As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) DURING INSPECTION, CRACKS WERE FOUND IN THE FORWARD PORTION OF THE NR 2 NACELLE OTBD ATTACHMENT ANGLE. SECTION CONTAINING CRACKS WAS REPLACED IAW RD 8-57-1053. SIMILAR FINDINGS ON THE AFT PORTION OF THE NR 1 NACELLE INBD DRAG ANGLE FWD PORTION OF THE NR 1 NACELLE OTBD DRAG ANGLE AFT PORTION OF THE NR 2 NACELLE OTBD DRAG ANGLE.