Bombardier Learjet 60

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
436
KTAS
Cruise Speed
9
Occupants
2398
nm
Max Range
908
lbs
Wet Payload

Estimated Ownership Costs

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About the Bombardier Learjet 60

Overview

The Bombardier Learjet 60, with the later 60XR designation covering the production run from 2007 onward, is a mid-size business jet inheriting the stand-up cabin of the Learjet 55 but moving to twin Pratt & Whitney Canada PW305A turbofans, FADEC engine control, and a full Rockwell Collins Pro Line glass-cockpit suite. First flown in 1990 and certificated in 1993, the Model 60 corrected the 55’s primary criticisms (the older TFE731 engines, mechanical thrust management, and analog instrumentation), while keeping the cabin volume and 51,000-foot ceiling that made the 55 the first stand-up Learjet. 318 standard 60s were built through 2007; the 60XR variant ran from 2007 to 2013 with cabin and avionics upgrades.

For the GA buyer, the Learjet 60 sits squarely in the mid-size cabin bracket alongside the Cessna Citation V/Ultra/Encore, Cessna Excel/XLS, and Hawker 800XP. It out-climbs and out-ceilings most direct competitors, with a typical climb to FL410 in 18 minutes and a 51,000-foot certified ceiling, and offers approximately 2,400 nm in optimum conditions. The trade-off is runway: the Lear 60 wants 5,000-plus feet at sea-level MTOW, more than the Excel and the Encore. PW305A engines, when enrolled in Pratt & Whitney’s ESP program, run on-condition; otherwise published TBO is 5,000 hours.

Key Features for GA Buyers

  • High-altitude performance. Certified to 51,000 ft with a typical climb to FL410 in 18 minutes, well above most weather, traffic, and competing midsize jets.
  • PW305A turbofans. 4,600 lbf each, FADEC-controlled, hot-and-high-friendly. ESP enrollment converts maintenance to on-condition.
  • Stand-up cabin. Roughly 5‘7” cabin height carried over from the Learjet 55, with a full club-four-plus-aft-galley layout.
  • Glass cockpit on the 60XR. Rockwell Collins Pro Line 21 in 60XR; Pro Line 4 in earlier 60s. Both are well-supported, single-pilot-capable suites.

Trade-offs

  • Runway demand. Balanced field length around 5,360 ft at sea level limits access to shorter runways relative to the Cessna Excel/XLS and similar lighter-midsize jets.
  • Operating cost. Approximately $3,200/hr DOC at 300 hours/year typical utilization, with around 235 GPH cruise fuel burn. Heavier per hour than the mid-light bracket but typical for the class.
  • Older airframes. Standard 60s built 1993 to 2007 may show more corrosion and fatigue exposure than the 60XR run; pre-buy diligence on landing-gear and brake-line wear is the typical inspector emphasis.

See Also

Technical Specifications

Dimensions

Wingspan
43.75 ft
Length
58.67 ft
Height
14.58 ft
Parking area (ft2)
3422.26 ft2

Weights

Max Takeoff Weight
23,500 lbs
Max Landing Weight
19,500 lbs
Useful Load
8,848 lbs
Fuel Capacity
1185 gal

Performance

Cruise Speed
436 KTAS
Never-Exceed (Vne)
492 KIAS
Approach Speed
125 KIAS
Stall, Clean (Vs1)
96 KIAS
Range
2398 NM
Service Ceiling
51,000 ft
Rate of Climb
4500 fpm
Takeoff over 50 ft obstacle
5,450 ft
Landing ground roll
3,009 ft

Engines

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