Return-Path: Received: from lanfear.nidlink.com ([216.18.128.7]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Wed, 9 Jun 1999 15:43:42 -0400 Received: from enaila.nidlink.com (root@enaila.nidlink.com [216.18.128.8]) by lanfear.nidlink.com (8.9.0/8.9.0) with ESMTP id MAA12887 for ; Wed, 9 Jun 1999 12:46:33 -0700 (PDT) Received: from regandesigns.com (tnt132-152.nidlink.com [216.18.132.152]) by enaila.nidlink.com (8.9.0/8.9.0) with ESMTP id MAA16976 for ; Wed, 9 Jun 1999 12:46:31 -0700 (PDT) Message-ID: <375EC491.D67DCC25@regandesigns.com> Date: Wed, 09 Jun 1999 12:46:25 -0700 From: Brent Regan To: lancair.list@olsusa.com Subject: Re: Brent Regan/Flap Actuator Tube Interference References: <19990609042001.AAA24562@truman.olsusa.com> X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Dear Dave: I sincerely apologize if you have taken personal offense at my comments. That was not my intent. I have always found that presenting a case in a reasonable, factual manner without making assumptions as to who is "at fault" consistently produces the most favorable outcome. Hyperbole aside, the situation here is simple, you know of one airplane that has a flap actuator alignment problem and I know of two that do not. I was heavily involved in the construction of the airplanes I am referring to (N170BR and N114L). Both are IV-Ps, both have won Outstanding Workmanship Awards at OSH, both have been inspected for flap mechanism interference and neither has a problem. I call this an "existence proof". I proves that it is possible to assemble the components as intended without a rubbing problem. The quality of construction of the IVs out there (and all homebuilts for that matter) varies widely. Some are better than you could hope to get from an assembly line and some are not airworthy. More than one builder has failed to remove peel ply from critical bond areas. These airplanes are complex machines and almost every one is built by a guy who hasn't built one just like it before. All of them have flaws. Uncovering these flaws and presenting them so that others may learn is one of the objectives of this forum. My personal motivations are to keep abreast of problems that develop in flying aircraft and the return the favor I received from those who assisted me. Benefiting from this forum without contributing would be very bad Ju-Ju. One tip for you. You mention in your posts that various manufacturers ignore you. I don't thing you want to be advertising that fact ;) Dave, one thing I am confused about is this, what is it you want? You have brought the problem you have had to the factory's attention, and ours, and it has been noted. Since you are an engineer I would think that you could propose a solution. If the problem is real and the proposed solution is workable it has been my direct experience that the folks at Lancair are responsive. Case in point. Early in the construction of my plane I visited the factory and saw the pressurized prototype under construction. Ross was working on the hydraulics and I noted that they were using electric solenoid actuated 4-way spool valves to operate the main gear. These valves are very sensitive to contamination and will stick it you look at them wrong. I proposed to Lance that they switch to the manually operated rotary valve that is currently used. This solution was far more reliable, cheaper and lighter. The only one who didn't benefit was poor Ross who had to tear out all his fine work to use the new valves. Sorry Ross. While I am passing out apologies, I am sorry for the bandwidth that rehashing these issues has taken. Can we move on now? Regards Brent >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html