As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:SV, RT BS 400 NOSE WHEEL WELL AFT CORNER SKIN PANEL/ EO FASTENER HOLE FOUND CRACKED THROUGH THICKNESS AT THE SECOND LAYER FROM BOTTOM IN THREE O/C AND NINE O/C DIRECTION REFER TO NDT TEST REPORT. ATTACH SPLICE REPLACED & INSTALLED IAW RI-53-11-10245, REV A & EO B747-5330-51344-A.