As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE STRINGER AT STGR44RH BETWEEN FR38.2 AND FR39 FOUND CORROSION REPAIRED THE FUSELAGE CORRODED STRINGER AT STGR44RH BETWEEN FR38.2 AND FR39 PER A300-600F SRM53-10-14-201 FIG.208. THIS IS CAT B REPAIR. THE FIRST INSPECTION WAS 51000FC / 89000FH AFTER REPAIR EMBODIMENT AND THE SUBSEQUENT INSPECTION INTERVAL AND INSPECTION METHOD WERE TBD PER A300-600F SRI53-10-14-2-008-00. MAJOR REPAIR IAW FEDEX GMM 6-2-100.