External - Avionics/Flight instruments - AFCS -

Question 1

The 115V AC external power receptacle is located?

Answer 1

Forward right nose area

Question 2

Where is the main battery located?

Answer 2

Nose compartment

Question 3

Where is the APU battery located?

Answer 3

Aft equipment bay

Question 4

Where is the crew oxygen bottle located?

Answer 4

Forward of the passenger door

Question 5

What is indicated if the green oxygen blowout disc is blown?

Answer 5

excessive pressure has occurred

Question 6

Will the flight deck P.A. override the flight attendant P.A.?

Answer 6

Yes

Question 7

How should we contact the flight attendant in an emergency?

Answer 7

Turn the audio panel selector knob to PA

Push the EMER call switchlight to generate:

three high/low chimes and

a flashing red light on the FA’s overhead panel.

Question 8

What indication do we get if the flight attendant is calling the flight deck because of an emergency in the cabin?

Answer 8

We hear one high/low chime and

the EMER call switchlight will be flashing

Question 9

How do we know if the company is trying to contact us?

Answer 9

An ACARS message or

“SELCAL, SELCAL” voice aural and a SELCAL advisory EICAS message

Question 10

How many Air Data Computers (ADC) are installed?

Answer 10

Two

Question 11

How many AHRS or IRS computers are installed?

Answer 11

Two

Question 12

In MAG mode, how long does it take the AHRS system to initialize?

Answer 12

30 to 70 seconds

Question 13

In DG mode, how long does it take the AHRS system to initialize?

Answer 13

10 to 11 minutes

Question 14

From which source do the captain’s flight instruments receive AHRS information?

Answer 14

AHRS 1 or IRS 1

Question 15

From which source do the first officer’s flight instruments receive AHRS information?

Answer 15

AHRS 2 or IRS 2

Question 16

From which source do the captain’s flight instruments receive pitot/static information?

Answer 16

System #1 pitot/static tube on left side of nose

Question 17

From which source do the FO’s flight instruments receive pitot/static information?

Answer 17

System #2 pitot/static tube on right side of nose

Question 18

From which source does the integrated standby instrument receive pitot/static information?

Answer 18

System #3 standby pitot under captain’s side window and two alternate static ports, one on left and one on the right side

Question 19

Where is the TAT probe located?

Answer 19

Under FO’s side window

Question 20

What is the definition of Total Air Temperature?

Answer 20

The temperature of the air corrected for compressibility and friction caused by high speed

Question 21

On the ground with the probe heat ON, which probes are heated?

Answer 21

All pitot probes are heated half way, all others are fully heated except the TAT probe which is not heated on the ground.

Question 22

In flight, which probes are heated?

Answer 22

All are fully heated regardless of probe heat switch position.

Question 23

Is there a LOC and GS indication on the standby attitude indicator?

Answer 23

Yes, referencing NAV 1

Question 24

When and where will the radio altitude information appear?

Answer 24

0 to 2500’ AGL Indicated in green below the altitude tape

Question 25

What does the speed trend vector indicate?

Answer 25

Predicted airspeed in 10 seconds if no changes are made

Question 26

When and where will the MACH readout appear?

Answer 26

Appears when accelerating through 0.45 Mach. Disappears when decelerating through 0.4 Mach. Appears just above the airspeed tape in white

Question 27

What does the green line on the airspeed tape indicate?

Answer 27

1.27 Vs based on current configuration. Not accurate at high altitudes

Question 28

Where is the slip and skid indicator located?

Answer 28

A rectangle located just under the sky pointer

Question 29

How many flight directors are installed?

Answer 29

two

Question 30

How many autopilots are installed?

Answer 30

one

Question 31

What does the autopilot follow when engaged?

Answer 31

The selected side flight director which defaults to the captain’s FD. The XFER button must be selected on the flight control panel to transfer to the FO’s FD

Question 32

What happens when TOGA is pushed on the ground?

Answer 32

Autopilot disengages TO lateral and vertical mode FMS aligns the aircraft at the end of the runway indicated on legs page

Question 33

What does the TO lateral mode do?

Answer 33

On the ground, it generates a wings level command. In the air it generates a heading hold command with a 5° bank limit using the heading existing at takeoff

Question 34

What does TO vertical mode do?

Answer 34

Generates an optimized pitch up attitude for takeoff

Question 35

What happens when TOGA is pushed in flight?

Answer 35

Autopilot disengages GA lateral and vertical mode Missed approach procedure depiction appears on the MFD if instrument approach procedure selected in FMS

Question 36

What does GA lateral mode do?

Answer 36

Same as TO lateral mode and follows heading flown when TOGA was pushed

Question 37

What does GA vertical mode do?

Answer 37

Generates a 10° pitch up attitude

Question 38

After takeoff or go-around, the autopilot must not be engaged below what altitude?

Answer 38

600 ft AGL

Question 39

During visual and non-precision approaches, the autopilot must be disengaged by?

Answer 39

400 ft AGL

Question 40

During precision approaches, the autopilot must be disengaged by?

Answer 40

80 ft AGL

Question 41

During single-engine precision approaches, the Autopilot must be disengaged by?

Answer 41

80 ft AGL (700), 110 ft AGL (900)

Question 42

When will autopilot automatically disconnect?

Answer 42

1. AP/SP DISC button pushed, 2. AP ENG button on FCP pushed, 3. AP DISC switch bar pushed down, 4. stick shaker activated, 5. TOGA buttons pressed, 6. STAB TRIM manually operated, 7. windshear warning (after 2 seconds), 8. excessive attitude, 9. one or both FCCs fail, both yaw dampers disc or fail.