As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED LT SIDE AT APPROX STR DATUM 55.62 PERCENT. FOUND TO BE OUT OF LIMITS IAW SRM 55-00-00-101-001. INSTALLED NEW SERVICEABLE ATTACH ANGLE IAW DWG JBA 670-23103, & SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.