Return-Path: Received: from smtp5.gateway.net ([208.230.117.249]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Sat, 26 Feb 2000 15:01:47 -0500 Received: from oemcomputer (1Cust175.tnt2.coeur-dalene.id.da.uu.net [63.20.49.175]) by smtp5.gateway.net (8.9.3/8.9.3) with SMTP id PAA06676 for ; Sat, 26 Feb 2000 15:07:15 -0500 (EST) Message-ID: <000901bf8095$f26d6040$af31143f@oemcomputer> Reply-To: "dfs" From: "dfs" To: "Lancair List" Subject: Stub Wing Skins Date: Sat, 26 Feb 2000 12:12:52 -0800 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I just happened to be looking thru my photos of the build process and it reminded me of how it was done in our shop. IMHO, this may be as good as any other methods I've heard of. 1. Four very straight lengths of 2x4 were cut to fit on the top and bottom of the wing stub along the spar/skin contact areas. The bottom one was wrapped in a plastic film to keep it from becoming part of the airplane from the inevitable adhesive squeeze-out at the skin edge along the main spar. 2. six pieces of 1x4 clear pine were cut so that they were about 12 inches longer than the stub-wing chord and 3/8 in. holes were drilled thru each end a couple of inches from the ends. 3. Steel hardware store 1/4 in. threaded rods were inserted thru each end of pairs of the 1x4 boards. The length of the rods need to allow the boards to be slipped over the stub-wings plus the 2x4's. Washers and nuts were installed on each end of the rods, capturing the two boards between them. 4. With the stub-wing skin in place (I remember this was a two-man job to keep the skin spread enough to keep from skimming off all the adhesive), and a few clecos inserted at the skin/fuselage mating flanges to hold it all in position, the straight 2x4's were stuck in position with a couple dabs of hot glue on the outside of skin, along the glue lines. 5. Finally, the 1x4 and threaded rod assemblies are slipped over the stub-wing and 2x4's (boards running fore and aft) and the nuts on each end run down to capture the 2x4's against the stub-wing (this also is probably a two-man task - unless you happen to have four arms with an eyeball on the tip of a couple of fingers). By judiciously tightening the nuts on each end of the boards (which are now clamps), you can apply the desired squeeze pressure along the glue lines with the 2x4's insuring that the skins remain straight and the pressure is evenly distributed. I recommend that you do a dry run to be sure everything fits and the nuts are run down to approximately the correct position. Makes the final installation much easier. Takes longer to describe than accomplish. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>