1574. 对于机翼/机身过热系统的指示和测试,必须要接通115V交流电源。当安装元件时,不得弯曲元件直到弯曲半径小于1英寸。如果弯曲半径小于1英寸,则会损坏元件。

1789. 如果它们掉落会出现永久性损坏。

1788. The normal pitch control law is basically the closed loop control of the load factor, and includes flight envelope protections

1787. Make sure that the movement of the elevators is slow

1786. In 1944, the British Civil Airworthiness Requirements was developed to form the code of the Airworthiness Standards through which the requirements of the Air Navigation, Orders and Regulations would be met

1785. 继续加压10分钟

1784. 文件必须易于修改。

1783. Any anomaly should be reported to ABC, through the Condition Reporting System so that additions and/or revisions can be made to the CAP where deemed necessary

1782. 在你继续测试之前,间隔5分钟是必要的

1781. 如果风速高得危险,请不要打开货舱门

1780. When you install the part, make sure that the rounded edge is against the structure