Rebuilding horizontal stabilizer continues. I found jumping between the old plans, new plans and the service bulletin was getting confusing. So I decided to take a different approach. I am going to finish rebuilding the HS as if I was building it from the old plans. I will get it ready to close up and rivet, then remove those components that need to be modified for the service bulletin. That is primarily HS-405 ribs and the HS-702 spars. After completing the service bulletin I can close everything up and finish riveting. This will allow me to focus on completing the HS and not skip or miss any steps. So to that end here are the tasks completed today:
1. The HS-404 rib flanges that are riveted to the forward spar had some significantly oversized holes. It made sense to fabricate new flanges for the ribs, something I ran by Vans technical support. They did not have a problem with the plan so I moved ahead. Understand these ribs are there for support of the stressed skin horizontal stabilizer. The flight loads are handled by the beefy aft spar not by these small ribs. This was definitely a case of NOT adding the value of my time to the equation. Two new ribs would have been $20.00, it took a couple of hours to design, fabricate, test fit, drill, dimple, prime and rivet two flanges. Oh well, they are done now.
2. There are four flush rivets on the spars so there was dimpling and some countersinking completed of HS-702, HS-710 & HS-714.
3. I clecoed all the ribs in place and then clecoed the new right skin in place. The new HS-702 spar and the new skin were pre-punched (there were about thirty rivet locations that were not prepunched on the spar. I match drilled the skin to the existing structure being careful to not make the holes in the existing ribs oversized. I drilled those 30 rivet locations in the spar using the skin for match drilling. I match drilled the HS-404 & HS-405 to the spars.
4. After checking the structure to make sure I did not miss any locations I removed the skin and spar for deburring and dimpling.
5. Dimpling went fairly quickly, so the skin and the spar are ready to be prepped for limited primer. But alas I am out of primer so that will have to wait until tomorrow.
This portion of the project has moved ahead fairly quickly. Again I have not found any corrosion on the older components. Certainly by the weekend (it is Thursday evening) this some be closed up, riveted and in storage. Probably move to the elevators next as they are almost complete and then the rudder.