1.2. A4 YM21

Question

What is NOT true regarding the Hot Air Valves:

Answer 1

a. In normal situation, hot bleed air is added to the air coming from the mix air unit in order to regulate the temperature.

Answer 2

b. The hot air valves control the flow of hot bleed air to the temperature regulating system.

Answer 3

c. There are two hot air valves on the A400M, one associated to each air conditioning pack.

Answer 4

d. None of the other options is correct.

Answer 5

a. All cockpit windows are defogged.

Answer 6

b. Left and right side windshield are fully segregated for redundancy.

Answer 7

c. Defogging and deicing is done using electrical heaters.

Answer 8

d. Middle left and right cockpit windows are not protected to allow their movement.

Answer 9

a. During approach

Answer 10

b. During take off

Answer 11

c. During taxi

Answer 12

a. The pressure value is continuously indicated in the DOOR/CARGO/OXYGEN SD.

Answer 13

b. The pressure value can be checked through a window from outside of the aircraft fuselage.

Answer 14

c. From two to four high pressure oxygen bottles can be installed in the left side of the aircraft.

Answer 15

d. From one to four high pressure oxygen bottles can be installed in the right side of the aircraft.

Answer 16

a. The Doors Control and Monitoring System (DCMS)

Answer 17

b. The Door Control and Monitoring Unit (DCMU)

Answer 18

c. The Ramp and Cargo Door Controller (RCDC)

Answer 19

d. The Autonomous Standby Power Supply Unit (ASPSU)

Answer 20

a. The corresponding fire extinguishing system arms.

Answer 21

b. The associated fuel, pneumatic and hydraulic valves close.

Answer 22

c. The propeller feathers.

Answer 23

d. All of the above.

Answer 24

a. Is GPS time

Answer 25

b. Is inserted manually

Answer 26

c. Is sincronized with HF stations

Answer 27

d. a and b

Answer 28

a. one transceiver, one antenna (transmission+reception).

Answer 29

b. two transceiver, two antenna (transmission+reception).

Answer 30

c. one transceiver, one transmission antenna, one reception antenna.

Answer 31

d. two transceiver, two transmission antenna, two reception antenna.

Answer 32

a. GADIRU 1 and 3 share OAT 1 and GADIRU 2 has OAT 2 dedicated.

Answer 33

b. GADIRU 1 and 2 share OAT 1 and GADIRU 3 has OAT 3 dedicated

Answer 34

c. Each GADIRU has its own dedicated OAT input.

Answer 35

d. GADIRU 2 and 3 share OAT 2 and GADIRU 1 has OAT 1 dedicated

Answer 36

a. Crew rest area lights.

Answer 37

b. Briefcase lights.

Answer 38

c. Console lights. The console light provides the console, the sidestick, and the nosewheel steering with lighting.

Answer 39

d. Floor lights. These lights are located under the seats, and provide lighting for the surrounding floor.

Answer 40

a. The console lights

Answer 41

b. The pedestal flood light

Answer 42

c. The dome lights

Answer 43

d. The main instrument panel flood lights

Answer 44

a. Vα max

Answer 45

c. Vα prot

Answer 46

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.

Answer 47

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.

Answer 48

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.

Answer 49

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.

Answer 50

a. Indicates an altitude constraint when the vertical guidance is managed. The altitude constraint is out of the altitude scale.

Answer 51

b. Indicates the altitude constraint when the vertical guidance is managed. The altitude constraint is within the altitude scale.

Answer 52

c. Indicates the AFS CP selected altitude when the vertical guidance is either selected or managed. The altitude target is within the altitude scale.

Answer 53

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.

Answer 54

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.

Answer 55

b. Thanks to architectural redundancy and despite of some systems lost, all main functions are still available if a Hydraulic system is lost.

Answer 56

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.

Answer 57

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.

Answer 58

a. For maintenance operations, the ELEC PMPs can supply all the hydraulic circuits.

Answer 59

b. All of the above.

Answer 60

c. The crew can use DRAS and kneeling capability thanks to BLUE or YELLOW ELEC PMPs.

Answer 61

d. As soon as hydraulic power is required, the corresponding ELEC PMP automatically activates to pressurize the related components.

Answer 62

a. The TEST pb enables to test the CVR.

Answer 63

b. The TEST pb enables to record a mark in the CVR recording for further investigation.

Answer 64

c. The BOOMSET jack enables to plug a headset in order to hear what is recorded on the CVR.

Answer 65

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.

Answer 66

a. Among others, it record parameters related to aircraft position, secure communications, crypto keys and DASS parameters.

Answer 67

b. The DFDRS is in the front part of the aircraft.

Answer 68

c. The Digital Flight Data Recording System (DFDRS) records all the mission parameters.

Answer 69

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.

Answer 70

a. Deploys the emergency rafts

Answer 71

b. Opens the paratroop doors for evacuation

Answer 72

c. Enables to open the aft ditching hatch and arms the evacuation ladder system

Answer 73

d. Enables to deploy the evacuation ladder

Answer 74

a. Weight and CG calculation

Answer 75

b. Optimum load position computation

Answer 76

c. Consistency check of LMWS entries (configuration, limitations).

Answer 77

d. All the other options plus Cargo data storage and CLP preparation and edition.

Answer 78

a. enables to switch ON/OFF the converters that supply power to the cargo hold.

Answer 79

b. enables to switch ON/OFF the converter that supplies power to the cockpit.

Answer 80

c. enables to switch ON/OFF the converter that supplies power to the LMWS.

Answer 81

d. b and c.

Answer 82

a. There are three lights related to the EXT PWR on the ground power panel.

Answer 83

b. External Power NOT IN USE indicates that the external power unit is not connected to the aircraft.

Answer 84

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.

Answer 85

d. all of the above are false.

Answer 86

a. There are TR reset buttons on the overhead reset panels

Answer 87

b. There are GCU reset buttons on the overhead reset panels

Answer 88

c. Information about reset panels can be found in FCOM Supplementary Procedures

Answer 89

d. All the above

Answer 90

a. Limit dependence on pilot skills.

Answer 91

b. Reduce pilot workload when flying manually

Answer 92

c. Provide aircraft flight envelope protections that enhance safety

Answer 93

d. Reduce aircraft weight

Answer 94

a. GADIRUs

Answer 95

c. Ice Detection

Answer 96

a. If the aircraft keeps accelerating, flaps may retract fully.

Answer 97

b. The flaps automatically retract to the next retracted flaps configuration.

Answer 98

c. The automatic retraction can occur slightly before reaching VFE.

Answer 99

d. A pulsing F RELIEF message appears in the flap zone of the EWD

Siguiente

1.2. A4 YM21

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Resumen del Recurso

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	Creado por Jose Antonio Vazquez hace alrededor de 3 años