Postings are scarce on KR net this holiday period so I'm putting this in
for anyone that's bored.

I admire you guys with your Subarus.  A lot of engineering complexity
goes into getting these engines to work well in an aircraft.  Besides the
thrust bearing issue Max Power is discussing, other Subaru issues are
water cooling, turbocharging, reduction drives and through using these
mechanical features, squeezing a huge amount of power out of such
relatively small displacement engines - 2.2 litres - roughly the same as
a GP 2180 or Revmaster 2100D.  Instead of getting the rated 76 HP at 3400
RPM of a GP2180, the Suburus are pulling 182 HP from an engine of roughly
the same displacement.

I had a hangar neighbor, a retired aircraft engineer/designer, really put
his heart and wallet into an EA-81 turbo installation on his Europa over
a period of 10 years.  He used the Marcotte PSRU (I've earlier
incorrectly posted that he used the Eggenfeller).  The Europa was
designed for a Rotax but Wayne was attracted to the idea of using more
power and making a really high flyer out of it with lots of range.  He
made many enhancements such as additional fuel capacity and added all the
available factory options and, of course, put a dual GRT panel in it
along with a plethora of back-up instruments.  A really first class
effort that taxed his excellent engineering skills.  It took a lot of
ingenuity to sculpt into the stock Europa design the radiators and
plumbing necessary for the Suburu.   The front end came out looking
rather bulky and not very sleek looking but it was engineered well.  When
finished the engine ran well for quite a few hours on the ground and even
ran well enough for Wayne to fly it up to the designated airport for
flying off the 40 hours.  Since it was a monowheel, he had a landing
mishap in a crosswind so brought it back to Gillespie to install the
tri-gear option that's offered for the Europa.  After running the engine
some additional time on the ground, when he again was headed to the 40
hour fly-off airport, the engine disintegrated shortly after takeoff. 
Wayne, although he had been doing very little flying while building this
plane, landed it on a busy freeway without mishap and had a flatbed truck
bring it back to his hangar.  The engine had broken a timing gear and
swallowed some valves and he hadn't the heart or trust in it to re-build
it.  He trashed it and all his elaborate plumbing, reshaped the cowling
and put in a Rotax.  He then sold it to a fellow who flies it (N951EU)
out of Apple Valley.   Wayne retired to the Ozarks.

Pictures at this link show what it looked like with both the Suburu and
the Rotax cowlings.

https://tinyurl.com/rckpda3

Discussing things afterwords the concensus seemed to be that trying to
squeeze so much power out of a 2.2 liter engine frequently causes failure
due to heat and stress.  Mainly stress.  Same thing that kills people
kills engines.  Sometimes the reduction drive is also a factor.  

https://www.nbcsandiego.com/news/local/small-homemade-plane-lands-on-stat
e-route-67/1928901/

What boggles the mind is how the automotive industry manages to make
reliable engines by doing the same thing - developing huge horsepower
numbers from very small displacement engines.  I think they get away with
it because the engines, while rated at a high HP, spend their lives
loafing along at very low power settings - unlike engines used in
aviation applications.  The fastest production car in the world (until
recently . . . it's always changing), the Koenigsegg Agera RS, gets its
1160 HP out of a 5 liter V8, about the same size engine as what's in my
Olds 98.  

Mike
KSEE
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