What was found
CORROSION ON FLOOR SUPPORT BS 312 - BS 328, RBL 11, WL 208. ORIGINAL THICKNESS .080 INCH. FOUND TO BE OUT OF LIMITS PER SRM 53-10-51. REMOVED AND REPLACED STIFFENER PER SRM 51-40-02. (X)
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CORROSION ON FLOOR SUPPORT BS 312 - BS 328, RBL 11, WL 208. ORIGINAL THICKNESS .080 INCH. FOUND TO BE OUT OF LIMITS PER SRM 53-10-51. REMOVED AND REPLACED STIFFENER PER SRM 51-40-02. (X)