Bombardier Learjet 60 offers an incomparable aircraft with one of the lowest operating costs among midsize jets. With a maximum range of 2,496 nautical miles (4,633 km) and a cabin that seats six to eight passengers, the Learjet 60 is capable of any number of long-range assignments.

Dual automatic heading & attitude reference systems (AHRS) WXR840 weather radar Dual nav/comm systems Dual UNS-1C FMS
PERFORMANCE

Height overall:

Internal
Cabin length: Cabin maximum width: (centerline) Cabin width: (floorline) Cabin height: (excluding cockpit) Total volume: 453 ft3 (12.80 m3) 17.67 ft (5.39 m) 5.95 ft (1.81 m) 3.9 ft (1.19 m) 5.71 ft (1.74 m) 68.9 ft2 (6.40 m2)
(from cockpit divider to end of pressurized compartment)

Range
Maximum range: 2,496 NM 2,872 SM 4,623 km
(IFR Reserves, ISA, with 4 pax/2 crew)

Speed
High-speed cruise Typical cruise speed

Mach
0.81 0.79

kts. mph km/h Floor area:


464 457 422 534 526 486 859 846 782

(from cockpit divider to end of pressurized compartment)

Long-range cruise speed 0.74

Weights Airfield Performance


Balanced field length (SL, ISA, MGTOW): Landing distance (SL, ISA, MLW): 5,450 ft (1,661 m) 3,420 ft (1,042 m) A. Maximum ramp weight: 23,750 lb (10,773 kg) B. Maximum takeoff weight: 23,500 lb (10,659 kg) C. Maximum landing weight: 19,500 lb (8,845 kg)

D. Maximum zero fuel weight: 17,000 lb (7,711 kg) E. Typical basic operating weight: F. Maximum fuel weight: Maximum payload (D-E): Payload full fuel (A-E-F): 14,746 lb (6,689 kg) 7,910 lb (3,588 kg) 2,254 lb (1,022 kg) 1,094 lb (496 kg) 6,750 lb (3,062 kg)

Ceiling
Maximum operating altitude: 51,000 ft (15,545 m)
BOMBARDIER AEROSPACE BUSINESS AIRCRAFT 400 CTE-VERTU ROAD WEST DORVAL, QUBEC, CANADA H4S 1Y9 IN NORTH AMERICA CALL 800-268-0030 ELSEWHERE CALL 514-855-7698 WWW.AERO.BOMBARDIER.COM
PERFORMANCE IS BASED ON MAXIMUM TAKEOFF/LANDING WEIGHT, SEA LEVEL, STANDARD DAY (ISA) CONDITIONS, UNLESS OTHERWISE NOTED. 2002 BOMBARDIER INC. ALL RIGHTS RESERVED. 08/02/USA

Climb to cruise altitude of 41,000 ft (12,497 m) after MGTOW departure:

18 min, 30 sec

Fuel with maximum payload:

REGISTERED TRADEMARK OF BOMBARDIER.

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