The Spring WS202 Sprint was a Canadian homebuilt aircraft that was designed and produced by William J.
[1][2] The WS202 Sprint featured a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed tricycle landing gear or conventional landing gear and a single engine in tractor configuration.
With full fuel of 14 U.S. gallons (53 L; 12 imp gal) the payload for the pilot, passenger and baggage was 396 lb (180 kg).
[1] The standard day, sea level, no wind, take off and landing roll with a 65 hp (48 kW) engine was 500 ft (152 m).
[1] The manufacturer estimated the construction time from the supplied plans as 1500 hours.