Range Map

Origin:

nm at current load

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Payload vs. Range

Configure weights

Default: 190 lbs

Default: 30 lbs

Occupants
lb + lbs / pax

gal

Fuel on board

lbs

Extra weight

nm

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.
Extra weight is the additional payload available with your selected passengers.

Mission Profile

Used market Only available used
420
KTAS
Cruise Speed
2,165
nm
Max Range
51,000
ft
Service Ceiling
10
Occupants
2157
lbs
Wet Payload
Endorsements & ratings:
  • High-Altitude
  • Pressurization
  • Multi-Engine
  • Instrument

Estimated Ownership Costs

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About the Learjet 55

Type certificated 1981 Source: FAA Type Certificate Data Sheet

Overview

The Learjet 55, branded the “Longhorn” for its distinctive winglets, is the first stand-up-cabin Learjet and a deliberate Gates Learjet attempt to compete with the larger Cessna Citation III and Hawker 800 brackets. First flown in 1979 and certificated in 1981, the Model 55 paired a new larger fuselage with the supercritical “Longhorn” wing originally developed for the abandoned Learjet 28/29 program. 147 airframes were built across the 55, 55B, and 55C variants through 1986; the line was succeeded several years later by the redesigned Learjet 60, which shared the cabin but moved to PW305A turbofans. All 55-series variants used twin Honeywell TFE731-3A turbofans rated at 3,700 lbf each.

For the GA buyer, the Learjet 55 sits in a transition bracket: it carries the Lear performance pedigree but adds the cabin volume that the rest of the family lacks. Compared with the Learjet 35/36 it gives up some cruise speed and trades up for stand-up cabin height, longer transcontinental range, and the supercritical wing’s improved low-speed manners. Compared with the Cessna Citation V, it offers a higher ceiling and a more spirited handling character but lower fuel economy and a longer required runway. The natural step-up is the Learjet 60, which inherits the cabin and adds modern avionics, FADEC, and meaningfully better range.

Key Features for GA Buyers

  • Stand-up cabin. Unlike previous Learjets, the Model 55 features a cabin height of roughly 5‘7”, allowing for much greater passenger comfort during longer flights.
  • High-altitude performance. Certified for flights up to 51,000 ft, allowing it to climb above most weather and commercial traffic for smoother, more direct routing.
  • Range. Capable of transcontinental flights (approximately 2,000+ nm), making it a versatile option for business travel.

Trade-offs

  • Runway performance. Requires a relatively long runway for takeoff (5,600+ ft at sea level), which may limit access to smaller general aviation airports compared to lighter jets or turboprops.
  • Operating costs. As an older jet with twin turbofan engines, fuel burn and maintenance costs are higher than modern light jets.

See Also

Technical Specifications

Dimensions & Weights

Wingspan 43.8 ft
Height
14.7 ft
Length
55.1 ft
Parking area (ft2)
3233.38 ft2
Max Takeoff Weight
21,500 lbs
Max Landing Weight
18,000 lbs
Useful Load
8,857 lbs
Fuel Capacity
1000 gal

Performance

Cruise Speed
420 KTAS
Never-Exceed (VNE)
Source: FAA Type Certificate Data Sheet 350 KIAS
Max Structural Cruise (VNO)
Source: FAA Type Certificate Data Sheet 300 KIAS
Approach Speed
143 KIAS
Stall, Clean (VS1)
110 KIAS
Range
2165 NM
Service Ceiling
51,000 ft
Rate of Climb
1240 - 4180 fpm
Takeoff over 50 ft obstacle
5,600 ft
Landing ground roll
2,800 ft

Engines

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Sources

Where the figures on this page come from. Learjet 55 specifications are traced to published references; estimated values are flagged inline next to the figure.

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See how the Learjet 55 stacks up against similar aircraft

External Media