735. 系统的自动控制油门杆位置的部分,以在着陆/进近和复飞过程中正确地将发动机功率与襟翼位置和飞机俯仰姿态融合在一起。这包括接通,感应,计算,放大,控制,作动和警告装置,例如放大器,计算机,伺服系统,限位开关,离合器,齿轮箱,警告灯等。

2628. 有必要对这些区域进行频繁检查。

2627. 如果在泵中发现金属颗粒,找到它们的来源并修复有缺陷的部分

2626. If the cable twists, disconnect the two connectors

2625. For simplicity of presentation and understandability, complex systems should be divided into system function rather than overall master schematic diagrams

2624. Artificial feel in aircraft flight control system is a type of the force feedback used in the automatic flight control systems of some aircraft, which produces an opposition to the pilot’s movement of the controls that is proportional to the aerodynamic loads acting on the control surfaces

2623. 再版是指手册的第二版或后面的版本,它取代了以前的版本。

2622. 压力超过7000千帕时停止测试。

2621. It gives the pilot pitch and roll information that is specially important when flying without outside visual references

2620. It is very important to clean the display lens using a clean , lint-free cloth and a cleaner that is specified as safe for antireflective coatings , preferable one recommended by the aircraft manufacture

2619. 一侧的适配器给另一侧的适配器提供抑制的离散信号,用于防止另一侧的无线电发射。