As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C M/D LEFT BS 880 TENSION TIE TO FRAME CONNECTION FOUND NR 10 HOLE CRACK AT FAILSAFE CHORD RUNNING UP. CRACK LENGTH 0.040 INCH. M/D LEFT BS 880 BETWEEN STR 8L TO STR 12L AREA FAILSAFE CHORD REPAIRED AS PER SRM 51-40-03 FIG 2.