Anti-Ice, Rain (FM: 6.30)

Question 1

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

a) Activates the FLT ignition system
b) Automatically energizes continuous ignition and activates approach idle for the associated engine
c) Automatically activates flight idle
d) Activates flight idle only when the flaps are out of UP

Answer 1

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

Question 2

757/767: According to the graphic, the wing anti-ice switch is in the ON position and the right-wing anti-ice VALVE light is illuminated. The right-wing anti-ice system is:

a) Not operational, as the valve position disagrees with the switch position
b) Fully operational, as this is just a pilot awareness light
c) Fully operational, as long as engine anti-ice is selected ON
d) Not operational when an overheat is sensed in flight

Answer 2

A) Not operational, as the valve position disagrees with the switch position

Question 3

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

a) If an overpressure condition is sensed in flight
b) When a wing overheat condition is sensed in flight
c) Upon touchdown
d) The wing anti-ice valve remains open during all phases of flight until the engines are shut down

Answer 3

C) Upon touchdown

Question 4

4) 757/767: Power to the electrically heated pitot probe(s) is applied:
a) After the first engine is started
b) Only when the airplane is airborne
c) When electrical power is established
d) Only after both engines have been started

Answer 4

A) After the first engine is started

Question 5

5) 757/767: According to the graphic, the R AOA light is illuminated. The R AOA is:
a) Not operational, but only during flight
b) Not operational as the probe heater has failed
c) Operational, but an air leak in the system has been detected
d) Operational, but a probe overheat has been detected

Answer 5

B) Not operational as the probe heater has failed

Question 6

6) 764: According to the graphic, the ICE DET light is illuminated, what does it indicate?
a) System anti-icing is no longer available
b) The ice detector system has failed
c) Icing conditions have been detected and an anti-ice valve is not open
d) Auto operation is still available but manual anti-ice/de-ice can no longer be selected

Answer 6

B) The ice detector system has failed

Question 7

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?
a) Auto operation is still available but manual anti-ice/de-ice can no longer be selected
b) System anti-icing is no longer available
c) The ice detector system has failed
d) An anti-ice valve is closed and engine/wing icing is detected

Answer 7

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