Return-Path: Received: from imf22aec.mail.bellsouth.net ([205.152.59.70] verified) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 2901787 for flyrotary@lancaironline.net; Mon, 22 Dec 2003 23:53:43 -0500 Received: from TOSHIBAjhr ([209.214.15.28]) by imf22aec.mail.bellsouth.net (InterMail vM.5.01.06.05 201-253-122-130-105-20030824) with SMTP id <20031223045342.SIYV20397.imf22aec.mail.bellsouth.net@TOSHIBAjhr> for ; Mon, 22 Dec 2003 23:53:42 -0500 From: "John Slade" To: "Rotary motors in aircraft" Subject: RE: [FlyRotary] Re: dual EWP plumbing? Date: Mon, 22 Dec 2003 23:53:41 -0500 Message-ID: MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook IMO, Build 9.0.2416 (9.0.2910.0) X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2800.1165 Importance: Normal In-Reply-To: > If 1 pump fails after achieving cruise altitude (done > with climbing), then you will be well within the "'Nuckols" > envelope of "it isn't critical - you can complete your flight" That's the point I was trying to make. Is this the case with only half the coolant? I suspect that with only half the coolant, and only one core, it might be hard to cool even at cruise. John