(a) Each instrument must have an integral visual power annunciator or separate power indicator to indicate when power is not adequate to sustain proper instrument performance. If a separate indicator is used, it must be located so that the pilot using the instruments can monitor the indicator with minimum head and eye movement. The power must be sensed at or near the point where it enters the instrument. For electric and vacuum/pressure instruments, the power is considered to be adequate when the voltage or the vacuum/pressure, respectively, is within approved limits.
(b) The installation and power supply systems must be designed so that—
(1) The failure of one instrument will not interfere with the proper supply of energy to the remaining instrument; and
(2) The failure of the energy supply from one source will not interfere with the proper supply of energy from any other source.
(c) There must be at least two independent sources of power (not driven by the same engine on multiengine airplanes), and a manual or an automatic means to select each power source.
[Doc. No. 26344, 58 FR 18976, Apr. 9, 1993]
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