As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
BROKEN LATCH AND SHEARED RIVETS ON AFTER CARGO DOOR SERVICE PANEL AND SCRATCHES ON FUSELAGE SKIN RT SIDE BETWEEN STA 1780 TO 1820 AND BETWEEN STRINGER 34 TO 40. INSTALLED NEW LATCH, SMOOTHED SCRATCHES AND AREA TREATED PER SRM 51-30-02 AND 51-10-01.