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The Alon parts manual calls for a standard AN bolt for the wing attach 
fittings, and I think all the other models of the plane use the same bolt.

By definition, a standard AN bolt is not a close tolerance bolt - so the
fit 
of the bolt in the wing attach fittings is not critical (within certain 
limits, of course).  The wings are held tightly in place by the torque on
the 
bolt.  The torque on the bolt develops friction between the "plates" of
the 
wing attach fittings.  The friction between the plates is what keeps the 
wings from moving.

If the holes in the wing attach fittings are worn, or if the bolts are
worn, 
then at some point in the life of the plane, those bolts were not torqued 
properly.  If they were torqued properly, the joint would have no relative

motion in it (because of the friction between the plates), and the parts 
would not have been able to move causing the wear.

If you hear a clunk when you lift your wing, and IF that clunk is coming
from 
the wing attach fittings, then in all probability it is because the bolt
is 
not properly torqued.   

The design and theory behind bolted joints is thoroughly discussed in 
mechanical engineering text books if anyone wants to look it up.

And of course.... all of this is just my opinion, so take it for what it's

worth.  I would consult with an aeronautical engineer before I did
anything 
to change the design of the wing attach joint.  In my opinion, if worn
parts 
are found, then they need to be replaced with factory original parts, not 
rigged with sleeves or wrapped with shims.  

Good Flying,

Wayne DelRossi
Alon N5618F
GYH  Greenville SC

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