Lots got done yesterday and today. Deburred and cortec treated the parts of the root area. Riveted top skin root to top skin. Assembled and riveted spar root angle, wing root angle. Riveted root nose skin and included an extra forward rivet to improve the fit. Applied Cortec to the trailing edges. Attached stand-off to the fuel lines before reassembling and riveting trailing edges. Did not rivet the root top skin to the wing, as that will come when attaching to fuselage.
With the exception of inspection nutplates, which I will do later (I may add more inspection plates), this completes the wing construction.
Riveting trailing edges
Root skin. The blemish on the nose skin looks like a dent, but is not.