Range
1704 NM
Max Speed
Mach 0.81
Capacity
Up to 4
Avionics
Honeywell
Engines
TFE731-20AR
Origin
United States
Ref ID: learjet-40. Subject to prior sale or removal from market.
About The Learjet 40
The Learjet 40 is a light jet business jet from Bombardier's Learjet family. It is an important part of Bombardier's private aviation history, serving owners, corporate flight departments, charter operators, and special mission users with a blend of speed, cabin utility, and proven systems for its generation.
1,704 Nautical Mile Range
Mission capability suited to short and medium-range executive, owner-flown, and charter missions.
Mach 0.81 Top Speed
High-speed performance for its class and production era.
Learjet Family Heritage
A notable Bombardier model that helped define the Learjet product line.
TFE731-20AR Engines
Twin Honeywell turbofans shape the aircraft's performance and maintenance profile.
Spotlight: 1,704 Nautical Mile Range
Mission capability suited to short and medium-range executive, owner-flown, and charter missions.
Milestones
Program Status
Out of Production
Learjet 40 Specifications
Performance
Max Cruise Speed
457 KTAS
(846 km/h)
Long Range Cruise
430 KTAS
(796 km/h)
Mach Speed
M 0.81
Max Range
1,704 NM
(3,156 km)
Service Ceiling
51,000 FT
(15,545 m)
Climb Rate
4,500 FPM
Takeoff Distance
4,330 FT
(1,320 m)
Landing Distance
2,660 FT
(811 m)
With a maximum range of approximately 1,704 nautical miles and a top operating speed of Mach 0.81, the Learjet 40 is designed for short and medium-range executive, owner-flown, and charter missions. Its 51,000 ft service ceiling, published runway performance, and mature support ecosystem make it a relevant aircraft for buyers evaluating capability, acquisition cost, and mission fit.
Powerplant
Engine Manufacturer
Honeywell
Engine Model
TFE731-20AR
Engine Type
Turbofan
Thrust Per Engine
3,500 LBF
Engine Count
2
Maintenance Plan
On Condition
Noise Stage
Stage 3/4 compliant by configuration
The Learjet 40 is powered by two Honeywell TFE731-20AR turbofan engines, each rated at approximately 3,500 pounds of thrust. This powerplant pairing defines much of the aircraft's climb, cruise, maintenance, and operating-cost profile, especially for legacy operators comparing engine programs and inspection status.
Operating Weights
MTOW (Max Takeoff)
20,500 LB
(9,299 kg)
Max Landing Weight
19,200 LB
(8,709 kg)
Max Zero Fuel Weight
16,000 LB
(7,257 kg)
Max Payload
1,900 LB
(862 kg)
Fuel Capacity
6,062 LB
(2,750 kg)
Operating Empty Weight
14,100 LB
(6,396 kg)
Operating weights dictate the structural limits and mission profile of the aircraft. With an MTOW of 20,500 lbs, the Learjet 40 offers a high payload-to-range ratio, allowing operators to carry a full cabin without sacrificing distance.
Learjet 40 Interior
Cabin Specs
Length
17.7 FT
(5.39 m)
Width
5.1 FT
(1.55 m)
Height
4.9 FT
(1.49 m)
The Learjet 40 cabin provides a compact high-speed cabin focused on efficient private travel. Cabin dimensions are approximately 17.7 ft long, 5.1 ft wide, and 4.9 ft high, with seating for up to 7 passengers depending on layout and about 65 cubic feet of baggage capacity.
Operating Economics
Based on an assumed utilization of 350 flight hours annually.
Variable Costs
Fixed Costs
Annual Budget
$0.91M
Estimated Total Spend
Market Leading Operators
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The Learjet 40 had an estimated new list price of about $8.0M. Current pre-owned values vary significantly by year, total time, engine status, avionics, inspection history, and interior condition.
The Learjet 40 has a maximum range of approximately 1,704 nautical miles under typical published long-range cruise assumptions.
The Learjet 40 can reach a top operating speed of about Mach 0.81, with normal cruise speeds varying by altitude, weight, and mission profile.
Depending on cabin configuration, the Learjet 40 can accommodate up to 7 passengers.