A320 ATA 31 T2

What is the purpose of the Electronic Centralized Aircraft Monitoring (ECAM) system?. Monitoring engine parameters. Displaying weather information. Controlling navigation systems. Managing cabin lighting.

Which Display Management Computer (DMC) drives the Captain's Primary Flight Display (PFD) in normal operation?. DMC 1. DMC 2. DMC 3. DMC 4.

When does the ADV symbol pulsate on the Engine/Warning Display (EWD)?. When there's an advisory on another SD page. During takeoff and landing. When a failure is detected by the FWC. When the CAPT PFD and ND fail.

What does the overflow arrow on the EWD indicate?. Engine failures. Excessive warning messages. Cabin temperature issues. Navigation system problems.

What is the role of the System Data Acquisition Concentrators (SDACs) in the aircraft system?. Generate warning messages. Compute engine parameters. Receive signals from aircraft systems. Provide navigation guidance.

In which situations does the Engine/Warning Display (EWD) display the title of a failure and the associated actions to take?. During takeoff and landing only. When there's an advisory on another SD page. When an aural warning is triggered. In case of aircraft system failure.

How are the CLeaR P/Bs used in response to a system failure?. They turn off the power to the Display Units (DUs). They release the Fault lights on the hydraulic panel. They indicate the phase of the flight. They clear the warnings and cautions.

What are the primary parameters displayed in the upper area of the Engine/Warning Display (EWD)?. Engine Pressure Ratio (EPR). Slat/flap position. Fuel On Board (FOB). All of above.

The Electronic Centralized Aircraft Monitoring (ECAM) system displays weather information. True. False.

In normal operation, DMC 1 drives the Captain's Primary Flight Display (PFD), while DMC 2 drives the First Officer's PFD. True. False.

The CLeaR P/Bs are used to activate the warnings and cautions. True. False.

The STATUS REMINDER and RECALL FUNCTION reminds the crew of cleared warnings. True. False.

The System Data Acquisition Concentrators (SDACs) send data to the Electronic Flight Instrument System (EFIS) displays. True. False.

Level 3 alerts correspond to an emergency configuration where corrective or palliative action must be taken by the crew __________. immediately. without any action. after a crew meeting. during routine maintenance.

A primary failure is a failure of an equipment or system causing the loss of __________ equipment. secondary. other. independent. advisory.

In ECAM Normal Dual Display mode, the flashing ADV symbol indicates multiple advisories on different pages or a failure __________. on the currently displayed page. detected by the FWC. requiring immediate action. in the ECP.

In ECAM MONO Display mode, when a value drifts from its normal range, a white ADV message flashes in the center of the EWD to attract crew __________. monitoring. attention. routine maintenance. emergency response.

Level 3 warnings are associated with a Continuous Repetitive Chime (CRC), warning messages on Liquid Crystal Display (LCD), and a flashing __________. caution light. advisory light. caution message. MASTER WARNing light.

Level 2 alerts require immediate crew awareness but not immediate __________ action. emergency. corrective. advisory. monitoring.

What happens when the PFD unit is switched off by its potentiometer?. ND is automatically displayed on the PFD unit. The PFD image remains on the PFD unit. The ND image is automatically displayed on the ND unit. The ECAM single display mode is activated.

How is the PFD/ND transfer (XFR) performed?. Physically swapping the PFD and ND units. Manually switching the PFD/ND outputs inside the DMC. Automatically by the ECAM Control Panel. Through the use of SDAC.

What happens when the upper EWD display fails?. Upper display is automatically transferred to the lower display. ECAM single display mode is activated. The ECAM/ND transfer selector is activated. Both PFD and ND units fail.

What reconfiguration options are available in case of lower DU failure?. No automatic reconfiguration is possible. The ECAM works in dual display mode. PFD automatically takes over the lower DU. ND image is displayed on the PFD.

In the case of an upper EWD failure or if the upper display control potentiometer is turned to off, the upper display is automatically transferred on the __________ display. lower. ND. PFD. ECAM.

A system page can be recovered by pushing and holding a system key on the ECP or by rotating the ECAM/ND XFR selector on the switching panel in order to display the system page on the __________ side. ND. ECAM. PFD. SDAC.

In case of lower DU failure or if the lower display is turned to off, no automatic reconfiguration is possible, and the ECAM works in __________ display mode. single. dual. triple. full.

n case of EWD unit and SD unit failure, each crew member can permanently present the EWD on the ND unit by rotating the ECAM/ND transfer selector switch on the switching panel. true. false.

It is still possible to recover a system page by pushing and holding a system key on the ECP. true. false.

How should the annunciator light switch be set to test the clock?. On. Off. TEST. RESET.

What is the operational consequence of Class 1 failures?. Affects flight. No operational consequence. Only affects the cockpit. Requires maintenance.

What does the crew report in the logbook after a malfunction?. Cockpit effect. Flight time. Weather conditions. Maintenance procedures.