162. 当进行每一步的活门测试时,确保没有渗漏,没有腐蚀,没有生锈并且在整个程序结束后再次确认。

3201. The flight controls furnish a means of manually controlling the flight attitude characteristics of the aircraft, including items such as hydraulic boost system, rudder pedals, control column linkages, control cables, tab controls, mounting brackets, etc

3200. 包括发动机、进气道、安装点、整流罩、气道、整流片、冷却挡板等在内的整个动力装置。

3199. Pressure surges and vibration can cause wear on the hoses

3198. 外径必须与内径同轴。

3197. Space permitting, legends shall be spelled out within the diagram rather than abbreviated by numerals to a list of legends at the bottom or on an adjacent page

3196. When you use the emergency pump, record the time of operation

3195. 支撑发动机并将其连接发动机吊舱或吊架的组合结构或锻件的框架。包括发动机支架,减震器,支撑连杆,安装螺栓等。

3194. Use the manual procedure if it is not possible to use the automatic control

3193. This Cap has been prepared with the intent to expand present inspection requirements as a further assurance of the ability of the airplane to perform within the limits of the original certification

3192. EGT shows only when EEC gets powered