Which Panelis highlighted in the image above?
Pedestal
Lateral
Overhead
Main instrument
Which Panel is highlighted in the image above?
Landing Gear
Flaps
Which number indicates the location of the LMWS?
1
2
3
4
What is the passenger capacity of the A400M?
106 Paratroops
116 Paratroops
126 Paratroops
76 Paratroops
Select the true statement:
Each color emphasizes an indication, and enables the flight crew to interpret rapidly the status and/or the importance of the information provided.
The same color can not be used for different types and status of information.
The important indications are displayed in colors to be easier to read.
Indications are randomly displayed in different colors.
What does the Electronic Centralized Aircraft Monitoring (ECAM) display after a primary failure has been cleared?
It automatically displays the AFTER TAKEOFF checklist.
It always displays the ENGINE SD page.
It shows the systems affected by the primary failure.
It automatically displays the CRUISE page.
How does the pilot acknowledge an alert?
By using the Passenger Address (PA).
By pressing the MASTER WARN pb or MASTER CAUT pb, depending on the alert.
By checking the alert in the Electronic Centralized Aircraft Monitoring (ECAM).
By changing the state of the alert on the Display Units (DUs).
Which alert is displayed on the Electronic Centralized Aircraft Monitoring (ECAM)?
A warning alert for the PRIM1 computer of the Flight Control System.
A caution alert that the Landing Distance is affected.
A warning alert that the PRIM1 computer of the Flight Control System must be switched off.
A caution alert for the PRIM 1computer of the Flight Control System.
What is the meaning of the blue box in the normal checklist?
The blue box surrounds a delayed alert.
The blue box surrounds the current applicable line.
The blue box surrounds the lines that could be cleared.
The blue box surrounds a caution alert.
When an action of the ElectronicCentralizedAircraftMonitoring (ECAM) is completed... (not a C/L)
The indications change from blue to green.
The indications change from blue to white.
The indications are surrounded by a blue box.
The indications are surrounded by a white box.
Which of the following is not a VIDEO Format
EVS
Air to Air Refueling
Cargo
Fuel
Which of the following formats does not have sub menus on the DCP
NTD 1
PFD
VIDEO
NTD 2
The APU generator provides:
115V DC at constant frequency 400 Hz
115V AC at variable frequency between 390 Hz to 620 Hz
115V AC at constant frequency 400 Hz
115V DC at variable frequency between 390 Hz to 620 Hz
Which function protects the system at Busbar level and high loads level (level 2)
Bus Tie Function
Electrical Load Management Function (ELMF)
Generator and Ground PowerControl Function
Electrical Network ManagementFunction (ENMF)
In flight with Engines 1 and 2 shut down and the APU not running (Bus Tie Normal) select the correct statement:
AC 4 powers AC 1 and AC 3 powers AC 2
AC 4 powers AC 2 and AC 3 powers AC 1
AC 4 powers AC 3 and AC 2 powers AC 1
APU powers AC 1 and 2
In flight with Engines 1 and 3 shutdown and the APU not running (Bus Tie Normal) select the correct statement:
APU powers AC 1 and 3
AC4 powers AC1 and AC2 powers AC3
AC 2 powers AC 1 and AC 4 powers AC 3
AC4 powers AC3 and APU powers AC1
In normal operation, the master PRIM Computer...:
A Computes only the direct law.
Controls the flight control surfaces only.
Computes the commands and sends them to the other PRIMS and SEC.
Sends feedback to the sidesticks.
The flight maneuvering function:
Provides lift augmentation at low speed.
Enables the control of the aircraft pitch, roll and yaw.
Automatically extends the spoilers at landing or in case of rejected.
Controls the propeller speed and engine fuel consumption.
Select the correct statement:
The pitch function is provided by the ailerons only.
The pitch function is provided by the ailerons and the spoilers.
The pitch function is provided by the rudder.
The pitch function is provided by the elevators and the trimmable horizontal stabilizer.
The rudder controls the aircraft on the yaw axis.
The flaps control the aircraft on the yaw axis.
The elevators control the aircraft on the yaw axis.
The trimmable horizontal stabilizer controls the aircraft on the yaw axis.
Select the correct statement about the hydraulic system:
The aircraft has two separate and independent hydraulic systems referred to as AMBER and GREEN.
The aircraft has two separate and independent hydraulic systems referred to as BLUE and YELLOW.
The aircraft has two separate and independent hydraulic systems referred to as RIGHT and LEFT.
The aircraft has three redundant and connected hydraulic systems referred as RIGHT, CENTER and LEFT.
The essential users are ailerons, spoilers, flaps, elevator and trimmable horizontal stabilizer, rudder and brakes. Select the correct statement:?
The hydraulic supply of each essential user is shared out between BLUE and YELLOW systems.
The hydraulic supply is provided by BLUE system to the essential users on the left side of the plane and by the YELLOW system to the essential users on the right side.
The hydraulic supply is provided by BLUE system to the essential users on the right side of the plane and by the YELLOW system to the essential users on theleft side.
The YELLOW system supplies hydraulic power only to the rudder, elevator and trimmable horizontal stabilizer.
What does the situation display on the picture mean?
The yellow electrical pump is running and the light disappears when the pump stops.
The blue electrical pump is running and still the light ON when the pump stops.
The blue electrical pump is running and the pb lights on when the pump stops.
The engine pumps 3 and 4 are running. The hydraulic indication is not display on the SD.
The hydraulic engine pumps operate continuously and automatically while the associated engine isswitch off.
When an engine is running, the associated electrical pump operates continuously and automatically.
The hydraulic engine pumps operate continuously and automatically while the associated engine is running.
When all the engines are switch off, the electrical pumps are inhibited by the Hydraulic System.
The CIV GPS part receives data from:
A multi function probe.
Three MIL Pattern Antennas.
Two integrated standby probes.
Two CIV GPS antennas.
Which parameters are computed by the Air Data Reference and are both displayed on the PFD and the HUD?
The wind direction and the heading.
The airspeed and the g load.
The side slip angle and the angle of attack.
The attitude and altitude.
Complete the sentence. The standby magnetic compass... :
Provides the aircraft true heading to the GADIRU2.
Is linked with the standby Pitot probe.
Is located on top of the windshield center post.
Provides to the flight crew an independent aircraft true heading.
An interrupted alignment function enables the flight crew to move the aircraft after only 2 minutes of alignment, but...:
With degraded navigation performance until next aircraft overhaul.
With full navigation performance even if the aircraft is moving.
With degraded navigation performance during 8 minutes.
IRs resumes the complete alignment process as soon as the aircraft stops moving.
Which of the following does not have a PTT to enable transmission on a radio
Sidestick
Thrust Levers
Steering Handwheel
ACP
Select the correct statement regarding the IFF
AUTO, in flight, all modes are operative. On ground, mode 2 and mode S are inhibited.
STBY, the IFF is not powered.
AUTO, in flight, all modes are operative. On ground, mode 3 and mode C are inhibited.
OFF, the IFF is powered but does not reply, except mode 4, theTCASis also in standby.
When COM CTL switch is selected to BACKUP position
V/UHF 1 & 2 can be controlled by all the RMP's.
V/UHF 1 & 2 can be controlled by RMP's and via the COM management format.
V/UHF 1 & 3 can be controlled by RMP's 1 & 2 only.
V/UHF 1 & 2 can be controlled by RMP's 1 & 2 only.
From the image, select the correct statement
CM1 can control their audio settings through ACP 1
CM2 can control their audio settings through ACP 3
CM1 can control their audio settings through ACP 3
CM1 can control their audio settings through ACP 2
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