As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 PYLON AT RIB 5 LOWER CHAFE PLATE IS WORN. REMOVED PLATE & BLENDED THE AREA. MATERIAL LOSS IS .002\ WITHIN LIMITS IAW SRM 54-51-12, PG 209-210. HFEC INSPECTED BLENDED AREA & FOUND NO CRACKS. REINSTALLED THE PLATE WITH AN EXTENDED WEAR STRIP IAW SRM 54-51-12.FIG.202.