Return-Path: Received: from tomcat.al.noaa.gov ([140.172.240.2] verified) by logan.com (CommuniGate Pro SMTP 4.2b2) with ESMTP id 3179020 for flyrotary@lancaironline.net; Mon, 19 Apr 2004 13:00:11 -0400 Received: from PILEUS.al.noaa.gov (pileus.al.noaa.gov [140.172.241.195]) by tomcat.al.noaa.gov (8.12.0/8.12.0) with ESMTP id i3JH0BKa029948 for ; Mon, 19 Apr 2004 11:00:11 -0600 (MDT) Message-Id: <5.2.1.1.0.20040419105401.01aaa490@mailsrvr.al.noaa.gov> X-Sender: bdube@mailsrvr.al.noaa.gov X-Mailer: QUALCOMM Windows Eudora Version 5.2.1 Date: Mon, 19 Apr 2004 10:59:15 -0600 To: "Rotary motors in aircraft" From: Bill Dube Subject: Re: [FlyRotary] Engine out In-Reply-To: Mime-Version: 1.0 Content-Type: text/plain; charset="us-ascii"; format=flowed > >I'm now convinced (after about half a dozen such engine outs) that the >constant velocity Mikuni carbs ARE susceptible to icing. All carbs are susceptible to icing. CV carbs are just less susceptible. As long as there is a Venturi there will be reduced pressure (with a concomitant reduced temperature) and thus the possibility of icing. EFI sounds like a wise choice.