Return-Path: Sender: (Marvin Kaye) To: lml Date: Mon, 23 Sep 2002 23:35:53 -0400 Message-ID: X-Original-Return-Path: Received: from smtprelay2.dc3.adelphia.net ([24.50.78.5] verified) by logan.com (CommuniGate Pro SMTP 4.0b8) with ESMTP id 1750983 for lml@lancaironline.net; Mon, 23 Sep 2002 23:10:49 -0400 Received: from worldwinds ([207.175.254.66]) by smtprelay2.dc3.adelphia.net (Netscape Messaging Server 4.15) with SMTP id H2XA5V01.12J for ; Mon, 23 Sep 2002 23:10:44 -0400 From: "Gary Casey" X-Original-To: "lancair list" Subject: vent check valves X-Original-Date: Mon, 23 Sep 2002 20:08:40 -0700 X-Original-Message-ID: MIME-Version: 1.0 Content-Type: text/plain; charset="Windows-1252" 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) Importance: Normal X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2600.0000 <> I thought the whole deal with the check valves was to add a second vent in parallel with the first one. The second would presumably be vented to a space probably at a lower pressure - such as inside the wingtip. Then if the first vent plugged the second would at least allow air to vent inward, preventing fuel starvation. Yes, I suppose if you had a plugged primary vent the tank could still overpressure at high altitude. Cessnas, I believe, have a check valve in the fuel cap for that purpose. I thought that certificated planes had to have a redundant fuel tank vent capability. No? Gary Casey ES project