As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RH I/B T/E AFT FLAP O/B UPR PANEL LWR SURFACE SEVERAL AREA CORROSION(<P>CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01, REWORK AREA MEASURE ORIGINAL THICKNESS 0.106" L:25" X W 1" X D : 0.009", WITHIN SRM 57-53-01-1A-0 FIG 101 LIMITS. NO FURTHER DEFECTS NOTED</P>)