X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Wed, 07 May 2008 09:32:08 -0400 Message-ID: X-Original-Return-Path: Received: from bay0-omc3-s22.bay0.hotmail.com ([65.54.246.222] verified) by logan.com (CommuniGate Pro SMTP 5.2.2) with ESMTP id 2900092 for lml@lancaironline.net; Mon, 05 May 2008 20:12:17 -0400 Received-SPF: pass receiver=logan.com; client-ip=65.54.246.222; envelope-from=gary21sn@hotmail.com Received: from hotmail.com ([10.4.19.14]) by bay0-omc3-s22.bay0.hotmail.com with Microsoft SMTPSVC(6.0.3790.3959); Mon, 5 May 2008 17:11:40 -0700 Received: from mail pickup service by hotmail.com with Microsoft SMTPSVC; Mon, 5 May 2008 17:11:40 -0700 X-Original-Message-ID: Received: from 68.186.114.52 by BLU130-DAV4.phx.gbl with DAV; Tue, 06 May 2008 00:11:35 +0000 X-Originating-IP: [68.186.114.52] X-Originating-Email: [gary21sn@hotmail.com] X-Sender: gary21sn@hotmail.com From: "Gary Edwards" X-Original-To: "Lancair Mailing List" References: Subject: Re: limit Gs for 235 X-Original-Date: Mon, 5 May 2008 17:11:35 -0700 MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_1AE2_01C8AED3.12A98090" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: MSN 9 X-MimeOLE: Produced By MSN MimeOLE V9.50.0039.1900 Seal-Send-Time: Mon, 5 May 2008 17:11:35 -0700 X-OriginalArrivalTime: 06 May 2008 00:11:40.0397 (UTC) FILETIME=[C1FB59D0:01C8AF0D] X-Original-Return-Path: gary21sn@hotmail.com This is a multi-part message in MIME format. ------=_NextPart_000_1AE2_01C8AED3.12A98090 Content-Type: text/plain; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable Terrance, The bigger wing spar was for the 320/360 airframes. There is no specific spar changes to the 235's before, at, or after Kit = #11 during the 235 model run. That kit number (#11) is only there = because of your or someone else's reference in sending a post to the = LML. Gary =20 ----- Original Message -----=20 From: terrence o'neill=20 To: lml@lancaironline.net=20 Sent: Sunday, May 04, 2008 8:06 PM Subject: [LML] Re: limit Gs for 235 (kit #11) Thanks, Gary. Now I have it printed out and in the Performance = folder. Two more questions:=20 1.As someone commented that Lance later increased the wing sparcap = thickness and re-tested... was that done just for the 320 kits, not the = 235 wing ... i.e. kit # 11.? 2. If so, when would that wing have gone to early kit builders, and = what sparcap thickness measurement, where?=20 Terrence L235/320 N211AL ------=_NextPart_000_1AE2_01C8AED3.12A98090 Content-Type: text/html; charset="iso-8859-1" Content-Transfer-Encoding: quoted-printable
Terrance,
 
The bigger wing spar was for the 320/360 airframes.
 
There is no specific spar changes to the 235's before, at, or after = Kit #11=20 during the 235 model run.  That kit number (#11) is only there = because of=20 your or someone else's reference in sending a post to the LML.
 
Gary
 
     
----- Original Message -----
From: terrence=20 o'neill
Sent: Sunday, May 04, 2008 8:06 = PM
Subject: [LML] Re: limit Gs for = 235 (kit=20 #11)

Thanks, Gary.  Now I = have it=20 printed out and in the Performance folder.
Two more=20 questions: 
1.As someone = commented that=20 Lance later increased the wing sparcap thickness and re-tested... was = that=20 done just for the 320 kits, not the 235 wing ... i.e. kit # = 11.?
2. If so, when would that = wing have=20 gone to early kit builders, and what sparcap thickness = measurement,=20 where? 
Terrence L235/320 = N211AL =20
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