As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AFT FUSELAGE BULKHEAD STA 2164, CRACK FOUND ON STIFFENER U-ANGLE RT SIDE LOWER ALIGNMENT PIN HOLE AREA. CRACKED STIFFENER REMOVED AND REPLACED WITH REWORKED STIFFENER AS PER SRM 51-35-01 REV 46. STIFFENER REWORKED AS PER DRAWING AJC7001 REV DT. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV 112.