10. OS 1

Question 1

Which speed is displayed as the top of a strip on the speed scale of the HUD and the PFD?

Accepted Answer

VLS speed.

Answer

VFE next speed.

Answer

Green dot speed.

Answer

VMAX speed.

Question 2

What are the main functions of the NORM TAWS system?

Accepted Answer

The Ground Proximity Warning System (GPWS), the Terrain Clearance Floor (TCF) and the Terrain(TERR) and obstacles.

Answer

The Enhanced Vision System (EVS) and the Tactical Terrain Awareness and Display (T-TAD).

Answer

The databases and DMAP information.

Answer

Only the Ground Proximity Warning System (GPWS).

Question 3

Which speed is displayed as the end of a strip on the speed scale of the HUD and the PFD? (picture pointing to the lower end of the barber pole)

Accepted Answer

VMAX speed.

Answer

VFE next speed.

Answer

Green dot speed.

Answer

VLS speed.

Question 4

Which Primary (PRIM) computer has the priority to manage the flight envelope (FE) function?

Accepted Answer

The master PRIM.

Answer

The PRIM 3.

Answer

The PRIM 2.

Answer

The PRIM 1.

Question 5

On the NTD format, the colour of any SEC F-PLN is:

Accepted Answer

White

Answer

Yellow

Answer

Blue

Answer

Green

Question 6

When a system fails, the ECAM may display some deferred procedures. They are displayed on the:

Accepted Answer

Normal checklist menu.

Answer

Loadmaster Workstation display.

Answer

Tactical checklist menu.

Answer

Abnormal checklist menu.

Question 7

Select the correct statement:

Accepted Answer

The NTD provides lateral and vertical navigation information, according to the flight plan, the navigation database and tactical data.

Answer

The NTD provides only long term information.

Answer

The NTD is used for aircraft position attitude.

Answer

The NTD provides only short term information.

Question 8

When a system fails, the ECAM may display some deferred procedures in the C/L menu page. What is the correct statement?

Accepted Answer

The deferred procedure appears in amber when it is not completed and in white when it is completed.

Answer

The deferred procedure appears in amber when it is not completed and in blue when it is completed.

Answer

The deferred procedure appears in blue when it is not completed and in white when it is completed.

Answer

The deferred procedure appears in blue when it is not completed and in grey when it is completed.

Question 9

Select the correct statement about the hydraulic system:

Accepted Answer

Each hydraulic system has a reservoir located on the rear wing fuselage fairing.

Answer

There is an hydraulic reservoir located on each engine nacelle that supplies hydraulic fluid to both hydraulic systems.

Answer

There is an hydraulic fluid reservoir shared by both hydraulic systems, situated on the central wing-fuselage-fairing.

Answer

Each hydraulic system has two reservoirs, one located on each side of the wing, on the rear wing-fuselage- fairing.

Question 10

When a fault light appears in the hot air pb:

Accepted Answer

The hot air valve is failed or an overheat is detected in the corresponding duct.

Answer

This is the normal indication in flight.

Answer

There is nothing to perform, the FAULT LIGHT will be displayed until the end of the flight.

Answer

The hot air valve has been manually closed.

Question 11

During an automatic starting sequence, if the engine does not light up, the FADEC automatically:

Accepted Answer

Turns off the ignition and shuts off the fuel.

Answer

Aborts the starting sequence and turns off all the engines.

Answer

Adjusts the propeller speed by controlling the engine fuel flow.

Answer

Starts the opposite engine next.

Question 12

The sidesticks are spring loaded to neutral. Do they receive any feedback from the control surfaces?

Accepted Answer

No, the sidesticks never receive feedback.

Answer

Yes, the sidesticks receive feedback in all stages of flight.

Answer

Yes, but only in alternate and direct law.

Answer

Yes, but only in electrical backup.

Question 13

It is possible to reset an application hosted on a CPIOM from the cockpit thanks to the:

Accepted Answer

Reset panels.

Answer

NSS panels.

Answer

ELEC panel.

Answer

PMAT.

Question 14

Which are the functionalities of the flight controls system of the A400M?

Accepted Answer

In flight manoeuvring, lift control and air braking.

Answer

Lift control and air braking only.

Answer

In flight manoeuvring only.

Answer

In flight manoeuvring and lift control.

Question 15

The navaids

Accepted Answer

Are automatically tuned by the FMS and can be tuned manually.

