Return-Path: Sender: (Marvin Kaye) To: lml Date: Wed, 04 Sep 2002 07:49:20 -0400 Message-ID: X-Original-Return-Path: Received: from imo-d07.mx.aol.com ([205.188.157.39] verified) by logan.com (CommuniGate Pro SMTP 4.0b7) with ESMTP id 1721239 for lml@lancaironline.net; Wed, 04 Sep 2002 02:27:52 -0400 Received: from Newlan2dl@aol.com by imo-d07.mx.aol.com (mail_out_v34.10.) id q.22.2e3a17ea (3924) for ; Wed, 4 Sep 2002 02:27:42 -0400 (EDT) From: Newlan2dl@aol.com X-Original-Message-ID: <22.2e3a17ea.2aa701de@aol.com> X-Original-Date: Wed, 4 Sep 2002 02:27:42 EDT Subject: Re: [LML] Aircraft Log X-Original-To: lml@lancaironline.net MIME-Version: 1.0 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit X-Mailer: AOL 7.0 for Windows US sub 10512 Hi Bill (et. al.) I was speaking with a friend of mine that is a DAR (Designated Airworthiness Representative) regarding kit planes and he had a number of suggestions regarding certification, unfortunately you may be too far along to really make any use of it. He provided me with a 4 page list of "reminders" that the FAA inspector should look for. This isn't a formal document but a list of single sentence reminders that says things like "Certificate of compliance on manufactured parts?" "Weave indicators for fabric orientation?", "Areas preped for bonding were sanded without faying the surface" and such. Since I work with him on the airline's "heavy iron" all over the world, we get to talk about these things quite a bit. One of the best pieces of advice he had was to write a QC document to illustrate that you have looked at the parts and pieces, have a way of evaluating them and if required, rejecting them if they are not up to standard. Since I do composite design and fabrication professionally, I plan on keeping retains and testing the resin at regular intervals with gel time and Shore hardness. This shows the inspector (and insurance company and a buyer after I'm ready to move on), that I tested these materials to make sure they were in spec and that they passed my own QC. I may also get a Barcol hardness tester to verify that the prepregs in my kit also pass the test to insure complete cure, or alternately get a cert from Lancair that they have a QC system that certified my parts passed their test and include that with my documentation. And of course this is on top of a log and photo's. I also plan to have production samples that show examples of properly bonded joints and such on some scraps I have of prepreg honeycomb panels. All of this is designed to show the inspector that I know what I'm doing and give him a level of comfort that it was built acording to a prescribed set of rules and not some hobby shopper that can barely stick the plug for his drill into the wall socket. I'll try and scan the document and post it here for everybody to read. Since I am only getting ready to begin, it's not a problem but unfortunately that still doesn't help you much. What I can suggest is that you contact the EAA technical counselor. They are GREAT and can get you the information in the unlikely event they don't know it themselves. Next I'd contact Lancair. Those folks have been absolutely super, as I'm sure you already know. And in the end, and having dealt with the FAA often, I can say that they can require you to do just about anything. If they feel that you have substandard bonds, YOU are the one that has to prove them wrong. They are under no obligation to pass you, and their first priority is not to get your plane flying but to protect everyone else from you. It's for reasons like that which cause most DAR's like my friend to outright not do homebuilts! Dan Newland ES #61