As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
MAIN DECK CROSSBEAM C14, LBL 55.0, INNERGRANULAR CORROSION ON LOWER FLANGE. REMOVED CORROSION PER SRM 51-74-10. MEASURED REMAINING THICKNESS PER NTM 51-10-04. FOUND WITHIN LIMIT (REMAINING THICKNESS: 0.096 INCH). APPLIED FLAP PEENING PER SRM 51-29-00. REPAINTED AREA PER SRM 51-75-10.