Re: Trailering a KitfoxTrailering a Kitfox


Subject:    Re: Trailering a KitfoxTrailering a Kitfox
From:    floran higgins (cliffh@outdrs.net)
Date:    Thu Jan 08 - 11:46 AM
There is a local pilot that trailered an Avid down from Alaska.
He did not use the support tubes from the leading edge spar to the lower 
wing strut attachment.
He completely destroyed the fuselage center section where the rear strut 
attaches.

Floran Higgins
Helena, Mt. 
Speedster
912ULS
  ----- Original Message ----- 
  From: Chuck Popenoe 
  To: kitfox-list@matronics.com 
  Sent: Thursday, January 08, 2009 7:49 AM
  Subject: Re: Trailering a KitfoxTrailering a Kitfox


  Bob-

  I welded up the trailer in my driveway specifically to fit the Avid -- 
it is a single axle with minimal spring stiffness --2 leaves. I live on 
the outskirts of Wash. DC and have to trailer the bird some 50 miles 
each way to Frederick Muni each time I fly to get out of the ADIZ. The 
mains are secured with tire chains and the tailwheel is secured with a 
specially welded up clamp.  I have recently added supports for the 
empennage which fasten iinto the cross tubes for towing on its own 
wheels which takes all of the weight off of the tail spring.  I will 
attach a couple of photos, but the trailer details can best be seen 
posted on the Avid Flyer list under Pops' Avid A.  

  Actually, while trailering, the wingtips are right behind the car's 
rear window, and their movement can be observed easily.  The struts that 
hold the wings in the folded position will keep the wings from swinging 
out, but do little to restrain their up/down movement.  This is why I 
added the struts down to the cross tubes to triangulate that support 
location.  Without the added struts, the tips would move up and down on 
rough roads. Presently, the tips are absolutely fixed and no movement is 
possible.  Other than truck vortices, I have never observed any wind 
generated movement since adding the braces.  

  I haven't used the front spar braces, as I don't think that do much 
with my triangulated wing support taking the load.  My attach point 
failure occurred some 7-8 years ago, and I did a lot of thinking then to 
make changes to prevent it from ever occurring again.

  Pops




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