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M11.5.1 Instrument Systems (ATA 31) Cat A V4.1.0

Total questions: 32

Worksheet time: 16mins

Name
Class
Date
1.

Where are the flight instruments located in large commercial aircraft?

a)

On the overhead panel

b)

On the flight engineer panel

c)

On the Captains and co-pilots instrument panels

d)

On the centre instrument panel

2.

Which instrument indicates the altitude of the aircraft above sea level or airport?

a)

Airspeed Indicator

b)

Vertical Speed Indicator

c)

Altimeter

d)

Mach meter

3.

What does the Artificial Horizon or Attitude indication show?

a)

Rate of climb or descent

b)

Speed of the aircraft

c)

Roll and pitch attitude of the aircraft

d)

Direction of the aircraft longitudinal axis

4.

What does the Mach meter indicate?

a)

Ratio of the aircraft’s true airspeed to the actual speed of sound

b)

Rate of climb or descent

c)

Temperature of the air around the aircraft

d)

Total air temperature

5.

How is altitude indicated when the baro reference is set to sea level pressure (QNH)?

a)

True altitude

b)

Field elevation

c)

Flight level

d)

Indicated altitude

6.

What is the purpose of the Pitot tube?

a)

To measure static pressure

b)

To indicate altitude

c)

To measure total pressure

d)

To provide dynamic pressure

7.

What does the Altitude Alert System do?

a)

Alerts the pilot about nearby aircraft

b)

Provides weather updates during flight

c)

Compares actual altitude with clearance altitude

d)

Monitors engine performance

8.

When does the altitude alert extinguish?

a)

When the aircraft returns to the correct altitude

b)

When the aircraft deviates more than 300 ft.

c)

When the autopilot is active

d)

When the aircraft climbs or descends

9.

What triggers the over speed warning in jet aircraft?

a)

Indicated airspeed

b)

Mach number

c)

Altitude deviation

d)

Flap position

10.

How does the stall warning system warn the pilot?

a)

Visual flashing lights

b)

Aural alerts and stick shaker vibrations

c)

Overhead loudspeaker announcements

d)

Auto-throttle system activation

11.

What does the Flight Data Recorder (FDR) record?

a)

Radio communications

b)

Time and date of the flight

c)

Air traffic control instructions

d)

Important flight parameters

12.

What provides the heading reference signal for the Horizontal Situation Indicator (HSI) and Radio Magnetic Indicators (RMI)?

a)

Rate Gyro

b)

Vertical Gyro (VG)

c)

Directional Gyro (DG)

d)

Gyro Drive

13.

What keeps the direction of its axis constant as long as no force acts on it?

a)

Rate Gyro

b)

Directional Gyro (DG)

c)

Space Gyro

d)

Gyro Principles

14.

What is the purpose of gyro precession?

a)

To maintain gyro stability

b)

To change the direction of the gyro axis

c)

To shift the force applied to the gyro

d)

To rotate the gyro clockwise

15.

How many degrees of freedom does a gyro with one gimbal have?

a)

b)

c)

d)

1½°

16.

Which instrument uses a Vertical Gyro (VG) as a reference?

a)

Attitude Director Indicator

b)

Direct Reading Compass

c)

Turn & Slip Indicator

d)

Horizontal Situation Indicator

17.

What is the angle between the aircraft longitudinal axis and the direction to the North Pole known as?

a)

Compass Deviation

b)

True North

c)

Magnetic North

d)

Indicated Heading

18.

What is the difference between True North and Magnetic North called?

a)

Compass Compensation

b)

Variation

c)

Inclination

d)

Flux Valve

19.

Where is the Standby Compass usually located in commercial aircraft?

a)

Between the centre-post of the front windshields

b)

On the main instrument panels

c)

In the cockpit's overhead panel

d)

In the flight deck's center console

20.

How is deviation minimized in direct reading compasses?

a)

By using a flux valve

b)

By adjusting the compensating magnets

c)

By installing potentiometers

d)

By conducting a 360° turn of the aircraft

21.

