Trimmed fiberglass tip rib per supplemental instructions and clecoed into place. Did not fasten to main spar support angle but riveted to rear angle. Little bit of a gap on upper part of leading edge to be fixed with fiberglass at a later time. Created aileron and flap hinge halves and clecoed into place. Discovered both ailerons are wider than depicted on plans and will need to be cut at a later time.
Hours Worked: 3.05
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