As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE RT SIDE FUSELAGE SKIN AT FS 225.20 ON THE SURROUND STRUCTURE FOR THE ACCESS PANEL WAS GOUGED APPROXIMATELY .5 INCH W X .4 INCH L X .012 DEEP. BLENDED DAMAGED AREA, PERFORMED EDDY CURRENT INSPECTION, ADDED PROTECTIVE TREATMENT AND EXTERIOR FINISH IAW SRM. (K)