DESCRIPTION：

Four cylinder, horizontally opposed engine, with liquid cooled cylinderheads, electronic fuel injection and dual ignition system, automatic altitude compensation, wet sump pressure lubrication

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.

Maximum Power 118 kW / 160 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.

Used for fixed wing, manned/unmanned, helicopter, gyrocopter, sailship.

OTHER INFORMATION:

We can also provide propellors,generators, UAV hybrid system and other spares for all our engines.