As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING C-09 CHECK, A .250 INCH CRACK WAS FOUND ON THE NR 2 ENGINE PYLON FRAME CUTOUT FOR PANEL 443GL AT FORWARD LOWER CORNER INBOARD SIDE OF PYLON. MAINTENANCE PERFORMED A HFEC INSPECTION OF CRACK AT NR2 ENGINE PYLON FRAME CUTOUT; STOP DRILLED CRACK AND PERFORMED ANOTHER HFEC INSPECTION TO VERIFY THE CRACK WAS CONTAINED; FABRICATED A REPAIR DOUBLER, AND INSTALLED REPAIR PART IAW AWA ER.