Return-Path: Received: from baron.nii.net ([209.113.172.16]) by truman.olsusa.com (Post.Office MTA v3.1.2 release (PO203-101c) ID# 0-44819U2500L250S0) with ESMTP id AAA20172 for ; Sun, 13 Sep 1998 23:20:13 -0400 Received: from nii.net (xcom50.nii.net [209.113.173.114]) by baron.nii.net (8.8.5/8.8.5) with ESMTP id XAA25788 for ; Sun, 13 Sep 1998 23:20:07 -0400 Message-ID: <35FC8CD9.40EEDC04@nii.net> Date: Sun, 13 Sep 1998 23:26:17 -0400 From: "Angier M. Ames" Organization: Alpha Delta Research X-Mailer: Mozilla 4.03 (Macintosh; U; 68K) To: lancair.list@olsusa.com Subject: Re: 320/360 cockpit sub-floors References: <19980913040740.AAA10379@truman.olsusa.com> X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Warning....when installing sound deadening material beneath the sub-floors, think twice before using expandable foam in a can. It will expand with considerable force in a confined area. I completed this construction four months ago, drilled numerous holes in the floors and injected foam. In due time, the foam expanded and found its way out through the holes as I had expected and about a week later, I filled the holes with micro. Four months later and much to my surprise, I found a ball of foam about six inches in diameter on the cockpit floor. Some of the origional foam had not completely cured and over time, it expanded with enough force to rupture a small area of 2bid tape I had applied around the sub-floor. The bottom of the fuselage had been wet sanded to 600 grit before being turned right side up and the force of expanding foam had produced a visual distortion in the exterior surface. It might have been only 2 or 3 mil and about the size of a slice of tomato. Noone else will ever see it but I know it's there and will deal with it during final painting. Just to be safe, fill the void between sub-floor and fuselage with rigid foam, cut to size and shape and benefit from my mistake. Angier Ames