ED Decision 2023/001/R
(a) For each engine, means must be provided in the cockpit so as to:
(1) control, either directly by the crew or by the crew via a system (such as the FADEC), each ignition circuit;
(2) readily allow the crew to conduct the flight and manage both ground start and in-flight restart;
(3) check the health condition of each ignition circuit; and
(4) maintain an isolation between each engine control.
(b) There must be means to quickly shut off all ignition by the grouping of switches or by a master ignition control.
(c) Each group of ignition switches, except ignition switches for turbine engines for which continuous ignition is not required, and each master ignition control, must have a means to prevent its inadvertent operation.
[Amdt No: 29/11]
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