Hi Guys,
I'm tyring to sort out aileron travel. In the construction manual there is a
dwg of the aileron bell crank.
Also in the manual it gives a list of control system travel. The travel of the
aileron is supposed to be + 20 -10 but there seems to be a conflict between
the limits & what y
The suggestion that keeping your oil below a given temperature means it
won't break down just doesn't work with internal combustion and conventional
oils. The overall crankcase oil temperature may never rise above 180
degrees, but small volumes are constantly at much higher temperatures,
partic
Bob
are these extra parts you've accumulated or are you getting out of the KR
business???
Jack
- Bob Glidden wrote:
> Netters
> I have gotten several emails about the parts for sale. If I don't get
> anything serious by this weekend I will start figureing prices for the parts
> and email ev
Netters
I have gotten several emails about the parts for sale. If I don't get anything
serious by this weekend I will start figureing prices for the parts and email
everyone in the order I got them to be fair. But just so you all know, Mark
Langford called me from England within five minutes of
My main axels are 19" back from the center section leading edge and the nose
wheel axel is 22.75" foreword of the center wing LE.
-Joe
> You must have a VW up front.
> george
> pueblo colorado
>
>
> -Original Message-
> From: Joe Beyer
> To: kr...@mylist.net
> Sent: Mon, 30 Mar 2009
you're welcome
Scott Black Beng Aero.
So force on the board is Cd * dyn press * area = 84 lbs
>
I know there has to be a formula out there to figure this and I hope someone
smarter than me can tell me the pounds of force I need to accomplish a
smooth and full deployment to 80 degrees from fuselag
On 03/30/2009 09:55 PM, ROBERT (Jack) COOPER wrote:
> Hooters on Florida Ave.
>
>
Now I wish I were going to Sun-n-Fun! :-)
-Dj
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