As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C NR 2 PYLON STRUT TO UPPER LINK FITTING, 2 UPPER VERTICAL HOLES HAVE CRACK INDICATIONS (HFEC). HFEC UPPER LINK FITTING NDT51-00-16 PT6 IND CRACK IN HOLES. HFEC UP LNK STRUT HOLES IAW NDT51-00-17 PT6 IND NO CRACK. REMOVED 2 DISCREP HOLES TO .5155 PER EA757-5454-27-A1833, PRELIM NR 2 HFEC INS 2 DISCREP HOLES PER NTM 51-00-16 PT6. NO CRACK INDICATIONS NOTED.