Return-Path: Received: from smtp.email.msn.com ([207.46.181.30]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Sat, 12 Aug 2000 01:10:36 -0400 Received: from gainza - 63.42.250.235 by email.msn.com with Microsoft SMTPSVC; Fri, 11 Aug 2000 22:16:31 -0700 Message-ID: <000d01c0041d$9bfd3800$ebfa2a3f@gainza> From: "cgza" To: "Lancair list" Subject: IV-P door Date: Fri, 11 Aug 2000 22:24:36 -0700 Return-Path: cgza@email.msn.com X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I am happy to hear of Carl's success with the new door. I saw it at Oshkosh and it looked great! I took the long route (no choice) and finished the door after two months. One of the problems that still plagues me is the bulge near the aft hinge. My 90 lb strut is positioned perpendicular to the door hinge axis. The 90 lb strut puts a significant force upward creating a bulge near the aft hinge. Sure, it goes away once the door is cranked into position, but it requires a lot of cranking pressure to pull the door down. The fast build door has a 60lb strut, and a new position. The fuselage attach point is near the hinge and the door attach point is near the middle latch. Although this does not appear an ideal placement from an engineering standpoint, I am interested in feedback regarding the operation of the 60 lb strut and the new position. Maybe I should consider going to the 60lb strut and moving it. Carl, why did you have to move your strut and are you happy with its operation? Bulging? Green with envy, Craig Gainza Green Valley, CA IV-P >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> 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. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>