The weather today turned out better than I expected, though far from perfect. There were sporadic showers through the afternoon, but in between it was ice and sunny out. So I managed to get in the spray gun practice that I’d wanted to do, which took up a lot of the day.

First I just filled the hopper with water and practiced spraying it against the side of the house. This was just to get familiar with the flow and pattern controls, and that didn’t take too long. Next I got some latex paint I had sitting around and thinned it to the recommended viscosity from Stewart (25 seconds in a viscosity cup). Pretty thin stuff. Then I went to town spraying the latex paint on some cardboard and the random sheet of plywood I use as a backer when I prime. This let me see how I could control the atomization of the paint with air pressure, but was kind of unsatisfying in terms of seeing how the paint was going on. So I scuffed a couple of pieces of scrap aluminum and shot paint on them. That was actually disappointing; the latex paint wouldn’t flatten out at all, and the coverage ended up spotty with tons of fisheye spots.

I wasn’t sure whether this was a problem with latex on aluminum, or me having not been particularly thorough about cleaning my test patches. So I decided to just go ahead and mix up a small batch of primer and shoot it on some more test patches. This time, I cleaned the patches thoroughly, using the EkoEtch stuff I got from Stewart. I also gave each patch a final wipedown with acetone before starting to prime.

I was relieved to see that the primer went onto the aluminum quite nicely, just about as easily as the rattle can stuff does. It did take a little experimentation to get the flow control at a place where I got good coverage; I overdid it on one patch and got some lovely runs. The other ones ended up looking halfway decent, though:

As you can see, I still got some orange peel texture, so I still need some practice, but overall the coat looks good. I especially like that it has a sort of semigloss finish; between that and the color, I think my idea of just using this as the topcoat for the cockpit interior is going to work great. I’ll give these patches a day or so to dry and then abuse them with solvents and sharp objects to get an idea of how durable the finish is, but with it being an epoxy primer, I’m pretty confident it should be plenty durable.

With that done, I moved on to match drilling the left aileron. This went a lot faster than the right one since there was a lot less time spent scrutinizing the plans to ensure everything had gone together right. After pulling the aileron apart, I got started deburring the rivet holes in the ribs, then I decided to get the counterweights countersunk for their flush rivets. That was a little more challenging than normal countersinking, since I was working on a piece of pipe. I cut a chunk of 2×4 at an angle and attached both halves to a base to make a sort of holder for the counterweight pipe. The holder was clamped onto the drill press table with the countersink cage in place. Turned out to be a pretty nice setup:

I got Josie to come help hold the pipe (it is 4+ feet long after all) while I ran the drill press. We made quick work of the countersinking this way:

After that, I countersunk some flush rivet holes in the spar reinforcements, did a bit more deburring, and called it a night. Tomorrow I should be able to finish deburring and dimpling all the parts, I think. Too bad the weather will be so-so again, but maybe I’ll be able to get in some priming. It’d be nice to be able to start assembling the ailerons this week. If I can’t prime, I guess maybe I’ll move on to messing with the flaps.

Finally back to work. It’s been a hectic week, between getting a flat on my car and dealing with various other annoyances. The good news is that we have no plans over the weekend – I’m not sen flying tomorrow – so I should be able to get in some good work.

Anyway, tonight I moved ahead to aileron match drilling tasks. First the nose ribs are fluted to straighten them, then they’re clecoed to the spars and those attach holes match drilled. Next the ribs are clecoed to the aft side of the spar and match drilled as well. I did all of these tasks on both ailerons together, since they were simple and didn’t take up a lot of work space. Next, though, the whole aileron gets clecoed together, so I put the left side parts away and focused only on the right aileron.

First the trailing edge skin is clecoed to the skeleton, and then the counterweight goes in place under the nose skin. Here’s the counterweight sitting in place just before I clecoed the nose skin on (it’s just steel water pipe):

And then with the nose skin in place:

Then there’s a lot of match-drilling of stuff, with a few extra tasks. Most notably, the holes between the two skins and the bottom of the spar are drilled out to #30; these will get flush blind rivets as the last step to closing out the aileron. The real fun, though, is drilling the nose skin to the counterweight. There are holes all along the nose that are used as a guide to drill to the counterweight; these holes will get blind rivets as well. The prepunched holes in the skin are #40 but the final holes need to be #30. In order to make things easier – drilling through steel is a good bit tougher than aluminum – I first drilled all the holes to #40, clecoing as I went, then went back and enlarged all the holes to #30. Finally, the trailing edge skin is removed and a long #30 bit is used to drill a hole through each nose rib into the back of the counterweight.

