Top speed 467 km/h Length 6.5 m | Wingspan 7.09 m | |
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The Stoddard-Hamilton Glasair III is an American two-seat dual-control monoplane designed and built by Stoddard-Hamilton Aircraft of Arlington, Washington as an addition to the Glasair range of aircraft for amateur construction.
Contents

Design and development

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. It has two seats side-by-side with dual controls, the aircraft can be fitted with wing tip fuel tanks.
Specifications
Data from Jane's All the World's Aircraft 1989-90
General characteristics

Performance



References
Stoddard-Hamilton Glasair III Wikipedia(Text) CC BY-SA