X-Virus-Scanned: clean according to Sophos on Logan.com X-SpamCatcher-Score: 2 [X] Return-Path: Received: from [68.202.132.19] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WEBUSER 5.1.6) with HTTP id 1821470 for lml@lancaironline.net; Wed, 07 Feb 2007 10:44:07 -0500 From: "Marvin Kaye" Subject: Re: [LML] Summary - when to turn on the fuel boost pump To: lml X-Mailer: CommuniGate Pro WebUser v5.1.6 Date: Wed, 07 Feb 2007 10:44:07 -0500 Message-ID: In-Reply-To: <181107.69034.qm@web51007.mail.yahoo.com> References: <181107.69034.qm@web51007.mail.yahoo.com> MIME-Version: 1.0 Content-Type: text/plain;charset="iso-8859-1";format="flowed" Content-Transfer-Encoding: 8bit Posted for Dr Andre Katz : you forgot one more factor in the myriad of answers, the duke's fuel pump is located inside the cockpit, therefore is pressurized, pressurization in a IV-P has a factor in the fuel flow, in my IV-P I believe its the reason for the acute engine power loss when shifting tanks, the only way to avoid it is to go high in the boost prior to switching, if you get a leak in the fuel pump like it occurred to me you loose pressure. This event never happens at low altitude, therefor my small brain tells me it pressure related. One more thing to consider. andres """ John Hafen wrote: I would like to thank all those who responded to my question about when to turn on the fuel boost pump when flying a Lancair IVP. Based on info gleaned from the posts, it appears that the answer is “whenever it is necessary depending on your specific plane.” As some never use their boost pump after engine start, others turn it on for take off, others turn it on at 3k feet or 6k feet or 10k feet or after reaching cruise at 24k feet, it appears that there is no dependably consistent answer that would apply to every plane, even in identical environments (temperature, pressure etc). We are left to figure it out on our own. But at least I know a little bit about why, thanks to your feedback. """