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The single seater was introduced in 1998 and retains the configuration and many features of the two seater, but with a revised, narrower fuselage. The aircraft was intended to meet the requirements of the US FAR 103 Ultralight Vehicles category, including that category's maximum 254 lb (115 kg) empty weight.
Free Bird Innovations, Inc. is an American aircraft manufacturer based in Detroit Lakes, Minnesota and formed in about 2003. The company specializes in the design and manufacture of ultralight aircraft in the form of plans and kits for amateur construction and ready-to-fly aircraft in the US FAR 103 Ultralight Vehicles category.
Data from Cliche and L'il Hustler General characteristics Crew: one Capacity: one passenger Length: 20 ft 6 in (6.25 m) Wingspan: 33 ft 6 in (10.21 m) Wing area: 172 sq ft (16.0 m 2) Empty weight: 500 lb (227 kg) Gross weight: 1,200 lb (544 kg) in the Canadian basic ultralight category, 1500 lbs in the amateur-built category. Fuel capacity: 10 US gallons (38 litres) Powerplant: 1 × Rotax 582 ...
Data from Cliche and SlipStream General characteristics Crew: one Capacity: one passenger Length: 19 ft 4 in (5.89 m) Wingspan: 30 ft 8 in (9.35 m) Height: 6 ft 3.5 in (1.918 m) Wing area: 154 sq ft (14.3 m 2) Empty weight: 465 lb (211 kg) Gross weight: 1,100 lb (499 kg) Fuel capacity: 10 US gallons (38 litres) Powerplant: 1 × Rotax 503 twin cylinder, two-stroke aircraft engine, 50 hp (37 kW ...
The Freebird II is a family of American side-by-side two-seat, high wing, tricycle gear, pusher configuration single engined kit aircraft originally designed for construction by amateur builders by the Freebird Airplane Company of Marshville, North Carolina, and later Pro Sport Aviation of Wingate, North Carolina.
Data from Jane's All the World's Aircraft 2010/11 General characteristics Crew: two Length: 12 ft 3 in (3.73 m) fuselage Width: 6 ft 1 in (1.85 m) fuselage maximum Height: 10 ft 0 in (3.05 m) overall Empty weight: 899 lb (408 kg) Gross weight: 1,499 lb (680 kg) Fuel capacity: 87 L (19.2 Imp gal, 23.0 US gal) usable Powerplant: 1 × Subaru EJ25 flat four piston, 160 hp (119 kW) Main rotor ...
Taylor Bird 1980 2 seat homebuilt, unk no. built [21] Strojnik S-2 1980 motorglider 1 seater, 8+ built. Aérostructure Lutin 80 1983 1 seat ultralight motorglider, 2 built [22] Birdman Chinook 1982 ultralight homebuilt, 1100+ built; Alpha J-5 Marco 1983 1 seat ultralight motorglider, unk no. built [20] Quad City Challenger 1983 2 seat ...
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 ...
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