Well I was able to trim out the left aileron during flight but I found there is some slop in the ailerons. At first, I thought it was my stick since the rivets holding the stick to the torque tube was a little loose, so I installed a bolt. The left aileron still did not seem to move up as much as the right, so I removed the fiberglass arm rest cover in the passenger section to expose the torque tube. Then I clamped the CS121 universal joint torque tube and when I move the left aileron, I can move it up and down 3/8 of and inch . The right moves as well. With the universal joint torque tube clamped, I found the CS124 bracket that the two aileron rod end bolt to is moving. The plans show the CS123 Boston Gear is floxed to the firewall so the only thing I think of that may be loose is the AN3-11A bolt that secures CS124 bracket tube that goes inside the CS121 torque tube. Unfortunately, I have no idea how to check this out since everything is behind the firewall. Any help would be appreciated or maybe this is something I can just live with?
After reviewing the plans and looking at my plane, I see the CS121 torque tube has two AN3-11A bolts located in the rear passenger section. Is the AN3-11A bolt that secures the CS124 bracket tube depicted on firewall detail drawing 17 right behind the firewall like the drawing indicates or is it actually located in the rear passenger section where I can get to it? If it is actual the second bolt in the passenger section, then maybe the hole there is oval and all I have to do is drill a new hole and install the bolt in the new hole? It kind of sucks not being the builder and not knowing how your plane is put together.