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Migrator Swan I Model with upgraded features and optional agricultural spray equipment as well as with partial cockpit fairing. Empty weight of 133 kg (293 lb) and a gross weight of 420 kg (926 lb), giving a useful load of 287 kg (633 lb). With full fuel of 70 litres (15 imp gal; 18 US gal) the payload is 237 kg (522 lb). [1] Meteor Swan II
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.
This division offers two models, the Summit Steel Breeze two-place and the United States ultralight category FAR 103 Ultralight Vehicles compliant Summit 103 Mini Steel Breeze. As of 2012 Steel Breeze was a line marketed by Summit Aerosports Inc of Yale, Michigan. [9] [16] [17] [18] [19]
The Diehl AeroNautical XTC Hydrolight is an American amphibious flying boat ultralight aircraft that was designed and produced by Diehl AeroNautical in the 1980s. [1] The prototype first flew in March 1982, with production of kits commencing the following year. [2]
With a standard empty weight of 254 lb (115 kg), it was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg). It features a strut-braced high-wing , a single-seat open cockpit with windshield, fixed tricycle landing gear and a single engine in pusher configuration .
The Hy-Tek Hurricane 103 is a family of single-engined, high wing tricycle gear-equipped aircraft that were available in kit form from Hy-Tek Hurricane of Aurora, Oregon. [ 1 ] [ 2 ] [ 3 ] The Hurricane 103 and Ultra 103 designs are intended to have empty weights under 254 lb (115 kg) and fit into the US FAR 103 ultralight category .
The aircraft was originally intended to meet the requirements of the US FAR 103 Ultralight Vehicles category, including that category's maximum 254 lb (115 kg) empty weight. It was only able to achieve that low empty weight with the 28 hp (21 kW) Rotax 277 , which provided marginal performance.
The aircraft 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 B1-RD has a standard empty weight of 220 lb (100 kg).