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 A FLANGE CRACK AT AN EXISTING HYDRAULIC CLAMP ATTACH POINT. THE CRACK IS JUST ABOVE THE AFT ENTRY STAIR TORQUE BOX. THE CRACK WAS ROUTED OUT OF THE FLANGE AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE. THE REPAIR WAS ACCOMPLISHED PER ER/A 380047- 14, REV A.