As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
PLEASE PERFORM HFEC TO VERIFY CRACK ON #2 ENGINE INLET COWL.<[01] PERFORMED HFEC OF SUSPECTED CRACK ON #2 ENGINE INLET COWL PER NDT PART 6; 51-00-00 PROCEDURE 23. VERIFIED CRACK IS .500' L AND ENDS AT THE FASTENER HOLE AND THE SKIN EDGE.