Mathews Petit Breezy

[1][2][3] The Petit Breezy 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, tricycle landing gear and a single engine in pusher configuration.

Its 30 ft (9.1 m) span wing is supported by V-struts with jury struts.

The fuselage consists of an aluminum keel tube that runs from the nose wheel to the tail.

Construction time from the plans is estimated at 200–300 hours[2][4] Data from Cliche and the Virtual Ultralight Museum[1][2]General characteristics Performance