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Date:  6-12-2010
Number of Hours:  4.25
Manual Reference:  
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.
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The right spar assembly with everything updrilled, but not for the angles

The right spar assembly with everything updrilled, but not for the angles

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The wing tie-down assembly drilled

The wing tie-down assembly drilled

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Then all the angles drilled as required

Then all the angles drilled as required

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