X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Received: from [69.171.52.140] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WebUser 4.3c4) with HTTP id 860042 for lml@lancaironline.net; Thu, 07 Apr 2005 00:21:16 -0400 From: "Marvin Kaye" Subject: Re: To: lml X-Mailer: CommuniGate Pro WebUser Interface v.4.3c4 Date: Thu, 07 Apr 2005 00:21:16 -0400 Message-ID: In-Reply-To: <001501c53afc$ce963fd0$0301010a@CRAIN> References: <001501c53afc$ce963fd0$0301010a@CRAIN> X-Priority: 3 MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for "Dominic V. Crain" : It was my understanding, all these long years, that the purpose of cycling the prop in the run up phase was to check the governor control, and to circulate warming oil through the hub to ensure efficient operation of the governor at the start of take-off and then though the remaining phases of flight, all being well. Certainly I have vivid recollection of engineering schools for DC3 and DC4 wherein the ground instructors stated clearly that was the reason. The prop cycling was full, and not just to obtain a "50 RPM" drop. Well, until someone can give me a statement that an engine blow-up can be sheeted home to run-up governor checks, then I will continue to do so. Further, it seems to me that in the event of an engine failure in flight, the first thing after all the standard checks is to get the prop into full coarse, which we all know improves the glide ratio considerably. Does in mine anyway. Wouldn't it be nice if we could have full feathering fan blades on the high bypass engines now operating. I reckon the A330 which had a double engine failure a few years ago could have made Lisbon. But I digress. Dom Crain