As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING THE MAINTENANCE INSPECTION, CORROSION WAS FOUND ON THE INNER SURFACE OF THE FUSELAGE SKIN AT FR82, BETWEEN STRG-27R AND STRG-28R. THE DAMAGE WAS CORRECTED IN ACCORDANCE WITH THE REPAIR INSTRUCTIONS OUTLINED IN ETD2025-190-900569 AND THE COOPESA ENGINEERING ORDER COO-EO-2025-21613-R00.