As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON REMOVAL OF PAINT, THE TECHNICIAN FOUND CORROSION ON INTERIOR FUSELAGE RT MLG PRESS BULKHEAD WEB JUST AFT OF FRAME 26 FLOORBEAM ON THE RT OTBD CORNER. THE CORROSION WAS CLEANED AWAY & BLENDING WAS PERFORMED AT THE LOCAL DAMAGE AREAS. NDT WAS THEN PERFORMED TO RECORD MATERIAL LOSS & DETERMINE THAT THE PART WAS FREE OF CRACK DEFECTS. REFERENCE EO 53-02-2014.