As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING ACCOMPLISHMENT OF AD 96-19-05 ULTRASONIC INSPECTION OF THE MAIN LANDING GEAR YOKES, THE FOLLOWING DEFECT INDICATIONS WERE NOTED. THE INBD SIDE OF THE S/N NR 2 MLG YOKE HAD A CRACK INDICATON .500 INCH IN LENGH BELOW THE FILL VALVE/RETAINING PIN HOLE. THE OUTBOARD SIDE HAD A .250 INCH CRACK INDICATION BELOW THE FILL VALVE/RETAINING IN HOLE. (X)