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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.
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.
26 Απρ 2021 · Information on maintenance and spare parts planning for ROTAX® Aircraft Engines. 912 Series. Installation of a propeller by usage of round-neck nut set for ROTAX® 912, 914, and 912 i (Series) Aircraft Engines. ROTAX Tech Talk: Troubleshooting the Rotax 912 ignition system.
914 UL | F 115 HP POWER MEETS RELIABILITY. The ultimate flight experience with the best power-to-weight ratio and reliability.
Engine Specifications. Type: Four-cylinder, four-stroke liquid-/air-cooled engine with opposed cylinders; Displacement: 1,211.2 cc; Bore: 79.5 mm; Stroke: 61 mm; Dry Weight: 78 kg with electric starter and other components; Design and Development. The Rotax 914 UL is a turbocharged development of the Rotax 912.
The turbo charged 115 HP 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. Price does not include shipping.
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
