Return-Path: Received: from csimo02.mx.cs.com ([205.188.156.53]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Mon, 29 Nov 1999 09:12:47 -0500 Received: from RicArgente@cs.com by csimo02.mx.cs.com (mail_out_v24.4.) id k.0.9b882442 (3970) for ; Mon, 29 Nov 1999 09:17:15 -0500 (EST) From: RicArgente@cs.com Message-ID: <0.9b882442.2573e4eb@cs.com> Date: Mon, 29 Nov 1999 09:17:15 EST Subject: Dynamic Prop/Engine Balancing To: lancair.list@olsusa.com X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> I happen to read an article from Kitplanes Magazine (September, 1997) regarding dynamic propeller/engine balancing and thought the following data would be of interest to some of you: Propeller/Engine Vibration Level Table IPS (inch/sec) Classification 0.8 or Greater Dangerous 0.4 - 0.8 Rough 0.2 - 0.4 Moderately Rough 0.1 - 0.2 Fair 0.1 or Less Smooth As I mentioned before, my vibration level was reduced from Rough (0.45ips) to Smooth (0.08 ips). Having flown N360ZR a couple of more hours after the balancing procedure was done just reinforces my initially findings, a much smoother aircraft all together! Highly recommended. Rick Argente N360ZR >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>