What was found
VERTICAL FIN FRONT SPAR; FWD SPRING ANGLE (176A3101-26) CRACKED AT LT ATTACH POINT<[01] REMOVED AND REPLACED VERTICAL FIN FRONT SPAR FWD SPRING ANGLE IAW SRM 51-40-02-0G-0 AND DWG #176A3101 SHEET 4 REV-.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
VERTICAL FIN FRONT SPAR; FWD SPRING ANGLE (176A3101-26) CRACKED AT LT ATTACH POINT<[01] REMOVED AND REPLACED VERTICAL FIN FRONT SPAR FWD SPRING ANGLE IAW SRM 51-40-02-0G-0 AND DWG #176A3101 SHEET 4 REV-.