As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NUMBER 2 PYLON LOWER SPAR HAD WEAR SPOT FROM CONTACT WITH THE CNA AT RIB 5. THE BLEND OUT IS .003 INCHES DEEP & 0.100 INCHES WIDE. AN ANTI-CHAFE PLATE WAS INSTALLED IAW SRM 54-51-12 PARA 5 B FIG 202. REQUIRES RE-INSPECTION IAW SRI 54-51-12-2-001-00 PARA 3 A TBL 202. INITIAL INSPECTION AT 49000FC OR 61200FH FROM TIME OF REPAIR EMBODIMENT, WITH SUBSEQUENT INSPECTION EVERY 16800FC OR 21000FH.