Concur with Mark.  No need to get concerned about this one folks.  I actually 
did a bad thing and forgot to tighten one, I found it during another 
maintenance check later. Probably flew with the nut loose for a couple hundred 
hours but it didn't make any difference. 


Rob Schmitt




-----Original Message-----
From: Mark Langford via KRnet <krnet at list.krnet.org>
To: KRnet <krnet at list.krnet.org>
Cc: Mark Langford <ml at n56ml.com>
Sent: Sun, Aug 30, 2015 6:00 pm
Subject: Re: KR> Reaming WAFs


Nobody's shown me a torque for KR wing attach fittings.  It's not in the

plans.  Why is that?  Because friction was not even considered in the

analysis of the wing attach joint. It was a pure shear calculation. 
It's
simply a pinned joint, and safe enough on that basis alone.

Although I'm
certainly not advocating anybody do this, you could likely 
fly around with
cottered pins in place of the bolts to keep them from 
sliding out of place,
and you'd be fine.  I'm pretty sure there are 
airplanes and ultralights that
use simple pinned joints.

Sure, torquing the bolts to some reasonable number
is the common-sense 
thing to do, and as Larry pointed out, people do exactly
that. 
Calculating optimal torque for a lubricated fastener and nut is

commendable, but not necessary.

I'm a mechanical engineer, and recognizing
that it's simply a pinned 
joint, I just torqued them by feel and got on with
my business. 
Sure...considering friction would be nice, but the designer
simply can't 
count on these connections being done perfectly, so he designs
them to 
be foolproof, and then add a factor of safety on top of that.  That's

what we're dealing with on these WAFs.  After all, this plane was touted 
as
being buildable with only simple tools...


Mark
Langford
ML at N56ML.com
http://www.n56ml.com



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