The first thing to do was to try and figure out what exactly I had. The aft fuselage side skins were corroded way beyond repair with heavy white corrosion and deeply pitted. They were trashed. The upper and lower wing skins were showing much less white corrosion, and I decided they needed to be replaced. The few parts that were riveted had anywhere from 25% to 40% bad rivets, so I decided to reject anything with rivets.
Finding a home for the project was net easy. I live in a high-rise condo in large urban area, no chance of "home" building. I was unable to find any space that was suitable within 50 miles. I ended up hitting pay dirt when I went to EAA chapter 260 at C56. I reached out to Jay Vieaux, an EAA technical counselor at 260 and I can't say enough about him. My hangar is next to his and he stops by at least once a weekend. The support I get from him, and the rest of the chapter, is phenomenal. It's good to be in a community of builders.
I'm feeling a bit frustrated about my progress lately. Life happens, Thanksgiving through new years is always slow build time, I made progress in Jan and Feb, and March. This month I has been slow at the hangar, Spent time in Texas visiting my Grand-kids and this weekend I'm recovering from oral surgery. (ugh)
Progress to date. Vertical stabilizer is ready to have the skin riveted. Not happy with the fiberglass tips. They were cut and pilot drilled by the previous builder, I'm trying to decide if I should Use, replace or fabricate the stabilizer tips. Jay is an expert with an English Wheel. The glass tips are asymmetric about the vertical longitudinal axis. see photos.
The vertical stab appears to lean to the left because it is only clamped to the table on the left side. I found the asymmetry in another Sonex of the same vintage as my kit.
What a long strange trip it's been....