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1105.Airplane performance data shall be presented in either graphical or tabular formats.

A、 Airplane primary data should be displayed neither in graphs and tables.

B、 Airplane behavior data shall be predicted in both graphical and tabular formats.

C、 Aircraft performance parameters can be represented graphically or in tables.

答案:C

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1255.Identify the disassembled parts with tags,this method will help you during the subsequent assembly procedures.
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74.Turn the clamps to free the pipes.
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2402.Adjust the clinometer until the bubble is in the center.
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2398.If you cannot hear the alarm,adjust the volume control.
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2935.此文件包含了附录 G 中描述的持续性适航的适当说明。
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1856.发动机功率控制系统可以控制主燃油控制器或调节器,包括涡轮螺旋桨发动机上螺旋桨调速器的控制装置。
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304.The next check interval is based on the inspection results of this time.
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923.执行此程序来保护碳钢钢索。
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1510.The limit is applicable if the aircraft is on the landing gear or on jacks.
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1263.Torquemeter is an indicating system that displays the output torque available on the propeller shaft.
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1105.Airplane performance data shall be presented in either graphical or tabular formats.

A、 Airplane primary data should be displayed neither in graphs and tables.

B、 Airplane behavior data shall be predicted in both graphical and tabular formats.

C、 Aircraft performance parameters can be represented graphically or in tables.

答案:C

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相关题目
1255.Identify the disassembled parts with tags,this method will help you during the subsequent assembly procedures.

A. 用标签识别拆下的零件,此方法将有助于随后的装配过程。

B. 保存好拆下标签的零件,此方法将有助于随后的装配过程。

C. 用标签识别拆下的零件,此方法将有助于子部件的安装。

https://www.shititong.cn/cha-kan/shiti/00059993-c618-f433-c057-47291d003a00.html
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74.Turn the clamps to free the pipes.

A. 转动凸轮以松开管路。

B. 转动卡箍以使管路自由移动。

C. 转动卡箍以松开管路。

https://www.shititong.cn/cha-kan/shiti/00059993-c60e-bfba-c057-47291d003a00.html
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2402.Adjust the clinometer until the bubble is in the center.

A. 调整倾斜仪,直到气泡位于中心。

B. 在倾斜仪上的气泡位于中心后进行调整。

C. 将倾斜仪调整到气泡的中心位置。

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2398.If you cannot hear the alarm,adjust the volume control.

A. 如果无法听到警告声,需调整音量控制器。

B. 调整音量控制器可能导致警告声过于响亮。

C. 调整音量控制器可能使警告声变得更加嘈杂。

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2935.此文件包含了附录 G 中描述的持续性适航的适当说明。

A. This document lists appropriate description of Continuous Airworthiness as indicated in Appendix G.

B. This document marks the Appendix G as an appropriate descriptions of Continuous Airworthiness.

C. This document contains appropriate instructions for Continued Airworthiness as described in Appendix G.

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1856.发动机功率控制系统可以控制主燃油控制器或调节器,包括涡轮螺旋桨发动机上螺旋桨调速器的控制装置。

A. The engine power control system manages and controls the main fuel control or synchronizer,which is inclusive of controls to the propeller modulator on a turboprop engine.

B. The engine power control system furnishes a means of controlling the main fuel control or coordinator,which includes controls to the propeller regulator on turbo-prop engines.

C. The engine power control system regulates and controls the main oil,coordinator and propeller regulator of a turboprop engine.

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304.The next check interval is based on the inspection results of this time.

A. 下一个检查内容是基于本次检查结果。

B. 下一次检查间隔是基于本次检查结果。

C. 下一次检查重点是基于本次检查结果。

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923.执行此程序来保护碳钢钢索。

A. Do the procedure to preserve the carbon steel cables.

B. Do the procedure to lubricate the stainless steel cables.

C. Do the procedure for the protection of the carbon steel harnesses.

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1510.The limit is applicable if the aircraft is on the landing gear or on jacks.

A. 该限制应在飞机处于起落架上或提升装置上时使用。

B. 如果飞机在起落架上或被顶起,请查阅此文件。

C. 该限制适用于飞机在起落架上或千斤顶上。

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1263.Torquemeter is an indicating system that displays the output torque available on the propeller shaft.

A. 扭矩测量仪是一个显示螺旋桨传动轴可用输出扭矩的指示系统。

B. 扭矩计可以显示传动轴的输出扭矩。

C. 指示系统必须显示扭矩计传动轴的可用输出扭矩。

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