As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT WING UPPER FIXED TRAILING EDGE PANEL HAS COMPOSITE CRACK, 3.5 INCHES FROM FORWARD EDGE OF PANEL AT WBL STA 515. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09, FIG 2, SHEET 1, 2 AND 5 PREPREG 250 DEGREES CURE PER SRM 51-40-12. REF: ATLAS AIR EO NR 4757A440.