Return-Path: Received: from [206.46.252.46] (HELO vms046pub.verizon.net) by logan.com (CommuniGate Pro SMTP 4.3c3) with ESMTP id 813678 for flyrotary@lancaironline.net; Mon, 21 Mar 2005 09:57:08 -0500 Received: from verizon.net ([71.99.155.4]) by vms046.mailsrvcs.net (Sun Java System Messaging Server 6.2 HotFix 0.04 (built Dec 24 2004)) with ESMTPA id <0IDP00DW0IUX2BY3@vms046.mailsrvcs.net> for flyrotary@lancaironline.net; Mon, 21 Mar 2005 08:57:04 -0600 (CST) Date: Mon, 21 Mar 2005 09:56:51 -0500 From: Finn Lassen Subject: Re: [FlyRotary] Fuel pump question In-reply-to: To: Rotary motors in aircraft Message-id: <423EE0B3.6010100@verizon.net> MIME-version: 1.0 Content-type: text/plain; charset=us-ascii; format=flowed Content-transfer-encoding: 7bit X-Accept-Language: en-us, en References: User-Agent: Mozilla/5.0 (Windows; U; Windows NT 5.1; en-US; rv:1.4) Gecko/20030624 Netscape/7.1 (ax; PROMO) Not a valid test. As you descend for landing things cool down rapidly. Suggest tapeing a cheap temp probe to the pump housing. (Link a Radio Shack in/out door thermometer.) Finn (finally getting fed up enough to move filter and flow sensor to after the pumps.) John Slade wrote: > I checked the pump after a flight and it was >quite cool. >