Learjet 45XR

http://www.sinoprivateaviation.com/components/com_gk2_photoslide/images/thumbm/105909l45_1.jpg

http://www.sinoprivateaviation.com/components/com_gk2_photoslide/images/thumbm/633049l45_2.jpg

http://www.sinoprivateaviation.com/components/com_gk2_photoslide/images/thumbm/468556l45_3.jpg

http://www.sinoprivateaviation.com/components/com_gk2_photoslide/images/thumbm/181376l45_4.jpg

Overview

With enhanced engine performance, Bombardier Learjet 45 XR brings you the world with best-in-class efficiency and direct operating costs

Spacious and functional cabin in its class
Carry more, farther and faster
Faster time-to-climb in its category

Technical Specifications

Capacity

Crew: 2

Passengers: Up to 8 + 1

Dimensions

Exterior

Length:

57.6 ft

17.56 m

Wingspan:

47.78 ft

14.56 m

Wing area (basic):

311.6 ft²

28.95 m²

Height overall:

14.13 ft

4.32 m

Interior

Cabin length:
(From cockpit divider to end of pressurized compartment)

19.75 ft

6.02 m

Cabin maximum width: (Centerline)

5.12 ft

1.56 m

Cabin width: (Floorline)

3.2 ft

0.98 m

Cabin height:

4.92 ft

1.50 m

Floor area: (Excluding cockpit)

66 ft²

6.13 m²

Cabin volume:
(From cockpit divider to end of pressurized compartment)

410 ft³

11.61 m³

Weights

A. Maximum ramp weight:

21,750 lb

9,866 kg

B. Maximum takeoff weight

21,500 lb

9,752 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:

14,125 lb

6,407 kg

F. Maximum fuel weight:

6,062 lb

2,750 kg

Maximum payload (D-E):

1,875 lb

850 kg

Payload – full fuel (A-E-F):

1,563 lb

709 kg

Fuel with maximum payload (A-D):

5,750 lb

2,608 kg

Performance

Range

Maximum range:

1,971 NM

2,268 SM

3,650 km

(NBAA IFR100 NM reserves, ISA, with 4 pax/2 crew)

Speed	Mach	kt	mph	km/h
High-speed	0.81	465	535	861
Typical cruise speed	0.81	465	535	861
Long-range cruise speed	0.75	432	497	800

Range Map - Beijing Shanghai Hong Kong

Download Factsheet

Takeoff distance

(SL, ISA, MTOW):

5,040 ft

1,536 m

Landing distance

(SL, ISA, MLW):

2,660 ft

811 m

Operating Altitude

Maximum operating altitude:

51,000 ft

15,545 m

Climb to cruise altitude of 43,000 ft (13,106 m) after MTOW departure:

24 min, 36 sec

Noise Level(EPNdB)	Fly over (thrust cutback)	Approach	Lateral
	75.5	93.4	85.1

Engines

Honeywell TFE731-20-BR

Thrust: 3,500 pounds (15.56 kN)

Flat-rating: ISA + 25°C (104°F)

Avionics

Honeywell Primus 1000 four-tube EFIS

Engine Instrument/Crew Advisory System (EICAS)

Honeywell Primus 660 weather radar

Dual Primus II nav/comm systems

Traffic Collision Avoidance System (TCAS 2000)

Enhanced Ground Proximity Warning System (EGPWS) with Wind Shear Alert

Emergency Locator Transmitter (ELT)

Flight Management System (FMS)