In the description of the airplane＇s Pitot Pressure Systems, anti-icing provisions, if installed, shall be explained.

The procedure that follows contains information as specified in the IATA Guidance Material on Standard Into-Plane Fueling Procedures.

A. 以下程序包含 IATA 关于标准飞机加油程序的指导材料中指定的信息。

B. 以下程序包含 IATA 关于标准飞机平面内加油程序的指导材料中指定的信息。

C. 以下程序包含 IATA 关于标准加油口加油程序的指导材料中指定的信息。

那些制造商对飞机及其系统和部件的检查、维护和大修的时间限制给出建议，也酌情给出零部件的使用寿命。

A. For inspections, repair and overhaul of the aircraft and its systems and units, those producers recommended time limits and life of parts if possible.

B. Those manufacturers recommended time limits for inspections, maintenance and overhaul of the aircraft, its systems and units, and life of parts, as applicable.

C. Those manufacturers gave time restrictions to inspect, repair and maintenance the aircraft, its systems and units, and according to the situation they gave the life of parts .

Outside Air Temperature is adjusted for instrument error and compressibility effects.

A. According to instrument error and compressibility effects, Outside Air Temperature is corrected.

B. Outside Air Temperature is set to avoid instrument error and compressibility effects.

C. Due to instrument error and compressibility effects, Outside Air Temperature is modified.

The condition of the radome is very important for its performance.

A. 雷达天线的状况对其性能有重要影响。

B. 雷达罩的状况对其性能有重要影响。

C. 雷达的性能受到其状态的重要影响。

Find the cause of the incorrect indication.

执行拧紧程序。

A. Do the tightening procedure.

B. Do the loosening procedure.

C. Do the strengthening procedure.

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MAT上显示的通过或不通过提示与维修页面上的提示不一致，请忽略MAT上的提示。

A. If the passed or failed indication that shows on the MAT does not agree with the indication on the maintenance page, ignore the indication on the MAT.

B. If the pass or fail prompt displayed on MAT is inconsistency with the prompt on the maintenance page, please ignore the prompt on MAT.

C. Neglect the instruction on MAT, whether the passing or failure sign shown on the MAT or not.

The main frame of the wing includes spars, ribs, stringers, integral fuel tank structure, tip tank supporting structure and frames around openings.

A. 大翼的主要结构框架包括梁、肋、桁条、燃油箱整体结构、翼尖油箱支撑结构和开口周围结构。

B. 大翼的主要框架包括隔框、肋、加强筋、内部燃油箱结构、翼尖油箱支撑结构和结构周围的开口。

C. 大翼的主要结构包括翼梁、隔框、肋条、内部燃油箱结构、翼尖油箱支撑结构和结构周围的开口。

In the description of the airplane＇s Instrument Panel, the instruments, lights, switches and controls found on the panel shall be named and their uses explained.

A. 描述飞机仪表面板时，应命名并说明面板上的仪表、灯光、电门和控件的使用。

B. 描述飞机仪表面板时，应明确面板上各个仪表、灯、开关和控制按钮的名称，并描述各自操作方法。

C. 描述飞机仪表面板时，应命名并说明台板上的仪器、灯光、电门和控件的使用。