539. 如果制造商选择以多册发布维护资料,则每个单独册的标题可视情为“线路图手册”,“部件维护手册”等。

2824. Inlet guide vanes are stationary vanes located in front of the first stage of the compressor in an aircraft gas turbine engine, with the purpose of directing the air into the first stage of the compressor at the proper angle for the most efficient compression

2823. 如果故障次数超过三次,请更换该组件。

2822. 适用时,本章可代替飞机的-00至-70部分,以飞机附带的供应商资料为准。本章中可能包含制造商认为适用的大修资料。

2821. An example is the pneumatic system, supplying air to both the air conditioning system and the engine starters

2820. 该部分系统用于控制空气中的水分,控制臭氧浓度,从经过调节的空气中过滤掉碎片,并在必要时用除臭剂,杀虫剂等处理空气,如适用。

2819. Braking system is used to decrease run-down time or stop propeller rotation during engine power-off conditions

2818. This document provides supplemental information to the applicable manual

2817. The checklist should be limited to the minimum number of items determined to be essential to aid the pilot in an emergency

2816. Examine the flow control orifice and make sure the restrictor holes are free from blockage and contamination

2815. Do an overhaul of the No2 engine