As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING COMPLIANCE WITH CESSNA SB11-32-01 ON THE RIGHT MAIN GEAR LEG A 3 INCH CRACK WAS FOUND EXTENDING UP THE GEAR LEG. THE CRACK ORIGINATED OUT OF THE UPPER AXLE MOUNTING HOLE. THIS CRACK WAS COMPLETELY HIDDEN UNDER THE AXLE AS IT SLIDES OVER AND COMPLETELY SURROUNDS THE GEAR LEG. THERE IS NO INSPECTION FOR SUCH A CRACK NOR WOULD ONE BE FOUND UNLESS THIS LOWER AXLE IS REMOVED FROM THE MAIN LANDING GEAR LEG. THIS CRACK IS COMPLETELY THROUGH THE TUBING WALL THICKNESS.