MarketRotax 914
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Rotax 914

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.

Design and development
Introduced in 1996, the Rotax 914 is a turbocharged development of the Rotax 912. The 914 oil system differs from most dry-sump designs in that lubricating oil is forced into the storage tank by crankcase pressure rather than by a separate scavenge pump. This requires a novel preflight inspection procedure: before checking the oil level with the dipstick, the engine is "burped" by removing the oil filler cap and turning the propeller until a gurgling sound is heard, which indicates that all oil has been forced into the tank and the oil level can now be checked accurately. If the 914 is operated using leaded fuel, lead sludge will accumulate in the oil tank and reduction gearbox, and the fuel is incompatible with the recommended synthetic oil because it cannot hold lead in suspension; consequently, using leaded fuel mandates additional maintenance, and unleaded fuel is recommended. ==Variants==
Variants
;914 F :Family of engine versions certified to US Federal Aviation Administration FAR 33 and EASA JAR-E. These include: :*914 F2: Version equipped to accept a fixed pitch propeller. :*914 F3: Version equipped with a hydraulic governor for a constant speed propeller. :*914 F4: Version equipped to accept a hydraulic governor for a constant speed propeller. ;914 UL :Non-certified engine version for homebuilt and ultralight aircraft. ==Applications==
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