What is NOT true regarding the Hot Air Valves:
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.
A30-012 Mark the WRONG statement about the Cockpit Windows Anti-Ice and Defogging System Architecture.
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.
A30-005 When can the flight crew activate the windshield rain removal system? Mark the INCORRECT one.
a. During approach
b. During take off
c. During taxi
d. Always
A35-004 About the protective crew oxygen bottles, choose the most correct answer:
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.
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.
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)
A26-013 When the crew presses the FIRE pb-sw.
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.
A34-020 The aircraft time reference:
a. Is GPS time
b. Is inserted manually
c. Is sincronized with HF stations
d. a and b
A34-034 Each RA system has:
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.
A34-023 Each GADIRU has its own set of probes, sensors, antennas except for:
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
A33-006 Each flight crew station has (Select the FALSE):
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.
A33-005 The storm function enables the flight crew to obtain maximum lighting in the cockpit, via (Select the FALSE):
a. The console lights
b. The pedestal flood light
c. The dome lights
d. The main instrument panel flood lights
A31-047 Regarding the following picture IN NORMAL LAW, the number 2 in the box corresponds to:
a. Vα max
b. Vα sw
c. Vα prot
d. VLS
A31-058 DMAP Media Insertion, select the WRONG answer:
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.
A31-041 The airspeed target is in managed mode (the FMS computes the airspeed target).
Verdadero
Falso
A31-050 Regarding the following picture:
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.
A29-013 Related to the hydraulic systems, select the FALSE sentence:
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.
A29-010 Select the correct sentence related to the hydraulic operations before engine start:
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.
About the Cockpit Voice Recorder (CVR), choose the WRONG answer:
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.
The communications recording is ensured by the Digital Flight Data Recording System (DFDRS).
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.
A31-026 The common message area displays the following information
A25-005 Which is the function of this T-handle?
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
A90-006 The Military Mission Management System (M-MMS) provides the following CLM functions:
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.
A24-022 230V AC CONVERTER PB-SW:
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.
A24-023 Ground Power Panel:
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.
A24-027 RESET Panels:
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
A27-002 The fly-by-wire system advantages over conventional systems are to (Choose the wrong answer)
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
A27-053 What system provides data to the PRIMs?
a. GADIRUs
b. FMS
c. Ice Detection
d. ISIS
A27-043 In flare mode, the pitch control is a direct relationship between the sidestick inputs and the elevator.
A27-026 Regarding the flap load relief function: (Choose the wrong answer)
a. If the aircraft keeps accelerating, flaps may retract fully.
b. The flaps automatically retract to the next retracted flaps configuration.
c. The automatic retraction can occur slightly before reaching VFE.
d. A pulsing F RELIEF message appears in the flap zone of the EWD
A27-055 SEC has two dedicated gyrometers:
Por favor, aguarde! Carregando...