As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
POSSIBLE CRACK AT ATTACHING ANGLE WHERE THE VERTICAL STAB AND FUSELAGE MEET APPROXIMATELY 67.5 SPAR DATUM AREA. (MARKED, OUT OF SCOPE) (C-CHECK) RO 6/24/2020 REPAIRED CRACK AT ATTACHING ANGLE WHERE THE VERTICAL STAB AND FUSELAGE MEET. APPROX 67.5 SPAR DATUM AS PER SRM. TASK CARD COMPLIED WITH.