In the description of the airplane＇s Brake System, how to recognize impending problems and what to do if malfunctions occur shall be explained.

A. Remove the test cap between the Precooler Control Valve and the 3908 sensor on the control pressure sense line and ensure that there is air flowing out of the port.

B. From precooler control valve to 3908 sensor, remove the sense line test cap, make certain that the air flows from the test hub.

C. The purpose of the test cap removal from the Precooler Control Valve to the 3908 sensor is to guarantee that there is airflow at the test port.

A. All aircraft engines must meet certain general efficiency, economy, and reliability requirements, which require that the ignition system can provide ignition pulses at the proper time to the spark plug in various weather and other adverse conditions.

B. All aircraft engines must meet certain overall efficiency, economy and reliability requirements, which require the ignition system should provide ignition pulses at appropriate times under meteorological and other unfavorable conditions.

C. All aircraft engines must meet certain general requirements of reliability, economic and efficiency, which dictates the use of ignition systems that deliver the firing impulse to the spark plugs in all kinds of weather and under other adverse conditions.

A. 如果刹车片接触到盘，根据文件移开不需要的材料。

B. 如果托架触碰到板，用锉刀去除不需要的材料。

C. 如果撑杆触及盖板，用填充剂移开不合适的材料。

A. 一些类型的飞机（如涡轮螺旋桨飞机）在确定VMCA时，可能受自动螺旋桨桨矩控制装置的影响，因飞机在降低发动机功率模拟一发失效时遇到的阻力要比实际一发失效时遇到的阻力更大。

B. 某些类型的飞机（例如涡轮螺旋桨驱动的）可以用自动螺旋桨桨距控制装置来确定VMCA，该装置可能比不工作的发动机具有更大的阻力，以模拟发动机故障。

C. 一些类型的飞机（如涡轮螺旋桨飞机）可能有自动螺旋桨间距控制装置确定的VMCA，与不工作的发动机相比，在模拟发动机故障降低功率运行时发动机可能有更大的阻力。

A. Overhaul of any components covered in this chapter shall be completed in accordance with data other than those provided by the manufacturer.

B. None of the components covered by this chapter shall be overhauled except in accordance with the manufacturer＇s data.

C. All components covered in this chapter must be overhauled according to the technical data provided by the manufacturer.

A. Independent, self-contained, gas reservoir assembly offers 7-9 seconds of pressure for operating after actuation.

B. Divided, self-contained, gas reservoir assembly stores the operating energy within 7-9 seconds prior actuation.

C. Single, self-contained, gas reservoir assembly provides the operating pressure within 7-9 seconds after actuation.

A. 在接近跑道过程中，偏差指针在航向指示器上显示飞行员正在朝哪个方向飞行。

B. 在接近跑道过程中，飞行员必须朝着航向指示器偏航指针的方向飞行。

C. 在接近跑道过程中，航向指示器的偏差指针向飞行员显示飞机必须向哪个方向飞行。

A. "EMERGENCY EXIT" placard at exit hatch over Left wing is illegal.

B. "EMERGENCY EXIT" placard at exit hatch over Left wing is not legible.

C. "EMERGENCY EXIT" placard at exit hatch over Left wing is missing.

A. 从新垫圈上标有"ANTENNA SIDE"的一侧，撕掉保护膜。

B. 从标有 ANTENNA SIDE记号的新垫圈上撕掉保护膜。

C. 从新垫圈一侧撕掉保护膜，然后标记“ANTENNA SIDE“。

A. Bleed the hydraulic system.

B. Pressurize the hydraulic system.

C. Depressurize the hydraulic system.