Return-Path: Received: from ace.cnl.com.au ([203.16.135.34]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Sat, 26 Aug 2000 11:51:39 -0400 Received: from cob-1098.cnl.com.au (default) [203.21.78.226] by ace.cnl.com.au with smtp (Exim 1.92 #1) id 13SiLU-0007h0-00 (Debian); Sun, 27 Aug 2000 01:58:12 +1000 Message-ID: <000901c00f7e$e0823720$e24e15cb@default> From: "rob wallace" To: Subject: fast build flaps iv-p Date: Sun, 27 Aug 2000 02:58:31 +1000 X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Hi, we have a question for everyone out there hoping that someone has a suggestion. We are in the final assembly and rigging stage of a fast build IV-P in Yarrawonga Victoria Australia. We have a problem with the right flap outboard end. That end is sitting 3/16 of an inch higher than the top wing skin with the flap in the fully retracted position. The trailing edge appears okay but we are not sure. Lancair has said that this is a cosmetic problem but aerodynamically it is okay. But we do not want to leave it like this. Lancair sent us another outboard flaptrack, which we redrilled to lower the leading edge of the flap whilst maintaining the trailing edge profile. However, because of the rotation that this caused the geometery of the flap actuating mechanism was upset. It appears to us that the setting up in the out of alignment during the fastbuild. We trust that the trailing edge of the flap was aligned because we have aligned the rest of the wing to it (ailerons, winglets and fairings). The bell cranks are aligned correctly because the system works properly until we move the leading edge to the flush position with the adjusted flaptrack. Does anybody have any thoughts? At this stage the options we have come up with: 1) remove wing and rejig to install 2 new flaptracks. or 2) modify the outboard flaptrack roller bracket to lower the leading edge, however we are concerned that this may put a twist through the flap to the inboard backet. We would be grateful for any input, as we are due to test fly soon. Regards Robert Wallace Yarrawonga Lancair Syndicate >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> 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. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>