1.2. A4 YM21

Question 1 of 30

1

What is NOT true regarding the Hot Air Valves:

Select one of the following:

a. In normal situation, hot bleed air is added to the air coming from the mix air unit in order to regulate the temperature.
b. The hot air valves control the flow of hot bleed air to the temperature regulating system.
c. There are two hot air valves on the A400M, one associated to each air conditioning pack.
d. None of the other options is correct.

Explanation

Question 2 of 30

1

A30-012 Mark the WRONG statement about the Cockpit Windows Anti-Ice and Defogging System Architecture.

Select one of the following:

a. All cockpit windows are defogged.
b. Left and right side windshield are fully segregated for redundancy.
c. Defogging and deicing is done using electrical heaters.
d. Middle left and right cockpit windows are not protected to allow their movement.

Explanation

Question 3 of 30

1

A30-005 When can the flight crew activate the windshield rain removal system? Mark the INCORRECT one.

Select one of the following:

a. During approach
b. During take off
c. During taxi
d. Always

Explanation

Question 4 of 30

1

A35-004 About the protective crew oxygen bottles, choose the most correct answer:

Select one of the following:

a. The pressure value is continuously indicated in the DOOR/CARGO/OXYGEN SD.
b. The pressure value can be checked through a window from outside of the aircraft fuselage.
c. From two to four high pressure oxygen bottles can be installed in the left side of the aircraft.
d. From one to four high pressure oxygen bottles can be installed in the right side of the aircraft.

Explanation

Question 5 of 30

1

A56-004 What is the name of the system in charge of monitoring and controlling all fuselage doors, emergency exits, and peripherals of the aircraft.

Select one of the following:

a. The Doors Control and Monitoring System (DCMS)
b. The Door Control and Monitoring Unit (DCMU)
c. The Ramp and Cargo Door Controller (RCDC)
d. The Autonomous Standby Power Supply Unit (ASPSU)

Explanation

Question 6 of 30

1

A26-013 When the crew presses the FIRE pb-sw.

Select one of the following:

a. The corresponding fire extinguishing system arms.
b. The associated fuel, pneumatic and hydraulic valves close.
c. The propeller feathers.
d. All of the above.

Explanation

Question 7 of 30

1

A34-020 The aircraft time reference:

Select one of the following:

a. Is GPS time
b. Is inserted manually
c. Is sincronized with HF stations
d. a and b

Explanation

Question 8 of 30

1

A34-034 Each RA system has:

Select one of the following:

a. one transceiver, one antenna (transmission+reception).
b. two transceiver, two antenna (transmission+reception).
c. one transceiver, one transmission antenna, one reception antenna.
d. two transceiver, two transmission antenna, two reception antenna.

Explanation

Question 9 of 30

1

A34-023 Each GADIRU has its own set of probes, sensors, antennas except for:

Select one of the following:

a. GADIRU 1 and 3 share OAT 1 and GADIRU 2 has OAT 2 dedicated.
b. GADIRU 1 and 2 share OAT 1 and GADIRU 3 has OAT 3 dedicated
c. Each GADIRU has its own dedicated OAT input.
d. GADIRU 2 and 3 share OAT 2 and GADIRU 1 has OAT 1 dedicated

Explanation

Question 10 of 30

1

A33-006 Each flight crew station has (Select the FALSE):

Select one of the following:

a. Crew rest area lights.
b. Briefcase lights.
c. Console lights. The console light provides the console, the sidestick, and the nosewheel steering with lighting.
d. Floor lights. These lights are located under the seats, and provide lighting for the surrounding floor.

Explanation

Question 11 of 30

1

A33-005 The storm function enables the flight crew to obtain maximum lighting in the cockpit, via (Select the FALSE):

Select one of the following:

a. The console lights
b. The pedestal flood light
c. The dome lights
d. The main instrument panel flood lights

Explanation

Question 12 of 30

1

A31-047 Regarding the following picture IN NORMAL LAW, the number 2 in the box corresponds to:

Select one of the following:

a. Vα max
b. Vα sw
c. Vα prot
d. VLS

Explanation

Question 13 of 30

1

A31-058 DMAP Media Insertion, select the WRONG answer:

Select one of the following:

a. The flight crew can insert the DMAP media into the front face of the DMGC at any time when the aircraft is on ground.
b. The flight crew can insert the DMAP media into the front face of the DMGC at any time when the aircraft is in flight.
c. When the flight crew inserts the DMAP media in the DMGC, the DMGC doesn't check the validity of the database stored on the DMAP media.
d. When the DMAP uploading is successfully achieved:
‐ The green light on the front face of the DMGC remains steady
‐ The DMAP background is normally displayed on the NTD when selected on the DCP.