What is the purpose of a flux valve in a remote compass system?

a)

To measure the aircraft's acceleration

b)

To compensate for magnetic deviations

c)

To transfer the direction of the magnetic field into an electrical signal

d)

To compare the aircraft's magnetic field with the heading shown on the indicator

22.

What is the term used by Airbus to refer to the Electronic Instrument Display System?

a)

Integrated Display System (IDS)

b)

Engine Indication and Central Warning System (ECAM)

c)

Electronic Centralised Aircraft Monitoring (ECAM)

d)

Electronic Instrument System (EIS)

23.

How are the displays in the Electronic Instrument Display Systems (EIDS) activated?

a)

By pressing the "ON" button on each display unit

b)

By pulling the brightness control knob

c)

By rotating the brightness control knob clockwise

d)

By adjusting the EFIS control panel

24.

What are the two main types of displays in the Electronic Flight Instrument System (EFIS)?

a)

Engine Indication and Crew Alerting System (EICAS) and Navigation Displays (ND)

b)

Primary Flight Displays (PFD) and Central Warning System (CWS)

c)

Primary Flight Displays (PFD) and Navigation Displays (ND)

d)

Electronic Centralised Aircraft Monitoring (ECAM) and Navigation Displays (ND)

25.

How are central warnings different from local warnings?

a)

Central warnings are controlled by specific aircraft systems, while local warnings are controlled by computers.

b)

Central warnings are controlled directly from the specific systems, while local warnings are controlled by the Central Warning System (CWS).

c)

Central warnings require immediate attention, while local warnings may not necessarily require immediate action.

d)

Central warnings are displayed only on the upper display units, while local warnings are displayed on the lower display units.

26.

What instrument is shown in position 1?

a)
  • Airspeed Indicator

b)
  • Altimeter

c)
  • Vertical Speed Indicator

d)

Attitude Director Indicator

e)

Turn & Bank Coordinator

27.

Which of the following instruments are within the Basic T?

a)

Horizontal Situation Indicator

b)
  • Airspeed Indicator

c)
  • Vertical Speed Indicator

d)
  • Turn & Bank Indicator or Coordinator

e)

Engine Oil Pressure Indicator

28.

How is the total amount of fuel presented on the ECAM/EICAS display?

a)

ECAM - Total Fuel (TF) in kilograms, EICAS - Fuel on Board (FOB) in metric tons.

b)

ECAM - Fuel on Board (FOB) in kilograms, EICAS - Total Fuel (TF) in metric tons.

c)

ECAM - Fuel on Board (FOB) in kilograms, EICAS - Total Fuel (TF) in kilograms.

d)

ECAM - Total Fuel (TF) in metric tons, EICAS - Fuel on Board (FOB) in kilograms.

29.

How is fuel temperature indicated on the EICAS and ECAM displays?

a)

EICAS displays individual temperature values for each wing tank, while ECAM displays fuel temperature in one tank.

b)

EICAS displays fuel temperature in one tank, while ECAM displays individual temperature values for each wing tank.

c)

Both EICAS and ECAM display fuel temperature in one tank.

d)

Both EICAS and ECAM display individual temperature values for each wing tank.

30.

What type of sensors are used as accelerometers in the engine vibration monitoring system?

a)

Optical sensors

b)

Thermocouples

c)

Electromagnetic accelerometers

d)

Ultrasonic sensors

31.

How many sensors are usually found on each engine for vibration monitoring?

a)

One sensor located in the compressor area

b)

One sensor located in the turbine area

c)

Two sensors, one in the compressor area and one in the turbine area

d)

Three sensors, two in the compressor area and one in the turbine area

32.

What does it mean when the EICAS display shows "FAN" as a vibration indication mode?

a)

The forward sensor is measuring the vibration of the N1 rotor.

b)

The aft sensor is measuring the vibration of the N1 rotor.

c)

The vibration of the N2 rotor system is measured by the aft sensor.

d)

The unfiltered vibration signal from the aft sensor is displayed.