Wings


Ailerons 7 (2.0 hrs)

This evening I set about final preparation of the right aileron.  Primarily deburring and dimpling the remaining structure.

I had an extra 3/32 dimple die set.  The male die was a little off, having at some point it its life being used for something it should have been. So its been sitting unused. The tight space at the trailing edge of the outer ribs presented a problem, and this little spare die was the solution. I ground down the male portion of the die so that it would not protrude from the back of the female close quarters die. This way I could use the no-hole yoke, close quarters dimple die, and modified male die, to get into very tight places. I have to be careful to make sure everything is aligned properly, but if you go slow, the male die will ensure the female die is properly aligned. IMG_0162.JPG

Here is a picture of the process.IMG_0163.JPG

The end result came out perfect.  The far dimple looks like its off, but that is artifact of the picture.  I’m very happy with the result, as it was difficult to even get the close quarters dimple die set in this location. IMG_0164.JPG

Not much to say for a post concerning deburring and dimpling. IMG_0165.JPG


Ailerons 6 (2.5 hrs)

Today I finished final drilling and dimpling the leading edge skin for the right aileron.  The counterweight attaches to the leading edge skin at the point where the curve in the skin is greatest.  As a result, you cannot use a standard dimple die to dimple the skin for the CS4-4 pop rivets.  The method recommend (not in the instructions) is to use to counter sink the counterweight pipe and then use that as your dimple die.

Here I have the counterweight pipe, after countersinking, attached to a 2×4.  IMG_0005.JPG

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With the counterweight securely in place, I clecoed the leading edge skin.IMG_0008.JPG

I used the steel rod from my c-frame and a male dimple die to achieve the dimple below. IMG_0010.JPG

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I was at the airport for a long time today, but I didn’t get much work done. We also had an EAA Chapter meeting and that made for a lot of visitors and hangar talk. Zack Chattler was nice enough to give me two very heavy duty rubber mats for the floor. The heavy weight is perfect for holding down the wood and providing a stable surface.

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Also, our EAA Technical Counselor, John Raffensparger, took a look at my project.  He was very pleased with the quality of the build and so far, no squawks!IMG_0012.JPG


Ailerons 5 (4.0 hrs)

Today’s first action was to back rivet the aileron stiffeners to the right skin.  I use simple scotch packing tape as my “rivet” tape.IMG_5748.JPG

I tape all the rivets for one side in place first. IMG_5749.JPG

I use a large bag of lead shot to hold the skin firmly down on the back riveting plate.  This is especially useful for the rivets that are very close to the trailing edge.  As you pull the top side of the aileron skin up to access the shop head with the rivet gun the side you are trying to rivet will also want to lift off the back riveting plate… which is a recipe for a nasty mistake. IMG_5750.JPG

Here you can see two photos of the end result. IMG_5751.JPG

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Next it was time to bend the trailing edge.  I use a large bending brake made from wood with some simple door hinges courtesy of Mr. Bullock. Squire is always ready to help. With the ailerons, I had to use another 2×4 and the bag of lead shot to stop the skin sliding out of the brake. IMG_5753.JPG

I am very happy with the results.  A quick check with a rule showed that the radius is within limits and there is no bend or bulge.  The skin is perfectly straight from the spar to the trailing edge.  I also checked the trailing edge for any bow or distortion and there is none. IMG_5754.JPG

I needed to lay everything out in order to be sure I was picturing it correctly in my head. IMG_5755.JPG

The aileron hinge brackets need to be drilled for #12 bolts.  I used a step bit. IMG_5756.JPG

Its always important to keep the hangar well stocked with brews.  They help you cope when you mess up!IMG_5759.JPG

I always tape the step bits when I use them to ensure I don’t go one step too far and enlarge the hole. IMG_5757.JPG

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I clecoed all the components together and set about match drilling.IMG_5761.JPG

The rivets on the bottom of the spar are drilled out to #30 in order to accommodate the CS4-4 rivet shown here. The aileron counterweight, otherwise known as a galvanized pipe, is also drilled out to #30. IMG_5762.JPG

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Use a long #30 drill bit to access the last attachment point for the counterweight. IMG_5764.JPG

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I haven’t gotten to use this yet, but my uncle gave me this, and I highly recommend it. This bad boy is perfect for the quick priming job or touch up.  Mix your primer in the glass jar and boom you’re ready to spray.  The propellant lasts enough for about a jar and a half.  No cleanup, setup or air compressor required!  I wish I had discovered this awhile ago. IMG_5767.JPGFinally, the components will need to be dimpled.  A word of caution here.  Van’s doesn’t mention anything in the instructions about dimpling the leading edge to counterweight.  Be careful.  Normal dimpling methods will distort the skin due to curvature of the skin at this point.  The method most builders use, and I will detail further when I do it is to use the countersunk counterweight pipe as the female die.