Ad
related to: aviat husky a1 b performance
Search results
Results From The WOW.Com Content Network
Data from Aviat website General characteristics Crew: one Capacity: one passenger Length: 22 ft 7 in (6.88 m) Wingspan: 35 ft 6 in (10.82 m) Wing area: 183 sq ft (17.0 m 2) Empty weight: 1,275 lb (578 kg) on wheels Gross weight: 2,200 lb (998 kg) on wheels and floats Fuel capacity: 50 US gallons (190 litres) Powerplant: 1 × Lycoming O-360-A1P four cylinder, four stroke piston aircraft engine ...
The Lycoming O-360 is a family of four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engines.Engines in the O-360 series produce between 145 and 225 hp (110 and 170 kW), with the basic O-360 producing 180 hp (130 kW).
[4] [5] The company then designed and manufactured the Christen Husky A-1 utility aircraft. In 1990, the company was the subject of a lawsuit claiming that the design of their aircraft was responsible for the death of a pilot. [6] Christen Industries was, in turn, bought by Aviat Aircraft, Inc. in 1991, who continued both product lines. [7] [8]
Albastar A1, Slovenian glider; Andrews A1, an unsuccessful New Zealand agricultural aircraft; Aviat A1 Husky, a 1987 American two seat, high wing, utility light aircraft; CallAir A-1, a version of the 1940 American CallAir Model A utility aircraft; Curtiss A-1, a 1911 American aircraft
Some AA-1s have had their original engines replaced with larger 150 or 160 hp engines that further increase performance. Other popular modifications include the addition of a dorsal strake on earlier model AA-1s to improve yaw stability or the addition of a transparent red rudder cap to fair the flashing beacon for reduced drag.
Christen Eagle II/Aviat Eagle II (1977) Culp Special; Curtiss JN-4 (1915) Curtiss F7C Seahawk (1927) Curtiss Hawk II (1932) Curtiss Gulfhawk (1923) D'Apuzzo Senior Aero Sport (Homebuilt - 1962) Franklin Demon-1 (Homebuilt) Freiberger Ron's 1 (Homebuilt - 1971) Giles G-200 (Homebuilt) Giles G-202 (Homebuilt) Great Lakes Sport Trainer (1929 ...
160 hp (119 kW) at 2700 rpm, Minimum fuel grade 91/96 avgas, compression ratio 8.50:1. Same as the D2G except with a O-320-B sump and intake pipes and with provisions for AC type fuel pump. [2] O-320-D2J
This category is for aircraft designed, manufactured or marketed by Aviat. Pages in category "Aviat aircraft" The following 3 pages are in this category, out of 3 total.