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LF39 specifications

TypeD- motor LF 39
Experimental/E-LSAMicrolight aircrafts
Engine6 cylinders, four stroke, liquid cooled
Displacement3993 cc
Bore103.6 mm
Stroke79 mm
Compression ratio8/1
Max power125Hp at 3000 RPM
Max continuous power112Hp hp at 2800 RPM
Accepted Fuels91, 93, 95 oct. 98 oct. or avgas
Fuel consumption19 liter at 75% performance
Maximum torque285 Nm at 2500 RPM
IntakeMultipoint sequential fuel injection
Alternator25 Amp integrated
Electric starterIncluded - 2 Mounting Options
IgnitionDouble
Installed dry weight (liquids 7 kg)78 kg

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