As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(AD2020-17-03) DURING HFEC SURFACE INSPECTION, CRACK WAS FOUND AT RH CONTINUITY FITTING WITH A CRACK LENGTH OF 0.165". END MARKED IN RED. CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT. W/C:69929 ACCOMPLISHED REPAIR IAW UAL EC/RA 5311-03076 REV WITH NO NOTED D EVIATIONS. W/C:69929