Return-Path: Sender: (Marvin Kaye) To: lml@lancaironline.net Date: Mon, 21 Jun 2004 16:30:50 -0400 Message-ID: X-Original-Return-Path: Received: from mta-out-1.udlp.com ([207.109.1.8] verified) by logan.com (CommuniGate Pro SMTP 4.2b6) with ESMTP id 220939 for lml@lancaironline.net; Mon, 21 Jun 2004 13:15:04 -0400 Received: from asdmngwia.mpls.udlp.com (asdmngwia.mpls.udlp.com [10.1.62.22]) by mta-out-1.udlp.com (8.12.10/8.12.10) with ESMTP id i5LFZ9UP021465 for ; Mon, 21 Jun 2004 10:35:09 -0500 Received: from DM-MN-06-MTA by asdmngwia.mpls.udlp.com with Novell_GroupWise; Mon, 21 Jun 2004 12:14:28 -0500 X-Original-Message-Id: X-Mailer: Novell GroupWise Internet Agent 6.0.2 X-Original-Date: Mon, 21 Jun 2004 12:14:25 -0500 From: "Christopher Zavatson" X-Original-To: Subject: CG and Gross Weight Mime-Version: 1.0 Content-Type: text/plain; charset=US-ASCII Content-Transfer-Encoding: quoted-printable Content-Disposition: inline <<4. Does the bigger tail have any effect on CG (the CAFE plane had the extended engine mount and the small tail)?>> You would have to know the weights of the two tails to determine any CG = shift. The big tail is carbon, the small tail is FG. The larger tail = does, however, buy you approx. 1.5 inches of additional aft CG range. The = published CG range remained unchanged, so for the same CG position you end = up with additional stability. Chris Zavatson N91CZ 360 std