X-Virus-Scanned: clean according to Sophos on Logan.com X-PolluStop: No license found, only first 5 messages were scanned Return-Path: Sender: To: lml Date: Fri, 23 Jun 2006 21:07:19 -0400 Message-ID: X-Original-Return-Path: Received: from smtp101.sbc.mail.mud.yahoo.com ([68.142.198.200] verified) by logan.com (CommuniGate Pro SMTP 5.1c.1) with SMTP id 1203727 for lml@lancaironline.net; Fri, 23 Jun 2006 14:04:45 -0400 Received-SPF: none receiver=logan.com; client-ip=68.142.198.200; envelope-from=n98pb@sbcglobal.net Received: (qmail 30106 invoked from network); 23 Jun 2006 16:17:22 -0000 Received: from unknown (HELO Sam) (n98pb@sbcglobal.net@69.235.250.64 with login) by smtp101.sbc.mail.mud.yahoo.com with SMTP; 23 Jun 2006 16:17:21 -0000 From: X-Original-To: "'Lancair Mailing List'" , , Subject: MT response to blade issue X-Original-Date: Fri, 23 Jun 2006 09:17:18 -0700 X-Original-Message-ID: <002801c696e0$82834700$0301a8c0@Sam> MIME-Version: 1.0 Content-Type: text/plain; charset="US-ASCII" Content-Transfer-Encoding: 7bit X-Priority: 3 (Normal) X-MSMail-Priority: Normal X-Mailer: Microsoft Outlook, Build 10.0.2627 X-MimeOLE: Produced By Microsoft MimeOLE V6.00.2900.2869 Importance: Normal Please understand that I sent the initial e-mail to the LML based upon what I believed was good information as the only thought I had was concern for those of us flying the MT propellers. With only 620 hours on my prop and the prop shop telling me that the blades needed replaced, I was concerned with safety. The final analysis is not complete but it appears that the overhaul manual and initial response to the overhaul shop by MT left American Propeller with no choice but to say the blades were not serviceable. The initial response from MT via email was "Blades, which are cracked in the root, are reject. There is no possibility to repair them." Further amplification by MT suggests that the overhaul manual might need some revision and the communications improved. This was and is a safety issue as far as I am concerned, not an indictment of either MT or American Propeller. Both have been very professional. I don't have a final decision on the blades yet, but I am comfortable that MT will make it right if there is an issue. The following was received by me from MT: "It looks to me that there is a misunderstanding from one of our Service Stations. In our blade root area inside the aluminum blade ferrule it is normal that there are small cracks extending from the lag screws. These cracks are normal and of no concern because the high plastified beech wood is compressed in this area between the outer aluminum ferrule and the inner aluminum bushing where we install the blade balancing weight. This small cracks in the plastified beech wood can do nothing as they are pressed between 2 aluminum parts. Our propeller overhaul station should send a digital picture of what they found. In any case, I am to 100% sure that there is no problem at all and we have more than 35000 blades flying since 25 years and we never lost a blade in flight and therefore you should not worry because definitely this is not an airworthiness issue but just a wrong information. We will also update our blade overhaul manual which addresses this issue that no service station is confused. The 1/16 lines are normal due to the different composition of our blade. Hope this information helps and please keep in mind that MT-Propeller is the only certified propeller manufacturer with no valid AD on hydraulic propellers and also the only one who never lost a blade in flight." American is sending photos of the blades to MT and has suggested that, because of the differing opinions as the serviceability of the blades, we send the blades to Germany for their visual inspection, which I am inclined to do. Both American Propeller and MT have been responsive and factual with their presentations. I believe both parties will be better able to service our community after the resolution and we should be able to sleep easier. I know I will. Pat Brunner N98PB