Explanation

Question 14 of 30

1

A31-041 The airspeed target is in managed mode (the FMS computes the airspeed target).

Select one of the following:

Verdadero
Falso

Explanation

Question 15 of 30

1

A31-050 Regarding the following picture:

Select one of the following:

a. Indicates an altitude constraint when the vertical guidance is managed.
The altitude constraint is out of the altitude scale.
b. Indicates the altitude constraint when the vertical guidance is managed.
The altitude constraint is within the altitude scale.
c. Indicates the AFS CP selected altitude when the vertical guidance is either selected or managed.
The altitude target is within the altitude scale.
d. Indicates the AFS CP selected altitude when the vertical guidance is either selected or managed.
The altitude target is out of the altitude scale.

Explanation

Question 16 of 30

1

A29-013 Related to the hydraulic systems, select the FALSE sentence:

Select one of the following:

a. If a low pressure is detected on both hydraulic systems, the corresponding caution appears on the EWD together with the aural and visual alerts.
b. Thanks to architectural redundancy and despite of some systems lost, all main functions are still available if a Hydraulic system is lost.
c. The hydraulic valves temporarily increase the hydraulic flow to non-essential consumers, and eventually isolate them if the system pressure drops under a certain threshold.
d. If pump performance is reduced, each hydraulic power system has a priority valve that secures the operation of the primary flight controls and brakes.

Explanation

Question 17 of 30

1

A29-010 Select the correct sentence related to the hydraulic operations before engine start:

Select one of the following:

a. For maintenance operations, the ELEC PMPs can supply all the hydraulic circuits.
b. All of the above.
c. The crew can use DRAS and kneeling capability thanks to BLUE or YELLOW ELEC PMPs.
d. As soon as hydraulic power is required, the corresponding ELEC PMP automatically activates to pressurize the related components.

Explanation

Question 18 of 30

1

About the Cockpit Voice Recorder (CVR), choose the WRONG answer:

Select one of the following:

a. The TEST pb enables to test the CVR.
b. The TEST pb enables to record a mark in the CVR recording for further investigation.
c. The BOOMSET jack enables to plug a headset in order to hear what is recorded on the CVR.
d. The GND ERASURE sw enables to erase all the audio recorded data, only if the aircraft is on ground and parking brake is ON.

Explanation

Question 19 of 30

1

The communications recording is ensured by the Digital Flight Data Recording System (DFDRS).

Select one of the following:

a. Among others, it record parameters related to aircraft position, secure communications, crypto keys and DASS parameters.
b. The DFDRS is in the front part of the aircraft.
c. The Digital Flight Data Recording System (DFDRS) records all the mission parameters.
d. The DFDRS stores the parameters of the last 25 hours of operation in a crash protected box. This box has also an underwater locator beacon.

Explanation

Question 20 of 30

1

A31-026 The common message area displays the following information

Select one of the following:

Verdadero
Falso

Explanation

Question 21 of 30

1

A25-005 Which is the function of this T-handle?

Select one of the following:

a. Deploys the emergency rafts
b. Opens the paratroop doors for evacuation
c. Enables to open the aft ditching hatch and arms the evacuation ladder system
d. Enables to deploy the evacuation ladder

Explanation

Question 22 of 30

1

A90-006 The Military Mission Management System (M-MMS) provides the following CLM functions:

Select one of the following:

a. Weight and CG calculation
b. Optimum load position computation
c. Consistency check of LMWS entries (configuration, limitations).
d. All the other options plus Cargo data storage and CLP preparation and edition.

