X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Mon, 13 Jul 2009 11:43:34 -0400 Message-ID: X-Original-Return-Path: Received: from fmailhost01.isp.att.net ([204.127.217.101] verified) by logan.com (CommuniGate Pro SMTP 5.2.14) with ESMTP id 3755442 for lml@lancaironline.net; Mon, 13 Jul 2009 09:36:20 -0400 Received-SPF: pass receiver=logan.com; client-ip=204.127.217.101; envelope-from=n427jb@bellsouth.net Received: from fwebmail30.isp.att.net ([207.115.11.170]) by isp.att.net (frfwmhc01) with SMTP id <20090713133543H0100c69s9e>; Mon, 13 Jul 2009 13:35:43 +0000 X-Originating-IP: [207.115.11.170] Received: from [69.88.226.141] by fwebmail30.isp.att.net; Mon, 13 Jul 2009 13:35:42 +0000 From: n427jb@bellsouth.net X-Original-To: lml@lancaironline.net X-Original-Date: Mon, 13 Jul 2009 13:35:42 +0000 X-Original-Message-Id: <071320091335.28395.4A5B382E000585B200006EEB22243651029B0A02D2089B9A019C04040A0DBF0D06C9CDCB02@att.net> X-Mailer: AT&T Message Center Version 1 (Mar 2 2009) X-Authenticated-Sender: bjQyN2piQGJlbGxzb3V0aC5uZXQ= MIME-Version: 1.0 Content-Type: multipart/alternative; boundary="NextPart_Webmail_9m3u9jl4l_28395_1247492142_0" --NextPart_Webmail_9m3u9jl4l_28395_1247492142_0 Content-Type: text/plain Content-Transfer-Encoding: quoted-printable The incident Bill Edwards describes lacks certain information that I believ= e would be important for those interested in "the rest of the story." Mr. = Edwards aircraft did not order the inspection, thus, Mr. Edwards was not fi= nancially responsible for the inspection. That means that he is not entitl= ed to a copy of the inspection report. Lancair requires that the aircraft = being inspected be located at a facility that maintains jacks sufficient to= lift the aircraft for landing gear operation and inspection as well as oth= er tools and materials that cannot be transported easily or economically to= the inspection site. The jacks and other equipment were available, and th= e aircraft was lifter using that equipment. Mr. Edwards had a different st= yle engine lifting point/pin and it is was this pin that failed during the = retract proceedure. The shifting weight of the aircraft was a major factor= in the jack coming out of the non-standard jack points. Irrespective of w= ho purchased the inspection, or how the jack came out of the jack point, it= is a fact that the jack came out of the jack point and, thankfully, produc= ed only minor damage. Since the damage was to be repaired, our inspector l= eft the interior panels uninstalled. When I heard of this incident, I advi= sed that Lancair would send the inspector back to install the panels upon t= he repairs being made. I even told the new owner that should he get the ai= rcraft to Redmond, we would make the repairs there at no cost to him. A lot has been said on the LML about nose struts. I believe one lister got= it right when he said that ESCO was still in business. They are, however,= they are no longer in the business of making nose struts. These struts ca= nnot easily be overhauled in the field. There are many changes that were m= ade to the strut over the years that they have been in service. Some inclu= de an increased shaft wall thickness, self centering and improved shimmy da= mpning. Shimmy is not exclusively a condition caused by the nose strut. M= any of you have correctly identified the other areas that must be examined = before coming to the conclusion that the shimmy is caused by the condition = of the strut. Tire pressure and tire balance are at the top of the list of= those things you must check. If the shimmy has continued for a extended p= eriod of time, you must check the condition of the engine mount. If the en= gine mount is damaged, you can be sure that it is contributing to the shimm= y.....but it is not necessarily the underlying cause of the shimmy. Yes, a= s Mr. Edwards has stated, I do have a small shimmy that exhibits itself on = rollout. I have the older ESCO strut. My strut does need to be occasional= ly serviced with Nitrogen as they all do. And yes, my strut has been overh= auled to include the newer parts available through Lancair. Keep in mind that Lancair did not willingly go into this insurance inspecti= on business. It was a requirement to maintain insurance for its customers.= Insurance is a necessary evil. If you want it you have to do comply with= the requirements established by AIG Insurance. I don't like it but there = it is! Keep training, fly safely, and maybe our rates and these requiremen= ts will be lowered. Joe=20=20 --NextPart_Webmail_9m3u9jl4l_28395_1247492142_0 Content-Type: multipart/related; boundary="NextPart_Webmail_9m3u9jl4l_28395_1247492142_1" --NextPart_Webmail_9m3u9jl4l_28395_1247492142_1 Content-Type: text/html; charset="utf-8" Content-Transfer-Encoding: quoted-printable
The incident Bill Edwards describes lacks certain information that I b= elieve would be important for those interested in "the rest of the story."&= nbsp; Mr. Edwards aircraft did not order the inspection, thus, Mr. Edwards = was not financially responsible for the inspection.  That means that h= e is not entitled to a copy of the inspection report.  Lancair require= s that the aircraft being inspected be located at a facility that maintains= jacks sufficient to lift the aircraft for landing gear operation and inspe= ction as well as other tools and materials that cannot be transported easil= y or economically to the inspection site.  The jacks and other equipme= nt were available, and the aircraft was lifter using that equipment.  = Mr. Edwards had a different style engine lifting point/pin and it is was th= is pin that failed during the retract proceedure.  The shifting weight= of the aircraft was a major factor in the jack coming out of the non-stand= ard jack points.  Irrespective of who purchased the inspection, or how= the jack came out of the jack point, it is a fact that the jack came out o= f the jack point and, thankfully, produced only minor damage.  Since t= he damage was to be repaired, our inspector left the interior panels uninst= alled.  When I heard of this incident, I advised that Lancair would se= nd the inspector back to install the panels upon the repairs being made.&nb= sp; I even told the new owner that should he get the aircraft to Redmond, w= e would make the repairs there at no cost to him.
 
A lot has been said on the LML about nose struts.  I believe one = lister got it right when he said that ESCO was still in business.  The= y are, however, they are no longer in the business of making nose struts.&n= bsp; These struts cannot easily be overhauled in the field.  There are= many changes that were made to the strut over the years that they have bee= n in service.  Some include an increased shaft wall thickness, self ce= ntering and improved shimmy dampning.  Shimmy is not exclusively a con= dition caused by the nose strut.  Many of you have correctly identifie= d the other areas that must be examined before coming to the conclusion tha= t the shimmy is caused by the condition of the strut.  Tire pressure a= nd tire balance are at the top of the list of those things you must check.&= nbsp; If the shimmy has continued for a extended period of time, you must c= heck the condition of the engine mount.  If the engine mount is damage= d, you can be sure that it is contributing to the shimmy.....but it is not = necessarily the underlying cause of the shimmy.  Yes, as Mr. Edwards h= as stated, I do have a small shimmy that exhibits itself on rollout.  = I have the older ESCO strut.  My strut does need to be occasionally se= rviced with Nitrogen as they all do.  And yes, my strut has been overh= auled to include the newer parts available through Lancair.
 
Keep in mind that Lancair did not willingly go into this insurance ins= pection business.  It was a requirement to maintain insurance for its = customers.  Insurance is a necessary evil.  If you want it y= ou have to do comply with the requirements established by AIG Insuranc= e.  I don't like it but there it is!  Keep training, fl= y safely, and maybe our rates and these requirements will be lowered.<= /DIV>
 
Joe 
--NextPart_Webmail_9m3u9jl4l_28395_1247492142_1-- --NextPart_Webmail_9m3u9jl4l_28395_1247492142_0--