As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING HFEC INSPECTION OF THE LOWER VERTICAL STABILIZER AT THE UPPER SECTION ON THE RT REAR SPAR CAP FORWARD FLANGE, CRACK FOUND APPROX 3/4 INCH LENGTH ALONG THE RADIUS LOCATED NEAR THE LOWEST FASTENER HOLE. REPAIRED IAW EA 1-5530-T0334788 P1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.