Return-Path: Received: from [65.173.216.66] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WebUser 4.1.5) with HTTP id 2636463 for lml@lancaironline.net; Tue, 14 Oct 2003 11:22:19 -0400 From: "Marvin Kaye" Subject: Re: [LML] Re: To supercharge or not to supercharge To: lml X-Mailer: CommuniGate Pro WebUser Interface v.4.1.5 Date: Tue, 14 Oct 2003 11:22:19 -0400 Message-ID: In-Reply-To: MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for rickschrameck : Tim, Dave Morss has already done that test. It is posted on our web site. The claim that Josh made was that the Normalized Legacy can our run the Supercharged Legacy to 12,000 Ft AGL. Turbocharged engines do not typically run 30" of MAP and under except for cruise conditions when they get to altitude, that is why you have them. I will talk to Dave and we will make up a proposed test plan that tests Josh's claims about Normalized Legacy performance. 30" of MAP for a Supercharged engine is just loafing along but we will test that parameter also. This is more fun than talking about EFIS competitors. We get to fly and prove who is right. Rick http://www.aerosuperchargers.com/testimonials.html