In the description of the airplane＇s Flight Controls, if controls are boosted, the revelant systems shall be explained.

A. 调整测试描述应该提供指导来完成测试或检查，来保证整个操作组件的系统、子系统或组件装配。

B. 为确保整合系统、子系统和单元组装件的运行，调整测试的说明应该提供指示来完成测试或检查。

C. 调整测试说明应提供完成测试或检查的指示，以确保作为系统、子系统或单元组装件的操作性组件的完整性。

A. Recommending or requiring life limited components is on the right side of the page in an appropriate margin.

B. Recommended or required retirement time of life limited parts is on the right side of the page in an appropriate space.

C. The required retirement time of life limited components is located on the right side of an appropriate space.

A. The items in the Emergency Procedures check list are determined to be essential in aid of the pilot in an emergency and should be limited to the minimum number.

B. A limited number of items in the Emergency Procedures check list are determined to be essential to aid the pilot in an emergency.

C. To aid the pilot in an emergency, it is determined that the Emergency Procedures check list should contain only essential items.

A. The same word “base” can go into different technical name categories when it is used with different meanings in different contexts.

B. The same word "base", when it has different meanings in different environment, it can be divided into different technical name categories.

C. When the word "base" can be divided into different technical noun categories, it has different meanings in different language environment.

A. Remove the test cap between the Precooler Control Valve and the 3908 sensor on the control pressure sense line and ensure that there is air flowing out of the port.

B. From precooler control valve to 3908 sensor, remove the sense line test cap, make certain that the air flows from the test hub.

C. The purpose of the test cap removal from the Precooler Control Valve to the 3908 sensor is to guarantee that there is airflow at the test port.

A. For clean configuration of landing, the limit load factor in g unit should be provided. For spinning and aerobatic aircraft, the load factor of flaps down should be provided as well.

B. The limit maneuvering load factors, in g units of acceleration, for clean cruise and landing configurations, shall be given. The negative g limit, flaps up, should be given for aircraft approved for spinning or aerobatics.

C. The flight maneuver load factor limit in the unit of g should be given for the smooth configuration of aircraft cruising and landing. For aircraft approved for spin or aerobatics, load limits should also be provided when flaps are opened.

A. 来自压气机的高压气体进入燃烧室并缓慢移动，并与被点燃的燃料混合。

B. 来自压气机的高压气体进入燃烧室并缓慢移动，并与易燃的燃料混合并点燃。

C. 来自压气机的缓慢移动的高压气体进入燃烧室，与易燃燃料混合并点燃。

A. It supersedes the preceding edition.

B. It updates the previous version.

C. It takes place of the following version.

A. 在运转的发动机附近时，必须佩戴听力保护装置。

B. 当你在附近要运转发动机时，你必须要带耳罩。

C. 当你靠近正在运转的发动机时，你必须保护耳朵。

A. 计算机计算偏离这些数值的能量消耗

B. 计算机根据这些值计算能源消耗

C. 计算机计算根据燃油价值来计算能量消耗目标。