As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE STRINGER 44RH FOUND HEAVY CORROSION BETWEEN FR38.2 AND FR39 REPAIRED THE CORRODED FUSELAGE STRINGER 44RH BETWEEN FR38.2 AND FR39 PER A300- 600 SRM53-10-14-201 FIG.201. THIS IS CATEGORY B REPAIR AND MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600 SRI53-10-14-2-010-00. FIRST INSPECTION AFTER REPAIR EMBODIMENT: 51000FC/89000FH. SUBSEQUENT INSPECTION AT INTERVALS: TBD. INSPECTION METHOD: TBD. MAJOR REPAIR IAW FEDEX GMM6-2-100. ORIG SUB DATE: 9/6/2022