What was found
CORRODED STIFFENER AT BS 553.75 RBL 39 INSIDE WHEEL WELL. THE STIFFENER WAS REPLACED IAW SRM 51-20-1, REV 110 AND 51-30-02, REV 110.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORRODED STIFFENER AT BS 553.75 RBL 39 INSIDE WHEEL WELL. THE STIFFENER WAS REPLACED IAW SRM 51-20-1, REV 110 AND 51-30-02, REV 110.