Date:	6-12-2010
Number of Hours:	4.25
Brief Description:	Spar web holes
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.