X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Tue, 13 Nov 2012 11:13:13 -0500 Message-ID: X-Original-Return-Path: Received: from cdptpa-omtalb.mail.rr.com ([75.180.132.120] verified) by logan.com (CommuniGate Pro SMTP 6.0c2) with ESMTP id 5875817 for lml@lancaironline.net; Mon, 12 Nov 2012 18:28:35 -0500 Received-SPF: pass receiver=logan.com; client-ip=75.180.132.120; envelope-from=tednoel@cfl.rr.com X-Original-Return-Path: X-Authority-Analysis: v=2.0 cv=KMfY/S5o c=1 sm=0 a=Juz4b5MAAxrvp7e3l7SsjA==:17 a=zv7pOm2hHFMA:10 a=1F-HOIdIGasA:10 a=TEk6DfFevhsA:10 a=05ChyHeVI94A:10 a=ayC55rCoAAAA:8 a=MdQN4CeMQAEA:10 a=Ia-xEzejAAAA:8 a=0KaQcUR7YW3sad6hu4kA:9 a=wPNLvfGTeEIA:10 a=CVU0O5Kb7MsA:10 a=4PR2P7QzAAAA:8 a=FXKzVU9fV9TOmpxxdOYA:9 a=_W_S_7VecoQA:10 a=djSSOgbfo6cA:10 a=0sw4ah1lqe7ysp_2:21 a=Juz4b5MAAxrvp7e3l7SsjA==:117 X-Cloudmark-Score: 0 X-Authenticated-User: X-Originating-IP: 97.101.122.192 Received: from [97.101.122.192] ([97.101.122.192:49465] helo=[127.0.0.1]) by cdptpa-oedge02.mail.rr.com (envelope-from ) (ecelerity 2.2.3.46 r()) with ESMTP id F4/58-01425-00681A05; Mon, 12 Nov 2012 23:28:00 +0000 X-Original-Message-ID: <50A185FD.7060502@cfl.rr.com> X-Original-Date: Mon, 12 Nov 2012 18:27:57 -0500 From: Ted Noel Reply-To: tednoel@cfl.rr.com User-Agent: Mozilla/5.0 (Windows NT 6.1; WOW64; rv:12.0) Gecko/20120428 Thunderbird/12.0.1 MIME-Version: 1.0 X-Original-To: Lancair Mailing List Subject: Re: [LML] Pressurization - IVP References: In-Reply-To: Content-Type: multipart/alternative; boundary="------------080909020000050308050901" This is a multi-part message in MIME format. --------------080909020000050308050901 Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit John, It strikes me that the normal way is to have a fitting that tightly attaches through the pressure vessel. That's a bit difficult at that location. Mine come in in front of the aileron box. Ted Noel On 11/12/2012 2:11 PM, John Barrett wrote: > I'm attempting to button up the pressure vessel in preparation for first > pressurization. These two photos are of boxes to seal off the aft spars > where they enter the cockpit just in front of the rear seat on the floor. > > Any thoughts on a good way to seal off these fuel lines? > > Thanks, > John Barrett > > > The message is ready to be sent with the following file or link attachments: > > IMG_0591 > IMG_0592 > > > Note: To protect against computer viruses, e-mail programs may prevent > sending or receiving certain types of file attachments. Check your e-mail > security settings to determine how attachments are handled. > > > -- > For archives and unsub http://mail.lancaironline.net:81/lists/lml/List.html --------------080909020000050308050901 Content-Type: text/html; charset=ISO-8859-1 Content-Transfer-Encoding: 7bit John,

It strikes me that the normal way is to have a fitting that tightly attaches through the pressure vessel. That's a bit difficult at that location. Mine come in in front of the aileron box.

Ted Noel

On 11/12/2012 2:11 PM, John Barrett wrote:

I'm attempting to button up the pressure vessel in preparation for first
pressurization.  These two photos are of boxes to seal off the aft spars
where they enter the cockpit just in front of the rear seat on the floor.

Any thoughts on a good way to seal off these fuel lines?

Thanks,
John Barrett

    
The message is ready to be sent with the following file or link attachments:

IMG_0591
IMG_0592


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security settings to determine how attachments are handled.

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