LF39 specifications

Type

Class

Engine

Displacement

Stroke

Compression ratio

Max power

Max continuous power

Used fuel

Fuel consumption

Maximum torque

Intake

Alternator

Electric starter

Ignition

Installed dry weight (liquids 7 kg)

D- motor LF 39

Microlight aircrafts

6 cylinders, four stroke, liquid cooled

3993 cc

79 mm

8/1

125Hp at 3000 RPM

112Hp hp at 2800 RPM

91, 93, 95 oct. 98 oct. or avgas

19 liter at 75% performance

285 Nm at 2500 RPM

Multipoint sequential fuel injection

25 Amp integrated

1.1 KW intergrated

Double

78 kg