As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION FOUND A .5 INCH CRACK AT FORWARD UPPER CORNER OF NR 2 ENGINE PYLON O/B ACCESS PANEL. AN INTERIM REPAIR HAD BEEN INSTALLED PREVIOUSLY AND THE ITEM WAS PLACED ON DIP. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01204. THE DIP WAS CLOSED.