US Aviation CAVU

The US Aviation CAVU (named for the aeronautical meteorology term meaning "Ceiling And Visibility Unlimited") is an American high-wing, strut-braced, single-seat, open cockpit, single engine in pusher configuration, ultralight aircraft that was designed and produced by AeroDreams of Manchester, Tennessee, but marketed by US Aviation of St Paul, Minnesota under their brand name. The aircraft was supplied as a kit for amateur construction.

Design and development
The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb. The CAVU has an empty weight of 220 lb. The design goals for the CAVU were a simple and inexpensive aircraft, achieving good performance with a small and inexpensive engine.

The aircraft is made from aluminium tubing, wood and fabric. The fuselage is built on an aluminium tube, which supports the tail as well as the pilot's seat. Its 31 ft span wing is braced by a single lift strut. Powered by a Zenoah G-25 engine of 22 hp, the CAVU cruises at 52 mph. Acceptable engines can range in power from 22 to 30 hp. The fuel capacity is 3 u.s.gal, with 5 u.s.gal optional. The landing gear is tricycle gear.

Estimated assembly time from the kit is 100 hours.