As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING UPPER FIXED L/E PANEL HAS AREA OF DELAMINATION, 4.0 INCH WIDE BY 45.0 INCH LONG. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18 SHEET 3 AND 5, PREPREG 250 DEGREE CURE PER SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A409.