As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
L/W UPPER L/E PANEL CRACKED LENGTHWISE APPROX 44". PANEL IS BEHIND NR 2 PYLON. REMOVED DAMAGED AREA, SANDED AND CLEANED AREA AS REQUIRED. PERFORMED HOT BOND REPAIR ON AREA AS PER SRM 51-40-12 NEEDS TO BE POTTED PRIMED AND PAINTED. POTTED AREA AND CURING PER SRM B747 SRM 51-40-12 RESTORED FINISH AS PER MM 51-24-11. ATLAS AIR EO 4757A295 ISSUED FOR REPAIR.