ICE AND RAIN/ANTI-ICE

Question 1

NAC Heat and Wing/Stab Heat use ( ) pressure bleed air.

Answer 1

High pressure bleed air. PTM Pg. 10-4

Question 2

Icing conditions can occur when the temperature is between ( + º) degrees C and ( - º) degrees C with visible moisture.

Answer 2

+10º degrees C and -40º degrees C with

visible moisture. PTM Pg. 10-1

Question 3

If ice is detected and the Wing/Stab heat and/or NAC heat is not turned ( “ ” ), an amber ICE DETECTED CAS message will be displayed.

Answer 3

On. PTM Pg. 10-2

Question 4

A red WING/STAB LEAK CAS message indicates a ( ) leak in the tail cone or in the ducting that runs through the aircraft to the leading edges of the wing or horizontal stabilizer.

Answer 4

Bleed air leak. PTM Pg. 10-11

Question 5

In the event of dual generator failure, pitot heat is only available to the ( ) Tube.

Answer 5

The Standby Pitot Tube. PTM Pg. 10-13

Question 6

The left and right windshields are heated electrically using ( ) power from the left and right engine driven alternators.

Answer 6

AC power from the left and right engine-

driven alternators. PTM Pg. 10-6

Question 7

When selecting the NAC heats or Wing/Stab heat “ON, thrust levers must be at ( ) or below.

Answer 7

MCT or below. QRH Pg. N-13