Return-Path: Received: from [65.41.23.202] (account marv@lancaironline.net) by logan.com (CommuniGate Pro WebUser 4.1.8) with HTTP id 2762250 for lml@lancaironline.net; Sat, 22 Nov 2003 18:15:42 -0500 From: "Marvin Kaye" Subject: Re: [LML] Lancair IV Wings To: lml X-Mailer: CommuniGate Pro WebUser Interface v.4.1.8 Date: Sat, 22 Nov 2003 18:15:42 -0500 Message-ID: In-Reply-To: <000001c3b11a$dce88d80$8014a8c0@comp20intel28> MIME-Version: 1.0 Content-Type: text/plain; charset="ISO-8859-1"; format="flowed" Content-Transfer-Encoding: 8bit Posted for "F. Barry Knotts" : Don't know the number of layers. But Advisory Circular AC43.13-1B Acceptable Methods, Techniques, and Practices--Aircraft Inspection and Repair has a note on the method: Chapter 3, Section 1, 3-3 Repairing holes,a. Scarf Method, "(6) The scarfed joint method is normally used on small puctures up to 3 or 4 inches in maximum dimension and in facings that are made of thin fabric that is difficult to peal." The next section describes the Step-Joint method that would be an alternative method or used for a larger defect. AC43.13-1B is occasionally useful. I like it. Barry Knotts LIV-P, Conti TSIO-550 (Probably), 20%, Toledo, Ohio > > Can anyone advise me on the number of carbon cloth layers used for the > > main wing skins? If one needed to repair puncture damage to a wing skin, > > would a scarf-type patch using the same number of layers be adequate if > > the damage is not near any internal components-rib or spar? Thanks, Bob > > Pastusek