Brief Description: Left main spar web - transfer hole locations
The left spar pieces are stacked slightly differently than the right wing spar. On the left spar, the root end of the long pieces, W10-01 (which has all the pilot holes drilled in it), is sandwiched below W10-05. In that position the holes at the top and bottom of W10-01 cannot be used to locate and drill through all 4 layers of web at once.
So I cleco'd W10-01 and W10-05 together so that I could transfer the hole locations from W10-01 to the face of -05 that will be exposed when the spar webs are stacked and the spar caps are positioned.
I also located and drilled the holes for the wing tie-down angle, which I had forgotten to do last night.
W10-01 laid over W10-05. Using -01, I located the holes on -05.
W10-05 from the opposite side
W10-05 shown below W10-01. See the holes at the top of -01 that were located on -05
