Return-Path: Sender: (Marvin Kaye) To: lml Date: Fri, 13 Jun 2003 10:42:28 -0400 Message-ID: X-Original-Return-Path: Received: from mailnw.centurytel.net ([209.206.160.237] verified) by logan.com (CommuniGate Pro SMTP 4.1b8) with ESMTP id 2420869 for lml@lancaironline.net; Fri, 13 Jun 2003 10:31:48 -0400 Received: from downstairs (pppoe-64-91-107-210-rb.gh.centurytel.net [64.91.107.210]) by mailnw.centurytel.net (8.12.9/8.12.9) with SMTP id h5DEVlIw015280 for ; Fri, 13 Jun 2003 07:31:48 -0700 (PDT) From: "Robert Smiley" X-Original-To: "'Lancair Mailing List'" Subject: RE: [LML] O-320 Fuel Flow X-Original-Date: Fri, 13 Jun 2003 07:31:47 -0700 X-Original-Message-ID: <000201c331b8$85ed22c0$927dfea9@downstairs> MIME-Version: 1.0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook CWS, Build 9.0.6604 (9.0.2911.0) Importance: Normal In-Reply-To: X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2727.1300 At sealevel 360 fuel injected engine, full throttle full rich on takeoff I see about 17-18 GPH. You should test your gravity flow with the plane inclined on a hill or on hill and blocks at your climbout angle and do a gravity flow from your tank. You should get about 50% more gravity flow rate than 17-18 gph or about 25-27 gph flow rate. Bob Smiley N94RJ