As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PUNCTURED AND GOUGED FUSELAGE SKIN AT AFT CENTERLINE INBOARD OF TAIL JACK POINT. REMOVED DAMAGED SKIN, PERFORMED HIGH FREQUENCY EDDY CURRENT INSPECTION PER BAC NDTM PART 6, NO CRACKS. INSTALLED NEW SKIN WITH DOUBLER AND TREATED PER BAC SRM 53-30-03 AND 51-10-02.