Return-Path: Sender: (Marvin Kaye) To: lml Date: Fri, 13 Jun 2003 10:23:06 -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 2420809 for lml@lancaironline.net; Fri, 13 Jun 2003 09:10:45 -0400 Received: from dynacomm.ws (adsl-66-72-182-80.dsl.sfldmi.ameritech.net [66.72.182.80]) by www.dynacomm.ws (8.10.2/8.10.2) with ESMTP id h5DDAh524731 for ; Fri, 13 Jun 2003 09:10:44 -0400 X-Original-Date: Fri, 13 Jun 2003 09:10:41 -0400 Mime-Version: 1.0 (Apple Message framework v552) Content-Type: text/plain; charset=US-ASCII; format=flowed Subject: O-320 Fuel Flow From: "Lorn H. Olsen" X-Original-To: Lancair List Content-Transfer-Encoding: 7bit X-Original-Message-Id: <6EF0C9B1-9DA0-11D7-9DF5-000393C2C1A6@dynacomm.ws> X-Mailer: Apple Mail (2.552) As I am getting my plane back to full flight status, I have a question. For anyone with a carbureted O-320-D1F engine with standard Slick magnetos. What is your takeoff fuel flow? At what altitude? At what temperature? In other words, what does the fuel flow meter read as the 100% fuel flow at full rich? -- Lorn H. 'Feathers' Olsen, MAA, DynaComm, Corp. 248-478-4301, mailto:lorn@dynacomm.ws LNC2, O-320-D1F, N31161, Y47, SE Michigan