As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT NR 1 PYLON LOWER SPAR HAD A .005 WEAR MARK ON THE PYLON LOWER SPAR FROM CONTACT WITH THE CNA. THE WEAR WAS BLENDED IAW SRM54-51-12 FIG 103, & AN ANTI-CHAFING PLATE INSTALLED IAW SRM 54-51-12, 5B FIG 202. REQUIRES INSPECTION IAW SRI 54-5 1-12-2-001-00 PARA 3 A. INITIAL INSPECTION 32700FC OR 40900FH FROM TIME OF REPAIR EMBODIMENT WITH SUBSEQUENT INSPECTION 11900FC OR 14900FH. MF4012 CREATED TO MONITOR.