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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. C115 offers more performance at high altitude and the best power to weight ratio at better than 1.134 kW/kg.
Standard version includes parts
Engine body (need to check with the customer whether there is an overload clutch optional) also includes: fuel pump (2), overflow bottle (1), fuel filter (1), air filter (1), exhaust system kit (1)
Standard Package includes:
Optional:
4-cylinder
4-stroke liquid-/air-cooled engine with opposed cylinders
With turbo charger
With automatic waste gate control Dry sump forced lubrication
with separate oil tank
Automatic adjustment
by hydraulic valve tappet
2 carburetors
Dual electronic ignition Electric starter
Propeller speed reduction gearbox
Engine mount assembly
Air intake system Exhaust system
TBO 2,000 H
4-cylinder
4-stroke liquid-/air-cooled engine with opposed cylinders
With turbo charger
With automatic waste gate control Dry sump forced lubrication
with separate oil tank
Automatic adjustment
by hydraulic valve tappet
2 carburetors
Dual electronic ignition Electric starter
Propeller speed reduction gearbox
Engine mount assembly
Air intake system Exhaust system
TBO 2,000 h
| WEIGHT | KG | |
| Engine with propeller speed reduction gearbox i = 2.43 | 74.5 | |
| Overload clutch | 1.6 | |
| Engine suspension frame | 2.3 | |
| PERFORMANCE | ||
| 84.5 kW | 115 hp | 5800 RPM |
| TORQUE | ||
| 140 Nm | 4900 RPM | |
| MAX RPM | 5800 RPM | |
| BORE | STROKE | |
| 79.5 mm | 61.0 mm | |
| DISPLACEMENT | FUEL | |
| 1211.2 cm³ | Min. RON 95 Mogas/ 100LL Avgas | |
