X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Tue, 21 Jun 2011 14:59:04 -0400 Message-ID: X-Original-Return-Path: Received: from ndmsnpf02.ndc.nasa.gov ([198.117.0.122] verified) by logan.com (CommuniGate Pro SMTP 5.4.0) with ESMTP id 5027628 for lml@lancaironline.net; Tue, 21 Jun 2011 12:13:03 -0400 Received-SPF: none receiver=logan.com; client-ip=198.117.0.122; envelope-from=michael.s.reinath@nasa.gov Received: from ndjsppt03.ndc.nasa.gov (ndjsppt03.ndc.nasa.gov [198.117.1.102]) by ndmsnpf02.ndc.nasa.gov (Postfix) with ESMTP id AFD80108448 for ; Tue, 21 Jun 2011 11:12:26 -0500 (CDT) Received: from ndjshub01.ndc.nasa.gov (ndjshub01-pub.ndc.nasa.gov [198.117.1.160]) by ndjsppt03.ndc.nasa.gov (8.14.4/8.14.4) with ESMTP id p5LGCM73008889 for ; Tue, 21 Jun 2011 11:12:26 -0500 Received: from NDJSSCC06.ndc.nasa.gov ([198.117.4.176]) by ndjshub01.ndc.nasa.gov ([198.117.1.160]) with mapi; Tue, 21 Jun 2011 11:12:24 -0500 From: "Reinath, Michael S. (ARC-AM)" X-Original-To: Lancair Mailing List X-Original-Date: Tue, 21 Jun 2011 11:12:23 -0500 Subject: 360 Dukes Fuel Pump Thread-Topic: 360 Dukes Fuel Pump Thread-Index: AcwwLgD7quwVzJDQnEGdIQ2jPNjNuQ== X-Original-Message-ID: Accept-Language: en-US Content-Language: en-US X-MS-Has-Attach: X-MS-TNEF-Correlator: user-agent: Microsoft-Entourage/13.8.0.101117 acceptlanguage: en-US Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: quoted-printable MIME-Version: 1.0 X-Proofpoint-Virus-Version: vendor=fsecure engine=2.50.10432:5.4.6813,1.0.148,0.0.0000 definitions=2011-06-21_07:2011-06-21,2011-06-21,1970-01-01 signatures=0 I am going to have my Dukes fuel pump overhauled. The pump I bought from Lancair around 1998 for the fuel injected 360 is a model 1500-00-67. I talked with someone at CJ Aviation about having it overhauled. He said that this model is a large-rotor pump, and that I should consider converting it to a small-rotor pump during the overhaul. It would then probably last longer since it is not bypassing so much fuel while it is running. Anyone have an opinion on this? Is there a good reason to have a large-roto= r pump for a Lycoming IO360. The guy at CJ Aviation seemed to think it was oversize for this engine and that the small-rotor pump would be a better match. The data plate on my pump says it flows 30 GPH at 22.5 psi, which does seem a bit high for an IO360, doesn't it? I would appreciate any guidance on this. Mike Reinath LNC2 360 at 1080 hrs San Jose, CA