Ailerons Mounted and Push Rods Started

Time: 5 Hours

Now that the flaps are done I needed to start to assembly of the control surfaces onto the wings. First item was to mount the aileron bell cranks to the main spars. These bell cranks transfer the motion from the control stick in the fuselage 90° towards aft and the ailerons. They are powder coated steel and rotate around a brass bushing.

20140514-172110.jpgI first cleaned up the top and bottom of the bell crank tube where the bushing slides into. I then made a measurement on the tube and the bushing. Van’s calls for the bushing to be 1/64″ to 1/32″ longer than the bell crank tube. I used the scotch-brite whell and sand paper to get the length perfect. The bushings were a little tight inside the tube so I put the bushings in my drill press which I bought after checking various Drill Press Reviews and turned it on while using some 400 grit sandpaper to hone them down until they slid nicely into the tubes.

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20140514-172505.jpgNow I had to ream the inside diameter of the bushing to accept the 1/4″ bolt that goes through it. I just placed the bushing in my padded vise and used the reamer in my hand drill. It work pretty slick and the reamer just guides itself and is always centered.

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20140514-172723.jpgI then assembled the bell crank pieces that will hold the push rod from the bell crank to the aileron. For this I had to cut a spacer from some stock that they give you.

20140514-172933.jpgI bolted the bell cranks back into position on the spars but didn’t torque them as I’m not sure if I will have to remove them later. I had originally torqued and sealed the 2 brackets that the bell crank bolts to on the spar back when I was working on the spar but relieved that I needed to remove them to install the bolts for the bell cranks.

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20140514-173329.jpgWith those back on I moved my attention to mounting the ailerons. The ailerons are connected at 2 points on the wings, 1 bracket on each end. They use a combination of bolts, small washers, a large washer and a spacer similar to the bell cranks. The ailerons need a travel limiter, a physical stop so they don’t travel to far and cause damn he to them or the wing skins. Van’s has you make a small angle piece and rivet to the leading edge rib of the aileron. This angle will eventually hit the aileron bracket as it moves closer to its full travel. When it hits that’s the farthest the aileron will travel. My buddy Glen had a much better design that he used on his first RV-8 and repeated it on the one he is building now. What he did was transfer the contact point of the stop from the angle that’s on the rib to the spacer that’s in the bracket on the aileron. Clear as mud? Let me show you in pictures. Normally the stop would happen prior to the spacer hitting the bracket, around 1/8″ as you wouldn’t want just the spacer to be the limiter as it is just aluminum tubing. Glen used a piece of delrin tubing, it’s like plastic to me, and cut it to match the length of the spacer. He then reamed the inside so that the spacer would slide into it. Now when the aileron travels it will hit this new soft covering of the spacer and stop the movement. I first cut the space and made it perfect then I cut the delron tubing to match and reamed it to final size. I then assembled it all together as the plans show along with this new part.

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20140514-174832.jpgThat white spacer will come in contact with the bracket on the spar and stop it’s travel. Glen said this work great and it was super easy to make and install. You can see in several of this photos the various washers and how tight they are. I bought a set of washer wrenches to help with inserting these. They are just thin stainless steel wrenches that have various sized ends that hold washers by spring pressure. You then can slide them into place and when the bolt is inserted pull on the wrench and they pop off.

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20140514-175229.jpgAgain I didn’t torque any of these as I’m not sure if they will need to come off later. I then turned my attention to the push rods for the ailerons. There are 2 per side, one short steel one that goes from the bell crank to the aileron and a larger aluminum one that goes from the fuselage controls to the bell crank. I cut them with my pipe cutter to the length described on the plans. The shorter ones are cut to 23 13/16″ and the larger ones to 69 3/16″ for the RV-8. The plans give you call outs for several different models. Once cut I cleaned up the ends and the insides so that the rod ends would slide into them easily.

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20140514-175840.jpgI repeated this process for the larger tubes which were a little easier to cut since they are aluminum.

20140514-180027.jpgThe large rods get riveted to their ends by 6 rivets. 360° divided by 6 is 60° so I downloaded a protractor online and printed it so that I could create a template to make the rod ends.

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20140514-182133.jpgI used the template to mark all 4 ends of the 2 rods and grabbed my jig I bought from Harbor Freight to drill them. After I bolted the jig down and made all the required adjustments I drilled 3 holes and went completely through the rod making all 6 holes. I started with a #40 bit and used my #30 reamer to enlarge the holes.

