Return-Path: Received: from ddi.digital.net ([198.69.104.2]) by truman.olsusa.com (Post.Office MTA v3.1.2 release (PO203-101c) ID# 0-44819U2500L250S0) with ESMTP id AAA9149 for ; Thu, 3 Sep 1998 23:10:24 -0400 Received: from john (max-tnt-45.digital.net [208.14.41.45]) by ddi.digital.net (8.9.0/8.9.0) with SMTP id XAA24765 for ; Thu, 3 Sep 1998 23:09:59 -0400 (EDT) Message-Id: <3.0.3.32.19980903230950.0070b920@mail.digital.net> X-Sender: heyduke@mail.digital.net X-Mailer: QUALCOMM Windows Eudora Pro Version 3.0.3 (32) Date: Thu, 03 Sep 1998 23:09:50 -0400 To: lancair.list@olsusa.com From: John Cooper Subject: L320 Wing Tank Fuel Line Fittings X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Parker-Hannifin makes a "long" elbow that might work. Contact your local hydraulic hose shop for a catalog. You know, the guys that make up hydraulic hoses for tractors and stuff. On my 235, I screwed an AN-823-6D into the outboard wing aluminum piece (which I had to drill out and tap for 3/8"NPT). The 45degree fitting was oriented "up", and I cut out a hole in the BL-50 rib to allow clearance. On the end of the 3/8" soft aluminum tubing I placed a 90deg bend as tight as I could make it. So when it is all hooked up, the gas flows up through the 45degree fitting, then turns aft to the rear spar where another 90 degree bend takes it inboard all the way to the center console. I epoxied a 3/8" bulkhead fitting where the rear spar meets the console on each side (not enough room for a jamb nut), then went forward from there, right along the belly pan and underneath the front spar. My transfer pumps are mounted on the back of the nose gear tunnel. Some people prefer to run the gas line along the forward spar, but I felt that having it run right along underneath my a** was the safest place in the plane . --John