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The colour of the V/S indications change to:

A、Red when in presence of a corrective RA detection.

B、Green when in presence of a corrective RA detection.

C、Red or green when in presence of a corrective RA detection depending on the sector band in which they are.

答案:C

320机型英语考试题库
When does the ECU Permanent Magnet Alternator or supply the ECU ?
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With the engine generators on line, what does the EXT PWR ON light indicate when lit ?
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What happens when the LAVatory pushbutton on the FAP is pressed?
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How can the avionic smoke detector be tested ?
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On ground, the engines are stopped, how do you close the LP valve ?
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What provides the selection of the igniters A/B ?
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AP1 is engaged, FDs are engaged, A/THR1 is engaged. How do the FMGCs work in normal conditions?
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When is the CVR energized,with the aircraft on ground and engines shut down ?
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To which tank does the recirculated fuel return ?
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What is displayed on the status page ?
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320机型英语考试题库

The colour of the V/S indications change to:

A、Red when in presence of a corrective RA detection.

B、Green when in presence of a corrective RA detection.

C、Red or green when in presence of a corrective RA detection depending on the sector band in which they are.

答案:C

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320机型英语考试题库
相关题目
When does the ECU Permanent Magnet Alternator or supply the ECU ?

A. When N2 is above 12%.

B. When an engine is started.

C. Only if the Aircraft Electrical Power fails.

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With the engine generators on line, what does the EXT PWR ON light indicate when lit ?

A. The external ground cart is supplying the AC BUS 1 and 2

B. The External Power Contactor is controlled to close.

C. The external ground cart is supplying the AC/DC ground service buses.

https://www.shititong.cn/cha-kan/shiti/00051009-33ab-c3ae-c0f1-a6c9d0d6c300.html
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What happens when the LAVatory pushbutton on the FAP is pressed?

A. The LAVATORIES are illuminated at FULL BRIGHTNESS, when the associated LAVATORY DOOR(s) is (are) locked.

B. The LAVATORIES are illuminated at 50% brightness, when the associated LAVATORY DOOR is open or closed.

C. A and B are correct.

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How can the avionic smoke detector be tested ?

A. Permanently by the AEVC.

B. By a dedicated TEST pushbutton.

C. By a manual test from the CFDS.

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On ground, the engines are stopped, how do you close the LP valve ?

A. By releaseing out the ENG FIRE P/B.

B. By removing electrical power form A/C.

C. The valve is already closed.活门早已关闭

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What provides the selection of the igniters A/B ?

A. The Engine panel.

B. The ECAM control panel.

C. The ECU.

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AP1 is engaged, FDs are engaged, A/THR1 is engaged. How do the FMGCs work in normal conditions?

A. Each FMGC drives its own FD symbols, FMGC1 supplies both FMAs and controls the flight controls and engines.

B. FMGC1 drives FD symbols on both PFDs,supplies both FMAs and controls the flight controls and engines.

C. FMGC1 drives FD sybols on the Captain PFD, supplies FMA on Captain PFD and controls the flight controls. FMGC2 controls the engines.

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When is the CVR energized,with the aircraft on ground and engines shut down ?

A. When the parking brake is applied.

B. During 5 minutes after the second engine is shut down.

C. When CVR TEST pushbutton is pressed.

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To which tank does the recirculated fuel return ?

A. Wing tank outer cell ,

B. Center tank ,

C. Wing tank inner cell .

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What is displayed on the status page ?

A. Memo messages.

B. Opearational status messages.

C. Warning message

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