Dear Col,
You will find many guys with power plants containing oversize piston kits
and/or extension set ups have had similar problems and been lucky enough to
have a feasible landing place with in the 7-1 glide. Nitrated cranks in non
air specific engines will save your life, as will a dual ignition and a
parachute. Laziness is the killer, that and gravity. I think even Mark
Langford had a crank break plus many others. Get in there and do it so we
can keep talking to you.
Steve Widdicombe.

-----Original Message-----
From: krnet-boun...@mylist.net [mailto:krnet-boun...@mylist.net] On Behalf
Of krnet-requ...@mylist.net
Sent: Wednesday, 18 January 2006 4:01 PM
To: kr...@mylist.net
Subject: KRnet Digest, Vol 348, Issue 26

Send KRnet mailing list submissions to
        kr...@mylist.net

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Today's Topics:

   1. Re:  serious information for Corvair builders (glenda mcelwee)
   2.  Corvair info post (Colin Rainey)
   3.  Carb heat (Serge VIDAL)
   4. RE:  Carb heat (Ron Freiberger)
   5. RE:  update on Flycorvair.com website (Ron Freiberger)
   6. Re:  Corvair info post (Mark Langford)
   7.  Corvair info post (Ronald R.Eason)
   8. RE:  Corvair info post (Ron Freiberger)
   9.  Heat muffs (JIM VANCE)
  10. Re:  Carb heat (Barry Kruyssen)
  11. Re:  Carb heat (Dan Heath)
  12.  Crankshaft Nitriding (Mark Jones)
  13.  Re: CorvAircraft> corvair cranks and track records (Bob Glidden)
  14.  Crankshafts and testing (Colin Rainey)
  15. Re:  Crankshafts and testing (Bob Glidden)
  16.  inexpensive mixture meter (Mark Langford)
  17. Re:  Crankshafts and testing (Kenneth Wiltrout)
  18. Re:  Corvair info post (Mark Langford)
  19.  improved EIS data plot (Mark Langford)
  20.  Come and get it! (Steve Bray)


----------------------------------------------------------------------

Message: 1
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 00:59:37 -0800 (PST)
From: glenda mcelwee <n5...@yahoo.com>
Subject: Re: KR> serious information for Corvair builders
To: KRnet <kr...@mylist.net>
Message-ID: <20060117085937.16903.qm...@web36912.mail.mud.yahoo.com>
Content-Type: text/plain; charset=iso-8859-1

Much of the post from William is a recap of old posts so all the information
is there.  If the information keeps us all safer as we fly it is great news.
To chang out the crank will not take more than a weekend.  It's much cheaper
than maintance AD's on aircraft engines.

  Glenda McElwee

Oscar Zuniga <taildr...@hotmail.com> wrote:
  Those who are building or flying Corvair engines should read William's 
latest technical report on the crankshaft, at 
http://www.flycorvair.com/crankissues.html

It's long and the news isn't great, but if you're planning to fly behind a 
Corvair, better take a look.

Oscar Zuniga
San Antonio, TX
mailto: taildr...@hotmail.com
website at http://www.flysquirrel.net



_______________________________________
Search the KRnet Archives at http://www.maddyhome.com/krsrch/index.jsp
to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
please see other KRnet info at http://www.krnet.org/info.html




---------------------------------
Yahoo! Photos  Showcase holiday pictures in hardcover
 Photo Books. You design it and well bind it!

------------------------------

Message: 2
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 09:45:38 -0500
From: "Colin Rainey" <brokerpilot9...@earthlink.net>
Subject: KR> Corvair info post
To: kr...@mylist.net
Message-ID: <410-220061217144538...@earthlink.net>
Content-Type: text/plain; charset=US-ASCII

Glenda and Oscar
I do not want to sound out of line, and I am obviously not privy to all the
information gathered at the testing site.

However, I find it alittle pre-mature to declare all non-nitrided cranks as
having a problem simply because the only example of that did not have a
crack in it.
Bill Clapp's did not either, but WW's language was such that he was going to
examine it until he found one.  The test appears from a distance to be more
of an attempt to support the need for nitriding, then to prove that it is
truly necessary.  Personally, before I go to the trouble to teardown my
engine, I would 
want to see several more examples of cranks run for similar times like
Bill's and have no damage, while more of the cranks without showing signs.  
To draw the conclusion that nitriding will correct the cracking tendency at
this point is premature.

