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learjet_60_xr_factsheet

learjet_60_xr_factsheet - GENEral Capacity PErFOrMaNCE...

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DIMENSIONS Exterior Length: 58.69 ft (17.89 m) Wingspan: 43.79 ft (13.35 m) Wing area: 264.5 ft 2 (24.57 m 2 ) (basic) Height overall: 14.56 ft (4.44 m) Interior Cabin length: 17.67 ft (5.39 m) (from cockpit divider to end of pressurized compartment) Cabin width: 5.95 ft (1.81 m) (centerline) Cabin width: 3.80 ft (1.16 m) (floorline) Cabin height: 5.71 ft (1.74 m) Floor area: 69 ft 2 (6.41 m 2 ) (excluding cockpit) Cabin volume: 453 ft 3 (12.83 m 3 ) (from cockpit divider to end of pressurized compartment) Weights 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: 15,180 lb (6,886 kg) F. Maximum fuel weight: 7,910 lb (3,588 kg) Maximum payload (D-E): 1,820 lb (826 kg) Payload – maximum fuel (A-E-F): 660 lb (299 kg) Fuel with maximum payload: 6,750 lb (3,062 kg) GENERAL Capacity Crew: 2 Passengers: Up to 8 + 1 Engines Pratt & Whitney Canada PW305A turbofans Thrust: 4,600 lb (20.46 kN) Flat rated to: ISA + 17°C (90°F) Avionics All-digital Rockwell Collins Pro Line 21 four LCD EFIS Dual automatic Attitude Heading Reference System (AHRS)
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  • Fall '08
  • Yousuff
  • Aviation terminology, Maximum Takeoff Weight, Bombardier Aerospace, Maximum Zero-Fuel Weight, Traffic Collision Avoidance System

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