As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENGINE INLET COWL WIRE MESH DELAMINATED AT 12 O'CLOCK POSITION. DAMAGED AREA EVALUATED AND FOUND OUTSIDE REPAIRABLE LIMITS IAW AMM 71-11-01 AND SRM 54-10-01. TRIMMED AND RESEALED LOOSE EDGES OF DAMAGED WIRE MESH IAW AMM SRM 71-11-01 AND SRM 54-10-01. REPLACE NR 1 ENGINE INLET COWL WITHIN 90 DAYS.