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