I'm in my 6th year flying 6399U with 1 bolt per attach point, been in 
weather bad enough ( windy ) to give you some religion if you had none 
previously. Personnally I prefer 1 bolt per attach point, If 1 bolt shears 
you still have 3 per spar end as opposed to 2. But why are we talking about 
this? If any body ever sheared a bolt in flight I would think that person's 
inclination was to over torque during assembly.

Ken Wiltrout
Ktown, Pa



----- Original Message ----- 
From: "Dan Heath" <[email protected]>
To: <[email protected]>
Sent: Friday, June 09, 2006 8:38 PM
Subject: Re: KR> WAF Bolt Sheer Load


> That seems to be what all the engineers say.  And, I am sure they are
> correct.  I just can't make myself do it that way.  I used 1 per attach
> point on my first KR, and it worked, so I feel comfortable with it.  I 
> think
> it is the thought that if any one of those bolts fail, it is all over.
>
> 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-------
> A better design is to use one long bolt with a
> compression member between the WAF pairs instead of paired short
> bolts, placing the joint in a balance double shear.   This is my
> considered opinion as a professional engineer.
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