Return-Path: Sender: (Marvin Kaye) To: lml Date: Sun, 24 Aug 2003 21:07:13 -0400 Message-ID: X-Original-Return-Path: <2thman@olympus.net> Received: from mail2.bllvwa.cablespeed.com ([66.235.59.9] verified) by logan.com (CommuniGate Pro SMTP 4.1.1) with SMTP id 2545281 for lml@lancaironline.net; Sun, 24 Aug 2003 19:17:46 -0400 Received: (qmail 26412 invoked by uid 0); 24 Aug 2003 23:17:37 -0000 Received: from unknown (HELO JohnHome) (66.235.31.92) by 0 with SMTP; 24 Aug 2003 23:17:37 -0000 From: "John Barrett" <2thman@olympus.net> X-Original-To: "Lancair Mailing List" Subject: RE: [LML] Damaged Fuselege X-Original-Date: Sun, 24 Aug 2003 16:17:32 -0700 X-Original-Message-ID: MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="----=_NextPart_000_0041_01C36A5B.391BD780" X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook IMO, Build 9.0.2416 (9.0.2910.0) X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2727.1300 Importance: Normal In-Reply-To: This is a multi-part message in MIME format. ------=_NextPart_000_0041_01C36A5B.391BD780 Content-Type: text/plain; charset="us-ascii" Content-Transfer-Encoding: 7bit bill, I have a 6 page document that spells out repair process for laminate structures. There is a hand written note at the top stating it is from "Aircraft Repair/Inspection and Alteration FAA EA-AC 43.13 - 1A & 2A (Rev.) If you wish I can FAX it to you in the next day or two. let me know your FAX number if you so desire. Regards, John Barrett Barrett/Garrett Enterprises, Inc. PO Box 428 Pt. Hadlock, WA 98339 www.carbinge.com -----Original Message----- From: Lancair Mailing List [mailto:lml@lancaironline.net]On Behalf Of Billhogarty@aol.com Sent: Sunday, August 24, 2003 8:59 AM To: Lancair Mailing List Subject: [LML] Damaged Fuselege Need suggestion for honeycomb repair. When picking up plane from Las Vegas, it appears that someone used a floor jack underneath the main spar tunnel. The floor of the tunnel is broken thru in a half-moon circular shape and protrudes up into the spar area about 3/4 inch. If I apply pressure, I can force the material back into place. I realize that there must be a preferred method to make this repair. I hope someone will take the time to enlighten me. Thanks, Bill Hogarty ------=_NextPart_000_0041_01C36A5B.391BD780 Content-Type: text/html; charset="us-ascii" Content-Transfer-Encoding: quoted-printable
bill,
 
I have=20 a  6 page document that spells out repair process for laminate=20 structures.  There is a hand written note at the top stating it is = from=20 "Aircraft Repair/Inspection and Alteration FAA EA-AC 43.13 - 1A & 2A = (Rev.)
 
If you=20 wish I can FAX it to you in the next day or two.
 
let me=20 know your FAX number if you so desire.
 

Regards,
John Barrett
Barrett/Garrett = Enterprises,=20 Inc.
PO Box 428
Pt. Hadlock, WA 98339
www.carbinge.com=20

-----Original Message-----
From: Lancair Mailing = List=20 [mailto:lml@lancaironline.net]On Behalf Of=20 Billhogarty@aol.com
Sent: Sunday, August 24, 2003 8:59=20 AM
To: Lancair Mailing List
Subject: [LML] Damaged = Fuselege


Need=20 suggestion for honeycomb repair.  When picking up plane from Las = Vegas,=20 it appears that someone used a floor jack underneath the main spar=20 tunnel.  The floor of the tunnel is broken thru in a half-moon = circular=20 shape and protrudes up into the spar area about 3/4 inch.  If I = apply=20 pressure, I can force the material back into place.

I realize = that=20 there must be a preferred method to make this repair.  I hope = someone=20 will take the time to enlighten me.

Thanks, Bill Hogarty =
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