As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND AN 8" CRACK IN LT WING FIXED LEADING EDGE SKIN PANEL UPPER SURFACE AT WS 425.5. PERFORMED OPERATION 04 OF EA 5731-01010 AND REPAIRED CRACKED AREA IAW SRM 51-70-17 AND ATTACHED LAYUP PROCEDURE WORK CARD (COMPOSITE REPAIR WITHOUT CORE REPLACEMENT).