As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FS 1303 FRAME INNER CHORD WAS FOUND WITH FLANGE DAMAGE FROM A HYDRAULIC CLAMP ATTACH POINT 6 INCHES ABOVE THE RT VENTRAL STAIRWELL TORQUE BOX STRUCTURE. THE DAMAGE SECTION OF FLANGE WAS TRIMMED OUT AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE PER ER/A 382311-14, REV A.