Return-Path: Received: from pop3.olsusa.com ([63.150.212.2] verified) by logan.com (CommuniGate Pro SMTP 3.5) with ESMTP id 971614 for rob@logan.com; Sun, 16 Dec 2001 05:15:31 -0500 Received: from util-1.kih.net ([209.209.190.230]) by pop3.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-71866U8000L800S0V35) with ESMTP id com for ; Sat, 15 Dec 2001 23:28:37 -0500 Received: from iswt.com (iswt.com [206.240.140.17]) by util-1.kih.net (8.11.4/8.11.4) with ESMTP id fBG4R7c22791 for ; Sat, 15 Dec 2001 23:27:07 -0500 (EST) Received: from 1vne2 [199.78.36.140] by iswt.com (SMTPD32-6.03) id A3136B8B00BA; Sat, 15 Dec 2001 22:29:07 -0600 Message-ID: <001701c185eb$82041940$8c244ec7@1vne2> From: "Brad and Tracy Simmons" To: References: <20011215054648.AAA3309@pop3.olsusa.com> Subject: IV De-ice systems Date: Sat, 15 Dec 2001 22:37:41 -0600 MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: 7bit X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> In 1997 we did install a BFG "slimline" boot de-ice system on a IV-P for a customer in Sweden. The boots covered the wings, horizontal stab and vertical stab, but not the winglets. A hot prop was installed on the Hartzell 3 blade prop. We designed a spray bar system for the windshield as well, but it was never installed. The boots were purchased from a builder in Texas in "kit" form. The boots themselves were brand new units, direct from BFG. Most other components were used/salvage items. No documentation (other than that from BFG) was provided with the "kit," leaving a lot to the imagination... We believe this to be the first, (of 2 or 3) and only actual working installation on a IV. I would be interested in hearing about any other successful installations. The finished installation weighed in at around 50/55 pounds, plus about 15 pounds for a supplemental electric vaccum pump to operate the system. All the valving was mounted in the baggage area on the back of the lower pressure bulkhead. In order to disrupt laminar flow as little as possible, the paint & primer under the boots was removed in order to fair them in as much as possible. The loss of speed was not greater than 5 knots, if that much. The owner flew successfully in Europe for 3 years, and reported the boots worked as advertised. The plane is back in the states and will be for sale in a few months. Additionally, we may have a complete boot kit for sale (including installation instructions) that was never installed on another customer's planes due to the project being sold because of a lost medical. If anyone is interested, contact me and I will check on availability. Lance mentioned Neico's involvement with a glycol system a few years ago. In 1995 we worked with a customer who desired a weeping wing system on his IV-P, and was willing to underwrite some of the development cost. We contacted AS & T (the USA arm of TKS, which is based in Europe) and Lancair about designing a system. The design progressed as far as engineering drawings and leading edge molds, which we made, before TKS Europe sort of "lost interest" due to the expanding Mooney market. Brad Simmons Airframes Inc. Milan, TN btsim1@iswt.com >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> 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. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>