The fuselage, stabilizer, elevator and rudder are welded tubular Chrome Molly 4130 steel and covered with Ceconite.

The wings and ailerons are 6061 T6 aluminium structure covered with Ceconite.

The leading edge is covered sheet aluminium to ensure the wing-foil shape.

The ailerons are full span and there are no flaps.

There are 2 fuel tanks in the wings, each 40 liters.

The landing gear has bungee cord suspension and large diameter tundra wheels with hydraulic disc brakes. The tail wheel is pneumatic and steers directly by compression springs from the rudder.