[1][2] 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).

Its biplane wing has a top span of 24 ft (7.3 m), a bottom span of 20.3 ft (6.2 m), employs cabane struts and one set of interplane struts.

The controls are conventional three-axis, with full-span ailerons on the top wing.

The landing gear is bungee suspended and includes main wheel brakes and tailwheel steering.

[1] Data from Cliche and Virtual Ultralight Museum [1][2]General characteristics Performance