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20140514-210541.jpgI then moved on to the smaller rods in the same fashion. These just use 2 rivets per end at a 90° to each other. Since these are steel I sprayed a bunch of primer inside and rolled them around to get the entire inside covered.

20140514-210859.jpgThat’s where I decided to call it a night. I should have a few hours in the Hangar tomorrow.

Right Flap Done

Time: 3 Hours

I got home this afternoon from my 2 day trip and was anxious to get out into the Hangar. I repeated the entire process that I used on the left flap item for item. As with any task it always seems that the second task goes much quicker as you learn from the first one. This flap was no exception to that rule and I finished it in about half the time.

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20140513-210525.jpgAnd that’s it! 2 flaps done and looking great!

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Left Flap Done

Time: 8 Hours

I had beautiful weather again today so I had the Hangar door open to enjoy the day while building. The first task was to get out the tools to dimple the skins of both flap skins. I had to use the DRDT, pneumatic squeezer and my close quarters rivet puller dies to get to all the holes. I didn’t take any pictures of this as you have seen them before. Before I did any riveting I decided to work on the V block jig Van’s describes. I used the boards that I used to sandwich the ailerons. I cut two of them 14″ and left one factory end on each of them so I had a square surface. I then lined them up and screwed them together. I then used one of the exterior ribs to come up with the V angles.

20140511-211557.jpgA couple of minutes at the bandsaw and I had 2 identical V brackets.

20140511-211713.jpgI then added a couple of 2×4 legs to allow me to screw them to the workbench. I just used one of the flap top skins to determine how far apart to put the brackets.

20140511-211935.jpgSo now was the time to start riveting. I decided that I would do an item on one flap then repeat it on the other. The first task is to rivet the single hole at the aft end of the interior ribs to the rear spar that is actually the bottom skin curled up. The interesting this is that during mock up I needed 4 shims on the left flap and when I set it up after dimpling I no longer needed them as the rib was right up against the spar! Go figure.

20140511-212504.jpgNext was to rivet the main spar angles to the spar making sure you leave the holes that attach to the inboard rib open for later.

20140511-212625.jpgI then decided to work on the piano hinge attachment point. Van’s gives you two options for the pin, leave it as one length and cut it in 2 pieces removing a couple eyelets of the hinge to access them. I chose the second as it is pretty popular and makes for easy removal of the flaps. My buddy Glen gave me a photo from his build on how he did it so I just replicated his. First up was to measure out where I wanted the ends to layout which told me which 3 eyelets to remove(2 from one side and 1 from the other). It ended up being that I wanted to leave 65 eyelets from the outboard end of the hinge, removing 66-68 eyelets. I then had the area that I would need a nutplate on the spar. I drilled matching holes on the left and right spars. I used that hole and a screw to align the nutplate to drill for the 2 rivets.

20140511-213619.jpgI then cut 2 eyelets to make my retaining brackets(you will get the idea at the end) and drilled them together for the screw and hit both sides with the scotch-brite wheel so the were perfectly matched.

20140511-213807.jpgThe inboard rib gets riveted to the double plate as well as the nutplate that connects the flap control arm to the flap.

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20140511-214029.jpgNow I had all those items done on both flaps I reassembled the flaps and set the right on the shelf and put the left in the V jig I had made.

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20140511-214252.jpgOnce you have the flap tight in the jig you can remove the spar so you have access to the inside to rivet. I got one of my bucking bars and taped it all up except on on the faces so I didn’t scratch up the inside of the skins.

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20140511-214606.jpgI took a couple of photos to see if you can see how I used this bar. For the top to bottom skin overlap the bar just rested on the rear spar and worked like a charm.

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20140511-220643.jpgI was able to rivet all the skin overlap holes pretty easy. For the skin to ribs I ended up using my little 3/8″ thick 1.5″x1.5″ bucking bar since it’s pretty tight in this space. It took me several hours to get all these interior rivets.

20140511-221448.jpgOn the inboard rib there are 4 rivets at the aft end on the top and bottom that are aft if the rear spar and you have no choice but to use MK319 blind rivets here.

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20140511-221718.jpgAfter you get all the interior ribs done you can slide in the spar and start riveting the spar to ribs with LP4-3 blind rivets. The lower side rivets are easy to get to but the top ones require a little manipulation of the rivet stem and the top skin. I found that my cheaper rivet puller fit pretty nice.

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20140511-222148.jpgI then moved on to the top skin to spar holes. I tried a couple of different bucking bars with different amounts of success. I ended up using my longer 1″x1″x6″ that had an angle on one end. I also tried this one too and it worked ok as well.

