Airbus A330 – Navigation - SmartCockpit - Airline training guides, Aviation, Operations, Safety

In case of both FMGECs failure, VOR 2 may be tuned on:

By RMP 1 or 2.

By RMP 2 only.

By any RMP.

Correct! Wrong!

During normal operations:

The GPS receiver 1 supplies the ADIRU1, and the GPS receiver 2 supplies the ADIRU2 and ADIRU3

The GPS receiver 1 supplies the ADIRU1 and the ADIRU3, and the GPS receiver 2 supplies the ADIRU2.

The GPS receiver 1 supplies the ADIRU2 and the ADIRU3, and the GPS receiver 2 supplies the ADIRU1.

Correct! Wrong!

ADIRS panel - If the ADR 2 FAULT light comes on steady. What does it mean?

Attitude information is not available anymore.

Air data output disconnected.

A fault is detected in the air data reference part.

Correct! Wrong!

When the NAV key is on and the flight crew presses one of these STBY NAV keys, the ACTIVE window displays the frequency/channel to which that receiver is tuned. The green monitor light on the selected key comes on, and the one on the previously selected STBY NAV or COM key goes out.

False.

True.

Correct! Wrong!

Using RMP for selecting NAVAID is allowed:

In case of both FMGECs or both MCDUs failure.

Without any restrictions.

In case of a single FMGEC or a single MCDU failure.

Correct! Wrong!

Ground Speed and TAS shown on ND 2 are supplied by:

IR 2 + ADR 2.

IR 2.

ADR 2.

Correct! Wrong!

The ADIRU 3 receives information from:

CAPT probes and F/O TAT.

STBY probes and CAPT TAT.

F/O probes and CAPT TAT.

Correct! Wrong!

Should PITOT STBY and STATIC STBY probes fail:

Both statements are correct.

ADIRU 3 receives wrong information.

Stand-by Altitude and speed information are wrong.

Correct! Wrong!

The 'ON BAT' light comes on for a few seconds. What does it mean?

The fast align sequence starts.

The IR battery is discharged.

The normal align sequence starts.

Correct! Wrong!

The ON BAT light also comes on for a few seconds at the beginning of a complete IRS alignment. The light does not come on in the case of a fast alignment.

Each ADIRU is divided in two parts. The ADR (Air Data Reference) and the IR (Inertial Reference). The IR part supplies:

Altitude, airspeed, Mach, temperature and overspeed warnings.

Attitude, track, heading, accelerations, ground speed, vertical speed and aircraft position.

Attitude, flight path vector, track, heading, accelerations, angular rates, ground speed, vertical speed and aircraft position.

Correct! Wrong!

In normal operation, heading information on the DDRMI, is coming from:

ADIRU 2.

ADIRU 1.

ADIRU 3.

Correct! Wrong!

In case of RA 1 failure:

There is no more Height information on the PFD 1 but a red flag on both PFD.

There is no more RA information on the PFD 1, but a red flag.

RA 1 information is replaced by RA 2 information on PFD 1 automatically and GPWS is lost.

Correct! Wrong!

The loudspeaker announces 'RETARD':

At 20 ft.

At 20 ft RA.

At 20 ft, or at 10 ft if the autothrust is active and one autopilot is in LAND mode.

Correct! Wrong!

In normal operation, PFD 2 and ND 2 receive their data from the ADIRU 2. With the AIR DATA switch on F/O ON 3, displayed data come from:

ADR 1.

DMC 3.

ADR 3.

Correct! Wrong!

ADIRS panel - If the IR 1 FAULT flashing light comes on:

IR 1 is lost.

Only attitude information may be available in ATT mode.

The attitude information and heading stabilization may be available in ATT mode.

Correct! Wrong!

The reference altitude for callouts is always the radio height for both precision and non precision approaches.

True.

False.

Correct! Wrong!

The reference altitude for callouts is the radio height for precision approaches (DH) and baro altitude (MDA/MDH) for non precision approaches.

Each ADIRU is divided in two parts. The ADR (Air Data Reference) and the IR (Inertial Reference). The ADR part supplies:

Altitude, attitude, aircraft position, airspeed, temperature and overspeed warning.

Altitude, airspeed, ground speed, Mach, temperature and overspeed warnings.

Altitude, airspeed, Mach, angle of attack, temperature and overspeed warnings.

Correct! Wrong!

There are ADMs (Air Data Modules) which convert pneumatic data from PITOT and STAT probes into numerical data for the ADIRUs.

Six.

Eight.

Four.

Correct! Wrong!

The DME1 and DME2 displays are dashed when a fault is detected or data invalid.

False.

True.

Correct! Wrong!

The DME1 and DME2 displays are blanked or dashed when a fault is detected or data invalid.

ADIRS panel - If the IR 1 FAULT light comes on steady:

IR 1 is lost.

