Which speed is displayed as the top of a strip on the speed scale of the HUD and the PFD?
VFE next speed.
Green dot speed.
VLS speed.
VMAX speed.
What are the main functions of the NORM TAWS system?
The Enhanced Vision System (EVS) and the Tactical Terrain Awareness and Display (T-TAD).
The Ground Proximity Warning System (GPWS), the Terrain Clearance Floor (TCF) and the Terrain(TERR) and obstacles.
The databases and DMAP information.
Only the Ground Proximity Warning System (GPWS).
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)
Which Primary (PRIM) computer has the priority to manage the flight envelope (FE) function?
The PRIM 3.
The PRIM 2.
The PRIM 1.
The master PRIM.
On the NTD format, the colour of any SEC F-PLN is:
Yellow
White
Blue
Green
When a system fails, the ECAM may display some deferred procedures. They are displayed on the:
Loadmaster Workstation display.
Tactical checklist menu.
Abnormal checklist menu.
Normal checklist menu.
Select the correct statement:
The NTD provides only long term information.
The NTD is used for aircraft position attitude.
The NTD provides lateral and vertical navigation information, according to the flight plan, the navigation database and tactical data.
The NTD provides only short term information.
When a system fails, the ECAM may display some deferred procedures in the C/L menu page. What is the correct statement?
The deferred procedure appears in amber when it is not completed and in white when it is completed.
The deferred procedure appears in amber when it is not completed and in blue when it is completed.
The deferred procedure appears in blue when it is not completed and in white when it is completed.
The deferred procedure appears in blue when it is not completed and in grey when it is completed.
Select the correct statement about the hydraulic system:
Each hydraulic system has a reservoir located on the rear wing fuselage fairing.
There is an hydraulic reservoir located on each engine nacelle that supplies hydraulic fluid to both hydraulic systems.
There is an hydraulic fluid reservoir shared by both hydraulic systems, situated on the central wing-fuselage-fairing.
Each hydraulic system has two reservoirs, one located on each side of the wing, on the rear wing-fuselage- fairing.
When a fault light appears in the hot air pb:
The hot air valve is failed or an overheat is detected in the corresponding duct.
This is the normal indication in flight.
There is nothing to perform, the FAULT LIGHT will be displayed until the end of the flight.
The hot air valve has been manually closed.
During an automatic starting sequence, if the engine does not light up, the FADEC automatically:
Aborts the starting sequence and turns off all the engines.
Turns off the ignition and shuts off the fuel.
Adjusts the propeller speed by controlling the engine fuel flow.
Starts the opposite engine next.
The sidesticks are spring loaded to neutral. Do they receive any feedback from the control surfaces?
Yes, the sidesticks receive feedback in all stages of flight.
Yes, but only in alternate and direct law.
Yes, but only in electrical backup.
No, the sidesticks never receive feedback.
It is possible to reset an application hosted on a CPIOM from the cockpit thanks to the:
Reset panels.
NSS panels.
ELEC panel.
PMAT.
Which are the functionalities of the flight controls system of the A400M?
Lift control and air braking only.
In flight manoeuvring only.
In flight manoeuvring and lift control.
In flight manoeuvring, lift control and air braking.
The navaids
Are automatically tuned by the AFS.
Are automatically tuned by the FMS and can be tuned manually.
Are automatically tuned by the GADIRS.
Are automatically tuned by the FMS and can not be tuned manually.
The JETTISON page of the FUEL format enables the flight crew:
To activate the jettisoning.
To defuel on the ground.
To prepare and monitor jettisoning.
To prepare, activate and monitor jettisoning.
The manoeuvre load alleviation deflects the ailerons:
Downwards in order to reduce the wing bending moments during low load factors manoeuvres.
Upwards in order to reduce the wing bending moments during high load factors manoeuvres.
Downwards in order to reduce the wing bending moments during high load factors manoeuvres.
Upwards in order to increase the wing bending moments during high load factors manoeuvres.
How many fire test pushbuttons are in the A400M?
Three, one for the engines, one for the MLG bays and one for the APU.
Two, one for the engines and the MLG bays and one for the APU.
One for the engines.
Two, one for the engines and one for the APU.
The Battery Charger Rectifier Units (TRs):
Transform 115 V AC power into regulated 28 V DC power.
Transform 28 V DC power into regulated 115 V AC power.
Transform 115 V AC power into 230 V AC power.
Transform 230 V AC power into 115 V AC power.
The V/UHFs and HFs settings can be modified through:
The RMP and the COM format.
The Audio Control Panel and the Audio Mode Panel.
The Audio Control Panel.
The Radio Management Panel and the ECAM Panel.
The avionics network includes:
Only links
Only switches
Only devices
Switches, links and devices
The avionic network switches:
Only receive data.
Receive data, check their integrity and transmit them to their appropriate addressees.
Transmit and then receive data.
Only transmit data.
AFS 4.1: The AUTO FLT CTL PNL FAULT alert advises the flight crew that the following systems are lost:
AP’s and FD’s only
AP's only
AP’s, FD’s, A/THR and AFS CTL PNL
HUD and PFD
AFS 4.2: Which of the next modes is a selected lateral guidances mode?
FMS Localizer (F-LOC).
Track.
Navigation (NAV).
Localizer (LOC).
AFS 5.1: In case of loss of A/THR on two engines
An alert reminds the flight crew to disconnect the AP.
The flight crew has to manually adjust the power of these two engines only.
The A/THR is still available on the other two engines.
The flight crew has to control manually the four engines via the thrust levers.
AFS 5.2: Which of the next modes is a selected vertical guidance mode?
FMS Glide Slope (F-G/S)
Speed Reference System (SRS)
Flight Path Angle (FPA)
Glide Slope (G/S)
AFS 7: Which PRIM has the priority to operate and manage the autothrust (A/THR)?
PRIM 3
PRIM 1
Master PRIM
PRIM 2
AFS 8.1: Which of the next conditions for the autopilot engagements is correct?
The aircraft attitude and speed are within limits defined for autopilot engagement.
The aircraft speed is over 250 kt.
The aircraft in flight is less than 5 sec.
The aircraft altitude is above 1500 ft.
AFS 8.2: The first line of the FMA is dedicated to:
Active guidance modes.
Armed guidance mode.
Messages.
Status of the guidance systems engagement.
FG 4: The active leg is referred to: The leg between the … waypoint and the … waypoint.
FROM/TO
PPOS/NEXT
TO/NEXT
FROM/PPOS
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