Avionics and Flight Instruments Flashcards

1
Q

How many Air Data Computers (ADC) are installed

A

Two

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

How many AHRS or IRS computers are installed

A

Two

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

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

A

30 to 70 seconds

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

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

A

10 to 11 minutes

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

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

A

AHRS 1 or IRS 1

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

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

A

AHRS 2 or IRS 2

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

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

A

System #1, pitot/static tube on left side of nose
(P1-S1)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

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

A

System #2, pitot/static tube on right side of nose
(P2-S2)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

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

A

System #3, standby pitot under captain’s side window and two alternate static ports, one on left and one on the right side Pitot Probe 3 (P3)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Where is the TAT probe located

A

Under FO’s (Right) side window

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

What is the definition of Total Air Temperature

A

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

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

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

A

All pitot probes are heated half way (50%) while pitot bases are not heated, angle of attack vanes and system 3 static ports are fully heated.

Note: The TAT probe and pitot bases which are not heated on the ground

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

In flight, which probes are heated regardless of probe heat switch position?

A

All are fully heated regardless of probe heat switch position

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

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

A

Yes, The ISI references NAV 1 only.

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

When and where will the radio altitude information appear

A

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

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

What does the speed trend vector indicate

A

Predicts airspeed in 10 seconds

17
Q

When and where will the MACH readout appear

A

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

18
Q

What does the green line on the airspeed tape indicate

A

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

19
Q

Where is the slip and skid indicator located

A

A rectangle located just under the sky pointer

20
Q

When will the yellow hashed rising runway indication be displayed on the radio altitude tape?

A

0ft to 200ft AGL

21
Q

What sends information to the Captain’s flight instruments?

A

Air Data Computer 1 (ADC1)

22
Q

What sends information to the First Officers flight instruments?

A

Air Data Computer 2 (ADC2)

23
Q

What sends pitot-static information to Air Data Computer 1?

A

Pitot-static probe 1 (P1-S1) on left side of nose

24
Q

What sends pitot-static information to Air Data Computer 2?

A

Pitot-static probe 2 (P2-S2) on right side of nose

25
Q

When will the green radio altitude tape be displayed?

A

0 ft to 1,000 ft AGL

26
Q

When and where will the MACH readout appear

A

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