As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING LOWER SKIN PANEL ABOVE THE O/B MID SPAR FITTING HAS A 0.55" CRACK. (REF NRC B583433) PERFORMED INTERIM REPAIR PER EA 1-A57-3318. REINSPECT EVERY 720 DAYS FOR CRACK PROPAGATION. PERFORM A PERMANENT REPAIR ON OR BEFORE THE 28Y CHECK.