As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
DURING AN INSPECTION, BOTH WHEEL BRAKE ASSEMBLIES WERE FOUND CRACKED AT THE ANCHOR BOLT BOSSES. THE CAUSE OF THE CRACK IS THE ANCHOR BOLT (PN 69-4) GETS RUSTY/DIRTY AND WOULD NOT SLIDE FREELY IN THE TORQUE PLATE (PN 75-37). SUBMITTER SUGGESTS DURING INSPECTION, BE SURE THE ANCHOR BOLTS AND HOLES IN THE TORQUE PLATE ARE CLEANED OF ALL RUST AND DIRT.