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 THE AFT END OF THE ANGLE. THE CRACK MEASURED 1" LONG AND IS TYPICAL OF CRACKS DOCUMENTED PER BAC S/B MD90-53-027. THE CRACK WAS TRIMMED OUT AND REPAIRED WITH A REPAIR ANGLE PER THE S/B AND PER DAL ER/A 460482-14.