Return-Path: Received: from aircraftersllc.com ([209.66.74.134]) by truman.olsusa.com (Post.Office MTA v3.5.1 release 219 ID# 0-64832U3500L350S0V35) with ESMTP id com for ; Tue, 15 Feb 2000 22:55:50 -0500 Received: from larry [216.126.137.31] by aircraftersllc.com with ESMTP (SMTPD32-5.01) id AFDC3710210; Tue, 15 Feb 2000 19:56:12 PST Message-ID: <00df01bf7832$9f2eb700$5d887ed8@larry> From: "Larry Graves" To: Jürgen Weber Cc: "Lancair Builders Group" , "Dave Saylor" References: <38A30089.9C9F6A6A@t-online.de> Subject: Re: Bird-strike repairs Date: Tue, 15 Feb 2000 19:58:02 -0800 X-Mailing-List: lancair.list@olsusa.com Mime-Version: 1.0 <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> << Lancair Builders' Mail List >> <<<<<<<<<<<<<<<<--->>>>>>>>>>>>>>>> >> Hello Jurgen, Didn't see any replies to your question on repairing the bird strike damage to your 320 wing leading edge, though there may have been some sent to you privately. There are some very good repair guidelines and recommendations for restoring damaged composite material in the latest edition of AC43.13 -- Acceptable Methods, Techniques and Practices -- Aircraft Inspection and Repair. The following procedure assumes the glass fibers have been structurally damaged, and that the glass itself should be replaced (e.g. not simply a cosmetic blemish). We use the following method when repairing composite leading edge sections that are not acting as the wall of a fuel cell: The repair is easier to make if the wing panel is removed and oriented leading-edge-up, but it can be done with the wing panel on the aircraft if you are careful, and a contortionist. First, "tap out" the area of damaged fiberglass to determine the size of the repair. Using a very small (2-oz) brass hammer, or even a quarter-dollar piece, continually tap the area of apparent damage, starting well away from the damaged spot, moving toward the damage until the sound of the tapping changes. This signals a density change in the material due to the damage. The tapping should produce a sharp high-pitched sound on healthy structure, and a dull thud on damaged areas. Mark the transition zone with a felt-tipped pen. Tap the area from every direction, moving toward the damage, and make a mark where the sound begins to change. Soon you will have a "map" of the damaged area. (Also, be aware that any pre-existing structure behind the leading edge in that area such as a rib, etc., will cause the sound to change as well.) Then, make a piece of pre-molded 2-ply Bi-Directional (BID) cloth layup in the exact shape of the leading edge that has been damaged. This layup will be used as a backing plate for the section under repair. Make this layup by taping a large piece of thin plastic (.35 mil to 1 mil thick) barrier sheet over the leading edge of your wing, immediately adjacent to (but not right on top of) the damaged area. Cut two pieces of BID cloth large enough to easily cover the entire damaged area, with plenty of overlap around the edges. Alternate the orientation of the weave of these two fiberglass pieces by 45-degrees. Brush a layer of resin onto the plastic sheet and then add the first piece of BID, wetting it out and chasing the bubbles by stippling with the brush ends. Add the second layer, with the cloth weave at a 45-degree angle to the weave of the first piece, and wet this out as well. Though not necessary, you could also lay on a piece of peel-ply at this point and squeegee out any excess resin and air. Be quick to catch and wipe up any resin drips heading for your nice finish at the edge of the plastic sheet... (Use a big piece of plastic.) Allow the layup to cure, then remove it and all the plastic and tape from the wing. You should now have a thin piece of fiberglass, pre-molded exactly to your leading edge shape. Now the scary part. Using a Dremel tool with a cutoff wheel, cut the damaged section of leading edge out of the wing. Sand an extremely wide feathered bevel (shallow angle) into the edge of the hole by hand with 100- or 120-grit so that the sanded margin resembles a wide beach all the way around the hole. For example if the area you cut out was 1-inch by 2-inches, the sanded margin should should extend at least several inches beyond the hole all around, for a total area of at least 4-inches by 5-inches. The existing fiberglass wing-skin thickness of the sanded margin area should feather down to almost nothing at the edge of the cutout. Technically, we are looking for a 30-1 bevel, so if the skin is 1/8" thick, the sanded margin should extend back 30 x 1/8", or 3-1/2" all around. Now lay your pre-molded BID layup piece directly over the sanded hole and draw a line all the way around the actual hole with a 1-inch margin all around. Cut this piece out with scissors or tin snips, and then drill a 1/8" hole in the center of the piece at the apex of the leading edge curve. Run a string through this hole into the interior of the curved backing piece and tie it to a piece of wooden dowel or a wooden coffee-stirrer slightly shorter than the long axis of the backing piece. Hot glue or epoxy this stick in place. Carefully make sure you can insert the backing piece by folding it gently and slipping it into the interior of the wing leading edge, then pulling it tight with the string up against the interior of the wing leading edge and centering it in the cutout hole. If you are repairing a larger hole, several of these string-pulls may be needed, spaced out around the backing piece. Next, simply brush resin onto the perimeter of the backing piece and into the interior surface of the prepared hole, and pull the backing piece with the string-pull tightly up against the interior curve of the leading edge, centered in the hole, and allow to cure. Use your creative ingenuity to rig up something that will keep a nice tension on the string-pull while things cure. Wipe up any excess or squeezed-out resin on the exterior of the area under repair before it sets up. Make sure you have bonded the dowel or coffee-stirring stick into the interior of the backing piece too, since you don't want it rattling around inside your wing... Once this backing piece has cured, cut the string off flush with the exterior and lightly sand the overall repair area again to break the glaze of any resin that has cured on the outside surface. Cut several pieces of BID cloth, with the first piece just fitting the area of the original hole cutout. The next piece should be 1/2" larger all around, and the next 1/2" larger and so on, alternating the orientation of the cloth weave. Since each layer of BID cloth when cured is about .040" thick, it will take about 4 layers of BID to repair a 1/8" skin. Wet out each layer of BID right on the repair with resin, starting with the smallest piece first and ending up with the largest piece, which should overlay most of the sanded area. Cover this with a final layer of peel-ply, and cover the peel ply with more of the thin plastic sheet. Squeege out any excess resin and air. Take care not to dent or deform the basic layup when using the squeege. Wipe up any excess resin and allow the repair to cure. When fully cured, remove the plastic and peel-ply, and you should have a nearly-finished repaired surface. Fill with Poly-Fiber's Super-Fil or a similar dry micro-balloon/resin mix, and once cured, sand to a ready-for-primer surface. We've got .jpg photos of most of these steps, so if you want them, let us know & I'll post them to the list or send them privately to you. Hope this helps! Larry Graves & Dave Saylor AirCrafters Builder Assistance Center 5810 Obata Way Unit 7 Gilroy, CA 95020 Tel 408-847-5957 Fax 408-847-6957 www.AirCraftersLLC.com >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>> LML website: http://www.olsusa.com/Users/Mkaye/maillist.html Builders' Bookstore: http://www.buildersbooks.com/lancair Please send your photos and drawings to marvkaye@olsusa.com. >>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>>