Return-Path: Received: from [161.88.255.140] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WebUser 4.3c2) with HTTP id 766829 for lml@lancaironline.net; Wed, 02 Mar 2005 14:01:58 -0500 From: "Marvin Kaye" Subject: Re: [LML] LNC 2 Hydraulics To: lml X-Mailer: CommuniGate Pro WebUser Interface v.4.3c2 Date: Wed, 02 Mar 2005 14:01:58 -0500 Message-ID: In-Reply-To: References: X-Priority: 3 MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for "Randy Snarr" : Scott, You bring up an interesting point in how your gear is adjusted. My system is adjusted as per the factory with the gear against the aluminum sleeve stops on the up side and the down side is stopped by the over center links. The over center links are not that beefy and there is an enormous amount of stress on them with the down pressure at maximum. I wonder if there has ever been a failure due to this stress. Your solution sounds reasonable to me. I am curious as to what other have done if anything regarding the down side adjustment. Whilst writing this post I called Ross at Lancair and he told me essentially the same thing in that the over center link was not designed to handle the total down side stress of the system but admitted that there are many airplanes flying that are set up that way. He recommended the same solution as Scott, and that is to have the hyd cyl bottom out about the same time as the over center link hits it's limit taking a significant amount of the stress off the over center link... Randy L. Snarr 235/320 92% threatening 93% any day now...