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Single seat helicopters are helicopters have one place. A commonly known type of the helicopter that must be single seat, is the FAA Ultralight Helicopter, though single place helicopters existed before this classification (See Ultralight aircraft (United States))
List of single seat helicopters is a list of helicopters with one seat. They may or may not be ultralight aircraft. Some single seat helicopters are evtols. [1] Adams-Wilson Hobbycopter; Airbus A³ Vahana (eVTOL) American Helicopter XH-26 Jet Jeep; Baumgärtl Heliofly III; Chrysler VZ-6; Curtiss-Wright VZ-7; De Lackner HZ-1 Aerocycle; Eagle ...
Huntair Pathfinder Mark 1 ultralight. Ultralight aviation (called microlight aviation in some countries) is the flying of lightweight, 1- or 2-seat fixed-wing aircraft. Some countries differentiate between weight-shift control and conventional three-axis control aircraft with ailerons, elevator and rudder, calling the former "microlight" and the latter "ultralight".
First flown in 1987, the original Sparrow Ultralight is a single seater designed as an FAR 103 Ultralight Vehicles compliant aircraft with an empty weight within that category's 254 lb (115 kg) empty weight limit, when equipped with a light enough engine. The Sparrow can also be built in the US homebuilt and light-sport aircraft categories.
The aircraft has a standard empty weight of 70 kg (154 lb). It features two contra-rotating main rotors, a single-seat open cockpit without a windshield, four-wheeled landing gear and four twin-cylinder, air-cooled, two-stroke , 10 hp (7 kW) GEN 125-F engines to provide operational redundancy since the aircraft cannot autorotate in the event of ...
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Single seat ultralight aircraft with aerobatic capabilities, first flown in 1982. Standard engine is the 40 hp (30 kW) Rotax 447, with the 50 hp (37 kW) Rotax 503 or 64 hp (48 kW) Rotax 582 as options. In the USA the aircraft could be completed as a FAR Part 103 ultralight vehicle or as an Experimental amateur-built aircraft.
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