As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING LANDING LT LOWER STRUT ASSEMBLY SEPERATED FROM UPPER CYLINDER. LOWER TORQUE LINK FAILED IN AREA ABOVE MACHINED BOSS AT THE LOWER STRUT ATTACHMENT END, ALLOWING THE LOWER STRUT / WHEEL ASSEMBLY TO BLOW OUT OF THE UPPER CYLINDER. THIS PN TORQUE LINK REQUIRES 500 HOUR RECURRING INSPECTION IAW AD. PROBABLE CAUSE, FATIGUE. REMOVE FROM SERVICE AND REPLACE WITH LATEST TORQUE LINK DESIGN.