As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
TWO CRACKS WERE REPORTED IN THE NR 2 ENGINE PYLON OUTBOARD STRUT SKIN AT THE FWD TORQUE BOX ACCESS HOLE. A .5 INCH CRACK WAS FOUND IN THE UPPER FORWARD CORNER AT APPROX NS 158. THE SECOND CRACK IS ALSO .5 INCH LONG AND IS IN THE UPPER AFT CORNER AT NS 192. REPAIRED PER DAL ER/A 360197.