Measure the bend radius of the hose from the point where the bend starts.

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. Based on different airplane design, the Emergency Procedures and other pertinent information necessary for safe operation should only be provided for some airplane.

B. Based on the particular airplane design, operating or handling distinguishing feature, Emergency Procedures and related information must be provided.

C. The Emergency Procedures and other special information necessary for safe operation shall be provided for emergencies that is common to all airplane design, operating or handling characteristics.

A. 确保区域测试没有人。

B. 确保测试区域没有人。

C. 确定任何人可以进入考试区域。

A. Drill the hole until it has a radius of 8.00 +/- 0.003 mm.

B. Ream the hole until it has a diameter of 8.00 +/- 0.003 mm.

C. Trim the hole until it has a width of 8.00 +/- 0.003 mm.

A. Find the related EICAS status message which present with the maintenance information .

B. Find the correlated maintenance message that shows with the EICAS status message.

C. Find the applicable maintenance message displaying with the EICAS status message.

A. 给液压系统增压。

B. 给液压系统释压。

C. 给燃油系统释压。

A. 计算航程时应考虑开车、滑行、起飞和爬升所需燃油以及储备燃油。对于开车、滑行和起飞，需考虑飞机以起飞功率运行5分钟的所需燃油量。对于储备燃油，应考虑巡航功率运行 45 分钟所需燃油量。

B. 航程值应包括起动、滑行、起飞、爬升和备用的燃油。对于起动，滑行和起飞，允许在起飞功率5分钟的燃油流量。预留燃油按飞行所需的巡航功率计算为45分钟。

C. 航程值应包括启动、滑行、起飞、爬升和备用时间所需的燃油量。对于开车、滑行和起飞，需考虑飞机以起飞功率运行5分钟的所需燃油量。对于备用时间，应按飞行所用巡航功率下的45分钟计算。

A. 降低系统温度。

B. 释放系统压力。

C. 解除系统警告。

A. The recommended fuel conservation procedures shall contain a caution, if useful, that the power settings recommended by the manufacturer must be used during the use period of new and newly overhauled engines.

B. The recommended fuel conservation procedures shall contain a caution, if applicable, that the power settings recommended by the manufacturer must be used during the break-in period of new and newly overhauled engines.

C. The receptable fuel conservation procedures shall contain a caution, if applicable, that the power settings recommended by the manufacturer must be used during the management period of new and newly overhauled engines.

A. The form of the climb performance presentation is decided by the airplane manufacturer.

B. The format of the cruise performance presentation is at the discretion of the airplane manufacturer.

C. The form of the cruise performance presentation is at the discretion of the airplane manufacturer.