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Hi Folks -

Are there any gurus out there with real experience with the 912 series
Rotax engines? (Not the old two-strokes)

For sure, they have issues that the Continentals don't have, and a couple of
pluses.

For what I hear from those who have them, some of the myths and issues
relate to:

1.  Liquid cooling.  Yes, they are partially liquid cooled in the cylinder
barrel area, with the heads being air cooled.  The manual for the Tecnam
says that if you lose coolant, retard power to 55%, and fly on all day long.
At low power like that, the air cooling is sufficient for the entire engine.

Remember that 60 years ago, the Mustang, Spitfire, Me-109, Hurricane, P-38,
Lancaster bomber, et al. went thru a whole war with liquid cooled engines.

2.  Hi RPM - True, the thing cruises around 4800 engine rpm.  High by the
standards of the 1930s when the Contis were designed, but not high by
today's standards.  My car runs 3400 rpm at 70 mph, and the one I had before
this one wasn't even burning oil when I sold it at 150,000 miles.

3.  Light weight and streamlined.  Here's why Rotax is being used in so many
LSAs - 100 hp from an engine that is far lighter than an O-200, and the
frontal area is far less, allowing a more aerodynamically efficient front
end for the airplane.

4.  Used to be far cheaper to overhaul.  Anyone know any real life overhaul
costs now?

5.  Premature top end failures/overhauls.  This seems to be directly tied to
the use of a steady diet of 100LL.  When operated on car gas, the issue goes
away.  Remember, that in Europe, Avgas is extremely expensive.  My cousin,
who is an FBO in Switzerland, tells me that he's seen Avgas as high as
$9.00/U.S. gallon (No typo - yes, $9.00).  So Rotax designed the engine to
run on lead free auto gas, and the certification for 100LL is an after
thought, mainly for the U.S. market where auto fuel is hard to deal with at
airports, unlike in Europe where it's available.

Thanks, and looking for any real life experiences.

Jerry E.

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