Return-Path: Received: from portal.udlp.com ([207.109.1.80]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Wed, 1 Mar 2000 10:34:25 -0500 Received: from portal.udlp.com (root@localhost) by portal.udlp.com with ESMTP id JAA01435 for ; Wed, 1 Mar 2000 09:39:55 -0600 (CST) Received: from ccmail.udlp.com ([10.1.6.254]) by portal.udlp.com with ESMTP id JAA01416 for ; Wed, 1 Mar 2000 09:39:54 -0600 (CST) Received: from ccMail by ccmail.udlp.com (IMA Internet Exchange 3.13) id 0004B8A8; Wed, 1 Mar 2000 09:36:25 -0600 From: CHRISTOPHER_ZAVATSON@udlp.com Date: Wed, 1 Mar 2000 07:29:16 -0600 Message-ID: <0004B8A8.C21254@udlp.com> Subject: Modified MS20001P hinge To: Lancair.list@olsusa.com X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Gary Hall is the source of the hinge pin kits. (garyhall@ix.netcom.com, 954-971-9731) Both of my ailerons used to vibrate as the fuel level would drop in the wing tanks. The ID had opened up several 1/1000th (can't remember the number) after 250 hours of use. On one aileron I replace the entire hinge and on the other only the pin. Now neither aileron vibrates and after 150 additional hours, I cannot detect any further wear. Even if there is wear and future maintenance becomes necessary, the Teflon is now the sacrificial element and this is immensely easier to replace than an entire hinge. Is it weaker? Of course it is. But reducing a safety factor from 30 to 15 has no bearing on the structure other than saving weight. Given the hinge pin material used in this mod, it would take about 14,000 lb of pull on the aileron to shear the pin. It's not an issue. Chris Zavatson 360 N91CZ >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>