Avionics and Flight Instruments Flashcards

1
Q

How many Air Data Computers (ADC) are installed

A

Two

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2
Q

How many AHRS or IRS computers are installed

A

Two

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3
Q

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

A

30 to 70 seconds

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4
Q

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

A

10 to 11 minutes

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5
Q

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

A

AHRS 1 or IRS 1

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6
Q

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

A

AHRS 2 or IRS 2

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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)

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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)

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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)

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10
Q

Where is the TAT probe located

A

Under FO’s (Right) side window

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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

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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

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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

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14
Q

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

A

Yes, The ISI references NAV 1 only.

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15
Q

When and where will the radio altitude information appear

A

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

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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
When will the green radio altitude tape be displayed?
0 ft to 1,000 ft AGL
26
When and where will the MACH readout appear
Appears when accelerating through 0.45 Mach. Disappears when decelerating through 0.4 Mach. Appears just above the airspeed tape in white