Range Map
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Payload vs. Range
Fuel on board
Cargo
nm
Range
Trip Preview
Name a destination in the map header above and this becomes your trip: time en route, what you burn, what it costs, and whether you get there without stopping — at the load you have set.
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We do not have a cruise speed on file for this aircraft, so there is no honest time or cost to give you for this leg.
En route
Fuel burned
Direct cost
Fuel cost
Tanks run dry about past before at this burn.
Mission Profile
- High-Altitude
- Pressurization
- Multi-Engine
- Instrument
Estimated Ownership Costs
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About the Eclipse 500
Type certificated 2006
Overview
The Eclipse 500 is a six-seat twin-turbofan Very Light Jet, type-certificated by the FAA in September 2006 under 14 CFR Part 23 in the Normal category. Built by Eclipse Aviation to be produced at high volume for the personal and air-taxi jet market, it pairs two aft-fuselage Pratt & Whitney Canada PW610F-A turbofans with a pressurized cabin, a T-tail, and retractable tricycle gear. About 260 were delivered between 2006 and 2008 before Eclipse Aviation ran out of money and entered liquidation; the design passed through Eclipse Aerospace and One Aviation, both since defunct, with type support now held by a single specialist, AML Global Eclipse.
For the owner-pilot, the appeal is genuine twin-jet capability at a direct operating cost near $736 per hour: it climbs to 41,000 feet, cruises near 370 knots true, and flies about 1,125 nm. This record covers the original Eclipse 500; the later Eclipse 550, an improved continuation with the more powerful PW615F engines and dual flight-management systems, shares the airframe but is a separate build. The Eclipse 500 earns the buyer who wants real jet speed, altitude, and twin-engine redundancy at the low operating cost that was the type’s whole reason for being, and who will accept a small cabin, a thin parts-and-service network, and the ownership risk of an airframe whose manufacturer no longer exists.
Key Features for GA Buyers
- Low jet operating cost. A direct operating cost near $736 per hour, built on roughly 59 GPH cruise fuel burn and two small turbofans, was the type’s founding promise.
- Flight-levels capability. Certificated to 41,000 feet with RVSM and flight into known icing, the aircraft reaches jet altitudes and smooth air a piston or light turboprop cannot.
- Twin-engine redundancy. Two FADEC-controlled PW610F-A turbofans give an engine-out margin single-engine VLJs and turboprops do not, with a single-engine service ceiling near 25,000 feet.
- Cross-country speed. A 370-knot maximum cruise covers 800 to 1,000 nm legs in under three hours.
Trade-offs
- Orphaned manufacturer. Eclipse Aviation, Eclipse Aerospace, and One Aviation are all gone; parts and type support now rest with a single third party. Component availability and lead times are a real, ongoing ownership risk that pre-purchase diligence must weigh.
- Small cabin and payload. Six seats are nominal; with full fuel the roughly 2,400-lb useful load supports about four occupants and light bags, not a filled cabin.
- Early avionics immaturity. The type was certificated with an incomplete original Avio avionics suite, and functions such as known-icing approval arrived after entry into service; the later Avio NG upgrade, certified in 2007, addressed much of the shortfall. Avionics and modification status vary widely across the used fleet, so two examples can differ sharply in capability.
- Type-specific training and endorsements. Operating the aircraft requires multi-engine, high-altitude, pressurization, and instrument competency plus type-specific training, a step up from a high-performance single.
See Also
- Cessna Citation Mustang – The direct twin-VLJ rival from an established OEM, with the factory support the Eclipse lacks. Compare
- Embraer Phenom 100 – The VLJ that outlasted the Eclipse, with a larger cabin and a supported production line. Compare
- Cirrus Vision SF50 – A modern single-engine personal jet, simpler and better-supported, trading the second engine for current-production backing. Compare
- Cessna Citation M2 – A step up to an entry light jet with a bigger cabin, more range, and a full factory network. Compare
Technical Specifications
Dimensions & Weights
- Height
- 11 ft
- Length
- 33 ft
- Parking area (ft²2)
- 1,802 ft²
- Max Takeoff Weight
- 6,000 lbs
- Max Landing Weight
- 5,600 lbs
- Useful Load
- 2,400 lbs
- Fuel Capacity
- 251 gal
Performance
- Cruise Speed
- Source: manufacturer figure 370 KTAS
- Never-Exceed (VNE)
- Source: FAA Type Certificate Data Sheet 285 KIAS
- Approach Speed
- 91 KIAS
- Stall, Clean (VS1)
- 70 KIAS
- Range
- 1125 NM
- Service Ceiling
- 41,000 ft
- Rate of Climb
- 3424 fpm
Engines
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Sources
Where the figures on this page come from. Eclipse 500 specifications are traced to published references; estimated values are flagged inline next to the figure.
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EASA TCDS EASA.IM.A.171 (Eclipse EA500, Issue 08), Section A.III.10 Air Speeds, the international counterpart to FAA TCDS A00002AC. The EA500 is certificated with VMO/MMO limits rather than a red-line VNE; the catalogue stores VMO as the hero limiting speed (same convention as the Epic E1000 and Piper M600 records). Value in KEAS. www.easa.europa.eu
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Eclipse Aviation published performance (maximum cruise speed, TAS). The catalogue stores maximum cruise TAS as the hero cruise figure (same convention as the Epic E1000 record). A prior catalogue value of 250 kt was corrected to the published 370 KTAS maximum cruise. en.wikipedia.org
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FlyRadius Eclipse 500 specifications www.flyradius.com
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