Return-Path: Received: from imo18.mx.aol.com ([198.81.17.8]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Tue, 8 Jun 1999 07:57:14 -0400 Received: from N295VV@aol.com (3960) by imo18.mx.aol.com (IMOv20) id kIIPa14117 for ; Tue, 8 Jun 1999 07:59:06 -0400 (EDT) From: N295VV@aol.com Message-ID: Date: Tue, 8 Jun 1999 07:59:05 EDT Subject: Re: Brent Regan/Flap Actuator Tube Interference To: lancair.list@olsusa.com X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> From: n295vv Well, Brent, as a matter of fact, I have SB044-0998 in my hot little fist, and it doesn't address the problem I am talking about, so your personal criticism of me is unfounded, and I will be pleased to accept your apology. The rubbing of the actuator arm on the control rod is not a builder alignment problem--it is a factory design problem....onother 1/4" on the axle length would prevent all interference. In fact, the EXACT REASON it doesn't address the problem, is because someone in the factory has chosen not to believe it exists, or for some other reason does not care to acknowledge it, despite my telling them about it. The end result is that others that may have this situation my not know it may exist in their airplane--including, apparently, yourself. If, Brent, you thought my criticism of the factory was without merit, I have several comments: Firstly, I have, indeed, been contacted by them in the past requesting that I tone down my criticism. Secondly, I am a very good engineer, perhaps even better than you, and in a previous instance I notified the Mooney factory of a problem in their plane which was not taken seriously. The net result was five crashes, two or more pilots killed, and one hell of a lawsuit which centered around my notification which was disregarded. And, yes they finally corrected the problem--two years after I brought it to their attention. We do agree on one thing--that this is a public forum, and I have a right to criticise them at every screw up, just as you have the right to defend them, as you have in the past, by putting the responsibility on the builder, and telling us "it is an experimental aircraft", which you have done many times. And since I am on the point, there was much discussion early on about the misalignment of the main gear axles, on the IV, resulting in the factory supplying shims to correct the misalignment. Mine took 2.3 degree shims in two axis, resulting in either elliptical bolt holes or the four bolts being bent. All you guys out there who have this fix--did you note the comment today about the tremendous forces occurring on landing, as exhibited by a cylinder rod being bent 65 degrees on a 320/360? Well, the IV is even heavier, and have you taken a look at these four bolts lately? Well, it indeed is an experimental project....but who in the world would have thought the guy in the factory was drilling the axle alignment holes by eye, rather than using a jig......I rest my case. David Jones, Pecatonica, Illinois >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html