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SZD 36 COBRA C-15
WARNING ON WING CONNECTION

An unofficial Advisory
To Whom it may concern, I am the brother of the pilot who was killed in
Sylacauga, Alabama on March 31, 2007 flying a SZD
36a cobra 15 #813. I also flew the airplane in question as much as he did. The
number one thing I want to tell you is, do not assume anything. We
assumed that because we could see the top bushing or pin seat all the up, than
the bottom one was doing the same thing. In our case this was not so. If you
don't do anything else to your glider make sure you provide a hole to visually
confirm that the bushing or pin (whatever you want to call it) that rides the
jack screw and pins your wing anchor points are fully in place. I am not going
to tell you where to drill holes in any airplane but it may be possible to put
a 1" or so hole in the partition of the
turtle deck, so that you can see directly
what is going on at the lower anchor point. Please consult a skilled A&P to
help evaluate the situation. Just make sure you can see that both of your main
wing anchor points are properly secure and than you should be safe.
I have include some photos below of the damaged wing connection to help you
see what happen. You will notice in photo, located top row 2nd from left, that the upper tab that is
suppose to keep the center flange centered
is worn away. That wear allowed the whole assembly
to ride up a 1/4" or so and that in my opinion
in only part of the problem. The lower pin failed to
penetrate about 3/4". What we really
missed is that if on screwing the pins out to a fully seated connected
position, if those anchor points where not perfectly aligned, than the lower
pin would bite like a pair of vice grips on top of the opposite wing's
anchor point but, not pin the connection.
The upper pin would than continue to travel up showing us a connected & fully
seated top pin. On the damaged assembly you
could hold with your fingers or block with a stick the lower pin entry and the
upper pin would continue up and the lower pin would wedge only on the
obstruction. It is unfortunate that the manufacturer did not provide a way to
visual confirm connection or that we did
not think to provide it for ourselves. In hindsight it seems so simple now
but, we did not have the benefit of someone
else's experience in this regard. I am
assuming, there is that word again, that this is the first time it has happen
to anyone. I find that a little hard to believe but, it is what it is.
What you cannot see in the photos is that the lower pin or bushing had about
1/8" to 1/4" (cannot really tell exactly how much) of it's bottom end sheared off, which must have been partly
penetrating the hole of the left wing
anchor point and was sheared as the wings lifted up and away. This seems to me
to be a bit of a contradiction, in that, if the pin was partly penetrating the
left wing anchor point hole instead biting down on top of it, than it should
have continued thru and pinned the connection. The tapered shoulder of the pin
may have just wedged itself and stopped. I really don't know exactly what
the mechanics are as I had limited time to inspect the damaged connection but, you had better be confirming that, in fact,
visually the connection is correct.
The official
investigation should release some advisory directives thru the
SSA & EAA
in a few weeks but, please contact me with any questions that you may have.
I am open to any comments or thoughts that anyone may have, as well. Please
anyone reading this information, have any other owner that you may know, or come across, of this
type of sailplane or a similar connection design,
get a hold of me immediately or at lease direct them to this site. If I cannot bring my brother back,
which I cannot, than I want to
at least keep someone else from being the victim
of the same problem. Post Scripts:
4-28-07 - I have been made aware that at least one other SZD 36A Cobra has
been found, in Great Britain, with a wore away tab or lug that serves to keep
the jack screw collar centered. Also, that
Foka (SZD24C)
sailplanes have a very similar wing connection and that this notice
should be extended to pilots and owners of the Foka SZD24C.
Sincerely,
Steve Wallace swallace500@aol.com
cell 205-365-0646
PLEASE NOTE WHEN VIEWING THESE PHOTOS THE PIN OR BUSHING
HAD BEEN RUN UP & DOWN THE SCREW BY SEVERAL PEOPLE SINCE THE ACCIDENT, SO THEY
COULD GET AN IDEA OF HOW IT WORKED, AND IT IS NOT IN THE POSITION IT WAS FOUND
IN AFTER THE ACCIDENT.
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LEFT WING, UPPER ANCHOR POINT SNAPPED OFF
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RIGHT WING, NOTE THE SNAPPED OFF ANCHOR POINT FROM THE OPPOSITE WING IS BENT UP AND REMAINS WITH THE JACK SCREW ASSEMBLY.
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TOP VIEW OF LEFT WING
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TOP VIEW OF RIGHT WING
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SIDE VIEW OF RIGHT WING FROM TRAILING EDGE
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RIGHT WING, THE PIN POSITION IS NOT IN THE AS FOUND POSITION.
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ANOTHER VIEW OF LEFT WING
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