DESCRIPTION: Four cylinders, horizontally opposed engine, aircooled, single magneto ignation, wet sump pressure lubrication
FEATURERS: 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.
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