Explanation

Question 23 of 30

1

A24-022 230V AC CONVERTER PB-SW:

Select one of the following:

a. enables to switch ON/OFF the converters that supply power to the cargo hold.
b. enables to switch ON/OFF the converter that supplies power to the cockpit.
c. enables to switch ON/OFF the converter that supplies power to the LMWS.
d. b and c.

Explanation

Question 24 of 30

1

A24-023 Ground Power Panel:

Select one of the following:

a. There are three lights related to the EXT PWR on the ground power panel.
b. External Power NOT IN USE indicates that the external power unit is not connected to the aircraft.
c. External Power AVAIL light indicates that external power is plugged and is available to supply to the electrical network. Voltage and frequency are normal.
d. all of the above are false.

Explanation

Question 25 of 30

1

A24-027 RESET Panels:

Select one of the following:

a. There are TR reset buttons on the overhead reset panels
b. There are GCU reset buttons on the overhead reset panels
c. Information about reset panels can be found in FCOM Supplementary Procedures
d. All the above

Explanation

Question 26 of 30

1

A27-002 The fly-by-wire system advantages over conventional systems are to (Choose the wrong answer)

Select one of the following:

a. Limit dependence on pilot skills.
b. Reduce pilot workload when flying manually
c. Provide aircraft flight envelope protections that enhance safety
d. Reduce aircraft weight

Explanation

Question 27 of 30

1

A27-053 What system provides data to the PRIMs?

Select one of the following:

a. GADIRUs
b. FMS
c. Ice Detection
d. ISIS

Explanation

Question 28 of 30

1

	Created by Jose Antonio Vazquez almost 3 years ago

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1.2. A4 YM21

Question 1 of 30

What is NOT true regarding the Hot Air Valves:

Select one of the following:

Explanation

Question 2 of 30

A30-012 Mark the WRONG statement about the Cockpit Windows Anti-Ice and Defogging System Architecture.

Select one of the following:

Explanation

Question 3 of 30

A30-005 When can the flight crew activate the windshield rain removal system? Mark the INCORRECT one.

Select one of the following:

Explanation

Question 4 of 30

A35-004 About the protective crew oxygen bottles, choose the most correct answer:

Select one of the following:

Explanation

Question 5 of 30

A56-004 What is the name of the system in charge of monitoring and controlling all fuselage doors, emergency exits, and peripherals of the aircraft.

Select one of the following:

Explanation

Question 6 of 30

A26-013 When the crew presses the FIRE pb-sw.

Select one of the following:

Explanation

Question 7 of 30

A34-020 The aircraft time reference:

Select one of the following:

Explanation

Question 8 of 30

A34-034 Each RA system has:

Select one of the following:

Explanation

Question 9 of 30

A34-023 Each GADIRU has its own set of probes, sensors, antennas except for:

Select one of the following:

Explanation

Question 10 of 30

A33-006 Each flight crew station has (Select the FALSE):

Select one of the following:

Explanation

Question 11 of 30

A33-005 The storm function enables the flight crew to obtain maximum lighting in the cockpit, via (Select the FALSE):

Select one of the following:

Explanation

Question 12 of 30

A31-047 Regarding the following picture IN NORMAL LAW, the number 2 in the box corresponds to:

Select one of the following:

Explanation

Question 13 of 30

A31-058 DMAP Media Insertion, select the WRONG answer:

Select one of the following:

Explanation

Question 14 of 30

A31-041 The airspeed target is in managed mode (the FMS computes the airspeed target).

Select one of the following:

Explanation

Question 15 of 30

A31-050 Regarding the following picture:

Select one of the following:

Explanation

Question 16 of 30

A29-013 Related to the hydraulic systems, select the FALSE sentence:

Select one of the following:

Explanation

Question 17 of 30

A29-010 Select the correct sentence related to the hydraulic operations before engine start:

Select one of the following:

Explanation

Question 18 of 30

About the Cockpit Voice Recorder (CVR), choose the WRONG answer:

Select one of the following:

Explanation

Question 19 of 30

The communications recording is ensured by the Digital Flight Data Recording System (DFDRS).

Select one of the following:

Explanation

Question 20 of 30

A31-026 The common message area displays the following information