Answer

Are automatically tuned by the AFS.

Answer

Are automatically tuned by the GADIRS.

Answer

Are automatically tuned by the FMS and can not be tuned manually.

Question 16

The JETTISON page of the FUEL format enables the flight crew:

Accepted Answer

To prepare and monitor jettisoning.

Answer

To activate the jettisoning.

Answer

To defuel on the ground.

Answer

To prepare, activate and monitor jettisoning.

Question 17

The manoeuvre load alleviation deflects the ailerons:

Accepted Answer

Upwards in order to reduce the wing bending moments during high load factors manoeuvres.

Answer

Downwards in order to reduce the wing bending moments during low load factors manoeuvres.

Answer

Downwards in order to reduce the wing bending moments during high load factors manoeuvres.

Answer

Upwards in order to increase the wing bending moments during high load factors manoeuvres.

Question 18

How many fire test pushbuttons are in the A400M?

Accepted Answer

Two, one for the engines and the MLG bays and one for the APU.

Answer

Three, one for the engines, one for the MLG bays and one for the APU.

Answer

One for the engines.

Answer

Two, one for the engines and one for the APU.

Question 19

The Battery Charger Rectifier Units (TRs):

Accepted Answer

Transform 115 V AC power into regulated 28 V DC power.

Answer

Transform 28 V DC power into regulated 115 V AC power.

Answer

Transform 115 V AC power into 230 V AC power.

Answer

Transform 230 V AC power into 115 V AC power.

Question 20

The V/UHFs and HFs settings can be modified through:

Accepted Answer

The RMP and the COM format.

Answer

The Audio Control Panel and the Audio Mode Panel.

Answer

The Audio Control Panel.

Answer

The Radio Management Panel and the ECAM Panel.

Question 21

The avionics network includes:

Accepted Answer

Switches, links and devices

Answer

Only links

Answer

Only switches

Answer

Only devices

Question 22

The avionic network switches:

Accepted Answer

Receive data, check their integrity and transmit them to their appropriate addressees.

Answer

Only receive data.

Answer

Transmit and then receive data.

Answer

Only transmit data.

Question 23

AFS 4.1: The AUTO FLT CTL PNL FAULT alert advises the flight crew that the following systems are lost:

Accepted Answer

AP’s, FD’s, A/THR and AFS CTL PNL

Answer

AP’s and FD’s only

Answer

AP's only

Answer

HUD and PFD

Question 24

AFS 4.2: Which of the next modes is a selected lateral guidances mode?

Accepted Answer

Track.

Answer

FMS Localizer (F-LOC).

Answer

Navigation (NAV).

Answer

Localizer (LOC).

Question 25

AFS 5.1: In case of loss of A/THR on two engines

Accepted Answer

The flight crew has to control manually the four engines via the thrust levers.

Answer

An alert reminds the flight crew to disconnect the AP.

Answer

The flight crew has to manually adjust the power of these two engines only.

Answer

The A/THR is still available on the other two engines.

Question 26

AFS 5.2: Which of the next modes is a selected vertical guidance mode?

Accepted Answer

Flight Path Angle (FPA)

Answer

FMS Glide Slope (F-G/S)

Answer

Speed Reference System (SRS)

Answer

Glide Slope (G/S)

Question 27

AFS 7: Which PRIM has the priority to operate and manage the autothrust (A/THR)?

Accepted Answer

Master PRIM

Answer

PRIM 3

Answer

PRIM 1

Answer

PRIM 2

Question 28

AFS 8.1: Which of the next conditions for the autopilot engagements is correct?

Accepted Answer

The aircraft attitude and speed are within limits defined for autopilot engagement.

Answer

The aircraft speed is over 250 kt.

Answer

The aircraft in flight is less than 5 sec.

Answer

The aircraft altitude is above 1500 ft.

Question 29

AFS 8.2: The first line of the FMA is dedicated to:

Accepted Answer

Active guidance modes.

Answer

Armed guidance mode.

Answer

Messages.

Answer

Status of the guidance systems engagement.

Question 30

FG 4: The active leg is referred to: The leg between the … waypoint and the … waypoint.

Accepted Answer

FROM/TO

Answer

PPOS/NEXT

Answer

TO/NEXT

Answer

FROM/PPOS

Nächster

10. OS 1

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	Erstellt von Jose Antonio Vazquez vor etwa 3 Jahre