As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE:C+SI INSPECT REMOVED STAB.RIBS. FOR CRACKS AND FORWARD FINDING TO ENGINEE RING(RETAIN CRACKED RIBS) DVI INSPECTION PERFORMED IAW CUSTOMER REQUEST :CRACKS NOTED @ L/H RI BS 17:20 AND 136:50 AND R/H RIBS 17:20 AND 66:50 AND 99:79.