Learjet 40
Turbofan • twin engine • Low Wing • Retractable gear
Range Visualization
Origin: · click map to move · nm at current load
Payload vs. Range
Customize assumptions
Default: 190 lbs (FAA standard)
Default: 30 lbs
Mission Profile
- High-Altitude
- Pressurization
- Multi-Engine
- Instrument
About the Learjet 40
Overview
The Learjet 40 entered service in 2004 as a successor to the Learjet 31A and a shorter, lighter alternative to the Learjet 45. Derived directly from the Model 45, it shares the same cross-section and systems but features a fuselage shortened by approximately two feet (removing two seats) and reduced fuel capacity. The standard Lear 40 is powered by Honeywell TFE731-20AR engines rated 3,500 lbf each, with single-channel DEEC and Honeywell MSP coverage as the industry-standard maintenance program.
Designed to outperform the Citation Bravo and Encore in speed and cabin volume, the Lear 40 retains the family’s classic high-altitude profile. Mach 0.81 cruise and a 51,000-foot service ceiling let it climb above most commercial traffic and weather, while the FAR Part 25 transport-category certification basis brings redundant systems not always present at this weight class.
Key Features for GA Buyers
- Class-leading altitude. Service ceiling of 51,000 ft and Mach 0.81 cruise let the Lear 40 fly above most commercial traffic and weather.
- Cabin comfort. The flat-floor cabin with no spar intrusion offers a cross-section larger than many light-jet competitors, putting mid-size comfort in the light-jet bracket.
- Part 25 safety. Built to FAR Part 25 transport-category standards, including redundant systems not always found at this weight class.
Trade-offs
- Range vs. payload. While capable of approximately 1,700 nm, filling the seats significantly reduces range. The Lear 40 carries about 100 gallons less fuel than the Lear 45.
- Climb performance. Initial climb rate of approximately 2,800 fpm is modest compared to the legacy Learjet 35 and 20-series figures, primarily due to the heavier, robust airframe.
See Also
- Bombardier Learjet 45 – Direct platform predecessor; the Lear 40 is a fuselage-shortened Lear 45. Compare
- Bombardier Learjet 31 – Prior-generation light Learjet on the typical step-up path. Compare
- Cessna Citation CJ4 – Closest direct competitor in the upper-light-jet bracket on speed, range, and payload. Compare
- Cessna Citation V / Ultra / Encore – Mid-light Citation cross-shopped on cabin and operating cost. Compare
- Hawker 800XP – Older mid-size cousin frequently cross-shopped at the upper end of the light-jet budget. Compare
Technical Specifications
Dimensions
- Wingspan
- 47.8 ft
- Length
- 55.5 ft
- Height
- 14.1 ft
- Parking area (ft2)
- 3496.9 ft2
Weights
- Max Takeoff Weight
- 20,350 lbs
- Max Landing Weight
- 19,200 lbs
- Useful Load
- 7,610 lbs
- Fuel Capacity
- 802 gal
Performance
- Cruise Speed
- 464 KTAS
- Never-Exceed (Vne)
- 330 KIAS
- Approach Speed
- 123 KIAS
- Stall, Clean (Vs1)
- 119 KIAS
- Range
- 1692 NM
- Service Ceiling
- 51,000 ft
- Rate of Climb
- 710 - 2820 fpm
- Takeoff over 50 ft obstacle
- 4,330 ft
- Landing ground roll
- 2,324 ft
Similar to the Learjet 40
Bombardier Learjet 35/36
Bombardier Learjet 45
Learjet 70
Learjet 75
Cessna Citation V/Ultra/Encore
Gulfstream G150
Learjet 24
Cessna Citation CJ2
Bombardier Learjet 23
Cessna Citation CJ3
Bombardier Learjet 31
Cessna 500/Citation I
Cessna Citation II/Bravo
See how the Learjet 40 stacks up against similar aircraft