Anti Ice/rain

Question 1

764: The anti-ice (WAI) annunciation appears above the EICAS EGT indication when:

Answer 1

When a wing anti-ice valve is open

Question 2

757/767: The ___ can be operated in flight only. It is inhibited on the ground.

Answer 2

Wing anti-ice

Question 3

767: The wing anti-ice system provides bleed air to:

Answer 3

The three outboard leading edge slats on each wing

Question 4

767: The wing anti-ice system provides bleed air to:

Answer 4

The three outboard leading edge slats on each wing

Question 5

757/763: Operation of the ___ system is fully automatic

Answer 5

Probe heat

Question 6

757/767: According to the graphic, the R AOA light is illuminated. This indicates:

Answer 6

Angle of attack vane heater failure or neither engine running on ground

Question 7

757/767: The thermal anti-ice (TAI) annunciation appears above the EICAS N1 indication when:

Answer 7

When an engine anti-ice valve is open

Question 8

764: According to the graphic, the ICE DET light is illuminated, what does it indicate?

Answer 8

The ice detector system has failed

Question 9

757/767: Power to the electrically heated pitot probes is applied:

Answer 9

Any time an engine is running

Question 10

757: The wing anti-ice system provides bleed air to:

Answer 10

Three leading edge slats immediately outboard of the engine on each wing

Question 11

757: The wing anti-ice system provides bleed air to:

Answer 11

Three leading edge slats immediately outboard of the engine on each wing

Question 12

757: Thermal anti-ice (TAI) pressure indicators are installed near the forward side of each engine directly aft of the intake. The TAI is normally flush, but extends outwards:

Answer 12

If a leak is detected in the inlet cowl ducting

Question 13

757/767: Maximum EPR/N1 limits are automatically reduced:

Answer 13

When the associated engine anti-ice switch is selected on

Question 14

757/767: The engine anti-ice valve is located upstream of the associated engine bleed air valve.
When the associated engine bleed air valve is closed, engine anti-ice is:

Answer 14

Available

Question 15

757/767 the ___ probe is not heated on the ground

Answer 15

TAT

Question 16

757/767: Maximum EPR/N1 limits are automatically reduced:

Answer 16

When the associated engine anti ice switch is on

Question 17

757/767: With the wing anti-ice switch ON, the wing anti-ice valves will automatically close:

Answer 17

Upon touchdown

Question 18

764: According to the graphic, the ICING light and engine anti-ice VALVE light are illuminated, The aircraft is airborne. What is the status of the anti-ice system?

Answer 18

An anti-ice valve is closed and engine/wing icing is detected

Question 19

757/767: In flight, provided the associated ENG START selector is positioned to AUTO, turning on the engine anti-ice switches:

Answer 19

Automatically energizes continuous ignition and activates approach idle for the associated engine

Question 20

757/767: According to the graphic, the total air temperature (TAT) probe(s) light is illuminated. This

Answer 20

Total air temperature probe(s) heater failure or neither engine running on ground