As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING UPPER L/E PANEL AT WBL 450 SURFACE HAS AREA OF COMPOSITE CRACK. ACCOMPLISHED PERMANENT REPAIR OF AREA OF CRACK AS PER B747 SRM 51-40-09 FIG 18 AND 747 SRM 51-40-12. CRACK LENGTH IS 2.0 INCHES LONG AND REPAIR AREA IS 4.0 INCH BY 7.0 INCH. ALSO, REFERENCE ATLAS EO 4757A333.