Brief Description: Finished passthrough holes for spar in fuselage
My concern for opening the holes in the fuselage for the center spar was the forcing function for a call to the factory for additional location data. Support received and the holes were finished. If I am to ever do this job again, I'm pretty sure it will be done from the inside of the fuse vs. the recommended outside approach. Picture 3 below is of the right side of the fuselage and shows the measurements taken from the rivet hole centerline to the critical edge of the cut out (so far anyhow).
