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Why can the 912 do this?


Ed Cesnalis

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Posted

Here at Mammoth there have always been crashes on departure due to the small piston single engine plane departing full rich. If you are behind a Lycoming or Continental and try to take off full rich, you will have degraded performance and rough running.

 

The lyc and cont need to be leaned at WOT in order to keep from fowling plugs while you taxi and in order to provide adequate power to climb and take off. The Rotax can do what they can't it can operate full rich and not run rough. I don't know if it loses power or not because I cannot adjust the mixture. With the lyc and cont at a full power run up we would lean until we found max RPM and then richen 2 twists from there and that way determine best power for takeoff. With a 912 there is no equivalent leaning, both carbed and FI have no leaning at WOT.

 

First I was curious as to why Rotax would not provide high altitude WOT leaning but now I realize there is first the question of why they can get away with it when it would mean departure crashes with other engines. Curious, would it be the high compression ratio making the difference?

Posted

Idle is a distinct circuit then the needle jet gets control all the way until approaching WOT.

 

Approaching wide open throttle the main jet takes control and the mixture is determined by the main jet.

 

Most throttle positions give control to the needle circuit and the needle height is adjusted by the diaphragm that it sits on. The diaphragm is at the pressure differential and adjusts mixture according to the differential.

Posted

Frankly, I don't know why the Bing Carbs work as well as they do, but I routinely take off at full gross with a density altitude of 8500' on a hot day. KLMO has a geographic altitude of 5050', and on a 90-95 degree day, the plane will still levitate.

 

The CT2k is an amazing aircraft.

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