Return-Path: Sender: (Marvin Kaye) To: lml Date: Tue, 30 Apr 2002 13:45:05 -0400 Message-ID: X-Original-Return-Path: Received: from [208.26.246.18] (HELO dewey.Cadwell.cadwell.com) by logan.com (CommuniGate Pro SMTP 3.5.9) with ESMTP id 1203416 for lml@lancaironline.net; Mon, 29 Apr 2002 12:48:32 -0400 content-class: urn:content-classes:message MIME-Version: 1.0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Subject: Engine hesitation X-MimeOLE: Produced By Microsoft Exchange V6.0.4712.0 X-Original-Date: Mon, 29 Apr 2002 09:47:19 -0700 X-Original-Message-ID: X-MS-Has-Attach: X-MS-TNEF-Correlator: Thread-Topic: Engine hesitation Thread-Index: AcHvniGPqVab4t1uR3aMqU75gcVogw== From: "Carl Cadwell" X-Original-To: "Lancair Mailing List" X-Original-Cc: , Comment from Gary Casey: What if the shaft seal leaked air into the pump, even though it is effective in keeping the fuel from leaking out. After a few minutes at altitude it has enough air in it to essentially vapor lock for a few seconds. Wouldn't it be good to put the pump in an insulated compartment forward of the firewall? I know, no room. Gary, This is a scenario we considered. As the pump is running continuously above 10k, nothing really changes if the 5psi differential were pushing air in through a leak. I would also expect to find blue stain somewhere, which there was none. We also plugged the drain/vent which would or could be the potential source. This did not help. Again for those who did not catch the previous posts, the only thing that has solved the hesitation on switching tanks the first time has been to lower the fuel pump to the floor. I climb full rich to altitude, pull back the RPM and Manifold to cruise, switch tanks and then lean. No more hesitations in 17 flight to FL 220-250. Mark at Lancair has pictures. markm@lancair.com Carl Cadwell, N25CL, IVP