IMHO for it to be scientific, the test should have been performed with (5)
2700cc cranks nitrided examined, and (5) 2700cc cranks w/o nitriding
examined for similar use engines and those results compared.  The 3100cc
engine is a throw away invalid, because rods and psitons are different which
contaminate the accuracy of the information.  I have nothing against safety
or being cautious, but drawing conclusions this way only means the
possibility of unnecessary work being done on engines, and the real problem
may not have been found.  I do not deny the importance of the testing, but
feel the results lack credibility at this time to draw the conclusions that
they
have.  More factors must be considered in order to properly prevent this
from occurring with other engines.

>From the (4)  2700cc engines, 50% cracked and 50% did not.  Why?  What was
the same about them, and what was different?  
How were they used differently or the same?  What was the fuel type used,
base timing settings, carbs, props, compression ratio?  How were the 2
engines used
that did not crack vs. the 2 that did suffer cracks?  We could all change
out our cranks for billet steel racing cranks and still develop cracks in
them
if the true cause of the cracks is not determined.
Until you establish the control group correctly, you are just guessing....


Colin Rainey
First National Mortgage Sources
Lending Solutions in All 50 States
386-673-6814 office
407-739-0834 cell
brokerpilot9...@earthlink.net

------------------------------

Message: 3
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 16:18:55 +0100
From: Serge VIDAL <serge.vi...@sagem.com>
Subject: KR> Carb heat
To: brokerpilot9...@earthlink.net, KRnet <kr...@mylist.net>
Message-ID:

<of791e54b7.30583c9a-onc12570f9.00528f4f-c12570f9.00542...@sagem.com>
Content-Type: text/plain; charset="us-ascii"

I changed my mind about the design of my carb heat system, after I made a 
Google seach on the subject. I needed to do some research, because 
although I have seen plenty information on how to make a carb air box, I 
could never figure out how to get the hot air source from the exhaust. 
This is why I considered taking air from the cylinders area instead. Well, 
the Google search indicated  a very interesting Web page with plenty 
pictures, and I saw the light. The pictures show a very simple way to make 
a box around an exhaust section by simply folding a sheet of stailess 
steel the fight way: making an octagon or decagon section. Brilliant,, 
simple, effective, and good looking. Oh, by the way,unsurprisingly,  the 
page's author is a guy called Mark Langford.

I will add my contribution to the subject: Mark, you battled to find a 
spring that would fill the box and help with the heat transfer. My 
solution will be to close the box both sides, let the air in through 
plenty little holes. For a spring, I will use stainless steel scrubs (sold 
in France in any convenience store, that are  use to scrub pots and pans), 
and pack them inside the box before I close it.

Serge Vidal
KR2 "Kilimanjaro Cloud"
Paris, France. 

------------------------------

Message: 4
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 11:38:00 -0500
From: "Ron Freiberger" <ronandmar...@earthlink.net>
Subject: RE: KR> Carb heat
To: "'KRnet'" <kr...@mylist.net>
Message-ID: <001201c61b84$65a960b0$6400a8c0@Disorganized>
Content-Type: text/plain;       charset="us-ascii"

Serge said...
Mark, you battled to find a 
spring that would fill the box and help with the heat transfer. My 
solution will be to close the box both sides, let the air in through 
plenty little holes. For a spring, I will use stainless steel scrubs
(sold 
in France in any convenience store, that are  use to scrub pots and
pans), 
and pack them inside the box before I close it.

Serge, I think you're overdoing it... You'll insulate the exhaust pipe
too much, and probably get excessively hot air.  The "screen door spring
is old practice, and should be easy to do.  Stretch it, wrap it, tie
with a bit of stainless safety wire, and go fly.  Most people use
aluminum for the outer wrap, and it's easy to do. 

Ron Freiberger
mail to ronandmar...@earthlink.net 










------------------------------

Message: 5
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 11:41:04 -0500
From: "Ron Freiberger" <ronandmar...@earthlink.net>
Subject: RE: KR> update on Flycorvair.com website
To: "'KRnet'" <kr...@mylist.net>
Message-ID: <001301c61b84$d21ae9d0$6400a8c0@Disorganized>
Content-Type: text/plain;       charset="us-ascii"

What are "others" saying about Oscar's timely posts, other than
"Thanks"?

