As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
#1 ENGINE I/B FAN COWL ; AFT UPPER CORNER HAS A CRACK 2.7 IN. LENGTH.<[01] PERFORMED HFEC INSPECTION OF THE REPAIR AREA PER NDT MANUAL PART 6; 51-00-00 PROCEDURE 23. NO DEFECTS NOTED. COMPLIED WITH SRM 54-20-01-2R-13 STEP 4E.;[02] PERFORMED HFEC (ROTARY SCANNER) INSPECTION OF THE REMOVED FASTENER HOLES PER NDT MANUAL PART 6; 51-00-00 PROCEDURE 16. NO DEFECTS NOTED. COMPLIED WITH SRM 54-20-01-2R-13 STEP 4F.;[03] REPAIRED PER EA 23-171-03496