As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE RT FUSELAGE TO VERTICAL STABILIZER ATTACH ANGLE WAS FOUND WITH A CRACK NEAR CANTED FS 1474. THE CRACK WAS REMOVED WITH A TRIMOUT TO THE HORIZONTAL FLANGE OF THE ANGLE. THE AREA WAS REPAIRED WITH A STEEL REPAIR ANGLE PER ER/A 384977-14, REV A.