A330 L&B - ATA 31, ATA 45

The flight is divided into 10 phases corresponding to an aircraft configuration change. The page displayed in the last phase when turning off the engine is: * (8 puntos). Wheel. Engine. Doors.

CUAL ES LA FUNCTION DEL SYSTEM DATA ACQUISITION CONCENTRATORS (SDACS)? (5 puntos). SUMINISTRAR INFORMACION AL FWCS PARA GENERAR LAS ALARMAS SI EXISTEN DISCREPANCIAS Y LOS DATOS PARA LOS DMCS . GENERAR TODAS LAS SEÑALES PARA EL EFIS. GENERAR TODOS LOS AURAL Y VISUAL WARNINGS.

Si falla el DMC 3 para que el ECAM display funcione se debe:(5 puntos). Automáticamente entran las pantallas. Se debe cambiar el SW a posición 1 del EFIS switching panel. Se debe cambiar el SW a posición 2 del ECAM switching panel.

In the System Display, System or status page can be called? (6 puntos). Only Manually. Automatically or manually through the ECAM control panel. Automatically or manually through the ECAM switching panel.

In normal operation the ECAM system pages are displayed according to the current flight phase, this mode is called:(5 puntos). Single mode. Advisory mode. Automatic mode.

In ECAM DUAL DISPLAY MODE, when any parameters value drift from its normal range (ADV MODE)? * (6 puntos). The corresponding ECAM SD page is displayed automatically. It’s necessary push and holds the associated system flashing key on the ECP. Only ADV indication is show in EWD.

Which is the name of the computer function that permits detect, isolate and memorize any failure? * (8 puntos). CMC function. BITE function. ACMS function.

ECAM SYSTEM DISPLAY can be show? * (8 puntos). 13 System pages, cruise page and status page. 15 System pages. 15 System pages, cruise page and status page.

The alerts are classified in three levels. They depend on the importance and urgency of the corrective actions required. The red warnings, (highest priority), with attention getters (MASTER WARN + sound) are: * (8 puntos). Level I. Level II. Level III.

Que tipo de falla encontramos en la siguiente imagen * (5 puntos). Primaria. Secundaria. Independiente.

When the PFD (primary flight display) fails or switched off? * (8 puntos). The ND image is transferred automatically on the PFD. The PFD image is transferred automatically on the ND (navigation display). The PFD image is transferred manually with PFD/ND push button switch.

The CMC (central maintenance system) operates in two modes? * (8 puntos). Normal mode and Flight mode. Normal mode and Interactive mode. Manual mode and Interactive mode.

The failures displayed may be of three different types, without depending on their classification:(8 puntos). Independent failure, primary failure and secondary failure. Primary failure, secondary failure and tertiary failure. Independent failure, dependent failure and secondary failure.

What computers make up the EIS system? * (4 puntos). 3 DMCs, 2 FWCs and 2 SDACs. 2 DMCs, 2 FWCs and 1 SDACs. 2 DMCs, 3 FWCs.

CMS reports can be transmitter to the ground using: * (8 puntos). Air service unit (ASU). Flight warning computer (FWC). Air traffic service unit (ATSU).