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Touring Motor Gliders Association (TMGA)
  • I don't know where you are placing the ruler, but an angle measurement on
    the verticality of the lg struts reads 88.5 degrees on my Ximango, with the
    struts bowlegged in.

    ==========================================================

    Date:         Wed, 18 Jun 2008 14:01:30 -0500
    Reply-To:     "Ximango Owners Group (XOG)" <XIMANGO@HOME.EASE.LSOFT.COM>
    Sender:       "Ximango Owners Group (XOG)" <XIMANGO@HOME.EASE.LSOFT.COM>
    From:         Ted Gordon <tedjgordon@ATT.NET>
    Subject:      Re: gear collapse, over center gap
    MIME-Version: 1.0
    Content-Type: text/plain; format=flowed; charset="iso-8859-1";
                  reply-type=original
    Content-Transfer-Encoding: 7bit

    Dear John and group:

    I don't know where you are placing the ruler, but an angle measurement on
    the verticality of the lg struts reads 88.5 degrees on my Ximango, with the
    struts bowlegged in.

    Best
    Ted Gordon

    --------------------------------------------------
    From: "John Lawton" <Thrmlseekr@AOL.COM>
    Sent: Wednesday, June 18, 2008 8:04 AM
    To: <XIMANGO@HOME.EASE.LSOFT.COM>
    Subject: Re: gear collapse, over center gap

    > In a message dated 6/18/2008 8:05:57 AM Eastern Daylight Time,
    > bruce@SCHIMMEL.COM writes:
    >
    > I  understand that if you hold a ruler across it, you get an "over
    > center" measurement of 5/16".
    >
    > Hey Bruce,
    >
    > Yes, that's what I'm referring to.  I compared mine back in December  to
    > make
    > sure they were similar. As I recall it was about 5/16" gap between the
    > straight edge and the locking arm when holding the straight edge across
    > the top  of
    > the locking arm. I'll measure mine today with my caliper before I fly,
    > get a
    > more precise measurement and report back later.
    >
    > I believe the tilt in the main gear legs is a direct result of  the
    > adjustment of the locking arm. Another way to measure the proper locking
    > arm
    > adjustment might be to put an angle finder on the strut and measure the
    > departure of
    > the strut from vertical (plumb). Angle finders can be sourced  at most any
    > home
    > improvement store. Usually, they have a magnetic strip on one  side that
    > holds them in place while the measurement is taken. A digital level  could
    > also be
    > used for this measurement, although I would prefer a mechanical  device
    > for
    > checking this angle because, in my experience, even the  pricey digital
    > levels
    > are nowhere near as accurate as a mechanical level. I  found that out the
    > hard
    > way when I was building my Europa setting the angle of  incidence on the
    > wings.
    >
    > Regards,
    >
    > John  Lawton
    > Whitwell, TN (TN89)
    > Ximango #135
    >
    >
    >
    > **************Gas prices getting you down? Search AOL Autos for
    > fuel-efficient used cars.
    > (http://autos.aol.com/used?ncid=aolaut00050000000007)
    =========================================================================
    Date:         Wed, 18 Jun 2008 20:20:45 EDT
    Reply-To:     "Ximango Owners Group (XOG)" <XIMANGO@HOME.EASE.LSOFT.COM>
    Sender:       "Ximango Owners Group (XOG)" <XIMANGO@HOME.EASE.LSOFT.COM>
    From:         John Lawton <Thrmlseekr@AOL.COM>
    Subject:      Re: gear collapse, over center gap
    MIME-Version: 1.0
    Content-Type: text/plain; charset="US-ASCII"
    Content-Transfer-Encoding: 7bit

    Hello again guys,
     
    Adding to what Bruce mentioned, my maintenance manual, dated April 02,  2002,
    page 1.31, step 2, says to turn the stop screw 2.5 turns clockwise and  lock
    it with the locking nut. It doesn't say 2.5 turns from start or 2.5 turns 
    from the screw bottomed out. Since it says "clockwise" and following the "righty 
    tighty" rule, I would assume that "2.5 turns clockwise" means from when it 
    is initially started into the threaded bushing which is welded to the upper 
    articulated strut, as is shown in the exploded diagram on this page of the 
    maintenance manual.

    For what it's worth, mine is nothing at all like this. Mine looks as it  the
    screw was threaded into the bushing all the way, then backed off 
    counterclockwise to a distance of between 4 and 5 threads. I don't  know how many turns
    that is, but I would reckon at least three and possibly as  many as four turns.
     
    I did a more precise measurement on the lower articulated strut (the flat 
    part of the over center locking mechanism) by placing a steel ruler on  the top
    edge of this part with the other end of the ruler situated on  top of the
    threaded bushing that holds the adjusting screw on the upper  articulated strut.
    While holding the ruler in place, using an  inside caliper I measured from the
    bottom of the ruler to the top of  the center pivot point on top of the lower
    articulated strut, where  the upper and lower articulated struts meet. The
    right side was .38" and the  left side was .33". I didn't measure the angle of
    the landing gear leg to  plumb because the clouds just looked too good to be
    fiddling with this  today. By the way, cloudbase was 7500'msl with 6-7 knot lift
    and some ridge  lift later in the glass off. Not bad for mid June here.
     
