As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
VERTICAL FIN FRONT SPAR FWD SPRING ANGLE (176A3101-26) CRACKED AT L/H ATTACH POINT (MARKED) <[01]. REMOVED AND REPLACED NEW VERTICAL FIN FRONT SPAR FWD SPRING ANGLE IAW SRM 51-40-02 AND AIPC 55-33-11-02A.; [02] VERIFIED CORRECTIVE ACTION ENTRY 1.