Drilled the final holes that go through the spar cap and the various angles on the face of the web. Also drilled for the wing tie-down assembly. There was about an .025 thickness of the flange left after the CNC milling, so I added an .025 spacer between the tie-down angle and the web of the spar cap. This made everything about flush.
Then went back and up-drilled all the holes throughout the spar assembly, for either rivets or screws.
Took everything apart and began deburring.
The right spar assembly with everything updrilled, but not for the angles