Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 3.5b3) with ESMTP id 857296 for rob@logan.com; Sat, 25 Aug 2001 23:19:53 -0400 Received: from imo-r04.mx.aol.com ([152.163.225.100]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71866U8000L800S0V35) with ESMTP id com for ; Sat, 25 Aug 2001 22:14:16 -0400 Received: from Klusmanp@aol.com by imo-r04.mx.aol.com (mail_out_v31_r1.4.) id k.bb.12ed0c22 (4365) for ; Sat, 25 Aug 2001 22:24:48 -0400 (EDT) From: Klusmanp@aol.com Message-ID: Date: Sat, 25 Aug 2001 22:24:48 EDT Subject: Weight of airframe components To: lancair.list@olsusa.com MIME-Version: 1.0 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I'm trying to collect data to estimate composite airframe weights. Has anybody out there weighed finished airframe components such as wing, horizontal stab, elevator, rudder? I'm interested in all Lancair models and Glassair as well for any Glassair folks reading this. Perhaps the construction manuals list component weights? Thanks, Paul Klusman >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>