A、 within night operation, make sure the panel lights are dim.
B、 During night operation, make sure the panel lights are bright.
C、 During night operation, make sure the panel lights are dim.
答案:C
A、 within night operation, make sure the panel lights are dim.
B、 During night operation, make sure the panel lights are bright.
C、 During night operation, make sure the panel lights are dim.
答案:C
A. WILL
B. HAVE TO
C. MUST
A. 简介中应包含主题的字母索引,用于定位重要的电路。
B. 字母表应按照主题分类后在简介中列出,用于定位理想电路。
C. 简介中应包含主题分类的字母索引,以帮助查找所需的电路。
A. 型号合格证
B. 类型合格证
C. 型号许可证
A. 其他信息可能会显示在封面上。
B. 其他信息可能会在盖板上留下。
C. 其他信息可能会显示在目录上。
A. to arrive at the incorrect value, set the switch to position 2.
B. to get the correct value, set the switch to position 2.
C. to get the incorrect value, set the switch to position 2.
A. 制造商应将制造商发布的类型服务信息以及为获取此类信息而连续的办公室
或部门的描述包括在内,以便飞机可以按照发布的最新信息进行维修。
B. 制造商应将其发布的服务信息的等级包括在内,以及能提供此类信息的办公
室或部门,从而按照最终发布的信息维护飞机。
C. 制造商应将其发布的服务信息的类型包括在内,以及能提供此类信息的办公
室或部门,从而按照最终发布的信息维护飞机。
A. 本规范旨在为最初以 12500 磅或以下(或 5700 千克)最大起飞重量认证的
所有类型通用航空飞机提供手册编制指南。
B. 本规范的制定是为手册编写提供规范性制导,用于 12500 磅(或 5700 千克)
或以下最大起飞重量的所有类型飞机。
C. 本规范规定了以起始为 12500 磅或以下(或 5700 千克)最大起飞重量认证
的所有类型通用航空飞机提供手指编制指导。
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. 它们可以是活页格式,有一个耐磨的、多环的封面,临时装订,“胶片”或其
他适当的形式。
B. 它们可以是活页格式,有一个耐磨的、多环的封面,永久装订,“胶片”或其
他适当的形式。
C. 它们可以是固定页格式,有一个耐磨的、多环的封面,永久装订,“胶片”或
其他适当的形式。
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.