Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 3.5b8) with ESMTP id 954450 for rob@logan.com; Wed, 14 Nov 2001 16:55:19 -0500 Received: from sfo.erg.sri.com ([128.18.4.100]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71866U8000L800S0V35) with ESMTP id com for ; Wed, 14 Nov 2001 15:08:46 -0500 Received: from thomasl (thomas-l.erg.sri.com [128.18.4.131]) by sfo.erg.sri.com (8.9.1/8.9.1) with SMTP id MAA26054 for ; Wed, 14 Nov 2001 12:09:02 -0800 (PST) From: "Tom Low" To: Subject: Facet Fuel Pumps Date: Wed, 14 Nov 2001 12:23:01 -0800 Message-ID: MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit Importance: Normal X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Ed As the owner of a L235 using the Pillar Point System, I don't understand why you want to use a selector valve on the wing to header tank fuel transfer system. I have two facet pumps installed for wing to header transfer, one for each . This approach permits transfer from both wings simultaneously, and doubles the refill rate of the header tank. This is the anticipated layout that the Pillar Point system was designed around. A third (different model) Facet pump is installed as a boost pump between the fuel shutoff valve (from the header tank) and the gascolator, the recommended distance upstream of the Vision Microsystems flow transducer. Tom Low N31CD >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://members.olsusa.com/mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please remember that purchases from the Builders' Bookstore assist with the management of the LML. Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>