As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LH VERTICAL STAB TO FUSELAGE ATTACH FORWARD DRAG ANGLE POSSIBLY CRACKED. AFTER DETERMINING THE END OF THE CRACK BY NDT INSP IAW NDTM PART 1 51-20-08-230 ON REPORTED FWD DRAG ANGLE, IT WAS REPAIRED BY INSTALLATION OF REINFORCEMENT ANGLE IAW SRM 55-31-00-201-001-A01, COMPLIED WITH 51-900-1002-SKY.