As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT WING, LOWER SKIN HAS CORROSION AROUND FASTENERS AT STRINGER 58 & FWD SPAR & XRS 763. PERFORMED UT INSPECTION. REMOVED FASTENERS & REMOVED CORROSION. PERFORMED OPEN HOLE HFEC, BLEND OUT OF LIMITS. FABRICATED REPAIR DOUBLER & INSTALLED IAW EA 008-5730-38-A6028.