Flight Instruments Flashcards

1
Q

The ESID system is responsible for displaying what?

A

Engine and system information

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2
Q

The air data computers receive heading, pitch, and roll data from the ______.

A

AHRS (Attitude and Heading Reference System)

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3
Q

With the ADC SOURCE selector in the NORM position, the displays on the left side receive information from ______.

A

ADU 1 (Air Data Unit)

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4
Q

In common color philosophy for the 5 display units, abnormal situations and conditions requiring immediate crew notification are what color?

A

Yellow

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5
Q

Pushing the BARO SET knob will accomplish what?

A

Set 29.92 (standard)

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6
Q

T/F: Bearing pointers can only use VOR radios as a navigation source.

A

FALSE, AUX, VOR, ADF, & FMS are all bearing NAV sources

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7
Q

When does the NO DATA flag appear?

A

FMS is not available (and data is pushed)

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8
Q

T/F: Radar and EGWPS displays cannot be selected at the same time on the same display.

A

TRUE

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9
Q

The center FMA field on each PFD is used to display what AFCS information?

A

Failure Messages

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10
Q

The ISI is powered by which sources?

A

Left essential DC bus and a rechargeable back up battery (lasts 1 hr)

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11
Q

A ______ interconnects all of the displays.

A

feed back bus (allows feedback and comparison of critical flight parameters)

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12
Q

What does the AHRS system accomplish?

A

Supplies attitude and heading (pitch, roll, yaw) information to EIS, auto flight, stall protection and other systems

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13
Q

Pitot static data is provided to the aircraft via how many Air Data Units?

A

2 ADUs

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14
Q

T/F: The 5 display units’ brightness can only be controlled manually.

A

FALSE, can be controlled automatically with photo sensors

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15
Q

T/F: A detent in the full counter-clockwise position selects the associated display unit OFF.

A

TRUE

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16
Q

Which of the following is NOT a designation of the 5 display units?
(Answer which IS a designation)

A

PFD (Primary Flight Display)
MFD (Multi Function Display)
ED (Engine Display)

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17
Q

If ED fails, the system will automatically transfer engine data to the ______.

A

MFD 1

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18
Q

Regarding the display units, which color indicates status messages, advisories, lines, references, and armed autoflight modes?

A

White

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19
Q

With regard to the display units, which color indicates active controlling modes and functions?

20
Q

The fixed area on the Captain’s MFD contains ______ information and the First Officer’s contains ______ information.

A

PFCS (Powered Flight Control Surface) // Flap position & Hydraulic pressure/quantity

21
Q

T/F: Cyan colors on the displays indicate pilot selectable items.

22
Q

Which color on the display units indicates FMS-related data or pointers?

23
Q

T/F: On the display units, magenta indicates FMS-related data or pointers.

24
Q

T/F: If a red indication is displayed on an instrument, it is a low priority indication.

A

FALSE, red = immediate crew notification and timely corrective action is necessary

25
On the display units, a ______ text message is used for messages that require subsequent action.
Flashing
26
T/F: Brackets are used on the displays for certain messages regarding flight crew instructions or required crew actions.
TRUE
27
The AHRS system includes how many operating modes?
3 Modes (ALIGN, NORMAL, SLAVE)
28
AHRS is able to operate in one of two reduced performance modes, ______ and ______, during non-normal operations.
BASIC // DG
29
T/F: If BASIC mode or DG mode is present on the AHRS, the crew is still allowed to takeoff.
FALSE, takeoff with BASIC or DG is prohibited
30
Takeoff is prohibited if either AHRS is in ______ mode or ______ mode.
BASIC // DG
31
The AHRS enters the alignment mode how many seconds after a power-on self test?
5 seconds after self test
32
A ______ colored annunciator on the ATT/HDG ALIGN switch light illuminates during the alignment.
Amber
33
T/F: After AHRS alignment is complete, the system automatically enters the NORMAL mode.
TRUE
34
Which ADU input is used to correct for acceleration-induced attitude errors?
True Airspeed is used
35
If both MFD selectors are not in SYS, pressing and holding any page button will display the system on the ______.
ED (Engine Display)
36
Which source will automatically display on MFD 1 during a failure?
ED (Engine Display)
37
T/F: If onside ADU inputs fail completely, the AHRU will automatically revert to the opposite side’s ADU.
TRUE
38
T/F: In SLAVE mode, the AHRUs use analog magnetic headlong data from the flux valves to set inertial heading data.
TRUE
39
T/F: If true airspeed information from the ADU is not available, the BASIC mode is automatically entered.
TRUE
40
Each index control panel controls certain elements on the associated pilot’s ______.
PFD
41
Display items that are adjusted by the index control panel include ______.
Speed bugs Barometric pressure Decision altitude (DA) or Minimum descent Altitude (MDA)
42
Adjustable speed bugs available for takeoff include V1, V2, and ______.
VR
43
If changes are not made to the V speeds within ______ seconds of pressing the speed bug on the index control panel, the box disappears.
5 seconds
44
T/F: The BARO SET knob is used to set the barometric correction, displayed on the bottom of the altitude tape on the MFD.
FALSE, altitude tape is on PFD
45
What happens if the DH or MDA setting on the PFD is set to 0 feet?
The display is removed from the PFD
46
The EFIS control panels are used to control the ______.
Display data on the associated side MFD and PFD
47
The BRG selector knob on the EFIS control panel has which 4 pointer navigation sources that are available for selection?
AUX FMS ADF VOR