Chapter
19: Wings
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I didn't take too many pics of the core cutting
process, but there really is nothing new here. The only tip to pass on
is well known but here it is anyway. Make little bridges across the
spar cap trough with mixing sticks, cut across them and then cut the
troughs separately . Makes a nicer cut, just like on the
canard.
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The first pics is the inboard core with John Epplin's templates
installed and ready to cut, second pic is one of the cores being
assembled with micro. I stood it on the trailing edge, lined everything
up as near perfect as possible, placed finish nails to hold it secure
and weighted it down for cure. One trick to pass along here, when
placing the micro, don't let it get near the edges, you don't want that
stuff to get to the wing surface or else you will be grinding it away
later with a dremel. You will need to LIGHTLY sand the wing
surface to remove any minor mis-match or defects, the micro will play
havoc with this process. If you can keep it off the wing surface you
will be way ahead of the game.
Also read the note, chapter 19 page 3 second
paragraph. Nat has you cut a wedge of wing core off using a band
saw
AFTER he tells you to micro it back together. If you cut it
first you can use the hot wire saw. I fooled him though and used the
hot wire saw anyway! Yes it will cut micro! One the second wing I had
my education and knew what to do.

Here's a shot of the shear web lay-ups.
Next
the leading edge cores are bonded into position with micro, this is a
big step with lots of checking, rechecking and finally a "leap of
faith" .
The spar cap troughs must be lined up perfectly to insure the spar cap
is the proper thickness all along the wing, the level lines must be
absolutely plumb and the cores must also match up to each other nicely
and
finally the trailing edge must be straight and lined up with each core.
There are plenty of places to screw things up in this step. Note
also the little blocks glued to the jigs. The jigs are generally a
lousy fit as anyone who has done this knows. I took this tip from Jay Hegeman's web site and
recommend it. What it does is guarantee that both wings will fit
the jigs the same way. Good Idea! Also preserve all those level lines
as long as possible! Transfer them onto the leading edge and shear web
whenever you can. After assembling the cores some of them will be
invisible to you, if you transfer them onto the LE and shear web you
can still use them to check alignment.
Next
the wing core is jigged to the bench. I spent some quality time
with string lines and shims to get the
core as straight as possible,
It ended up straight within 1/16" over the length of the core.
Better than any Cessna I bet, well maybe not a Citation X.
Spar
cap layups, nothing new here from the main spar or canard, just make
sure you have enough to finish when you start the last one.
My wife Paula & I hard at work on one of the wing layups. These
typically took about 8 - 10 hours to complete.
I'm very fortunate to have her support on this project, although I'm
not sure she believes it will ever fly!
These shots show part of the aileron installation. I ran
into trouble here, in center pic you can see the glass to glass bond is
not at the minimum .5" called for in the plans. I had to make a repair
on this one. Also seen is the straight edge I used to keep the hinges
in line with each other. This worked very well and my ailerons move
easy with no binding at all. Also seen here are the Click Bond studs I
used to mount the hinges to the wings. I received a few emails from
people very concerned that I should just follow the plans and use
screws. I'm not the first guy to do this, also I
don't think they know how the click bond stud is
used and are under the impression that the aileron hinges are glued or
bonded to the wing! This is not true, in fact the click bonds are
installed just as if they were a screw. That is they go thru the skin
with the head above the wing skin, the head bonds to the top wing skin
and all the adhesive (flox) does is keep them from turning. The head of
the CB's is only .020" thick. This allows them to be filled over with
micro or in my case I recessed the foam locally before glassing
the wing, mine are completely flush. Wayne Hicks suggest using a
small rivet to insure the stud does not turn. I did this but now think
it unnecessary, if anything just grind a few notches along the
perimeter and this is probably over kill, the Flox really grips these
tight. Also you should put a layer of BID over them to keep them
secure and prevent any paint issues later.
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Here you can see the spherical bearing I used for the
Aileron torque tube . The plans phenolic block is subject to early
wear, the supplied Triangle bearing is made from Delrin or Nylon and
works fine except at this location it is subject to flame
impingement in the event of an engine fire. Also, it is a self aligning
bearing not spherical, and not designed to swivel in use. Most
people use it anyway
and it works. The spherical bearings Infinity sells cost $50.00 each
and I'm sure they are very nice.
These were $3.00 ea. Stamped plated steel housing with a
machined steel insert and oil impregnated bronze
"ball". I did need to machine little bushings to fit over my -3
click bond studs as the holes are 5/16".

Here
you can see the aileron torque tube, bell-cranks and push rods.
If
you study it closely and compare it to the plans you will note all of
my
hardware
is installed in accordance with standard practice, ie all of the
bolts are pointing
down and thru the rod ends, the rod ends are on top of the bell
cranks. I don't know why the plans don't show it this
way, and there may be something I'm missing, but it works. I have all
the required travel, clearance etc. All I needed to do to allow
this is flip the CS-128 bellcrank over. If you see a problem with
this, I'm all ears! In the photo it looks like I don't have 90 degrees
between the push rod and bellcrank, but it is perpendicular.
Next and last step is match drilling the wings to
the main spar. I managed to get the whole enchilada in the garage from
corner to corner. I started out
using my auto-level-laser. About half way thru I decided to do a
reality check with a water level to make sure before I drilled
any holes, good thing I did! The laser was off by about .5" over
100'. I didn't want to wait to have it fixed so I just went with the
water level like most others have done. The water levels are not
fool proof either! Make sure all the air is out of the tubing or
it can
be off., also let things settle for a bout a minute as sometimes it
takes a moment for the columns to equalize
I also tried to use the hole saw method and after
about one hole decided to buy a reamer instead. To me this seems like
the only way to go for this step. Just drill it up to 39/64", then run
the .625" reamer thru it, couldn't be easier! The bushing will
fit perfect this way. My holes all came out center except both
outboard lower hard-points were off center by about 1/8" high.
This is no problem, the hole is well inside the hard point, but
it
makes
me wonder how I made the same measuring error on both wings! It
also forced me to enlarge one of the pockets as I could not get a
socket over the bolt.
One more
thing, You will note that I have installed 2 level boards on the wings.
The plans call for 1 on each wing but I was concerned that one might
get knocked off so I went with a backup. Both were
perfectly
level when installed, however weeks later when I needed them
the boards out of agreement on the RH wing by .1 degrees.
Now I had to decide which one was wrong! Luckily I still had the
level line on the outboard core to use. The outboard level board
agreed
with the level line. Afterwards I investigated a little further and
found the inboard board was no longer flat. I had been when installed
so it warped somehow. So my tip of the day for this step is to
cut your level boards so that only the ends will touch your level, in
other words cut a relief along the top center 80% or so of the board so
the
level only touches near the ends. This makes for a more
repeatable surface to measure against.
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