各大翼油箱给中央油箱的燃油供油流量一致。

A. Data shall be managed as time, fuel and distance to climb from sea level versus outside air temperature, altitude and weight.

B. Data shall be presented as time, fuel and distance to climb from sea level versus outside air temperature, altitude and weight.

C. Data shall be presented as time, fuel and distance to lift from sea level to outside air temperature, altitude and weight.

A. When preparing dangerous goods, follow the operational instructions.

B. Before you use dangerous materials, obey these precautions.

C. Prior to applying any hazardous material, understand the principles of it.

A. 该控制组件安装在机身尾部。

B. 该控制组件安装在驾驶舱后部。

C. 该控制组件位置在驾驶舱底部。

A. 把上凸轮放到与拆下时所做标记一致的位置。

B. 上部卡箍安装的位置应该与拆卸标记保持一致。

C. 经同意后，对应拆卸时所作的标记将上部曲柄安装在位。

A. The damper prevents abnormal movement of the control.

B. The control is protected from unusual movements by the damper.

C. The damper prevents sudden movement of the control.

A. Put the repair patch accurately on the damaged area.

B. Put the repair patch on the correct damaged area.

C. Correctly put the repair sealant on the damaged parts.

A. 任何以ATA No.100格式发布的技术数据将满足本规范的要求，尽管预期在没有ATA-100要求的情况下将使用第19段格式。

B. 任何以ATA No. 100格式发布的技术数据将满足本规范的要求，但在没有预见ATA-100要求的情况下，将使用第19段格式。

C. 任何以ATA No. 100格式发布的技术数据将满足本规范的要求，但在预见不需要满足ATA-100要求的情况下，将使用第19段格式。

A. 现代飞机都安装单元体结构的发动机。

B. 一个铸造结构的发动机安装在现代飞机上。

C. 一个整体发动机安装在所有现代飞机上。

A. 此外， 申请必须包括一个检查方法，该方法包括必要的检查频次和检查范围并提供给飞机持续适航部门。

B. 此外， 申请方必须有一个检查方案，该方案包括为保证飞机持续适航所需要的检查频次和检查程度。

C. 此外， 申请方必须有一个检查目标，包括检查频次和检查内容，必须保障飞机的持续适航。

A. With the aid of the component manufacturer, all components in this chapter can be overhauled in any workshops with different qualifications.

B. Without the data supplied by the component manufacturer, it is possible for the most qualified shop to overhaul any components included in this chapter.

C. You must overhaul any or all components in this chapter in an eligible shop on the basis of data provided by the component manufacturer.