Return-Path: Sender: (Marvin Kaye) To: lml Date: Thu, 11 Sep 2003 22:55:26 -0400 Message-ID: X-Original-Return-Path: Received: from imo-m04.mx.aol.com ([64.12.136.7] verified) by logan.com (CommuniGate Pro SMTP 4.1.3) with ESMTP id 2576581 for lml@lancaironline.net; Thu, 11 Sep 2003 22:20:47 -0400 Received: from JLINKJR@aol.com by imo-m04.mx.aol.com (mail_out_v36_r1.1.) id q.16.350026dc (4418) for ; Thu, 11 Sep 2003 22:20:35 -0400 (EDT) From: JLINKJR@aol.com X-Original-Message-ID: <16.350026dc.2c928773@aol.com> X-Original-Date: Thu, 11 Sep 2003 22:20:35 EDT Subject: legacy flaps X-Original-To: lml@lancaironline.net MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="part1_16.350026dc.2c928773_boundary" X-Mailer: 8.0 for Windows sub 6015 --part1_16.350026dc.2c928773_boundary Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit I have fit my flaps on the legacy and the leading edges seem to droop about 1/4" below the trailing edge of the wing when its lined up with the aileron/wingtip. The only thing I can think of is to redrill new holes in the flap for the brackets to make the flap sit higher in the recessed area. A call to lancair said both theirs and a customers that had stopped by were drooped a bit...hmmm...maybe its ok...any ideas? John Link --part1_16.350026dc.2c928773_boundary Content-Type: text/html; charset="US-ASCII" Content-Transfer-Encoding: quoted-printable I have fit my flaps on the legacy and the leading edge= s seem to droop about 1/4" below the trailing edge of the wing when its line= d up with the aileron/wingtip. The only thing I can think of is to redrill n= ew holes in the flap for the brackets to make the flap sit higher in the rec= essed area. A call to lancair said both theirs and a customers that had stop= ped by were drooped a bit...hmmm...maybe its ok...any ideas?

John Link --part1_16.350026dc.2c928773_boundary--