As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE #2 ENGINE INBD FAN COWL HAS A CRACK NOTED ON A SUPPORT ANGLE AT APPROXIMATELY 7 INCHES BELOW PANEL 423AL AND 14 INCHES FROM THE FWD EDGE. (MARKED)<[01] VERIFIED NO CRACK INDICATION ON BRACKET PER NDT PART 6 51-00-00 PROCEDURE 23.;[02] REINSTALLED T CLIP PER SRM 51-10-02. AFTER NDT PART 6 51-00-00 PROCEDURE 23. FOUND NO DAMAGE.;[03] 02 - INSPECTED PER [SRM 51-10-02-0G-0-B00388 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - TRACKED COMPONENT - PERMANENT)]