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2526. The turbine clearance control sensor supplies the EEC with temperature data from the high pressure turbine shroud

A、 涡轮间隙控制传感器提供高压涡轮保护罩的温度数据给EEC。

B、 涡轮间隙控制传感器提供来自高压涡轮保护罩的EEC温度数据。

C、 涡轮间隙控制传感器提供高压涡轮的温度数据给EEC。

答案:A

设备系统操作理论翻译
3303. CDCCL是一种识别特定设计配置特征的方法,旨在排除飞机在使用寿命内的燃油箱点火源。
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66. Vertical axis of an aircraft is an imaginary line passing vertically through the center of gravity of an aircraft The vertical axis is called the Z-axis,or the yaw axis
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2357. When you hyphenate long technical names to make them clearer to the reader, a hyphenated group of words also counts as one word in the applicable noun cluster
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331. The format of the cruise performance presentation is at the discretion of the airplane manufacturer but should not rely on devices such as a power computer
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2758. The design authority must give approval to changes that you make to the repair scheme
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2657. Manually override the start sequence
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2822. 适用时,本章可代替飞机的-00至-70部分,以飞机附带的供应商资料为准。本章中可能包含制造商认为适用的大修资料。
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1553. 在你移动副翼之前,告诉所有人离开机翼
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1833. Examine the surface for cracks
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1812. 重着陆会导致发动机冲击负荷。
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设备系统操作理论翻译
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设备系统操作理论翻译

2526. The turbine clearance control sensor supplies the EEC with temperature data from the high pressure turbine shroud

A、 涡轮间隙控制传感器提供高压涡轮保护罩的温度数据给EEC。

B、 涡轮间隙控制传感器提供来自高压涡轮保护罩的EEC温度数据。

C、 涡轮间隙控制传感器提供高压涡轮的温度数据给EEC。

答案:A

设备系统操作理论翻译
相关题目
3303. CDCCL是一种识别特定设计配置特征的方法,旨在排除飞机在使用寿命内的燃油箱点火源。

A. CDCCLs are a means of identifying certain design configuration features intended to preclude a fuel tank ignition source for the operational life of the airplane.

B. CDCCLs are a means of sign certain design configuration features intended to preclude a fuel tank ignition source for the operational life of the airplane.

C. CDCCLs are a means of mark certain design configuration features intended to preclude a fuel tank ignition source for the operational life of the airplane.

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66. Vertical axis of an aircraft is an imaginary line passing vertically through the center of gravity of an aircraft The vertical axis is called the Z-axis,or the yaw axis

A. Vertical axis passes horizontally through the center of gravity of an aircraft.

B. Vertical axis passes vertically through the center of gravity of an aircraft.

C. Vertical axis of an aircraft is an imaginary line passing vertically through the center of gravity of an aircraft. The vertical axis is called the pitch axis.

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2357. When you hyphenate long technical names to make them clearer to the reader, a hyphenated group of words also counts as one word in the applicable noun cluster

A. 当你连接较长的技术名称以使它们更清楚地展示给读者时,连接的一组单词也可以算作适用的名词词组中的一个单词。

B. 当你用连字符连接较长的技术名称以使读者更清楚时,用连字符连接的一组单词也可视为适用的名词词组中的一个单词。

C. 当你使用较长的技术名称来使其结构更清楚地呈现给读者时,所使用的词组也可视为复杂的名词词组中的一个单词。

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331. The format of the cruise performance presentation is at the discretion of the airplane manufacturer but should not rely on devices such as a power computer

A. The form of the cruise performance presentation is at the option of the airplane manufacturer but should not be independent of devices such as a power computer

B. The format of the cruise performance presentation is decided by the airplane manufacturer itself but should not depend on devices such as a power computer

C. The layout of the cruise performance presentation is at the discretion of the airplane manufacturer, however, devices such as a power computer should not be relied on

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2758. The design authority must give approval to changes that you make to the repair scheme

A. The design authority must approve any amendments you make to the repair scheme.

B. The design authority must approve any supports you make to the repair scheme.

C. The design authority must approve any amendments you make to the maintenance plan.

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2657. Manually override the start sequence

A. 人工超控起动顺序。

B. 按手册重写起动顺序。

C. 手动覆盖起动序列。

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2822. 适用时,本章可代替飞机的-00至-70部分,以飞机附带的供应商资料为准。本章中可能包含制造商认为适用的大修资料。

A. This Chapter may refer to supplier data, furnished with the aircraft, in lieu of the following sections -00 through -70, as applicable. Overhaul data, considered applicable by the manufacturer, may be included in this chapter.

B. This Chapter may refer to manufacturer material, furnished with the aircraft, in lieu of the following sections -00 through -70, as applicable. Overhaul data, considered applicable by the manufacturer, may be included in this chapter.

C. This Chapter may refer to supplier data, furnished with the aircraft, in lieu of the following sections -00 through -70, as applicable. Manual data, considered applicable by the supplier, may be included in this chapter.

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1553. 在你移动副翼之前,告诉所有人离开机翼

A. Before you move the spoilers, tell all persons to get off the wings.

B. Before telling all persons to get off the wings, you move the ailerons.

C. Before you move the ailerons, tell all persons to get off the wings.

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1833. Examine the surface for cracks

A. 检查表面是否有腐蚀。

B. 检查表面是否有凹坑。

C. 检查表面是否有裂纹。

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1812. 重着陆会导致发动机冲击负荷。

A. A hard landing may be the result of shock loading of the engine.

B. Shock loading of an engine may result in a heavy landing.

C. A heavy landing can cause shock loading of the engine.

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