As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL STAB LOWER RT DRAG ANGLE IS CRACKED. PERFORMED EDDY CURRENT INSPECTION OF RIGHT V/STAB TO FUSELAGE DRAG ANGLE TO LOCATE END OF CRACK IAW NDTM 51-20-006 END OF CRACK IS MARKED. CUT AWAY DAMAGE FROM VERTICAL STAB LOWER RT DRAG ANGLE IAW REO 670-55-31-018. PERFORMED EDDY CURRENT INSPECTION OF CUT LINES ON RIGHT VERTICAL STAB TO FUSELAGE DRAG ANGLE IAW REO 670-55-31-018 PER NDTM 51-20-006 NO DEFECTS NOTED.