As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENGINE AFT PITCH LOAD FITTING FASTENER REMOVED FOUND TO BE DIFFERENT GRIP LENTH FROM THOSE STATED IN EA 01-451812-03, AD OPN 2801 TO VERIFY. EARN NR N1607B-0056 RAISED AND NR 1 ENGINE AFT PITCH LOAD FITTING INSTALLED IAW ERA 507119-14 AD, REV 0 SDR RAISED AND ATCL LOG PG 2050 RAISED IAW FINAL ERA 507119-14 AD REV ORIGINAL COMPLIED WITH.