MarketRotax 912
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Rotax 912

The Rotax 912 is a horizontally-opposed four-cylinder, naturally-aspirated, four-stroke aircraft engine with a reduction gearbox. It features liquid-cooled cylinder heads and air-cooled cylinders. Originally equipped with carburetors, later versions are fuel injected. Dominating the market for small aircraft and kitplanes, Rotax produced its 50,000th 912-series engine in 2014. Originally available only for light sport aircraft, ultralight aircraft, autogyros and drones, the 912-series engine was approved for certified aircraft in 1995.

Design and development
The Rotax 912 was first sold in 1989 in non-certificated form for use in ultralights and motorgliders. The original 912 UL engine has a capacity of and a compression ratio of 9.1:1, and is designed to work with regular automotive gasoline, with up to 10% ethanol. The later certified 912 ULS variant has a compression ratio of 11:1, and requires 91-octane ("premium") auto gas (100LL leaded avgas can be used, sparingly). The engine differs from previous generation aircraft engines (such as the Lycoming O-235) in that it has air-cooled cylinders with liquid-cooled heads and uses a 2.43:1 PSRU reduction gearbox to reduce the engine's relatively high 5,800 rpm shaft speed to a more conventional 2,400 rpm for the propeller. The gearbox has proven to be generally trouble-free. The 912's lubrication system differs from most dry-sump designs in that 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. A torsional shock absorber consisting of 2 dog gears serves to smooth the power pulses and reduce gearbox wear during startup and shutdown. In addition to the lower fuel consumption, the 912 is certified to run on automotive fuel (mogas), further reducing running costs, especially in areas where leaded avgas is not readily available. with ECUs supplied by Rockwell Collins. The version weighs , which is more than the standard 912S. The non-certified 912 iS targets the light sport and homebuilt aircraft market and 912 iSc will be certified. Production started in March 2012, and the engine has a 2000-hour recommended time-between-overhaul. On 1 April 2014, the company announced its new 912 iS Sport upgrade with greater power, torque, and reduced fuel consumption. A derivative, the Rotax 915 iS, was announced in July 2015, and a further upgrade, the Rotax 916 iS was announced in March 2023. Rotax's warnings to flyers Rotax publishes extensive warnings in the owner's manual about both the certified and non-certified versions of the engine design. Pilots are cautioned that the 912 engine is not suitable for: • use in situations where a safe landing cannot be made • use in rotorcraft • night flying (unless equipped with redundant electrical power), or • aerobatics. ==Variants==
Variants
The engine is available in the following versions; coloured cylinder head caps are used to easily identify the different horsepower ranges: ;912 A# :Certified to JAR 22, , with dual carburetors and electronic ignition. Black cylinder head caps ;912 F# :Certified to FAR 33, , with dual carburetors and electronic ignition. Black cylinder head caps ;912 iS :Uncertified, with direct fuel injection and an electronic engine management unit. Green cylinder head caps ;912 iSC Sport Green cylinder head caps ;912 S# :Certified to FAR 33, with larger bore than 912A/F/UL, with dual carburetors and electronic ignition. Green cylinder head caps ;912 UL# :Uncertified, , similar to the 912A/F. Black cylinder head caps ;912 ULS# :Uncertified, , similar to the 912S. Green cylinder head caps ;912 ULSFR# :Uncertified French Authority specification. The # in the designation stands for: • Shaft with flange for fixed pitch propeller, P.C.D. 100 mm • Shaft with flange for fixed pitch propeller, P.C.D. 75 mm, P.C.D. 80 mm and P.C.D. 4 inches • Shaft with flange for constant speed propeller P.C.D. 75 mm, P.C.D. 80 mm, P.C.D. 4 inches and drive for hydraulic governor for constant speed propeller • Shaft with flange for fixed pitch propeller P.C.D. 75 mm, P.C.D. 80 mm, P.C.D. 4 inches also can be fitted with an adaptor, drive and governor for a constant speed propeller. ==Specifications (Rotax 912 UL/A/F)==
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