Ice & Rain Protection

Question 1

1. Anti-ice systems should be turned on in flight when operating in visible moisture with a MFD displayed RAT of:

Answer 1

D. +10°C (50°F) or below

Question 2

The P/S HTR OFF annunciator:

Answer 2

A. Illuminates with the system selected when current fails to any main system pitot or static heating element

Question 3

3. At night, ice formation can be detected by:

Answer 3

B. Red windshield ice detection lights

Question 4

4. Regarding the windshield anti-ice system:

Answer 4

C. An overheat light, with the system ON, indicates excessive bleed-air temperature.

Question 5

5. Select the one correct statement concerning the W/S AIR O’HEAT annunciator:

Answer 5

A. If the annunciator illuminates when the system is operating, the solenoid valve should close, shutting off windshield air.

Question 6

6. Failure of the main DC electrical system results in:

Answer 6

B. Continuous flow of hot bleed air, with windshield temperature control possible only through regulation of the volume of bleed air permitted to the windshield

Question 7

7. The WIS AIR O’HEAT annunciator illuminates:

Answer 7

A. If 5-psi pressure is sensed in the duct with the WINDSHIELD BLEED AIR switch OFF

Question 8

8. When using rain removal:

Answer 8

D. The augmenter doors should be opened prior to applying bleed air on the windshield

Question 9

9. The windshield alcohol system:

Answer 9

D. Both A and C are correct

A. Is a backup system for the windshield anti-ice system

C. Utilizes a pump that supplies alcohol to the pilot windshield only for a maximum of 10 minutes

Question 10

10. Once necessary conditions are satisfied to extinguish the ENG ANTI-ICE annunciators, a minimum power setting to sustain the operation in flight is:

Answer 10

B. Anti-ice idle 70% N2 rpm, landing gear up

Question 11

11. The time for the ENG ANTI-ICE annunciators to extinguish after initiating operation in flight varies with outside air temperature at cruise or climb thrust settings. Normally, no more than:

Answer 11

B. 2 minutes

Question 12

12. The L or R ENG ANTI-ICE light illuminates if the engine inlet temperature of the engine drops below:

Answer 12

B. 10°C (50°F)

Question 13

13. In flight, cockpit indications that the engine anti-ice system is operating is:

Answer 13

C. ITT rise, Ny and N2 decrease, and the ENG ANTI-ICE switchlights) extinguish after a few minutes

Question 14

14. If the MASTER CAUTION RESET switch-light and the WING ANTI-ICE switchlights illuminate:

Answer 14

A. Bleed-air temperature at the wingtip is too cold

Question 15

15. When using the TAIL DEICE boots:

Answer 15

D. MANUAL MODE serves as a backup if AUTO mode fails