As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT STABILIZER LEADING EDGE HAS A APPROX 1-2 IN DENT OR CRACK ON RIVET ROW APRROX 11 RIBS OUT FROM FUSELAGE. REMOVED SKIN DAMAGE TO ACCESS RIB. FOUND RIB DENTED .040" WITH GOUGE. BLENDED AND REWORK. ACP HFEC INSPECTION AND CONFIRMED NO CRACKS. INSTALLED INTERIM RPR ON SKIN REF SRM 55-10-01 REPAIR 3.