531. Calibrated Airspeed means the indicated speed of an aircraft, corrected for position and instrument error

2832. Auxiliary Structure Includes leading edge, trailing edge, wing tip, tip fuel tank and fuel or water cell backing boards Does not include plates/skin

2831. If the air intake flap has failed, deactivate air inlet valve

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。