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Edition – Rev 0
24-10
GENERAL
24-00 GENERAL
Primary DC power is provided by an engine-driven generator ( 20-Amps or 40-Amps) which,
during normal operations, recharges the battery.
“The generators do not operate in parallel since if the 20-Amps one is enable, the external
one will not be installed. If the 40-Amps generator is installed the 20-Amps one will be
disabled”.
Secondary DC power is provided by a battery (GILL G25) which provides the energy
necessary for feeding the essential electrical loads in the event of a generator failure. For
ground maintenance and/or starting, an external power socket is provided.
12V electrical power socket IS installed on the instrument panel.
Electrical power is distributed through:
battery bus;
avionics bus (optional).
Electrical wiring diagrams are addressed on Chapter 92.
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