As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE AFT PITCH LOAD FITTING FASTENER REMOVED. FOUND TO BE DIFFERENT GRIP LENGTH FRON THOSE STATED IN EA 01-451812-03AD, OPN 2801 TO VERIFY. EARN NR 1607B-0057 RAISED AND NR 2 ENG AFT PITCH LOAD FITTING INSTALLED IAW ERA 507119-14AD PRI REV 0 SDR RAISED AND ACTL LOG PAGE 2050 RAISED IAW FINAL ERA 507119-14AD REV ORIGINAL COMPLIED WITH ON NON ROUTINE 0669.