200.Mix the material with a spatula.

A. Detach the sensor to establish a physical connection with the adjoining structure.

B. Install the sensor to block access to the adjacent structure.

C. Take out the sensor to reach to the neighboring structure.

A. The Check List may be designed by "Challenge" and "Response" headings or by "Item" and "Condition" headings for two pilot airplanes or for single pilot Airplanes.

B. The Check List for the pilot may be set by "Challenge" and "Response" headings for two airplanes or by "Item" and "Condition" headings for single Airplane.

C. For two pilot airplanes,"Challenge" and "Response" headings may be used on the Check List.For single pilot Airplanes,"Item" and "Condition" headings may be used.

A. 本章应提供制造商认为必要的信息,以便在飞机使用寿命期内可能需要进行的各种维修、大修或重大维修时正确校平飞机。

B. 本章提供制造商认定的必要信息用以保证飞机在全寿命期中进行各种维护,翻修或大修后正确校准飞机。

C. 本章提供制造商确定需要的信息用以保证飞机在运行期间进行各种维修,翻修或大修后适当配平飞机。

D. C.本章提供制造商确定需要的信息用以保证飞机在运行期间进行各种维修,翻修或大修后适当配平飞机。

A. Rapid operation of the accelerometer can cause unexpected movement of the vertical stabilizer.

B. Accidental movement of the compass can cause unwanted operation of the oriental stabilizer.

C. Sudden operation of the gyro can cause unwanted movement of the horizontal stabilizer.

A. 本节中所规定的各项空速应为指示空速。假设仪表误差为零,尽可能使信息直接可用。

B. 本节中使用的空速应在指示空速中规定,假设仪器误差为零,以使信息尽可能直接可用。

C. 本节中使用的空速代表指示空速。由于仪表误差为零,所以信息直接可用。

A. Emergency illumination refers to an individual and dependent subsystem which is used to provide lighting when the main electrical power fails.

B. Emergency lighting can provide illumination for an individual and independent subsystem in case of main electrical power failure.

C. Emergency lighting is the separate and independentsubsystem used to provide illumination in case of primary electrical power failure.

A. 给机械工分配不同的维修任务。

B. 给工程人员分配不同的操作任务。

C. 给技术人员分配不同的维修任务。

A. 关键字、开关及杠杆在“条件栏”大写。

B. 大写关键词的开关和杠杆位置。

C. “条件栏”中的关键字或开关及手柄位置使用大写。

A. 制动系统用于降低滑行速度,以及发动机停车状态下的停止螺旋桨旋转。

B. 制动系统是用来减少停车时间或在发动机关车的情况下使螺旋桨停止转动。

C. 在发动机低速运转或螺旋桨低速旋转时,制动系统能快速刹住。

A. The turboprop engine controls include linkages and controls to the coordinator or equivalent and from the coordinator or equivalent to the propeller governor,fuel control unit,or other units being controlled.

B. The control device of a turbojet engine includes a linkage mechanism and control device to a coordinator or equivalent device,as well as a linkage mechanism from a coordinator or equivalent device to a propeller governor,fuel control component,or other controlled components.

C. The turboprop engine controls include a coordinator or equivalent device,a linkage mechanism,a control device,a propeller governor,a fuel control component,or other controlled components.