As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND CRACKS AT EIGHT FASTENERS IN RT SECTION 41 SKIN PANEL. THE CRACKS WERE APPROXIMATELY .5 INCH LONG. THE SKIN PANEL WAS REMOVED AND A NEW PANEL WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-7, AND 51-20-4.