ED Decision 2003/15/RM
(a) There must be a separate power control for each engine.
(b) Power controls must be grouped and arranged to allow:
(1) Separate control of each engine; and
(2) Simultaneous control of all engines.
(c) Each power control must provide a positive and immediately responsive means of controlling its engine.
(d) If a power control incorporates a fuel shut-off feature, the control must have a means to prevent the inadvertent movement of the control into the shut-off position. The means must:
(1) Have a positive lock or stop at the idle position; and
(2) Require a separate and distinct operation to place the control in the shut-off position.
(e) For rotorcraft to be certificated for a 30-second OEI power rating, a means must be provided to automatically activate and control the 30-second OEI power and prevent any engine from exceeding the installed engine limits associated with the 30-second OEI power rating approved for the rotorcraft.
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