Bombardier Learjet 55

Turbofan • twin engine • Low Wing • Retractable gear

Range Visualization

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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
420
KTAS
Cruise Speed
10
Occupants
2165
nm
Max Range
2157
lbs
Wet Payload

Estimated Ownership Costs

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About the Bombardier Learjet 55

Overview

The Bombardier 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

Wingspan
43.8 ft
Length
55.1 ft
Height
14.7 ft
Parking area (ft2)
3233.38 ft2

Weights

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
Max Structural Cruise (Vno)
461 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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