Hi Joe, Glenn, Patrick and Robin .
Thank you for your comments and just to clarify, I didn't mean to justify
slop, quite the opposite.I have wing tip slop on my aircraft and am not
happy with it.
I also believe that, with the standard parallel bolt system, it is not
possible to eliminate al
: "Martin Pearce"
To:
Subject: KR> RE: re wing tip slop .. Wear mechanism and proposed fix .. long
List-Post: krnet@list.krnet.org
Date: Fri, 20 May 2011 12:13:34 +1000
Thanks to everyone who has chipped in so far with advice and assistance.
This is a bit long, for which my apologies, ..
On 5/20/2011 6:15 AM, Patrick and Robin Russo wrote:
> Now if you have a new and improved design for wing attach fittings, put
> it on the table. Many of us think that there is room for change there.
If I were to make any change to the WAF, and it would be mostly for
those who need to remove and
Wow Martin, after that dissertation I wouldn't dare make a comment! It is
much like saying 2 plus 2 equals 4, does anyone want to refute this or make
comment? My answer remains the same to your original question regarding
wing tip movement. There should be NONE when you have finished installing
Thanks to everyone who has chipped in so far with advice and assistance.
This is a bit long, for which my apologies, ..
Bolt to bolt hole clearance and the effect at the wing tip
As far as I can see, if parallel bolts and bolt holes are used, there has to
be some clearance in order to fit the
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