如果温度降到零下，排空水系统。

给定襟翼设置时，不要超过此速度。

A. Do not reach this speed with a given flap setting.

B. Do not exceed this speed with a give flap setting.

C. Do not exceed this speed with a given flap setting.

Tank and reservoir capacities in U.S., imperial and metric measure, shall be included. ANA or other standard specification number and grade (if applicable) of fuel, oil, fluid, and other material used shall be given. Specifications and grades shall be shown grouped on one page to facilitate revisions. For fuel, given expansion volume, total fuel capacity, sump capacity, net fuel capacity (as applicable). For oil, given allowance for expansion.

A. 必须列出储液箱的容量，包括美制、英制和公制单位。必须提供燃油、滑油、液压油和其他材料使用的ANA或其他标准规范号和等级（如果适用）。为了便于修改，规格和等级应显示在一页上。对于燃油，应给出膨胀体积、总燃油容量、油箱容积和净燃料容量（如适用）。对于滑油，应考虑到膨胀的余地。

B. 必须列出储液箱的容量，包括美制、英制度量和其他测量单位。必须提供燃料、油、液体和其他材料使用的ANA或其他标准规范号和等级（如果适用）。为了便于修改，规格和等级应显示在一页上。对于燃料，应给出膨胀体积、总燃料容量、沉淀容量和净燃料容量（如适用）。对于油，应给出膨胀允许量。

C. 必须列出储液箱的容量，包括美制、英制度量和其他测量单位。必须提供燃料、油、液体和其他材料使用的ANA或其他标准规范号和等级（如果适用）。为了便于修改，规格和等级应显示在一页上。对于燃料，应给出膨胀体积、总燃料容量、沉淀容量和净燃料容量（如适用）。对于油，应考虑到膨胀的余地

如果发现裂缝，请参考下表。

A. If you find cracks, refer to the table that follows.

B. If you find dents, refer to the table that follows.

C. If you find scratches, refer to the table that follows.

The drain and vent system consists of lines collecting and carrying waste fluids and vapor overboard from the engine and nacelle accessories. Drains are provided to carry fluids from any point where lines and accessories may leak and where fluids may accumulate in a cavity. Fluid from forward and aft sumps, oil-fuel heat exchanger, VBV, and VSV are discharged overboard through drains. In addition, some drain lines serve as vents to carry air and vapor from the engine and accessory cavities.

A. 放泄系统由管路组成，管路收集来自发动机和短舱的废液和水汽，并把它们排向机外。放泄管出现在可能泄漏的管路、附件的任何点上，也可能出现在油液会聚集于某一个腔的地方。来自于前后腔、滑油-燃油换热器、可调放气活门、可调静子叶片的油液也会通过这些放泄管排到外面。有些放泄管还有通风口的作用，它们会把发动机和附件内的空气和水气带到外面。

B. 放泄系统由管路组成，管路收集来自发动机和吊舱的废液和水汽，并把它们排向机外。放泄管出现在可能泄漏的管路、附件的任何点上，也可能出现在油液会聚集于某一个腔的地方。来自于前后腔、液压油-燃油换热器、可调引气活门、可调静子叶片的油液也会通过这些放泄管排到外面。有些放泄管还有通风口的作用，它们会把发动机和附件内的空气和水气带到外面。

C. 放泄系统由管路组成，管路收集来自发动机和短舱的废液和水汽，并把它们排向机外。放泄管出现在可能泄漏的管路、附件的任何点上，也可能出现在油液会聚集于某一个腔的地方。来自于前后腔、滑油-燃油换热器、可调放气活门、可调静子叶片的油液也会通过这些放泄管被放压。有些放泄管还有通风口的作用，它们会把发动机和附件内的空气和水气带到外面。

系统的该部分用于飞机在地面时支撑飞机的机头。

A. The system part is used to support the head of the aircraft when the aircraft is on the ground.

B. The part of the system is to keep the aircraft nose on the ground.

C. That portion of the system supports the nose of the aircraft while the aircraft is on the ground.

The section containing "Emergency Procedures" shall have a red plasticized tab divider.

A. 包含“备份程序”的部分应有一个红色塑化标签分隔。

B. 包含“应急程序”的部分应有一个红色塑化标签分隔。

C. 包含“应急程序”的部分应使用一个红色金属的标签分隔。

If there is no contamination in the fuel sample, continue the procedure.

A. Ignore the absence of contamination in the fuel sample and continue with the procedure.

B. Continue with the procedure if the fuel sample does not exhibit any contamination.

C. Proceed with the procedure regardless of any contamination found in the fuel sample.

The engine power system directly or indirectly indicates power or thrust, inclusive of BMEP, pressure-ratio, RPM, etc.

A. 发动机动力是系统中直接或间接表示动力或推力的部分，包括刹车平均有效压力、压力比、每分钟转数等项目。

B. 发动机动力系统能够直接或间接指示功率或推力,包括平均有效压力、压比、转速（RPM）等。

C. 发动机动力系统通过刹车平均有效压力、压力比、每分钟转数等项目，来直接或间接表示动力或推力。

The flight data recorder system gets and stores airplane parameters from airplane systems and sensors.

A. 飞行数据记录器系统从飞机系统和传感器获得存储的飞机参数。

B. 飞行数据记录系统给飞机系统和传感器提供并存储飞机指数。

C. 飞行数据记录器系统从飞机系统和传感器获得并存储飞机参数。

航空器审定服务办公室是在副局长领导下的各办公室中的一个，它的职责是监督航空器审定管理局及华盛顿总部与设计、生产和适航审定有关的各项工作。

A. Among the offices under the Associate Administrator is the Aircraft Certification Service, which has the responsibility for overseeing the Aircraft Certification Directorate, and the Washington Headquarters operations related to design, production, and ai

B. Aircraft Certification Directorate which is one of the offices under the Associate Administrator is responsible for overseeing the Aircraft Certification Service, and the Washington Headquarters operations related to design, production, and airworthiness

C. Overseeing the Aircraft Certification Directorate, and the Washington Headquarters operations related to design, production, and approval is the duty of Aircraft Certification Service that is among the offices under the Associate Administrator.