1.4 Joint Aircraft SystemComponent (JASC) Code联合飞机系统/组件(JASC)代码-航修札记

Joint Aircraft SystemComponent (JASC) Code联合飞机系统/组件(JASC)代码

The Joint Aircraft System/Component (JASC) Code table is a modified version of the Air Transport Association of America (ATA) Specification 100 code, developed by the FAA’s Regulatory Support Division (AFS-600). Over the years, the JASC Code format of the ATA-100 Specifications has gained widespread industry acceptance. In a harmonized effort, the FAA’s counterparts in Australia and Canada have adopted the JASC Code with only a few exceptions. Some Canadian aircraft manufacturers have also adopted this new standard.

联合飞机系统/组件(JASC)代码表是美国航空运输协会(ATA)规范100的修改版本,由美国联邦航空管理局(FAA)监管支持部门(AFS-600)开发。多年来,ATA-100规范的JASC代码格式已获得业界的广泛认可。在共同努力下,澳大利亚和加拿大的同行也采用了JASC代码,只有少数例外。一些加拿大飞机制造商也采用了这一新标准。

This table can be used as a quick reference chart, to assist in the coding and review of aircraft structures or systems data. It uses the new JASC code four (4) digit format, in which the first two digits represent the code “chapter” title. The titles have been modified in some cases to clarify the intended use of the accompanying code.

该表可作为快速参考图表,用于飞机结构或系统数据的编码和审查。它采用新的JASC代码四(4)位数字格式,其中前两位数字代表代码“章节”标题。在某些情况下,标题已修改,以阐明附带代码的预期用途。

Note: The JASC Code divides the engine-related codes into two groups to separate turbine and reciprocating engines. The codes for the turbine engines are in JASC Code Chapter 72, Turbine/Turboprop Engine. The codes for the reciprocating engines are now exclusively found in Chapter 85, Reciprocating Engine.

注:JASC代码将发动机相关代码分为两组,以区分涡轮发动机和往复式发动机。涡轮发动机的代码位于JASC代码第72章“涡轮/涡轮螺旋桨发动机”中。往复式发动机的代码现在仅位于第85章“往复式发动机”中。