Learjet 40

· Learjet · 2 × Garrett TFE731
Length
16.764 m
Flat Wing Span
14.3256 m
Height
4.2672 m
Flat Wing Area
28.9486 m²
Flat Wing Aspect Ratio
7.3
Max Seating
7
Cruise Speed
859.3273 km/h
Max Mach
0.81 Mach
Max Ceiling
15544.8 m
Number of Engines
2
Aircraft Engine
First Flight
2002-08-31
Entry Into service
2004-01-01
Number Built
133
Maximum Take-Off Weight
9.2306 t (paragliders: kg)
Total Fuel Capacity
3425.798
Maximum Range
3439.164 km

Pictures

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Total Fuel Capacity Maximum Range (km)
Learjet 40 9.2306 3425.798 3439.164

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
HFB 320 Hansa Jet 16.61 14.49 11 Compare
Learjet 55 Garrett TFE731 16.8 13.35 Compare
Learjet 45 Garrett TFE731 17.68 14.58 9 Compare
Northrop Tacit Blue 16.764 14.6304 Compare
Saunders-Roe SR.A/1 15.24 14.0208 Compare
Learjet 70/75 Garrett TFE731 17.7 15.5 1 Compare
All data (27 fields)
Name
Learjet 40
Manufacturer
Learjet
Description
The Learjet 40 (LJ40) is a light business jet produced by Bombardier Aerospace.
ICAO Code
LJ40
First Flight
2002-08-31
Entry Into service
2004-01-01
Production End
2013-01-01
Designer
Learjet
Type
Business jet
Length (m)
16.764
Height (m)
4.2672
Cockpit Crew
2
Max Seating
7
Cruise Speed (km/h)
859.3273
Max Ceiling (m)
15544.8
Capacity Description
7 passengers
Max Mach (Mach)
0.81
National Origin
Azerbaijan
Number Built
133
Powerplant Description
2 × Honeywell TFE731-20AR turbofan engines
Wikipedia Article (URL)
en.wikipedia.org/wiki/Learjet_40
Flat Wing Span (m)
14.3256
Flat Wing Area (m²)
28.9486
Flat Wing Aspect Ratio
7.3
Wake Category
M
Aircraft Engine
Garrett TFE731
Number of Engines
2