As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RT LEADING EDGE CAVITY INTERIOR SKIN SHOWS SIGN OF CRACK AT UPPER PART AT APPROX WS 385.9 JUST INBOARD OF NR 4 L/E ACTUATOR. REMOVED FASTENERS AND STOP DRILLED CRACK PER SRM 51-10-1. INSTALLED DOUBLER REPAIR PER SRM 57-30-4 FIG 9. TREATED AND PRIMED PER SRM 51-10-2.