Left Flap Drilling

Time: 1 Hour

I got home tonight from my 2 day trip and did a few house items before going out to look at the flaps. I decided to get an hour of work in and match drill the skins on the left flap. This didn’t take too long so I decided to lay out the flap hinge and drill it to the flap. The process is to drill one side to the flap and leave the other undrilled until you install it on the wing. You make the trailing edge of the aileron and flap match. This adjustment of the position of the flap in relationship to the aileron happens on the flap hinge either moving the hinge aft or forward. From what I have read it is always aft, meaning the centerline of the hinge moves aft or away from the rear spar of the wing. What can happen is you have to move it so much you can make the holes in the wing side of the hinge get too close to the edge and impede on your edge distance for rivets. To help me with this potential problem I moved the flap side of the hinge out 1/32″ vs flush with the edge if the skin.

20140508-213453.jpgI then worked on drilling the hinge. These new deep reach clamps work awesome for this. I just drilled and then clecko’d as I went down the line. That’s all I did tonight as storms were approaching and I wanted to get my truck in the garage.

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Flaps Start

Time: 1 Hour

I actually had plans to get a lot done in the Hangar today but we had a pop up trip to Arkansas so that didn’t happen. I did want to get a little work done when I got home so I grabbed all the parts for the flaps and started assembling so that match drilling could begin. There are a couple other tasks ahead of this step but I wasn’t going to make a lot of noise so my neighbors don’t begin to hate me. Van says that these are the easiest control surfaces to build and I believe them as it ink took me 30 minutes to put these completely together.

20140506-213908.jpgI then grabbed a section of the piano hinge for the right flap and and clamped it in place with my new deep reach clecko clamps.

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20140506-220741.jpgThat’s where I stopped for tonight and will get back at it Friday and this weekend.

Right Aileron Complete

Time: 5 Hours

I had an early flight this morning and was a little tired when I finally got home but wanted to get the right aileron finished today. The process was the same as the left aileron so I won’t go into every detail as I did for that one. I will add that forgot to mention on the other aileron that I used my edge roller on the top and bottom of the leading edge skin to help these sit flat on the main skins after riveting. I also got out my pneumatic rivet puller and did the repairs on it that I knew it needed from a couple of years ago. This was a tool from Harbor Freight and haven’t used it in a long time. My reasoning for using it today was that I could barely squeeze my manual puller after all those blind rivets I did in the left aileron. I hurt muscles that I apparently never use! It took an hour to fix the tool but well worth it as it made quick work of the CS4-4 rivets. Here are a few pics from today’s work. Now on to the flaps!

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Left Aileron Complete

Time: 6 Hours

Today’s task was to get the left aileron buttoned up and riveted while watching game #2 of the Blackhawks vs Wild. I had prime red all the parts last night before heading out to dinner so they would be ready for today.

20140504-141938.jpgFirst thing to do is rivet the spar reinforcement plates on both ends of the spar. There are only a couple holes you can do, the 3 inner one on both ends, as the rest will be done in sequence with the forward and main ribs. You also can rivet the nutplate on the inboard end. This is needed as the 3 bolt for the inboard aileron bracket will be inboard of the main rib and you have no access to put a nut on it.

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20140504-142255.jpgThe leading edge ribs are then blind riveted to the counterbalance.

20140504-144851.jpgI then put the counterweight/ribs into the leading edge skin. I then slid the aileron spar into the main skin and the attached it to the leading edge assembly. I only clecko’d the top side of the skins to the spar as I need the bottom skins open to rivet the top skins. I set this aileron on the shelf for a while so I could work on the right aileron. I did this because I need the 2×4’s I used for the counterweight drilling to make the next jig for the riveting process. The right side is done with the same process as the left. All parts were assembled to match drill including the counterweight. The countersinking was done by sight again.

20140504-162214.jpgThe riveting process for the aft skins is to lift up the bottom skin enough to get a bucking bar inside the skin to access the spar. To aid this I have seen other builders some 2×4’s to make brackets for you to screw down the aileron and hold it securely so you can rivet.

