X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Sun, 08 Jan 2006 23:11:37 -0500 Message-ID: X-Original-Return-Path: Received: from outbound-mail.lax.untd.com ([64.136.28.164] verified) by logan.com (CommuniGate Pro SMTP 5.0.6) with SMTP id 917611 for lml@lancaironline.net; Sun, 08 Jan 2006 12:56:37 -0500 Received-SPF: pass receiver=logan.com; client-ip=64.136.28.164; envelope-from=jkezele@juno.com Received: from webmail44.lax.untd.com (webmail44.lax.untd.com [10.131.27.184]) by smtpout02.lax.untd.com with SMTP id AABB6CWS4ASUNDPS for (sender ); Sun, 8 Jan 2006 09:55:38 -0800 (PST) Received: (from jkezele@juno.com) by webmail44.lax.untd.com (jqueuemail) id LD79KKA3; Sun, 08 Jan 2006 09:54:57 PST Received: from [192.168.0.130] by webmail44.lax.untd.com with HTTP: Sun, 8 Jan 2006 17:54:42 GMT X-Originating-IP: [192.168.0.130] Mime-Version: 1.0 From: "jkezele@juno.com" X-UOL-SENDER: jkezele@juno.com X-Original-Sender: jkezele@juno.com X-Original-Date: Sun, 8 Jan 2006 17:54:42 GMT X-Original-To: lml@lancaironline.net Subject: To header tank or not....that is the question X-Mailer: Webmail Version 4.0 Content-Transfer-Encoding: quoted-printable Content-Disposition: inline Content-Type: text/plain X-Original-Message-Id: <20060108.095457.29358.333201@webmail44.lax.untd.com> X-ContentStamp: 2:2:47122378 X-UNTD-OriginStamp: 9OvJUXd2tUqhLb258iQtPSzy9grzWQikC1ZdFAkeguSVA2kA0qFtxg== X-UNTD-Peer-Info: 10.131.27.184|webmail44.lax.untd.com|webmail44.lax.untd.com|jkezele@juno.com I recently purchase an uncompleted 360 MKII SFB with outback gear and ex= tended engine mount. The previous owner has closed the wings and added = extra fuel bays with slosh valve per Lancair. I now have the option of = not installing the header tank. I have the forward hinge canopy. My or= iginal plans were to omit the header tank, build a bulkhead for the cano= py attachment and utilize the extra space for battery and hydraulic pump= placement. As I understand the 360 with CG's fwd is less likely to hav= e the pilot put himself into a pilot induced oscillation (PIO)in the fla= re. Some have stated that the header fuel system is a simple system and woul= d be easier to plumb for return fuel management, say in the case of the = Delta Hawk engine. Engine weight for the Delta Hawk is comparable to th= e Lycoming IO-360. = The manual refers to utilizing the header tank as forward ballast for CG= purposes and setting the CG forward of the forward limit, thus the CG w= ill move aft as the fuel is burned. Any thought from the experts that have the header system and those that = don't would be helpful. A return system would require a duplex fuel val= ve the is costly, but I don't see that the header system is all that sim= ple to fabricate as well, and what about those facet pumps? Regards John Kezele