DESCRIPTIONï Four cylinders,horizontally opposed engine,aircooled,single magneto ignation,wet sump pressure lubrication FEATURERSï 1.The ratio of power weight is higher. 2.Extremely low failure rate. 3.Turbo charger,full take off power up to 3500 meters. TECHNICAL DATA: Maximum Power 64 kW/87 HP at 3200 rpm Displacement 2424 cm3 / 147.91 cub. in. Compression ratio 8.5:1 Two carburetors Fuel min. octane 98 RON (Unleaded) / AVGAS 100 LL Dry weight 82 kg, plus accessories Fuel consumption 14L/hour APPLICATION: Used for fixed wing, manned/unmanned, helicopter, gyrocopter, sailship. OTHER INFORMATION: We can provide propellers, generators(for UAV), start-generators and other accessories.