As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 1 ENGINE ACOUSTIC LINER HAS A 1.25 INCH CRACK LOCATED 0.25 INCH FWD OF THE FAN RUBSTRIP AT THE 10 O'CLOCK POSITION. THE DAMAGED CRACKED AREA IS ALSO DENTED FROM CRACK AFT TO RUBSTRIP JOINT. CRACK MUST BE CHECKED PRIOR TO EACH DEPARTURE AND INLET COWL MUST BE REPAIRED OR REPLACED WITHIN 5 CYCLES. REPLACED NR 1 ENGINE NOSE COWL.