Return-Path: Received: from vc1.videocomm.com ([205.178.100.98]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Mon, 14 Jun 1999 20:02:20 -0400 Received: by vc1.videocomm.com with MERCUR-SMTP/POP3/IMAP4-Server (v3.00.15 AS-0098306) for at Mon, 14 Jun 99 16:57:14 +-700 From: "Skip Long" To: "Lancair Builders Mail List" Subject: LIV Fuel System Date: Mon, 14 Jun 1999 17:02:55 -0700 Importance: Normal Message-Id: <99061416571448000@vc1.videocomm.com> X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> This past weekend a Glassair builder walked in to my hanger for a visit. During this visit he proceeded to tell me that the LIV's fuel system is very dangerous. Prone to vapor lock and that the position of the boost pump is wrong. He claims that the boost pump must be below the level of the tanks. I remember a few months ago their was a big discussion regarding the 320/360 fuel system but no comments about the LIV's. I always felt that the LIV's system was very straight forward. Very much like the Mooney's fuel system. I would appreciate any comments from those builders who are flying and whether their system is by the book or modified. Thanks Skip Long LIV N47SL HWD >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html