Return-Path: Sender: (Marvin Kaye) To: lml Date: Wed, 05 Feb 2003 18:56:06 -0500 Message-ID: X-Original-Return-Path: Received: from [64.4.23.64] (HELO hotmail.com) by logan.com (CommuniGate Pro SMTP 4.0.5) with ESMTP id 2009876 for lml@lancaironline.net; Wed, 05 Feb 2003 10:03:37 -0500 Received: from mail pickup service by hotmail.com with Microsoft SMTPSVC; Wed, 5 Feb 2003 07:03:36 -0800 Received: from 66.137.130.109 by lw15fd.law15.hotmail.msn.com with HTTP; Wed, 05 Feb 2003 15:03:35 GMT X-Originating-IP: [66.137.130.109] From: "Andres Katz" X-Original-To: lml@lancaironline.net X-Original-Bcc: Subject: loss of pressurization IV-P X-Original-Date: Wed, 05 Feb 2003 15:03:35 +0000 Mime-Version: 1.0 Content-Type: text/html X-Original-Message-ID: X-OriginalArrivalTime: 05 Feb 2003 15:03:36.0353 (UTC) FILETIME=[C2177110:01C2CD27]
Without personal experience of a loss of pressurization in my IV after 120 hrs I can only make a comment based on previous accidents. Initially 2-3 lancairs went down with engine stoppage and loss of pressurization following turbo duct separation. Charlie Kohler's manual indicates a process to restart the engine after reaching 12-10K altitude. Loss of pressurization without engine stoppage may indicate partial loss of turbos and not cabin integrity fault. Having flown my 182 turbo for years at 20K and experienced O2 depletion a few times due to incomplete tank filling and connecting hardware I can attest to the ability of the pilot to descend to a more oxygen appropiate environment without declaring an emergency. I will be tempted to make an emergency landing at the closest airport rather than a leisure descent.
andres 18AK


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