Ron Freiberger
mail to ronandmar...@earthlink.net 





Thanks Oscar and no matter what others may say regarding your timely
posts, keep it up as some of us don't have the time to constantly check
William's site.
Doug Rupert






------------------------------

Message: 6
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 10:40:21 -0600
From: "Mark Langford" <n5...@hiwaay.net>
Subject: Re: KR> Corvair info post
To: "KRnet" <kr...@mylist.net>
Message-ID: <00ca01c61b84$b66fa180$d004a...@net.tbe.com>
Content-Type: text/plain; format=flowed; charset="iso-8859-1";
        reply-type=original

Colin Rainy wrote:

> IMHO for it to be scientific, the test should have been performed with (5)

> 2700cc cranks nitrided examined, and (5) 2700cc cranks w/o nitriding 
> examined for similar use engines and those results compared.  The 3100cc 
> engine is a throw away invalid, because rods and psitons are different 
> which contaminate the accuracy of the information.
>>From the (4)  2700cc engines, 50% cracked and 50% did not.  Why?  What was

>>the same about them, and what was different?
> How were they used differently or the same?  What was the fuel type used, 
> base timing settings, carbs, props, compression ratio?  How were the 2 
> engines used
> that did not crack vs. the 2 that did suffer cracks?

Having read the comments of engine experts (aircraft, heavy equipment, etc) 
in the field who's first question was "are you sure that crank was nitrided"

(see http://home.hiwaay.net/~langford/corvair/flexplate/problem.html ) is 
all I need to know.  It's considered standard practice in industries in 
which maximum crankshaft longevity is expected.   It's guaranteed insurance 
of significantly more fatigue resistance for the crank.  The reason William 
didn't use 5 cranks of either type is because he doesn't HAVE 5 nitrided 
cranks to check, and it would be irresponsible to sit around waiting for 
them. But seeing 7-8 cracked or broken cranks (most of them in KRs) in the 
last year is enough for any logical thinker to conclude that there is a 
problem that needs fixing, and a $50 nitride job is a pretty good step in 
the right direction.  If he kept quiet on this issue it would just be a 
matter of time before he had a broken crank that didn't just result in a 
forced landing and a trashed engine, but would involve totalled airplanes 
and/or deceased friends...

Mark Langford, Huntsville, Alabama
see KR2S project N56ML at http://home.hiwaay.net/~langford
email to N56ML "at" hiwaay.net 




------------------------------

Message: 7
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 10:54:22 -0600
From: "Ronald R.Eason" <r...@jrl-engineering.com>
Subject: KR> Corvair info post
To: <brokerpilot9...@earthlink.net>,    "'KRnet'" <kr...@mylist.net>
Message-ID: <002f01c61b86$aaa86c90$6501a8c0@CADENGINEERING>
Content-Type: text/plain;       charset="us-ascii"

I have been reading some of these emails with interest from an engineer
stand point and find that flight testing is laborious way to test.

Why not simply test the cranks in a physical lab where gradual eccentric
dynamic loads can be placed on the shafts and record loaded failure?  



Some fan shafts geometries have critical harmonic RPM's that will cause
failure if the shaft rotates at that RPM for extended time periods. The
solution is to stay out of this RPM range i.e. above or below. I think the
problem may be fatigue failure due to critical harmonic loading caused by
the prop. This would require solids modeling the shaft and stress analyzing.



When I worked for John Deere I learned that Deere folks stress relieved all
rotating parts in their engines after each machining operation and nitrating
all bearing assemblies. The process was similar to the one explained at this
web site. http://www.440source.com/crankshafts.htm



Ronald R. Eason Sr.

President / CEO

Ph: 816-468-4091

Fax: 816-468-5465 

http://www.jrl-engineering.com 

Our Attitude Makes The Difference!



-----Original Message-----
From: krnet-boun...@mylist.net [mailto:krnet-boun...@mylist.net] On Behalf
Of Colin Rainey
Sent: Tuesday, January 17, 2006 8:46 AM
To: kr...@mylist.net
Subject: KR> Corvair info post



Glenda and Oscar

I do not want to sound out of line, and I am obviously not privy to all the
information gathered at the testing site.



However, I find it alittle pre-mature to declare all non-nitrided cranks as
having a problem simply because the only example of that did not have a
crack in it.

