Anchor bolts (2) Pressure plate lining Backplate lining Bushings Torque plate Rivets (8) Pressure plate Cylinder assembly Cylinder housing to back plate bolts(4 each) Backplate Figure 13-123.  A Cleveland brake disassembles once the four bolts holding the cylinder to the backplate are removed while the aircraft  wheel remains in place. The pressure plate slides off the anchor bolts and linings can be replaced by riveting on the pressure plate and  back plate. Figure 13-124.  Rivet setting tool is used to install brake linings on  Cleveland brake pressure plates and back plates.  Aircraft brakes operate under extreme stress and varied  conditions. They are susceptible to malfunction and damage.  A few common brake problems are discussed in this section. While aircraft brakes slow the aircraft by changing kinetic  energy into heat energy, overheating of the brakes is not  desirable. Excessive heat can damage and distort brake  parts weakening them to the point of failure. Protocol for  brake usage is designed to prevent overheating. When a  brake shows signs of overheating, it must be removed from  the aircraft and inspected for damage. When an aircraft is  involved in an aborted takeoff, the brakes must be removed  and inspected to ensure they withstood this high level of use. The typical post-overheat brake inspection involves removal  of the brake from the aircraft and disassembly of the brakes.  All of the seals must be replaced. The brake housing must  be checked for cracks, warping, and hardness per the  maintenance manual. Any weakness or loss of heat treatment  could cause the brake to fail under high-pressure braking. The  brake discs must also be inspected. They must not be warped,  and the surface treatment must not be damaged or transferred  to an adjacent disc. Once reassembled, the brake should be  bench tested for leaks and pressure tested for operation before  being installed on the aircraft. 13-74 Overheating  Brake Malfunctions and Damage 