Section 10. Electrical Eclipse 5OO Systems Manual
Copyright © — Eclipse Aviation Corporation
Version 2.0 April 2007 235
Figure 144. Electrical Synoptic With One Engine Running
TWO ENGINES RUNNING/ IN-FLIGHT
With both engines running and during normal flight operation with power output from
both generators, the left and right electrical systems are split (bus tie contactor is
open). The left system is powered by the left generator, and is connected to and
charges the systems battery. The right system is powered by the right generator and
is connected to and charges the start battery.
AIR-GROUND LOGIC
The ACS uses the current status of the aircraft (on-ground or in-flight, as determined
through the Weight-On-Wheels sensor) to determine the appropriate control functions
for normal operation and failure conditions.
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