609.当使用该组件前,需先进行特定的测试程序。

163.Flight Idle Power is the power required to run an engine,in flight,
at the lowest speed that will ensure satisfactory engine operation and
airplane handing characteristics.

162.THE SHOCK MOUNT( ) THE VIBRATION.

161.IF THE LOW PRESSURE CONDITION ( ) , REPLACE THE UNIT.

160.所有的修改都要得到设计部门的批准。

159.The same symbol, device, or code shall be used throughout the Handbook
to depict the same system, valve or control.

158.最大允许误差 5 毫米。

157.确保发动机进气道无外来物。

156.泵安装在液压马达后面。

155.CAREFULLY LIFT THE MAGNETIC LEVEL INDICATOR UNTIL YOU ( ) THE MAGNETS.

154.Optional information including ( ) the rationale
utilized to select CAPs - how the CAP requirements were determined.