Anti-Ice Flashcards
WING ANTI-ICE VALVE OPEN lights (L and R)
extinguished
- switch is OFF and corresponding wing anti-ice control valve is closed
- normal ops
- illuminated (dim)
- switch is ON and corresponding wing anti-ice control valve is open
- normal ops with WAI operating
- illuminated (bright)
- corresponding wing anti-ice control valve is in transit, or
- the position of the valve is contrary to the position of the wing anti-ice switch (disagreement lights)
ENG ANTI-ICE switches
OFF
- engine anti-ice valve closes and the COWL VALVE OPEN light goes out
ON
- opens corresponding engine anti-ice valve (illuminates the cowl valve open light), signals EEC for high idle, and signals the FMC to bias fuel schedules for bleed loads.
- adjusts stick shaker and minimum maneuver speed bars on airspeed indicators
- FMC displayed VREF is not automatically adjusted.
- stick shaker and minimum maneuver speed indications return to normal when engine anti-ice is positioned off if wing anti-ice has not been used in flight
- approach idle is selected in flight if flaps are in landing configuration or engine anti ice is ON for either engine
- 72-79% N2
COWL VALVE OPEN lights (blue)
- illuminated (bright) = corresponding control valve is in transit, or if not in transit, the position of the valve is contrary to the position of the associated Engine Anti-Ice switch (disagreement lights)
- illuminated (dim) = corresponding control valve is open (switch on)
- extinguished = corresponding control valve is closed (switch off)
COWL ANTI-ICE light
Amber
- illuminated indicates an overpressure
WING ANTI-ICE switch
OFF
- wing anti-ice control valves are closed
- VALVE OPEN lights are extinguished
ON (on the ground)
- VALVE OPEN lights illuminate bright then dim
- look for slight decrease in both duct pressure gauges
- 2nd segment climb consideration - turn on after 1000’ AGL
- adjusts stick shaker and minimum maneuver speed bars on airspeed indicators
- FMC displayed Vref is not automatically adjusted
Note: stick shaker and minimum maneuver speed bars on airspeed indicators remain set for icing conditions for the remainder of the flight, regardless of subsequent wing anti-ice switch position
CAUTION: use above approximately FL350 may cause a dual bleed trip