1/30
Question ID: 103222

A thermocouple type temperature sensor is composed of?

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A

Two identical metals joined together at both ends (called hot and cold junctions)

B

A single-wire metal winding

C

Two dissimilar metals joined together at one end (called hot junction or measuring junction)

D

Two identical metals joined together at one end (called hot junction or measuring junction)
2/30
Question ID: 102634

A laser gyro consists of?

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A

2 electrodes (anode and cathode)

B

A gyro with 2 degrees of freedom

C

A laser generating two light waves

D

Two moving cavities provided with mirrors
3/30
Question ID: 102627

A standby artificial horizon must have the following properties?

1) A remote gyro

2) Its own power supply

3) Only to be used in emergency

4) Its own gyro

5) One for each certified pilot

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A

1,3,5

B

2,4

C

2,3,4

D

All the above
4/30
Question ID: 102649

The latitude at which the apparent wander of a directional gyro is equal to 0 is?

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A

South pole

B

The North Pole

C

The Equator

D

Mid-Latitude
5/30
Question ID: 102735

An aircraft is at 400 ft AGL on an approach. 

What can the TCAS generate regarding an "intruder'?

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A

RA, red solid circle, aural alert

B

TA, yellow / amber solid circle, no aural alert

C

TA, yellow / amber hollow circle, aural alert

D

RA, red solid square, no aural alert
6/30
Question ID: 103152

The total pressure probe (pitot tube) comprises a mast which moves its port to a distance from the aircraft skin in order?

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A

It is easily accessible during maintenance checks

B

To locate it outside the boundary layer

C

It is protected from icing

D

Not to disturb the aerodynamic flow around the aircraft
7/30
Question ID: 103199

When flying in cold air (colder than standard atmosphere), the altimeter will?

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A

Underread

B

Show the actual height above the sea level

C

Overread

D

Show the actual height above ground
8/30
Question ID: 102519

The pendulum type detector system of the gyromagnetic compass indicator feeds?

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A

2 torque motors arranged horizontally

B

A levelling erection torque motor

C

Torque motor in the sensitive axis

D

A nozzle integral with the outer gimbal ring
9/30
Question ID: 102833

When engaged in the FMS lateral navigation mode (LNAV) the autopilot uses the command provided by the?

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A

VOR receiver

B

VOR or Localizer receiver

C

Track selector

D

FMS
10/30
Question ID: 102628

The operating principle of the pendulous vane unit erecting system is?

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A

The influence of gravity on the pendulous vanes and the gyro rotors

B

The influence of gravity on the gyro rotors

C

The influence of gravity on the pendulous vanes

D

The air flow reaction through the open vanes
11/30
Question ID: 102557

According to AMC 25.11 concerning the electronic display systems, the colour associated with a caution-type alert is?

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A

Amber or yellow

B

Red

C

Magenta

D

White
12/30
Question ID: 103065

In an inertial navigation system, the ground speed is computed?

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A

By integrating gyroscopes precessions in N/S and E/W directions

B

With TAS and W/V provided by the ADC

C

By integrating the measured accelerations

D

With TAS and W/V from RNAV data
13/30
Question ID: 103416

Maintaining CAS and flight level constant, a fall in ambient temperature results in?

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A

Lower TAS because air density increases

B

Lower TAS because air density decreases

C

Higher TAS because air density decreases

D

Higher TAS because air density increases
14/30
Question ID: 103168

The pressure altitude is the altitude corresponding?

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A

In ambient atmosphere, to the pressure PS prevailing at this point

B

In ambient atmosphere, to the reference pressure PS

C

In standard atmosphere, to the pressure PS prevailing at this point

D

In standard atmosphere, to the reference pressure PS
15/30
Question ID: 102589

In a typical aircraft EFIS display, the glideslope deviation indication consists of a?

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A

Moving pointer on a scale

B

Dial and pointer display

C

Moving numerical tape display

D

Numerical display only
16/30
Question ID: 102847

The FMS provides the following functions 

1) Fuel management 

2) Lateral flight plan management 

3) Deicing management 

4) Aircraft position computation 


The combination which regroups all of the correct statements is?

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A

2,3

B

1,2,3

C

1,2,4

D

3,4
17/30
Question ID: 102720

Choose the option which correctly describes the difference between TAWS, HTAWS and GPWS?

