Return-Path: Sender: "Marvin Kaye" To: lml@lancaironline.net Date: Mon, 20 Dec 2004 00:27:30 -0500 Message-ID: X-Original-Return-Path: Received: from imo-d23.mx.aol.com ([205.188.139.137] verified) by logan.com (CommuniGate Pro SMTP 4.2.5) with ESMTP id 573600 for lml@lancaironline.net; Sun, 19 Dec 2004 22:35:51 -0500 Received-SPF: pass receiver=logan.com; client-ip=205.188.139.137; envelope-from=Sky2high@aol.com Received: from Sky2high@aol.com by imo-d23.mx.aol.com (mail_out_v37_r3.8.) id q.f6.46350e1a (3310) for ; Sun, 19 Dec 2004 22:35:19 -0500 (EST) From: Sky2high@aol.com X-Original-Message-ID: X-Original-Date: Sun, 19 Dec 2004 22:35:19 EST Subject: Re: [LML] Thanks for the help - 235 pitch trim problem X-Original-To: lml@lancaironline.net MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="-----------------------------1103513719" X-Mailer: 9.0 Security Edition for Windows sub 5000 -------------------------------1103513719 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit In a message dated 12/19/2004 7:26:39 P.M. Central Standard Time, rick@belleaireaviation.com writes: As near as I can tell, the stab is installed on the airplane with about 1 1/2 degrees nose up incidence. According to the manual, it should be 1/2 degree nose down incidence. Rick, Bummer. I think you should check the main wing incidence, washout, and dihedral before major surgery. Some 320 360 fliers have replaced the original installed small horizontal stab with the larger one. I am not suggesting you do that but they may be able to describe the procedures they used to perform the replacement and that may be useful to you when the surgery is begun to reposition the stab. Good Luck. Scott Krueger AKA Grayhawk N92EX IO320 Aurora, IL (KARR) Some Assembly Required Using Common Hand Tools And a Digital Level. -------------------------------1103513719 Content-Type: text/html; charset="US-ASCII" Content-Transfer-Encoding: quoted-printable

In a message dated 12/19/2004 7:26:39 P.M. Central Standard Time,=20 rick@belleaireaviation.com writes:

<= FONT=20 style=3D"BACKGROUND-COLOR: transparent" face=3DArial color=3D#000000 size= =3D2>As near=20 as I can tell, the stab is installed on the airplane with about 1 1/2 degr= ees=20 nose up incidence. According to the manual, it should be 1/2 degree=20= nose=20 down incidence.

Rick,

Bummer.

I think you should check the main wing incidence, washout, and dihedral= =20 before major surgery.

Some 320 360 fliers have replaced the original installed small horizont= al=20 stab with the larger one. I am not suggesting you do that but the= y=20 may be able to describe the procedures they used to perform the replace= ment=20 and that may be useful to you when the surgery is begun to reposition the=20 stab.

Good Luck.=20

Scott Krueger=20 AKA Grayhawk
N92EX IO320 Aurora, IL (KARR)

Some Assembly Required=20
Using Common Hand Tools

And a Digital Level.

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