As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION OF FR40 LOWER OUTBOARD RADIUS AREA BETWEEN STGR32-33LH FOUND CRACK SIGNAL IN THE UPR SECOND CRACK STOP HOLE REPAIRED THE CRACKED FR40 FWD FRAME FITTING LOWER OUTBOARD RADIUS AREA BETWEEN STGR32-33LH PER A300-600 SRM 51-40-21 & EA: 6-5710-161345 H P6. MAJOR REPAIR IAW FEDEX GMM6-2-100.SEE WRI 57-10/4765 FOR WORK DETAILS.