As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT PRESSURE BULKHEAD WEB SKIN HAS A CRACK INDICATION RADIATING TOWARD THE CENTER OF THE APB AT THE MOST CENTERED FASTENER COMMON TO THE RADIAL STIFFENER ALIGNED WITH STRINGER 22L. FOUND DURING HFEC INSPECTION OF NDT PART 6; 53-10-64, PER TASK CARD 5311-I-11681. APB WEB CRACK HAS BEEN REPAIRED, AS PER EA 20-153-01881 REF SA-M 326 - A1131890.