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  2. Glasair GlaStar - Wikipedia

    en.wikipedia.org/wiki/Glasair_GlaStar

    The Glasair GlaStar (sometimes Glastar) is an American amateur-built aircraft that was designed by Tom Hamilton and produced by Stoddard-Hamilton Aircraft and later Glasair Aviation. It was first flown in 1994 and was superseded in production by the Glasair Sportsman 2+2 c. 2005. When it was available the aircraft was supplied as a kit for ...

  3. Glasair Aviation - Wikipedia

    en.wikipedia.org/wiki/Glasair_Aviation

    Tom Hamilton began flight testing the Glasair TD and founded Stoddard-Hamilton Aircraft in 1979. Glasair Aviation was formed in 2001 when Thomas W. Wathen purchased the Glasair assets from bankrupt Stoddard-Hamilton Aircraft, Inc. and signed an agreement with Arlington Aircraft Development, Inc. (AADI) to buy all rights to and assets of the GlaStar model.

  4. Stoddard-Hamilton Aircraft - Wikipedia

    en.wikipedia.org/wiki/Stoddard-Hamilton_Aircraft

    Retractable gear and up-engined models were later introduced, with the Glasair III Turbo capable of speeds in excess of 300 mph (483 km/h), and another model being fitted with a turboprop engine. In the mid-1990s, Glasair introduced the Glastar, a high-wing, short-field capable utility aircraft with two seats. [citation needed]

  5. Glasair Sportsman 2+2 - Wikipedia

    en.wikipedia.org/wiki/Glasair_Sportsman_2+2

    Glasair Sportsman 2+2 Diesel A Thielert Centurion 2.0s powered variant. Carbon Sportsman A variant with the fuselage constructed of carbon fiber rather than fiberglass.The weight savings of carbon fiber are negated by heavier duty cage, wing struts, and wing skins; both variants have the same empty weight, but the carbon variant gross weight is increased by 150 lb. [6]

  6. Stoddard-Hamilton Glasair III - Wikipedia

    en.wikipedia.org/wiki/Stoddard-Hamilton_Glasair_III

    The Glasair III is an all-composite cantilever low-wing monoplane. It is an improved variant of the earlier Glasair II with a retractable landing gear and powered by a 300 hp (224 kW) Lycoming IO-540-K1H5 engine.

  7. Stoddard-Hamilton Glasair II - Wikipedia

    en.wikipedia.org/wiki/Stoddard-Hamilton_Glasair_II

    A development of the earlier Glasair I, the Glasair II features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit accessed via gull-winged doors, fixed or retractable tricycle landing gear or fixed conventional landing gear and a single engine in tractor configuration.