Found this. https://www.highskyf...on_Requirements
Aircraft Brakes Certification Requirements
Many certification requirements govern the approval, replacement, and modification of aircraft brakes. In general, it is required that the braking system of an aircraft must have the ability to stop the aircraft at maximum certified takeoff weight with the rejected takeoff initiated at decision speed.
The certification process must be done with all brakes worn to near their service limit (nominally 10% left on the lifespan). Also, the brake and wheel heat sink must be robust enough that no intervention in terms of fire fighting or artificial cooling is required for 5 minutes after the aircraft has been stopped.
Other certification requirements demand that the components of the wheels, brakes, and braking systems should be designed to:
- Withstand all pressures and loads, applied separately and in conjunction, to which they may be subjected in all operating conditions for which the airplane is certificated.
- Accommodate simultaneous applications of normal and emergency braking functions, except other appropriate design measures have been taken to prevent such a contingency.
- Satisfy all the requirements pertaining to energy absorption requirements without making use of secondary cooling devices (e.g. cooling fans, etc).