Return-Path: Received: from wind.imbris.com ([216.18.130.7]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Thu, 7 Sep 2000 13:46:44 -0400 Received: from regandesigns.com (nortel131-126.imbris.com [216.18.131.126]) by wind.imbris.com (8.9.3/8.9.3) with ESMTP id KAA84929; Thu, 7 Sep 2000 10:52:25 -0700 (PDT) Message-ID: <39B7B9DE.1646E9AE@regandesigns.com> Date: Thu, 07 Sep 2000 10:53:03 -0500 From: Brent Regan To: Lancair List Subject: RE: Sierra Flight Systems X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Ahhh, the double edge sword of beta systems. You want to test hardware in actual conditions but, if you do, any flaw is exposed to everyone. In this case, it isn't even a flaw. Charlie rode to SnF with Tony Durizzi. Tony's plane has Version 2 hardware installed. Currently SFS is shipping Version 5 hardware. The changes from 2 and 5 include; elimination of the separate processor box, implementation of the voice warning system, improved display optics, multiport IO, armored IO and more. Tony's voice warning system "wasn't working" because it is not supported in his version of the hardware. The heading was off by 20 degrees because Tony did not have the opportunity to calibrate the heading sensor in his AHRS. AHRS calibration takes only about ten minutes but it requires a compass rose. Before calibration my system was off by 18 degrees, after calibration it is right on (less than 2 degrees). I understand that Tony's system is now calibrated and is accurate as well. Actual flight testing is essential to uncover unexpected interactions between the airplane in flight and the system under test. Just last weekend I discovered that in a 28 volt airplane, with a solid state voltage regulator and tired GR batteries, the IDU's input protection circuitry can interpret the avionics on power surge as an over voltage condition and shut down the IDU power supply (protecting the rest of the system). Once the problem was identified, a fix was tested and implemented and will be incorporated in any system that may be affected. An interaction like this would NEVER have been found in the lab. Naturally it reveled itself at the worst possible time, just before my demo flight with Filidauro. All products have problems. Any company that tells you otherwise is either lying or hasn't done enough testing. The measure of a company is how it reacts when a problem is discovered. I think you will find that SFS excels in their problem remediation. Since installing the system in my airplane, just before OSH, I have uncovered several minor squawks, all have been corrected. Regarding Megget, why would you pay more to get less? Do yourself a favor and put the two systems side by side before you buy. Regarding the comparison to Darkangel, that is just rude. Darkangel was designed by a PhD college professor (Those who can, learn. Those who can't, teach). SFS was designed by IFR rated pilots who fly behind the hardware in their own planes. If one part of a Darkangel system fails the whole system comes to it's knees. If one part of the SFS system fails the other parts step up and pick up the slack. If an IDU fails, the other IDU takes over. If the GPS fails, the inertial system takes over. If the AHRS fails you still have moving map. If your aircraft electrical system fails, the optional UPS will power the system for 45 minutes. Whatever you do, don't believe me or anybody else. Do what Filidauro did and go see first hand. Be warned though, if you don't have the cash for the SFS don't even look or you will be trying to rationalize a second mortgage on the homestead. My company designed the hardware for the SFS IDU (under contract) so anything I say should suspect and independently verified before taken as a fact. Regarding 12 or 28 volt systems, I chose 28 volt because the big wires are smaller (lighter) and a 60 amp 28 volt alternator produces twice the energy of a 60 amp 12 volt alternator. Also, since current flows are less, voltage drops through switches and contactors are less as well. Some argue that 12 volt components are easier to source but in my experience this is only true if you plan to use automotive components. I had no difficulty finding 28 volt components for my plane. Check the archives for more on this topic. Regarding the fly in, there were a lot more 2 place planes there than 4 place because there are a lot more 2 place planes out there. The light turnout was probably because the weather Saturday was perfect for ice and nobody likes ice. I even picked up some rime on Sunday. While it is true that you can fly over most weather in a IV, you still have to get up there and get back down. Regards Brent Regan >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> 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. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>