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题目内容
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单选题
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In normal operation,are the navigation systems controlled by RMP1 ?

A、Yes.

B、No.

答案:B

机型英语-翻译南航
The inner cell is refuelled only when :
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When is FD engaged?
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The speed/Mach switching during a managed flight:
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With the MAIN OFF pushbutton previously pressed, how can you switch on the WINDOWS lighting at FULL BRIGHTNESS ?
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Which equipment controls the battery contactor ?
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How can a flap runaway be detected ?
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When is the aileron servo-control actuator in damping mode ?
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How are the smoke detectors connected to the SDCU ?
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Which computer controls the engine thrust, either in manual mode or autothrust mode ?
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When there is a low level in one inner cell :
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机型英语-翻译南航
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机型英语-翻译南航

In normal operation,are the navigation systems controlled by RMP1 ?

A、Yes.

B、No.

答案:B

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机型英语-翻译南航
相关题目
The inner cell is refuelled only when :

A. Center tank is full

B. Outer cell is full

C. Outer cell is empty

https://www.shititong.cn/cha-kan/shiti/00051010-5716-70c1-c0f1-a6c9d0d6c300.html
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When is FD engaged?

A. As soon as at least one AP is engaged.

B. As soon as A/THR is engaged.

C. As soon as electrical power is available.

https://www.shititong.cn/cha-kan/shiti/00051010-57a8-d4e2-c0f1-a6c9d0d6c300.html
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The speed/Mach switching during a managed flight:

A. Is automatic.

B. Must be performed by the crew for the climb phase only.

C. Must be performed by the crew both for the clim and the descent phases.

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With the MAIN OFF pushbutton previously pressed, how can you switch on the WINDOWS lighting at FULL BRIGHTNESS ?

A. You can press the BRIGHT(BRT) pushbutton associated to the WINDOWS lighting.

B. You can press the MAIN ON pushbutton and then press the ENTRY AREAS BRIGHT(BRT) and CEILING(CLG) pushbuttons.

C. You can press the WINDOWS(WDO) pushbutton.

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Which equipment controls the battery contactor ?

A. GCU.

B. BCL.

C. Static inverter.

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How can a flap runaway be detected ?

A. By comparison between the SFCC commands and the Asymmetry PPU signals.

B. By comparison between the SFCC commands and the Feedback PPU signals.

C. By comparison between Asymmetry PPU and the Feedback PPU signals.

https://www.shititong.cn/cha-kan/shiti/00051010-5757-78cc-c0f1-a6c9d0d6c300.html
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When is the aileron servo-control actuator in damping mode ?

A. When there is no command signal to the servo-valve.

B. Only when the solenoid valve is de-energized.

C. When the solenoid valve is de-energized or the actuator is not pressurized.

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How are the smoke detectors connected to the SDCU ?

A. In parallel

B. In series

C. In a loop

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Which computer controls the engine thrust, either in manual mode or autothrust mode ?

A. FMGC.

B. FCU.

C. ECU.

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When there is a low level in one inner cell :

A. One Intercell Transfer Valve opens.

B. Two transfer Valve in one wing, open.

C. Two transfer Valve, one in each wing, open.

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