1459.This torque shaft cannot move inboard.Thus,before you remove it,remove the outboard torque shaft.

A. 飞机维修手册或章节包括说明性资料,如对飞机的维修或预防性维修的特点和资料所做的说明。

B. 飞机维修手册或章节包括说明性资料,如对飞机的结构和数据给出维修或预防性维修程度的说明。

C. 飞机维修手册或章节包括说明性资料,如对维修或预防性维修所需要的飞机特性和数据的说明。

D. B.飞机维修手册或章节包括说明性资料,如对飞机的结构和数据给出维修或预防性维修程度的说明。

E. C.飞机维修手册或章节包括说明性资料,如对维修或预防性维修所需要的飞机特性和数据的说明。

A. 需要提供紧急程序。

B. 应提供紧急下降程序。

C. 紧急下降时提供应急程序。

A. This tool is mandatory.

B. This tool is optional.

C. This tool is necessary.

A. 在飞机座舱增压系统部分,应描述如何识别潜在问题和处理紧急情况。

B. 在飞机座舱增压系统部分,应说明识别可能问题和处理障碍的方法。

C. 在飞机座舱增压系统部分,说明识别问题和处理紧急情况的方法。

A. 确保这片区域的设备都清空了。

B. 确保这个区域的设备都已打扫干净。

C. 确保那台设备在这个区域里是收好的。

A. 这一系统部分包括控制手柄、钢索、作动筒、告警系统、连接装置、操纵面、位置指示器等部件。

B. 这一系统部分包括控制手柄、电线、作动筒、告警系统、连接装置、操纵面、位置指示器等部件。

C. 这一系统部分包括控制杆、电缆、作动筒、告警系统、连动装置、操纵面、位置指示灯等部件。

A. The air conditioning cooling system supplies cooled air to the cabin.Includes items such as the cooling unit,indicating systems related to the cooler operation,etc.

B. The air conditioning cooling system supplies cold air to the passenger cabin.Includes items such as the cooling unit,indicating systems related to the cooler operation,etc.

C. The air conditioning cooling system supplies cooled air to the passenger cabin.Includes items such as the cooling pack,indicating systems related to the cooler operation,etc.

A. Modifications,additions and omissions,a black line should be drawn vertically at the footer outside of the page parallel to the part of the change.

B. Revisions,additions and deletions shall be identified by a vertical black line along the outside of the page opposite only that portion of the printed matter that was changed.

C. Alterations,substitutions and eliminates should be marked with a black slash outside the scope of the page to coincide with the section being changed.

A. 当飞机处于常态速度和巡航仰角时,通气油箱内的燃油将排放到主燃油箱内。

B. 当飞机处于恒定速度和巡航俯仰角时,通气油箱内的燃油将排放到主燃油箱内。

C. 当飞机处于超常速度和巡航俯仰时,通气油箱内的燃油将排空到主燃油箱内。

A. A three-axis accelerometer gives acceleration data of the horizontal,lateral,and longitudinal axis.The flight data recorder system sensors send data about the position of the flight surfaces and controls the FDAU.

B. A three-axis accelerometer gives accelerating data with the vertical,parallel,and longitudinal axis.The flight data recorder system sensors send data and the position of the flight surfaces and controls to the FDAU.

C. A three-axis accelerometer gives acceleration data along the vertical,lateral,and longitudinal axis.The flight data recorder system sensors send data about the position of the flight surfaces and controls to the FDAU.