Product Description
C80 is a naturally aspirated, liquid-/air-cooled, horizontally opposed four-cylinder, four-stroke, gear reduction-drive engine commonly used on ultralight aircrafts, light sport aircrafts, and unmanned aerial vehicles.
Product Advantages
4-cylinder
4-stroke liquid-/air-cooled engine with opposed cylinders
Dry sump forced lubrication
with separate oil tank, automatic adjustment by hydraulic valve tappet
2 carburetors
Mechanical fuel pump
Dual electronic ignition
Electric starter
Propeller speed reduction gearbox
Dual constant depression carburetors
TBO 2000 h
| WEIGHT | KG | |
| Engine with propeller speed reduction gearbox i = 2.43 (opt. i = 2.27) | 58 | |
| Exhaust system | 4.0 | |
| Overload clutch | 1.7 | |
| Engine suspension frame | 2.0 | |
| PERFORMANCE | ||
| 59.6 kW | 80 hp | 5800 RPM |
| TORQUE | ||
| 103 Nm | 4800 RPM | |
| MAX RPM | 5800 RPM | |
| BORE | STROKE | |
| 79.5 mm | 61.0 mm | |
| DISPLACEMENT | FUEL | |
| 1211.2 cm³ | Min. RON 95 Mogas/ 100LL Avgas | |