X-Virus-Scanned: clean according to Sophos on Logan.com Return-Path: Sender: To: lml@lancaironline.net Date: Fri, 02 Mar 2012 12:19:20 -0500 Message-ID: X-Original-Return-Path: Received: from imr-db02.mx.aol.com ([205.188.91.96] verified) by logan.com (CommuniGate Pro SMTP 5.4.4) with ESMTP id 5424859 for lml@lancaironline.net; Fri, 02 Mar 2012 08:26:28 -0500 Received-SPF: pass receiver=logan.com; client-ip=205.188.91.96; envelope-from=n5276j@aol.com Received: from mtaomg-ma02.r1000.mx.aol.com (mtaomg-ma02.r1000.mx.aol.com [172.29.41.9]) by imr-db02.mx.aol.com (8.14.1/8.14.1) with ESMTP id q22DPho4001845 for ; Fri, 2 Mar 2012 08:25:43 -0500 Received: from core-mlb004c.r1000.mail.aol.com (core-mlb004.r1000.mail.aol.com [172.29.186.146]) by mtaomg-ma02.r1000.mx.aol.com (OMAG/Core Interface) with ESMTP id 98515E000087 for ; Fri, 2 Mar 2012 08:25:43 -0500 (EST) References: X-Original-To: lml@lancaironline.net Subject: Re: [LML] Re: 320/360 Hydraulic Pressure Switch In-Reply-To: X-MB-Message-Source: WebUI MIME-Version: 1.0 From: steve X-MB-Message-Type: User Content-Type: multipart/alternative; boundary="--------MB_8CEC68F1A9491DF_954_4CF7_webmail-d158.sysops.aol.com" X-Mailer: AOL Webmail 35647-STANDARD Received: from 166.250.7.11 by webmail-d158.sysops.aol.com (205.188.58.143) with HTTP (WebMailUI); Fri, 02 Mar 2012 08:25:43 -0500 X-Original-Message-Id: <8CEC68F1A83E823-954-168C@webmail-d158.sysops.aol.com> X-Originating-IP: [166.250.7.11] X-Original-Date: Fri, 2 Mar 2012 08:25:43 -0500 (EST) x-aol-global-disposition: G X-AOL-SCOLL-SCORE: 0:2:409167104:93952408 X-AOL-SCOLL-URL_COUNT: 0 x-aol-sid: 3039ac1d29094f50ca5760b5 This is a multi-part message in MIME format. ----------MB_8CEC68F1A9491DF_954_4CF7_webmail-d158.sysops.aol.com Content-Transfer-Encoding: quoted-printable Content-Type: text/plain; charset="utf-8" Chris, I have just started flying my 360, have a big total of 3.7 h -----Original Message----- From: Chris Zavatson To: lml Sent: Fri, Mar 2, 2012 5:56 am Subject: [LML] Re: 320/360 Hydraulic Pressure Switch Wolfgang, =20 It is a sad day when removing a pump from the aircraft is too much effort t= o investigate an anomaly.=20 =20 Wolfgang wrote:<> =20 As aircraft owners we are responsible for knowing the configuration of the = aircraft systems. If something is out of the ordinary, investigate. We kn= ow a lot about what the configuration should be and how it works and behave= s. We also know of configurations that do not work. You may very well be = holding the key to a new, as of yet, unidentified failure mode, but we may = never know. =20 Wolfgang wrote: <> =20 If my tire has a flat and I see a nail sticking through the side wall, I am= rather confident in assuming the nail was the source of my leak. Likewise= , if I open up a lock-up prone pump and find return springs, I will have a = high degree of confidence I have found the source of the problem. Could th= ere be a second cause? Possibly, but as of yet, none have been documented. =20 Wolfgang wrote:<<=E2=80=A6original suspicion of the spool coming off it's e= nd point (with the help of springs and airframe vibration) is in fact what'= s causing the problem.>> =20 Springs definitely - that is what they were designed to do. Oildyne starte= d adding springs to center the spool to the Legacy pump in ~2003. Our syst= em will eventually fail if these springs are installed. Fortunately the vas= t majority of our pumps do not have them. If you have springs installed, s= imply remove them. =20 Vibration - the evidence says otherwise. Measurements of various spool and= pump combinations required from 13 g's (9 year old 'soft' o-ring) to 70 g'= s (new 'stiff' o-ring) to move the spool. Aircraft vibration at the pump w= as measured to be +/- 0.1 g (flying) to +/-1.3 g (engine start). Vibration = is not nearly sufficient to have any effect on the spool.=20 =20 Wolfgang wrote:<> The springs are very strong, 26 lb/in. =20 Wolfgang wrote:<> See MIL-STD-810 for expected vibration levels in aircraft environments. =20 Wolfgang wrote:<> I would still like to know how push buttons can overload anything. And why= would anyone want to override more than one at a time? =20 Wolfgang wrote:< I have never had a thermal lock up, yet I use pressure gauges and the momen= tary push buttons on a regular basis. They were originally installed to de= al with sticking VEP switches, but it is like getting a new tool. After yo= u have it, you can't imagine how you lived without out it. I have already = discussed the benefits of momentary switches not related to hydraulic lock-= up. =20 Wolfgang wrote:<> One should label the push buttons appropriately. =20 Wolfgang wrote:<> Recall that the Legacy pump configuration =E2=80=9CCZZ=E2=80=9D is propriet= ary to Lancair. Companies generally don=E2=80=99t post proprietary materia= ls on-line. =20 <> Not really. I avoid them by thorough examination, no matter what it requir= es. =20 Chris Zavatson N91CZ 360std www.N91CZ.net =20 =20 ----------MB_8CEC68F1A9491DF_954_4CF7_webmail-d158.sysops.aol.com Content-Transfer-Encoding: quoted-printable Content-Type: text/html; charset="utf-8"
Chris,
 
