Return-Path: Received: from [65.33.164.252] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WebUser 4.2.5) with HTTP id 576028 for flyrotary@lancaironline.net; Tue, 21 Dec 2004 19:26:40 -0500 From: "Marvin Kaye" Subject: Re: [FlyRotary] front cover oil fitting thread? To: "Rotary motors in aircraft" X-Mailer: CommuniGate Pro WebUser Interface v.4.2.5 Date: Tue, 21 Dec 2004 19:26:40 -0500 Message-ID: In-Reply-To: References: MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit "Russell Duffy" <13brv3@bellsouth.net>: """ My current oil system started out as AN12 all the way, but I ended up having to use an AN10 fitting at the engine, so the lines change from AN12 to AN10 along the way. ...snip.... Rusty (I know bigger is better, but AN10 is going to have to do) """ Here's a data point for you, Rusty. On the Eagle we use AN8 for the oil presssure lines (between engine and oil coolers) and AN10 for the returns. The pressure side can typically be smaller than the return, something about flow under pressure vs flow under suction. Ditto for the coolant lines... 1.25ID for pressure, 1.50ID for suction. I thought you'd be interested.