Return-Path: Sender: (Marvin Kaye) To: flyrotary Date: Fri, 04 Oct 2002 00:24:02 -0400 Message-ID: X-Original-Return-Path: Received: from mtiwmhc23.worldnet.att.net ([204.127.131.48] verified) by logan.com (CommuniGate Pro SMTP 4.0b8) with ESMTP id 1797516 for flyrotary@lancaironline.net; Fri, 04 Oct 2002 00:18:58 -0400 Received: from unknown ([12.86.89.54]) by mtiwmhc23.worldnet.att.net (InterMail vM.4.01.03.27 201-229-121-127-20010626) with SMTP id <20021004041858.LNUZ28665.mtiwmhc23.worldnet.att.net@unknown> for ; Fri, 4 Oct 2002 04:18:58 +0000 X-Original-Message-ID: <003101c26b5d$9ba975e0$3659560c@unknown> From: "Michael D. Callahan" X-Original-To: "Rotary motors in aircraft" References: Subject: Re: [FlyRotary] Re: turbo sizing common sense..... X-Original-Date: Thu, 3 Oct 2002 23:22:09 -0500 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 5.00.2314.1300 X-MimeOLE: Produced By Microsoft MimeOLE V5.00.2314.1300 >For me, it's a stock turbo, or nothing. The price of aftermarket turbos is exorbitant, and I really don't need the power. If I can do some normalizing for dirt cheap, I will, otherwise, I'll skip it. If you just normalize, I would imagine you should be OK up to a pretty reasonable altitude. Mike C.