- 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. |
| DISPLACEMENT |
|
| 1211.2 cm³ |
73.9 cu in |
* leaded, unleaded, AVGAS 100LL, Ethanol 10
UL: ASTM compliant | A: certified according to JAR 22
F: certified according to FAR33
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