As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPPER FUSELAGE SKIN EXTERIOR HAS AREAS OF CORROSION AROUND FASTENERS AND BETWEEN BAYS APPROXIMATELY BS 887- BS 1006 STR 3L TO STR 3R. CORROSION ON UPPER FUSELAGE EXTERIOR SKIN AROUND FASTENERS AND BETWEEN BAY APPROXIMATELY BS 887-1006 STR 3L TO STR 3R REPAIRED IAW ATS ER 20-02696; REV IR, AND PER EA 20-153-00768 REV IR. 55981U.