Learjet 40

Turbofan • twin engine • Low Wing • Retractable gear

Range Visualization

Origin: · click map to move · nm at current load

Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

Endorsements & ratings:
  • High-Altitude
  • Pressurization
  • Multi-Engine
  • Instrument
464
KTAS
Cruise Speed
8
Occupants
1692
nm
Max Range
2237
lbs
Wet Payload

Estimated Ownership Costs

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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

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

Engines

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