2433. 每次转动调节螺钉后,使压力稳定

930. 调节门操作杆,直到它与连接点对齐。

929. The cockpit voice recorder records signals from four audio inputs during the flight

928. Position the sprayer unit nozzles in the APU air intake as required

927. 每个探测器内的烟雾传感器监控高于预设限制的烟雾密度。如果密度保持高于限制大约8秒,则传感器设定探测器到警报状态。

926. 右后轮舱的控制机构里的右内襟翼控制钢索走向错误,且有扭结。

925. 右大翼机身整流罩前部有几颗螺钉松动。

924. Tank unit capacitance varies as a function of the fuel level in the tank

923. Make sure that there are safety barriers around the engine exhaust area

922. For general aviation aircraft this material may be covered in Sys/Chap25

921. Engine Failure Procedures shall be provided for all airplanes for all cases of engine failure, including partial failure, during takeoff and in flight