AS4461C-2016

Assembly and Soldering Criteria for High Quality/High Reliability Soldering Wire and Cable Termination in Aerospace Vehicles


AS4461C-2016 发布历史

Applicability This standard is applicable to manual soldering and machine soldering processes utilizing controlled soldering devices@ for electrical connections for wiring and cabling used in aerospace vehicles. Description of a component or device herein is not to be construed as authorizing the use of the component or device. Safety Considerations This standard may involve hazardous materials@ operations@ and equipment. This standard does not purport to address all of the safety problems associated with its use. It is the responsibility of users of this standard to comply with appropriate safety and health practices and regulatory limitations. Strain Relief The use of solder devices for wire or cable terminations in aircraft requires strain relief in all applications or designs with no strain on the solder terminations. Soldered wire or cable terminations may separate under physical load. The separation time is function of the ambient and electrical temperatures. Solder Joint Protection Sealing protection for solder terminations is recommended when a potential electrical overload could cause the solder to melt and short adjacent terminations.

AS4461C-2016由SAE - SAE International 发布于 2016-07-01,并于 2016-07-14 实施。

AS4461C-2016的历代版本如下:

 

 

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标准号
AS4461C-2016
发布日期
2016年07月01日
实施日期
2016年07月14日
废止日期
中国标准分类号
/
国际标准分类号
/
发布单位
SAE - SAE International
引用标准
38
适用范围
Applicability This standard is applicable to manual soldering and machine soldering processes utilizing controlled soldering devices@ for electrical connections for wiring and cabling used in aerospace vehicles. Description of a component or device herein is not to be construed as authorizing the use of the component or device. Safety Considerations This standard may involve hazardous materials@ operations@ and equipment. This standard does not purport to address all of the safety problems associated with its use. It is the responsibility of users of this standard to comply with appropriate safety and health practices and regulatory limitations. Strain Relief The use of solder devices for wire or cable terminations in aircraft requires strain relief in all applications or designs with no strain on the solder terminations. Soldered wire or cable terminations may separate under physical load. The separation time is function of the ambient and electrical temperatures. Solder Joint Protection Sealing protection for solder terminations is recommended when a potential electrical overload could cause the solder to melt and short adjacent terminations.




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