Very cool, congrats.
Do you think you did the toe-in check too late in your build? I'm actually still doing a bunch of welding-- just reformed my gear leg trailing edge fairings, so perhaps now is the time to do it.
IIRC you load the aircraft to 2000 lbs on grease plates and take the measurement?
Yes, I would totally recommend checking this at least prior to fabric.
So we bought ours as a "quickbuild" kit, and it came with the fuselage and landing gear as a matched set. Our understanding from the documentation was that these two items, since they in effect are "unique" to each other, were drilled and attached to the fuselage attach points and a "pipe" or piece of tubing was supposed to be run through both axles prior to welding the clusters on the gear. The engineer suggests that there be as close to ZERO toe in/out as possible. This factory procedure would accomplish that spec. But unfortunately, there have been a few kits that this wasn't done at the factory. 6 that are known, is our understanding.

Assumptions right?
We checked it, we just checked it a little later than we should have. The rough check procedure was to roll the aircraft straight backwards 10ft (measure distance between center tread), roll it forward 10ft (and check again distance). Ours was producing 3 inches worth of delta!
Long story short, our options were:
Two new gear from factory, with the high chance that they indeed would be incorrect as well.
Heat the clusters on both landing gear to a specified temperature and bend them to get the gear to as close to zero toe as possible
Some we are told, have left varying amounts of toe alone and hope for the best
After talking it over for some time, we chose to heat and bend. We obtained the procedure from Bob, found a hangar to use (THANK YOU Soldotna Aircraft repair) and hung the airplane up once again. We cut the fabric back a ways on the gear legs, heated with a rose bud and melt stick to 900 degrees, and used an 8 foot pipe with an ID 1.5" to bend the axles back in our case a few inches (at the end of 8 feet). After letting the gear cool, we found that we were now well in spec at near zero toe.
Here is a pic of the procedure, you can barely see a chalk line travelling fore-aft of the fuselage for centerline. Notice we did in fact use grease plates for the adjustment although we did not load the aircraft beyond empty weight.

So it worked out, no biggy - we have already spent many years on this - whats another 8 hours of work not including phone calls and emails getting a procedure, right?

ha
Now this won't be a problem for a person who is scratch building their aircraft, as you would hopefully produce near zero toe by accomplishing the factory procedure during initial welding of the gear clusters. But one thing we found out, is that if you damage a gear leg - chances are that you would need to heat/bend the new one to get correct toe measurements - either on a scratch or kit built aircraft. One plus we assumed by getting a factory jigged fuselage and gear leg, was we wouldn't need to modify replacement parts in the future.
Our aircraft now tracks perfectly straight and it was just another hurdle. "You gotta WANT it"
