The G2SA Genesis Duo features a single main rotor, a two-seats-in tandem open cockpit with a windshield, tricycle landing gear with wheel pants, plus a tail caster and a twin cylinder, air and liquid-cooled, four-stroke, dual-ignition, turbocharged 1150NaN0 Rotax 914 engine in pusher configuration. Other engine options include the 500NaN0 Rotax 503 and the 1000NaN0 Rotax 912 ULS.[1]
The aircraft fuselage is made from bolted-together aluminum tubing and is equipped with a composite fairing. Its two-bladed rotor has a diameter of 9.11NaN1 and a chord of 181NaN1. The aircraft has a typical empty weight of 2400NaN0 and a gross weight of 5600NaN0, giving a useful load of 2200NaN0. With full fuel of the payload for the pilot, passengers and baggage is 1630NaN0.[1]
The ready-to-fly version comes with the Rotax 503 as standard equipment. The kit version does not include the engine, propeller or main rotor pre-rotator.[1]