Mailing List lml@lancaironline.net Message #17292
From: <RWolf99@aol.com>
Sender: Marvin Kaye <marv@lancaironline.net>
Subject: LNC2 Nose Gear Drag Link
Date: Thu, 23 Jan 2003 15:13:07 -0500
To: <lml>
"shimming the drag link" -- I had to carefully file my drag link so that it
would fit in between the tabs in the first place!  Maybe mine is installed
ever-so-slightly crooked.  I only took off a few thousandths but that was
required for a friction-free rotation.

Scott -- when I presented aluminum hardware to NASA for flying on the Space
Shuttle in the mid 1980's, they made me remove all of the coarse-threaded
bolts and replace them with fine-threaded bolts using helicoils.  Now if you
ask me, NASA ain't had no rocket scientists for a long time now (OK,OK, Mike
Reinath and Valin Thorn and any other NASA Lancair builders are notable
exceptions) but maybe they know something about this that I don't.  So
fine-threaded bolts in helicoiled aluminum do not worry me.  However, I would
be concerned about only having 1/8 inch of material around the hole.  
Standard engineering formulas often assume material properties for holes in a
semi-infinite sheet -- having such a small edge distance means you have to
analyze it differently.  However, the primary load here is in compression,
not tension, so I don't think the rod end will pull out of the hole.

- Rob Wolf
jaded ex-rocket scientist
Subscribe (FEED) Subscribe (DIGEST) Subscribe (INDEX) Unsubscribe Mail to Listmaster