As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
INSPECTION TYPE: C, FWD ROTARY ACTUATOR SUPPORT FITTING FOUND CRACK AT HOLE NR 8 (LOOKING FWD) APPROX 0.030 INCH LONG AS MARKED. CRACKED HOLE OVERSIZED TO 0.688 INCH AND CRACK / CORROSION FREE. BUSHING FABRICATED AND INSTALLED AS PER RS R53-65-34855 WITH ENGINEERING FILE NUMBER : 747-53-20096.