Return-Path: Received: from mail.arc.nasa.gov ([143.232.48.201]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Tue, 26 Sep 2000 10:33:23 -0400 Received: from [128.102.191.43] (reinath.arc.nasa.gov [128.102.191.43]) by mail.arc.nasa.gov (8.9.3/8.9.3) with ESMTP id HAA20012 for ; Tue, 26 Sep 2000 07:38:29 -0700 (PDT) Message-Id: Date: Tue, 26 Sep 2000 07:38:28 -0700 To: lancair.list@olsusa.com From: "Mike S. Reinath" Subject: VMS Fuel Flow Transducer Location X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I need a little advice in picking a good location for my VMS fuel flow transducer. For a fuel injected engine, the VMS manual says to mount it between the fuel control unit and the flow divider. I would prefer to mount mine between the gascolator and the engine-driven fuel pump instead. The pressure might be lower at this location, but the fuel flow will be the same, since I have no bypass pluming that returns fuel to the tank. Does anyone see a problem with this location? Mike Reinath Std. build 360 MkII 90% N3602M >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>