Return-Path: Received: from mta6.snfc21.pbi.net ([206.13.28.240]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Mon, 17 Jul 2000 20:07:09 -0400 Received: from postoffice.pacbell.net ([206.170.6.132]) by mta6.snfc21.pbi.net (Sun Internet Mail Server sims.3.5.2000.01.05.12.18.p9) with ESMTP id <0FXV0020A9WQ3T@mta6.snfc21.pbi.net> for lancair.list@olsusa.com; Mon, 17 Jul 2000 17:12:28 -0700 (PDT) Date: Mon, 17 Jul 2000 17:06:50 -0700 From: fmoreno4@postoffice.pacbell.net Subject: Long Range Tank for Lancair IV To: Lancair List Reply-to: fmoreno4@pacbell.net Reply-to: lancair.list@olsusa.com Message-id: <39739F99.FD815451@postoffice.pacbell.net> X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I sent Marv the photos of the long range tank for John Forker's journey from New Zealand to California so he can post them elsewhere on the site. John is in the final stages of building and testing a battery powered capacitive fuel gage that will sit in the top of the tank with a digital readout. Capacity is 74.8 gallons which provides adequate range if the power is reduced somewhat to yield a 15 gallon per hour fuel burn with the Lycoming TSIO 540. Computed speed at that fuel burn is 260 knots at 27,000 feet. Total fuel on board will be about 180 gallons. The design and build time was a bit over 60 hours including all the special carbon clevis parts and such that permits the unit to be shipped flat and easily assembled in the cockpit. The assembly is designed for 10 g forward impact load with a 2 to 1 safety factor (10,000 pound limit load on the restraining straps anchored to rear seat belt anchors). The bladder cost was about $1600 and the prepreg panels, hardware, and such added about another $400. When we have more time we will document the design and make the information available for others to use. The design can be modified to provide up to 125 gallons, but one will need to be careful with aft CG constraints with such large quantities. John selected 75 gallons because it keeps this particular airplane within the CG envelope with the fuselage tank brim full. Fred Moreno >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> 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. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>