As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE FORWARD O/B LUG OF THE NR 1 ENGINE PYLON DRAG STRUT WAS FOUND WITH CORROSION DAMAGE ON THE OUTER SURFACE OF THE LUG. THE LUG HAS BEEN SPOTFACED 0.050 TO REMOVE CORROSION. THE NR 1 PYLON DRAG STRUT O/B LUG THICKNESS REMAINING IS 1.353. THE LUG WAS REWORKED.