As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
LT MLG TORQUE LINK BROKE ABOUT 1" BELOW UPPER MOUNT AFTER LANDING. TORQUE LINK WAS SENT TO NTSB FOR TESTING WITH THE FOLLOWING REPORT. THE FATIGUE ORIGIN AREAS CONTAINED NO EVIDENCE OF GOUGE DAMAGE OR CORROSION DAMAGE. ON ONE SIDE OF THE LINK THE FATIGUE CRACK EXTENDED APPROX THROUGH 40 PERCENT OF THE WALL AND ON THE OTHER SIDE THE FATIGUE CRACK EXTENDED THROUGH APPROX 30 PERCENT OF THE WALL.