The Light Weight Engine Houtekietstraat 11
B-8540 Deerlijk, Belgium
EFFECTIVITY page 16
ALL 19-3-2019
The above is one option, please contact our sales team for all possible options, incl. heli options.
Short specification list
• Type: D- motor LF39
• Class: Microlight aircrafts
• Engine: 6 cylinders, four stroke, liquid cooled
• Displacement: 3993 cc
• Stroke: 79 mm
• Compression ratio: 8/1
• Max power: 125 Hp at 3000 RPM
• Max continuous power: 112Hp hp at 2800 RPM
• Used fuel: 91, 93, 95 oct. 98 oct. or avgas
• Fuel consumption: 19 liter at 75% performance
• Maximum torque: 285 Nm at 2500 RPM
• Intake: Multipoint sequential fuel injection
• Alternator: 25 Amp integrated
• Electric starter: 1.1 KW integrated
• Ignition: Double
• Installed dry weight (liquids 7kg): 78 kg
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