Return-Path: Sender: (Marvin Kaye) To: lml Date: Mon, 16 Jun 2003 10:24:09 -0400 Message-ID: X-Original-Return-Path: Received: from www.dynacomm.ws ([198.22.63.66] verified) by logan.com (CommuniGate Pro SMTP 4.1b8) with ESMTP id 2430986 for lml@lancaironline.net; Mon, 16 Jun 2003 10:23:15 -0400 Received: from dynacomm.ws (adsl-66-72-186-247.dsl.sfldmi.ameritech.net [66.72.186.247]) by www.dynacomm.ws (8.10.2/8.10.2) with ESMTP id h5GEMw530078 for ; Mon, 16 Jun 2003 10:22:58 -0400 X-Original-Date: Mon, 16 Jun 2003 10:22:55 -0400 Subject: Re: O-320 Fuel Flow Content-Type: text/plain; charset=US-ASCII; format=flowed Mime-Version: 1.0 (Apple Message framework v552) From: "Lorn H. Olsen" X-Original-To: "Lancair Mailing List" Content-Transfer-Encoding: 7bit In-Reply-To: X-Original-Message-Id: <05952F7A-A006-11D7-AB60-000393C2C1A6@dynacomm.ws> X-Mailer: Apple Mail (2.552) I am going to ask again. Does anyone out there have an O-320? If so, what is the maximum fuel flow that you can get. At takeoff at 1,000 ft, with an EPI 800, I am reading 11.5 to 12.5 gph. I need to know the flow with a carburetor and an EPI 800. TIA, -- Lorn H. 'Feathers' Olsen, MAA, DynaComm, Corp. 248-478-4301, mailto:lorn@dynacomm.ws LNC2, O-320-D1F, N31161, Y47, SE Michigan