在动力装置表面或其周围安装有阻热隔板或封严层。 | 民用航空器维修人员执照英语参考试题

单选题 Each manual shall contain an Introduction which shall include a brief statement explaining the organization, content and method of using the manual in addition to lists, or references tolocations of lists, of vendor technical publications.

A、每本手册都应有导言, 内容除了包括厂家技术出版物清单、或清单的参考位置以外,还需简要说明手册的组织、内容和使用方法。

B、每本手册都应包括介绍,简要说明其组织机构、手册内容和手册使用方法。额外的清单或参考清单位置要包括在制造商技术出版物中发布。

C、每本手册都应有前言,其中要说明机构、内容,以及除了制造商技术出版物清单、清单位置的引用手册使用方法做简要说明。

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单选题 The Boeing 747 marked the beginning of a new era in air transport.

A、 The Boeing 747 symbolizes the beginning of a new era in air transport.

B、 The Boeing 747 is the first type of airplane in air transport.

C、 Modern air transport started from the Boeing 747.

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单选题 Accelerate Stop Distance is the distance required to accelerate an airplane to a specified speed and, assuming failure of an engine at the instant that speed is attained, to bring theairplane to a stop.

A、加速停止距离是指飞机按照要求加速到指定速度所需的距离,并假定在达到该距离的那一刻发动机发生故障,飞机需要停下来。

B、加速停止距离是指将飞机加速到指定速度,并假定在达到该速度的那一刻发动机发生故障,使飞机停下来所需的距离。

C、加速停止距离是指将飞机加速到规定速度,并推测在达到该速度时发动机故障,飞机须立即停下来。

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单选题 A position transmitter is located below the PCUs.

A、位置发射机安装在 PCU 下部。

B、位置发射机安装在 PCU 上方。

C、位置传感器位于 PCU 的下方。

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单选题相关组件和部件包含:乙醇泵、阀门、存储箱、螺旋桨防冰系统、机翼加热器、水管加热器、空速管加热器、进气道加热器、风挡雨刮,以及风挡防冰中的电防冰和热防冰装置。不包括基本的风挡面板。

A、 Those units and components include alcohol pump, valves, alcohol container, propelleranti-icing system, wing warmers, water line warmers, pitot warmers, scoop warmers, windshield wipers and the electrical anti-icing and heated air ice control. Does not include the basicwindshield panel.

B、 Those units and components include alcohol pump, valves, tanks, propeller anti-icing system, wing heaters, water line heaters, pitot heaters, scoop heaters, windshield wipers and theelectrical and heated air portion of windshield ice control. Does not include the basic windshield panel.

C、 Those units and components include alcohol pump, valves, tanks, propeller anti-icing system, wing heaters, plumbing heaters, air speed tube heaters, intake heaters, windshield wipers and the electrical and heated air ice control for windshield. Does not include the basic windshieldpanel.

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单选题涡桨发动机控制装置包括到调节器或等效装置的连杆装置和控制装置,以及从调节器或等效装置到螺旋浆调速器、燃油控制组件的连杆装置和控制装置,或其他受控组件。

A、 The turboprop engine controls include linkages and controls to the coordinator or equivalent and from the coordinator or equivalent to the propeller governor, fuel control unit, or other units being controlled.

B、 The control device of a turbojet engine includes a linkage mechanism and control device to a coordinator or equivalent device, as well as a linkage mechanism from a coordinator orequivalent device to a propeller governor, fuel control component, or other controlled components.

C、 The turboprop engine controls include a coordinator or equivalent device, a linkagemechanism, a control device, a propeller governor, a fuel control component, or other controlled components.

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单选题涡轮发动机包括控制流经发动机空气流量的压气机引气系统、空气冷却系统、用于发动机防冰的热空气系统和发动机启动系统。

A、 The turbo engine includes a compressor bleed system, air cooling system, hot air system, and engine starting system. The compressor bleed system can control the airflow through the engine, and the air cooling and hot air systems are used for engine anti-icing.

B、 The turbo engine includes a compressor exhaust system for controlling the airflow through the engine, a cooling air system for engine icing, and an engine starting system.

C、 The turbine engines include compressor bleed systems used to control flow of air through the engine, cooling air systems, heated air systems for engine anti-icing, and engine starting systems.

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单选题 Water displacing corrosion inhibiting compound has been applied during construction on certain airplanes in the locations shown in this figure. Periodic reapplication in these, and other locations, is required to maintain effectiveness of this protection.

A、 At the location shown in the figure, waterproof corrosion inhibiting compound has been used on certain aircraft construction. To keep the effectiveness of this protection, reapply the compound in these and other locations periodically.

B、 Water displaying corrosion inhibiting compound has applied on certain airplanes structure inthe locations in this figure. Periodic reapplication must be applied in these and other locations, so as to maintain effectiveness of this protection.

C、 Water displacing anti-seize compound has been applied on certain airplanes construction inthe locations in this figure. Periodic reapplication should be utilized in these and other locations, in order to keep effectiveness of the protection.

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