As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 3 PYLON TOP SKIN, AFT EDGE, ABOVE LINK FITTING HAS A 0.375 INCH CRACK. TRIMMED OUT SKIN TO REMOVE CRACK AS PER 747 SRM 51-10-01. ACCOMPLISHED HFEC INSPECTION TO VERIFY REMOVAL OF CRACK AS PER 747 NDT MANUAL PAR 6 SECTION 51-00-00 FIG 4. ALSO, REFERENCE ATLAS AIR XEO NR 54-022807.