Instruments Flashcards

1
Q

During normal operations, which flight instrument receives information directly from the ADC?

A

Pilot’s altimeter by ADC#1 and co-pilot’s by ADC#2

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2
Q

What information does the #1 ADC receive?

A

Pitot, static, temperature, altimeter setting, encoding altitude, altitude selection, overspeed, HSI selection #1 Nav Data

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3
Q

What does the HSI SEL switch do?

A

Couples the HSI selected side and the ADC to the autopilot

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4
Q

What is the indication of an ADC failure?

A

A flag will appear on the affected altimeter.

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5
Q

What action should be taken if an ADC fails?

A

Switch HSI SEL to the other side

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6
Q

What are the standard operating modes for the AHRS?

A

Normal for Attitude, Slaved for heading

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7
Q

What are the reduced operating modes of the AHRS?

A

Basic for Attitude, DG for Heading

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8
Q

What is the BASIC mode of AHRS?

A

Attitude information not corrected for acceleration

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9
Q

What are the limitations for take-off in reduced operating mode of the AHRS?

A

Not Approved - Prohibited

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10
Q

What action should be taken in the event of an ATT failure?

A

Engage ATTITUDE REVERSION by pushing ATT REV on the EFIS Controller

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11
Q

What happens when you engage ATT REV on the EFIS Controller?

A

Attitude information is displayed on the EADI from the cross-side and the opposite side ATT1 or ATT2 is displayed on the reverted EADI

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12
Q

What action should be taken in the event of a HDG failure?

A

Engage Heading Reversion by pushing HDG REV on the EFIS controller

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13
Q

What happens when you engage HDG REV on the EFIS Controller

A

Heading information is displayed on the EHSI from the cross-side and the opposite side MAG1 or MAG2 is displayed on the reverted EHSI

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14
Q

Where does the standby altimeter receive static pressure from?

A

Pilot Static Source or Alternate Static Source (depending on MOD)

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15
Q

What does the alternate static selector do?

A

Provides an Alternate Static Source for either the Pilot or Co-pilot

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16
Q

What does the AOA F-S indicator on the left side of the EADI indicator?

A

Speed relative to the Vref speed

17
Q

What are the indications of a radio altitude failure?

A

Dashes after the RA on the EADI and the Rising Runway is removed

18
Q

Where is the digital RAD ALT information displayed?

A

Lower right corner of the EADI

19
Q

What are the indication of a CRT failure?

A

Blank screen

20
Q

What action should be taken following a CRT failure?

A

Turn the failed unit off and switch to the composite mode display

21
Q

What limitations are there when using composite mode

A

No ILS permitted on the composite side

22
Q

What is the indication of a symbol generator failure?

A

Blank screen on EADI and EHSI

23
Q

What is the indication of a symbol generator data failure?

A

Large X across screen, SG FAIL screen

24
Q

What action should be taken in the event of a symbol generator failure and what is the indication following the action?

A

Push REVN button above the EADI to get the opposite side information on the failed side, noted on left side of EADI

25
Q

What are the marker indications displayed?

A

EADI under the vertical Glide Slope. On the annunciator panel above the EADI

26
Q

Where is the DH set and displayed?

A

Set on the EFIS controller and displayed on the lower left side of the EADI

27
Q

Where does the standby altimeter receive static pressure from?

A

Pilot or Alternated Static depending on MOD

28
Q

How does the standby attitude indicator operate?

A

Electrically powered gyro