Bill Clapp's did not either, but WW's language was such that he was going to
examine it until he found one.  The test appears from a distance to be more

of an attempt to support the need for nitriding, then to prove that it is
truly necessary.  Personally, before I go to the trouble to teardown my
engine, I would 

want to see several more examples of cranks run for similar times like
Bill's and have no damage, while more of the cranks without showing signs.  

To draw the conclusion that nitriding will correct the cracking tendency at
this point is premature.



IMHO for it to be scientific, the test should have been performed with (5)
2700cc cranks nitrided examined, and (5) 2700cc cranks w/o nitriding
examined for similar use engines and those results compared.  The 3100cc
engine is a throw away invalid, because rods and psitons are different which
contaminate the accuracy of the information.  I have nothing against safety
or being cautious, but drawing conclusions this way only means the
possibility of unnecessary work being done on engines, and the real problem
may not have been found.  I do not deny the importance of the testing, but
feel the results lack credibility at this time to draw the conclusions that
they

have.  More factors must be considered in order to properly prevent this
from occurring with other engines.



>From the (4)  2700cc engines, 50% cracked and 50% did not.  Why?  What was
the same about them, and what was different?  

How were they used differently or the same?  What was the fuel type used,
base timing settings, carbs, props, compression ratio?  How were the 2
engines used

that did not crack vs. the 2 that did suffer cracks?  We could all change
out our cranks for billet steel racing cranks and still develop cracks in
them

if the true cause of the cracks is not determined.

Until you establish the control group correctly, you are just guessing....





Colin Rainey

First National Mortgage Sources

Lending Solutions in All 50 States

386-673-6814 office

407-739-0834 cell

brokerpilot9...@earthlink.net

_______________________________________

Search the KRnet Archives at http://www.maddyhome.com/krsrch/index.jsp

to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net

please see other KRnet info at http://www.krnet.org/info.html





------------------------------

Message: 8
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 11:59:15 -0500
From: "Ron Freiberger" <ronandmar...@earthlink.net>
Subject: RE: KR> Corvair info post
To: "'KRnet'" <kr...@mylist.net>
Message-ID: <002501c61b87$5c6b5230$6400a8c0@Disorganized>
Content-Type: text/plain;       charset="us-ascii"



Mark, well said.  From my engineering days, I was so frustrated by
Product Assurance types that always wanted to wait for more databefore
accepting the obvious..  Our "experimental " category is supposed to be
a learning process, using past good practices wherever possible.
Nitriding cranks is a perfect example.  I had a Jodel D-11 with and
engine older than I was (that's old).  The new buyer had the crank
ground and polished, (and it'll bet not nitrided).  It failed very
shortly after the "automotive" overhaul, and the aircraft was destroyed
landing in a cornfield.

It would be interesting to know if it's acceptable practice to yellow
tag a reground crankshaft without nitriding.

W Wynne certainly makes a real effort to understand and report.  Thanks,
William.


Ron Freiberger
mail to ronandmar...@earthlink.net 
EAA Tech Counselor #4125

Mark said;

Having read the comments of engine experts (aircraft, heavy equipment,
etc) 
in the field who's first question was "are you sure that crank was
nitrided" 
(see http://home.hiwaay.net/~langford/corvair/flexplate/problem.html )
is 
all I need to know.  It's considered standard practice in industries in 
which maximum crankshaft longevity is expected.   It's guaranteed
insurance 
of significantly more fatigue resistance for the crank.  The reason
William 
didn't use 5 cranks of either type is because he doesn't HAVE 5 nitrided

cranks to check, and it would be irresponsible to sit around waiting for

them. But seeing 7-8 cracked or broken cranks (most of them in KRs) in
the 
last year is enough for any logical thinker to conclude that there is a 
problem that needs fixing, and a $50 nitride job is a pretty good step
in 
the right direction.  If he kept quiet on this issue it would just be a 
matter of time before he had a broken crank that didn't just result in a

forced landing and a trashed engine, but would involve totalled
airplanes 
and/or deceased friends...

