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