As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING POST FLIGHT INSPECTION MAINTENANCE DISCOVERED A HOLE/TEAR IN THE FUSELAGE SKIN UNDER THE NUMBER TWO ENGINE FROM APPARENT GROUND DAMAGE. THE DAMAGE WAS LOCATED BETWEEN FRAME 66-07 STRINGER 14-15 RIGHT. MAINTENANCE REMOVED THE DAMAGED SECTION OF SKIN AND PERFORMED A DOUBLER REPAIR. PRESSURIZATION CHECKS PASSED WITH NO DEFECTS AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.