Return-Path: Sender: (Marvin Kaye) To: lml Date: Tue, 03 Dec 2002 13:57:14 -0500 Message-ID: X-Original-Return-Path: Received: from [199.184.251.195] (HELO tsnci.com) by logan.com (CommuniGate Pro SMTP 4.0.2) with SMTP id 1893629 for lml@lancaironline.net; Tue, 03 Dec 2002 13:44:23 -0500 Received: from TSNC#u#DOM-Message_Server by tsnci.com with Novell_GroupWise; Tue, 03 Dec 2002 13:43:02 -0500 X-Original-Message-Id: X-Mailer: Novell GroupWise 5.2 X-Original-Date: Tue, 03 Dec 2002 13:42:50 -0500 From: "Dr. Weinsweig" X-Original-To: lml@lancaironline.net Subject: ivpt garrett engines and fuel capacity Mime-Version: 1.0 Content-Type: text/plain; charset=US-ASCII Content-Transfer-Encoding: quoted-printable Content-Disposition: inline hi all- does anyone have any info/insight into the garrett turbine engine as an = alternative to the walter-?viable option? 40% less fuel burn sounds very = appealing. i actually called garrett this am and talked to a very = friendly/helpful chap who said he would forward me some info but did not = seem overly enthusiastic about using the garrett in this application. he = actually really seemed to like the walter engine calling it a reliable = tractor type of engine. just trying to check out all options. also would be interested in any innovative ways to increase fuel capacity = on the ivpt and any pireps on customer flying ivpt's. thanks, david ivpt dreamin to fly in 2004