(a) The system must meet the requirements specified in §23.1419.
(b) The system and its components must be designed to perform their intended function under any normal system operating temperature or pressure, and
(c) Means to indicate to the flight crew that the pneumatic de-icer boot system is receiving adequate pressure and is functioning normally must be provided.
[Amdt. 23–23, 43 FR 50593, Oct. 30, 1978]