Mailing List lml@lancaironline.net Message #39041
From: colyncase on earthlink <colyncase@earthlink.net>
Sender: <marv@lancaironline.net>
Subject: Re: [LML] Re: electric attitude indicators
Date: Mon, 18 Dec 2006 11:55:06 -0500
To: <lml>
I guess it is just my naiveté but I am just not familiar enough with what it takes to get a TSO rating on an instrument except that once it gets it, the price goes way up
 
Joe,
    I think the issue is that there is a statistical interaction
among a number of variables totally out of your control.  
Testing tries to capture a larger portion of the statistical
population so that you aren't dead because a few of
those independent variables aligned one day in a way
that will result in malfunction.
 
    Is there a vibration in your particular plane
that the mechanical isolation the ahrs doesn't
damp out sufficiently?
 
    Is there electical noise in your airplane
that is somehow different enough to affect
your unit?
 
    How does the unit respond to static
discharge?
 
    How does the unit behave if there is a large
current near by?
 
    Is there an attitude excursion that is beyond
 the capacity of the unit to track?
 
    Will you do something in your airplane that
will cause the micro-code in the unit to execute
a code path that no one else has?
 
    Is there a marginal wire connection in the
chip that is going to turn into a fuse over time?
   
    The problem with these kind of statistics is that
even though the failure mode may only occur 1%
of the time, when it does occur and you are out
of backups,  you are having a 100% bad day.
It's not like you have a 99% good day every day.
 
    I would just note that the cross-bow 425 was
built by an experienced company and it failed;
not 100% of the time but enough that people
eventually walked away.
 
    The garmin gmx200 - another piece of digital
avionics -  is on hold right now because it "sometimes"
powers itself down.   I bet that unit got more
testing than most of these low unit volume ai's.
 
    The stec 55x auto-pilot has so much misbehavior in
the field that Tom West got 300 replies when he
made a post about pitch oscillation problems in a c210.
 
    IMO the state of avionics in the field is that
certified avionics "almost work", in a statistical
sense, leaving anything less well tested somewhere
south of that.
 
    Is an old vacuum gyro more reliable? maybe not by
design but by shear numbers it's been exposed
to a much richer set of statistical variables without
doing something weird.
 
 
 
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