I have just started flying my 360, have a big total of 3.7 h



= -----Original Message-----
From: Chris Zavatson <chris_zavatson@yahoo.com>
To: lml <lml@lancaironline.net>
Sent: Fri, Mar 2, 2012 5:56 am
Subject: [LML] Re: 320/360 Hydraulic Pressure Switch

Wolfgang,
 <= /SPAN>
It is a= sad day when removing a pump from the aircraft is too much effort to inves= tigate an anomaly.
 
Wolfgang wrote:<<We= would all like to get at the root cause of the problem but, as yet, that h= asn't happened. Likely because it's too much work to track down the actual = cause and fix it. =E2=80=A6>>
 <= /SPAN>
As airc= raft owners we are responsible for knowing the configuration of the aircraf= t systems.  If something is out of the ordinary, investigate.&nbs= p; We know a lot about what the configuration should be and how it works an= d behaves.  We also know of c= onfigurations that do not work.  You may very well be holding the key to a new, as of yet, uni= dentified failure mode, but we may never know.
 <= /SPAN>
Wolfgang wrote: <<= ;So far we only have a good plausible theory missing only demonstratable pr= oof.>>
 
If my tire has a flat and I see a nail sticking thro= ugh the side wall, I am rather confident in assuming the nail was the sourc= e of my leak.  Likewise, if I= open up a lock-up prone pump and find return springs, I will have a high d= egree of confidence I have found the source of the problem.  Could there be a second cause?  Possibly, but as of yet, none have been documented.
 <= /SPAN>
Wolfgang wrote:<<=E2=80=A6original s= uspicion of the spool coming off it's end point (with the help of springs a= nd airframe vibration) is in fact what's causing the problem.>>
 <= /SPAN>
Springs definitely - that is what they were designed to do.  Oildyne started adding springs to cen= ter the spool to the Legacy pump in ~2003.  Our system will eventually fail if these springs are install= ed. Fortunately the vast majority of our pumps do not have them. =  If you have springs installed, simply remove them.
 <= /SPAN>
Vibrati= on - the evidence says otherwise.  Measurements of various spool and p= ump combinations required from 13 g's (9 year old 'soft' o-ring) = to 70 g's (new 'stiff' o-ring) to move the spool.  Aircraft vibra= tion at the pump was measured to be +/- 0.1 g (flying) to +/-1.3 g (engine = start). Vibration is not nearly sufficient to have any effect on = the spool. 
 <= /SPAN>
Wolfgang wrote:<<If it takes that mu= ch force to move the spindle against the O-rings then those springs must be= pretty darn strong. I find that dificult to accept.>>
The spr= ings are very strong, 26 lb/in.
 
Wolfgang wrote:<<Vibration levels can exceed 70 G's>= ;>
See MIL= -STD-810 for expected vibration levels in aircraft environments.
 &= nbsp;
Wolfgang wrote:<<Yes, that would be = easy . . . except . . . you can only override one pressure switch at a time= or overload the system>>
I would= still like to know how push buttons can overload anything.  And = why would anyone want to override more than one at a time?
 <= /SPAN>
Wolfgang wrote:<<The items you cited= are more a one-of condition ...>
I have never had a thermal lock up, yet I use pressure gauges and the= momentary push buttons on a regular basis.  They were originally inst= alled to deal with sticking VEP switches, but it is like getting a new tool= .  After you have it, you can't imagine how you lived without out it.&= nbsp; I have already discussed the benefits of momentary switches not relat= ed to hydraulic lock-up.
 
Wolfgang wrote:&= lt;<In the event of a problem you have to make sure you push the right s= witch.>>
One sho= uld label the push buttons appropriately.
 <= /SPAN>
Wolfgang wrote:<<Are you saying that= Oildyne is putting springs in the spool to center it when the pump is not = running ?
Springs that are not documented in the Oil= dyne spec sheet ?>>
Recall = that the Legacy pump configuration =E2=80=9CCZZ=E2=80=9D is proprietary to = Lancair.  Companies generally= don=E2=80=99t post proprietary materials on-line.
 <= /SPAN>
<<You seem to want to be "involved"= in the anomalies of flight.>>
Not really.  I avoid th= em by thorough examination, no matter what it requires.
 
Chris Zavatson
N91CZ
360std
 
 
----------MB_8CEC68F1A9491DF_954_4CF7_webmail-d158.sysops.aol.com--