A、 Make sure that the bolt heads are attached to the skin.
B、 Make sure that the screw heads are connected with the metal.
C、 Make sure that the fastener heads are flush with the skin.
答案：C
A、 Make sure that the bolt heads are attached to the skin.
B、 Make sure that the screw heads are connected with the metal.
C、 Make sure that the fastener heads are flush with the skin.
答案：C
A. 定义措辞应尽可能简单,并必须符合手册中所定义的术语的使用。
B. 定义应尽可能简单地被记录,且必须保证手册中已定义术语的使用。
C. 定义应尽可能用词简单,且必须强制使用手册中规定的术语。
A. 如果左 CMC 故障,会自动转换使右 CMC 提供输出
B. 如果左 CMC 失效,会自动打开电门,由右 CMC 提供输出
C. 如果左 CMC 掉落,自动电门会使右 CMC 提供输出
A. Check left engine inboard wing leading edge if have damage and dent before the aircraft takes off.
B. Check wing leading edge inboard left engine for damage and dent before the aircraft takes off.
C. Check the wing leading edge of left engine inboard for damage and dent before the aircraft takes off.
A. 如果剪切销遭受撞击,要测试牵引杆。
B. 如果定位销断裂,要检查两根杆。
C. 如果剪切销断裂,要检查牵引杆。
A. You may use alerts and cautions to emphasize some important places.
B. The important parts must be highlighted by using the warnings,cautions and notes.
C. Warnings,cautions and notes may be used to highlight or emphasize important points.
A. 确保厕所组件正确冲洗。
B. 确保厕所马桶正常工作。
C. 确保厨房组件正常工作。
A. 在维护和修理期间支撑飞机所需的说明,包括支撑材料和设备、外形尺寸、支撑位置等信息。
B. 这些必要的说明是支撑飞机维修和修理期间使用的,包括顶升材料和设备,大概尺寸,顶升位置等信息。
C. 在维护和修理期间支撑飞机所需的文件,包括支撑材料和设备、大概尺寸、支撑位置等信息。
D. C.在维护和修理期间支撑飞机所需的文件,包括支撑材料和设备、大概尺寸、支撑位置等信息。
A. 制造商应在本节中提供一个设备列表,并以单独文件形式附在《飞行员运营手册》中,或作为单独的文件。如果设备列表未包含在本节中,说明其位置。
B. 制造商应提供一份相关设备清单,可以包含在本节中,也可以作为《飞行员操作手册》的附录,也可以作为单独的文件。设备清单未包含在本节中时,应说明其位置。
C. 制造商应在本节中提供一份设备清单,并把《飞行员操作手册》作为单独附件或单独文件。如果装备列表未包含在本节中,说明其方向。
A. Mach digit is the percent of true airspeed to the speed of sound.
B. Mach number is the ratio of true airspeed to the speed of sound.
C. Mach number is the proportion of real airspeed to the speed of light.
A. The EEC processes the simulated signal from the fuel filter differential pressure bulb.
B. The fuel filter differential pressure sensor sends an modulated signal to the EE
C. The EEC receives the analog signal from the fuel filter differential pressure switch.
D. C.The EEC receives the analog signal from the fuel filter differential pressure switch.
