A、 如果格式参数或规则不适合于飞机的类型,则可以使用可能达到相同目的的对等物。
B、 如果表格参数或条款与机型不符,必须使用批准的等效部件。
C、 如果使用可以达到相同目的的对等物,格式参数或规则能够用于不适合的飞机类型。
答案：A
A、 如果格式参数或规则不适合于飞机的类型,则可以使用可能达到相同目的的对等物。
B、 如果表格参数或条款与机型不符,必须使用批准的等效部件。
C、 如果使用可以达到相同目的的对等物,格式参数或规则能够用于不适合的飞机类型。
答案：A
A. Replace the unit at the next check.
B. Repeat the unit at the next check.
C. Perform the unit at the next check.
A. COMMENCE
B. START
C. ACTIVATE
A. This is the low limit of flight speed at which the airplane can be controlled directionally and laterally.
B. This is the upper limit of flight speed at which the aircraft is directionally and later ally controllable.
C. This is the largest flight speed at which the airplane is directionally and laterally steerable.
A. Dry all metal parts that have different metal inserts or deep blind holes in an oven at 225 to 275℉ (107 to 135℃) for a minimum of one hour.
B. Put all different metal inserts or deep blind holes metal parts in an oven at 225 to 275℉ (107 to 135℃) for a maximum of one hour.
C. All metal parts that have different metal inserts or deep blind holes are dry in an oven of 225 to 275℉ (107 to 135℃) for a minimum of one hour.
A. Hydraulic pressure byasses the valve and drives the hydraulic motor;
B. Hydraulic pressure overrides the valve and drives the hydraulic motor;
C. Hydraulic pressure passes the valve and drives the hydro-motor;
A. 绕其轴线旋转此曲柄
B. 绕其圆心旋转此杆
C. 绕其轴线旋转此轴
A. It is made up of a turbine, a compressor and a fan. The compressor and the fan are connected by a common shaft.
B. It consists of a turbine. The compressor and the fan are connected by a common shaft.
C. It consists of a turbine, a compressor and a fan. The turbine, the compressor and the fan are connected by a common shaft.
A. 对只包含一个小节的持续适航方案页面按节标识顺序进行编号
B. 对只包含一个章的持续适航方案页面按章标识顺序进行编号
C. 对只包含一个章节的持续适航方案页面按章节标识顺序进行编号
A. 本文件中的任何零件没有出版商的许可不得复制
B. 本文件中有任何一个部分是没有得到出版商许可的
C. 未经过出版商书面许可,本文件任何部分不得以任何形式复制
A. 系统中用于记录机组成员通讯的部分。
B. 系统中用于记录机组成员通话的部分。
C. 系统中用于记录机组成员协调的部分。
