Return-Path: Received: from conure.mail.pas.earthlink.net ([207.217.120.54] verified) by logan.com (CommuniGate Pro SMTP 4.2) with ESMTP id 372308 for flyrotary@lancaironline.net; Fri, 20 Aug 2004 09:54:32 -0400 Received-SPF: pass receiver=logan.com; client-ip=207.217.120.54; envelope-from=Dastaten@earthlink.net Received: from user-0cetjkt.cable.mindspring.com ([24.238.206.157] helo=earthlink.net) by conure.mail.pas.earthlink.net with esmtp (Exim 3.33 #1) id 1By9qE-00002A-00 for flyrotary@lancaironline.net; Fri, 20 Aug 2004 06:54:02 -0700 Message-ID: <412602B4.3050802@earthlink.net> Date: Fri, 20 Aug 2004 08:55:00 -0500 From: David Staten Reply-To: Dastaten@earthlink.net User-Agent: Mozilla/5.0 (Windows; U; Windows NT 5.1; en-US; rv:1.4) Gecko/20030624 Netscape/7.1 (ax) X-Accept-Language: en-us, en MIME-Version: 1.0 To: Rotary motors in aircraft Subject: Initial teardown questions... Content-Type: text/plain; charset=ISO-8859-1; format=flowed Content-Transfer-Encoding: 7bit I have completed tearing down a 13B 2nd gen turbo and have pretty much cleaned up the rear side housing, rear rotor housing and rear rotor.... with the other large parts on a soak cycle... I am intending to go ahead and use Tracy's "Master Rebuild" kit with replacement of all the internal seals, springs and O-rings.. partially because when the engine was disassmbled, the case split in an unexpected fashion and some of the side and apex seals came out in an uncontrolled manner, to the point I am not sure exactly where they originated from... I know which side of the rotor they came from, but not which "groove" they belong in with certainty. After cleaning the rear rotor, I observed a small "ding" in the face of the rotor adjacent to the apex seal groove.. I am estimating it is less than 1 mm wide and minimal in depth. It will catch a fingernail. I was unable to take a picture of good enough resolution (3.1 mpix camera) to show the blemish.. but my question (first of many) is.. what are the limitations to surface anomalies on rotors with regards to scratches, dings and the like? Also, are there any limitations on having the housings bead blasted to remove water jacket corrosion and external grime? If permissible, any material to use or not use? Finally, when I do get around to reassembly, something I am not ENTIRELY clear on is determining top-dead-center. I see how the front e-shaft flange bolt pattern is unique and limits installation to only one possible way with regards to the timing marks on the eshaft pulleys, but what is the trick to aligning the eshaft with the rotor? Is it truly just as simple as having a rotor apex at one of four positions when reinstalling? If not, what is the rotor apex position associated with TDC (perhaps determined after reassembly, if need be)? Dave Staten partner in Velocity N17010 (reserved) Mazda 13B 2nd gen turbo rebuild