[1] The EViva was originally designed by Martin Wezel in conjunction with the Czech company Composit and initially intended to be powered by a 50 hp (37 kW) Rotax 503 two-stroke or 60 hp (45 kW) HKS 700E four-stroke powerplant.

The design was purchased by Yuneec, development shifted to China and the aircraft was adapted for electric power.

[1] The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight rules.

It features a cantilever wing, a T-tail, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, retractable monowheel gear with wing tip and tail casters, and a single electric motor in tractor configuration driving a folding propeller.

The aircraft will come equipped with a Ballistic Recovery Systems ballistic parachute[1][2] Data from World Directory of Leisure Aviation 2011-12 and Yuneec[1][2]General characteristics Performance