As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
RIGHT PYLON, INBOARD SIDE OF HYDRAULIC BAY SUPPORT CHANNEL IS CRACKED ACROSS THE FORWARD END BY THE FORWARD BAY DOOR LATCH PAD CRACK IS APPROX 2.5". REMOVED AND REPLACED P/N 313T1380-245 IAW B767 DWG 313T1380 AND B767 SRM 51-40-02, ACFT WAS GROUNDED.