Removed rear spar carry through from fuselage then updrilled attach angle holes through fuselage. Removed attach angles from fuselage then deburred rear spar carry through, shear web, and attach angles. Finished riveting rear spar carry through then riveted shear web onto carry through. Placed assembly back into fuselage and clecoed into place with spars pinned in place as well. Riveted attach angles to carry through then riveted shear web onto lower crossmember. Will rivet attach angles to fuselage skins once wings are removed.
Hours Worked: 2.38
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