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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.
Typical wings used have a 9.5 to 10.2 m (31.2 to 33.5 ft) span wing, are supported by a single tube-type kingpost and use an "A" frame weight-shift control bar. The standard powerplant is the twin cylinder, air-cooled, two-stroke , dual-ignition 64 hp (48 kW) Rotax 582 engine.
Regulation of ultralight aircraft in the United States is covered by the Code of Federal Regulations, Title 14 (Federal Aviation Regulations), Part 103, or 14 CFR Part 103, which defines an "ultralight" as a vehicle that: has only one seat [1] [2] Is used only for recreational or sport flying [1] [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 .
Many of the early ultralights used a "weight shift" method of control, requiring the pilot to push a control bar to shift the center of gravity of the aircraft. The Weedhopper differed from most other ultralights of the period in that it has a control stick which moves the rudder and elevator, giving it two axis control in pitch and yaw.
Single seat, wired-braced Part 103 ultralight flying boat. Engines available were the 28 hp (21 kW) Rotax 277 and the 35 hp (26 kW) Rotax 377. [1] Buccaneer SX Single seat, strut-braced flying boat. Engines available were the 40 hp (30 kW) Rotax 447 and the 50 hp (37 kW) Rotax 503. [1] Buccaneer II Two seat, strut-braced flying boat.
The Hornet has the largest wing area and lightest wing loading of any ultralight of its period. The acceptable power range is 30 to 35 hp (22 to 26 kW) and the standard engine used is the 35 hp (26 kW) Cuyuna 430 powerplant. The engine is mounted between four tubes that support the tail surfaces. [1] [3]
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