Mark Langford, Huntsville, Alabama
see KR2S project N56ML at http://home.hiwaay.net/~langford
email to N56ML "at" hiwaay.net 


_______________________________________
Search the KRnet Archives at http://www.maddyhome.com/krsrch/index.jsp
to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
please see other KRnet info at http://www.krnet.org/info.html





------------------------------

Message: 9
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 14:22:39 -0600
From: "JIM VANCE" <va...@hbcomm.net>
Subject: KR> Heat muffs
To: "krnet" <kr...@mylist.net>
Message-ID: <001601c61ba3$c35e6380$6a88f53f@Vance>
Content-Type: text/plain;       charset="iso-8859-1"

To increase the amount of hot surface area in the heat muff, I used an
ordinary screen door spring.  It was about 18 inches long when I bought it.
I put one end in the vise and stretched it out to about 12 feet.  I then
spiraled it around a piece of one inch o.d. pipe.  I heated it with my
propane torch until the shiny galvanized coating turned gray.  That removed
the temper from the spring.  It was then very easy to wrap around the
exhaust pipe.  I secured it at each end with stainless steel wire.

My heat muffs are tear drop shaped in cross section.  I joined the small
edge with piano hinge.  The heater hose to the carburetor attaches to one
end.  The reason for making the muff easily removable is that it must be
removed for inspection, since it would be a most dangerous place for cracks
to occur.

I have pictures if anyone would be interested.

Jim Vance
va...@hbcomm.net


------------------------------

Message: 10
List-Post: krnet@list.krnet.org
Date: Wed, 18 Jan 2006 07:58:23 +1000
From: "Barry Kruyssen" <k...@bigpond.com>
Subject: Re: KR> Carb heat
To: "KRnet" <kr...@mylist.net>
Message-ID: <00ad01c61bb1$23fe0850$5600a...@technologyonecorp.com>
Content-Type: text/plain;       charset="iso-8859-1"

Hi Serge,

The stainless steel scrubs may break up over time and go through your
engine.

I would stay with the spring idear or just roll stainless wire around dowle
to build your own spring.

regards
Barry Kruyssen
Cairns, Australia
RAA 19-3873 

k...@bigpond.com
http://www.users.bigpond.com/kr2/kr2.htm 



  ----- Original Message ----- 
  I will add my contribution to the subject: Mark, you battled to find a 
  spring that would fill the box and help with the heat transfer. My 
  solution will be to close the box both sides, let the air in through 
  plenty little holes. For a spring, I will use stainless steel scrubs (sold

  in France in any convenience store, that are  use to scrub pots and pans),

  and pack them inside the box before I close it.

  Serge Vidal
  KR2 "Kilimanjaro Cloud"
  Paris, France. 



------------------------------

Message: 11
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 17:56:56 -0500 (Eastern Standard Time)
From: "Dan Heath" <da...@alltel.net>
Subject: Re: KR> Carb heat
To: <kr...@mylist.net>
Message-ID: <43CD7638.000001.03044@DANHOMECOMPUTER>
Content-Type: Text/Plain;  charset="iso-8859-1"

Carb heat for those of you who have not seen it.  A similar way of doing it.

http://krbuilder.org/FirewallForward/index.html 

See N64KR at http://KRBuilder.org - Then click on the pics 
See you in Mt. Vernon - 2006 - KR Gathering
There is a time for building and a time for FLYING and the time for building
is OVER.
Daniel R. Heath - Lexington, SC
-------Original Message-------
I would stay with the spring idear or just roll stainless wire around dowle
to build your own spring.

My solution will be to close the box both sides, let the air in through
plenty little holes. 

------------------------------

Message: 12
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 19:05:10 -0600
From: "Mark Jones" <flyk...@wi.rr.com>
Subject: KR> Crankshaft Nitriding
To: "KR Net" <kr...@mylist.net>, "Corvaircraft"
        <corvaircr...@mylist.net>
Message-ID: <005201c61bcb$3b1cebe0$6401a...@wi.rr.com>
Content-Type: text/plain;       charset="iso-8859-1"

