Navegation 34

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

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

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

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 Transceivers are installed in the Aft Cargo Compartment. The antennas are installed close to the nose gear. Each system is equipped with one antenna.

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

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

If the Nose Wheel Steering command is coming.... Each ELAC receive a NWS command from FMGC and it is sent to the BSCU. The BSCU receives a NWS command directly from FMGC. The FAC receives 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?. G/S and LOC scales, G/S and LOC Deviation, selected Course, Frequency and Identifier. Only LOC and G/S scales. 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 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. The Triple Click is only heard when the Approach Mode is active or during Land Test.

ILS N2 is being tested.Where can you see the ILS N2 indications?. Fist Officers PFD and Captains No. Captain's PFD and ND. Captain's PFD and First Officer ND.

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

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

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

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

Where are the windshear indications shown?. PFDs and NDs. Only on the 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 FAC1. the FAC2. the FMGC 1.

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

What happens when the G/S p/b is pressed in, on the GPWS control panel?. The Glide Slope mode is inhibited. The self test sequence is initiated. 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?. The EGPWS generates aural and visual warnings. It is necessary to switch 'ON' the cockpit loudspeakers to get the aural 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, AP 1 is disengaged. AP 2 becomes active with AP 1 in standby. AP 1 remains active, AP 2 is in standby.

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

Which LRU computes the landing capability in the AFS?. The FAC according to the availability of the others computers. The FMGC 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?. only the FACS. FACs normally, the ELACs as an alternative. ELACs normally, FAC as an alternative.

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

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

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

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

The AP/FD basic modes are ... HDG and VIS. A/THR only. 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 O iftwo 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 is disconnected. the A/THR must be engaged manually. 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.