334.Includes the functioning and maintenance aspects of items such as accessory section cowls, cowl flaps, cowling supports, and attach and locking mechanisms, etc Does not include the structure integral with the airframe which shall be covered in the applicable Structures Chapter ( )

603.The related caution light must go off after 30 seconds ( )

602.关于一般信息,参见发动机工作限制指南和专用程序 ( )

601.很难确定腐蚀的影响,但是如果收到持续适航大纲检查报告,检查时间将根据任何严重的问题进行调整( )

600.再次启动发动机前,清除地面燃油。( )

599.For pressurized airplanes and turbo supercharged or turboprop Eller powered airplanes , the Maximum Altitude Limits shall be stated ( )

598.然而,制造商可能会省略不适用于该产品的系统/章,或者在可行的情况下合并系统/ 章。( )

597.The flight crew can use the flight director commands to control the attitude of the airplane ( )

596.使用危险品前,要遵守这些注意事项( )

595.If it is possible that the temperature values will be more than the permitted limits ,
decrease the power( )

594.仅仅在表面上施加很小的压力。 ( )