I have quietly sat back and listened to all of you discuss this issue. No
one really knows why or how or anything else, except the facts we have now.
Just keep this in mind.....It is your life that is in most danger coupled
with any passengers you may carry and then there are the people on the
ground you could take out if you go down. But what about your loved ones who
are affected by your loss, losses. You guys and gals are intelligent people.
If you were not, then you could not build an airplane. Why would any of you
take such a risk? Why would you not spend a few extra dollars to make your
plane safer whether it is a Piet or a high performance 250 mph plane. Why
would you not spend a few extra hours on the engine to make it more bullet
proof? Those of you who are taking this seriously and doing the nitriding as
recommended, I applaud you!!!!!!! Those who are ignoring the findings and
are not concerned about nitriding well, may God be with you!!!!!!! And
please don't fly over my house, at least while my family is at home. Kind of
puts it in perspective doesn't it? Personally, I love life and am enjoying
doing what I love to do. When William called and asked for my crank, I had
no plans of nitriding. Thank God I let him talk me into it since mine was
cracked. And by the way, I flew gently those 71 hours and never turned it
over 3150 rpm. Also, thanks to William asking for my crank, I discovered a
faulty harmonic balancer during the teardown which also would have caused a
forced landing. That's two things I am proud to say William saved me from.
Now, the next time I go fly, I will be just that much more confident in my
airplane as being that much safer.

Mark Jones (N886MJ)
Wales, WI  USA 
E-mail me at flyk...@wi.rr.com
Visit my NEW
KR-2S CorvAIRCRAFT web site at www.flykr2s.com




------------------------------

Message: 13
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 20:05:44 -0500
From: "Bob Glidden" <glid...@ccrtc.com>
Subject: KR> Re: CorvAircraft> corvair cranks and track records
To: "KRnet" <kr...@mylist.net>, "Corvair engines for homebuilt
        aircraft" <corvaircr...@mylist.net>
Message-ID: <00cd01c61bcb$4faf08e0$6401a8c0@ADMINISTRATOR>
Content-Type: text/plain; format=flowed; charset="iso-8859-1";
        reply-type=original

If you stop and think about it.WW's opinion is just that.You do not have to 
read his manual or buy conversion parts from him or watch his tapes.Many of 
us choose to listen to him because he doe's a lot of the leg work that we 
don't have time to do(family,church,kids basketball,flying,fly-ins) or what 
ever.$50.00 is pretty cheap insurance,but this is experimental aviation and 
if you don't believe that getting your crank nitrided is necessary,then that

is your opinion.I am not convinced that grinding then under with the wrong 
radius is not more of a factor then the issue of nitiding,but that is my 
opinion and again $50.00 is cheap insurance.I just spent $90.00on a Turn & 
Bank indicator,I could fly without it,but feel better having it....Just my 
thought,I'm glad I was not in Mark Langfords position and found out the hard

way...

Bob Glidden
Eminence,Indiana
KR2S N181FW (building)
Corvair 110
glid...@ccrtc.com 




------------------------------

Message: 14
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 22:02:33 -0500
From: "Colin Rainey" <brokerpilot9...@earthlink.net>
Subject: KR> Crankshafts and testing
To: kr...@mylist.net
Message-ID: <410-2200613183233...@earthlink.net>
Content-Type: text/plain; charset=US-ASCII

Mark and Mark and netters I agree whole heartedly.
And if I find that the cranksahft that WW sold me is NOT nitrided I will
have it nitrided.

What I should have said is that it is premature to draw conclusions that
nitriding will do anything 
to address the broken crankshafts in OUR CASES.  If nitriding is known for
adding durability
to a crank then it is a good thing regardless, I agree.  But I believe there
is ALOT more 
investigating to be done on this issue, then just treat the cranks and
re-install and fly.
That is all I wanted to make clear.  With the volume of knowledge and
numbers of engines
this group has collectively, a collaboration should be able to yield a great
deal of useful
information in this pursuit that all will benefit by, including WW.  I would
like to stimulate
all of us to work together to go beyond where WW is now with this and SOLVE
this 
issue, not wait on him to discover it.

By WW's words himself the problem did not begin until after 2004 when his
version engines began
to become widely used.  What has been changed from the way they were
previously used
in airplanes prior to 2004?  A good starting point for understanding where
the problem is, is to
look at the way the engines were installed and used prior to WW, and compare
to our engines
now.  Then  we know what needs to be tested like Ron Eason suggested, and we
can save 
alot of time and energy, and money.  Like Ron said, maybe the way Bill Clapp
and Steve
Makish flew their engines has much more of a factor on the cracks then the
machining.  Yes
we all could benefit from better cranks, but we should not stop there.  We
need to find out for 
sure why these crankshafts are/were cracked.

That is my main point, take it for what it is worth...


