The Matto features a single main rotor, a two-seats-in
side-by-side configuration enclosed cockpit with a windshield,
tricycle landing gear with
wheel pants and a
GG 912 VT engine in
pusher configuration. The aircraft
fuselage is made from a combination of
carbon fibre and
Kevlar. Its two-bladed rotor has a diameter of and a chord of . The aircraft has a typical empty weight of and a gross weight of , giving a useful load of . With full fuel of the payload for the pilot, passenger and baggage is . The design incorporates a number of safety features, including a
ballistic parachute mounted inside the rotor mast, which ensures that the rotor will not contact the parachute as it is deployed. Other safety features include a fire-proof cockpit, rupture-resistant and fuel tanks and anti-collision
strobe lights. ==Specifications (Matto) ==