Rotax 912 iS Sport Aircraft Engine

<p>- 4-cylinder<br>- 4-stroke liquid-/air-cooled engine with opposed cylinders<br>- Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappets<br>- Redundant electronic fuel injection<br>- Engine management system<br>- Electric starter<br>- Propeller speed reduction unit<br>- Air intake system</p> <p>Engine data</p> <p>VERSION</p> <p>PERFORMANCE</p> <p>TORQUE</p> <p>MAX RPM*</p> <p>kW hp 1/min Nm ft. lb. 1/min 1/min</p> <p>912 iS1 / iSc2 Sport 73.5 100 5800 121 89 5800 5800</p> <p>72.0** 98 5500 125 92 5500</p> <p>68.0 92.5 5000 132*** 97 5000</p> <p>*Limited for max. 5 min. **Max. continuous power at 5500 1/min ***MOGAS, no hydraulic governor</p> <p>BORE</p> <p>STROKE</p> <p>DISPLACMENT</p> <p>FUEL</p> <p>84.0 mm 3.31 in 61 mm 2.4 in 1352 cm³ 82.6 cu.in. min.MON 85 RON 95*<br>min. AKI 91*</p> <p>* leaded, unleaded, AVGAS 100LL or E10</p> <p>WEIGHT</p> <p>KB</p> <p>LB</p> <p>Engine with propeller speed reduction unit. i = 2.43 with overload clutch 63.6 140.2</p> <p>Exhaust system 4.8 9.5</p> <p>Air guide hood 0.4 0.8</p> <p>External alternator 3.0 6.6</p> <p>Fuel pumps assy 1.6 3.5</p> <p>Engine mount 2.0 4.4</p>