20140511-222628.jpgThose rivets went really fast as I worked down the line. You then can work on the bottom skin to spar to hinge holes.

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20140511-222917.jpgSo that was all the rivets on that flap! It was a long day but I still wanted to finish the hinge pins so I could clean the flap and call it complete. I cut the pin in half and made several measurements and took them to the vise to make some bends. One bend to follow the spar flange and one to send it to the nutplate and retaining clip I made earlier. Once I had all the bends right where I wanted them in bent the ends just a little to keep the retaining clips from falling off when removing the pins.

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20140511-223654.jpgI was real happy with how the pins came out. I just need to do a final trim of the other ends as I left them a little long. I then took the flap out of the jig and cleaned it all up. 1 down and 1 to go, sometime this week.

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And More Flap Work

Time: 9 Hours

Today started out with our weekly builder breakfast with my good buddies. I made it home by 10:30 and got hard at it working on the flaps. My work consisted of deburring every hole, finishing all edges, edge rolling and priming. It took me around 3.5 hours per flap to accomplish all those tasks. There are 6 ribs, 1 spar, 2 skins, 2 angle/plates and multiple shims. This work is the toughest and most boring on this build but it must be done and my OCD is in full effect as I want all my edges perfect. Again I only primed the mating surfaces and left the sides that will be painted unprimed. Here are a few pics of the work today but I didn’t take that many since it’s just boring.

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20140510-220009.jpgI was able to get everything done except to dimple the skins as my back was getting sore and 9 hours is enough I think. After I finished up the first flap I took a break and went over to my buddy Glen’s house to look at his finished flaps and how his hinges turned out. I also got a chance to sit in his fuselage to see how the 8 feels, and it feels awesome!

20140510-220331.jpgSo tomorrow is supposed to be a great day weather wise and I should get a bunch of work done if I don’t take the Harley out for a ride! 😉

More Flap Work

Time: 8 Hours

I started today with a few errands I needed to finish before heading out into the Hangar. When I got back a set out to match drill all the holes in the right flap skins and the hinge like I did on the left flap. That went pretty fast since I had just did the left side. Before I broke down all the parts I decided to jump ahead a couple of steps and fabricate the flap support plate and angle. These two pieces beef up the inboard rib/spar area where the flap control arm will connect. First you need to cut down a couple of angles from a piece of 1.5″ x 2″ stock.

20140509-161837.jpgI then cut down the shorter edge to 3/4″ per the plans.

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20140509-162303.jpgThe inboard rib angles towards the inboard as it goes aft which means the plate must be bent to match so that the end that rivets to the angle I just made is square. Vans says that the angle is to be 6.3° First I clamped the piece in my bench top vise at the prescribed 25/32″ line.

20140509-162904.jpgI then used my digital level to establish 0°. You can see that it wasn’t perfectly 90° in the vise, probably my bench is off a little. I then zeroed it out to establish my starting point. I then clamped two boards on both sides of the plate and made a sandwich to give me some leverage and bent away. After a couple of try’s I got the angle perfect.

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The end result leaves the angle square with the spar and the plate matched to the inboard rib.

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20140509-165026.jpgI then fabricated the 4 spacers needed on the aft tips of the inboard and outboard ribs. These are needed where the bottom flap skin stops short of the aft end if the rib and the top skin wraps around and overlaps the bottoms skin.

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20140509-170041.jpgThe bottom skin curls up at the aft end to essentially create the rear spar of the flap. The aft end of the 4 inner ribs get a single rivet to attach to this rear spar. Van’s says that sometimes the rib does not touch the rear spar and you need to add spacers. I had to make 4 of them for the right flap out if .020 sheet but I didn’t need any on the left flap, go figure.

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20140509-182359.jpgI then I larger the forward most hole in the support plate to 1/4″ and drilled the 2 holes for the platenut. This is where the flap push rod will connect.

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20140509-182531.jpgI then put the assembled right flap on the shelf and took the left flap completely apart for deburring and edge finishing. The first thing I did was to drill the spar holes to my workbench to allow for countersinking of the bottom flange of the spar. The top flange can be dimpled but the bottom flange has the hinge on it so you want the inside edge of the spar flange flat so that the hinge sits flush. You don’t want to dimple or countersink the hinge flanges as they are too soft.

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20140509-215629.jpgI did a little edge finishing before deciding that 8 hours was enough for today and my back is getting a little sore. I will get another good weekend worth of work over the next 2 days.