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Phantom I Single seat ultralight aircraft with struts in place of cable-bracing. Standard engine is the 50 hp (37 kW) Rotax 503 with the 64 hp (48 kW) Rotax 582 as an option. [6] Phantom I-E Single seat ultralight aircraft with struts in place of cable-bracing and enclosed cockpit with removable doors.
As a copy of the Phantom X1, the Hurricane family shares its construction. The wings, tail and fuselage are constructed of anodized aluminum tubing, bolted together. The wings and tail surfaces are covered with Dacron envelopes. The wings are supported by cable-bracing from an inverted V-kingpost. The cockpit fairing, or pod, is made from ...
The Corvus Phantom is a Hungarian two-seat ultralight aircraft produced by Corvus Aircraft. [1] [2] In the USA it is marketed as the Falcon LS, from 2008 until 2010 by T&T Aviation, since 2010 by Renegade Light Sport. [3] In Germany the aircraft is called the Wild Angel and in the United Kingdom the Crusader. [2] An Iranian registered Phantom
The Spitfire is a derivative of the Phantom X1 that was created by former Phantom Aeronautics employee Fred Bell, who also designed the Bell Sidewinder. The Spitfire 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 ...
The Sidewinder is a copy of the Phantom X1 that was built by former Phantom Aeronautics employee Fred Bell. 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). The aircraft has a standard empty weight of 250 lb (113 kg).
The company produced three simple ultralight designs, the Worldwide Ultralite Clipper, the Worldwide Ultralite Skyraider S/S and the Worldwide Ultralite Spitfire, which was derived from the Phantom X1. After the demise of Worldwide Ultralite, the Spitfire design was produced by Don Ecker and later Air Magic Ultralights of Houston, Texas [1] [2] [3]
The MZ 202 was developed first as a 60 hp (45 kW) lightweight competitor to the liquid-cooled 64 hp (48 kW) Rotax 582.Later the MZ 201 was developed from the MZ 202 as a de-rated 45 hp (34 kW) version intended for motorgliders and single place ultralights that needed more power than the single-cylinder Zanzottera MZ 34.
A copy of the popular Phantom X1, the Mosquito 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).