As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT INBOARD FLAP CORROSION BLEND AREA UNDER INTERIM REPAIR ALONG RIB LOCATED APPROXIMATELY 17.5 FROM INBOARD END OF UPPER INBOARD SKIN PANEL OUT OF LIMITS PER SRM 57-53-01-1A. INSTALLED PERMANENT HOT BONDED DOUBLER REPAIR SRM 51-70-10-2R 4 AND EA COMP-57-025207.