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C80 is a naturally aspirated, liquid-/air-cooled, horizontally opposed four-cylinder, four-stroke, gear reduction-drive engine commonly used on ultralight aircraft, light sport aircraft, and unmanned aerial vehicles.
The standard version includes parts:
Engine body (with overload clutch) also includes: fuel pump (2), overflow bottle (1), fuel filter (1), air filter (2), exhaust system kit (1)
Standard Package includes:
- Gearbox with Overload Clutch i=2.43
- Electric Starter (12V/700Wt)
- Starter Relay
- Electronic Dual ignition System
- Regulator Rectifier
- 2 x Carburetors
- Expansion Tank
- Exhaust Sockets
- Fuel Tank without Tubes
- Coolant Pump & Internal Coolant Hoses
- Sensors x 2 for Cylinder Head Temperature
- Sensor x 1 for fuel temperature
- Sensor x 1 for fuel Pressure with Harness
- Mechanical Fuel Pump
- Integrated AC Generator (12V/20A DC)
Optional:
- Oil Radiator
- Coolant Radiator
- Exhaust Gas Temperature Sensor
- Overflow Bottle
- Motor Mount and Motor mount ring
- Air Filter
- 6. Exhaust Pipes and Muffler
- Engine Suspension Frame & Shock Mount Sets
- Overload Clutch (i.e.slippery clutch)
- Electric Starter (12V/900Wt)
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 | |