X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from omr-d01.mx.aol.com ([205.188.252.208] verified) by logan.com (CommuniGate Pro SMTP 6.0.8) with ESMTPS id 6702481 for flyrotary@lancaironline.net; Sat, 25 Jan 2014 12:17:40 -0500 Received-SPF: pass receiver=logan.com; client-ip=205.188.252.208; envelope-from=shipchief@aol.com Received: from mtaomg-mcc01.mx.aol.com (mtaomg-mcc01.mx.aol.com [172.26.253.85]) by omr-d01.mx.aol.com (Outbound Mail Relay) with ESMTP id 8E0E0700567DC for ; Sat, 25 Jan 2014 12:17:04 -0500 (EST) Received: from core-ddc002a.r1000.mail.aol.com (core-ddc002.r1000.mail.aol.com [172.29.52.133]) by mtaomg-mcc01.mx.aol.com (OMAG/Core Interface) with ESMTP id 5AD0338000082 for ; Sat, 25 Jan 2014 12:17:04 -0500 (EST) To: flyrotary@lancaironline.net Subject: Exhaust Leak at Turbo Outlet Flange X-MB-Message-Source: WebUI X-MB-Message-Type: User MIME-Version: 1.0 From: shipchief@aol.com Content-Type: multipart/alternative; boundary="--------MB_8D0E80866CE3D8C_92C_39CDE_webmail-d222.sysops.aol.com" X-Mailer: AOL Webmail 38306-STANDARD Received: from 72.171.16.246 by webmail-d222.sysops.aol.com (149.174.160.229) with HTTP (WebMailUI); Sat, 25 Jan 2014 12:17:04 -0500 Message-Id: <8D0E80866C256A7-92C-F8D7@webmail-d222.sysops.aol.com> X-Originating-IP: [72.171.16.246] Date: Sat, 25 Jan 2014 12:17:04 -0500 (EST) x-aol-global-disposition: G DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=mx.aol.com; s=20121107; t=1390670224; bh=9KitswJ7jnt9kyk+14v0SdmOihibXBlIbTq97crqULE=; h=From:To:Subject:Message-Id:Date:MIME-Version:Content-Type; b=xNvWYVdDJxZDiPkhFcRkfKt+4BwEWQtX5k+Qh+/JbvbQ+bed3VFXnSq/3TEzrZunf Kq1h3+Jxl5Ifs5CJ1nxpbyRMOnlISh+8lr/iezG86gGAt2KDzkUQMHewNeyxs5f5Vk 3NWD5l+6pct7QnGSIi37jJ+AlK2xHO/Z09m9qxq4= x-aol-sid: 3039ac1afd5552e3f19021ee This is a multi-part message in MIME format. ----------MB_8D0E80866CE3D8C_92C_39CDE_webmail-d222.sysops.aol.com Content-Transfer-Encoding: quoted-printable Content-Type: text/plain; charset="us-ascii" During the 8th flight of my RV8 with 13B Turbo, I experienced an exhaust le= ak at the turbo exhaust flange. I mistakenly used brass exhaust nuts which= are twice as tall as regular nuts. They work great on most engines. I shou= ld have know better, as the temperature at the turbo outlet, under the insu= lation is much higher. The brass nuts softened and deformed into a flange face at the washer! Once= the tension was gone, the heat & vibration did the rest. The exhaust gasket blew where the gap was widest, at the top. The escaping heat burned thru the insulating jacket and the stick on reflec= tive aluminum. Then the fiberglass cowl charred, I smelled that! I was close to my destination, and high, so I was able to pull off the powe= r, put down the nosed and get on the ground without incident. I'm disassembling it now, looks like I need 4 high temperature lock nuts an= d a TO-4 exhaust flange gasket. I should review and improve the insulation = over the turbine housing. Also I need to repair the charred area of the cow= l, which might be in the form of an aluminum access hatch. ----------MB_8D0E80866CE3D8C_92C_39CDE_webmail-d222.sysops.aol.com Content-Transfer-Encoding: quoted-printable Content-Type: text/html; charset="us-ascii"
During the 8th flight o= f my RV8 with 13B Turbo, I experienced an exhaust leak at the turbo exhaust= flange. I mistakenly used brass exhaust nuts  which are twice as tall= as regular nuts. They work great on most engines. I should have know bette= r, as the temperature at the turbo outlet, under the insulation is much hig= her.
The brass nuts softened and deformed into a flange face at the washer!= Once the tension was gone, the heat & vibration did the rest.
The exhaust gasket blew where the gap was widest, at the top.
The escaping heat burned thru the insulating jacket and the stick= on reflective aluminum. Then the fiberglass cowl charred, I= smelled that!
I was close to my destination, and high, so I was able to pull off the= power, put down the nosed and get on the ground without incident.
I'm disassembling it now, looks like I need 4 high temperature lo= ck nuts and a TO-4 exhaust flange gasket. I should review and improve the i= nsulation over the turbine housing. Also I need to repair the charred area = of the cowl, which might be in the form of an aluminum access hatch.
----------MB_8D0E80866CE3D8C_92C_39CDE_webmail-d222.sysops.aol.com--