Return-Path: Sender: "Marvin Kaye" To: lml@lancaironline.net Date: Sat, 18 Dec 2004 05:03:31 -0500 Message-ID: X-Original-Return-Path: Received: from [64.4.35.180] (HELO hotmail.com) by logan.com (CommuniGate Pro SMTP 4.2.5) with ESMTP id 571907 for lml@lancaironline.net; Sat, 18 Dec 2004 02:06:30 -0500 Received-SPF: pass receiver=logan.com; client-ip=64.4.35.180; envelope-from=gary21sn@hotmail.com Received: from mail pickup service by hotmail.com with Microsoft SMTPSVC; Fri, 17 Dec 2004 23:06:00 -0800 X-Original-Message-ID: Received: from 67.42.59.100 by BAY12-DAV6.phx.gbl with DAV; Sat, 18 Dec 2004 07:05:26 +0000 X-Originating-IP: [67.42.59.100] X-Originating-Email: [gary21sn@hotmail.com] X-Sender: gary21sn@hotmail.com From: "Gary Edwards" X-Original-To: "Lancair Mailing List" Subject: Re: First flight and intro X-Original-Date: Fri, 17 Dec 2004 23:05:25 -0800 MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0068_01C4E48C.E485E0F0" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: MSN 9 X-MIMEOLE: Produced By MSN MimeOLE V9.10.0009.2900 Seal-Send-Time: Fri, 17 Dec 2004 23:05:25 -0800 X-OriginalArrivalTime: 18 Dec 2004 07:06:00.0829 (UTC) FILETIME=[07CAFAD0:01C4E4D0] This is a multi-part message in MIME format. ------=_NextPart_000_0068_01C4E48C.E485E0F0 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable That is exactly how my airplane handles. I accept this for now until I = can look into the pitch trim servo travel limits. I limit the approaches = to half flaps and 90 - 100 mph. Unless the 235 flaps are changed and thus hinged from the bottom, they = are significantly different in range than the 320/360 flaps. 1. They reflex up from neutral (faired in) approx. 9 degrees. 2. Unless significant mods are done, the maximum down flap is about 23 = degrees on the ground and about 19 degrees in flight (from neutral). So, one-half flaps in a 235 airframe is about 9 - 10 degrees which = would be somewhat less than the 320/360 airframe. Gary Edwards LNC2 N21SN 235/320 ------=_NextPart_000_0068_01C4E48C.E485E0F0 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
That is exactly how my airplane handles. I = accept this for=20 now until I can look into the pitch trim servo travel limits. I limit = the=20 approaches to half flaps and 90 - 100 mph.
 
Unless the 235 flaps are changed and thus hinged from the bottom, = they are=20 significantly different in range than the 320/360 flaps.
 
1.  They reflex up from neutral (faired in) approx. 9 = degrees.
 
2.  Unless significant mods are done, the maximum down flap is = about=20 23 degrees on the ground and about 19 degrees in flight (from = neutral).
 
So,  one-half flaps in a 235 airframe is about 9 - 10 = degrees=20 which would be somewhat less than the 320/360 airframe.
 
Gary Edwards
LNC2 N21SN
235/320
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