121-140

Question 1

If the PAX Cabin knob is set to ATTND, the flight attendant has control of the cabin temperature.

Answer 1

True

Question 2

On a flight from DFW to SFO, you are filed for FL380 however while enroute ATC advises you that FL360 will be your final cruise altitude. What considerations do you have in regards to the pressurization system?

Answer 2

Change the cruise attitude in the MCDU to FL360 in order to lengthen the life of the airframe

Question 3

The buttons on the AIR COND/PNEUMATIC control panel are in the AUTO position pressed in and dark (no white stripe bar).

Answer 3

True

Question 4

What protects the airplane’s structure from damage due to over or under pressurization?

Answer 4

Safety valve and Negative pressure relief valve

Question 5

While cruising at FL390, you receive a master caution light accompanied by a “PACK 1 FAIL” EICAS message. You were unable to restore the pack using the QRH procedure. What is the maximum altitude at which you may cruise?

Answer 5

FL310

Question 6

The APU can supply bleed air for engine and wing anti-ice.

Answer 6

False

Question 7

In AUTO mode, when the cabin DUMP button is depressed, this will command the following to occur:

Answer 7

Both answers A and B are correct:
The recirculation fans are turned off, the packs are turned off and the outflow valve opens to maintain 2,000 feet per minute climb to 12,400’

Question 8

Choose the on-board sources of bleed air:

Answer 8

APU, Engine 1 and Engine 2

Question 9

PACKS are automatically turned off during engine start (the button is in the AUTO position).

Answer 9

True

Question 10

If the Pressurization Mode button is in AUTO, the LFE is automatically set based on the flight plan destination.

Answer 10

True

Question 11

Shortly after takeoff you observe an “AI WING VLV OPEN” status message in VMC conditions. What is the most likely cause of this message?

Answer 11

This is a normal test that will occur 10 minutes after takeoff or at 10,000 feet AGL, whichever occurs first

Question 12

After landing in DEN during a light snow shower, what action by the crew is required to turn the Anti-lce system ON while taxiing in to the gate on contaminated surfaces?

Answer 12

The Ice Protection switch should be moved to ON

Question 13

When the buttons on the ice protection panel are pushed in (dark), operation is automatic.

Answer 13

True

Question 14

The maximum windshield wiper speed is?

Answer 14

250 KIAS

Question 15

Which of the following considerations should be given during an approach when the EICAS message “STALL PROT ICE SPEED” is displayed?

Answer 15

Pilot must use the “With Ice Accretion” chart when determining their V speeds for landing if ACARS is not available

Question 16

If both ice detectors fail in flight, you will lose ice protection.

Answer 16

False

Question 17

The ATIS reports an OAT of 7° C and overcast skies at 1500 feet. How should the pilot configure the aircraft’s ice protection system for takeoff?

Answer 17

TO DATASET MENU on the MCDU must be set to ENG

Question 18

The tail (vertical and horizontal stabilizer) of the aircraft is provided with anti-icing.

Answer 18

False

Question 19

When the Ice Protection Mode knob is set to AUTO, the ice protection will turn on in flight if the ice detector detects ice.

Answer 19

True

Question 20

During taxi out the windshield is automatically heated under which of the following conditions?

Answer 20

Two engine taxi