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Data from Manufacturer General characteristics Crew: 1 Length: 15 ft 4 in (4.67 m) Wingspan: 19 ft 4 in (5.89 m) Height: 6 ft 5 in (1.96 m) Empty weight: 450 lb (204 kg) Gross weight: 850 lb (386 kg) Fuel capacity: 15 U.S. gallons (57 L; 12 imp gal) Powerplant: 1 × VW Great Plains Aircraft Supply Company Volkswagen air-cooled engine, 60 hp (45 kW) Performance Maximum speed: 126 kn (145 mph ...
It is made from 7075-T6 aluminum tubing, with the control bar and kingpost made from 6061-T6 aluminum. The single-surface wing is covered in Dacron sailcloth. Its 39.0 ft (11.9 m) span wing is cable braced from a single kingpost. The nose angle is 115°, wing area is 330 sq ft (30.7 m 2) and the aspect ratio is 5:1. Pilot hook-in weight range ...
N 1] The Hall Aluminum Aircraft Company submitted the only seaplane design; [3] a single prototype was ordered by the Navy for evaluation on June 30, 1934. Given the designation XPTBH-1, [5] it became the only aircraft to receive three mission-type letters under the U.S. Navy's designation system used between 1922 and 1962. [6] [7] [8]
Two seat, high-wing, conventional landing gear, open cockpit ultralight trainer Rans S-19 Venterra: 2007 11 (November 2010) Two seat, low wing, tricycle landing gear light-sport aircraft Rans S-20 Raven: 2013 1 (January 2014) Two seat, high wing, tricycle or conventional landing gear light-sport bush aircraft Rans S-21 Outbound: 2017 1 (May 2018)
The F1 Rocket is a tandem two-seat low-wing cantilever monoplane built mainly in aluminum. [1] The Rocket has a titanium fixed conventional landing gear with a tailwheel. . Designed to be built with a range of nose-mounted engines between 235 and 350 hp (175 and 224 kW) the prototype has a Lycoming IO-540 with a three-bladed propelle
Pterodactyl production commenced in 1979 and was completed in 1984, when the company was sold to a group of partners under the name "Freedom Fliers" and moved to Rowlett, Texas. The company quickly went out of business, and few aircraft were completed. McCornack was never paid for the sale of the company.
The fuselage was constructed of aluminum angle braces bolted together to form a truss frame. [4] An innovative feature of the BD-4 was the wing structure, which employed a 'panel-rib' constructed in sections, consisting of a rib whose upper edge was extended horizontally to become one section of the wing surface.
The Aero Designs Pulsar is an American two-seat, low wing, ultralight and homebuilt aircraft that was designed by Mark Brown and first produced by Aero Designs of San Antonio, Texas, introduced in 1985. When it was available the Pulsar was supplied as a ready-to-fly aircraft and as a kitplane for amateur construction. [1] [2]