Return-Path: Sender: (Marvin Kaye) To: lml@lancaironline.net Date: Tue, 09 Mar 2004 13:24:00 -0500 Message-ID: X-Original-Return-Path: Received: from [63.150.227.63] (HELO admsmxs2usr10.ad.jocoks.com) by logan.com (CommuniGate Pro SMTP 4.1.8) with ESMTP id 3070647 for lml@lancaironline.net; Tue, 09 Mar 2004 11:20:26 -0500 X-MimeOLE: Produced By Microsoft Exchange V6.0.6487.1 Content-Class: urn:content-classes:message MIME-Version: 1.0 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: quoted-printable Subject: RE: [LML] Re: LNC2 Flap Rods X-Original-Date: Tue, 9 Mar 2004 10:20:25 -0600 X-Original-Message-ID: <4B9B1B1833408C40AE2F14A881F276F601D6AC62@admsmxs2usr10.ad.jocoks.com> X-MS-Has-Attach: X-MS-TNEF-Correlator: Thread-Topic: [LML] Re: LNC2 Flap Rods thread-index: AcQFSJgvPJCPqWfJQx+t5Ux75iI2KQAqRp2g From: "Metcalfe, Lee, AIR" X-Original-To: "Lancair Mailing List" =20 Based on the input I've gotten (some off-list) and a conversation with Vern, I'm going to have rods fabricated to match the length of the old rods. Both Vern and Grayhawk urged me to avoid re-rigging the flap system if at all possible if the plane flies satisfactorily as it is currently rigged, which it does. In case anybody is wondering, the rods are 4130 hardened after threading. Lee