Return-Path: Received: from lanfear.nidlink.com ([216.18.128.7]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Fri, 19 May 2000 10:56:58 -0400 Received: from wind.imbris.com (enaila.nidlink.com [216.18.128.8]) by lanfear.nidlink.com (8.9.0/8.9.0) with ESMTP id IAA09324 for ; Fri, 19 May 2000 08:02:55 -0700 (PDT) Received: from regandesigns.com (tnt149-62.imbris.com [216.18.149.62]) by wind.imbris.com (8.9.3/8.9.3) with ESMTP id IAA61887 for ; Fri, 19 May 2000 08:01:54 -0700 (PDT) Message-ID: <39253B5D.B2E78A3F@regandesigns.com> Date: Fri, 19 May 2000 08:02:21 -0500 From: Brent Regan To: Lancair List Subject: Nose Strut SDR X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Jim Frantz writes: What is the (new) procedure? De we send a separate email to Jim or Marv? I inspected my strut and discovered the Lock Tite is neither. The threads are free to turn with about 20 pounds of force on the side of the wheel. The roll pin is the only thing keeping the flange from unscrewing from the strut. I suspect that the threads were not adequately degreased prior to the application of the thread locker during assembly. The SDR would read as follows: Affected parts: Early IV nose strut with centering mechanism and without "clamped" wheel flange. Problem: The thread locking between the nose gear wheel flange and the strut failed allowing the shearing forces to be borne by the rollpin which subsequently also failed. This allowed the nose gear to yaw relative to the centering mechanism enough to cause the nose wheel to jam in the nose gear tunnel, preventing nose gear extension. Inspection: With the plane on jacks, note if the nose wheel is centered to the aircraft. Inspect the rollpin for damage. Manually twist the nose wheel both directions in yaw and note if there is any relative motion between the flange and the chrome portion of the strut. Any motion between the flange and strut is an indication that the thread locker has failed. Repair: Remove the strut and return for service. This has been noted on two aircraft. One aircraft with a failed rollpin had just finished an annual inspection where the nose strut was recharged with nitrogen. Brent [All SDR's (and any other LNN-bound information) should be addressed to me at the Lancair Network News snail mail address in Fort Myers, FL, or to my private email address: marvkaye@olsusa.com. This one is already included in the next issue of the LNN, as I was able to glean enough info from the various posts to pass it along. Your submission as shown will be fully detailed in the following issue. Thanks for sending it to the LML. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html LML Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>