A、 Supply electrical power to both solenoids.
B、 Apply hydraulic power to either of the solenoids.
C、 Apply electrical power to one of the two solenoids.
答案：C
A、 Supply electrical power to both solenoids.
B、 Apply hydraulic power to either of the solenoids.
C、 Apply electrical power to one of the two solenoids.
答案：C
A. 把 O 形封圈浸泡在液压油里面。
B. 防止液压油腐蚀 O 形封圈。
C. 用液压油润滑 O 形封圈。
A. If no tabs are used,an identification method should be supplied to facilitate the location of each system or section.
B. If tab dividers are not used,a method of identification shall be provided to permit easy location of each System or Chapter.
C. An identification way should be offered to locate the system and chapter easily if the dividers are improper.
A. 慢慢地拧动活门。
B. 慢慢地转动叶片。
C. 慢慢地松开电门。
A. 将孔铰成比标准尺寸大 0.20 英寸。
B. 将孔铰成比标准尺寸大 0.20 英尺。
C. 将孔定位成比标准尺寸大 0.20 英寸。
A. 在制作壳体之前,确保钻头的尖端锋利。
B. 在钻孔之前,确保钻头的尖端锋利。
C. 在钻孔之前,确保电锯的尖端锋利。
A. ASD 感谢所有对本规范做出整理的组织、公司和个人。
B. ASD 感谢所有对本规范做出贡献的组织、公司和个人。
C. ASD 感谢所有对本特例做出解释的组织、公司和个人。
A. 对于非 FAA 批准的飞机,其声明要写在飞行手册中。
B. 对非 FAA 批准的飞机飞行手册,做如下声明。
C. 在非 FAA 批准的飞行手册中要包括以下声明。
A. Ground Idle Power refers to the power required to run an engine on the ground,as slowly as possible,yet sufficient to ensure satisfactory engine,engine accessory,and airplane operation with a minimum of thrust.
B. Ground Idle Power refers to the power required to run an engine as slowly as appropriate on the ground while still ensuring satisfactory airplane operation with a maximum of thrust of engine and engine accessory.
C. For Ground Idle Power,it determines the minimum power necessary to initiate and maintain safe airplane operation,engine accessory function,and satisfactory engine performance whilelimiting the degree of thrust utilized.
D. C.For Ground Idle Power,it determines the minimum power necessary to initiate and maintain safe airplane operation,engine accessory function,and satisfactory engine performance whilelimiting the degree of thrust utilized.
A. The portion of the systemis used to eliminate or prevent the formation of ice on all airfoil surfaces,including wings and airfoil sections of the empennage.
B. The portion of the systemis used to dispel or get rid of ice gathering on some aircraft surfaces,including wings and empennage surfaces.
C. The portion of the system is used to eliminate or forbid ice forming on outside parts of all airfoils,including the airfoils of wings and empennage.
A. Tool is adjacently available for the installation procedure.
B. Tool is subsequently available for the installation procedure.
C. Tool is subsequently available for the installation task.
