Return-Path: Received: from mailarray.mpx.com.au ([203.29.192.90]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Wed, 3 Feb 1999 07:05:35 -0500 Received: from 198.142.139.90(really [198.142.155.102]) by mailarray.mpx.com.au via smtpd with smtp id for ; Wed, 3 Feb 99 23:06:28 +1100 (/\##/\ Smail3.1.30.13.SOL #30.20 built 28-jun-97) Message-ID: <36B858DF.676B@mpx.com.au> Date: Wed, 03 Feb 1999 06:11:12 -0800 From: Julie Byrnes Reply-To: byrnes@mpx.com.au Organization: Massive To: lancair.list@olsusa.com Subject: gear doors etc X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> 1. I have just finished doors for the outback gear. The length of the inner door is 11 1/2 inches. Ground clearance on the outer door is 6 inches. As you may now be all aware the left wing stub is 5/8" thinner than the right - too thin for the outback gear to fit. It required coring out part of the upper skin and covering the area with 3BID, coring out the gear doors and covering with 2 layers of carbon cloth and finally heat bending the door to create an almost undetectable speed-bump. The doors were stiffened with strips of half round foam covered with 2 layers of carbon fibre cloth. The strips on the inner door were in the shape of an angular inverted "U" and the outer doors had a "K" with the long stroke to the front. Bending the doors would have been easier if I realised before I put on the stiffeners that it had to be done! 2. Why not just glider gap-sealing tape for the flaps? I doubt that anyone would see or notice it. The glider fraternity also have gap-seals which go inside rudder-housings etc if that is of interest. 3. Finishing with a linear sander is fine if you want a good finish. If you want a perfect finish there is no substitute for sandpaper attached to long "torture boards" - gets the reflections razor sharpe. 4. Things change during construction. I recently put the 3bid on the front of the stub-wing spar. This small thickness was sufficient to change the conture, flap fitting etc and necessitated re-profiling. 5. A mention of the rod which holds the front u/c overcentre link in the centre wheel housing. This rod can be a tight fit in the overcentre assembly and may then rotate in the phenolic blocks. the latter will wear and the whole assembly becomes sloppy. I have now fixed the rod so it cannot rotate and have put a grease nipple on the overcentre bearing. 6. I lost the reference to Oshkosh accommodation. I would be grateful if someone could pass this on. Cheers David Byrnes