Flight Instruments Flashcards

0
Q

Is the radar display available in all modes of the ND selector?

A

No, radar is not available in PLAN

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1
Q

Are there any procedures that call for the use of the VOR switch installed on the EFIS CONTROL panel?

A

Yes, VOR approaches or DME info

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2
Q

When the ILS pb is selected, where will the localizer and g/s scales be displayed?

A

Onside PFD

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3
Q

What does STS indicate when displayed on the EWD?

A

The STATUS page holds messages

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4
Q

If the upper ECAM display fails, what happens automatically?

A

EWD display replaces the SD display on the lower ECAM

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5
Q

If the lower ECAM fails, can we display the lower ECAM data?

A

We could press and hold the desired systems page pb on the ECAM control panel, and the page will be displayed on the upper ECAM. we could also select the rotary switch labeled ECAM/ND XFR on the switching panel to Capt or FO.

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6
Q

Describe the purpose of the EIS switching panel?

A

Permits cockpit display screens to access secondary sources.

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7
Q

Can the lower ECAM display be transferred to another display?

A

Yes

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8
Q

DMC 1 (or 2) has failed. Can the information on the affected displays be restored?

A

Yes. Rotate the switch labeled EIS DMC to replace the failed DMC with DMC 3.

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9
Q

What happens when TO CONFIG pb is depressed?

A

An application of takeoff power is simulated. A warning occurs if The aircraft is not in the takeoff configuration

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10
Q

If during flight we received continuous spurious warning messages that we knew to be incorrect, is there a way to cancel this caution?

A

By depressing the EMER CANC pb, we can cancel the level 1 and 2 caution msgs only (along with the MC), however that specific caution is now inhibited for the remainder of the flight.

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11
Q

We have pressed the EMER CANC pb. How can we get the system back to normal?

A

By pressing the RCL pb for more than 3 seconds.

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12
Q

How could we check the status page for inoperative systems or MX messages?

A

Press the STS pb

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13
Q

Why is it very important to maintain a ‘lights out’ condition on the ECP during the flight?

A

Because the automatic phase of flight function and display of the relative system on the lower ECAM during an abnormal will be inhibited by the page we have displayed.

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14
Q

We have 3 DMCs which acquire and process all info and signals received from the sensors and computers to generate the images displayed on the DUs. Where is the information normally displayed from DMC 1 and 2?

A

Normally DMC 1 supplies data to PFD 1, ND 1, and upper ECAM. DMC 2 supplies data to PFD2, ND 2, and lower ECAM.

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15
Q

How is a DMC failure displayed?

A

A diagonal display on the associated DUs.

16
Q

If a display unit failed, would the screen have a diagonal line through it?

A

No, the display would be blank.

17
Q

How many VOR and DME receivers are on the aircraft?

A

2 of each

18
Q

If all systems were working normally, and a crew member wanted to remotely tune a VOR through the RMP, would that have any effect on the FMGC NAV functions?

A

Yes, if either pilot lifts the guard and presses NAV, auto tuning and FMGC radio position updating is superseded and the RAD NAV page is blanked. NAV on RMP3 will have no effect.

19
Q

When would you use the RMP to tune an ILS?

A

When both FMGCs or MCDUs are inoperative, or during emergency electrical configuration.

20
Q

Can 2 different ILS frequencies be tuned at the same time?

A

No, whether auto tuned, manually tuned, or RMP tuned, we can only input one ILS freq.

21
Q

If the LOC or G/S fails, what would be indicated on the PFD?

A

In place of the LOC or GS diamond, we would see LOC or GS in red on the PFD of the failed receiver. In ROSE ILS, we would see a red LOC or GS flag.