1/30
Question ID: 103409

Regarding the operating system used for an on-board documentation (charts and company information)?

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A

There are no certification requirements

B

The certification requirements are detailed in EASA AIR OPS

C

The certification requirements are detailed in EUROCAE standards

D

The certification requirements are detailed in CS 25/29
2/30
Question ID: 102922

The purpose of an FCU / MCP is to?

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A

Operate the FMC

B

Verify thrust mode selections

C

Verify engaged modes of operation

D

Operate automation modes
3/30
Question ID: 103117

Match ground speed (GS) with the associated definition?

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A

Actual speed of an aircraft over ground

B

Indicated airspeed corrected for installation and instrument errors

C

Calibrated airspeed corrected for altitude and non-standard temperature

D

The airspeed you read directly from airspeed indicator
4/30
Question ID: 103266

A light illuminates in the cockpit which has the purpose to inform the crew that immediate awareness and response are required. 

According to CS 25, the light has to be?

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A

Magenta

B

Amber

C

Yellow

D

Red
5/30
Question ID: 102941

Assuming that the CAS remains constant, if the total pressure probe is blocked, the IAS?

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A

Remains constant during all the phases of the flight

B

Remains constant during level flight, increases during a climb and decreases during a descent

C

Remains constant during level flight, decreases during a climb and increases during a descent

D

Increases during level flight, remains constant during a climb and a descent
6/30
Question ID: 103049

Among the following functions of an autopilot, those related to the aeroplane stabilization are:

1) Pitch attitude holding

2) Indicated airspeed or Mach number holding

3) Horizontal wing holding

4) Displayed heading or inertial track holding

5) VOR axis tracking


The combination regrouping all the correct statements is?

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A

1,3,4

B

1,3

C

1,2,4

D

1,3,4,5
7/30
Question ID: 103357

While maintaining a constant TAS the OAT decreases?

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A

Mach number remains constant

B

Mach number increases

C

The difference between surrounding conditions and ISA must be known to deduce the Mach number variation

D

Mach number decreases
8/30
Question ID: 103365

When descending at a constant CAS in a standard atmosphere?

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A

TAS decreases

B

Mach number increases

C

Mach number remains constant

D

TAS increases
9/30
Question ID: 103329

If an aircraft is equipped with one altimeter which is compensated for position error and another altimeter which is not, and all other factors being equal?

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A

At high speed the non-compensated altimeter will indicate a lower altitude

B

At high speed, the non-compensated altimeter will indicate a higher altitude

C

Atc will get an erroneous altitude report SSR

D

There will be no difference between them if air the data computer is functioning normally
10/30
Question ID: 103128

Which of these statements concerning the fuel quantity measurement are correct or incorrect?

1) The quantity of fuel can be measured by volume

2) The quantity of fuel can be measured by mass

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A

1) correct; 2) is incorrect

B

1) incorrect; 2) is correct

C

1) correct; 2) is correct

D

1) incorrect; 2) is incorrect
11/30
Question ID: 102493

The magnetic heading can be derived from the true heading by means of a?

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A

Map showing the isoclinic lines

B

Map showing the isogonal lines

C

Deviation correction curve

D

Compass swinging curve
12/30
Question ID: 103122

Given E = Electromotive force (emf) 

T = Hot junction temperature 

K = Constant 


The relationship that applies to a thermocouple is?

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A

E = K x T

B

E = K x T2

C

E = K / T

D

E = K + T
13/30
Question ID: 102682

The inputs to the GPWS (Ground Proximity Warning System), are?

Select 5 options from the below:

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A

Landing gear (position)

B

NAV/ILS (glide slope)

C

Air data computer - (Mach number and vertical speed)

D

Radio altimeter

E

NAV/VOR

F

Flap (position)

G

Angle of attack
14/30
Question ID: 102465

The flight data recorder must automatically stop data recording when the?

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A

Landing gear is extended and locked

B

Main gear shock strut compresses when touching the runway

C

Airplane cannot any longer move by its own power

D

Airplane clears the runway
15/30
Question ID: 102607

Rigidity in a gyroscope is?

