As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EXISTING REPAIR ON FUSELAGE STRINGER S56L BETWEEN FR54 AND FR54.2 REQUIRES EVALUATION FOR CONFORMITY. REPAIRED FUSELAGE STRINGER S56L BETWEEN FR54-FR54.2 PER A300-600 SRM53-10-14 FIG.203. THIS IS A CATEGORY B REPAIR. THE FIRST INSPECTION THRESHOLD WAS 51000FC / 89000FH AFTER REPAIR EMBODIMENT AND THE SUBSEQUENT INSPECTION INTERVAL AND METHOD WERE TBD PER A300-600 SRI 53-10-14-2-008-00. MAJOR REPAIR IAW FEDEX GMM 6-2-100.