As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
EVIDENCE OF CORROSION LOCATED ON STIFFENER BETWEEN FR.86-87 STR.27R AND 28R AS MARKED. (C-CHECK RO 9/26/2024) REMOVED AND REPLACED STIFFENER BETWEEN FR. 86 - 87 STR. 27R - 28R REF: SRM 51-40-08. STIFFENER REPLACED WITH OEM PART NO CHANGE TO WEIGHT AND BALANCE NOTED