Return-Path: Received: from mail.ens.net ([204.248.18.55]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Wed, 6 Jan 1999 20:45:32 -0500 Received: from [204.248.18.240] by mail.ens.net (NTMail 4.01.0008/NS0001.00.c4f5c1e7) with ESMTP id ykghbaaa for ; Wed, 6 Jan 1999 19:56:48 +0000 Message-Id: <3.0.5.32.19990106194801.00841240@mail.ens.net> Date: Wed, 06 Jan 1999 19:48:01 -0600 To: From: rcblumenstein Subject: Re: Fuel selector valve "both" in low wing aircraft Cc: TByrnes133@aol.com,ticavers@hotmail.com In-Reply-To: <19981230051926.AAA659@truman.olsusa.com> X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> This is in reply to about Tristan Cavers concerns about a "both" position in a fuel selector for a low wing plane. Tom Byrnes replied: ">You mentioned that you do not have a header tank and that you have a fuel >selector that has positions for R - L - Both and off. A both position in a >low wing aircraft is considered dangerous by the FAA and not allowed in a >certified low wing aircraft because if one tank unports or runs dry before the >other one the fuel pumps would suck air even though fuel is present at the >other port." I had flown for some years a '79 Rockwell Commander 114A which had a "Both" position for the fuel selector. It too was a certificated low wing plane. They must have done something right in the design to pass the FAA certification. Richard (Dick) Blumenstein E-Mail: rcblumenstein@sysdyne.com