As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ENGINE PYLON BOX BEAM LOWER WEB CRACKING FROM ANCHOR NUTS AT STRESS PANEL FS 640 LEFT AND RIGHT SIDES. REPAIRS ACCOMPLISHED IAW REO 601R-53-61-366, LEFT AND RIGHT SIDES OF BOX BEAM. HFEC INSPECTION CARRIED OUT IAW REO 53-61-366. NO CRACKS FOUND.