Flight Instuments Flashcards

1
Q

There are two air data systems (ADS),
What are the components of each?

A

Each system consist of one air data computer, one pitot tube, one TAT probe, and two static ports 

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2
Q

Which instrument/sensors make up the standby ADS system?

A

One pitot/static tube, one standby altimeter, and one standby airspeed indicator 

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3
Q

In addition to the standby instruments to which other system does the number three Pitot/static tube provide air pressure information? 

A

CPAM

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4
Q

What does an amber colored ADC1/ADC2 message on the PFD indicate

A

Only one ADC is supplying both the captains and first officers instruments 

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5
Q

What is the purpose of the air data computer? (ADC)

A

It senses processes and transmits air data information to various systems and instruments of the airplane 

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6
Q

What information does the air data computer (ADC) provide to the IC-600

A

Airspeed (true, calibrated, mock number, vertical) VMO, and temperature
(Static and total)

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7
Q

What other systems receive information from the ADCs?

A

FADEC (total pressure, mock number, TAT)
HSCU (calibrated airspeed)
Transponder/TCAS (pressure, altitude)
AHRS (AH-900 only - true airspeed)
FMS (true airspeed speed)
Radar (altitude)
SPS (Mach number)
GPWS (calibrated, and true airspeed, altitude, vertical speed)
CPCS (pressure, altitude and baro correction, altitude rate of change)
Ice protection (altitude trip point)
Rudder system (calibrated airspeed, tripoint)
AWU (over speed, warning, output)

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8
Q

How are barometric pressure data discrete inputs to the ADCs set

A

On the PFD bezel

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9
Q

What is indicated by an amber RA
label inside an Amber box at the bottom of the altitude indicator

A

Radio altimeter failure

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10
Q

If the acceleration trend vector exceeds VMO or MMO, and what color are the digits in the airspeed window and the digital mack read out shown

A

Amber

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11
Q

The magenta, airspeed trend vector represents the airspeed which the aircraft will attain, and how many seconds

A

10

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12
Q

The altitude trend vector represents the altitude which the aircraft will attain in how many seconds

A

6

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13
Q

A red X on the airspeed and altitude tapes and a red V/S on the vertical speed indicator indicates what

A

 An air data computer failure

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14
Q

Which pitot tube and static port supply the number one ADC

A

Pitot 1 and static port 1 and 4

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15
Q

An Amber IAS message shown on the airspeed tape, indicates a difference of how many knots, or more between airspeed indications

A

5 kias

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16
Q

An Amber ALT shown on the PFD indicates a difference of how many feet between altitude indicators 

A

200ft

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17
Q

ROL message shown on the PFD indicates a discrepancy more than how many degrees of bank

A

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18
Q

PIT comparison monitor will be shown on the PFD when there is a discrepancy of more than how many degrees of pitch

A

19
Q

How many hours of aircraft data is recorded by the DFDR

A

25hrs

20
Q

How is decision height set on the radio altimeter

A

By using the RA knob located on the display control panel

21
Q

What does an amber MIN label shown inside a box at the lower right of the attitude indicator indicate

A

The aircraft is at a radio, altitude, equal to, or lower than, the decision height, setting

22
Q

When does the “Brown ground” appear on the altitude tape?

A

When the radio altitude is less than 550 feet

23
Q

What is the radio altimeter Range?

A

From -20 feet to 2500 feet

24
Q

Which instruments are combined into the ISIS

A

Attitude, altitude, and airspeed

25
Q

Which components are responsible for the interaction among the many airplane systems, besides managing information shown on the displays

A

IC-600

26
Q

How many channels does each DAU have

A

Two

27
Q

What is the purpose of DAU channel B?

A

It is kept as a standby source, which must be manually selected through the EICAS revisionary button

28
Q

IC–600 number 1 normally provides images to which screens

A

PFD, one, MFD one, and EICAS

29
Q

If IC-600 number 1 fails, how can you get information back to the pilot screens?

A

IC-600 number two will control all five displays by pressing the symbol generator (SG) button on the left revisionary panel

30
Q

How can the MFD be used to show PFD or EICAS information, if those screens fail

A

By making the appropriate selection on the revisionary panel

31
Q

What are the main indications shown on the EICAS screen

A

Engine indications, flaps, landing gear, spoilers, and trim positions, total fuel quantity, APU, and pressurization information

32
Q

Where are the master warning and caution lights?

A

On each pilots glareshield panel

33
Q

Regarding EICAS messages, what does the inhibition logic do?

A

It prevents some messages from being shown during takeoff and approach/landing phases to avoid nuance effects upon the flight crew

34
Q

What color are normal indications shown in?

A

Green

35
Q

What color are caution, messages, and lights?

A

Amber

36
Q

Voice messages are normally associated with which type of messages on EICAS or other crew awareness systems

A

Warning

37
Q

How is the back up aural warning unit channel activated, if channel a fails

A

Automatically

38
Q

Where can you set V speed bugs for the airspeed tapes

A

MFD SPDS sub menu

39
Q

How is the barometric pressure set for either? “NHG” or “HPA “

A

A button on the lower left of the PFD 

40
Q

The TCAS provides vertical direction and minimum vertical speed information during evasive maneuvers for resolution advisories where is this information shown

A

On the PFD VSI

41
Q

In an electrical emergency for how many minutes will the ISIS operate solely on the airplane batteries

A

40 minutes

42
Q

Where are the decision height and the associated RA label shown

A

 Adjacent to the lower right side of the attitude sphere

43
Q

Where is the button for setting/starting/stopping the chronometer

A

On the inner half of each control wheel

44
Q

On the PDF FMA, what are the correct color codes for normal operation in FMS, active mode and armed mode

A

FMS active mode: magenta
Armed mode: white