The ZR 250 was designed to comply with the US FAR 103 Ultralight Vehicles rules as well as European regulations. It features a paraglider-style wing, single-place, or two-place in tandem accommodation and a single 220NaN0 Zenoah G-25 engine in pusher configuration with a 2.5:1 ratio reduction drive and a 1230NaN0 diameter two-bladed propeller. The fuel tank capacity is .[1]
As is the case with all paramotors, take-off and landing is accomplished by foot. Inflight steering is accomplished via handles that actuate the canopy brakes, creating roll and yaw.[1]
In reviewing the ZR 250 Rene Coulon wrote in 2003, "Their range of paramotors is of the same calibre as their other services: serious and functional".[1]