Range
1767 NM
Max Speed
Mach 0.82
Capacity
Up to 4
Avionics
General Electric
Engines
CJ610-8A
Origin
United States
Ref ID: learjet-25. Subject to prior sale or removal from market.
About The Learjet 25
The Learjet 25 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.
1,767 Nautical Mile Range
Mission capability suited to short and medium-range executive, owner-flown, and charter missions.
Mach 0.82 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.
CJ610-8A Engines
Twin General Electric turbofans shape the aircraft's performance and maintenance profile.
Spotlight: 1,767 Nautical Mile Range
Mission capability suited to short and medium-range executive, owner-flown, and charter missions.
Milestones
Program Status
Out of Production
Learjet 25 Specifications
Performance
Max Cruise Speed
464 KTAS
(859 km/h)
Long Range Cruise
430 KTAS
(796 km/h)
Mach Speed
M 0.82
Max Range
1,767 NM
(3,272 km)
Service Ceiling
51,000 FT
(15,545 m)
Climb Rate
6,000 FPM
Takeoff Distance
3,850 FT
(1,173 m)
Landing Distance
2,950 FT
(899 m)
With a maximum range of approximately 1,767 nautical miles and a top operating speed of Mach 0.82, the Learjet 25 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
General Electric
Engine Model
CJ610-8A
Engine Type
Turbofan
Thrust Per Engine
2,950 LBF
Engine Count
2
Maintenance Plan
On Condition
Noise Stage
Stage 3/4 compliant by configuration
The Learjet 25 is powered by two General Electric CJ610-8A turbofan engines, each rated at approximately 2,950 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)
15,000 LB
(6,804 kg)
Max Landing Weight
13,000 LB
(5,897 kg)
Max Zero Fuel Weight
11,000 LB
(4,990 kg)
Max Payload
1,800 LB
(816 kg)
Fuel Capacity
4,810 LB
(2,182 kg)
Operating Empty Weight
8,400 LB
(3,810 kg)
Operating weights dictate the structural limits and mission profile of the aircraft. With an MTOW of 15,000 lbs, the Learjet 25 offers a high payload-to-range ratio, allowing operators to carry a full cabin without sacrificing distance.
Learjet 25 Interior
Cabin Specs
Length
12.9 FT
(3.93 m)
Width
4.9 FT
(1.49 m)
Height
4.3 FT
(1.31 m)
The Learjet 25 cabin provides a compact high-speed cabin focused on efficient private travel. Cabin dimensions are approximately 12.9 ft long, 4.9 ft wide, and 4.3 ft high, with seating for up to 8 passengers depending on layout and about 40 cubic feet of baggage capacity.
Operating Economics
Based on an assumed utilization of 350 flight hours annually.
Variable Costs
Fixed Costs
Annual Budget
$0.72M
Estimated Total Spend
Market Leading Operators
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The Learjet 25 had an estimated new list price of about $1.3M. Current pre-owned values vary significantly by year, total time, engine status, avionics, inspection history, and interior condition.
The Learjet 25 has a maximum range of approximately 1,767 nautical miles under typical published long-range cruise assumptions.
The Learjet 25 can reach a top operating speed of about Mach 0.82, with normal cruise speeds varying by altitude, weight, and mission profile.
Depending on cabin configuration, the Learjet 25 can accommodate up to 8 passengers.