As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LEFT WING L/E UPPER SURFACE PANLE HAS A TWO FOOT CRACK JUST AFT OF THE NR 10 VARIABLE CAMBER FLAP FROM ILES 693 - 822. REMOVED THE SKIN AND HONEYCOMB CORE, FABRICATED AND INSTALLED A REPLACEMENT SKIN AND HONEYCOMB CORE IAW SRM 51-70-07, PARA 4.