A330 Illuminati

The Flight Management Guidance and Envelope System (FMGES) mautomatically aligns the Inertial Reference System (IRS) based on the entered departure airport coordinates. False. True.

The ADIRUs compute inertial data using internal laser gyros and accelerometers. False. True.

With the latest ADIRUs, the GPS position appears on the INIT page less than 1 minute after setting ADIRS to NAV. True. False.

If the ALIGN IRS prompt key is not pressed, the ADIRS will align on the reference point coordinates of the departure airport. False. True.

The ADIRUs are a combination of which two references?. Air Data Reference (ADR) and Inertial Reference (IR). Air Data Reference (ADR) and Airspeed Reference (AR). Airspeed Reference (AR) and Inertial Reference (IR). Angle Of Attack (AOA) and Total Air Temperature (TAT).

Which sensor inputs are directly sent to the ADIRUs?. Global Positioning System (GPS). Angle Of Attack (AOA) and Total Air Temperature (TAT). Standby pitot and static data. Pitot and static inputs.

What type of data does the inertial part of the ADIRUs calculate and output?. Airspeed and Mach number. Barometric altitude. Attitude, heading, and angular rate. Total temperature.

Which ADIRU provides heading data to the DDRMI in normal configuration?. ADIRU 1 only. ADIRU 1 and ADIRU 2. ADIRU 1 and ADIRU 3. ADIRU 2 and ADIRU 3.

What does the ADIRU SWITCHING panel allow in case of ADIRU 1 or 2 failure?. Switch to ADIRU 3 manually. Turn off all ADIRUs. Switch to ADIRU 2 only. Switch to GPS mode.

What does the ADIRS MSU control?. OFF/NAV/ATT switch. Only the OFF/NAV switch. Only the NAV/ATT switch. Only the OFF/ATT switch.

Where is the IRS initialization normally performed?. Through the FMGEC via the MCDU. Directly on the ADIRUs. On the ADIRS MSU. On the Flight Control Unit (FCU).

Which conventional standby instruments does the ISIS replace?. Standby altimeter, standby airspeed indicator, standby compass. Standby altimeter, standby horizon indicator, standby airspeed indicator. Standby compass, standby horizon indicator, standby airspeed indicator. Standby altimeter, standby horizon indicator, standby compass.

Which of the following data can the ISIS display?. Airspeed, lateral acceleration, ILS information, temperature. Airspeed, altitude, pitch and roll angles, ILS information. Airspeed, Mach number, temperature, altitude. Airspeed, lateral acceleration, temperature, altitude.

How is FM switching performed if one FMGEC fails?. Automatically by the remaining FMGEC. Manually through the FM rotary switch. By using the third MCDU. By turning off the failed FMGEC.

In backup tuning mode, which RMPs are used to control the receivers?. Only the third RMP. Only the CAPT RMP. The CAPT and F/O RMPs. All three RMPs.

ADIRU 3 can be manually selected to supply data if ADIRU 1 or ADIRU 2 fails. True. False.

ISIS can display airspeed, Mach number, altitude, and ILS information. True. False.

The ILS function is solely responsible for providing vertical deviation signals. True. False.

The LGCIU does not interact with the receiver BITE module. True. False.

The EGPWS continues to receive radio altitude data even if RA 1 system fails. False. True.

The Weather Radar (WXR) uses the principle of ______ to detect the level of precipitation. radio echoing. doppler effect. frequency modulation. radar scanning.

The transceiver digitalizes the video signal for display on the ______. PFD. ND. MFD. CDU.

The RA provides altitude data for the automatic activation of the windshear function. True. False.

Predictive windshear alerts are inhibited by signals from the ADIRUs. False. True.

What types of warnings does TCAS generate?. Traffic Advisories (TA), Resolution Advisories (RA). Traffic Advisories (TA). Resolution Advisories (RA). Ground Proximity Warnings (GPW).

What corrective data does the PFD provide to the flight crew?. Vertical speed correction data. Horizontal speed correction data. Altitude correction data. Heading correction data.

What checks the signal validity of the TCAS?. Flight Warning Computers (FWCs). Flight Management Guidanceand Envelope Computers (FMGECs). Air Data and Inertial Reference Units (ADIRUs). Landing Gear Control Interface Unit (LGCIU).