1350. As a rule,the engines are attached under the wings,but,in the case of the modern aircraft,the two side engines are mounted on struts outboard of the fuselage ( )
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2950. 本章介绍了记录、存储或计算来自不相关系统数据的组件。( )
2949. 如适用,提供增压,加热,冷却,湿度控制,过滤和处理用于通风增压密封机身内部区域的空气的装置和组件( )
2948. 在无保护的表面上涂抹两层密封剂。( )
2947. 副翼的通道从发射机接收输入信号 ( )
2946. 确保罗盘系统 1 和罗盘系统 2 是同步的 ( )
2945. 所有的修改都要得到设计部门的批准。 ( )
2944. [ ]THE ENGINE( )
2943. The manufacturer may establish procedures to provide feedback[from operators and maintenance facilities who comply with a CAP)on unairworthy conditions[whether covered or not covered by the CAP)that were discovered when complying
2942. All publications shall use the standard numbering system for indexing and assignment of subject matter prescribed in this specification even though all chapters may not be applicable to the aircraft or to the publication ( )
2941. To prevent the friction, polish the surface( )
