A330 L&B - ATA 34, ATA 22

How can be performed the autopilot disengagement?. Manually. Automatically. Manually and Automatically.

Which mode is shown by a dashed line on FCU?. Selected mode. Managed mode. Slave mode.

Where is displayed the landing capability during approach, in case of degradation?. ND and ECAM. PFD and ND. FMA and ECAM status page.

Which functions compose the FE part?. AP and FD. AP,FG and A/THR. Acquisition, speed envelope computation and detection of the abnormal conditions.

Which is the P/B to inhibit all GPWS warnings)?. TERR P/B. G/S P/B. SYS P/B.

Which information is send from Fuel Control and Monitoring computers (FCMCs) to the FMGEC?. Aircraft Gross weight and The CG position. Lateral Asymmetry. Fuel consumption for each engine in auto trust function.

Which Software must be periodically updated?. Performance data base each 28 days. Navigation data base each 30 days. Navigation data base each 28 days.

The ADIRUs receive data from?. Pitot and static inputs directly. AOA and TAT inputs processed by ADM. Pitot and static inputs processed by ADM and AOA and TAT information directly.

What is the function of the ON BATT indicator on the ADIRS MSU (mode selector unit)?. The ON BAT indicator comes ON when one or more ADIRUs are selected and come on for a few seconds in order to test the batteries. The ON BAT light of the ADIRS MSU comes on for a few seconds in order to test the switching to aircraft batteries. The ON BAT light comes on when one or more ADIRUs are supplied by the aircraft batteries to test the ADIRUs..

Which functions compose the FG part?. AP,FG and A/THR. AP,FD and A/THR. AP,FG and FD.

The TCAS generate two types of Warnings?. Traffic Advisories and the Resolution Advisories. Traffic speed and the Resolution speed. Other Traffic and proximate Traffic.

Which action is performed in “selected mode”. Enter a data on MCDU and PUSH the relevant selector knob on the FCU. PULLS the knob and then turns the relevant selector knob on the FCU to set the parameter. Turns the relevant selector knob on the FCU to set the parameter, and then PUSH the knob.

Which functions the FM part performs?. Flight planning, navigation and performance optimization using a navigation database and a performance database, lateral functions, vertical functions, performance functions. Lateral execution, vertical execution, Autothrust comands. Both are true.

What is a ADIRUs function interface with the Weather Radar Antenna?. Pitch and roll angles to ensure antenna stabilization. Airspeed and QNH. Air speed for Doppler mode correction.

The short term pilot orders are normally entered through______ while the long term pilot orders are entered through_____________. MCDUs, FCUs. FCU, MCDUs. MCDU in both cases.

Which functions compose the FMGEC 1?. Auto Pilot, Flight guidance. Auto thrust and auto pilot and FIM. FM, FG,FE and FIDS.

When the auto thrust function is engaged and active?. A/THR system controls the engines, A/THR P/B is ON, FMA displays A/THR engagement status (in white in the leftth column) and the A/THR mode in the right column. A/THR system controls the engines, A/THR P/B is OFF, FMA displays A/THR engagement status (in white in the right column) and the A/THR mode in the left column. A/THR system controls the engines, A/THR P/B is ON, FMA displays A/THR engagement status (in White in the right column) and the A/THR mode in the left column.

Which is the RMP does not operate in radio navigation backup tuning?. RMP1. RMP2. RMP3.

ISIS is fitted with a BITE. Specific maintenance and test menus are directly accessible by using the keys on the front face of the instrument. True. False.

If both FMGECs have failed, the receivers can be manually tuned: FMGEC auto and MCDU manual tuning is inhibited.. Via the RMPs. This is the backup tuning mode. Flight Management Guidance and Envelope Computer (FMGEC) automatically tunes its own side receivers via its associated Radio Management Panel (RMP).