    I also looked at a Navion in my hangar that belongs to our resident  A&P/IA
    to compare how it is done relative to the Ximango. The landing  gear on the
    Navion is almost identical to what the Ximango has, both in terms of  the way it
    operates and the relative size of the parts. The only difference is  the
    "lower articulated strut" on the Navion is tubular, instead of being made  from
    flat bar stock. Both look equally "beefy".
     
    It would be nice if we could get a more thorough definition of what is 
    acceptable in terms of this adjustment of the upper and lower articulated  strut
    alignment. Clearly, mine is not set up as the maintenance manual dictates.  It
    appears to me that if it were I doubt there would any  over-centering of these
    articulated strut parts and, as such, it wouldn't  lock the gear down.
    Assuming I understand the theory of operation here, it seems  to me that this is an
    important adjustment. If it is improperly adjusted it  could lead to a gear
    collapse, especially in a rough runway situation.  I  think it's important that
    these parts over center on their connecting pivot bolt  to properly to lock the
    gear leg down.

    Comments?
     
    Regards,
     
    John  Lawton
    Whitwell, TN (TN89)
    Ximango #135



    **************Gas prices getting you down? Search AOL Autos for
    fuel-efficient used cars.      (http://autos.aol.com/used?ncid=aolaut00050000000007)
    =========================================================================
    Date:         Wed, 18 Jun 2008 21:13:17 -0400
    Reply-To:     "Ximango Owners Group (XOG)" <XIMANGO@HOME.EASE.LSOFT.COM>
    Sender:       "Ximango Owners Group (XOG)" <XIMANGO@HOME.EASE.LSOFT.COM>
    From:         Bruce SCHIMMEL <bruce@SCHIMMEL.COM>
    Subject:      Re: gear collapse, best metric
    In-Reply-To:  <d2f.25111229.358b005d@aol.com>
    Mime-Version: 1.0 (Apple Message framework v753.1)
    Content-Type: text/plain; charset=US-ASCII; delsp=yes; format=flowed
    Content-Transfer-Encoding: 7bit

    John --

    Thanks for your careful investigation. I wonder if Ted's metric might 
    also be useful. You've said .33" and .38" on the gap. Ted writes: an 
    angle measurement on the verticality of the lg struts reads 88.5 
    degrees.

    Are these two expressions of the same condition?

    yrs, B

    On Jun 18, 2008, at 8:20 PM, John Lawton wrote:

    Hello again guys,

    Adding to what Bruce mentioned, my maintenance manual, dated April 
    02,  2002,
    page 1.31, step 2, says to turn the stop screw 2.5 turns clockwise 
    and  lock
    it with the locking nut. It doesn't say 2.5 turns from start or 2.5 
    turns
    from the screw bottomed out. Since it says "clockwise" and following 
    the "righty
    tighty" rule, I would assume that "2.5 turns clockwise" means from 
    when it
    is initially started into the threaded bushing which is welded to the 
    upper
    articulated strut, as is shown in the exploded diagram on this page 
    of the
    maintenance manual.

    For what it's worth, mine is nothing at all like this. Mine looks as 
    it  the
    screw was threaded into the bushing all the way, then backed off
    counterclockwise to a distance of between 4 and 5 threads. I don't  
    know how many turns
    that is, but I would reckon at least three and possibly as  many as 
    four turns.

    I did a more precise measurement on the lower articulated strut (the 
    flat
    part of the over center locking mechanism) by placing a steel ruler 
    on  the top
    edge of this part with the other end of the ruler situated on  top of 
    the
    threaded bushing that holds the adjusting screw on the upper  
    articulated strut.
    While holding the ruler in place, using an  inside caliper I measured 
    from the
    bottom of the ruler to the top of  the center pivot point on top of 
    the lower
    articulated strut, where  the upper and lower articulated struts 
    meet. The
    right side was .38" and the  left side was .33". I didn't measure the 
    angle of
    the landing gear leg to  plumb because the clouds just looked too 
    good to be
    fiddling with this  today. By the way, cloudbase was 7500'msl with 
    6-7 knot lift
    and some ridge  lift later in the glass off. Not bad for mid June here.

    I also looked at a Navion in my hangar that belongs to our resident  
    A&P/IA
    to compare how it is done relative to the Ximango. The landing  gear 
    on the
    Navion is almost identical to what the Ximango has, both in terms of  
    the way it
    operates and the relative size of the parts. The only difference is  the
    "lower articulated strut" on the Navion is tubular, instead of being 
    made  from
    flat bar stock. Both look equally "beefy".

    It would be nice if we could get a more thorough definition of what is
    acceptable in terms of this adjustment of the upper and lower 
    articulated  strut
    alignment. Clearly, mine is not set up as the maintenance manual 
    dictates.  It
    appears to me that if it were I doubt there would any  over-centering 
    of these
    articulated strut parts and, as such, it wouldn't  lock the gear down.
    Assuming I understand the theory of operation here, it seems  to me 
    that this is an
    important adjustment. If it is improperly adjusted it  could lead to 
    a gear
    collapse, especially in a rough runway situation.  I  think it's 
    important that
    these parts over center on their connecting pivot bolt  to properly 
    to lock the
    gear leg down.

    Comments?

    Regards,

    John  Lawton
    Whitwell, TN (TN89)
    Ximango #135


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