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  2. 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. It has two seats side-by-side with dual controls. The aircraft can be fitted with wing tip fuel tanks.

  3. Team Mini-Max Hi-MAX - Wikipedia

    en.wikipedia.org/wiki/Team_Mini-Max_Hi-MAX

    The company claims that a builder can complete the aircraft in 350–400 hours from the kit. [5] [9] The aircraft was originally intended to meet the requirements of the US FAR 103 Ultralight Vehicles category, including that category's maximum 254 lb (115 kg) empty weight. It was only able to achieve that low empty weight with the 28 hp (21 kW ...

  4. Mini-MAX - Wikipedia

    en.wikipedia.org/wiki/Mini-MAX

    As this is a US aircraft the name is pronounced "Zee-Max". [1] [3] [4] 1300Z Z-MAX Single seat, enclosed cockpit, mid-wing aircraft with the 45 hp (34 kW) Zenoah G-50 engine. First flight 1990, out of production. Manufacturer claimed construction time 400 hours. 231 completed and flown by 2001. As this is a US aircraft the name is pronounced ...

  5. Rihn DR-107 One Design - Wikipedia

    en.wikipedia.org/wiki/Rihn_DR-107_One_Design

    The aircraft is supplied by Aircraft Spruce & Specialty of Corona, California in the form of plans and a materials kit for amateur construction. [1] The DR-107 was designed as a low-cost one design aircraft for competition and sport basic to advanced aerobatics, including International Aerobatic Club Class One competitions.

  6. Team Mini-Max AeroMax - Wikipedia

    en.wikipedia.org/wiki/Team_Mini-Max_AeroMax

    The aircraft's recommended engine the 50 hp (37 kW) Hirth F-23 two-stroke powerplant. Tricycle landing gear, tundra tires and floats are under development. Construction time from the supplied kit is estimated as 200–300 hours. [1] [2] A tandem two seat model is also under development by the company. [1]

  7. Phantom X1 - Wikipedia

    en.wikipedia.org/wiki/Phantom_X1

    Data from Kitplanes General characteristics Crew: one Length: 16 ft 8 in (5.08 m) Wingspan: 28 ft 6 in (8.69 m) Height: 8 ft 2 in (2.49 m) Wing area: 142 sq ft (13.2 m 2) Empty weight: 250 lb (113 kg) Gross weight: 510 lb (231 kg) Fuel capacity: 5 US Gallons (19 litres) Powerplant: 1 × Rotax 447 twin-cylinder, single-ignition, two-stroke aircraft engine, 40 hp (30 kW) Performance Maximum ...

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  9. Glasair Aviation - Wikipedia

    en.wikipedia.org/wiki/Glasair_Aviation

    Aircraft built by Stoddard-Hamilton Aircraft and Glasair Aviation Model name First flight Number built Type Glasair I: 1979 807 [7] Low-wing, two seat kit aircraft Glasair II: 1989 1200 Low-wing, two seat kit aircraft Glasair III: 1986 500 Low-wing, two seat kit aircraft GlaStar: 1994 300 High-wing, two seat kit aircraft Sportsman 2+2: 2003 400

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