Avionics, Flight instruments Flashcards

0
Q

How should we contact the flight attendant in the emergency?

A

Turn the audio panel selector knob to PA, push the EMER call switch light to generate three high/low chimes and a flashing red light on the FA’s overhead panel

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1
Q

Will the flight deck PA override the flight attendant PA?

A

Yes

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2
Q

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

A

We hear one high/low chime and the EMER call switch light will be flashing

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3
Q

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

A

“SELCAL, SELCAL” voice aural and SELCAL advisory EICAS message or an ACARS message

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4
Q

How many ADC’s are installed on the CRJ900’s?

A

Two

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5
Q

How many AHRS computers are installed?

A

Two

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6
Q

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

A

30 to 70 seconds

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7
Q

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

A

10 to 11 minutes

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8
Q

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

A

AHRS 1 or IRS 1

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9
Q

From which source do the FO flight instruments receive AHRS information?

A

AHRS 2 or IRS 2

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10
Q

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

A

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

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11
Q

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

A

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

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12
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 side, and one on the right side.

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13
Q

Where is the TAT probe located?

A

Under FO’s side window

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14
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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15
Q

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

A

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

16
Q

In flight, which probes are heated?

A

All are fully heated regardless of probe heat switch position

17
Q

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

A

Yes, referencing NAV 1

18
Q

When and where will the radio altitude information appear?

A

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

19
Q

What does the speed trend vector indicate?

A

Predicted airspeed in 10 seconds if no changes are made

20
Q

What does the green line on the airspeed tape indicate?

A

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

21
Q

Where is the slip and skid indicator located?

A

A rectangle located just under the sky pointer

22
Q

How many flight directors are installed?

A

Two

23
Q

How many autopilots are installed?

A

One

24
Q

What does the autopilot follow when engaged?

A

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.

25
Q

What happens when the TOGA is pushed on the ground?

A

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

26
Q

What does the TO lateral mode do?

A

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

27
Q

What does TO vertical mode do?

A

Generates an optimized pitch up attitude for takeoff

28
Q

What happens when the TOGA is pushed inflight?

A

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

29
Q

What does the GA lateral mode do?

A

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

30
Q

What does GA vertical mode do?

A

Generates a 10 degree pitch up attitude