As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING SCHECULED INSPECTION. LT MAIN GEAR ACTUATOR BODY WAS FOUND TO BE CRACKED NEAR FORWARD ATTACH BOLT HOLE. ACTUATOR BODY REMOVED AND CRACK WAS VERIFIED BY METHOD OF DYE PENETRANT INSPECTION. ACTUATOR BODY HAD A DYE PENETRANT INSPECTION PREVIOUSLY PERFORMED 283.3 HRS PRIOR, WITH NO ANOMALIES NOTED.