Return-Path: Received: from [65.33.85.194] (account ) by logan.com (CommuniGate Pro WebUser 4.1b9) with HTTP id 2472321 for lml@lancaironline.net; Fri, 11 Jul 2003 17:50:30 -0400 From: "Marvin Kaye" Subject: Re: [LML] Electrical System Planning To: lml X-Mailer: CommuniGate Pro WebUser Interface v.4.1b9 Date: Fri, 11 Jul 2003 17:50:30 -0400 Message-ID: In-Reply-To: <20030711203057.60994.qmail@web11308.mail.yahoo.com> MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for Scott Richardson : Hi Paul, Absolutely agree. My thinking was to keep any firewall penetration outside of the area where the firewall gusset layups contact the firewall itself. The only exception I've found so far is for the throttle/mixture/carb ht controls that run next to the nose gear tunnel and through the inboard layups on the pax-side lower engine mount. The wiring hole(s) would then be inboard of the gussets allowing me to run the cables along the fuselage sides from the panel to the firewall. I've seen some builder pictures where the main starter/ground cable penetrates the firewall near the top of the nose gear tunnel - just not sure where it goes next. How they get from the center of the firewall to the starter without alot of snaking on the firewall to get to an engine mount strut or a "free-air" jump from the firewall to the engine itself. Scott > I'm not an engineer, but wouldn't that tend to weaken the structure > of the firewall in an area where fairly heavy loads are being > transfered?