As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON FUSELAGE CROWN SKIN COMMON TO FASTENER LOCATIONS FROM STA 1016+2; TO STA 1016+23; BUTT LINE 8 TO 13; LEFT AND RIGHT.<[01] CERTIFIED APPLICABILITY OF SRM 53-00-01-1A-1;[02] ' AS PER EA 24-153-00521; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS.';[03] VERIFIED CORRECTIVE ACTION 2