As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C LEFT BS 820 TENSION TIE TO FRAME CONNECTION NR 4 AND NR 10 FASTENER HOLE FOUND CRACK AT FRAME WEB DOUBLER RUNNING UP THRU THICKNESS. CRACK LENGTH .125 INCH. LEFT BS 820 TENSION TIE TO FRAME WEB ATT DOUBLER REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.