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Which ADIRU does not supply the DMC 1 ?

A、ADIRU 1

B、ADIRU 2

C、ADIRU 3

答案:B

机型英语-翻译南航
A/THR cyan indication in the engagement status zone indicates that the autothrust is:
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When are the IGVs commanded to the idle position ?
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What is the purpose of the IDG SHUT-OFF sensor ?
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In normal opearation ,how is the height data provided ?
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Where is the main drain port of the potable water system ?
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How is the engine LP fuel shut off valve controlled ?
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The Electronic Control Box has :
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The aircraft is in cruise with AP1 engaged. What happens when Ap2 is engaged?
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Which Centralized Fault Display System functions are available in BACKUP mode on ground ?
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What happens when a generator fault is detected?
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机型英语-翻译南航
题目内容
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机型英语-翻译南航

Which ADIRU does not supply the DMC 1 ?

A、ADIRU 1

B、ADIRU 2

C、ADIRU 3

答案:B

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机型英语-翻译南航
相关题目
A/THR cyan indication in the engagement status zone indicates that the autothrust is:

A. Disengaged.

B. Engaged and not active.

C. Engaged and avtive.

https://www.shititong.cn/cha-kan/shiti/00051010-57bc-a288-c0f1-a6c9d0d6c300.html
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When are the IGVs commanded to the idle position ?

A. During main engine start.

B. During APU start, or above 23000ft.

C. If EGT is too high.

https://www.shititong.cn/cha-kan/shiti/00051010-567a-972e-c0f1-a6c9d0d6c300.html
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What is the purpose of the IDG SHUT-OFF sensor ?

A. To stop the Center Tank Pumps.

B. To restart Cooling fuel recirculation.

C. To stop the Cooling fuel recirculation.

https://www.shititong.cn/cha-kan/shiti/00051010-571b-f5dd-c0f1-a6c9d0d6c300.html
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In normal opearation ,how is the height data provided ?

A. By system 1 to Capt PFD and F/O PFD

B. By system 2 to CAPT PFD and F/O PFD

C. By system 1 to CAPT PFD and by system 2 to F/O PFD

https://www.shititong.cn/cha-kan/shiti/00051010-56b5-b292-c0f1-a6c9d0d6c300.html
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Where is the main drain port of the potable water system ?

A. On the potable water service panel.

B. On the forward water service panel.

C. On both.

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How is the engine LP fuel shut off valve controlled ?

A. By the Engine fire pushbutton.

B. Automatically when a fire is detected.

C. By the MASTER lever or by the Engine fire Pushbutton.

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The Electronic Control Box has :

A. Restricted authotity over APU operation.

B. Only APU monitoring function.

C. Full authority over APU operation.

https://www.shititong.cn/cha-kan/shiti/00051010-5674-f962-c0f1-a6c9d0d6c300.html
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The aircraft is in cruise with AP1 engaged. What happens when Ap2 is engaged?

A. AP1 remains active,AP2 is in standby.

B. AP2 becomes active with AP1 in standby.

C. AP2 becomes active, AP1 is disengaged.

https://www.shititong.cn/cha-kan/shiti/00051010-57a4-5af4-c0f1-a6c9d0d6c300.html
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Which Centralized Fault Display System functions are available in BACKUP mode on ground ?

A. None.

B. SYSTEM REPORT/TEST for main systems.

C. LAST LEG REPORT and LAST LEG ECAM REPORT.

https://www.shititong.cn/cha-kan/shiti/00051010-56e6-825d-c0f1-a6c9d0d6c300.html
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What happens when a generator fault is detected?

A. The exciter field is no longer supplied and the GCR trips.

B. The exciter field is still supplied and the GCR stays closed.

C. The exciter field is increased and the GCR trips

https://www.shititong.cn/cha-kan/shiti/00051010-5772-b133-c0f1-a6c9d0d6c300.html
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