As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE STATION 2360 RT SIDE, BETWEEN STRINGERS 30R AND 32R HAS AN AREA OF 3.0 INCH LONG BY 11.0 INCHES WIDE OF CORROSION ON SKIN. ACCOMPLISHED PERMANENT REPAIR AS PER 747-200 SRM 53-30-03 FIG 1. AREA OF CORROSION WAS CUT-OUT AND HFEC WAS ACCOMPLISHED TO VERIFY ANY CRACKS AS PER 747 NDT MANUAL 51-00-00 FIG 23 PAR 6, DOUBLER AND FILLER WERE INSTALLED PER 747-200 SRM 53-30-03 FIG 1. ALSO, REFERENCE ATLAS AIR XEO 53-040207.