Also, aerobatic engines are "shock cooled" to the
extreme. Again, due to amazing engineering by
Lycoming, this really isn't a problem. You would
think that aerobatic engines would crack cylinders
and have several replaced every annual, but that's
not the case.
Just want to point out a little detail about Lycomings:
Cylinders can either be parallel valve, or angle-valve.
Note that the angle-valve jugs are NINE POUNDS
heavier than the parallel-valve jugs.
So you can have a 180hp (AE)IO-360 (parallel valve)
or 200hp (AE)IO-360 (angle valve) engine, but the
angle valve engine weighs 4x9=36 lbs heavier.
Or, you can have a 260hp (AE)IO-540 (parallel valve)
or 300hp (AE)IO-540 (angle valve) engine, but the
angle valve 540 engine weighs 6x9=54 lbs heavier.
You can modify any of the above to produce more
horsepower, with improved exhaust, cold air induction,
or higher compression pistons. Non-certified, of course.
For example, you can easily make a 300hp AEIO-540
with parallel-valve jugs. Light and powerful.
My long-winded point is that you would think that
the heavier angle-valve heads, with all that meat,
would be more resistant to cracking from the abuse
of shock cooling, but that doesn't appear to be the
case. The lighter parallel-valve jugs are very resistant
to cracking. Again, amazing engineering by Lycoming.
This thread has been really educational and with a lot of great information that otherwise is hard to find
That's what aviation is all about. The people, oddly
enough, not the hardware. You will meet the weirdest
collection of scoundrels and saints in aviation. The fun
part is that when you meet someone for the first time,
you never know which one they are. All you know is
that it won't be boring!