Eclipse 500

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).
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Mission Profile

250
KTAS
Cruise Speed
6
Occupants
1125
nm
Max Range
718
lbs
Wet Payload

Estimated Ownership Costs

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About the Eclipse 500

The Eclipse 500 is a very light jet (VLJ) aircraft originally produced by Eclipse Aviation. It first flew in 2002 with Williams EJ22 engines, which were later replaced by Pratt & Whitney Canada PW610Fs in 2004. The aircraft received provisional FAA type certification in July 2006 and full certification in September of the same year. It has a six-seat capacity, all-metal airframe, and is powered by two turbofan engines in aft fuselage-mounted nacelles. Eclipse Aviation ceased production in 2008 due to lack of funding, but the Eclipse 550 update was announced in 2011 by Eclipse Aerospace, which later merged into One Aviation. The aircraft has undergone various modifications and refurbishment programs, including the Total Eclipse and Eclipse Special Edition programs, to enhance its performance and features.

Technical Specifications

Dimensions

Wingspan
37.3 ft
Length
33.1 ft
Height
11.0 ft

Weights

Max Takeoff Weight
5,950 lbs
Max Landing Weight
5,415 lbs
Useful Load
2,400 lbs
Fuel Capacity
251 gal

Performance

Cruise Speed
250 KTAS
Range
1125 NM
Service Ceiling
41,001 ft
Rate of Climb
3424 fpm

Engines

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