A、 Atmospheric conditions, including large supercooled water droplets, freezing rain or a mixture of conditions, may exceed the FAR parameters and the capabilities of the certified ice protection system.
B、 Atmosphere conditions which include large too cold water drip, ice rain or a mixed conditions, may deviate the FAR specifications and the ability of the qualified anti-ice system.
C、 The atmospheric conditions except for large overcold water drops, frozen rain or the combination condition, may exceed the FAR data and the verified anti-ice system capability.
答案：A
A、 Atmospheric conditions, including large supercooled water droplets, freezing rain or a mixture of conditions, may exceed the FAR parameters and the capabilities of the certified ice protection system.
B、 Atmosphere conditions which include large too cold water drip, ice rain or a mixed conditions, may deviate the FAR specifications and the ability of the qualified anti-ice system.
C、 The atmospheric conditions except for large overcold water drops, frozen rain or the combination condition, may exceed the FAR data and the verified anti-ice system capability.
答案：A
A. The basis for assuring an airplane remains airworthy and safe to operate is to combine the manufacturer＇s requirements with sound inspection and maintenance practices.
B. To ensure airworthiness and safe operation of an airplane, it is essential to follow the manufacturer＇s instructions in the utilization of airplane, and perform sound inspection and maintenance practices as well.
C. Airworthiness and safe operation are fundamental to aircraft utilization as required by the manufacturer, so sound inspection and maintenance practices are carried out.
A. 持续权威程序测试通常由两页组成：一个文本页和一个图解页。
B. 持续适航工作检查总是包含两页：一个文本页和一个描述页。
C. 持续适航程序检查通常包括两页：一个文本页和一个图解页。
A. 应当提供在客舱内或发动机冒烟或起火的情况的处理程序。
B. 应对机舱内或发动机的烟雾报警有特定的处理说明。
C. 手册中专门描述了如何应对飞机起火或冒烟的紧急情况的处理措施。
A. 发动机附件冷却系统用于发动机舱及附件通风，包括阀门、管路、引射泵、涡流发生器等部件。
B. 发动机辅助冷却系统能帮助发动机及附件通风，包括阀门、波导设备、喷射泵、扰流器等组件。
C. 发动机辅助冷却系统用于发动机舱、活门、管路、引射泵、涡流发生器等附件通风。
A. 描述飞机电源系统时，应阐述容量和装载减少。
B. 描述飞机电源系统时，应阐述电源的容量和卸载。
C. 描述飞机电源系统时，应阐述容量和载荷去除。
A. The System/Chapter, sub-System/Section and Subject Number, the page number and date of issue will disappear in the lower left-hand corner, on the left-hand pages and the review date in the lower right-hand corner.
B. The System/Chapter, sub-System/Section and Subject Number, the page number and date of issue will appear in the lower left-hand corner, on the left-hand pages and the review date in the lower right-hand corner.
C. The System/Chapter, sub-System/Section and Subject Number, the page number and date of public will appear in the lower left-hand corner, on the left-hand pages and the revision date in the lower right-hand corner.
A. Maximum Limiting speed Unsticks is the speed restrain which will not be intentionally surpassed in typical flight operations. V is communicated in knots and M in Mach Number.
B. Maximum Restriction Speed is the fastest a plane can fly without breaking the rules in normal flight. The speed is measured in knots and Mach Number.
C. Maximum Operating Limit Speed is the speed limit that may not be deliberately exceeded in normal flight operations. V is expressed in knots and M in Mach Number.
A. When described the aircraft and its system, you should always use third people talking.
B. Generally, in describing the airplane or its system, third person wording should be used.
C. When you describing the airplane systems, third person mood shall be used.
A. Make sure there is no leakage of hydraulic fluid at the router.
B. Make sure there is no leakage of hydraulic fluid at the transducer.
C. Make sure there is no leakage of hydraulic fluid at the transponder.
A. Maximum altitude loss during stall recovery is approximately 800 feet.
B. Maximum altimeter loss during spin recovery is about 800 feet.
C. Maximum weight loss during stall recovery is nearly 800 feet.
