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1644. This tool is used to align the mark on the cable tension regulator with the related graduation on the fixed scale

A、 该工具用于将钢索张力调节器上的标记与固定标盘上的相关指针对齐。

B、 该工具用于将钢索张力调节器上的标记与固定标盘上的相关刻度对齐。

C、 该工具用于将钢索弹簧调节器上的标记与固定标盘上的相关刻度对齐。

答案:B

设备系统操作理论翻译
941. IF THE FLAP EXTENSION DOES NOT( ) WITH THE POSITION OF THE FLAP CONTROL LEVER, DO THE RIGGING PROCEDURE AGAIN
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2421. Excessive trim, however, has the effect of reducing not only aerodynamic efficiency but also primary control travel distance in the direction the trim is applied
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1820. make sure that there is no blockage in the pipe
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1011. When the entire storage area is full, new fault data, ie data for the current flight leg, will replace/overwrite the data for the oldest flight leg in the fault history
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486. The CAP will address primary and secondary airframe components, and primary and secondary systems to accomplish the stated objective of continued airworthness
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887. Questions of compliance with the Specification shall be referred to the General Aviation Manufacturers Association ( ) and the Federal Aviation Administration ( ) for resolution
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1093. The roll command continues to hold track The pitch command continues to hold speed, attitude, or a mix of speed and attitude
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2617. Examine the bottom skin panels of the fuselage for cracks
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1749. If it is necessary to decrease the cable tension more,use the turnbuckle
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1037. The bar moves down after 20 seconds
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设备系统操作理论翻译

1644. This tool is used to align the mark on the cable tension regulator with the related graduation on the fixed scale

A、 该工具用于将钢索张力调节器上的标记与固定标盘上的相关指针对齐。

B、 该工具用于将钢索张力调节器上的标记与固定标盘上的相关刻度对齐。

C、 该工具用于将钢索弹簧调节器上的标记与固定标盘上的相关刻度对齐。

答案:B

设备系统操作理论翻译
相关题目
941. IF THE FLAP EXTENSION DOES NOT( ) WITH THE POSITION OF THE FLAP CONTROL LEVER, DO THE RIGGING PROCEDURE AGAIN

A. UNIFY

B. CONFORM

C. AGREE

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2421. Excessive trim, however, has the effect of reducing not only aerodynamic efficiency but also primary control travel distance in the direction the trim is applied

A. 然而,过度的配平不仅减少了飞机的空气动力效能,而且减少了配平主控制舵面方向上的偏转行程。

B. 然而,额外的配平不仅减少了飞机的空气动力效能,而且减少了配平应用方向上的主控制舵面的偏转行程。

C. 然而,额外的配平不仅减少了飞机的空气动力效能,而且减少了配平主控制舵面方向上的偏转行程。

https://www.shititong.cn/cha-kan/shiti/0009ffb1-44bf-3e63-c0b8-ef8d402da900.html
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1820. make sure that there is no blockage in the pipe

A. make sure that there is something in the pipe

B. make sure that there is nothing in the pipe

C. make sure that blockage is in the pipe

https://www.shititong.cn/cha-kan/shiti/0009ffad-f67f-ae16-c0b8-ef8d402da900.html
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1011. When the entire storage area is full, new fault data, ie data for the current flight leg, will replace/overwrite the data for the oldest flight leg in the fault history

A. 当整个存储区域已满时,新的故障数据和当前航班的数据,将替换/覆盖故障历史中最老的航班的数据。

B. 当整体存储区域已满时,新的故障数据,例如当前飞行段的数据,将替换/覆盖具有最早故障历史航班的数据。

C. 当整个存储区域已满时,新的故障数据,即当前飞行段的数据,将替换/覆盖故障历史中最早的飞行段的数据。

https://www.shititong.cn/cha-kan/shiti/0009ffaa-70d1-4809-c0b8-ef8d402da900.html
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486. The CAP will address primary and secondary airframe components, and primary and secondary systems to accomplish the stated objective of continued airworthness

A. The CAP focuses on primary and secondary components of the fuselage structure,as well as primary and secondary systems.The purpose is to achieve the goal of sustained airworthiness.

B. The CAP emphasizes not only the primary and secondary components of the airframe,but also its primary and secondary systems to achieve the higher goal of continued airworthiness

C. The CAP stresses both the primary and secondary components of the airframe,as well as its primary and secondary systems,with the aim of modifying the direction of continued airworthiness

https://www.shititong.cn/cha-kan/shiti/0009ffa1-9bf9-8d91-c0b8-ef8d402da900.html
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887. Questions of compliance with the Specification shall be referred to the General Aviation Manufacturers Association ( ) and the Federal Aviation Administration ( ) for resolution

A. Questions regarding compliance with this Code should be referred to the General Aviation Manufacturers Association (GAMA) and the Federal Aviation Administration (FAA).

B. Disputes concerning this specification shall be referred to the General Aviation Manufacturers Association (GAMA) and the Federal Aviation Administration (FAA) for resolution.

C. Questions regarding this specification should be referred to the General Aviation Manufacturers Association (GAMA) and the Federal Aviation Administration (FAA) for compliance.

https://www.shititong.cn/cha-kan/shiti/0009ffa7-3b42-c155-c0b8-ef8d402da900.html
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1093. The roll command continues to hold track The pitch command continues to hold speed, attitude, or a mix of speed and attitude

A. The roll command continues to hold attitude.

B. The pitch command continues to hold attitude.

C. The roll command continues to hold speed, attitude, or a mix of speed and attitude.

https://www.shititong.cn/cha-kan/shiti/0009ffaa-70d2-5b39-c0b8-ef8d402da900.html
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2617. Examine the bottom skin panels of the fuselage for cracks

A. 检查机身蒙皮盖板的底部有无裂纹。

B. 检查底部蒙皮盖板和机身有无裂纹。

C. 检查机身底部蒙皮盖板有无裂纹。

https://www.shititong.cn/cha-kan/shiti/0009ffb5-69cf-b82e-c0b8-ef8d402da900.html
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1749. If it is necessary to decrease the cable tension more,use the turnbuckle

A. 如有必要进一步减小钢索张力,可使用松紧螺套。

B. 如有必要进一步降低钢索张力,可使用张力计。

C. 如有必要进一步调节钢索长度,可使用旋转带子。

https://www.shititong.cn/cha-kan/shiti/0009ffad-f67e-cadd-c0b8-ef8d402da900.html
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1037. The bar moves down after 20 seconds

A. 20秒后将杆向下移。

B. 20秒后将杆消失。

C. 20秒后将阻块消失。

https://www.shititong.cn/cha-kan/shiti/0009ffaa-70d1-a043-c0b8-ef8d402da900.html
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