Eclipse 500 System Manual page 232

Section 9. Climate Control
9.7 Abnormal Procedures
9.8 Cold Weather Operations
(Temperature Sensor Indications)
In the event that the aircraft cabin has become cold soaked to -13°F or less the pilot
may initially see ACS indications of failed temperature sensors. These indications
should be considered false due to the extreme cold. The temperature regulation
control will also default to a special mode of operation for cold temperatures. Once
the engines are started and warm bleed air warms the system, the ACS will stop
displaying senor failures and temperature regulation will resume to normal.
9.8.1 Single Engine Operations
In the event of an engine shutdown or failure, bleed air from the operating engine is
routed to the cockpit. This automatic function can be overridden by the pilot with the
AIR DISTR line select key on the pressurization synoptic.
212
Copyright © — Eclipse Aviation Corporation
Eclipse 5OO Systems Manual
Version 2.0 April 2007