X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Thu, 29 Nov 2007 14:30:27 -0500 Message-ID: X-Original-Return-Path: Received: from bay0-omc1-s17.bay0.hotmail.com ([65.54.246.89] verified) by logan.com (CommuniGate Pro SMTP 5.2c1) with ESMTP id 2510864 for lml@lancaironline.net; Thu, 29 Nov 2007 11:51:00 -0500 Received-SPF: pass receiver=logan.com; client-ip=65.54.246.89; envelope-from=gary21sn@hotmail.com Received: from hotmail.com ([65.54.250.83]) by bay0-omc1-s17.bay0.hotmail.com with Microsoft SMTPSVC(6.0.3790.3959); Thu, 29 Nov 2007 08:50:22 -0800 Received: from mail pickup service by hotmail.com with Microsoft SMTPSVC; Thu, 29 Nov 2007 08:50:22 -0800 X-Original-Message-ID: Received: from 71.34.227.229 by BAY115-DAV11.phx.gbl with DAV; Thu, 29 Nov 2007 16:50:20 +0000 X-Originating-IP: [71.34.227.229] X-Originating-Email: [gary21sn@hotmail.com] X-Sender: gary21sn@hotmail.com From: "Gary Edwards" X-Original-To: "Lancair Mailing List" References: Subject: Re: linit Gs for 235 (kit #11) X-Original-Date: Thu, 29 Nov 2007 08:50:17 -0800 MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_039C_01C83264.DD70BA50" X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: MSN 9 X-MimeOLE: Produced By MSN MimeOLE V9.50.0039.1900 Seal-Send-Time: Thu, 29 Nov 2007 08:50:17 -0800 X-OriginalArrivalTime: 29 Nov 2007 16:50:22.0262 (UTC) FILETIME=[EE841560:01C832A7] X-Original-Return-Path: gary21sn@hotmail.com This is a multi-part message in MIME format. ------=_NextPart_000_039C_01C83264.DD70BA50 Content-Type: text/plain; charset="Windows-1252" Content-Transfer-Encoding: quoted-printable The gross limit for the 235 is because of the airframe. The airframe is = different than the 320/360 airframe. If a 290 or 320 engine is = installed on a 235 airframe, the gross weight is still the same. The = factory subsequently raised the gross weight for the 235 airframe to = 1,500# on take-off and 1,400# on landing. Gary Edwards LNC2 Medford, Oregon Getting close to asking for airworthiness... and noticed my Pilots = Operating Handbook gives Limit Gs' allowed as 4.5, but does not specify = for which of the three airframes the POH covers: 235, 320 and 360. It also gives allowable gross as 1400# for the 235, and 1685# for the = 320 and 360. Sounds like the gross limit for the 235 is because of lower HP, not = airframe... do you have a reference spec?=20 thanks, Terrence O'Neill ------=_NextPart_000_039C_01C83264.DD70BA50 Content-Type: text/html; charset="Windows-1252" Content-Transfer-Encoding: quoted-printable

The gross limit for the 235 is because of the airframe. The=20 airframe is different than the 320/360 airframe. If a = 290 or 320=20 engine is installed on a 235 airframe, the gross weight is still the = same. =20 The factory subsequently raised the gross weight for the 235 airframe to = 1,500#=20 on take-off and 1,400# on landing.

Gary Edwards

LNC2

Medford, Oregon

Getting close to = asking for=20 airworthiness... and noticed my Pilots Operating Handbook gives = Limit Gs'=20 allowed as 4.5, but does not specify for which of the three airframes = the POH=20 covers: 235, 320 and 360.

It also gives = allowable gross=20 as 1400# for the 235, and 1685# for the 320 and = 360.

Sounds like the = gross limit=20 for the 235 is because of lower HP, not airframe... do you have a=20 reference spec?

thanks,

Terrence=20 O'Neill

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