What was found
RIGHT VERTICAL STAB TO FUSELAGE ATTACH ANGLE HAS A 1/2" CRACK. REMOVED AND REPLACED RIGHT VERTICAL STAB TO FUSELAGE ATTACH ANGLE IAW SRM 51-40-02. RESTORED SURFACE PROTECTION IAW CPM 51-21-06.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
RIGHT VERTICAL STAB TO FUSELAGE ATTACH ANGLE HAS A 1/2" CRACK. REMOVED AND REPLACED RIGHT VERTICAL STAB TO FUSELAGE ATTACH ANGLE IAW SRM 51-40-02. RESTORED SURFACE PROTECTION IAW CPM 51-21-06.