A320- 31 INSTRUMENTOS

In case of failure of PFD (primary flight display) it is transferred to the screen of nd (navigation display). Manually. automatically. Manually and automatically.

how many screens has the eis (electronic instrument system). Two screens ecam. Two screens ecam, plus four screens efis. Four efis screens.

Which is the basic rule of the DMCs (displays manament computer). Generate audio alarms. Generate amber alarms. Generate images to be displayed on the screens.

through which selector in the ECP (ECAM control panel) can transfer the image of ECAM to EFIS. The eis / dmc knob. The att / hgd knob. The ecam / nd xfr knob.

Of which consist the attention calls (attention getters). A master warning button and a master caution button in front of the pilot and co-pilot position. A call of attention aural and a light of master warning in the screen of e / wd. A master warning button and a master caution button on the overhead panel.

Where are the primary motor parameters displayed. Ecam lower. E/WD. PFD.

The EIS (electronic instrument system) screens are interchangeable with each other. yes. no.

Which computer generates all the alarm messages that are displayed?. The SDACs. The DMCs. The FWCs.

The inputs that the FWC receives are to process what kind of alarms. Any. Amber. Red.

Which computer processes flight phases as well as checklists. DMCs. SDACs. FWCs.

The basic function of the SDACs is. Receive, process, send signals to DMCs and FWCs. Send direct information to the screens. To process aural alarms.

What types of alarms do SDACs process. Aural. Amber. Red.

If we lose the DMC1, how can we recover the screens. placing the selector knob ecp ECAM / nd xfr. placing the selector knob of the EIS DMC to the position capt3. Can not be retrieved.

If we lose the screen where the primary engine parameters are displayed, is this transferred. Manually. automatically. nothing happens.

During takeoff and landing, many of the alarms are inhibited to avoid crew distraction. yes. no.

The FOB (fuel on board) is displayed on the SD (system display). yes. no.

a fault occurred page shows a summary of the affected systems. cruise page. status page. no page.

In which configuration we are shown on the screen E / WD ADV (advisory). Without any screen. Ecam dual display (dual display operation). Ecam mono display (single-screen operation).

What does an overflow arrow mean at the bottom of the E/WD screen. A- That we have no more space on the screen to view messages. B - Are displayed in the right area E/WD. A and B are correct.

that screens are permanent data. SD. E/WD. PFD.

The status page of the airplane (status page), when it is called automatically. With Slats > 2 (in approach). When lowering the landing gear in approach. you have to call it manually.

How many ways does the system for presenting ECAM pages operate. Two modes. Four modes. Three modes.

What page is displayed on the ground with engines off. Cruise page. Door page. Wheel page.

Which page is displayed in phase 6. Flt / crt page. Wheel page. Cruise page.

When we press the (all) key on the ECP (Ecam control panel) we display the pages with. 2 sec intervals. 3 sec intervals. 1 sec intervals.

The function key (emer canc) on the ECP is for. Cancel any aural alarm. Cancel the red warning (atettention geaters). Cancel the T.O inhibit.

If we call the status page from the ECP and there is no content for how long it will be viewed. 10 seconds. 3 seconds. 5 seconds.

An alarm level three match. A-amber warning. B-red warning. C-aural warning. D- b and c are correct.

An alarm level two matches. A-amber warning. B-red warning. C-aural warning. D- a and c are correct. E-b and c are correct.

Where alarms level 1 are displayed. E/WD. S/D. Status page in the maintenance area.

An independent fault is. Which has no consequence in other systems has direct. consequences in other systems. None of the above.

A secondary fault is. Is that caused by another fault. Has no consequences on other systems. None of the above.

When a parameter increases outside the normal range. An aural alarm is present. Is called the page automatically, showing the parameter by pressing. Presents a master caution and a single chime.

Which basically consists of the ECAM (electronic centralized aircraft monitoring). PFDs and NDs. SDACs, DMCs, FWCs. DMCs and SDACs.

The bus where the messages travel (memo messages) Is format. Arinc 429. Rs422. analogous.

Who control the master lights caution and master warning. SDACs. DMCs. FWCs.

Which is the connection used to transmit signals and display them in the DU/S (Display units). Feefback. Bus for messages and data. A master dsdl (master didicated serial data link).

Which keys are wired directly from the ECP (ecam control panel) to the FWCs. Clr, rcl and sts. Clr, rcl, sts, and emer. Cancel. Clr, sts, and emer. Cancel.

in which screen is displayed barometric altitude. NDs. PFDs. SD.

in which screen is displayed the attitude of the aircraft. NDs. PFDs. SD.