Return-Path: Sender: (Marvin Kaye) To: lml@lancaironline.net Date: Wed, 22 Oct 2003 00:19:45 -0400 Message-ID: X-Original-Return-Path: Received: from imo-m03.mx.aol.com ([64.12.136.6] verified) by logan.com (CommuniGate Pro SMTP 4.1.5) with ESMTP id 2646064 for lml@lancaironline.net; Tue, 21 Oct 2003 21:39:08 -0400 Received: from Sky2high@aol.com by imo-m03.mx.aol.com (mail_out_v36_r1.1.) id q.12d.330b207a (16781) for ; Tue, 21 Oct 2003 21:38:41 -0400 (EDT) From: Sky2high@aol.com X-Original-Message-ID: <12d.330b207a.2cc739a1@aol.com> X-Original-Date: Tue, 21 Oct 2003 21:38:41 EDT Subject: Re: [LML] Re: Horsepower Calculation X-Original-To: lml@lancaironline.net MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="-----------------------------1066786721" X-Mailer: 9.0 for Windows sub 1100 -------------------------------1066786721 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit OK, OK, I withdraw the formula--- Grabbing the 1985 Cessna 152 POH, assuming that MAP = atmospheric pressure at standard conditions and 2400 rpm: alt POH Formula %HP %HP 2000 74 76 4000 70 70 6000 67 64 10K 63 58 I am still looking for a way to chart % power without knowing the max sea level power that is delivered by the engine. If I need different charts for different altitudes, so be it. Scott Krueger Sky2high@aol.com II-P N92EX IO320 Aurora, IL (KARR) -------------------------------1066786721 Content-Type: text/html; charset="US-ASCII" Content-Transfer-Encoding: quoted-printable

OK, OK, I withdraw the formula---

Grabbing the 1985 Cessna 152 POH, assuming that MAP =3D atmospheric pre= ssure at standard conditions and 2400 rpm:

alt POH Formula

%HP %HP

2000 74 76

4000 70 70

6000 67 64

10K 63 58

I am still looking for a way to chart % power without knowing the max s= ea level power that is delivered by the engine. If I need different ch= arts for different altitudes, so be it.

Scott Krueger
Sky2high@aol.com
II-P N92EX IO320 Aurora, IL (KARR)

-------------------------------1066786721--