As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING VISUAL INSPECTION OF AFT FUSELAGE INTERNAL RIGHT SIDE WALLS FOUND BENT KICKPLATE AT BS 1800. AFTER OPENING SIDE WALLS FOUND BS 1800 FRAME CRACK 3.5 INCHES BETWEEN STRINGER 10R AND 11R. FOUND FRAME STATION 1820 INNER CHORD DENTED BELOW STRINGER 12R. PERFORMED REPAIR IAW SRM 51-20-01, 51-30-02, 51-10-02, 51-10-00 AND SOPM 20-41-02. (M)