SAE AS 4273A-2007
航空器发动机和航空器发动机装置用流体处理部件的防火测试

(R) Fire Testing of Fluid Handling Components for Aircraft Engines and Aircraft Engine Installations

SAE AS 4273A-2007 发布历史

This document establishes requirements, test procedures, and acceptance criteria for the fire testing of fluid handling components and materials used in aircraft fluid systems. It is applicable to fluid handling components other than those prescribed by AS1055 (e.g., hoses, tube assemblies, coils, fittings). It also is applicable to materials, wiring, and components such as reservoirs, valves, gearboxes, pumps, filter assemblies, accumulators, fluid-cooled electrical/electronic components, in-flight fluid system instrumentation, hydromechanical controls, actuators, heat exchangers, and manifolds. These components may be used in fuel, lubrication, hydraulic, or pneumatic systems.

SAE AS 4273A-2007由美国机动车工程师协会 US-SAE 发布于 2007-02-01。

SAE AS 4273A-2007 在中国标准分类中归属于: V30 发动机总体，在国际标准分类中归属于: 49.060 航空航天用电气设备和系统。

SAE AS 4273A-2007 发布之时，引用了标准

• ISO 2685-1998 航空器 机载设备的环境试验程序 指定防火区的防火
• SAE AS 1055D-1997 柔性软管,导管总成,线圈,接头和类似系统部件的耐火试验R(2001)
• SAE AS 8028-1980 热和火焰控制类动力设备火警探测仪器 (往复式和涡轮发动机驱动飞机)[代替: SAE AS 401B]

SAE AS 4273A-2007的历代版本如下：

• 2007年02月01日 SAE AS 4273A-2007 航空器发动机和航空器发动机装置用流体处理部件的防火测试

SAE AS 4273A-2007 航空器发动机和航空器发动机装置用流体处理部件的防火测试 由 SAE AS 4273-1996 变更而来。

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标准号

SAE AS 4273A-2007

发布日期

2007年02月01日

实施日期

废止日期

无

中国标准分类号

V30

国际标准分类号

49.060

发布单位

US-SAE

引用标准

ISO 2685-1998 SAE AIR 1377 SAE AS 1055D-1997 SAE AS 8028-1980

被代替标准

SAE AS 4273-1996

适用范围

This document establishes requirements, test procedures, and acceptance criteria for the fire testing of fluid handling components and materials used in aircraft fluid systems. It is applicable to fluid handling components other than those prescribed by AS1055 (e.g., hoses, tube assemblies, coils, fittings). It also is applicable to materials, wiring, and components such as reservoirs, valves, gearboxes, pumps, filter assemblies, accumulators, fluid-cooled electrical/electronic components, in-flight fluid system instrumentation, hydromechanical controls, actuators, heat exchangers, and manifolds. These components may be used in fuel, lubrication, hydraulic, or pneumatic systems.