Learjet 40XR

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Overview

Bombardier Learjet 40 XR is a leader in its category and elevates performance to new heights

Best-in-class and high speed cruise, rockets to 51,000 ft
Fully fueled it flies 7 passengers to their destinations faster than any competing jet
The Learjet 40 XR cabin is 20 percent larger than any other light business jet

Technical Specifications

Capacity

Crew: 2

Passengers: Up to 6 + 1

Dimensions

Exterior

Length:

55.56 ft

16.93 m

Wingspan:

47.78 ft

14.56 m

Wing area (basic):

311.6 ft²

28.95 m²

Height overall:

14.13 ft

4.31 m

Interior

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

17.67 ft

5.39 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)

55.7 ft²

5.17 m²

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

363 ft³

10.28 m³

Weights

A. Maximum ramp weight:

21,250 lb

9,639 kg

B. Maximum takeoff weight:

21,000 lb

9,525 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:

13,949 lb

6,327 kg

F. Maximum fuel weight:

6,062 lb

2,750 kg

Maximum payload (D-E):

2,051 lb

930 kg

Payload – full fuel (A-E-F):

1,239 lb

562 kg

Fuel with maximum payload (A-D):

5,250 lb

2,381 kg

Performance

Range

Maximum range:

1,991 NM

2,291 SM

3,687 km

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

Speed	Mach	kt	mph	km/h
High-speed cruise	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):

4,680 ft

1,426 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:

23 min, 12 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) thrust at takeoff

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)