X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Mon, 14 Nov 2011 07:44:08 -0500 Message-ID: X-Original-Return-Path: Received: from [199.185.220.223] (HELO defout.telus.net) by logan.com (CommuniGate Pro SMTP 5.4.2) with ESMTP id 5198389 for lml@lancaironline.net; Sun, 13 Nov 2011 15:35:03 -0500 Received-SPF: pass receiver=logan.com; client-ip=199.185.220.223; envelope-from=npaczkowski@telus.net Received: from edtncm04 ([199.185.220.240]) by priv-edtnes24.telusplanet.net (InterMail vM.8.01.03.00 201-2260-125-20100507) with ESMTP id <20111113203428.TFJO5031.priv-edtnes24.telusplanet.net@edtncm04> for ; Sun, 13 Nov 2011 13:34:28 -0700 Received: from costcoPC ([23.16.88.25]) by edtncm04 with bizsmtp id wkaU1h00D0YoXan01kaUG9; Sun, 13 Nov 2011 13:34:28 -0700 X-Authority-Analysis: v=1.1 cv=X/gNs4UVylE7+Vx6qGAThGP3nyIFTMv4OpHLIQ+Ovr8= c=1 sm=2 a=LGgl8L9ij00A:10 a=c01CeosAtK_-PLpqiI4A:9 a=CjuIK1q_8ugA:10 a=yMhMjlubAAAA:8 a=SSmOFEACAAAA:8 a=D_A8rQSeQ3nALK3q6fIA:9 a=Tj7KiCMuMDMPrf3kzC4A:7 a=gKO2Hq4RSVkA:10 a=hTZeC7Yk6K0A:10 X-Telus-Outbound-IP: 23.16.88.25 From: "Nicholas Paczkowski" X-Original-To: Subject: Wing root fuel fittings X-Original-Date: Sun, 13 Nov 2011 12:34:29 -0800 X-Original-Message-ID: <000001cca243$a4fbb690$eef323b0$@net> MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0001_01CCA200.96D89DA0" X-Mailer: Microsoft Office Outlook 12.0 Thread-Index: AcyiQ6RfNjeN9B64RUOK7k+sJfSpqg== Content-Language: en-ca This is a multi-part message in MIME format. ------=_NextPart_000_0001_01CCA200.96D89DA0 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit My airplane (under construction) is a non-pressurized IV. My engine is a TSIO 550C. I have installed 1/2" fuel supply lines and 3/8" returns in the fuselage. However, when I built the wing I used the fittings that Lancair supplied in the kit for the wing root which (I believe) were 3/8" for the supply and 1/4" for the return (even though I vented the tanks using 3/8" vent lines.) The wing is finished and pressure tested. Now what do I do? (hoping for a non 'motivation killing' fix.) Thanks Nick Paczkowski ------=_NextPart_000_0001_01CCA200.96D89DA0 Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable

My = airplane (under construction) is a non-pressurized IV. My engine is a = TSIO 550C. I have installed 1/2" fuel supply lines and 3/8" = returns in the fuselage. However, when I built the wing I used the = fittings that Lancair supplied in the kit for the wing root which (I = believe) were 3/8" for the supply and 1/4" for the return = (even though I vented the tanks using 3/8" vent lines.) The wing is = finished and pressure tested. Now what do I do? (hoping for a non = 'motivation killing' fix.) Thanks

 

Nick Paczkowski

 

------=_NextPart_000_0001_01CCA200.96D89DA0--