The attitude information and heading stabilization may be available in ATT mode.

Only attitude information may be available in ATT mode.

Correct! Wrong!

Only one RMP can manage both ILS receivers:

No, it is necessary to select the ILS on each RMP.

Yes, but only if radio nav back up mode key is engaged on RMP 1 and RMP 2.

Yes, in any case.

Correct! Wrong!

The Flight Management Guidance Envelope Computers (FMGECs) have three functions:

Flight guidance, ECAM control and EIS control.

Flight guidance, flight management and flight envelope.

Flight guidance, EIS control and flight envelope.

Correct! Wrong!

ADR 1 sends aerodynamic data to CAPT instruments and ADR 2 to F/O instruments. In case of ADR 1 or ADR 2 failure:

Emergency information must be used.

ADR 3 data are available by switching the ATT HDG selector.

ADR 3 data are available by switching the AIR DATA selector.

Correct! Wrong!

The ADIRU provides navigation information:

By using satellites signals.

On an independent basis, without reference to ground stations or satellites.

By using ground stations signals.

Correct! Wrong!

The Air Data and Inertial Reference System (ADIRS) supplies temperature, anemometric, barometric and inertial parameters to the EFIS system (PFD and ND) and to other user systems (FMGEC, FADEC, PRIM, SEC, FWC, SFCC, ATC, GPWS, etc.).

False.

True.

Correct! Wrong!

The Radio Navigation Tuning may be automatic (FMGEC), manual (MCDU) or stand-by mode (RMP). What is the true statement about RMP:

Only RMP 1 or 2 can switch independently every navaid.

The 3 RMPs can switch independently every navaid.

RMP 1 controls VOR 1 and ADF 1, RMP 2 controls VOR 2 and ADF 2.

Correct! Wrong!

Inertial data (TK/GS, PPOS, WIND, HDG) are available if ADIRS selector is on:

NAV or ATT.

ATT only.

NAV only.

Correct! Wrong!

The aircraft has two radio altimeters (RA). CAPT PFD displays the RA1 height, and the F/O PFD displays the RA2 height. If one RA fails, both PFDs display the height from the remaining RA.

True.

False.

Correct! Wrong!

In ELEC EMER configuration, DDRMI displays:

ADF 2, VOR 1.

ADF 1, VOR 1.

ADF 1, VOR 2.

Correct! Wrong!

In EMER ELEC configuration, only the VOR1 or ADF1 are available, according to the position of the VOR1/ADF1 selector.

During a turnaround, you notice that there is a residual groundspeed on both NDS. How do you correct this?

It is possible to carry out a rapid re-alignment by turning all three ADIRS off momentarily.

There is no corrective action possible until the aircraft is completely shut down.

As the engines have been shut down, it is necessary to carry out a full re-alignment of ADIRS 1 and 2 only.

Correct! Wrong!

In flight, an IR selector set on ATT, may we use again the NAV function?

Yes.

No.

Yes, but only after stabilizing the aircraft.

Correct! Wrong!

By switching ADIRS selector on ATT, available data are:

Attitude and heading information.

Attitude, heading and wind information.

Attitude information.

Correct! Wrong!

In case of ADR 2 failure:

Before any transfer, speed and altitude information are lost on PFD 2.

AP 2 and FD 2 are lost.

All statements are correct.

Correct! Wrong!

In normal operation, the NAVAIDS are tuned:

Manually through the RAD NAV page.

Automatically by the FMGEC (Flight Management Guidance Envelope Computers).

Manually through the RMP (Radio Management Panel).

Correct! Wrong!

The information produced by the ADIRUs:

Is displayed on the PFD, ND, DDRMI and supplied to other system.

Is only available when TRUE/MAG pb is set on TRUE.

Can never be seen by the flight crew.

Correct! Wrong!

IR 1 sends inertial data to captain instruments and IR 2 to F/O instruments. In case of IR 1 or IR 2 failure:

IR 3 data are available by switching the AIR DATA selector.

IR 3 data are available by switching the ATT HDG selector.

Emergency information must be used.

Correct! Wrong!

ILS 1 and ILS 2 are available on:

ILS 1 on PFD 1 and ND1, ILS 2 on PFD 2 and ND 2.

ILS 1 on PFD 1 and ND2, ILS 2 on PFD 2 and ND 1.

ILS 1 on PFD 2 and ND1, ILS 2 on PFD 1 and ND 2.

Correct! Wrong!

What are the possible modes of FMGEC operation?

Dual, Independent, Single and Back-up.

Dual, Single, Automatic and Manual.

Dual, Single, Back-up and Manual.

Correct! Wrong!

In case of both FMGECs failure, ILS may be tuned on:

By RMP 1 only.

By RMP 1 or 2.

By any RMP.

Correct! Wrong!

Airbus A330 – Navigation