Return-Path: Sender: (Marvin Kaye) To: lml Date: Thu, 23 Jan 2003 15:13:07 -0500 Message-ID: X-Original-Return-Path: Received: from imo-r03.mx.aol.com ([152.163.225.99] verified) by logan.com (CommuniGate Pro SMTP 4.0.5) with ESMTP id 1995975 for lml@lancaironline.net; Thu, 23 Jan 2003 15:01:28 -0500 Received: from RWolf99@aol.com by imo-r03.mx.aol.com (mail_out_v34.13.) id q.2b.36bd4875 (25305) for ; Thu, 23 Jan 2003 15:01:25 -0500 (EST) From: RWolf99@aol.com X-Original-Message-ID: <2b.36bd4875.2b61a415@aol.com> X-Original-Date: Thu, 23 Jan 2003 15:01:25 EST Subject: LNC2 Nose Gear Drag Link X-Original-To: lml@lancaironline.net MIME-Version: 1.0 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit X-Mailer: AOL 5.0 for Windows sub 108 "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