As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CENTER WING VAPOR WEB FWD WALL AREA ABOUT RBL10 SUPPORT ANGLE EVIDENCE OF CRACK<[01] PERFORMED A HFEC INSP. ON SUPPORT ANGLE PER B737 NDT PART 6 51-00-00 PROC. 23; 0.500' CRACK CONFIRMED. TOOL USED OLYMPUS NORTEC 600; B/C 172389; CAL DUE DATE 03/23.;[23] REMOVED UPPER ATTACH ANGLE FABRICATED AND INSTALLED REPAIR PER SRM 57-10-10-2R-5 REPAIR 5 FIG. 202 DETAIL A;[24] VERIFIED STEP 23 INSTALLAED NEW UPPER ATTACH ANGLE