759. This Specification was developed by the General Aviation Manufacturers Association as guidance for airplane, engine and component manufacturers in preparing Continuing Airworthiness Program Inspection Documents ( ) CAPs may be prepared for all types of general aviation airplanes and components certificated under the applicable Federal Aviation Regulations

2604. For purposes of this specification, airplane" refers to the airframe and related components specified in the Type Certificate or made available as options by the airplane manufacturer"

2603. The related caution light must go off after 30 seconds

2602. 关于一般信息,参见发动机工作限制指南和专用程序

2601. 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

2600. 再次启动发动机前,清除地面燃油。

2599. For pressurized airplanes and turbo supercharged or turboprop Eller powered airplanes, the Maximum Altitude Limits shall be stated

2598. 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。

2597. The flight crew can use the flight director commands to control the attitude of the airplane

2596. 使用危险品前,要遵守这些注意事项

2595. If it is possible that the temperature values will be more than the permitted limits, decrease the power