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A

TAWS and HTAWS use a radio altimeter and a 3D database and GPWS uses a radio altimeter

B

TAWS and HTAWS use a pressure altimeter and a 2D database and GPWS uses a radio altimeter

C

One is for aeroplanes and the other one is for helicopters

D

TAWS, HTAWS and GPWS are the same system but the names are different depending on the manufacturer
18/30
Question ID: 102577

The Flight Mode Annunciator?

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A

Instructs the Flight Director system to perform the required control movements

B

Is the only reliable source of information about which Autopilot, and Flight Director functions are in use

C

Indicates the proper operation of the Yaw Damper system

D

Instructs the Autopilot system to perform the required control movements
19/30
Question ID: 102432

A computer memory can consist of?

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A

Voltage

B

Capacitors

C

Diodes

D

Resistors
20/30
Question ID: 102793

The autopilot system?

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A

Instructs the Flight Director system to move the control surfaces

B

Includes a set of servo actuators that move the control surfaces

C

Instructs the FMS to move the control surfaces

D

Controls the FMS
21/30
Question ID: 102470

During the approach the radio altimeter indicates 950 ft. This is?

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A

The height of the pilot eyes with regard to the ground

B

The relative height of the aircraft with regard to the runway

C

The relative height of the aircraft above airport level (AAL)

D

The height of the lowest wheels with regard to the ground
22/30
Question ID: 102857

The FMS navigation database includes the following data?

Select 3 options from the below:

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A

Terrain cells

B

Obstacles

C

Waypoints

D

Magnetic variation

E

SID, STAR
23/30
Question ID: 103100

The navigation precision of a stand-alone inertial system decreases along the flight, due to?

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A

The drift of the gyroscopes

B

The meteorological conditions

C

The accelerations of the aircraft

D

The motion of the aircraft
24/30
Question ID: 103008

After alignment of the stable platform of an Inertial Navigation System, the output data from the platform is?

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A

Latitude, longitude and true heading

B

Acceleration north/south and east/west and true heading

C

Acceleration north/south and east/west, attitude and true heading

D

Latitude, longitude, and attitude
25/30
Question ID: 102797

The EFIS flight path vector (FPV) may show?

This question has been flagged as being in an exam by multiple students, give it more attention

A

Resolution Advisory pitch commands

B

Excessive vertical speed of an intruding aircraft

C

The glide angle

D

The airspeed trend arrow
26/30
Question ID: 103273

In the picture, which conical AoA probe is moving in the direction indicated?

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A

C) Clockwise

B

A) Clockwise

C

D) Anti Clockwise

D

B) Anticlockwise
27/30
Question ID: 103294

A serviceable altimeter indicates the elevation of the point selected, plus the height of the altimeter above this point, within a tolerance of?

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A

±25 m or 80 ft for altimeters with a test range of 0 to 30000 ft

B

±25 m or 80 ft for altimeters with a test range of 0 to 50000 ft

C

±15 m or 30 ft for altimeters with a test range of 0 to 60000 ft

D

±20 m or 60 ft for altimeters with a test range of 0 to 50000 ft
28/30
Question ID: 102914

Due to a drive failure, the slats of a transport category aircraft do not retract properly after take-off. 

How will this impact the FMS in terms of ETA and fuel predictions?

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A

ETA and fuel prediction will no longer be accurate

B

ETA will no longer be accurate, and fuel prediction will be accurately calculated

C

ETA or fuel prediction indications remain reliable

D

ETA will be calculated accurately but fuel prediction will no longer be accurate
29/30
Question ID: 102764

Concerning a fail-passive flight control system, in the event of a failure:

1) There may be a significant deviation of flight path or attitude

2) There is no significant deviation of flight path or attitude

3) The landing is not completed automatically

4) The landing is completed automatically


The combination that regroups all the correct statements is?

This question has been flagged as being in an exam by multiple students, give it more attention

A

2,4

B

1,4

C

2,3

D

1,3
30/30
Question ID: 102629

A stand-by-horizon or emergency attitude indicator?

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A

Is fully independent of external energy resources in an emergency

B

Is automatically connected to the primary vertical gyro if the alternator fails

C

Only works if there is a complete electrical failure

D

Contains its own separate gyro
Finish Test
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