AC Tech quiz 2

Question 1

Heat for which windows, are controlled by the Window Heat switches?
A. Only the Captain’s and First Officer’s windshields.
B. The Captain’s and First Officer’s windshields and the Captain’s side window.
C. All flight deck windows.

Answer 1

C. All flight deck windows.

Question 2

Selecting the Camera Light switch ON illuminates the main and nose landing gear if:
A. The nose gear is down a locked.
B. The BEACON Light switch is ON.
C. Both A and B

Answer 2

C. Both A and B

Question 3

With the ND in MAP mode, what additional information is displayed when the WPT switch is pushed?
A. Locations of all navaids in the database within the selected range.
B. Frequencies of all radio aids within 40 nm.
C. Location of all waypoints in the database (at or below 40 nm range).

Answer 3

C. Location of all waypoints in the database (at or below 40 nm range).

Question 4

Following an alternate extension, the landing gear can be retracted if the centre system is operating
A. True.
B. False.

Answer 4

A. True.

Question 5

The NORMAL minimum width of pavement for a 180 degree turn for the - 300ER is:
A. 129.4 feet (39.4m).
B. 148.8 feet (45.2m).
C. 185.5 feet (56.5m).

Answer 5

C. 185.5 feet (56.5m).

Question 6

Two Outflow valves are installed. Cabin altitude and full ventilation rates can be maintained by either valve.
A. True.
B. False.

Answer 6

A. True.

Question 7

If the cabin altitude exceeds 11,000 ft. both outflow valves close.
A. True
B. False

Answer 7

B. False

2.30.1 15,000’

Question 8

The LOC mode can be disengaged after LOC capture by:
A. Selecting TO/GA
B. Selecting LNAV
C. Selecting FLCH

Answer 8

?

Question 9

On the ground with both engines shut down, any VHF radio that transmits for more than 35 seconds is automatically disabled.
A. True.
B. False.

Answer 9

A. True.

transmit more than 30 secs: Eicas RADIO TRANSMIT

5.20.3

Question 10

When will the ELEC CABIN / UTIL OFF light illuminate?
A. When a Utility or Galley Bus is load shed.
B. When the CABIN/UTILITY Power Sw is selected OFF.
C. Both A and B

Answer 10

B. When the CABIN/UTILITY Power Sw is selected OFF.

6.10.3

Question 11

The Ground Service Bus is normally powered by:
A. The APU Generator.
B. The primary external power.
C. The Right Main Bus.

Answer 11

C. The Right Main Bus.

6.20.5

Question 12

On the ground with both engines OFF and APU fire signal from either fire detector loop causes:
A. The APU to shut down and extinguisher to discharge.
B. The APU fire warning to illuminate, the extinguisher must be manually discharged.
C. The APU fire warning to illuminate and auto shut down of the APU.

Answer 12

A. The APU to shut down and extinguisher to discharge.

8.20.3

Question 13

If smoke is detected in a lavatory, an aural alert sounds in the cabin and the lavatory. The flight deck EICAS indication is SMOKE LAVATORY.
A. True.
B. False.

Answer 13

A. True.

8.20.6

Question 14

What function(s) does the yaw damper system provide in the normal mode?
A. Rudder load relief and turn co-ordination.
B. Turn co-ordination and dutch roll damping.
C. Improved directional stability.

Answer 14

B. Turn co-ordination and dutch roll damping.

9.20.16

Question 15

What is the maximum flap extension available using the alternate flaps system?
A. 20 B. 25 C. 30

Answer 15

A. 20

9.20.20

Question 16

Which is correct when the EICAS message HYD PRSS DEM is displayed with the Demand Pump Selector in AUTO?
A. Pump operating with full hydraulic pressure.
B. Pump commanded to operate, pump output is low.
C. Pump operating but heavy hydraulic loads are operating.

Answer 16

B. Pump commanded to operate, pump output is low.

13.30.1

Question 17

What cost index provides maximum range?
A. 0
B. 1000
C. 9999

Answer 17

A. 0

11.31.4

Question 18

The IAS/MACH window during climb automatically changes from IAS to Mach at:
A. M.82.
B. When the IAS/MACH Sw is pushed or at M.84.
C. Does not change unless VNAV is engaged.

Answer 18

B. When the IAS/MACH Sw is pushed or at M.84.

4.10.6

Question 19

When do the Pitot probes receive anti-icing protection?
A. When either engine is operating.
B. When the airplane is airborne.
C. When Engine anti-ice is selected to ON

Answer 19

A. When either engine is operating.

3.20.4

Question 20

LNAV engages when selected if above:
A. 50 feet and 1.5 miles of the active leg.
B. 100 feet and 2.5 miles of the active leg.
C. 50 feet and 2.5 miles of the active leg.

Answer 20

C. 50 feet and 2.5 miles of the active leg.

4.10.7

Question 21

What is operated by L HYD SYS?

Answer 21

L THR REV

SOME FLT CTRLS

Question 22

What is operated by R HYD SYS?

Answer 22

L THR REV
SOME FLT CTRLS
AUTO BRAKE SYS
NORMAL BRAKES

Question 23

What is operated by C HYD SYS?

Answer 23

ALT BRAKES
AUTO SPEED BRAKES
FLAPS
GEAR
N/W & MAIN GEAR STEERING
SOME FLT CTRLS