naaveegacion

When is the red FD flag displayed?. In case of one FMGC failure. In case of both FMGCs failure and the FD push buttons are ON. In case of both FD push buttons are in OFF condition.

If both Flight Management parts agree after Power up: The independent mode is active. The single mode is active. The Normal mode is active.

How is the simultaneous transmission between the DME,ATC and TCAS systems avoided?. Allowing the DME, ATC and TCAS simultaneous operation. Intercepting the ATC replies when the DME is in standby. With a coaxial supressor installed between them.

Who is the main user of the GPIR signal?. The FMGCs. The DMCs. The VOR and ILS system.

Which statement about the Low Range Radio Altimeter System is right?. The antennas are installed close to the nose gear. The Transceivers are installed in the Aft Cargo Compartment. Each system is equipped with one antenna.

The A/P can be engaged: 5 seconds after the lift off. On ground with both engines running. Only in cruise phase.

The No. 1 VOR/MKR System consists of ... a VOR/MKR Receiver, two VOR/MKR Antennas. a VOR/MKR Receiver and a VOR Antenna. a VOR/MKR Receiver, a VOR/MKR Antenna.

If the Nose Wheel Steering command is coming.... The FAC receives a NWS command from FMGC and it is sent to the BSCU. The BSCU receives a NWS command directly from FMGC. Each ELAC receive a NWS command from FMGC and it is sent to the BSCU.

Which MMR / ILS information is displayed with the ND in ROSE-ILS Mode?. Only LOC and G/S scales. G/S and LOC scales, G/S and LOC Deviation, selected Course, Frequency and Identifier. FMGC Approach Data.

Which Radio Altimeter activates the modes at the Ground Proximity Warning System?. The Radio Altimeter # 1. The Radio Altimeter # 2. The Stanby Altimeter.

In the cockpit a Triple Click is heard. What is the correct statement?. The Triple Click is only heard when the Approach Mode is active or during Land Test. The Triple Click is heard when the FMGCs computes a downgrading of the Land Capability. The Triple Click indicates the pilots that the autoflight system is LAND 3 FAIL OPERATIONAL.

ILS N2 is being tested. Where can you see the ILS N2 indications?. Captain's PFD and First Officer ND. Captain's PFD and ND. First Officers PFD and Captains ND.

If the A/THR function is engaged and active... the Thrust Lever position controls the engines. the FMGC by means of A/THR function controls the engines. the A/THR pushbutton light is OFF.

ENHANCED. The Predictive Windshear is active when ... the ATC switch is set in the AUTO or ON position. one engine running and the groundspeed is less than 15 kts. one engine is running and the groundspeed greather than 30 kts.

The WXR-System... ..is not able to display a test pattern during the test. ...consists of 1 Transceiver, 1 Antenna and a Control Panel. ...has no interface to the CFDS.

Where is the Flight Mode Annunciator (FMA) located?. In the upper ECAM display. It is part of the ND. In the upper part of the PFD.

Where are the windshear indications shown?. Only on the NDs. PFDs and NDs. DDRMI.

Both FMGCs are inoperative. How are the VOR frequency and course selected?. Manually via STANDBY NAV key on RMPs. Automatically via the backup nav stored on the MCDUs. Manually via the RAD NAV page on MCDUs.

The BITE function of the AFS is performed by ... the FMGC 1. the FAC 1. the FAC 2.

With the autopilot engaged, the Rudder Trim is ... Automatic, Manual/Reset Selection are not available. Used by the Pilot via the Rudder Trim Selector. Fixed to one value.

What happens when the G/S p/b is pressed in, on the GPWS control panel?. The self test sequence is initiated. The Glide Slope mode is inhibited. PULL UP message sound through the speakers.

When is FD engaged?. As soon as electrical power is available. As soon as at least one AP is engaged. After 5 sec. lift off or 400 ft RA.

Which statement of EGPWS is correct?. It is necessary to switch 'ON' the cockpit loudspeakers to get the aural warnings. The EGPWS generates aural and visual warnings. The EGPWS consists of two GPWS-computers.

The aircraft is in cruise with AP 1 engaged. What happens when AP 2 is engaged?. AP 2 becomes active with AP 1 in standby. AP 2 becomes active, AP 1 is disengaged. AP 1 remains active, AP 2 is in standby.

CAT IIl aircraft. A discrepancy related to the category condition of the Airplane has not been solved, so the Airplane... is operative degraded. remains in Cat Ill. is technically degraded.

Which LRU computes the landing capability in the AFS?. The FAC according to the availability of the others computers. The FMC according to the availability of various sensors and functions. The ELAC according to the availability of the sensors.

How many Marker beacon (LRU) are in the A/C?. There is one system active. This system doesn't exist in the A/C. There are 2 systems and only operate on GND.

Which Computer performs normally the Rudder Travel Limitation?. ELACs normally, FAC as an alternative. FACs normally, the ELACs as an alternative. Only the FACs.

During the final approach the Pilot set both Thrust Lever to the IDLE stop. What happens with the autothrust system?. The A/THR function disengages and the THR pb light is OFF. The A/THR pb is ON and the function remain engaged but is not active. The autothrust remains engaged and the ASYM message is displayed on PFDs.

Where is the used Tuning Mode displayed?. On the PFDs. On the NDs. On the lower ECAM DU.

If one channel in the FCU is inoperative: The A/Thr and A/P will be inoperative. The F/D # 1 and # 2 will be inoperative. The other channel will be active and all FCU function operative.

What is the correct position of TCAS Mode Switch for displaying of Resolution Advisories on the PFD?. ALT RPTG. TA. TA/RA.

The AP/FD basic modes are... A/THR only. HDG and VIS. TRK/FPA.

When is the Auto Thrust activated?. When the thrust levers are between CLB and a point slightly above IDLE detents if two engines are operative. When the Thrust Levers are in TO/GA detents if one engine is inoperative. When the thrust levers are between CLB and IDLE detents if two Engines are operative.

Where is the DH (Decision Height) selected?. In the MCDU, APPROACH page. In the EFIS control panel. In the RMP panel.

Aircraft on the ground, engines running. In TO/GA (take off/ go around) mode: the A/THR must be engaged manually. the A/THR is disconnected. the A/THR is engaged automatically.

When do the G/S and LOC scales appear on the PFD?. When the ILS pushbutton is selected. When ILS is captured. When G/S and LOC beams are received.

Which statement about the ATC System is right?. There are 2 ATC-Antennas installed. The Transponder Select Switch connects both Antennas to the active Transponder. There is one Antenna per Transponder installed. Each transponder has two Antennas.

The Radio Navegation frecuencies are automatically tuned by .... FMGC. ACPs. The passenger cabin system communication.

The Rudder Travel Limitation function is: The limitation of the rudder travel through a control law in relation to the corrected speed(Vc). The limitation of the rudder travel through a control law in relation to the flap position. The limitation of the rudder travel through a control law in relation to the angle of attack.