As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE LT FWD COWL FWD FUSELAGE MATING SURFACE WORN THROUGH AT BS 1350. FOUND AREA ON 1350 RING CHORD TO HAVE 100 PERCENT MATERIAL LOSS AND CRACKED OUT OF LIMITS. REMOVED 1350 RING CHORD. DRILLED UP AND INSTALLED NEW 1350 CHORD IAW SRM 51-30-2, 51-30-5.