The process of self-aligning interlocking construction utilized for the first half of the wing construction minimizes the potential for accidentally building a warp into the wing. It is very effective. However, the method used for building the second half of the wing was not up to the same standard. The completion of the top portion of the wing is similar to that of the bottom. I used the thin CA for all framing and the thick CA to attach the sheeting to the frame.
Construction then shifts to the fuselage.
This made it easier to know where to drill. The fuselage construction is superb. The self-aligning interlocking construction works very effectively. The firewall is not attached during the early stages of fuselage construction. This design will more effectively absorb the shock of landings than the traditional method of bolting the gear into the bottom of the fuselage.