Avionics

Question 1

2 large red X’s on DU 3 and DU 4 indicate a ( ).

Answer 1

failure of the right IC 600.

PTM 16-6

Question 2

Failure of the left IC 600 is indicated by ( ).

Answer 2

2 large red X’s on DU 1 and DU 2.

PTM 16-6

Question 3

In the event of an IC 600 failure, the appropriate checklist is found using the table of contents, ( ).

Answer 3

QRH, amber, Instrument/Avionics section.

QRH A-4

Question 4

Red X’s over the airspeed and altitude tapes on DU 1 is an indication of a(n) ( ).

Answer 4

ADC 1 Failure.

PTM 16-30

Question 5

Failure of ADC 2 is indicated by ( ).

Answer 5

red X’s over the airspeed and altitude tapes on DU 4.

PTM 16-30

Question 6

In the event of an ADC failure, the appropriate checklist is found using the table of contents, ( ).

Answer 6

A-26
Instrument/Avionics category of the amber section of the QRH.
QRH A-5

Question 7

What is indicated by ATT FAIL over a blue ADI (blue ball of death), compass rose with a red X, and the words HDG FAIL displayed on DU 1?

Answer 7

AHRS 1 failure.

PTM 16-35

Question 8

Failure of the AHRS 2 is indicated by ( ), ( ), and ( ).

Answer 8

ATT FAIL printed across a blue ADI (blue ball of death), red X across the compass rose, and the words HDG FAIL displayed on DU 4.

PTM 16-35

Question 9

The checklist for AHRS failure is found using the table of contents of the ( ).

Answer 9

A-28
Instrument/Avionics category of the amber section of the QRH.

“Loss of PFD Attitude or Heading Displays”

QRH A-5

Question 10

The QRH title of AHRS 1 or AHRS 2 failure is ( ).

Answer 10

“Loss of PFD Attitude or Heading Displays”
A-28
Amber section of the QRH

QRH A-5

Question 11

A red AP will display on both PFDs along with a ‘cavalry charge’ aural alert when ( ).

Answer 11

the autopilot does a self-monitoring disconnect.

PTM 16-86

Question 12

How can you extinguish a red AP and/or turn off the ‘cavalry charge’ aural alert?

Answer 12

Press either Control Wheel Master.

PTM 16-86

Question 13

Activating the trim switch on either yoke will disconnect the ( ).

Answer 13

autopilot.

PTM 16-88

Question 14

What 6 things are disconnected or interrupted when you press and hold the Control Wheel Master?

Answer 14

1. Disconnects autopilot
2. Disconnects Yaw Dampener
3. Interrupts All trims
4. Interrupts Rudder boost
5. Interrupts Pitch trim bias
6. Nose Wheel Steering

PTM 15-4

Question 15

To display engine data on the RMU, select the ( ) button, then press the line select key beside ( ).

Answer 15

PGE
ENGINE

PTM 16-14

Question 16

To display nav data on the RMU, select the ( ) button, then press the line select key beside ( ).

Answer 16

PGE
NAVIGATION

PTM 16-14

Question 17

The Clearance Delivery Head can be powered with both aircraft batteries off by using the ( ).

Answer 17

Radio Control Hot Bus switch.

PTM 16-26

Question 18

What is an alternate way to tune com 1?

Answer 18

The Clearance Delivery Head

PTM 16-26

Question 19

What is indicated if there is an ATT, PIT, or ROL displayed above both ADIs on the PFDs?

Answer 19

There is a mis-compare between AHRS 1 & 2 in pitch and/or roll.

PTM 16-44

Question 20

How will you know if there’s a mis-compare between AHRS 1 & 2 in heading?

Answer 20

Amber HDG above the HSI on both PFDs.

PTM 16-44

Question 21

What happens when the IC Reversion switch is placed in the #1 position?

Answer 21

Information from IC 600 #1 will be displayed on both PFDs.

PTM 16-6

Question 22

What happens when the AHRS Reversion switch is placed in the #1 position?

Answer 22

AHRS 1 data is displayed on both PFDs.

PTM 16-35

Question 23

What happens when the AHRS Reversion switch is placed in the #2 position?

Answer 23

AHRS 2 data is displayed on both PFDs.

PTM 16-35

Question 24

What happens when the ADC Reversion switch is placed in the #1 position?

Answer 24

ADC 1 data is displayed on both PFDs.

PTM 16-30

Question 25

Will the autopilot function without the yaw dampener?

Answer 25

No. YD comes on automatically when the AP is turned on. AP will disconnect if the YD is turned off.