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设备系统操作理论翻译
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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。

答案:C

设备系统操作理论翻译
2447. 将襟翼控制手柄移动到一个单位位置
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3245. 注:该试验旨在确保襟翼位置指示系统处于零能量状态。
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1541. 检验/检查部分应提供接近和检查系统、组件或区域所需的信息和程序。
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314. This method is recommended as minimizing errors of distribution, and also informs owners of the availability of systems and equipment
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375. Keep tools away and pick up debris near the engine
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1026. List these sections under each trouble in order of probability
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1244. Flaperon is aircraft controls used on some swept wing airplanes that serve as both ailerons and wing flaps
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3084. This part provides for a uniform method of arranging and identifying specific subject material
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352. The air data computer( ) is an electronic computer in an aircraft that senses pitot pressure, static pressure, and total air temperature The ADC produces an indication of altitude, indicated airspeed, true airspeed, and Mach number, and its output is usable by any of the engine or flight control computers
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967. This chapter shall provide that information considered necessary by the manufacturer to properly level the aircraft for any of the various maintenance, overhaul or major repairs which might become necessary during the life of the aircraft
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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

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。

答案:C

设备系统操作理论翻译
相关题目
2447. 将襟翼控制手柄移动到一个单位位置

A. Move the slat control lever to a unit position

B. Move the flap control lever to the 1 unit position

C. Move the flaperon control lever to the 1 unit position

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3245. 注:该试验旨在确保襟翼位置指示系统处于零能量状态。

A. CAUTION: This test is to make sure that the flap position indicating system is in a zero condition.

B. NOTE: This test is to make sure that the flap position indicating system is in a zero condition.

C. NOTE: This tryout is to make sure that the flap position indicating system is in a zero energy state.

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1541. 检验/检查部分应提供接近和检查系统、组件或区域所需的信息和程序。

A. The inspection/check portion shall provide information and procedures necessary to supply access to system and check of a system, a unit, or an area.

B. The inspection/inspection section shall provide the information and procedures required to access and inspect the system, component or area.

C. The inspection/check portion shall provide information and procedure necessary to gain access to and inspection or check of a system, a unit, or an area.

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314. This method is recommended as minimizing errors of distribution, and also informs owners of the availability of systems and equipment

A. 为了减少分配误差,推荐使用该方法,同时将系统和设备的功能特性告知所有者。

B. 为使辨别时产生的误差最小化,推荐使用该方法,同时对所有者说明系统和设备的使用方法

C. 建议采用该方法,以最大程度地减少分配出错,同时使所有者获知系统和设备的可用性。

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375. Keep tools away and pick up debris near the engine

A. 请勿将工具和碎片置于发动机附近。

B. 把除工具外的其它物品(例如碎片)从发动机附近清除

C. 把工具和发动机上的碎片移除。

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1026. List these sections under each trouble in order of probability

A. 把这些部分中的每一个故障按概率的顺序列出。

B. 把这些部分按概率的顺序列在每个故障下面。

C. 把这些故障列在每个部分下面为了增加概率。

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1244. Flaperon is aircraft controls used on some swept wing airplanes that serve as both ailerons and wing flaps

A. Flaperon plays the role of both ailerons and spoiler On some swept wing airplanes.

B. On some swept wing airplanes, Flaperon functions both ailerons and flaps.

C. Flaperon is aircraft controls used on some swept wing airplanes that serve as both elevator and wing flaps.

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3084. This part provides for a uniform method of arranging and identifying specific subject material

A. 本部分用于相同的安排方法和识别特定主材料

B. 本部分规定了安排和识别某些主材料的同类方法

C. 本部分提供了安排和识别特定主素材的统一方法

https://www.shititong.cn/cha-kan/shiti/0009ffba-8e34-edff-c0b8-ef8d402da900.html
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352. The air data computer( ) is an electronic computer in an aircraft that senses pitot pressure, static pressure, and total air temperature The ADC produces an indication of altitude, indicated airspeed, true airspeed, and Mach number, and its output is usable by any of the engine or flight control computers

A. Air date computer got pitot and static pressure, together with the total air temperature.

B. The ADC is not able to give output to flight control computers.

C. The ADC can produces an indication of indicated airspeed and true airspeed, but can not produce Mach number.

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967. This chapter shall provide that information considered necessary by the manufacturer to properly level the aircraft for any of the various maintenance, overhaul or major repairs which might become necessary during the life of the aircraft

A. 本章应提供制造商认为必要的信息,以便在飞机使用寿命期内可能需要进行的各种维修、大修或重大维修时正确校平飞机。

B. 本章提供制造商认定的必要信息用以保证飞机在全寿命期中进行各种维护,翻修或大修后正确校准飞机。

C. 本章提供制造商确定需要的信息用以保证飞机在运行期间进行各种维修,翻修或大修后适当配平飞机。

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