As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ATTACH ANGLE ALONG FRAME 12A RIGHT IS CRACKED ON FWD SIDE APPROX 6 INCHES BELOW THE FLOOR. REMOVED ANGLE IN REF TO A300-600F SRM 51-40-21; PARA 6. RECEIVED A NEW ANGLE, PO 624972.1. LOCATED AND DRILLED IN REF TO A300-600F SRM 51-40-21; PARA 6. INSTALLED IN REF TO AIRBUS DWG A5361037801.