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On the reception mode, in order to listen in the selected transceiver you must operate. On the RMP the corresponding reception knob, when is released out becomes white and is ready to be turned and adjust the reception volume via AMU. On the ACP the corresponding reception knob, when is released out becomes white and is ready to be turned and adjust the reception volume via FMGC. On the ACP the corresponding reception knob, when is released out becomes white and is ready to be turned and adjust the reception volume via AMU.

How are the navigation systems tuned?. In normal operation, the navigation systems are tuned manually from the MCDU by the FMGCs via the RMPs. In normal operation, the navigation systems are tuned automatically or manually from the RMPs by the FMGCs via the MCDU. In normal operation, the navigation systems are tuned automatically or manually from the MCDU by the FMGCs via the RMPs.

What happen when the CAP 3 POSITION is selected in the audio switching panel?. In this position the CAPT will use the ACP of the 3rd occupant. The ACP of the 3rd occupant can be used. In this position the CAPT will use the ACP of the 3rd occupant. The ACP of the 1st officer cannot be used. In this position the CAPT will use the ACP of the 3rd occupant. The ACP of the 3rd occupant cannot be used.

What are the two types of calls that may be received for the SELL/CALL card. Ground call and Cabin attendant call. Cabin attendant call and Passengers call. Ground stations call only.

. When is the BOOM SET connected to the transmission system?. When the PTT is pressed in on the Side Stick or the RAD transmission key is pressed on the RMP. When the PTT is pressed in on the Side Stick or the RAD transmission key is pressed on the ACP. When the PTT is pressed in on the Side Stick or the INT transmission key is pressed on the ACP.

What is the function of the static discharges?. The static dischargers avoid static electricity discharging noise and ensure a good quality of video transmission, without interference. The static dischargers avoid only static electricity. The static dischargers avoid static electricity discharging noise and ensure a good quality of radio transmission, without interference.

What component in the CIDS system becomes inoperative if the SVCE BUS is unavailable?. The first DIR, the non essential DEU circuits, the FAP, AIP/ACP. The second DIR, the non essential DEU circuits, the FAP, AIP/ACP. The second DIR, the essential DEU circuits, the FAP, AIP/ACP.

What is the main function of the autoflight system?. AFS calculates the orders to hydraulically control the flight controls and the engines through the FMGC and FADEC. AFS calculates the orders to automatically control the flight controls and the engines through the EFCS and FADEC. AFS calculates the orders to automatically control the flight controls and the engines through the MCDU and FADEC.

What statement regarding autoflight is correct?. During AFS operation the side sticks and thrust levers do not move automatically. During AFS operation the side sticks and thrust levers move automatically. During AFS operation the side sticks and thrust levers do not move manually.

Which part of the FMGC gives the flight plan definition?. Flight management. Flight guidance. Both function can manage the flight plan.

What are the main functions of the Yaw Damper. Rudder trim, turn coordination in cruse, engine failure compensation in auto flight, yaw guidance order execution. Dutch roll damping, turn coordination in cruise, engine failure compensation in auto flight, yaw guidance order execution. Dutch roll damping, flight envelope, engine failure compensation in auto flight, yaw guidance order execution.

What is the alpha floor protection?. Is a protection against an excessive angle of attack. Is a protection against an excessive thrust. Is a protection against an excessive angle of steering.

How can the flight plan be changed in flight after being selected on ground through the MCDU?. On the MCDU the pilots can engage the AP and can modify different flight parameters leading to a immediate change in the control of the aircraft. On the FCU the pilots can engage the MCDU and can modify different flight parameters leading to a immediate change in the control of the aircraft. On the FCU the pilots can engage the AP and can modify different flight parameters leading to a immediate change in the control of the aircraft.

Which component display guidance commands on the PFD, allowing the pilots to flight manually according to the FMGC demands?. Flight director (FD). Auto thrusts. Primary Flight display (pfd).

