Return-Path: Received: from mail.ptd.net ([207.44.96.65]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with SMTP id com for ; Fri, 12 May 2000 22:23:57 -0400 Received: (qmail 10847 invoked from network); 13 May 2000 02:29:50 -0000 Received: from du184019.spa.ptd.net (HELO ?204.186.184.52?) (204.186.184.19) by mail.ptd.net with SMTP; 13 May 2000 02:29:50 -0000 Message-Id: Date: Fri, 12 May 2000 22:15:40 -0400 To: Lancairlist From: "Jeffrey T. Liegner, M.D." Subject: Who's Using Extra Fuel Bays in IVP? X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Survey: how many IVP builders have grabbed 8 extra gallons of fuel capacity per wing by using the two aft inboard bays between rib 22.5 and rib 76 (after first isolating the airleron push rods from the bay's fuel)? Follow up question: how many are flying with this configuration, and how has it affected Wt & Balance, plus performance based on the extra fuel weight aft of CG? Anyone using transfer pumps to drain these tanks during flight? Jeffrey T. Liegner, M.D. Ophthalmologist in New Jersey N334P >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>