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Flight Safety Lear 45/40 Required Knowledge Areas > AVIONICS > Flashcards

AVIONICS Flashcards

1
Q

Failure of the ( ) IC 600 is displayed by two large red X’s on DU 3 and DU 4.

A

Right. PTM Pg. 16-6

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2
Q

Failure of the ( ) IC 600 is displayed by two large red X’s on DU 1 and DU 2.

A

Left. PTM Pg. 16-6

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3
Q

In the event of an IC 600 ( ), the appropriate checklist to run can be found using the table of contents pages, Instrument/Avionics category of the amber section in the QRH.

A

Failure. QRH Pg. A-4

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4
Q

Failure of ( ) is indicated by red X’s over the airspeed and altitude tapes on DU 1.

A

ADC 1 . PTM Pg. 16-30

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5
Q

Failure of ( ) is indicated by red X’s over the airspeed and altitude tapes on DU 4.

A

ADC 2. PTM Pg. 16-30

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6
Q

In the event of ( ) failure, the appropriate checklist to run can be found using the table of contents pages, Instrument/Avionics category of the amber section in the QRH.

A

ADC. QRH Pg. A-5

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7
Q

Failure of ( ) is indicated by ATT FAIL printed on a cyan ADI (‘blue ball of death’), a compass rose with a red X and the words HDG FAIL displayed on DU 1.

A

AHRS 1. PTM Pg. 16-35

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8
Q

Failure of ( ) is indicated by ATT FAIL printed on a cyan ADI (‘blue ball of death’) a compass rose with a red X and the words HDG FAIL displayed on DU 4.

A

AHRS 2. PTM Pg. 16-35

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9
Q

In the event of ( ), the appropriate checklist to run can be found using the table of contents pages, Instrument /Avionics category of the amber section in the QRH.

A

AHRS failure. QRH Pg. A-5

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10
Q

The QRH title for AHRS 1 or AHRS 2 failure is “Loss of PFD ( ) or ( ) Displays.”

A

Attitude or Heading. QRH Pg. A-5

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11
Q

If the auto-pilot does a self-monitoring disconnect, a red AP will be displayed on the PFDs along with a ( ) aural alert.

A

Cavalry charge. PTM Pg. 16-86

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12
Q

To extinguish a red AP and/or turn “OFF the ‘cavalry charge’ aural alert, either aircrew can depress the red ( ) button on the control yokes.

A

Control Wheel Master Switch (MSW). PTM Pg. 16-86

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13
Q

Activating the ( ) switch on either yoke will disconnect the auto pilot.

A

Trim. PTM Pg. 16-88

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14
Q

Depressing and holding the red Control Wheel Master Switch (MSW) button on either control yoke disconnects the auto pilot and yaw dampener along with:

A

Interrupting all trims, Rudder Boost and

Pitch Trim Bias. PTM Pg. 15-4 and 16-88

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15
Q

The ( ) can display engine data and navigation data along with radio and transponder information.

A

RMU. PTM 16-14

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16
Q

To display engine data on the RMU, select the PGE button, then depress the line select key next to:

A

ENGINE. PTM Pg. 16-14

17
Q

To display navigation data on the RMU, depress the PGE button, then depress the line select key next to:

A

NAVIGATION. PTM Pg. 16-14

18
Q

The Clearance Delivery Head (CDH) can be powered with both aircraft main ship batteries OFF by using the:

A

Radio Control Hot Bus switch. PTM Pg. 16-26

19
Q

The Clearance Delivery Head (CDH) is an alternate way to tune:

A

Comm 1. PTM Pg. 16-26

20
Q

To display FMS navigation information data, such as an RNAV/GPS approach on the PFD, select the ( ) button on the display controller.

A

FMS. PTM 16-41

21
Q

To display ILS information on the PFD, select the ( ) button on the Display Controller.

A

NAV. PTM Pg. 16-41

22
Q

To switch the display on the PFD between ILS 1 and ILS 2, ( ) the NAV button on the display controller.

A

NAV. PTM Pg. 16-41

23
Q

If there is a mis-compare between AHRS 1 and AHRS 2 in pitch and/or roll, an ATT, PIT, or ROL will be posted on both ( ).

A

ADIs on the PFDs. PTM Pg. 16-44

24
Q

If there is a mis-compare between AHRS 1 and AHRS 2 in heading, an amber ( ) will be posted just above the compass rose on both PFDs.

A

HDG. PTM Pg. 16-44

25
Q

When the IC Reversion switch is placed to the (# ) position, information from IC 600 #1 will be dis-
played on all the Display Units.

A

1. PTM Pg. 16-6

26
Q

When the IC Reversion switch is placed to the (# ) position, information from IC 600 #2 is displayed
on all the Display Units. PTM Pg. 16-6

A

2. PTM Pg. 16-6

27
Q

When the AHRS Reversion switch is placed to the (# ) position, AHRS #1 data will be displayed on
both PFDs on DU 1 and DU 4.

A

1 position. PTM Pg. 16-35

28
Q

When the AHRS Reversion switch is placed to the (# ) position, AHRS #2 data will be displayed on
both PFDs on DU 1 and DU 4. PTM Pg. 16-35

A

2 position. PTM Pg. 16-35

29
Q

When the ADC Reversion switch is placed to the (# ) position, ADC #1 data will be displayed on
both PFDs on DU1 and DU4.

A

1. PTM Pg. 16-30

30
Q

When the ADC Reversion switch is placed to the (# ) position, ADC #2 data will be displayed on
both PFDs on DU1 and DU4.

A

2. PTM Pg. 16-30

Flight Safety Lear 45/40 Required Knowledge Areas (22 decks)

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