As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING A PHASE I AND II INSPECTION A CRACK WAS FOUND IN THIS PART ATTACHED TO THE RT GEAR ASSY. THE CRACK IS ON THE TORQUE PLATE UPPER FORWARD BRAKE CYLINDER PIN ATTACH HOLE. A BUSHING INSTALLED IN THIS HOLE HAS NO SIGN OF DAMAGE. PROBABLE CAUSE OF CRACKING WOULD BE STRESS RELATED. (K)