Return-Path: Received: from imo-d06.mx.aol.com ([205.188.157.38]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-52269U2500L250S0V35) with ESMTP id com for ; Sun, 5 Sep 1999 01:54:42 -0400 Received: from Fredmoreno@aol.com by imo-d06.mx.aol.com (mail_out_v22.4.) id kYQGtMpzE_ (4244) for ; Sun, 5 Sep 1999 01:58:20 -0400 (EDT) From: Fredmoreno@aol.com Message-ID: Date: Sun, 5 Sep 1999 01:58:19 EDT Subject: Instrumentation Errors To: lancair.list@olsusa.com X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Scott: If you think the errors I note which creep into the manifold pressure gage are bad, be aware that the standard run of Cessna/Beech/Piper tachometers are notoriously bad, frequently being off 100 RPM or more. I once knew how to check the gyro using the hour meter based on an article I read. The hour meter reads accurately (actual clock time) at a given RPM, and it is a weird intermediate value like 2357 RPM or some such. If one starts a stopwatch when the hourmeter on the tach turns over to a new digit, and you track it for a half hour or so, one can measure and correct the error. When my TR-182 was nearly new, I did such a check and found the tach reading 83 RPM low, and I placarded it as such. I no nonger complained when it appeared to be turning about 100 RPM low on takeoff. It was an instrumentation error. So, in answer to your question: how do we set POWER if the manifold pressure and tachometer instruments are so much in error? The answer is: VERY APPROXIMATELY. Sorry, but it's true. Fred >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML homepage: http://www.olsusa.com/Users/Mkaye/maillist.html