1883. Connect the fittings to the hydraulic test bench

A. LOOK

B. SEE

C. WATCH

A. 系统中使用无线电/雷达波束、定向和垂直航向仪、皮托管静态和手动感应输入的部分,用于自动控制飞机的偏航、俯仰和滚转。这包括电源装置、联锁装置和放大、计算、集成、控制、驱动、指示和警告装置,如计算机、伺服系统、控制面板、指示器、告诫灯等。

B. 系统中使用收音机/雷达波束、转向和垂直陀螺仪、静压孔和手动感应输入的部分,用于自动控制飞机的偏航、俯仰和滚转。这包括电源装置、自锁装置和放大、计算、集成、控制、驱动、指示和警告装置,如计算机、伺服系统、控制面板、指示器、警告灯等。

C. 系统中使用无线电/雷达波束、定向和垂直陀螺仪、皮托管静态和手动感应输入的部分,用于自动控制飞机的偏航、俯仰和滚转。这包括电源装置、联锁装置和放大、计算、集成、控制、驱动、指示和警告装置,如计算机、伺服系统、控制面板、指示器、警告灯等。

A. 确认减速板是否立即收回。

B. 确认减速板是否立即放出。

C. 确认减速板是否缓慢收回。

A. When there are too many positive or subtractive pressure in the fuel tanks the pressure relief valve eliminates damage to the wing structure.

B. When there is too much plus or minus pressure in the fuel tanks, the pressure relief valve previews damage to the wing structure.

C. The pressure relief valve prevents damage to the wing structure when there is too much positive or negative pressure in the fuel tanks.

A. It is expected that the manufacturers of major components will provide maintenance, troubleshooting, inspection and repair data in the format of this specification.

B. It is expected that the manufacturers of major equipments will provide maintenance, troubleshooting, inspection and removal data in the format on this specification.

C. It is expected that the manufacturers of most components will provide maintenance, troubleshooting, inspection and installation data in the format of this specification.

A. GO INTO

B. SPILLS

C. FLOW

A. When fuel or lubricating oil overflows, clean the area at once. There exists a danger due to the wet surface that can cause falling.

B. Clean the area where fuel or lubricating oil are knocked over without delay because the wet surface that may lead to the fall is dangerous.

C. The area contaminated by fuel or lubricating oil shall be cleared up firstly because the dirty surface brings a risk of fall.

A. The shock strut is an elastic oil-air unit.

B. The shock absorber is a flexible hydraulic-pneumatic unit.

C. The shock absorber is a telescopic oleo pneumatic unit.

A. Loosen the screws that attach the clamp to the support;

B. Loosen the nuts that attach the clamp to the support;

C. Loosen the bolts that attach the clamp to the support;

A. Check the servo controls every 400 flight cycles.

B. Examine the servo controls at intervals of 400 flight hours.

C. Inspect the feedback controls every 400 flight hours.