Return-Path: Received: from smtp0.mindspring.com ([207.69.200.30]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Wed, 27 Jan 1999 14:04:15 -0500 Received: from u2kmz (ip49.southern-pines.nc.pub-ip.psi.net [38.30.55.49]) by smtp0.mindspring.com (8.8.5/8.8.5) with SMTP id OAA13792 for ; Wed, 27 Jan 1999 14:05:45 -0500 (EST) From: marklisalally@mindspring.com Message-ID: <001201be4a28$37fb0ea0$31371e26@u2kmz> To: "lancair mail" Subject: ES manual mistakes Date: Wed, 27 Jan 1999 14:06:58 -0500 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> First let me thank Dan Obrien for bringing the H. stabilizer incidence mistake in the manual to light, without his input I may have not received this info until it was to late. On that note, let me point out a few other manual mistakes that I have had the misfortune of discovering the hard way. First in section I, aileron actuator mechanism page 9-49 . when you remove the core on rib BL145.5 you should consider placing your forward cut at 5" aft of the L.E. not at 6" as indicated in the manual. The reason for this is that the mounting hole location on the bellcrank mounting bracket would put your nutplates smack dab in the center of your microradius, and this is a large radius because of the 8 bid reinforcement. after finding this problem I called the factory and they said to simply move the bellcrank aft to compensate. This I did. BIG mistake. I have constructed my wings with the two extra fuel bays per wing .as Im sure many of you have also done. Now because of this mistake in the manual my aileron pushrods interfered with my outboard fuel bay. Man was I pissed!!!. the only reasonable solution I could come up with was to remove the core on the fuel bay rib in the interference area and reinforce it with a large and heavy 3 bid. This all wasted about 15-20 hours of my time. An earlier mistake in the manual I ran into was in section A chapter 8 flap hinge locations, page 8-7 . Figure 8:A:4 shows the hinge at BL120 to be set at 14 degrees. This angle can not be achieved without cutting the hinge itself (DO NOT CUT) you will have to come up with your own angles. These are but two of the many manual mistakes that I have run into so far ,while I expect some mistakes in a manual this large,I also expect them to be corrected when they are discovered., and I know lancair is aware of the mistakes. One time saving solution for Lancair would be to post the correction on this website, Even better would be to have and attachment sent with the corrections that we could print out and put in out manuals. MARK LALLY ES 15%