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A

The tendency it has to remain in its plane of rotation and resist attempts to alter its position

B

A way to express the stability of the inner and outer gimbal rings

C

The reaction 90° in the direction of rotation when applying force to the spinning wheel

D

To what extremes the flight attitudes might be before the gyro topples
16/30
Question ID: 103331

Given: 

M = The Mach number

TS = The static temperature

TT = The total temperature

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A

TS = TT x (1 + 0.2 × M2)

B

TS = TT ÷ (0.2 x M2)

C

TS = TT x (0.2 x M2)

D

TS = TT + (1 + 0.2 × M2)
17/30
Question ID: 103307

If, when correcting an EAS value of 150 kts, a TAS value of 146 kts is obtained?

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A

No allowance has been made for compressibility

B

The density of the atmosphere must be greater than the isa mean sea level air density

C

No allowance has been made for position error

D

An error must have been made in the calculation
18/30
Question ID: 102783

The sequence of the automatic landing comprises several phases, from final approach to touch-down. 

Transition from one phase to another is triggered by?

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A

The DME of the ILS

B

The altimeter set to the QNH

C

The distance left before the touch down zone

D

The radio altimeter
19/30
Question ID: 102814

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. There is no significant out-of-trim condition

4. There may be a significant out-of-trim condition


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

1,4

B

1,3

C

2,4

D

2,3
20/30
Question ID: 103370

For the same TAS, when pressure altitude decreases below the tropopause?

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A

Mach number remains constant

B

Mach number decreases

C

Mach number increases

D

The difference between surrounding conditions and ISA must be known to deduce the Mach number variation
21/30
Question ID: 102549

The following ATC clearances can be received via the datalink application?

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A

Departure, Enroute, Landing

B

Departure, Oceanic

C

Departure, Take-off, Enroute

D

Take-off, Enroute, Landing
22/30
Question ID: 102888

Concerning the flight warning system (FWS), warning messages?

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A

Are inhibited by caution messages

B

Are never associated to a fire engine

C

Are highest priority alert messages

D

Indicate that subsequent crew action may be required
23/30
Question ID: 102725

Which statement is true about the IVSI?

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A

The IVSI has its own power supply, independent of the aircraft

B

The use of the IVSI reduces turning errors

C

The almost instantaneous indications from the IVSI provide the flight crew with reliable information in all phases of flight

D

The IVSI can give erroneous readings while initiating or ending turns at bank angles of more than around 40°
24/30
Question ID: 102656

The inclination of the Earth's magnetic field at the magnetic equator is equal to?

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A

45°

B

90°

C

0°

D

180°
25/30
Question ID: 102742

The control law of a transport airplane autopilot control channel may be defined as the relationship between the? 

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A

Input and output signals at the amplifier level respectively control deviation data and control deflection signals

B

Computer input deviation data and the output control deflection signals

C

Computer input deviation data and the signals received by the servo actuators

D

Crew inputs to the computer and the detector responses (returned to the airplane)
26/30
Question ID: 103244

Which statement regarding the North magnetic pole is correct?

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A

It is co-located with the geographic North pole

B

It remains static

C

It wanders at an average rate of about 15 km per year

D

It moves at a steady rate of 15 mm per year
27/30
Question ID: 103366

The Mach meter is subject to position error. 

This error concerns?

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A

Static ports only

B

Pitot tubes only

C

Pitot tubes and static ports

D

Alternate static sources only
28/30
Question ID: 102506

A pilot wishes to turn right on to a northerly heading with 20° bank at a latitude of 40°. 

North Using a direct reading compass, in order to achieve this, he must stop the turn on to an approximate heading of?

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A

330°

B

350°

C

030°

D

010°
29/30
Question ID: 102616

If the needle and the ball of a Turn and Slip indicator both show right, what does it indicate?

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A

Turn to left and too little bank

B

Turn to right and too little bank

C

Turn to left and too much bank

D

Turn to right and too much bank
30/30
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?

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

A

3,4

B

1,2,3

C

2,3

D

1,2,4
Finish Test
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