As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UNDERSIDE LEADING EDGE ABOVE NR 2 ENGINE PYLON (PANEL) HAS CRACK GREATER THAN 1 INCH. REPAIRED REF ECRA 5740- 02327. STOP DRILL MUST BE CHECKED EVERY "A" CK AND REPAIRED AT "D04" CK. PERFORMED HFEC. NO CRACK. MADE A REPAIR PART AND INSTALLED PER ECRA5720-02355.