Return-Path: <marv@lancaironline.net>
Received: from [65.33.166.167] (account <marv@lancaironline.net>)
  by logan.com (CommuniGate Pro WebUser 4.0b7)
  with HTTP id 1724923 for <lml@lancaironline.net>; Mon, 09 Sep 2002 21:40:13 -0400
From: "Marvin Kaye" <marv@lancaironline.net>
Subject: Re: [LML] Re: Engine Sag
To: lml
X-Mailer: CommuniGate Pro Web Mailer v.4.0b7
Date: Mon, 09 Sep 2002 21:40:13 -0400
Message-ID: <web-1724923@logan.com>
In-Reply-To: <20020909.201324.-16712297.12.Earl_Schroeder@juno.com>
MIME-Version: 1.0
Content-Type: text/plain; charset="ISO-8859-1"; format="flowed"
Content-Transfer-Encoding: 8bit



Posted for earl_schroeder@juno.com:
My engine hung on the airframe for several years during final
construction and after 65 hrs of flying (including several non-greaser
landings), I have not noticed any additional sag.  I would guess you
could expect less than 1/4 inch additional sag.  (0-320 in a 235
airframe) IMHO