X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Mon, 27 Jun 2005 16:06:26 -0400 Message-ID: X-Original-Return-Path: Received: from www.dynacomm.ws ([198.22.63.66] verified) by logan.com (CommuniGate Pro SMTP 4.3.5) with ESMTP id 1023592 for lml@lancaironline.net; Mon, 27 Jun 2005 15:47:44 -0400 Received-SPF: none receiver=logan.com; client-ip=198.22.63.66; envelope-from=lorn@dynacomm.ws Received: from [10.0.1.202] (adsl-69-209-184-29.dsl.sfldmi.ameritech.net [69.209.184.29]) by www.dynacomm.ws (8.10.2/8.10.2) with ESMTP id j5RJkqi04769; Mon, 27 Jun 2005 15:46:52 -0400 In-Reply-To: References: Mime-Version: 1.0 (Apple Message framework v730) Content-Type: text/plain; charset=WINDOWS-1252; delsp=yes; format=flowed X-Original-Message-Id: <7F6BCE2C-B90D-439E-8119-F8AEFB446686@dynacomm.ws> X-Original-Cc: BILL HANNAHAN , John Stchur LML Content-Transfer-Encoding: quoted-printable From: "Lorn H. Olsen" Subject: Re: Induction (not just carb) heat requirements. X-Original-Date: Mon, 27 Jun 2005 15:46:51 -0400 X-Original-To: Lancair Mailing List X-Mailer: Apple Mail (2.730) Bill, I flew in a Tiger last year. The Tiger had a carb air temp (CAT) =20 gauge. When I pulled the carb heat, the CAT increased by about 10=B0F. =20= In my Lancair with an O-320-D1F, and the heat muff stuffed with =20 stainless steel Brillo pads, the CAT only increases by about 8=B0F. I =20= know that this is not enough but I would be happy with a 15=B0F = increase. The new CAT increase requirements must be much more stringent than in =20= the past. Lorn > From: BILL HANNAHAN > Date: June 24, 2005 11:32:15 AM GMT-04:00 > > Here are the minimum performance specifications for a certified =20 > induction > heat system. > > //// > > Part 23 AIRWORTHINESS STANDARDS: NORMAL, UTILITY, ACROBATIC, AND =20 > COMMUTER > CATEGORY AIRPLANES > > Sec. 23.1093 > > Induction system icing protection. > > (a) Reciprocating engines. Each reciprocating engine air induction =20 > system > must have means to prevent and eliminate icing. Unless this is done by > other means, it must be shown that, in air free of visible moisture =20= > at a > temperature of 30=B0 F.=97 > > (1) Each airplane with sea level engines using conventional venturi > carburetors has a preheater that can provide a heat rise of 90=B0 F. =20= > with > the engines at 75 percent of maximum continuous power; > . > . > . > //// > > These specifications are the result of extensive testing in =20 > response to > accidents. There is a large envelope of possible induction icing > conditions. A 50 degree temperature rise may be sufficient for 95% of > induction icing encounters, but surviving a few encounters does not =20= > prove > that you can survive the full range of possible encounters. My =20 > guess is > that many homebuilts are woefully inadequate in this department. > > > BILL HANNAHAN > WFHANNAHAN@YAHOO.COM -- Lorn H. 'Feathers' Olsen, MAA, DynaComm, Corp. 248-345-0500, mailto:lorn@dynacomm.ws LNC2, O-320-D1F, 1,100 hrs, N31161, Y47, SE Michigan