of Castel Maggiore, Italy, had its TDA CR 1.9 8V EASA certified on 11 June 2010 : a 1.9 l liquid cooled, 4 cylinder, 4 stroke, 8 valves engine, with a turbocharger and Common Rail injection, a 1:0.644 reduction gearbox and dual FADEC, it produces 118 kW (160 hp) at take-off and 107 kW (146 hp) continuously at 2450 propeller RPM for 205 kilograms .