As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE INNER CHORD OF THE FS 1303 FRAME WAS FOUND CRACKED AT A HYDRAULIC LINE CLAMP ATTACHMENT LOCATION JUST ABOVE RT VENTRAL STAIRWAY TORQUE BOX STRUCTURE. THE CHORD WAS CUT ABOVE THE DAMAGE AND THE LOWER SECTION OF CHORD REMOVED. A NEW SECTION OF CHORD WAS INSTALLED AND SPLICED WITH A REPAIR ANGLE PER ER/A 383919-14, REV A.