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19 Cards in this Set
- Front
- Back
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All flight deck windows are electrically heated. The forward windows have anti-ice and anti-fog protection. Side windows have ____.
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anti-fog protection only
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Probe heat is provided ____.
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anytime an engine is running
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The engine anti-ice system uses engine bleed air to provide ice protection to the ____.
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engine cowl
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On some B767-300 ER airplanes, electrical power for the aft most cockpit window heat is load shed when ____.
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the Fuel Jettison switch is selected ON
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The B757 wing anti-ice system provides bleed air to ____ leading edge slats on each wing.
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3 mid wing
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On B767-300ER aircraft, prior to reducing thrust for descent in visible moisture and TAT less than _____, including SAT less than _____, engine anti-ice switch must be in the ON position. At or below _______feet, wing anti-ice selector must be in the ON position.
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10 degrees C, -40 degrees C, 22,000
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Engine anti-ice should be operated ____.
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during all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise when temp is below -40 degrees C SAT
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The CAPT PITOT light indicates _
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That probe is not being heated in flight or neither engine is running on the ground
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A probe heat light on the overhead panel indicates that ____.
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a probe is not being heated
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The Engine Anti-Ice Switch VALVE light illuminates if ____.
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the respective valve position disagrees with the switch position
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The Side Window Heat Switch INOP lights illuminate while ____.
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the window is not being heated
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The (green) TAI annunciator below the EICAS N1 gage indicates that the ____.
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Engine anti-ice valve is open
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Wing anti-ice may be turned on during climb in icing conditions ____.
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above 1000 feet AFL
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On the 767-300ER, engine anti-ice should be turned on when TAT is below ____ degrees C and _____ is present.
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10, visible moisture
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Operation of the Probe Heat System is fully automatic. Power to the electrically heated probes is applied ____.
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anytime an engine is running
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Engine anti-ice should be used if TAT is below 10 degrees C ____.
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when operating on ramps, taxiways, or runwways where surface snow, ice, standing water, or slush may be ingested by the engines
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On the B767-300ER, when engine anti-ice is turned on, the __________ is anti-iced.
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engine cowl inlet
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If the left or right AOA vane heat failed, which light and EICAS message indications will appear?
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L/R AOA light, PROBE HEAT, L/R message
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Icing conditions exist when OAT/TAT is ____°C or below and visible moisture in any form is present.
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10
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