SAE AS 5498-2001
飞行中冰检测系统的最低操作性能规范

Minimum Operational Performance Specification for Inflight Icing Detection Systems

SAE AS 5498-2001 发布历史

The objective of this Minimum Operational Performance Specification is to specify the minimum performance of onboard inflight icing detection systems. Throughout the document, these devices are referred to as Flight Icing Detection Systems (FIDS). These systems are intended to either provide information which indicates the presence of ice accreted in flight on monitored surfaces or indicate the presence of icing conditions in the atmosphere. They may operate the airplane anti-ice/deice systems. Detection of ice accreted on the ground is not considered in this document but can be found in ED-104. This MOPS was written for the use of FIDS on airplanes only, as defined in paragraph 1.5. Use on other aircraft may require additional considerations.

SAE AS 5498-2001由美国机动车工程师协会 US-SAE 发布于 2001。

SAE AS 5498-2001 在中国标准分类中归属于: V46 航空器试验设备，在国际标准分类中归属于: 49.090 机上设备和仪器。

SAE AS 5498-2001 发布之时，引用了标准

• SAE AIR 4367-1995 
• SAE ARP 4761-1996 对民用机载系统和设备进行安全性评估过程的准则和方法
• SAE AS 8034-1982 

SAE AS 5498-2001的历代版本如下：

• 2001年 SAE AS 5498-2001 飞行中冰检测系统的最低操作性能规范

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标准号

SAE AS 5498-2001

发布日期

2001年

实施日期

废止日期

无

中国标准分类号

V46

国际标准分类号

49.090

发布单位

美国机动车工程师协会

引用标准

SAE AIR 4367-1995 SAE ARP 4256-1996 SAE ARP 4761-1996 SAE AS 8034-1982 MIL-STD-1472

适用范围

The objective of this Minimum Operational Performance Specification is to specify the minimum performance of onboard inflight icing detection systems. Throughout the document, these devices are referred to as Flight Icing Detection Systems (FIDS). These systems are intended to either provide information which indicates the presence of ice accreted in flight on monitored surfaces or indicate the presence of icing conditions in the atmosphere. They may operate the airplane anti-ice/deice systems. Detection of ice accreted on the ground is not considered in this document but can be found in ED-104. This MOPS was written for the use of FIDS on airplanes only, as defined in paragraph 1.5. Use on other aircraft may require additional considerations.

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