The highly reliable and efficient entry-level motor for light aviation aircraft manufacturers.
Four-stroke piston engine with four liquid and air-cooled cylinders
Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet
The lightest engine in the Rotax aircraft engine portfolio
2 carburetors
Mechanical fuel pump
Dual electronic ignition
Electric starter
Propeller speed reduction gearbox
TBO 2,000 hrs
Engine with propeller speed reduction gearbox i = 2.27 (opt. i = 2.43) - 55.4 - 122.0
Exhaust system - 4.0 - 8.8
Overload clutch - 1.7 - 3.7
External alternator - 3.0 - 6.6
Air guide hood - 0.4 - 0.8
Engine suspension frame - 2.0 - 4.4