When is engage the Auto pilot?. The autopilot can be engaged in flight, provided the aircraft has been airborne for at least 10 seconds. The autopilot can be engaged in ground, at take off only. The autopilot can be engaged in flight, provided the aircraft has been airborne for at least 5 seconds.

When is the Autothrust engaged automatically?. When the AP is engaged in flight below 100 feet RA. When the AP/FD is engaged in take off or go around modes. When the DU is engaged in take off or go around modes.

What type of test is done with the LAND TEST?. The land test gives the capability of the LANDing mode and equipment requires to obtain CATegory 1. The land test gives the capability of the LANDing mode and equipment requires to obtain CATegory 2. The land test gives the capability of the LANDing mode and equipment requires to obtain CATegory 3.

The AUTO FLIGHT test is done to?. To check AFS LRU removal and installation, get troubleshooting data even if the test is OK. To check FMGCs LRU removal and installation, get troubleshooting data even if the test is OK. To check AFS LRU removal, get troubleshooting data to check if the test is OK.

The recommended conditions to do a safety test are. Aircraft on ground, engines stopped, hydraulic power (green/yellow) for FAC only. Aircraft in flight, engines stopped, hydraulic power (green/yellow) for FAC only. Aircraft on ground, engines running, hydraulic power (green/yellow) for FAC only.

Which computer calculates the yaw damper orders with the normal law when the autopilot is not engaged?. ELAC. FAC. FMGC.

What happen when the FAC cannot be engaged on ground after power up during the 30 seconds test?. The white off light flashes. There is no indication. The amber fault light flashes.

What indications are displayed in the cockpit if a windshear is detected. WINDSHEAR message is displayed on the ND and the aural warning ¨WINDSHEAR, WINDSHEAR¨ is triggered. WINDSHEAR message is displayed on the ECAM and the aural warning ¨WINDSHEAR, WINDSHEAR¨ is triggered. WINDSHEAR message is displayed on the PFD and the aural warning ¨WINDSHEAR, WINDSHEAR¨ is triggered.

The Air Traffic Service Unit has been designed to. To take provisions of all foreseen evolutions. To verify all the communication system. To notice the pilot about any dangerous condition of the aircraft.

How can the ATSU SW be uploaded?. Vía AIDS. Vía MCDU. Via the multipurpose disk drive unit.

What functions are given by the MCDU?. AOC hosted applications and air flight communication management. AOC hosted applications and air ground communication management. AOC hosted applications and maintenance status.

What for the VOICE MODE TEST serves?. To check the ATSU router configuration and test the voice mode. To check the ATSU router communication and test the voice mode. To check the ATSU router configuration and test the voice recorder.

The ATSU/FDIMU interface is used for?. Flight performance in uplink request and downlink AIDS reports. Flight parameters in uplink request and downlink AIDS reports. Flight envelope in uplink request and downlink AIDS reports.

What happen if the Bite detects a fault which requires removal of the unit from the aircraft during SSCVR test?. The bite indicator will activate and will remain activated until repair is accomplished. This test requires aircraft in flight. The bite indicator will activate and will remain activated until repair is accomplished. This test requires engines not running. The bite indicator will activate and will remain activated until repair is accomplished. This test requires engines running.

Flight interphone allows voice communication between?. Flight crew members and ground handling, cabin crew members, towing and taxiing personnel via ACP. Flight crew members and ground handling, towing and taxiing personnel via ACP. Flight crew members and ground handling, towing and taxiing personnel via RMP.

For maintenance purpose the HF bites are storage in?. HF AMU and monitored for the CFDS. CFDIU and monitored for the AIDS. HF XVCR and monitored for the CFDS.

Alpha-floor detection and windshear protection are computed by: FAC or ELAC and send to the FMGC. FAC or SEC and send to THE FMGC. FMGC or ELAC and send to the FAC.

