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Model originally projected for introduction in 2011 as a single seat US FAR 103 ultralight aircraft with a design empty weight under 254 lb (115 kg). The 103 intended to use the LiteSport Ultra wing mated to a newly CAD designed fuselage frame to save weight and was to be built by Free Bird Innovations. The project was set back when the lead ...
The Aero-Works Aerolite 103 is an American single seat, high-wing, pusher configuration ultralight aircraft, designed by Terry Raber and introduced by Aero-Works, Inc, of Millersburg, Ohio, in 1997. The aircraft's model number indicates that it was designed to comply with the Federal Aviation Administration FAR 103 ultralight rules. [1] [4] [5 ...
Data from Cliche and Kitplanes General characteristics Crew: one Length: 17 ft 0 in (5.18 m) Wingspan: 26 ft 3 in (8.00 m) Wing area: 110 sq ft (10 m 2) Empty weight: 240 lb (109 kg) Gross weight: 500 lb (227 kg) Fuel capacity: 5 US gallons (19 litres) Powerplant: 1 × Rotax 277, 28 hp (21 kW) Propellers: 2-bladed wooden Performance Maximum speed: 63 mph (101 km/h, 55 kn) Cruise speed: 60 mph ...
Raceair Designs LLC is an American aircraft manufacturer based in Gilbert, South Carolina, founded by designer Ed Fisher. The company was formerly located in Mayville, New York and Warren, Ohio . The company specializes in the design and manufacture of ultralight aircraft in the form of plans and kits for amateur construction and complete ready ...
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 ...
Challenger I (Challenger UL) Single seat, 31.5 ft (9.6 m) wingspan gives lower stall speed. Can be fitted with a variety of engines. Qualifies as a US "Experimental - Amateur-Built", Light sport aircraft or with the 22 hp (16 kW) Hirth F-33 engine as a US FAR 103 Ultralight Vehicle, 800 reported completed and flown by the fall of 2011.
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 is a monoplane derivation of the biplane H-2 Honey Bee and was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg). The aircraft has a standard empty weight of 252 lb (114 kg), when equipped with the now-out of production Rotax 277 single cylinder engine.