As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
FUSELAGE - BS 540 S-22L REF FIG 2 CIRCLE NOTE 1 AD 2019-11-06; EO 14516. CRACK INDICATION FOUND. REF B737 NDT PART 4 53-20-02. B/C19498. REQ. REMOVE FASTENERS AND PERFORM A OHEC PROCEDURE TO VERIFY CRACK INDICATION IAW B737 NDT PART 6; 51-00-00 PROC. 16. / ACCOMPLISHED FUSELAGE BS 540 S22L DRAG LINE AND SKIN REPAIR PER INSTRUCTIONS ON EO 5331-E-14519-NG