As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
R/H INBD LEADING EDGE SKIN FASTENER HOLE HAS A CRACK INDICATION IN THE FASTENER HOLE/COUNTERSINK COMMON TO THE FRONT SPAR AT KRAS 206.2 +12IN APPROX. PER BOEING NDT MANUAL PART6;51-00-00 PROC.16 AND 53-30-00 PROC.3 / INSTALLED REPAIR IAW SRM 57-41-01-2R3 REPAIR 3.