As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FOUND TYPICAL DENT DAMAGE TO STATIONS 478 TO 500, FUSELAGE FRAME INNER CHORD BETWEEN STRINGER 30 LEFT AND 31 LEFT DUE TO IMPACT DAMAGE FROM CARGO PALLETS. COLD WORKED AS BEST POSSIBLE, HIGH FREQUENCY EDDY CURRENT SURFACE SCAN BOTH SIDES OF REWORKED FLANGE. FABRICATED, TREATED AND SEALED PER EA B767-53-013924.