As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
(CAN) LEFT MAIN LANDING GEAR CYLINDER MOUNT, 2 BOLTS OF P/N AN525-416-20 AND P/N AN4-11A WERE SHEARED OFF. THERE WAS NO DAMAGE TO THE CYLINDER, BUT THE REMAINING 3 BOLTS WERE FOUND LOOSE. SUBMITTER SUGGESTED THESE BOLTS BE TORQUE CHECKED EVERY 100 HOURS.