Hi Mark,
Live and learn I guess, I am amazed that no one picked this up, but your 
system really looks
good. These baffles would cause a turbulence inside. We all have a 
tendency to make our
inlets too large and this causes turbulence, it is better to have small 
inlets for a smooth
cooling flow. Absolutely no obstructions from outside through the inlets 
to the cylinders.
A hard lesson for sure but I hope this is a heads up for others that are 
at this point.
Now for the Happy Flying when it gets together!
Adrian

Mark Jones wrote:

>A lot of you have e-mailed and asked what happened to my engine and why is
>it torn down right now. Incorrect air inlet baffling on the front of the
>cowl caused my two front cylinders to over heat. This in turn resulted in a
>cracked piston and
>a broken ring in the #5 cylinder. The resulting compression on this cylinder
>was 14/80. The opposing #6 cylinder had problems also with a compression of
>25/80. The rings and piston on #6 were not broken or cracked but the rings
>were no longer sealed and the gaskets were leaking as were the gaskets on
>#5. The front cylinders were blocked from any direct cooling air as you can
>see in this link http://mywebpage.netscape.com/n886mj/baffles.html . Notice
>how the air inlet baffles cover the entire front of the cylinders. A costly
>design mistake on my part. The top half of the cylinders must be exposed to
>the inlet air. The strange thing is that my FSDO inspector did not catch the
>bad design nor did anyone else who looked over my plane. The photos on the
>link above were posted long before I made the first flight and not a single
>person on the net caught the design flaw either. That really surprised me
>since everything posted on the net is picked over with a fine tooth comb. Oh
>well, my loss, your gain since you learn from my mistake. I have a total of
>about $250 in repair parts (one piston,  one full set of 6 piston rings,
>lifters, head gaskets, base gaskets, top engine gaskets, valve cover
>gaskets, push rod tube o-rings, push rod guide o-rings, etc.) headed my way
>and should be here by mid week. I have already surfaced my heads and cross
>hatch honed the cylinders and cleaned up the five good pistons. The re-build
>should be a piece of cake. If you guys remember, I had the EFS-2 crab which
>was too small and replaced it with a EFS-3. After installing the bigger
>crab, I did not get any performance increase and was doing everything
>possible to figure out why. I finally purchased a differential compression
>tester and that revealed the problem. Looking back over my flight records, I
>see where my oil temps went from 190° to 220° back on 4-7-05. I also made a
>notation that two days later, I had an oil temp spike of 260°. These
>temperatures were discussed in depth with very knowledgeable Corvair guys
>and I was assured by them that this was nothing to worry about. Of course I
>worried anyway and made several changes to my oil cooling duct to improve
>the temps. I honestly feel that the damage was done during the flight on
>4-8-05 when the oil spiked to 260°. Since that day, I flew the engine for an
>additional 23.8 hours. Cruise ranged from 135 to 145 mph and climb out on
>take off was 1100fmp all the while basically flying on four cylinders. This
>is a testament of just how strong the Corvair engine is. I am extremely
>excited about getting back in the air with a healthy engine and seeing what
>increase in performance I get. Another point is that I only had one cht
>probe located at the GM stock location between #1 and #3 cylinders on the
>head. I highly recommend getting six probes for mounting under the spark
>plugs with a six way switch to monitor all six cylinders.
>
>Mark Jones (N886MJ)
>Wales, WI  USA
>E-mail me at [email protected]
>Visit my KR-2S CorvAIRCRAFT web site at
>http://mywebpage.netscape.com/n886mj
>
>
>
>
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>
>  
>

-- 
Adrian VE6AFY
Mailto:[email protected]
http://www.spots.ab.ca/~cartera



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