608.MAKE SURE THAT THE TRANSPONDER ( ) THE SIGNAL CORRECTLY.

A. 　飞机维修手册(或持续适航指令)是包含飞机持续适航方案的主要文件,CAP
对其进行补充。

B. 　飞机维修手册(或持续适航指令)是包含飞机持续适航方案的补充文件,CAP
是主要文件。

C. 　飞机维修手册(或持续适航指令)是包含飞机持续适航方案的唯一文件,CAP
对其进行扩展。

A. 　 确保箭头指向燃油流量流动的方向。

B. 　 确保标记指向燃油流量流动的方向。

C. 　 确保标记指向燃油流量相反的方向。

A. 　文本应尽可能简单易懂。

B. 　文本可以尽量简单易懂。

C. 　文本应该尽可能简明扼要。

A. 　This chapter of the Pilot's Operating Handbook shall contain only those
limitations required by regulation or necessary for safety operation of
the airplane and approved by the regulatory authority.

B. 　This Section of the Pilot's Operating Handbook shall abstain only those
limitations required by regulation or necessary for safe operation of the
airplane and approved by the regulatory authority.

C. 　This Section of the Pilot's Operating Handbook shall contain only those
limitations required by regulation or necessary for safe operation of the
airplane and approved by the regulatory authority.

A. 　BYPASS

B. 　BYPASSED

C. 　BYPASSES

A. 　基本控制和操作信息,描述如何控制及操作飞机部件,涉及到一些特殊程序和
飞行控制信息适用的限制。

B. 　基本控制和操作信息,描述如何控制及操作飞机部件,涉及到许多特殊程序和
飞机部件适用的限制。

C. 　基本控制和操作信息,描述如何控制及操作飞机部件,涉及到所有特殊程序和
飞机部件适用的限制。

A. 　Apply a load to the panel until it moves into position with a click.

B. 　Bear down on the panel until it moves into place with a click.

C. 　Use a load to the panel until it moves into position with a click.

A. 　The CAP will come up with main and subordinate airframe components,
and main and subordinate systems to achieve the stated objective of
continued airworthiness.

B. 　Primary and secondary airframe components, and Primary and secondary
systems are contained in CAP to complete the stated objective of continued
airworthiness.

C. 　To continue the stated objective of sustain airworthiness, major and
minor airframe components, and major and minor system are covered in CAP.

A. 　在这种结构中,液压流过这个活门。

B. 　在这种构型中,液压旁通这个活门。

C. 　在这种构型中,水流旁通这个活门。

A. 　Maneuvering Speed is the maximum speed what required of full uncommitted
aerodynamic control will not exceed the airplane.

B. 　Maneuvering Speed is the largest speed that the aerodynamic application
by the full available control will not cause the aircraft overexert.

C. 　Maneuvering Speed is the maximum speed at which application of full
available aerodynamic control will not overstress the airplane.