As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FUSELAGE SKIN WAS FOUND DENTED COMMON TO THE CREASE BEAM BETWEEN STA 360 TO STA 380. FURTHER INSPECTION FOUND THE CREASE BEAM OUTBOARD CHORD AND SHEAR WEB DAMAGED. THE SKIN DENT WAS WITHIN SRM LIMITS. THE DAMAGE WAS REPAIRED IAW ECRA 5310-04100. A DIP WAS ISSUED TO PERFORM A PERMANENT REPAIR WITHIN 24 MONTHS 0R 3000 CYCLES, WHICHEVER COMES FIRST.