Colin Rainey
First National Mortgage Sources
Lending Solutions in All 50 States
386-673-6814 office
407-739-0834 cell
brokerpilot9...@earthlink.net

------------------------------

Message: 15
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 22:08:31 -0500
From: "Bob Glidden" <glid...@ccrtc.com>
Subject: Re: KR> Crankshafts and testing
To: <brokerpilot9...@earthlink.net>,    "KRnet" <kr...@mylist.net>
Message-ID: <013a01c61bdc$7632e5c0$6401a8c0@ADMINISTRATOR>
Content-Type: text/plain; format=flowed; charset="iso-8859-1";
        reply-type=original


Bob Glidden
Eminence,Indiana
KR2S N181FW (building)
Corvair 110
glid...@ccrtc.com



  Like Ron said, maybe the way Bill Clapp and Steve
> Makish flew their engines has much more of a factor on the cracks then the

> machining.

I don't know about Steve,but I have seen Bill fly several times and he gets 
his moneys worth out of that corvair. 




------------------------------

Message: 16
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 21:12:39 -0600
From: "Mark Langford" <n5...@hiwaay.net>
Subject: KR> inexpensive mixture meter
To: "Corvair engines for homebuilt aircraft"
        <corvaircr...@mylist.net>,      "KRnet" <kr...@mylist.net>
Message-ID: <004201c61bdd$0a22c110$2802a8c0@2600xp>
Content-Type: text/plain; format=flowed; charset="iso-8859-1";
        reply-type=original

NetHeads,

I've been flying with an inexpensive mixture meter for 120 hours now, so I 
guess you could call it "flight tested".  I consider this thing to be 
indispensible, so I figured some of you guys might appreciate it too.  I 
really can't imagine flying without it.  See 
http://home.hiwaay.net/~langford/corvair/o2meter/ for details.

I have my GPS programmed for Fall Creek Falls State Park, Tennessee. 
Tomorrow afternoon I plan to turn a 3 hour drive into a half hour flight 
over some really cool waterfalls in the Tennessee mountains...

Mark Langford, Harvest, AL
see homebuilt airplane at http://www.N56ML.com
email to N56ML "at" hiwaay.net






------------------------------

Message: 17
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 22:18:44 -0500
From: "Kenneth Wiltrout" <kwiltrout1...@verizon.net>
Subject: Re: KR> Crankshafts and testing
To: "KRnet" <kr...@mylist.net>
Message-ID: <000601c61bdd$e3def540$2f01a8c0@gatewayzk8r233>
Content-Type: text/plain; format=flowed; charset="iso-8859-1";
        reply-type=original

I've always wondered why some pilots with a VW that is designed to fly at 
3200 rpm cruise it well beyond that. The same can be said for Vairs as well.

Over rev any engine for an extended period of time and your flirting with 
disaster. My honest cruise at 3200 is 140 mph, if I wanna stretch the truth 
and tell people it cruises close to 150 then I should tell them I'm running 
it WOT as well.


----- Original Message ----- 
From: "Bob Glidden" <glid...@ccrtc.com>
To: <brokerpilot9...@earthlink.net>; "KRnet" <kr...@mylist.net>
Sent: Tuesday, January 17, 2006 10:08 PM
Subject: Re: KR> Crankshafts and testing


>
> Bob Glidden
> Eminence,Indiana
> KR2S N181FW (building)
> Corvair 110
> glid...@ccrtc.com
>
>
>
>  Like Ron said, maybe the way Bill Clapp and Steve
>> Makish flew their engines has much more of a factor on the cracks then 
>> the
>> machining.
>
> I don't know about Steve,but I have seen Bill fly several times and he 
> gets
> his moneys worth out of that corvair.
>
>
> _______________________________________
> Search the KRnet Archives at http://www.maddyhome.com/krsrch/index.jsp
> to UNsubscribe from KRnet, send a message to krnet-le...@mylist.net
> please see other KRnet info at http://www.krnet.org/info.html
> 





------------------------------

Message: 18
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 21:42:37 -0600
From: "Mark Langford" <n5...@hiwaay.net>
Subject: Re: KR> Corvair info post
To: "KRnet" <kr...@mylist.net>
Message-ID: <008101c61be1$39be4440$2802a8c0@2600xp>
Content-Type: text/plain; format=flowed; charset="iso-8859-1";
        reply-type=original

Ron Eason wrote:

>I have been reading some of these emails with interest from an engineer
> stand point and find that flight testing is laborious way to test.
> Why not simply test the cranks in a physical lab where gradual eccentric
> dynamic loads can be placed on the shafts and record loaded failure?

