787 Flight Crew Operations Manual
DO NOT USE FOR FLIGHT
Anti-Ice, Rain Chapter 3
Controls and Indicators Section 10
Copyright © The Boeing Company. See title page for details.
D615Z003-TBC 3.10.1
3.10 Anti-Ice, Rain-Controls and Indicators
Anti-Ice, Rain10 Controls and In dicatorsControls and Indicators
Anti-Ice Panel and Indications
Anti-Ice Panel
OFF – wing ice protection system is not powered.
Note: To enter the OFF position, switch must be pulled during rotation from
AUTO to OFF.
AUTO – in flight, wing ice protection system is powered on and off automatically
by the ice protection system.
ON – in flight, wing ice protection system is powered on and operates without
input from automatic ice detection system (with TAT less than 10º C).
OFF – the engine anti–ice valve is commanded closed.
AUTO – in flight, the engine anti–ice valve is opened or closed automatically by
the ice detection system.
ON – the engine anti-ice valve is commanded open.
Note: Approach idle is selected by the EEC if:
• ENGINE ANTI-ICE selector is in AUTO and the anti-ice valve is
commanded open, or
• ENGINE ANTI-ICE selector is ON
1
WING ANTI–ICE Selector
2
ENGINE ANTI–ICE Selectors
ANTI-ICE
OFF ON
AUTO
ENGINELRWING
OFF ON
AUTO
OFF ON
AUTO
OVERHEAD PANEL
1
2
August 14, 2009
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