The MIL GPS part receives data from:
Two integrated standby probes.
Three MIL pattern antennas.
The multi functional probes.
Two CIV/GPS antennas.
According to the illustration, if the CM1 presses the takeover pb:
The CM2 reactivates his sidestick.
The CM1 is unable to reactivate his sidestick.
The CM2 is unable to reactivate his sidestick.
The CM1 reactivates his sidestick.
When the ‘B’ or ‘Y’ indication on the wheel SD is amber, it means that:
The accumulator pressure is too high.
The braking system is faulty.
The ‘B’ or ‘Y’ hydraulic pressure is low.
The ‘B’ or ‘Y’ hydraulic pressure is available.
The transfer network:
Has one inlet valve in each INR TK.
Has two inlet valves, two transfer pumps and two alternate transfer pumps in each INR TK.
Has one inlet valve and two pumps in each feed tank.
Has one inlet valve in each FEED TK and two transfer pumps in the INR TKs.
The A400M power plant has one FADEC. Select the true statement:
The A400M has one FADEC control lever per engine.
Each FADEC controls, protects and monitors the engine.
The FADEC is in charge of the power plant indications displayed on the LMWS.
The flight crew normally interface with the FADEC using the FADEC GrouND PoWeR (GND PWR) pb-sw.
According to the illustration identify the status of the TAWS system:
The normal TAWS is selected and operative.
The TERR alerts are inhibited.
The system is failed.
The G/S mode is failed.
During a manual starting sequence, the FADEC:
Starts the engine when the ignition is manually activated.
Defeathers the propellers in order to save time.
Provides passive monitoring of the starting sequence.
Starts the opposite engine.
In accordance with the illustration, identify the status of the TAWS system:
The system is operative and alerts the crew to increase the sink rate.
The system is operative and warns that the aircraft is 30s or less away from conflict terrain.
The system is operative and warns that the aircraft is 30 min or less away from conflict terrain.
In flight, the APU:
Is normally fed by the main pump or the FEED TK 1.
Is normally fed by the main pump of the FEED TK 3.
Is normally fed by its own APU fuel pump.
Is normally fed by gravity.
The inerting system:
Does not provide an indication of the time required to inert the TKs.
Also protects the CHTs.
Is activated manually via the inerting pb-sw.
Is activated automatically by the FQMS.
The TURB function detects:
The intensity of the wingtip vortices and the wake turbulence produced by the aircraft.
Malfunctions or anomalous gas flow in the turbines of any engine.
Wet turbulence using movements of the precipitations ahead of the aircraft.
Both wet turbulence and clear air turbulence.
With reference to a checklist, which statement is correct?
A checklist is a reminder of abnormal operations that can be performed only during flight.
A checklist is a reminder of abnormal operations that can be performed at a more appropriate time.
A checklist is a reminder of normal operations that must be performed in a specific flight phase.
A checklist is a reminder of normal operations that can be performed at any time during the flight.
The takeoff and landing memos appear on the left column of the EWD. How is each item of these memos displayed?
It always appears green. Some limitations can also appear in blue in this column.
It appears in green when the applicable action is not yet performed and in blue when the applicable action is performed.
It appears in green when the applicable action is performed and in blue when the applicable action is not yet performed.
It always appears in blue.
According to the EWD illustration, what does the green arrow indicate?
It indicates an overflow state above/below.
It indicates the end of the procedure.
It indicates an overflow state above.
It indicates an overflow state below.
Select the true statement:
The pump symbol is a circle.
The valve system is a square.
The degraded data information consists of two amber crosses.
The system availability is indicated by the colour of the triangle.
The inner ring selector enables the modification of (picture of the DU turn knob shown):
The zoom of the NTD.
The mode of display of the NTD.
The background of the NTD.
The range on the NTD.
Each KCCU can display a different cursor on the SD/mailbox at the same time. Which is the correct statement for this situation?
The amber cursor is active as the yellow cursor is not on the screen and thus cannot interact with the mailbox.
The yellow cursor is active. That corresponds to the CM that has given the last interaction on the mailbox.
Both cursors are active.
The yellow cursor is active. That corresponds to the CM that has given the first interaction on the mailbox.
If a given format currently displayed on a cockpit side is called on another DU on the same cockpit side:
The called format does not appear in any DU.
The called format appears twice in the same cockpit side.
Both formats automatically swap.
There is no change.
What is a management format?
A management format is a format that can be displayed on the LMWS.
A management format is an interactive display that enables flights crew to monitor and control aircraft systems.
A management format is a frozen display that enables the flight crew to monitor aircraft systems.
A management format is any format displayed on the ECAM.
What is the function of the DCP?
It enables the selection of different ECAM formats on any DU.
It enables the configuration of its corresponding display unit via different menus.
It enables the selection of the different management formats in the HUD.
It enables the tuning of the communication means.
What is the main function of the ECAM formats?
The ECAM formats help to manage and monitor aircraft systems during both normal and abnormal operations.
The ECAM formats display the flight and navigation displays.
They enable the monitoring of the engine parameters only during the starting phase.
The ECAM formats enable the flight crew to monitor navigation displays.
Select the correct statement on displays:
The green colour emphasises the emergency status of an indication.
The green colour emphasises the normal status of an indication.
The green colour emphasises the abnormal status of an indication.
The green colour emphasises that the flight crew has to perform an action.
Which is the objective of the Flight Guidance System of the Automatic Flight System?
To provide lateral and vertical guidance, and speed/Mach control based on targets.
To protect the aircraft against external environmental hazards, and propose evasive manoeuvres to the flight crew.
To help the flight crew in the management of the flight profile.
To enhance safety by preventing the a/c from exiting the flight envelope.
About the master FMS, which of the next sentences is not true?
If AP 2 is engaged FMS 2 is the master.
The FMS master selection is associated to AP engagement.
If no AP or AP 1 is engaged the FMS 1 is master.
The FMS master selection is not associated with AP engagement.
Which of the next sensors is not authorized for civil navigation (CIV NAV)?
CIV GPS/WAAS-EGNOS.
The navaids.
Terrain Reference Navigation (TRN).
IRS
Which are the three main functions included in the Automatic Flight System?
Flight Envelope, Flight Guidance and Flight Management functions.
Flight Guidance, Aircraft Maintenance Data and Flight Surveillance functions.
Flight Management, Emergency Management and Tactical Management functions.
Flight Coordination, Flight Diversion and Aircraft Operational Data functions.
When the flight crew sets the thrust levers to TOGA or MCL/MCT detent:
The A/THR must be armed manually.
The Speed Reference System (SRS) mode engages provided V1 speed is inserted in the FMS PERF page and the flaps are extended.
The Speed Reference System (SRS) mode engages provided V2 speed is inserted in the FMS PERF page and the flaps are extended.
The Speed Reference System (SRS) mode engages, even if the takeoff speeds are not inserted in the FMS PERF page and the flaps are retracted.
In case of FMS 1 failure:
The FMS 2 only provides information to the CM2.
The FMS 2 automatically supplies the CM1 and CM2 sides.
FMS information is lost for both CM.
The ECAM procedure requests the flight crew to set the FMS source selector to the ALL ON 2 position in order for the FMS 2 to supply both CM1 and CM2.
Which of the following systems is a guidance system?
The IFF.
The Flight Director.
The direction finder.
The military radar.
Complete the sentence. On the A400M, the engagement of the AP:
Is automatic, except when the ac is on the ground.
Is always possible on the ground.
Is always manual.
Is automatic, except in emergency situations.
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