As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE LT HORIZONTAL STABILIZER HAD DAMAGE ON THE L/E REQUIRING A MAJOR REPAIR. THE DAMAGE WAS 6" IN LENGTH, AND LOCATED 1.5 FT FROM THE STABILIZER ROOT. THE DAMAGED SKIN WAS CUT OUT, THE SURROUNDING STRINGER AND RIB STRUCTURE WAS INSPECTED WITH NO FURTHER DAMAGE NOTED. AN INTERNAL DOUBLER AND PATCH REPAIR WAS USED TO REPAIR THE STABILIZER IAW THE SRM DOCUMENTS 02305, REV 8, CHAP 12-B-55-00-00-00A-661A-A AND 12-B-57-00-00-00A-664A-A. REPAIR RM 06361, PART 3.