Return-Path: Sender: (Marvin Kaye) To: lml@lancaironline.net Date: Wed, 31 Dec 2003 12:26:04 -0500 Message-ID: X-Original-Return-Path: Received: from mxsf07.cluster1.charter.net ([209.225.28.207] verified) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 2912137 for lml@lancaironline.net; Wed, 31 Dec 2003 10:45:02 -0500 Received: from fisher3p813qd9 (c68.113.193.164.ts46v-12.ftwrth.tx.charter.com [68.113.193.164] (may be forged)) by mxsf07.cluster1.charter.net (8.12.10/8.12.8) with SMTP id hBVFirXi030490 for ; Wed, 31 Dec 2003 10:44:55 -0500 (EST) (envelope-from jerryfisher@charter.net) From: "Jerry Fisher" X-Original-To: "Lancair Mailing List" Subject: Engine and Prop Weight X-Original-Date: Wed, 31 Dec 2003 09:40:20 -0600 X-Original-Message-ID: MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook IMO, Build 9.0.2416 (9.0.2910.0) X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 Importance: Normal I am trying to calculate the CG for my Mk II aircraft with some non-standard components in the engine bay, and need a starting point for the standard fit. Does anyone have an accurate weight for the Lycoming 320 or 360 engine with all of the attachments (alternator, starter, mags etc)? Similarly do you have the weight of the "standard" constant speed prop, e.g. the Hartzell 2 or 3 blade unit? It will make the calculations a lot easier,not to say more accurate. Thanks. Jerry