X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Mon, 03 Aug 2009 11:16:59 -0400 Message-ID: X-Original-Return-Path: Received: from mta21.charter.net ([216.33.127.81] verified) by logan.com (CommuniGate Pro SMTP 5.2.15) with ESMTP id 3793219 for lml@lancaironline.net; Mon, 03 Aug 2009 10:26:25 -0400 Received-SPF: pass receiver=logan.com; client-ip=216.33.127.81; envelope-from=troneill@charter.net Received: from imp11 ([10.20.200.11]) by mta21.charter.net (InterMail vM.7.09.01.00 201-2219-108-20080618) with ESMTP id <20090803142542.FZQB3344.mta21.charter.net@imp11> for ; Mon, 3 Aug 2009 10:25:42 -0400 Received: from axs ([75.132.241.174]) by imp11 with smtp.charter.net id PqRi1c00B3mUFT705qRi3G; Mon, 03 Aug 2009 10:25:42 -0400 X-Original-Message-ID: <64F1237BA5604F7DACE6A1ABE801A206@axs> From: "terrence o'neill" X-Original-To: "Lancair Mailing List" References: Subject: Re: [LML] Build with maintenance in mind X-Original-Date: Mon, 3 Aug 2009 09:25:47 -0500 MIME-Version: 1.0 Content-Type: text/plain; format=flowed; charset="utf-8"; reply-type=response Content-Transfer-Encoding: 7bit X-Priority: 3 X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook Express 6.00.2900.5512 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.5579 Excellent note. Don't know how many times I'v e complained about the archaic cowl attachment used by our 235/320. On my (own designed) last planes, the Model W and the Magnum, both had cowls that opened in a few seconds (with gloves on), with four camlocks from an old BT-13 cowl. Instead, trying to live with this project, I've had the cowl off and on, top and bottom, at LEAST 30 to 40 times. How much time did I save by not redesigning it to fast-open? How about some tips on modifying our projects for maintenance --dos and don'ts--? Terrence N211AL 13 hours... cowl off again! and header too, to modify the failed quantity gages. ----- Original Message ----- From: "Tom Gourley" To: Sent: Monday, August 03, 2009 06:53 Subject: [LML] Build with maintenance in mind > This is a suggestion brought about by a problem I found on my plane and > the recent LML series on cowling fasteners. When deciding how to build > something, like the cowl fastenings, coming up with some really slick > method is fine; as long as it doesn't make it a hassle to remove pieces > for maintenance access and inspection. In my experience if the cowl, or > some access panel, is a pain to remove people tend not to remove it unless > they really have to; like the required yearly inspections. If it's simple > to remove inspections are likely to happen more often. > > Case in point. I currently fly a Rockwell Commander 112. (Apparently I'm > trying to find out just how long you can make a Legacy project last, but > that's another story.) A couple of months ago my A&P and I replaced all > four cylinder assemblies on the 112; high oil consumption. (Another long > story. I've got a lot of them.) The 112's cowl is fiberglass and the > upper half is a snap to remove. I can do it by myself less than 60 > seconds. With the top cowl removed you can inspect pretty much everything > with a flashlight and mirror. For the first few hours after replacing the > cylinders I removed the upper cowl after every flight and did a visual > inspection. After that I removed the cowl every 2 to 3 hours for visual > inspection up to about 15 or 16 hours. The only problem found was during > the inspection after the first flight. One of the nuts on a fuel > injection line wasn't tightened properly and we found a small amount of > blue stain from the 100LL on the injector line. Easy fix. > > After 15+ hours with no more problems I figured everything was fine, but > at a little over 20 hours I popped the cowl anyway and took a look around, > and found a large oil patch on the bottom cowl. The oily area was about > the size of a dinner plate and since the inside of the 112's cowl is rough > fiberglass it meant there was a pretty serious leak; one that wasn't there > at 15-16 hours. A little flashlight and mirror work traced the source to > a fitting on the #4 cylinder oil return line where it goes into the > cylinder head. I was able to tighten the fitting's compression nut almost > a full turn with just my thumb and one finger! I don't like to think > about what might have happened if I'd put off the inspection a few more > hours. (And yes, the other nuts were all tight.) > > Bottom line, frequent inspections are a good thing. Finding a problem in > the hanger is much better than finding one in flight. Build safe. > > Tom Gourley > > > -- > For archives and unsub > http://mail.lancaironline.net:81/lists/lml/List.html