X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Sun, 09 Jun 2013 17:34:48 -0400 Message-ID: X-Original-Return-Path: Received: from mail-ie0-f173.google.com ([209.85.223.173] verified) by logan.com (CommuniGate Pro SMTP 6.0.5) with ESMTPS id 6315521 for lml@lancaironline.net; Sun, 09 Jun 2013 08:20:28 -0400 Received-SPF: pass receiver=logan.com; client-ip=209.85.223.173; envelope-from=doramsey@gmail.com Received: by mail-ie0-f173.google.com with SMTP id k5so7654547iea.32 for ; Sun, 09 Jun 2013 05:19:54 -0700 (PDT) MIME-Version: 1.0 X-Received: by 10.50.50.164 with SMTP id d4mr2291437igo.69.1370780394002; Sun, 09 Jun 2013 05:19:54 -0700 (PDT) Received: by 10.64.8.111 with HTTP; Sun, 9 Jun 2013 05:19:53 -0700 (PDT) X-Original-Date: Sun, 9 Jun 2013 08:19:53 -0400 X-Original-Message-ID: Subject: Lancair IV nose strut From: Dennis Ramsey X-Original-To: Lml Content-Type: multipart/alternative; boundary=047d7bdc186a73278c04deb7ae28 --047d7bdc186a73278c04deb7ae28 Content-Type: text/plain; charset=ISO-8859-1 Just days before my first conditional inspection was due, I noticed my nose strut was lowered with only about inch to 1.5 inches before bottoming out. I dont have any experience with struts and assumed some slow leakage must have occurred over the year and I reinflated the strut during the conditional inspection. Over the next 24 hours the strut lowered again. I pressurized again thinking maybe I got a piece of trash in the shrader valve and it was leaking. Once again it deflated slowly. I checked for external leaks with soapy water on the shrader valve and all the fittings and have found none. For background, in the final stages of construction I took my old kits strut and sent to Lancair and had them overhaul it and install the new centering device. That was 6-9 months before first flight. In the first year I put 210 hours on the bird with approximately 200 landings. I fortunately had no hard landings during that time period. So I have some sort of failing strut in what I consider a relatively short period of time. Is this normal? Does anyone have a troubleshooting manual or ideas? All I can come up with is that perhaps the top o-ring is leaking nitrogen into the oil side. The only evidence I can think of for that is that when charged with 300psi, the strut extends to 2 5/8 inch exposed shaft. I seem to recall that I had 3 inches when I pressurized it during install. Perhaps further evidence or at least confusion on my part is that after inflation I get a small amount of some sort of oil out the shrader valve as I remove the nitrogen connection. I would not think that oil should be up there. Any help would be appreciated. --047d7bdc186a73278c04deb7ae28 Content-Type: text/html; charset=ISO-8859-1 Content-Transfer-Encoding: quoted-printable Just days before my first conditional inspection was due, I noticed my nose= strut was lowered with only about inch to 1.5 inches before bottoming out.= =A0=A0 I dont have any experience with struts and assumed some slow leakag= e must have occurred over the year and I reinflated the strut during the co= nditional inspection. =A0 Over the next 24 hours the strut lowered again. = =A0I pressurized again thinking maybe I got a piece of trash in the shrader= valve and it was leaking. =A0Once again it deflated slowly. =A0 I checked= =A0for external leaks with soapy water on the shrader valve and all the fit= tings and have found none. =A0=A0

For background, in the final stages of construction I took m= y old kits strut and sent to Lancair and had them overhaul it and install t= he new centering device. =A0 That was 6-9 months before first flight. =A0 I= n the first year I put 210 hours on the bird with approximately 200 landing= s. =A0I fortunately had no hard landings during that time period. =A0

So I have some sort of failing strut in what I consider= a relatively short period of time. =A0Is this normal? =A0 Does anyone have= a troubleshooting manual or ideas? =A0All I can come up with is that perha= ps the top o-ring is leaking nitrogen into the oil side. =A0 The only evide= nce I can think of for that is that when charged with 300psi, the strut ext= ends to 2 5/8 inch exposed shaft. =A0I seem to recall that I had 3 inches w= hen I pressurized it during install. =A0 Perhaps further evidence or at lea= st confusion on my part is that after inflation I get a small amount of som= e sort of oil out the shrader valve as I remove the nitrogen connection. = =A0I would not think that oil should be up there. =A0Any help would be appr= eciated.

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