As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
AT BODY STA 827 R CRACK NOTED AT I/B RIVET BETWEEN STR 8 & 9 AT THE ACFT OUTLET EXTRUSION SUPPORT ATTACHMENT RIGHT SIDE OF CABIN MARKED. (REF NR 99836082) ACCOMPLISHED PERMANENT REPAIR AT FUSELAGE FRAME STA 827 R STRINGER 8 TO 9 R PER EC/RA 5311-02173. REF EA 5310-04716 REV 1. NO FURTHER ACTION REQUIRED.