547. 分解转子顺序如下

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

2814. Do not point the compressed air outlet at your skin

2813. 条件控制杆是飞机启停的主要控制。

2812. Record of Revisions is optional if information is provided elsewhere

2811. Install the safety devices

2810. 温度下降率从海平面到海拔高度-56℃是每英尺-000198℃,并在该高度以上降至零。

2809. 此构型具有所有惯性与空气数据功能的三重冗余数据。

2808. These items will be evaluated by ABC and, if applicable to the airplane configurations concerned, will be added to the document for the benefit of all

2807. 机载辅助动力装置是那些装于飞机上的机载动力装置(发动机),用于产生和供应单一类型或辅助电力、液压、气动或其他动力的组合