As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE-C/CK, NR 1 PYLON I/B DRAG ANGLE CRACKED EXTENDING APPROX .25 INCH PAST STOP DRILL HOLE. STOP DRILL END OF CRACK .250 AND POLISH TO 32 MICRO INCH FINISH. VERIFIED AND MARKED END OF CRACK UTILIZING HFEC. STOP DRILLED CRACK AS MARKED BY NOT VERIFIED CRACKS ENDS AT STOP DRILLED UTILIZING HFEC.