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The engines were replaced by Pratt & Whitney Canada PW610Fs in 2004 and Eclipse Aviation won the Collier Trophy in February 2006 for the design. A provisional FAA type certification was received on 27 July 2006 and the first delivery occurred on 31 December 2006. The six-seat aircraft has an all-metal airframe with a T-tail and straight wings.
Diamond formed its subsidiary, Austro Engine, to produce the engine. [4] The engine is a single rotor four-stroke, air and liquid-cooled, 294 cc (17.9 cu in) gasoline Wankel engine design, with a mechanical gearbox reduction drive employing a helical gear set with a reduction ratio of 3.225:1. Cooling is predominantly liquid, with forced air ...
The engine could be either Eurojet EJ200 or General Electric F414 with thrust of 89 to 98 kN (20,000 to 22,000 lbf), roughly 12–25% higher than the F404's thrust; [22] [23] and are offered to prospective customers for the T-50. The radar of the FA-50 has a range two-thirds greater than the TA-50's radar. [24]
This is a cross-country airplane with many exclusive features including carbon fiber construction, pressurized cabin, high strutless wing, and seating for six. The EA-500 was introduced as an alternative version of the EA-400 with the piston engine replaced by a Rolls-Royce Model 250 -B17F/2 turboprop yielding 450 horsepower (340 kW), weighing ...
Hush kits can adversely affect the range and performance of the aircraft they are fitted to because of the extra weight. It also reduces engine performance and aerodynamic efficiency. For example, the hush kit fitted to the Gulfstream II adds 106 kilograms (234 lb) to the total airplane weight of 65,500 lb (29,700 kg), causing around a 1.6% ...
The standard engine used is the 310 hp (231 kW) Continental IO-550 but engines as small as the 200 hp (149 kW) Lycoming IO-360 four-stroke powerplant can be fitted. [3] [4] [5] Four Lancair Legacy aircraft have won the Grand Champion Kit Built award at the EAA AirVenture airshow, in 2012, 2013, 2014, and 2016. [6] [7] [8] [9]
The aircraft's recommended engine power range is 210 to 310 hp (157 to 231 kW) and standard engines used include the 310 hp (231 kW) Continental IO-550 four-stroke powerplant. Construction time from the supplied kit is estimated to be 2000 hours. [1] [4]
The LSA features a strut-braced high-wing, a tandem enclosed cockpit accessed by doors, fixed conventional landing gear and a single engine in tractor configuration. The cockpit is 31 in (79 cm) wide. [1] [4] In 2015 a quick-build kit was introduced at the U.S Sport Aviation Expo. [5]
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