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.
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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
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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
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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>
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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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