Finally, it all comes back apart. Time to set this stuff aside and get going on the left aileron:

Unfortunately, it looks rainy this weekend, so I don’t think I’ll be able to get any priming done. Maybe I can at least tinker with the spray gun a bit to get the hang of setting it up. Even if it’s rainy, I could probably set up just inside the garage door to shoot some thinned latex paint as a test run. I guess maybe I could prime in the garage like that too if I had to. If not, priming might end up being a roadblock here. At least daylight saving time will be back soon, which will give me some more flexibility to prime after work if need be.

Well, today turned out to mostly be a construction day. I set off for Home Depot with a bit of a shopping list and came home with quite the assortment of lumber. The first thing I wanted to get done – which I’ve been planning for a while now – is a work surface for building the ailerons and flaps. The instructions specifically mention using a good flat surface when building these parts, lest one accidentally build in a twist. Problem is, my workbench tops are not flat, they both have a bit of bow to them. After some research, I went with an idea I got from VAF to construct a work surface. The basic idea is to use two pieces of MDF and sandwich pieces of good straight hardwood between them. The result is a very stiff unit sort of reminiscent in construction to a hollow core door.

In lieu of MDF that I’ve have to cut – which I hate doing, it generates ridiculous amounts of fine dust – I bought two 12”x6’ veneered MDF shelves, along with a few pieces of 1×2 poplar (and I spent a fair amount of time going through the pieces of poplar to find really good straight ones). Once home, I cut two long poplar pieces to go lengthwise on the shelves, then cut the rest of what I had into short cross pieces. Then there was a lot of measuring, drawing layout lines, and so forth, until I finally got to start putting stuff together. The shelves and poplar pieces are joined using wood glue and finishing nails. Here’s the first shelf with all the poplar nailed/glued in place, just before I put the other shelf on:

After nailing/gluing the second shelf to complete the sandwich, I put the finished unit on the sawhorses and used a digital level to check for twist:

I figure .2° of twist is an acceptable margin of error. And before anyone feel compelled to comment that it’s actually .4°, remember that the level was rotated. so the sign of one of those numbers has to be inverted before comparison. So it’s not .3 – -.1 = .4, it’s .3 – .1 = .2. Anyway, sorry for the math lesson.

With that done, I moved on to putting together the bending brake. I’d already cut the 2×6 I had into two lengths for this earlier, so now all I had to do was install the hinges to make the brake. I didn’t get any pictures of the brake by itself, because I was so eager to use the thing that I recruited Josie to come out and help me complete the skin bends. Here’s a 100% staged photo of the bending process:

Note the two large clamps on the top half of the brake. These were necessary in order to get sufficient leverage. That is, I couldn’t get the skin to bend simply by pushing on the board itself. In fact, to get the bend done, I was pushing down on the ends of those clamps with most of my (considerable) body weight while also leaning into the top of the board. If you’re wondering if it feels wrong to put that much force into a carefully-constructed aircraft part, then you’re 100% right. Funny thing is, I did this same thing with the elevators and rudder and I don’t remember it being this bad. I think maybe those skins were thinner than the aileron skin, but who knows.

Anyway, after finishing both bends, I clecoed the aileron spars into place so I could check the bends. The plans say the skins should be straight right up to the bend, and the bend itself should have a 1/8-3/32 radius. My bend radius actually came in a hair under the minimum (5/64), but I imagine that should be fine. It’s not as if I’m off by a huge degree. And the skins right up to the bend do look nice and straight:

After that, I removed the spars and went to work preparing those. The next step in the plans is to clamp the spar reinforcements into place and match drill with the spar ends, then clamp the hinge points into place and drill their mount holes to full size. I meant to get a photo of this assembly, but I got carried away and tore everything apart for deburring before I remember about the photo. Whoops. I’m sure you’ll get to see it at some point down the road.