What happen when the CAP 3 POSITION is selected in the audio switching panel?. In this position the CAPT will use the ACP of the 3rd occupant The ACP of the 1er officer cannot be used. In this position the CAPT will use the ACP of the 3rd occupant The ACP of the 3rd occupant cannot be used. In this position the CAPT will use the ACP of the 3rd occupant .The ACP of the 3rd occupant can be used.

The FAULT light on (FAC) P/BSW remains OFF if one or more of the following functions fail: yaw damper, rudder trim, rudder travel limitation. Only the amber message appears on the ECAM display unit. The FAC remains engaged. True. False.

When is the BOOM SET connected to the transmission system?. When the PTT is pressed in on the Side Stick or the INT transmission key is pressed on the ACP. When the PTT is pressed in on the Side Stick or the RAD transmission key is pressed on the RMP. When the PTT is pressed in on the Side Stick or the RAD transmission key is pressed on the ACP.

What is the main function of the auto flight system?. AFS calculates the orders to automatically control the flight controls and the engines through the MCDU and FADEC. AFS calculates the orders to automatically control the flight controls and the engines through the EFCS and FADEC. AFS calculates the orders to hydraulically control the flight controls and the engines through the FMGC and FADEC.

If the standby navigation mode is selected, the navigation systems frequencies are controlled by: RMP 1 and RMP 2 only. RMP 1 and RMP 3 only.|. RMP 3 and RMP 2 only.

What statement is correct regarding to the Very High Frequency (VHF) system?. The Very High Frequency (VHF) system is used for all short-range voice communications. The High Frequency (VHF) system never is install on A320 aircraft. The very High Frequency (VHF) system serves for all long-distance voice communications.

What components in the CIDS system become inoperative if the SVCE BUS is unavailable?. The second DIR, the non-essential DEU circuits, the FAP, AIP/ACP. The first DIR, the non-essential DEU circuits, the FCU, AIP/ACP. The second DIR, the essential DEU circuits, the FAP, AIP/FAC.

What statement is correct regarding to the High Frequency (HF) system?. The High Frequency (HF) system serves for all short-distance voice communications. The High Frequency (HF) system serves for all long-distance voice communications. The High Frequency (HF) system never is install on A320 aircraft.

The FAC computes various characteristic speeds using data from: The ADIRU, the LGCIU, the FAC, and the SFCC. The ADIRU, the LGCIU, the FMGC, and the ELAC. The ADIRU, the LGCIU, the FMGC, and the SFCC.

What happen if the Bite detects a fault which requires removal of the unit from the aircraft during SSCVR test?. The bite indicator will activate and will remain activated until repair is accomplished. This test requires aircraft in flight. The bite indicator will activate and will remain activated until repair is accomplished. This test requires engines not running. The bite indicator will activate and will remain activated until repair is accomplished. This test requires engines running.

How can the flight plan be changed in flight after being selected on ground through the MCDU?. On the FCU the pilots can engage the AP and can modify different flight parameters leading to an immediate change in the control of the aircraft. On the MCDU the pilots can engage the AP and can modify different flight parameters leading to an immediate change in the control of the aircraft. On the FAC the pilots can engage the AUTOTHRUST and can modify different flight parameters leading to an immediate change in the control of the aircraft.

When is engaged the Auto pilot?. The autopilot can be engaged in flight, provided the aircraft has been airborne for at least 5 seconds. The autopilot can be engaged in ground, at take-off. The autopilot can be engaged in flight, provided the aircraft has been airborne for at least 10 seconds.

Which is the purpose of the muting circuit?. A muting circuit is installed to avoid acoustic coupling between the loudspeakers and the microphones. A muting circuit is installed to avoid acoustic coupling between the loudspeakers and the aural warnings. A muting circuit is installed to allow acoustic coupling between the loudspeakers and the microphones.

Which is the function of the SATCOM?. Is the transmission and processing of signals via satellites supplying aeronautical services in the Ka-Band?. Is the reception and processing of signals via satellites supplying aeronautical services in the HF.?. Is the reception and processing of signals via satellites supplying aeronautical services in the L-Band?.