As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT SIDE OF FUSELAGE, STRINGER 26R LAP SEAM HAS FASTENERS PULLING THRU SKIN LAP SEAM AT BS 1670. EVIDENCE OF CORROSION. CUT OUT DAMAGE AT RT SIDE AT FUSELAGE, STRINGER 26R LAP SEAM BS 1670. FABRICATED DOUBLER & FILLER & INSTALLED IAW EA F-5330-T0 305495 REV NR PS P1.