(Somewhere in the middle of all this I remembered that I was going to rivet the flap braces today. I got so carried away with the ailerons that I forgot. Guess I’ll backtrack to that maybe tomorrow night.)

Anyway, that’s it for tonight. Tomorrow my Stewart Systems epoxy primer is supposed to arrive, which is good, since I want to use that on the aileron counterweights. If I haven’t mentioned it before, the counterweights are galvanized water pipe. I want to take particular care to avoid having any direct contact between the steel pipe and the aluminum skins, to head off any possible galvanic corrosion. Probably overkill, but hey, it’s a primary flight control. Plus it’ll be a good thing for me to try the epoxy primer out on.

Update: I did a bit of research about the trailing edge bend radius. It seems that the bend radius has a significant effect on control forces; a larger radius reduces forces, whereas smaller increases them. Similarly, if the skins are slight convex up to the bend, this decreases forces, and concavity would increase forces. Some reports are that any significant concavity can lead to the ailerons being so sensitive as to be unpleasant…I’ll be paying close attention to that when the ailerons come together for good. But my slightly-undersize bends err on the better side, I think. It sounds like I can always increase the radius a bit by tapping on the bend with a piece of wood to swell it a bit, but I’m not going to bother with that unless flight testing makes me feel that the roll forces are too much. Even then, I think it’d have to be pretty bad for me to go monkeying with the ailerons.

Didn’t get started until late in the afternoon, between flying in the morning and taking the dogs for a walk in the park in the afternoon. Once we got back home, my first order of business was to get the flap braces primed, since tomorrow’s weather is looking iffy. So I got those scuffed and cleaned and then went to work shooting primer once they were dry. I’m really liking the rig I came up with for holding parts upright while I prime:

Once that was done, I went to work back riveting all the stiffeners to the aileron skins. I had to get Josie to come out and help me get to the rivets way back near the bend in the skins, but most of this was easy solo work.

I also set all the rivets between the aileron gap fairings and the skin. I don’t see where they rivet in assembly with anything else, so no reason not to go ahead and get those rivets done.

Tomorrow I’ll hopefully be able to run to Home Depot to get materials to make a bending brake, then I can finish the trailing edge bend on the ailerons. I’ll also probably rivet the flap braces to the rear spar. I’ll have to shoot all those rivets with the gun, as the brace prevents access with a squeezer.

I didn’t really get started in the garage until 1 or so, since I flew with Joy again this morning. (and beat the plane up a bit, but that’s another story…) I also had a prospective builder who wanted to stop by, see the project, and get his hands dirty a bit. I was getting started countersinking the flap braces when he showed up, so I went ahead and finished those in between talking about all sorts of build-related stuff.

Countersunk braces:

From there, I got him to help me dimple the aileron skins, so they’re ready to have the stiffeners back riveted now, and then I can do the final bend of the trailing edge, assuming I ever get around to building a new bending brake:

After that, knowing that for me riveting was the most mysterious skill to me before I started building, I took some time and drilled a couple of pieces of scrap for my friend to practice riveting on. He squeezed a few, both with my cheap squeezer and the totally-not-cheap Main Squeeze, then shot a few with the rivet gun. So now at least that mystery has been assuaged a bit for him. Not too long after that, he had to go, so it was back to work for me.

Next I cleaned, scuffed, and primed my replacement spar reinforcement and aileron bracket angle:

Then I sat down and deburred all the rivet holes on the flap braces and aileron gap fairings. Yay, more deburring!

Unfortunately, it was while doing this that I cast a critical eye on the trims I made on the flap braces. When I made these cuts, I convinced myself that I was leaving sufficient edge distance between the cut line and the inboard most rivet hole, but upon looking at them again tonight, they just didn’t look right. So I looked up the real specs, measured, and…yep, I don’t have sufficient edge distance here. Time to put in an email to Van’s, I suppose. This might be an OK location to get away with this, but it’s not a call I feel like I should make. Worst case, replacements are $27 each, and maybe since my fuse kit is shipping this week they could just crate the replacement braces in with that. We shall see…

One of the edge distance offenders:

Well, at least I can clean and prime the aileron gap fairings tomorrow. I’ll hold off on the flap braces for obvious reasons. I also have the new aileron hinge stuff to rivet, and all the aileron stiffeners.