A、 如适用，该信息应包含在供应商出版物中。如果供应商数据已并入为飞机手册的一部分，则该信息同时包含在飞机维修手册中。
B、 这些信息包含在适用的供应商出版物中，并包含在飞机维护手册中，手册中也包括了部分相关的供应商数据。
C、 这类信息不仅包含在供应商出版物的适当位置，还包含在飞机维修手册中，同时部分供应商数据也合并入飞机手册中。
答案：A
A、 如适用，该信息应包含在供应商出版物中。如果供应商数据已并入为飞机手册的一部分，则该信息同时包含在飞机维修手册中。
B、 这些信息包含在适用的供应商出版物中，并包含在飞机维护手册中，手册中也包括了部分相关的供应商数据。
C、 这类信息不仅包含在供应商出版物的适当位置，还包含在飞机维修手册中，同时部分供应商数据也合并入飞机手册中。
答案：A
A. When hydraulic power is supplied, keep persons and equipment away from all control surfaces and landing gear.
B. When supplying power to the hydraulic system, persons and equipment should be away from all control surfaces and landing gear.
C. Persons and equipment shall be away from all hydraulic system control surfaces and landing gear when supply pressure.
A. 拧紧螺栓时使用不同的措辞。
B. 使用不同的扳手拧紧螺栓。
C. 拧螺栓时使用不同的扭矩。
A. If the unit is not modified, its service life will be possibly shorter.
B. Without the modification of the unit, its service life is likely shorter than present.
C. Without the modification, it is possible that the service life of this unit will be shorter than usual.
A. 文本说明和有关例句构成了每个规则。
B. 每项规则都附有文字解释和相应事例。
C. 每条规则包括解释性的文本和相关的例子。
A. 左1号登机门1号地板右前边缘有一条1英寸深6英寸长的凹陷。
B. 左1号登机门1号地板离右前边缘6英寸处有一条1英寸深的凹槽。
C. 左1号登机门有一块地板到右前边缘6英寸处有一条1英寸深的凹坑。
A. 保留部分未达到满意粘合度的密封。
B. 丢弃所有粘合效果达标的密封件。
C. 丢弃所有黏合不好的密封件。
A. The user of the schematic diagram is the pilot.
B. The captain must use the schematic diagram.
C. The principle scheme should be used by the co-pilot.
A. In STE, there are different rules for how to write sentences for procedures (Section 5) and for how to write them for descriptive text (Section 6).
B. In STE, there are different rules for why to write paragraphs for procedures (Section 5) and for why to write them for descriptive text (Section 6).
C. How to write sentences for programs (Section 5) and how to write sentences for operative text (Section 6) have different means in STE.
A. Make up for all gaps which are larger than 0.05 mm.
B. Repair all cracks that are wider than 0.05 mm.
C. Overhaul all fissures which are greater than 0.05mm.
A. Make sure that the pressure in the cabin is almost zero.
B. Verify that the cabin pressure is not above zero.
C. Ensure that the pressure in the cabin is completely zero.
