The Bombardier Learjet® 45 flies faster and farther, with more passengers, than any other corporate aircraft in its class. Combining superior comfort and legendary Learjet performance, it offers easy handling characteristics, enhanced fuel efficiency, and outstanding reliability and maintainability. The Bombardier Learjet 45 is the only aircraft under 35,000 pounds (15,876 kg) to offer the latest systems software and architecture to minimize pilot and maintenance workload. It is also the only aircraft in this weight class certified by both the U.S. Federal Aviation Administration (FAA) and European Joint Aviation Authorities (JAA).
Features built for comfort:
Eight luxurious leather double club style executive seats that swivel, recline, and adjust laterally for individual comfort- Spacious Cabin design with plenty of head, shoulder, feet, and elbow room
- Sixteen executive size windows along the fuselage add to an extremely spacious feeling
- Refreshment centre with microwave and a variety of food selections available
- On board, there are 17 cubic feet of in-cabin baggage storage, plus a separate forward coat closet
- Baggage compartment provides 51 cubic feet of heated cargo space
- Private and spacious lavatory
- Extra Large handcrafted fold-out tables provide a very generous working space
- Digital Airborne telephone provides direct dialing, multiple calls, fax/data, and modem up-link
- Video Monitor with the Air Show 400 network system allows passengers to see moving map of flight information, up to the minute stock quotes, news briefs, business updates & can be interfaced with a laptop for PowerPoint presentations
- DVD Entertainment System for both Video and 10 stack CD Audio (headphones provided at each seat location)
GENERAL
Capacity
- Crew: 2
- Passengers: Up to 8
Engines
- Honeywell TFE731-20-AR
- Thrust: 3,500 pounds (15.56 kN) thrust at takeoff
- Flat-rating: ISA + 16ºC (88ºF)
Avionics
- Honeywell Primus 1000 four-tube EFIS
- Engine Instrument/Crew Advisory System (EICAS)
- Honeywell Primus 660 weather radar
- Dual Primus II nav/comm systems
PERFORMANCE
Range
- Maximum range: 2,102 NM 2,419 SM 3,893 km (IFR Reserves, ISA, with 4 pax/2 crew)
Speed - Mach | kts. | mph | km/h
- High-speed cruise - 0.81 | 464 | 534 | 859
- Typical cruise speed - 0.79 | 457 | 526 | 846
- Long-range cruise speed - 0.75 | 430 | 495 | 796
Airfield Performance
- Balanced field length (SL, ISA, MGTOW): 4,350 ft (1,326 m)
- Landing distance (SL, ISA, MLW): 2,660 ft (811 m)
Ceiling
- Maximum operating altitude: 51,000 ft (15,545 m)
- Climb to cruise altitude of 43,000 ft (13,106 m) after MGTOW departure: 23 min, 6 sec
Noise Level
- EPNdB
- Takeoff: 74.4
- Approach: 93.4
- Sideline: 85.2
DIMENSIONS
External
- Length: 57.6 ft (17.56 m)
- Wingspan: 47.78 ft (14.56 m)
- Wing area: 311.6 ft2 (28.95 m2)(basic)
- Height overall: 14.13 ft (4.31 m)
Internal
- Cabin length: 19.75 ft (6.02 m)(from cockpit divider to end of pressurized compartment)
- Cabin maximum width: 5.12 ft (1.56 m)(centerline)
- Cabin width: 3.1 ft (0.94 m)(floorline)
- Cabin height: 4.92 ft (1.50 m)
- Floor area: 62 ft2 (5.76 m2)(excluding cockpit)
- Total volume: 410 ft3 (11.61 m3)(from cockpit divider to end of pressurized compartment) .
Weights
- A. Maximum ramp weight: 20,750 lb (9,412 kg)
- B. Maximum takeoff weight: 20,500 lb (9,299 kg)
- C. Maximum landing weight: 19,200 lb (8,709 kg)
- D. Maximum zero fuel weight: 16,000 lb (7,257 kg)
- E. Typical basic operating weight: 13,695 lb (6,212 kg)
- F. Maximum fuel weight: 6,062 lb (2,750 kg)
- Maximum payload (D-E): 2,305 lb (1,046 kg)
- Payload - full fuel (A-E-F): 993 lb (450 kg)
- Fuel with maximum payload: 4,750 lb (2,155 kg)