Return-Path: Received: from marvkaye.olsusa.com ([205.245.9.98]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with SMTP id com for ; Fri, 23 Apr 1999 22:10:32 -0400 Message-Id: <3.0.3.32.19990423221343.00a0ea40@olsusa.com> Date: Fri, 23 Apr 1999 22:13:43 -0400 To: lancair.list@olsusa.com From: Marvin Kaye Subject: Hydraulic manifold X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> ACS sells some AL manifolds that I thought would be perfect for the hydraulic system on my airplane... I was very surprised to see that they limit the pressure on these units to 150psi, which obviously obviates their use in this system. Since I don't know what alloy they're made of, or their actual dimensions, I can see no reason to question their recommendation and court potential disaster. My question is this... can anyone out there see any reason why I can't manufacture my own manifolds out of a piece of 1x1x3" 6061T6 with five 1/8NPT ports (one in the end and 4 cross-drilled and tapped)? The wall thickness at any port would far exceed the wall thickness of either the AL tubing which is being used, or even the AN fittings which tie everything together, and I would think that it should be more than capable of withstanding 1000psi, as that's not all that much pressure. What say you? >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html