As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
#1ENGINE AFT PYLON SUPPORT FITTING CRACKED<[01] COMPLIED WITH EA 23-154-00799 FOR STOP DRILL OF CRACK. REF TTG8Q00JEESY;[02] ADDED CRACK LENGTH OF 0.500' AND NDT REQUIRED TO YES.;[03] EDITED TO ADD TOOLING T016002 S/N WN0011 AND T010052 S/N 161212 PER E40330 VIA EMAIL (ATTACHED);[04] CERTIFIED