925. 右大翼机身整流罩前部有几颗螺钉松动。

2438. 当靶标移动到或离开临近传感器激活区域则将改变临近传感器电子性能。

2437. Divide the crosswind component by the aircraft speed to get the correction

2436. 向相反的方向移动连杆。

2435. Before you install the duct and check valve assembly, you must do an inspection of the check valve to make sure the spring holds the check valve open a short distance

2434. 使用第10章给出的扭矩值。

2433. 每次转动调节螺钉后,使压力稳定

2432. The airplane were delivered with recommended inspection programs to keep them airworthiness

2431. ADD FLUID TO the HYDRAULIC RESERVOIR AS NECESSARY

2430. There is one rigid bus assembly located at the rear of each of the power distribution panels

2429. Speed-Attitude Correction system autocratically maintains a safe flight attitude by correcting for effects of speed