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Home Aircraft Learjet 85
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Overview
True to its heritage, Bombardier Learjet 85 is an all-new platform that embodies dramatic advances in aerodynamics, structures, efficiency and comfort

  • Greater cabin choices and a range of floor plan options
  • 3-place divan, deluxe galley and more for optimal comfort and convenience
  • Equipped with superior long range cruise speed and highly competitive field performance
Technical Specifications
Capacity
Crew: 2
Passengers: Up to 8 + 2
Dimensions
Exterior
Length: 68.1 ft 20.76 m
Wingspan (overall): 61.5 ft 18.75 m
Wing area (basic): 401 ft² 37.25 m²
Height overall: 19.9 ft 6.07 m
Interior (finished Dimensions)
Cabin length (±1%):
(From cockpit divider to end of pressurized compartment)
24.75 ft 7.54 m
Cabin width (±1%):
(maximum)
6.08 ft 1.85 m
Cabin height (±1%):
(maximum over aisle)
5.91 ft 1.80 m
Cabin volume (±3%): 665 ft³ 18.83 m³
Target Weights and Capacities*
A. Maximum ramp weight: 33,750 lb 15,309 kg
B. Maximum takeoff weight (±2%): 33,500 lb 15,195 kg
C. Maximum landing weight (±2%): 30,150 lb 13,676 kg
D. Maximum zero fuel weight: 24,200 lb 10,977 kg
E. Standard basic operating weight**: 21,500 lb 9,752 kg
F. Approximate Fuel Capacity (±2%): 11,310 lb 5,130 kg
(usable 6.70 lb/gal)
* These figures may change at anytime and without prior notice during the datailes design and development of the aircraft.
** Includes unusable fuel, oil, standard interior, standard avionics, paint and 2 crew. Actual weight will vary with individual aircraft as a result of customization and optional equipement.
Performance
Range
Maximum range (±5%): 3,000 NM 3,455 SM 5,556 km
(NBAA IFR 100 nm alternate fuel reserves, 4 passengers (200 lb each), 2 crew, standard BOW, sea level departure and landing, unrestricted climb, cruise and descent with zero wind and standard ISA conditions en route)
Speed Mach kt mph km/h
High-speed 0.82 470 541 871
at 43,000 ft, 31,200 lb cruise weight, standard ISA conditions
 
Long-range cruise speed (±3%) 0.78 447 515 829
at 43,000 ft, 31,200 lb cruise weight, standard ISA conditions
 

Range Map - Beijing Shanghai Hong Kong

Download Factsheet
Airfield Performance
Takeoff distance (±5%): 4,800 ft 1,463 m
(SL, ISA, MTOW. Field lengths are based on
a level hard surface, dry paved runway with zero wind.)
Landing distance (±5%): 2,700 ft 823 m
(SL, ISA, MLW, 14CFR 91. Field lengths are based on
a level hard surface, dry paved runway with zero wind.)
Operating Altitude
Maximum operating altitude: 49,000 ft 14,935 m
Initial cruise ceiling :
(SL, ISA, MTOW)
43,000 ft 13,106 m
Relative Cabin Pressure altitude at 49,000 ft (14,935 m) 6,000 ft (1,829 m)
Engines
Pratt & Whitney Canada PW307B turbofans
Thrust: 6,100 lb (27.13 kN)
Flat-rated to: ISA + 15°C (86°F)
Avionics
Rockwell Collins Pro Line Fusion avionics suite, with three 15.1”(38.4 cm) Active Matrix Liquid Crystal Displays (AMLCD)
Electronic Flight Instrument System (EFIS)
Inertial Reference System (IRS)
Integrated Flight Information System (IFIS) with electronic charts
One Class II Electronic Flight Bag (EFB)
Synthetic Vision System for Situational Awareness (SVS)
Terrain Awareness and Warning System (TAWS)
Dual Flight Management System (FMS)
Weather Radar System
Autothrottle
Wide Area Augmentation System (WAAS)
Single HF
 
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