Return-Path: Sender: (Marvin Kaye) To: lml Date: Mon, 27 Oct 2003 23:40:40 -0500 Message-ID: X-Original-Return-Path: Received: from mxsf11.cluster1.charter.net ([209.225.28.211] verified) by logan.com (CommuniGate Pro SMTP 4.1.6) with ESMTP id 2662056 for lml@lancaironline.net; Mon, 27 Oct 2003 17:06:01 -0500 Received: from computer (cc2-24.217.124.116.charter-stl.com [24.217.124.116]) by mxsf11.cluster1.charter.net (8.12.10/8.12.8) with SMTP id h9RLcseV025572; Mon, 27 Oct 2003 16:38:54 -0500 (EST) (envelope-from bobjude@charter.net) X-Original-Message-ID: <002401c39cd3$217a46c0$747cd918@computer> From: "Bob Jude" X-Original-To: "Gary Fitzgerald" X-Original-Cc: "Mail List Lancair" Subject: 320/360 Flaps X-Original-Date: Mon, 27 Oct 2003 15:41:49 -0600 MIME-Version: 1.0 Content-Type: text/plain; charset="Windows-1252" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2800.1158 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 >1. Even after searching the LML archives, I'm unclear as to whether the fuselage faired position for the flaps is the zero-degree position, or the reflex position The blueprints indicate that the fuselage-faired position is the -7 degrees reflex position, but the manual seems to indicate that the reflex position is with the flap trailing edges above the fuselage fillet. Which is correct? Gary Fitz, Sometimes searching the Lancair Technical Bulletins is more productive than "searching the LML archives". See TB 11 for information on this question. Bob