Flight Instruments Flashcards

0
Q

In the event of a Display Control Panel failure (DCP), both MFD’s can be controlled by one DCP by making a selection on the:

A

Display Control Panel (DCP)

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1
Q

In the event a PFD Fails, PFD information can be displayed on the MFD by using the:

A

Display Control Panel (DCP).

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2
Q

The Total Air Temperature Probe (TAT) supplies temperature informations on to the:

A

Air Data Computers

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3
Q

Pitot/Static inputs and Total Air Temperature provide raw Air Data Information which converted to digital format through the:

A

Air Data Computers (ADC’s)

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4
Q

What is the time required to align the AHRS in the MAG Mode?

A

30-70 seconds

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5
Q

What is the time required to align the AHRS in the DG Mode?

A

10-11 minutes

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6
Q

Radio Altitude will be displayed on the PFD when?

A

Below 2500 ft AGL

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7
Q

What is the primary purpose of the Digital Clocks?

A

It serves as a time base for the avionics system

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8
Q

The Airspeed trend vector indicates the predicted airspeed in?

A

10 seconds

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9
Q

The Mach number will be displayed when the aircraft reaches?

A

.45 Mach

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10
Q

The green line on the Airspeed Tape indicates?

A

1.27 Vs

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11
Q

The Skid and Slip Indicator on the PFD is:

A

A rectangle under the Roll Pointer

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12
Q

When a common Attitude/Heading source is selected, an annunciation will appear on the?

A

EICAS Secondary Page

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13
Q

The Integrated Standby Indicator can display Localizer and Glide slope information True or False

A

True

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14
Q

The Standby Instrument (ISI) is located where

A

In between PFD and MFD

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15
Q

On the Coarse Altitude Tape the large rectangles represent - what increments?

A

100 ft increments

17
Q

The Co-Pilots PFD and MFD normally receives Air Data, Attitude and Heading information from the
ADC ? and AHRS ?

A

ADC 2 and AHRS 2