Section 7. Fuel
7. Fuel
7.1 General
The fuel system is a supply pressurized wet-wing design. Normally each engine
receives fuel from the corresponding wing tank, but fuel from either wing can supply
both engines through a crossfeed valve. Fuel Management and balancing is
automatically controlled by the ACS, but can be overridden by the pilot.
114
Copyright © — Eclipse Aviation Corporation
Eclipse 5OO Systems Manual
Version 2.0 April 2007