As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
ABNORMALITIES NOTED ON LEFT PYLON MID SPAR FITTING INBOARD AND OUTBOARD EDGE OF UPPER TANG. PYLON WAS REMOVED AND AREAS WERE POLISHED PER 767-300 SRM CHAPTER 51, HIGH FREQUENCY EDDY CURRENT INSPECTION SHOWED NO CRACKS. AREAS WERE CAD PLATED PER SOPM 20-42-10. EA B767-54-013104 CLASSIFIED MAJOR AND APPROVED FOR STAGE I STATIC STRENGTH.