Return-Path: Received: from smtp4.gateway.net ([208.230.117.248]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Sat, 3 Jun 2000 20:06:15 -0400 Received: from oemcomputer (1Cust208.tnt1.coeur-dalene.id.da.uu.net [63.27.107.208]) by smtp4.gateway.net (8.9.3/8.9.3) with SMTP id UAA05302 for ; Sat, 3 Jun 2000 20:12:15 -0400 (EDT) Message-ID: <002501bfcdba$b27fe300$d06b1b3f@oemcomputer> Reply-To: "dfs" From: "dfs" To: "Lancair List" Subject: 235 aileron pivot pins Date: Sat, 3 Jun 2000 17:20:31 -0700 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> To all 235'ers who have the original top-surface hinged flaps. Meant to post this earlier following my annual inspection but got distracted by my recent hydro cylinder problem (since solved). While inspecting the inboard flap pivot pins, the ones made from a 1/4 inch bolt and that engage the hole in the phenolic plates just inside the fuselage, I found that the jam-nut had come off and was lying on the floor. The pin was still in the aileron weldment and still engaged in the phenolic plate, but it was obviously not doing much to react the push-rod forces. When I installed the pivot pin, I used a lock washer and blue Loctite. How it came loose is beyond me but come loose, and even fall off, it did. Suggest you all take a look at yours to be sure all's well in there. The fact that the nut fell off, but the pin stayed in might be easy to miss on a cursory look. Cheers, Dan Schaefer >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>