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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Trade Leads Directory -> All Trade Leads -> Transportation -> Aircraft, Spacecraft -> Limbach L2400EB Avaiation Engine Limbach L2400EB Aircraft Engine UAV E
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