2130.Reserve shall be computed as 45 minutes at the cruise power to be used for the flight.

A. 应提供重量平衡装载表,同时提供相关计算程序的解释说明

B. 应提供重量和平衡载荷表以及说明计算程序。

C. 应提供重量和平衡载荷表以及计算步骤说明。

A. Warnings,cautions and notes may be used to highlight or emphasize important points.

B. Highlight or underline the key points with alerts,attentions and comments.

C. Alerts,cautions and comments can be used to protrude or underline the key points.

A. 应提供空速限制和限制的执行程序。

B. 应描述空速限制及其操作意义。

C. 应描述各项空速限制和相应空速限制在运行中的重要性。

A. Ensure that you do activate the control adjacent to it.

B. Adjust the adjacent control for optimal results.

C. Make sure that you do not operate the adjacent control.

A. Use multipurpose plate driver to load flight management data.

B. To upload flight management data,you can utilize multi-function disc generator.

C. Download the flight management data with the multipurpose disk drive unit.

A. These buses consume power directly from the battery.

B. These buses accept the direct current of battery.

C. The battery supplies power directly to these buses.

A. 如果滑油渗漏超过 5 滴,每分钟检测密封胶。

B. 如果滑油渗漏超过每分钟 5 滴,检查密封胶。

C. 如果燃油渗漏超过每分钟 5 滴,更换密封胶。

A. The data may be supplemented by brief descriptions of additional characteristics or features if desired.

B. If necessary,the detail may supplement some simple descriptions of additional characteristics or properties.

C. If desired,the data may be added by simple presentations of additional values or properties.

A. When the movement of input rod is ranged from 5 to 10 mm,measure the piston retraction.

B. When the input lever is between 5 and 10 mm,measure the piston extension.

C. When the interval of input shaft changes between 5 and 10 mm,measure the expansion of the piston.

A. When there are too many positive or subtractive pressure in the fuel tanks,the pressure relief valve eliminates damage to the wing structure.

B. When there is too much plus or minus pressure in the fuel tanks,the pressure relief valve previews damage to the wing structure.

C. The pressure relief valve prevents damage to the wing structure when there is too much positive or negative pressure in the fuel tanks.