The PSE-2 Osprey was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 2540NaN0. The aircraft has a standard empty weight of 2350NaN0. It features a Hi-Pro 370square feet parachute-style wing, single-place accommodation, tricycle landing gear and a single 500NaN0 Rotax 503 engine.[1]
The aircraft carriage is built from aluminium tubing. In flight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw. On the ground the aircraft has foot pedal-controlled nosewheel steering. The main landing gear incorporates spring rod suspension.[1]
The standard day, sea level, no wind, take off with a 500NaN0 engine is 2000NaN0 and the landing roll is 750NaN0.[1]
The manufacturer estimates the construction time from the supplied assembly kit as five hours.[1]