As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENGINE FAN EXIT ACOUSTIC LINER HAS A FOUR INCH CUT. DAMAGE IS LOCATED AT THE 5 O'CLOCK POSITION ON THE INNER C DUCT INNER SKIN. THIS DAMAGE IS ON THE REVERSER COWL INNER AIRSTREAM HALF. SEE SRM 54-33-01 PG2 ITEM 9 FOR SKIN DAMAGE LOCATION. DAMAGE IS 3.25 INCHES IN TOTAL LENGTH WITH 2.5 INCH OF THAT DAMAGE THROUGH SKIN SURFACE. ACCOMPLISHED INTERIM REPAIR PER UA-EVA-80738.