Return-Path: Received: from [144.54.3.2] (HELO picker.com) by logan.com (CommuniGate Pro SMTP 3.4.3) with ESMTP id 734942 for lancair.list@logan.com; Fri, 06 Apr 2001 20:17:03 -0400 Received: from by picker.com (CommuniGate Pro RULES 3.3b1) with RULES id 3657966; Fri, 06 Apr 2001 20:16:59 -0400 X-Autogenerated: Mirror X-Mirrored-by: Received: from [144.54.37.11] (HELO ct.picker.com) by picker.com (CommuniGate Pro SMTP 3.3b1) with ESMTP id 3657964 for rob@med.marconi.com; Fri, 06 Apr 2001 20:16:55 -0400 Received: from picker.com (central.picker.com [144.54.3.2]) by ct.picker.com (8.9.1/8.9.1) with ESMTP id UAA24692 for ; Fri, 6 Apr 2001 20:16:59 -0400 (EDT) Received: from pop3.olsusa.com ([63.150.212.2] verified) by picker.com (CommuniGate Pro SMTP 3.3b1) with ESMTP id 3657958 for rob@ct.picker.com; Fri, 06 Apr 2001 20:16:50 -0400 Received: from mclean.mail.mindspring.net ([207.69.200.57]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71175U5500L550S0V35) with ESMTP id com for ; Fri, 6 Apr 2001 20:05:53 -0400 Received: from t3g3m5 (user-v3qs4md.dialup.mindspring.com [199.174.18.205]) by mclean.mail.mindspring.net (8.9.3/8.8.5) with SMTP id UAA16680 for ; Fri, 6 Apr 2001 20:11:39 -0400 (EDT) Message-ID: <001701c0bef8$3fb57f80$cd12aec7@t3g3m5> From: "Jeremy F Fisher" To: "Lancair List" Subject: 360 Flaps Date: Fri, 6 Apr 2001 19:18:18 -0500 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I am looking for some advice for a problem that I have with the Outback flap system on my 360. The flaps are built and fitted with the cross shaft (torque tube) and motor. However the fit is extremely tight, since the fast build structure does not match the plans. The rear spar is about one inch aft of the position on the plans, and the result is that there is virtually no clearance for the flap mechanism. From a brief conversation with Lancair, I gather that this is pretty standard, and most people have this problem. The new problem is that the flaps do not travel symmetrically. The port flap travel is about 1.5 inches greater measured at the trailing edge than the starboard flap over the full range from 5/8" up to 8.75" down. There is no obvious reason, but the tight clearance, and some asymmetry in the left and right fuselage mouldings, make it difficult to assess. I need to find a way to eliminate this differential. I can only see two solutions. The obvious one is to drill a new pivot hole in the torque tube crank on the port side to reduce its throw; however this will be difficult without running into the existing hole. The other is to move the attachment bracket that is fitted to the inboard rib on the port flap to the rear (or the starboard bracket forward). This is the bracket that retains the pushrod going to the torque tube crank. I could do this by using a 1/4" phenolic spacer under the bracket, bolting the spacer to the flap mounting holes, and the bracket to the spacer through new holes. Has anyone got a better idea? I am very conscious of the stress on this mechanism in flight, and do not want to create a bigger problem in the future. Jerry Fisher >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> 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. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>