Return-Path: Sender: "Marvin Kaye" To: lml@lancaironline.net Date: Mon, 03 Jan 2005 23:40:14 -0500 Message-ID: X-Original-Return-Path: Received: from [198.36.178.141] (HELO stoel.com) by logan.com (CommuniGate Pro SMTP 4.2.5) with ESMTP id 590724 for lml@lancaironline.net; Mon, 03 Jan 2005 23:31:41 -0500 Received-SPF: none receiver=logan.com; client-ip=198.36.178.141; envelope-from=JJHALLE@stoel.com Received: from PDX-SMTP.stoel.com ([172.16.101.137]) by gateway1.stoel.com with ESMTP id <334098>; Mon, 3 Jan 2005 20:39:38 -0800 Received: from PDX-MX6.stoel.com ([172.16.101.64]) by PDX-SMTP.stoel.com with Microsoft SMTPSVC(5.0.2195.6713); Mon, 3 Jan 2005 20:31:05 -0800 X-MimeOLE: Produced By Microsoft Exchange V6.0.6249.0 content-class: urn:content-classes:message MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Subject: RE: Legacy Rudder Bellcrank X-Original-Date: Mon, 3 Jan 2005 20:31:04 -0800 X-Original-Message-ID: <17E9FE5945A57A41B4D8C07737DB60726EB5CA@PDX-MX6.stoel.com> X-MS-Has-Attach: X-MS-TNEF-Correlator: Thread-Topic: lml Digest #1079 Thread-Index: AcTxg8la3eWju/acQeWRtXehxtxLwwAkJifw From: "Halle, John" X-Original-To: "Lancair Mailing List" X-Original-Return-Path: JJHALLE@stoel.com X-OriginalArrivalTime: 04 Jan 2005 04:31:05.0063 (UTC) FILETIME=[341B6770:01C4F216] Two of us have recently replaced the rudder bellcrank and bushing in our = Legacies. The problem first surfaced when it seemed like someone was = kicking on the rudder pedals Carl Lewis' Legacy on landing rollout. On = inspection, the rudder could be moved back and forth about three inches = without moving the rudder pedals and the bellcrank was tilting forward = and aft as the rudder was moved back and forth. When we got the = bellcrank out, the bushing was very loose in the hole. It wouldn't = quite fall out but it could be pushed out without any effort and it = could be rotated to about 15 degrees of tilt in any direction while = still inside the hole. Carl's Legacy has about 100 hrs. of flight time. = When I got back to base, I inspected my airplane (in which I had not = experienced any unusual rudder action) and discovered the same problem. = Mine was not as bad as Carl's even though it has about 400 hrs. The = rudder moved back and forth about one inch and the bellcrank tilted = less. Sure enough, the bushing was also quite loose in my bellcrank but = not as loose as Carl's. After reinstallation, the rudder still has = about 1 inch of slop so that seems to be normal. The replacement parts had a very tight bushing fit, requiring = installation with a vice. Neither Carl nor I, nor Leighton Mangels, who = helped with building both airplanes, remembers doing that with the = original parts so it is possible that there is a spec change. We think = a tight fit is essential since any movement of the bushing against the = bellcrank will eventually gouge out the hole. It is also possible that = over-tightening the bolt that goes through the bushing could pinch down = on the bushing and cause it to rotate against the bellcrank (instead of = the bellcrank and bushing rotating against the bolt as designed.) The replacement was a challenge in a number of ways. Space back where = the bellcrank is installed is severely limited and for both of us was = more limited than when we made the original installation because of = avionics installations and the elevator pushrod, which both of us = ultimately removed. Removal of the bellcrank assembly went fairly = smoothly but only because during construction we had made an access = panel that allowed us to unhook the rudder pushrod at the rudder end and = pull the entire assembly forward. Getting to the bellcrank bolts was = bad enough; I don't want to think about how we would have unhooked and = reattached the rudder pushrod at the bellcrank end. Reinstallation was quite a bit trickier. The rudder cables tend to pull = forward once the bellcrank is unbolted and need to be pulled back. The = composite material to which the bolt nutplates are attached was not = drilled out wider than the bolt diameter, which required us to unscrew = the bolt using a ratchet wrench all the way through the composite. On = the reinstall, we could not get any of my bolts (there are three) to = thread by hand and ultimately used a 90 degree angle drill with a socket = attachment to get enough pressure and speed on the bolt to make it work. = Carl got the front and back bolts in ok but seems to have messed up the = center nutplate a bit on removal. A tap fixed the problem but only = after several unpleasant hours wedged in the tail. If you are still building, here are some suggestions: =B7 Check to make sure the bushing fits tightly into the bellcrank. If = you can just push it in or out, it is not tight enough. =20 =B7 Put some grease on the AN 4 bolt (that goes thru the bushing). = Couldn't hurt. =B7 Make sure you don't overtighten the bolt. Ratchet it all the way in = and back off a hair. =B7 Make an access panel in the rudder to access the pushrod. =B7 Hog out the composite above the nutplates so the bolts don't hang up = on it. =B7 When you are installing all your neat EFIS stuff, think about how = you will get past it if you ever need to get to the bellcrank. If you are already flying and the rudder seems more than usually floppy, = check out your bellcrank. If it tilts forward and aft as the rudder is = moved, the bushing is loose and will only get worse. If you have the = problem, find a 98 lb. A&P with really long arms and wish him lots of = luck. Don't forget to put something under the tail. If you want more information, please contact me or Carl; or, better = still, contact Leighton (leighton@teleport.com) who knows more about it = than either of us.