Return-Path: Received: from hil-img-1.compuserve.com ([149.174.177.131]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Fri, 5 Mar 1999 07:11:52 -0500 Received: (from root@localhost) by hil-img-1.compuserve.com (8.8.6/8.8.6/2.18) id HAA03513 for lancair.list@olsusa.com; Fri, 5 Mar 1999 07:13:46 -0500 (EST) Date: Fri, 5 Mar 1999 07:11:27 -0500 From: Rick Argente Subject: New Adjustable Rudder Springs from Nieco Sender: Rick Argente To: "INTERNET:lancair.list@olsusa.com" Message-ID: <199903050711_MC2-6CD4-5AEF@compuserve.com> Mime-Version: 1.0 Content-Type: text/plain; charset=ISO-8859-1 Content-Disposition: inline X-Mailing-List: lancair.list@olsusa.com <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I just received the new 'rat-trap' springs from Nieco for the passenger side adjustable rudder pedals. As builders who installed DUAL ADJUSTABLE rudder pedals know, the spring pressure of the combined system causes an unacceptable (to me at least) amount of pressure requred to move the rudder pedals. While waiting for these new springs, I decided to install the stock springs on the passenger side. I will remove this installation and try out the new springs and will report here again to report the results. Just in case the pressure is still too much, I asked Vern to send me another set and I MAY install the same on the pilot side also. All depends on the resulting rudder pressure results. BTW, installing the STOCK springs (using the firewall to mount the other end of the springs) will NOT work satisfactory when adjusting the rudder pedals to it's foremost position. It will only work from the mid-setting to the aft-most setting. The springs strart to sag and produces NO pressure at all when pushed to the fore-most position. As an aside, here's a project update: - Total Construction Hours: 2,628!!! (and it's not yet painted!!, nor is it flying..) - both wings installed (but BOY, it was a bit_h**@@!! to safety wire the OUTBD wing bolts!!) - ailerons and flap travel movement adjusted to within limits and secured. - all push rod check nuts secured - gear doors installed and secured (BTW, do not forget to safety wire the OUTBD gear door) - getting the aircraft ready for the weight and balance measurements!!! Later, Rick Argente