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20140504-194842.jpgI bought a new bucking bar that was 1″x1″x6″ with a angled end and a squared end. The angled end was too steep so I ground the squared end to a good angle. I then wrapped it in tape to protect all the parts from getting scratched. Here you can see how it fits and how you rivet the top skin.

20140504-195125.jpgIt took me about 30 minutes to rivet the total line of rivets and they turned out real nice.

20140504-195235.jpgYou then rivet the top of the leading edge ribs and slide in the 2 main ribs and rivet their top holes along with all the rib to spar holes. You can then bolt on the aileron brackets and torque them.

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20140504-195529.jpgSo you then flip the aileron onto the top so the bottom is available to work on. The first task is to rivet the counterweight with the blind CS4-4 blind rivets.

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20140504-213526.jpgThe plans say that you need to weight down the bottom skin to keep it flat as you rivet the skin. I decided to use a couple of flat shelve boards and clamps to keep the skins flat. Then you can rivet the bottom skin to leading edge and main ribs.

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20140504-214043.jpgI then riveted every other hole of the leading edge skin, main skin and spar holes with the same CS4-4 blind rivets and then the remaining holes.

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20140504-214409.jpgThat’s the left aileron all done! Now I need to finish up the right one tomorrow. Most of the prep is done on it except the edges of the leading edge skin and priming. I couldn’t resist and had to put the aileron in the wing to see I what it looks like! Fun weekend in the Hangar.

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Left Aileron Work

Time: 7 Hours

I started to work on the assembly of left aileron so I could match drill all the parts. First up was to match drill the inboard and outboard brackets to the spar/spar reinforcement plates.

20140502-124443.jpgI also grabbed the leading edge rib and the main rib and match drilled those with the skin off.

20140502-124624.jpgThen the spar/rib assembly was slid into the skin and the leading edge skin clecko’d in place along with the galvanized pipe used as a counterweight.

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20140502-124802.jpgWith the skins I place I match drilled the holes in the leading edge to the ribs and there counterweight.

20140502-125028.jpgI will be tossing that drill bit away since it was getting full from going thru the pipe. I had to enlarge the holes into the pipe to a #30 for the larger flush blind rivets that go here as well as the row on the skin to spar line of the bottom side if the aileron.

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20140502-125314.jpgThere is one rivet that gets place through the leading edge rib to the counterweight. To drill this you have to remove the leading edge and drill through the aft hole of the rib with a long bit.

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20140502-125540.jpgAfter all the holes are drilled I disassembled the aileron and worked on the counterweight. You need to countersink the holes so it will accept the dimple of the skin. I’m not sure how dull this made my bit but I think I will order a new one when I’m all finished. I just used the bit without the cage since this is a round surface.

20140502-125815.jpgAfter I took care of the counterweight i figured I would tackle the dimpling of the skin that rivets to the counterweight. The issue is that the holes are right on the radius of the skin. This caused a problem with the female side if the dimple dies as the die is flat ad would cause some serious deformation of the skins curve. I read a couple other builders blogs where they made a rod to attach the male end if the dies to. Then they would strike that rod/die against the skin while using the countersink in the counterweight as the female side. Instead of fabricating a rod I just drilled a 3/16″ hole in the unused side of one if my bucking bar.

20140502-184520.jpgNow the question is how to hold the skin and counterweight so that you can dimple it? I read a post by Brad Oliverand how he accomplished this task. I just copied his technique and it worked out great. I used two 2×4″ and made a jig where I taped two 1/4″ dowels on the top to give the counterweight a place to rest.

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20140502-213237.jpgI hit the the bucking bar with a rubber mallet and the dimple turned out really nice.

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20140502-213542.jpgI then turned my attention to deburring all edges, corners and holes. I also used the countersink to hit the holes that will be under the rib flanges and attach the single nutplate that holds the aileron bracket on. All the holes got dimpled as well.

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20140502-214117.jpgIt was a great day in the Hangar!