As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
A STRESS CORROSION FRACTURE OCCURRED IN THE RADIUS AREA WHERE THE HIGH CARBON SPRING STEEL MAIN LANDING GEAR LEG AND THE LANDING GEAR EXTENSION CONTACT. SUBMITTER SUGGESTED IMMEDIATE INSPECTION AND REPETITIVE INSPECTIONS AFTER 50 LANDINGS OR 50 HOURS WHICHEVER OCCURS FIRST. STC 268GL.