As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ON REMOVEL OF THE VERTICAL STABILIZER AND REINFORCEMENT PLATE FROM THE AFT FUSELAGE BULKHEAD AT FS 317.75, A CRACK APPROXIMATELY .75 INCHES IN LENGTH WAS LOCATED IN THE BEND RADIUS OF THIS BULKHEAD JUST ABOVE AND TO THE RIGHT OF THE UPPER LEFT VERTICAL STABILIZER ATTACHMENT HOLE.