相关题目
2830. Soak the area with warm water
2829. Make sure that you complete the procedure before you tow the airplane back to its initial position
2828. Make an analysis of the oil
2827. Outlet pressure of control unit fails to stabilize at proper pressure
2826. Stagger the tab dividers and label them with section numbers or titles, or both
2825. 动力装置仪表标记的说明应紧接动力装置限制说明之后。
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
