The Glasair I is a kit airplane that was first introduced in 1979 by Glasair Aviation. It is a high-performance, single-engine, two-seat general aviation aircraft that is designed to be built by amateur builders.
The Glasair I is made primarily from composite materials, which makes it lightweight and strong. It has a wingspan of 23 feet and a length of 19.5 feet. The airplane can reach a maximum speed of 250 mph and has a range of approximately 1,000 miles.
The airplane is powered by a variety of engines including Lycoming O-235, O-320, and IO-360, as well as Continental IO-240 and IO-360 engines. It has a maximum takeoff weight of 1,500 lbs and can carry up to 31 gallons of fuel.
The Glasair I has undergone several design changes over the years, with many aftermarket modifications available to enhance its performance and appearance. It remains a popular choice among amateur builders for its affordability, ease of construction, and impressive flight characteristics.
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