A、 The following components are recommended for alteration. The swap of other components can be made on condition.
B、 The following parts are recommended to be refurbished. Other parts can be plated according to on wing status.
C、 The following parts are recommended for modification. Utilization of other parts can be by in-service experience.
答案：C
A、 The following components are recommended for alteration. The swap of other components can be made on condition.
B、 The following parts are recommended to be refurbished. Other parts can be plated according to on wing status.
C、 The following parts are recommended for modification. Utilization of other parts can be by in-service experience.
答案：C
A. 解释如何避免和注意燃油消耗。
B. 解释如何避免和注意燃油污染。
C. 解释如何避免和注意燃油泄漏。
A. 本程序给出了不同的扭矩范围以及相应的规定。
B. 本文件给出了不同的扭矩值和其适用的条件。
C. 本程序给出了适用的差异扭矩值和条件。
A. 球型接头很少应用于现代飞机，因为它减少了应力。
B. 球型接头很少应用于现代飞机，因为它减少了摩擦力。
C. 因为可以减小摩擦力，滚珠轴承广泛应用于现代飞机。
A. The removal/installation portion shall state clearly the sequence of steps required to remove and reinstall a component or unit. This portion shall also state precautions to be obeyed.
B. The removal/installation portion shall state clearly the sequence of steps required to remove and reinstall a component or unit. This portion shalln’t include precautions to be obeyed.
C. The removal/installation portion shall hardly state the sequence of steps required to move and reinstall a component or unit. This portion shall also include precautions to be watched.
A. For clean configuration of landing, the limit load factor in g unit should be provided. For spinning and aerobatic aircraft, the load factor of flaps down should be provided as well.
B. The limit maneuvering load factors, in g units of acceleration, for clean cruise and landing configurations, shall be given. The negative g limit, flaps up, should be given for aircraft approved for spinning or aerobatics.
C. The flight maneuver load factor limit in the unit of g should be given for the smooth configuration of aircraft cruising and landing. For aircraft approved for spin or aerobatics, load limits should also be provided when flaps are opened.
A. CAP是飞机持续适航的初级文件，包括各相关程序。
B. CAP是包含飞机持续适航程序的主要文件。
C. CAP是飞机持续适航的初始文件，由相关程序组成。
A. Limitations related to operable systems or equipment may contain in this section or in section 9, supplements.
B. The supplements in this section or section 9 include the limitations associated with selectable systems or equipment.
C. Limitations associated with optional systems or equipment may be included in this section or in section 9, supplements.
A. 温度降低，钢索的拉力会减小。
B. 钢索上的张力会随着温度升高而增加。
C. 温度升高，钢索张力会减小。
A. Troubleshooting can only be performed after the cause of the malfunction has been found out.
B. You should perform troubleshooting according to the procedure and find out the technical failure.
C. According to the procedure, perform the troubleshooting to solve the cause of the malfunction.
A. 滤油器内如有金属颗粒，应检查滤芯是否有磨损。
B. 滤油器内如有金属残留物，立即检查滤芯是否有磨损。
C. 滤油器内如有金属颗粒，应确认滤芯的磨损情况。
