Rotax 916 iS Turbo Aircraft Engine

<p>Dynamic, turbocharged iS engine with best power-to-weight ratio and TBO 2,000h.</p> <p>- Four-stroke piston engine with four liquid and air-cooled cylinders<br>- Redundant electronic fuel injection and ignition, eco mode<br>- Turbocharger, stainless steel exhaust<br>- Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappets<br>- Engine management system (EMS)<br>- Electric starter (12 or 24 Volt)<br>- Propeller speed reduction gearbox<br>- Intercooler<br>- TBO 2,000 hrs<br>- Maximum operating altitude 23,000 feet<br>- Full take-off power up to 15,000 feet</p> <p>ENGINE DATA</p> <p>WEIGHT kg lb</p> <p>Engine with propeller speed reduction gearbox i= 2,54 with overload clutch, turbocharger, intercooler, exhaust system 85.8 189</p> <p>Engine suspension frame 2.0 4.4</p> <p>External alternator 3.0 6.6</p> <p>Air guide baffle 0.4 0.8</p> <p>PERFORMANCE</p> <p>117 kW 160 hp 5800 1/min</p> <p>**101 kW 137 hp 5500 1/min</p> <p>TORQUE</p> <p>193 Nm 142 ft lb 5800 1/min</p> <p>175 Nm 129 ft lb 5500 1/min</p> <p>BORE</p> <p>84.0 mm 3.31 in</p> <p>STROKE</p> <p>61.0 mm 2.4 in</p> <p>DISPLACEMENT</p> <p>1352 cm³ 82.6 cu in</p> <p>FUEL*</p> <p>min. MON 85 RON 95 min. AKI 91</p>