As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FRAME 1 BULKHEAD WEB, SURFACE CORROSION. DURING INSPECTION, MINOR CORROSION WAS FOUND IN AREAS SHOWN IN FIGURE 2. THE SURFACE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGE AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINED THAT THE PART WAS FREE OF CRACK DEFECTS. REFERENCE EO 53-01-2014.