As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
CRACK INDICATION ON FRAME 68 STGR 8 LH UPPER CORNER BETWEEN UPPER FASTENER AND UPPER RADIUS. CRACK LENGTH IS 0.130 INCH APPROX. AT AFT GALLEY AREA (1 EA), PERFORMED PERMANENT REPAIR LOC. ON FRAME 68 STRG 8LH UPPER CONER BETWEEN UPPER FASTENER AND UPPER RADIUS, AS PER SRM A320 53-41- 12- 300-012 FIGURE 003