Return-Path: Received: from dewey.cadwell.com ([208.26.246.18]) by ns1.olsusa.com (Post.Office MTA v3.5.3 release 223 ID# 0-64832U3500L350S0V35) with SMTP id com for ; Fri, 11 Aug 2000 12:45:18 -0400 Received: by dewey.cadwell.com with SMTP (Microsoft Exchange Server Internet Mail Connector Version 4.0.993.5) id <01C0037A.268F8FD0@dewey.cadwell.com>; Fri, 11 Aug 2000 09:54:33 -0700 Message-ID: From: Carl Cadwell To: "'lancair.list@olsusa.com'" Subject: IVP Fast build door installation Date: Fri, 11 Aug 2000 09:54:30 -0700 X-Mailing-List: lancair.list@olsusa.com Reply-To: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> It took 2 days to prep, fit, adjust and install the fast build door. We made small adjustments to the chain operating the lower latches and the exterior handle. We moved the stud/ball holding the upper end of the strut about 1" up and out filling the hole with epoxy/flox and 2 bid carbon on both sides of the frame. Installation variances from the manual following discussions with Mark at Lancair: 1. We bolted the top of the fuselage in position. This allows us to remove the top with the door installed and install the overhead console without working overhead. 2. After fitting the door frame to the opening, the frame needed to be aligned to flush out with the fuselage. 3. Holes were drilled about every 6" around the door frame to hold the door in place. 1.5" #8 machine screws and nuts with fender washers on the inside and outside were used in lieu of clecos. This allowed positive adjustment of the door frame to flush it to the fuselage 4. Where the frame needed to be spaced out (held in) from the fuselage, 1"x1" phenolic blocks were cut and thinned to the appropriate thickness. 8 of these were required. 5. The door and frame were placed in dry and adjustments were verified. The door and frame were removed and readied to bond to the upper fuselage. 6. The door and frame were attached using 1 2/3 cans of hysol mixed with flox. This allowed enough working time. The phenolic spacers were wetted with hysol and incorporated into the hysol/flox. 7. The frame was adjusted utilizing the machine screws with fender washers to flush it with the fuselage. 8. It took 11/4 hours to mix, place and adjust the frame. All looks great. 2 days vs. 2 months is 2 months closer to flying. Carl Cadwell >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> 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. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>