As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT WING UPPER FIXED LEADING EDGE PANEL CRACKED AND DELAMINATED, ILES 833.00, 20 INCHES FROM AFT EDGE OF PANEL. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 18, SHEETS 3 AND 5 PREPREG 250 DEGREES CURE PER SRM 51-40-12. REF: ATLAS AIR EO NR 4757A438.