DESCRIPTIONï Four cylinder, horizontally opposed engine, with liquid cooled cylinderheads, electronic fuel injection and dual ignition system, automatic altitude compensation, wet sump pressure lubrication FEATURERSï 1.Liquid cooled cylinderheads, electronic fuel injection and dual ignition system. 2,The ratio of power weight is higher. 3.Extremely low failure rate. TECHNICAL DATA: Maximum Power 74 kW / 100 HP at 3000 rpm Displacement 2424 cm3 / 147.91 cub. in. Compression ratio 9.5 : 1 Ignition Electronic engine management Fuel min. octane 98 RON (Unleaded) / AVGAS 100 LL Dry weight 76 kg, plus accessories Fuel consumption 265 g/kWh at WOT,245 g/kWh at part throttle. APPLICATION: Used for fixed wing, manned/unmanned, helicopter, gyrocopter, sailship. OTHER INFORMATION: We can provide propellers, generators(for UAV), start-generators and other accessories.