As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CORROSION ON THE PLATE LOCATED IN THE FRAME UPPER PART (INNER STRUCTURE) WHICH IT IS SUPPORTING THE ACCESS PANEL 447BR, RIGHT ENGINE, AFT NACELLE STRUT FAIRINGS.(<P>PLATE OF THE ACCESS PANEL 447BR WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 52. NO FURTHER DEFECTS NOTED.</P>)