A、 Ensure that you do activate the control adjacent to it.
B、 Adjust the adjacent control for optimal results.
C、 Make sure that you do not operate the adjacent control.
答案：C
A、 Ensure that you do activate the control adjacent to it.
B、 Adjust the adjacent control for optimal results.
C、 Make sure that you do not operate the adjacent control.
答案：C
A. Procedures shall be provided for all airplanes for all cases of engine failure, including partial failure, during takeoff and in flight.
B. Procedures shall be provided for all airplanes for all cases of engine failure, including intermittent failure, during roll out and in flight.
C. Procedures shall be provided for all airplanes for all cases of engine flame out, including parts failure, during takeoff and in flight.
A. That portion of the system is used to perform the cranking portion of the starting operation.
B. That portion of the system is used to perform the igniting portion of the starting operation.
C. That portion of the system is used to perform the cranking portion of the igniting operation.
A. This section includes all the limits of the optional systems and equipment.
B. Limitations related to optional systems may be contained in this section.
C. Only the limitations which are relevant to optional systems might be including in this section.
A. Extend the nose landing gear.
B. Extend the main landing gear.
C. Retract the main landing gear.
A. 径向施加载荷。
B. 轴向施加载荷。
C. 周向释放载荷。
A. 原理图应倾向于处理整个系统，而不是附属系统。例如，空调系统，而不是空调系统内的压缩机。
B. 原理图应倾向于处理整个系统，而不是附件系统。例如，空调系统，而不是空调系统内的压缩机。
C. 原理图应尽量呈现整个总系统，而非各个子系统。例如，空调系统原理图不应把重点放在其中包含的压气机上。
A. 处理边缘锋利的零件时要戴手套。
B. 处理边缘有凹痕的零件时要戴手套。
C. 当接触边缘有锯齿的零件时要戴手套。
A. 当飞机在地面上时支撑飞机机头的那部分系统，包括减震支柱、阻力支柱、门、连接装置、固定螺栓等。
B. 当飞机在地面上时支撑飞机机头的那部分系统。包括刹车、浮子、门、轮胎、固定螺栓等。
C. 当飞机在地面上时支撑飞机机头的那部分系统。包括驱动机构、转向架饰件、门、跳板、上下门闩等。
A. After 10 flight cycles or 25 flight hours, which comes first, the rod end bearing shall be discarded if its wear is greater than 0.010 inch of diameter.
B. If the rod end bearing wear is greater than 0.010 inch in radial play, reject it within next 10 flight cycles or 25 flight hours whichever comes first.
C. Destroy the rod end bearing during 10 flight cycles or 25 flight hours when its wear is more than 0.010 inch of its radius, whichever comes first.
A. 确认减速板能够立即收回。
B. 确保速度刹车立即缩回。
C. 确保减速制动器立即断开。
