What was found
CRACK APPROX .25 INCH GOING TO RIVET HOLE AT TOP AFT CORNER OF NR 2 PYLON CUTOUT FOR PANEL 463CL. DYE CHECK CONFIRMED CRACK, EDDY CURRENT CK PER BAC NDT MANUAL PART 6 AND INSTALLED DOUBLER PER BAC SRM 54-30-03.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
CRACK APPROX .25 INCH GOING TO RIVET HOLE AT TOP AFT CORNER OF NR 2 PYLON CUTOUT FOR PANEL 463CL. DYE CHECK CONFIRMED CRACK, EDDY CURRENT CK PER BAC NDT MANUAL PART 6 AND INSTALLED DOUBLER PER BAC SRM 54-30-03.