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The Rotax 914 is a turbo-charged, four-stroke, four-cylinder, horizontally opposed aircraft engine with air-cooled cylinders and water-cooled cylinder heads. It is designed and built by the Austrian company BRP-Powertrain, owned by Bombardier Recreational Products (BRP), as part of its Rotax brand.
Low-weight engine with excellent performance at high altitudes. Four-stroke piston engine with four liquid and air-cooled cylinders. Turbocharger. Automatic wastegate control. Dry sump forced lubrication with separate oil tank, automatic adjustment by hydraulic valve tappet. 2 carburetors.
914 UL | F 115 HP POWER MEETS RELIABILITY. The ultimate flight experience with the best power-to-weight ratio and reliability.
The ROTAX 914 engine is equipped with two air-pressure sensors. One measures aircraft ambient pressure and the other measures airbox pressure. Both air-pressure sensors report to the TCU and play a vital function in helping the TCU achieve the optimum level of boost.
Datasheet 914. ROTAX AIRCRAFT ENGINES www.rotax-aircraft-engines.com DESCRIPTION 4-cylinder, 4-stroke liquid/air cooled engine with opposed cylinders, with turbo charger, with automatic waste gate control, dry sump forced lubrication with separate oil tank, au- tomatic adjustment by hydraulic valve tappet, 2 carburators, dual electronic ...
Rotax 914 UL with options, delivery state Turbo charged low weight engine with more performance on high altitudes.
The turbo charged Rotax 914 series offers more performance at high altitudes while keeping weight at a low level. This series offers a time between overhauls of 2.000 hrs and is available as certified (Rotax 914 F) according to FAR 33 and JAR-E and non-certified version. (Rotax 914 UL). ENGINE TORQUE FUEL CONSUMPTION
