X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from [71.42.21.121] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WEBUSER 5.3.5) with HTTP id 4191867 for lml@lancaironline.net; Thu, 01 Apr 2010 10:05:33 -0400 From: marv@lancair.net Subject: Re: [LML] Legacy maintenance idea To: X-Mailer: CommuniGate Pro WebUser v5.3.5 Date: Thu, 01 Apr 2010 10:05:33 -0400 Message-ID: In-Reply-To: <9752a.544be675.38e5f5fb@aol.com> References: <9752a.544be675.38e5f5fb@aol.com> MIME-Version: 1.0 Content-Type: text/html;charset=iso-8859-1 Content-Transfer-Encoding: 8bit
Posted for Sky2high@aol.com:

 Tom,
 
 You're kidding, right?  Of course, it's April fool's day.  [Gold star!!!!  <M>]
 
 This aircraft is of monococque construction - i.e. the skins are part of  
 the structure - i.e. your "door" is no longer structural.  If you  remember,
 the airflow over upper wing skins creates a very strong low pressure  and
 the skin will not rest on the ribs in flight with unknown results because of
 
 a new airfoil shape, assuming the skin stays attached at all.  But, what  
 the heck, it's experimental.
 
 Grayhawk, now Whitehawk.
 
 
 In a message dated 3/31/2010 11:49:14 P.M. Central Daylight Time,  
 tom.gourley@verizon.net writes:
 
 Posted:  April 1,2010
 
 While working on my Legacy  kit it occurred to me that once it's flying
 inspection
 and maintenance of the main gear would be so much easier if the stub wing  
 skin
 could be removed.  I attached a hinge to the leading edge so  that the skin
 could be
 opened as shown in the picture.  Now I'm  trying to decide what sort of
 fasteners
 I should use on the trailing edge.  Any  suggestions?
 
 Tom Gourley