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 DATA | WEIGHT | kg | lb | | 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 |
| | PERFORMANCE |
|
| | 59.6 kW | 80 hp | 5800 1/min. |
| TORQUE |
|
| | 103 Nm | 75.9 ft. lb. | 4800 1/min. |
|
