X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from elasmtp-spurfowl.atl.sa.earthlink.net ([209.86.89.66] verified) by logan.com (CommuniGate Pro SMTP 6.0.7) with ESMTP id 6651685 for lml@lancaironline.net; Tue, 24 Dec 2013 08:57:15 -0500 Received-SPF: none receiver=logan.com; client-ip=209.86.89.66; envelope-from=colyncase@earthlink.net DomainKey-Signature: a=rsa-sha1; q=dns; c=nofws; s=dk20050327; d=earthlink.net; b=mk7iIOw1SVERkPY0DFvIAzs9xeERL+QxFTYTqJs75hqz0aw78eMC0GD7kQr5pnL0; h=Received:Content-Type:Mime-Version:Subject:From:In-Reply-To:Date:Content-Transfer-Encoding:Message-Id:References:To:X-Mailer:X-ELNK-Trace:X-Originating-IP; Received: from [71.181.111.243] (helo=[192.168.1.24]) by elasmtp-spurfowl.atl.sa.earthlink.net with esmtpa (Exim 4.67) (envelope-from ) id 1VvSTQ-0004Bq-GW for lml@lancaironline.net; Tue, 24 Dec 2013 08:56:40 -0500 Content-Type: text/plain; charset=us-ascii Mime-Version: 1.0 (Apple Message framework v1085) Subject: Re: [LML] [LNC2] Wing Tank Drains From: Colyn Case In-Reply-To: Date: Tue, 24 Dec 2013 08:56:39 -0500 Content-Transfer-Encoding: quoted-printable Message-Id: <457E4F17-6460-455B-9E95-EFFF3B45A255@earthlink.net> References: To: "Lancair Mailing List" X-Mailer: Apple Mail (2.1085) X-ELNK-Trace: 63d5d3452847f8b1d6dd28457998182d7e972de0d01da940b951aaa54c80a6a97105350c83b899e6350badd9bab72f9c350badd9bab72f9c350badd9bab72f9c X-Originating-IP: 71.181.111.243 The approach taken by some is to simply arrange for the fuel pickup to = be higher in the tank than the sump drain. This does lead to a question I hadn't thought about: If the sump drain = is under water when it freezes, how do you get the water/ice out of your = tanks, short of bringing the whole airplane into a warm hangar? On Dec 24, 2013, at 7:45 AM, John Cooper wrote: When building my 235 wing tanks, I was concerned that the drain valve = wasn't located at the lowest part of the tank, possibly allowing water = to accumulate next to the BL-51(?) rib. Here is what the instruction = manual showed: I chose to mount the flush drain exactly in the lowest portion of the = bottom wing skin where there was no foam core. I drilled a hole at the = lowest point then used structural adhesive to glue the aluminum hard = point onto the outside of the bottom wing skin so that the drain holes = in the quick-drain were peeking just above the interior of the tank = sealant. Afterwords, I fiberglassed over the hard point, which I had = previously rounded and beveled. When it came time to finish the = aircraft, I used micro to build up an aerodynamic "blister" to cover the = hard point and quick drain. I probably lost a couple of Potential Knots = of airspeed by sticking the drain out into the wind, but I won't have to = worry so much about un-drainable water in the wing tanks. Speaking of water, we had a recent weather change here in NC from 40-ish = to warm and humid and rainy. The entire aircraft was sweating in the = hangar - not just the engine but the fiberglass airframe as well. I'd = never seen anything like that and I have to assume that under such = conditions, moisture could also build up inside the fuel tanks. It's = something to think about. Here's what my "blister" looks like, and you = can actually see the condensation in the photo: