I just want to understand/confirm something. I'm currently working on my slow build RV8 wings and was concerned about the Wing Tiedowns. Looking at the construction, it seems like the tiedowns are only being supported by 4 AN3 bolts. Is it true that these 4 AN3 bolts (and possibly some support from two of the spacer screws) are strong enough in shear strength to support nearly 1/2 the weight of the aircraft when it is up on jacks using the tiedowns as jack points? Or is there another source of support for the weight?