Description Four cylinder, horizontally opposed engine, with liquid cooled cylinderheads, electronic fuel injection and dual ignition system, turbo charger, automatic altitude compensation, wet sump pressure lubrication Featurers 1.Liquid cooled cylinderheads, electronic fuel injection and dual ignition system. 2, the ratio of power weight is higher. 3.Extremely low failure rate. 4.Turbo charger, full take off power up to 3500 meters. Technical data: Maximum power 96 kw / 130 hp at 3000 rpm Displacement 2424 cm3 / 147.91 cub. In. Compression ratio 8 : 1 Ignition electronic engine management Fuel min. Octane 98 ron (unleaded) / avgas 100 ll Dry weight 86 kg, plus accessories Fuel consumption 255 g/kwh at wot, 240 g/kwh at part throttle Application: Used for fixed wing, manned/unmanned, helicopter, gyrocopter, sailship.