Nearly there…

I keep finding little things that still need to be done on this wing. At least it won’t take as long to do the next one. I’ve been getting over there nearly every day, but the little bits of work here and there didn’t seem worthy of a complete build log post. But since the last update:

  • Cleaned, primed, and drilled the fittings for the upper/lower aileron pushrods
  • Located and drilled holes for the aileron bearing block screws
  • Managed to punch a hole in the aileron LE skin, and glued a patch over that (will need to smooth it out with some micro)
  • Worked to trim the upper aileron bay piece to get full UP travel on the aileron

I also found that the aileron DOWN travel is restricted by one of the bolts for a fitting on the rear spar. I recall reading that the rear spar thickness was changed from 1/2″ to 3/4″ at some point, and that causes interference. The aileron should have 22 degrees travel in both directions; I get about 15 – 17 degrees down right now. It would be less if the aileron and wing were covered. I need to dig though the plan supplements and find the section that talks about that and see how to fix it. The obvious choice would be to notch the lower front corner of the aileron leading edge to clear the bolt head, but I’d really prefer some other solution… it sure would have been nice for whoever did the plan changes along the way to have properly documented this stuff on the drawings themselves, rather than just tacking on random pages with these “Oh, by the way…” notes (which are themselves occasionally wrong).

Aileron freedom – and wing walk work

Today I located and temporarily screwed the bearing blocks in, and cut the aileron free from the wing.

With that done, I decided to have another look at the wing walk situation. I don’t know why the support bits were the way they were, but I decided to just get on with making them work. When I look at the plans, especially the oblique view, indicate that the parts may have been cut in an attempt to match a much earlier version of the wing without much of the reinforcement at the main spar root. Anyway… Two of them had the aft end cut well enough to work at the rear spar. The inboard support needed to be trimmed at both ends. All had to be modified to fit the main spar.

In the end I got all three to fit, though I’m not terribly thrilled with the lack of good options for supporting and blocking the ends.

Next up were the notches for the cross braces. Most were too shallow and look to have been cut out with an end mill or router; the corners were rounded. I used a file to square up the corners and deepen the notches to fit the 1/2 x 3/4 pieces.

I figure I’ve got another hour or so of work to get all of the blocking and support in place before mixing epoxy. Probably more; I still haven’t figured out what I’m going to do about the extension of the walk forward of the main spar. If I build it to plans I’ll need to remove or hack up the first false rib. And of course the plywood pieces require significant modification.

On the bright side, the plywood skin for the wing walk curves nicely and won’t be a problem to get glued down. I’d been worried about that, and had visions of needing to make my own laminated piece there, but it’s fine.

Wing work thru 2/20

Top and bottom leading edge plywood has been scalloped. That wasn’t as big a chore as I thought it would be. We used a thin stainless scale to establish a curve between each pair of ribs, marked along it with a pencil, and cut the wood with a utility knife. Some cleanup with sandpaper and Bob’s your uncle.

I’ve made a few iterations of the bearing block. Today I’ll print a couple more test pieces and I think I’ll be done. They fit great, the aileron is very well located, all in all I think it’s a lot more precise than a piece of plywood and a chunk of PVC pipe.

I’ve been preparing some of the wing attachment fittings. I have one or two of each part drilled with 1/8 pilot holes; I’ll use those to match drill the rest, then enlarge the holes for the AN4 bolts. The biggest question was hot wo round off the ends. For that I drilled a 1/8 hole exactly 1/2 inch from the disk on my disc/belt sander. Now I can use the tail end of a drill bit as a pivot pin and put a nice radius on the end of the fitting. I’m glad I kept my gray Scotch-Brite wheel on the bench polisher; it makes quick work of cleaning up the ends of the AL bars.

Wing work – 2/16, and a better idea

Yesterday (2/16) I cut and glued in some corner blocking I had missed on each end of the aileron and the ends of the aileron bay. Lesson learned: that would have been a lot easier had I done it before the geodetic bits and plywood stiffeners had been installed.

I’m getting to the point where I kind of need the torque tube bearing blocks installed. Then there are the 3/8” spacers, which the plans call out as pieces of PVC pipe. I figure, since I’m going to CNC machine the bearing blocks anyway, why not just make those and the spacers one piece? I pulled up the design in OpenSCAD and added the spacer. I gave it a slightly larger ID than the bearing block so it doesn’t add drag to the aileron control. I 3D printed a couple samples to use for fit & function testing. If that goes as expected I’ll get a chunk of 1” UHMW and pass the design file to Stew for machining. I’d planned to use some 1/2” UHMW I have for the bearing blocks, but I’ll keep that for now and use it for something else.

3D printed test part. It’s difficult to see but there’s a step in the bore for the torque tube.

Rib modifications

I built all of the wing ribs exactly to plans, per Sheet 1 of the plan set. Unfortunately, that sheet has not been updated since the rear spar was changed from using 1/2″ square spar caps to 3/4″. As a result, the X braces just aft of the rear spar were way too far forward in all of the ribs I built — all except for the 16 aileron ribs, which don’t get those X braces. Installing the rear spar would require extensive trimming or notching of the geodetic stock — I just wasn’t happy with that. Plus, there’s another piece of square stock on the aft face of the rear spars on the upper wings. It already needs to be beveled to clear the ribs, and with the braces in place would need to be cut down to almost nothing.

So, out came the razor saw. I cut those two X braces from every one of the ribs, cut new ones, and glued them in place with enough clearance for the rear spar. It was a couple hours’ work, but since I have a lot of extra rib geodetic material wasn’t that big of a deal. On the bright side, I got to test the glue joints on all of the pieces I pulled out. We want the wood to fail before the glue does. Every single one of them broke the brace or separated it along a grain line before the glue gave up — 100% successful tests. That was not unexpected, but was reassuring nonetheless.

Now we can move forward with assembling the wings.