As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CHAFE STRIP UNDER NR 2 ENGINE HORSE COLLAR PANEL (LT SIDE) IS PULLING UP AND LOOSE. UNINSTALLED CHAFE STRIP UNDER NR 2 ENGINE HORSE COLLAR PANEL LT SIDE BY REMOVING 3 BOLTS, 8 RIVETS AND 4 NUTPLATES IAW SRM 51-40-07. INSTALLED NEW CHAFE STRIP UNDER NR 2 ENGINE HORSE COLLAR PANEL BY INSTALLING 3 BOLTS AND 8 RIVETS IAW SRM 51-42-05-02-01. NO OTHER DEFECTS NOTED.