As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CENTER WING REAR SPAR VAPOR WEB RIGHT SIDE FRONT WALL ACCESS BY AC BAY SUPPORT ANGLE SIGNS OF CRACK DOR EV16<[01] PERFORMED HFEC ON UPPER SUPPORT ANGLE PER B737 NDT PART 6 51-00-00 PROC.23; SUPPORT HAS APROX. 0.625' CRACK. TOOL USED OLYMPUS NORTEC 600; B/C 166317; CAL DUE DATE 10/23.;[02] FAULT RESOLVED ON OTHER FAULT (FAULT WAS RESOLVED ON ANOTHER FAULT)<BR> TTG8Q00HQLSS;[03] VERIFIED STEP 2