As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
UPON VISUAL INSPECTION OF FRICTION DAMPERS AND TRANSMISSION MOUNTS, FOUND LIFT LINK FITTING CRACK ON THE AFT LUG BUSHING AREA COVERING THE ENTIRE LATERAL (SIDE). TRANSMISSION MOUNTS WERE REMOVED AND INSPECTED FOUND PRESSURE REQUIRED TO DEFLECT MOUNT WAS BEYOND LIMITS ALLOWED.