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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 ...
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 ...
Plans remained on sale until 1986, [8] [15] after which time Bartoe continued to sell wing and rib kits to existing plan owners. [11] Plans were available for purchase again, in October 2004. [16] Pete Bartoe's personal aircraft (cn/1, N25PB) is currently on display at the Wings Over the Rockies Air & Space Museum in Denver, Colorado.
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 ...
Data from Kitplanes, Purdy and RagWing General characteristics Crew: one Length: 16 ft 0 in (4.88 m) Wingspan: 18 ft 0 in (5.49 m) Height: 5 ft 6 in (1.68 m) Wing area: 120 sq ft (11 m 2) Empty weight: 225 lb (102 kg) Gross weight: 525 lb (238 kg) Fuel capacity: 5 US gallons (19 litres) Powerplant: 1 × 2si 460 twin cylinder two stroke aircraft engine, 35 hp (26 kW) Propellers: 2-bladed wooden ...
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]
The Elite features a strut-braced high-wing, three seats, tricycle landing gear and a single engine in tractor configuration. [1] [2] [5] [6] The aircraft is made from aluminum sheet. Its 30.3 ft (9.2 m) span wing is supported by single lift struts. The occupants are accommodated in an enclosed cabin of 44 in (111.8 cm) width, with doors for ...