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Data from Ultralight News, Pilot Mix. General characteristics Crew: one Capacity: one (ultralight configuration) Length: 17 ft 3 in (5.26 m) Wingspan: 27 ft 5 in (8.36 m) Height: 5 ft 0 in (1.52 m) varies by main landing gear wheel diameter Wing area: 123 sq ft (11.4 m 2) Empty weight: 254 lb (115 kg) Gross weight: 540 lb (245 kg) Fuel capacity: 5 US gallons (19 litres) Powerplant: 1 × Rotax ...
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]
Bartoe applied for certification on 17 February 1977, [1] however, it was not until July 1981 that the first of the two aircraft intended for the certification program (Bartoe's own aircraft, cn/1, N25PB) flew. [1] Plans remained on sale until 1986, [8] [15] after which time Bartoe continued to sell wing and rib kits to existing plan owners. [11]
Data from Purdy, Cliche & InterPlane General characteristics Crew: one Capacity: one passenger Length: 20 ft 0 in (6.10 m) Wingspan: 34 ft 5 in (10.49 m) Wing area: 163.6 sq ft (15.20 m 2) Empty weight: 490 lb (222 kg) Gross weight: 1,000 lb (454 kg) Fuel capacity: 10 US gallons (38 litres) Powerplant: 1 × Rotax 582 twin cylinder two-stroke aircraft engine, 64 hp (48 kW) Performance Maximum ...
The all-metal aircraft is made from sheet aluminum. Its 18.40 ft (5.6 m) span wing lacks flaps and has a wing area of 63.00 sq ft (5.853 m 2). The cabin width is 22 in (56 cm). The acceptable power range is 70 to 100 hp (52 to 75 kW) and the standard powerplant is the 70 hp (52 kW) Volkswagen air-cooled engine.
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]
They are commonly used in the fuselage, wing, and supporting structure of aircraft because they are resistant to corrosion and have a good strength to weight ratio. [17] Aluminum that is used in aircraft is commonly mixed with copper, lithium, magnesium, manganese, silicon, silver, and zinc to form alloys. [2]
The Angel Aircraft Corporation Model 44 Angel is a twin-engine STOL utility aircraft produced in the United States since the mid-1990s. Designed by Carl Mortenson and The King's Engineering Fellowship to be well-suited for missionary work from remote locations around the world, it is a low-wing cantilever monoplane with a retractable tricycle undercarriage and eight seats.
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