LF26 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 5kg)

D- motor LF 26

Microlight aircrafts

Four cylinders, four stroke, liquid cooled

2690 cc

80 mm

8/1

91.8 hp (67.5KW) at 3000 RPM

88.8 hp (65.3KW) at 2800 RPM

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

see fuel consumption table

220 Nm at 2500 RPM

Multipoint sequential fuel injection

25 Amp integrated

1.1 KW intergrated

Double

58 kg (battery and liquids not included)