The C115 aero engine is a widely used turbocharged aircraft engine for ultralight and light-sport aircraft as well as medium altitude long endurance unmanned aerial vehicles. The C115 offers more performance at high altitude and one of the best power to weight ratios, in excess of 1.134 kW/kg.

Technical Parameters

- 4-cylinders

- 4-stroke liquid-/air-cooled engine with opposed cylinders

 

- Dry sump forced lubrication with a separate oil tank

- Turbo charger

- Automatic waste gate control

 

- Automatic hydraulic valve tappet adjustment

- Dual carburettors

- Mechanical fuel pump

- Dual electronic ignition

- Electric starter

- Propeller speed reduction gearbox

- Engine mount assembly 

- Air intake / exhaust system 

- TBO 2000 h