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1475. The section of the engine in which the air and fuel are combined and burned Includes items such as burner cans, cases, etc

A、 发动机中空气和燃油混合并燃烧的部分。包括项目,如火焰筒,壳体等。

B、 发动机中空气和燃油混合并在火焰筒和壳体内燃烧。

C、 发动机中空气和燃油混合并燃烧的部分。包括火焰筒,壳体。

答案:A

设备系统操作理论翻译
184. The primary function of the hydraulic pressure system is to supply pressure flying controls for the operation of flying controls
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2164. Those units and components are used for recording data not related to specific systems
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3173. The manufacturer shall include, wherever applicable, the office or department to contact to obtain special repair or overhaul information not covered in the Maintenance Manual
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2287. 用温度计测量外界大气温度和驾驶舱温度
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2487. Heat causes the pressure to increase
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61. Each section shall be started on a right-hand page The manufacturer’s masthead, publication title, airplane model, and issue or revision date shall appear on all pages
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177. The page number shall be in the lower left corner and the date of issue in the lower right corner, for left-hand pages
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1589. 燃油渗漏会降低发动机性能。
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899. 该规范根据飞机的复杂性提供了手册编制的灵活性,同时保持了结构、定义和性能信息的商度标准化。
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225. This Section shall contain a legible statement in a prominent location to the effect that the Airworthiness Limitations Section is FAA approved
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设备系统操作理论翻译

1475. The section of the engine in which the air and fuel are combined and burned Includes items such as burner cans, cases, etc

A、 发动机中空气和燃油混合并燃烧的部分。包括项目,如火焰筒,壳体等。

B、 发动机中空气和燃油混合并在火焰筒和壳体内燃烧。

C、 发动机中空气和燃油混合并燃烧的部分。包括火焰筒,壳体。

答案:A

设备系统操作理论翻译
相关题目
184. The primary function of the hydraulic pressure system is to supply pressure flying controls for the operation of flying controls

A. 液压系统的主要压力用于飞行控制系统

B. 飞行控制运行所需的压力来源于起主要作用的液压系统

C. 液压系统的主要功能是为飞行控制系统的操作提供压力。

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2164. Those units and components are used for recording data not related to specific systems

A. Those units and components are used to keep account of data that is unrelated to a particular system.

B. The purpose of those units and components is to obtain values that are independent of a particular system.

C. The function of these units and components is to save the files that have nothing to do with a peculiar system.

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3173. The manufacturer shall include, wherever applicable, the office or department to contact to obtain special repair or overhaul information not covered in the Maintenance Manual

A. 制造商应该在适当的地方,如办公室或部门,联系获得超出手册以外其他关于特殊修理和大修的信息。

B. 制造商应该在适当的地方,如办公室或部门,以联系来获得手册中没有涵盖的重要修理或者大修信息。

C. 制造商应该在适当的地方包括办公室或部门,以联系到来获得在维修手册中没有涵盖的特殊修理或者大修的信息。

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2287. 用温度计测量外界大气温度和驾驶舱温度

A. Measure the Outside Air Temperature and the temperature in the cockpit with a thermometer.

B. Do the Outside Air Temperature and the temperature in the cabin with a barometer.

C. Measure the Surrounding Air Temperature and the temperature in the cockpit with a thermometer.

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2487. Heat causes the pressure to increase

A. Heat will lead to an increased pressure.

B. The pressure will go up with increasing amount of heat.

C. The increased pressure is caused by the heating system.

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61. Each section shall be started on a right-hand page The manufacturer’s masthead, publication title, airplane model, and issue or revision date shall appear on all pages

A. 每个部分应从右侧页面开始。 制造商的标头,出版物标题,飞机注册号以及发行或修订日期应显示在所有页面上。

B. 每个部分应从右侧页面开始。 制造商的标头,出版物标题,飞机注册号以及发行日期应显示在所有页面上。

C. 每个部分应从右侧页面开始。 制造商的标头,出版物标题,飞机型号以及发行或修订日期应显示在所有页面上。

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177. The page number shall be in the lower left corner and the date of issue in the lower right corner, for left-hand pages

A. 对于右侧页面,页码应位于右下角,发行日期应位于左下角

B. 对于左侧页面,页码应位于右下角,发行日期应位于左下角

C. 对于左侧页面,页码应位于左下角,发行日期应位于右下角

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1589. 燃油渗漏会降低发动机性能。

A. Fuel leaks can decrease engine performance.

B. A fuel leak can cause the engine to operate badly.

C. Fuel leakage may be lower engine performance.

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899. 该规范根据飞机的复杂性提供了手册编制的灵活性,同时保持了结构、定义和性能信息的商度标准化。

A. The Specification provides flexibility in Handbook preparation based on the complexity of the airplane while maintaining a high degree of standardization of arrangement, definitions, and performance information.

B. The Specification provides flexibility in Handbook preparation based on the complicacy of the airplane, but ignoring a high degree of standardization of structure, definitions, and performance information.

C. The Specification provides uniformity in Handbook preparation based on the simplicity of the airplane while retaining a high degree of standardization arrangement. definitions; and performance information.

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225. This Section shall contain a legible statement in a prominent location to the effect that the Airworthiness Limitations Section is FAA approved

A. 在本节显著的位置应包括一个清楚的声明,内容是适航限制部分由FAA批准

B. 当本节很显著标示出适航限制部分,这说明FAA批准了其影响。

C. 本节应在显著位置包括一份清晰的声明,说明适航限制部分的影响是FAA批准的。

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