As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PERFROMED EDDY CURRENT INSPECTION OF VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE IAW MAC NDT INSP PROCEDURE ET-2. ATTACH DRAG ANGLE IS VERIFIED CRACKED. PERFORMED CUTOUT OF DAMAGED AREA ON FWD DRAG ANGLE IAW REO 670-53-31-018. PERFORMED NDT OF AREA IAW REO 670-55-31-018. NO INDICATIONS NOTED.