Do you have any idea how expensive this "simple test" would be?  And it 
still would not come close to  replicating the real-world environment of an 
airplane in flight.

> Some fan shafts geometries have critical harmonic RPM's that will cause
> failure if the shaft rotates at that RPM for extended time periods. The
> solution is to stay out of this RPM range i.e. above or below. I think the
> problem may be fatigue failure due to critical harmonic loading caused by
> the prop. This would require solids modeling the shaft and stress 
> analyzing.

I'm a CAD kinda guy, and use solid modeling to solve a lot of my problems 
before they ever crop up.   We even solid modeled our house before we built 
it....but solid modeling a crankshaft and replicating the dynamic forces and

their reactions on an entire engine/propeller system installed on an 
airplane are two different things.  In my view, engines are simply too 
complicated to model  all of the complex dynamics of all the reciprocating 
and rotating parts, at least with software mere mortals can afford (even 
Nastran/Patran).  We have Nastran/Patran at work, and if I thought there was

a prayer of getting useful info out of it, I'd have done it already.  Ford 
and GM may have something like that, but even those guys have to do real 
world testing on a new engine and test and fine tune it after prototyping...

Mark Langford, Harvest, AL
see homebuilt airplane at http://www.N56ML.com
email to N56ML "at" hiwaay.net




------------------------------

Message: 19
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 21:55:23 -0600
From: "Mark Langford" <n5...@hiwaay.net>
Subject: KR> improved EIS data plot
To: "KRnet" <kr...@mylist.net>
Message-ID: <000701c61be3$03653b90$2802a8c0@2600xp>
Content-Type: text/plain; format=flowed; charset="iso-8859-1";
        reply-type=original

Now that Bob Lee has educated me on Excel 2 axis plotting, I've managed to 
make the recent trip's EIS data make a little more sense.  See 
http://home.hiwaay.net/~langford/flights/jan2006farm/ for a new plot that is

easier to read (maybe), or at least has more information on it...

Mark Langford, Harvest, AL
see homebuilt airplane at http://www.N56ML.com
email to N56ML "at" hiwaay.net






------------------------------

Message: 20
List-Post: krnet@list.krnet.org
Date: Tue, 17 Jan 2006 22:01:46 -0600
From: "Steve Bray" <rsb...@hotmail.com>
Subject: KR> Come and get it!
To: kr...@mylist.net
Message-ID: <bay13-f116de8dce8b6fa521a2dc8c6...@phx.gbl>
Content-Type: text/plain; charset="us-ascii"



-------------- next part --------------
---------- Forwarded message ----------
From: clyde hubbart <chubb...@mshs.org>
List-Post: krnet@list.krnet.org
Date: Jan 9, 2006 9:15 AM
Subject: Come and get it!
To: rsb...@gmail.com

Steve, I may have already sent this by mistake before I was finished
with it, so please bear with me(I HATE COMPUTERS)

Hi Steve,

   We had our monthly EAA meeting yesterday, thought I would take a
minute and update you to what is going on around here. We decided to
continue our regular meetings the second Sunday of each month at 2pm and
starting this month we are going to have another informal meeting at
noon the last Saturday of each month. For those that driving in we are
located 5 miles east of the Jonesboro airport (JBR) on highway 18, for
those flying in the GPS cord. are N35 49.49', W90 32.90', please monitor
and use 122.9 for our traffic. Our airstrip is ? mile grass north/south
orientation.

   Now here is the point of interest for you and all of your friends and
their buddies. We will be cooking lunch, nothing fancy, just hamburgers,
hot dogs, brats, and polish sausage with all the trimmings and drink for
$5.00 a head, all you can eat. If you fly-in to the meeting the PILOT
EATS FREE, no dual piloted aircraft please. We have decided to do this
to see if we can spark an interaction between chapters, friends or just
plain flyers of any type of aircraft. You do not have to be an EAA
member or a member of Chapter 437 to attend, EVERYONE IS WELCOME, if you
like airplanes come eat with us.

  Please spread this around, yours truly will be the chef of this
extravaganza, so don't make me do all this cooking for nothing.

Clyde
ps. Please send this to anyone you might think would be interested, I
personally would love to have to send the chapter president back to the
store because we don't have enough food.


------------------------------

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