Eclipse 500 Jet Performance
  Imperial Metric
Takeoff Distance
Sea level, ISA to 50 ft @ MGTOW
2,155 ft 657 m
Landing Distance
Sea level, ISA @ 4,600-lb landing weight
2,040 ft 622 m
Rate of Climb - 2 engines 2,990 ft/min 911 m/min
Rate of Climb - 1 engine 888 ft/min 271 m/min
Time to Climb - 35,000 ft

19 min

 
Takeoff at 5,000 ft at ISA +15°C
(1,524 m)
3,350 ft 1,021 m
Single Engine Takeoff Climb at 5,000 ft at ISA +15°C (1,524 m) 293 ft/min 89 m/min
Single Engine Service Ceiling 25,000 ft 7,620 m
Cruise Speed 375 kt 694 km/hr
Vso 67 kt 124 km/hr
Vmo/Mmo 285 kt /
0.64 Mach
528 km/hr /
0.64 Mach
Max. Altitude 41,000 ft 12,497 m
Range, 4 occupants
NBAA IFR, 100 nm alternate, 200-lb Pilot, three 170-lb passengers
1,280 nm 2,371 km
Range, 4 occupants
IFR 45-minute reserve
1,395 nm 2,584 km

Preliminary Trip Profile Data

The Eclipse 500 promises to be efficient for a wide range of missions. Here are some typical trips. Trip profiles are based on preliminary engine performance data provided by Pratt & Whitney Canada. These profiles are subject to revision following flight testing. All trips are with NBAA IFR reserves, 100 nm alternate.

Long Range
1248 nm
Phoenix to Chicago

Medium Range
566 nm
Dallas to Denver

Short Range
198 nm
Washington DC to New York

Trip Planning Assumptions

Range Capability

The Eclipse 500 has excellent range as illustrated on the maps below. The following range calculations assume 1 pilot, 3 passengers, high-speed cruise, 85% annual probability winds, ISA, and 100 nm NBAA IFR reserve.

Performance based on preliminary engine data supplied by Pratt & Whitney Canada. Final performance data subject to revision following flight testing. Pilot weight is 200 lb, passenger weight is 170 lb each.

Boston

 

Miami

 

Chicago

 

Dallas

 

Los Angeles

 

Seattle


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Last modified February 21, 2005
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