Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 3.4.7) with ESMTP id 803725 for rob@logan.com; Tue, 26 Jun 2001 15:10:26 -0400 Received: from mail.arc.nasa.gov ([143.232.48.201]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71175U5500L550S0V35) with ESMTP id com for ; Tue, 26 Jun 2001 10:14:35 -0400 Received: from [128.102.191.43] (reinath.arc.nasa.gov [128.102.191.43]) by mail.arc.nasa.gov (8.9.3/8.9.3) with ESMTP id HAA30020 for ; Tue, 26 Jun 2001 07:22:55 -0700 (PDT) Mime-Version: 1.0 Message-Id: Date: Tue, 26 Jun 2001 07:22:53 -0700 To: lancair.list@olsusa.com From: "Mike S. Reinath" Subject: LNC2 CG Range Content-Type: text/plain; charset="us-ascii" ; format="flowed" X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> The LNC2 Handbook says the cg range is 15 to 29% MAC or 24.5 to 30.3 in. F.S. An article in the Lancair Mail newsletter, 1st quarter issue, 1999, states that Orin and Doug performed flight tests with both the small tail and the MKII tail and found that the forward limit could be moved to 11% MAC. This moves the forward limit forward 4% or 1.65 in. The new range is then 22.9 to 30.3 in. F. S. Has anyone flown their LNC2 with a cg as far forward as 22.9 FS? I just finished my weight and balance, and my worst case forward cg puts me at this limit (low wing fuel, full header, no baggage, no passenger). Thanks for the help. Mike Reinath Std. Build 360 MKII at 99% N3602M >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> 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. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>