SAE AMS 3694B-2012
-55至+130℃(-65至+270°F)柔性的空气动力校平复合物

Aerodynamic Smoothing Compound, Flexible, -55 to +130°C (-65 to +270°F)

SAE AMS 3694B-2012 发布历史

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This specification covers a two-component air-curing resin-base material in the form of a paste or putty, suitable for application by spatula or putty knife. Primarily to fill aircraft skin depressions to a maximum depth of 0.250 in. (6.25 mm) and be capable of being painted with subsequent specified coatings. These materials are meant for filling small holes, crevices, and gaps or for smoothing areas requiring thin layers of flexible material to produce the required smoothness on aerodynamic surfaces. Suitable for maintaining adhesion to surfaces subject to service temperatures from -55 degrees to +130 degrees C (-65 degrees to +270 degrees F).

SAE AMS 3694B-2012由美国机动车工程师协会 US-SAE 发布于 2012-01-17。

SAE AMS 3694B-2012 在中国标准分类中归属于: V10 航空、航天材料基础标准，在国际标准分类中归属于: 49.040 有关航空航天制造用镀涂和有关工艺。

SAE AMS 3694B-2012的历代版本如下：

• 2012年01月17日 SAE AMS 3694B-2012 -55至+130℃(-65至+270°F)柔性的空气动力校平复合物

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标准号

SAE AMS 3694B-2012

发布日期

2012年01月17日

实施日期

废止日期

无

中国标准分类号

V10

国际标准分类号

49.040

发布单位

US-SAE

引用标准

ASTM D 412-2006 ASTM D 471-2010 ASTM D 1210-2005 ASTM D 1824-1995 ASTM D 2240-2005 ASTM D 3182-2007 ASTM D 3359-2009 ASTM STP 500 MIL-A-8625-1993 SAE AMS 2350BA-1989 SAE AMS 2471 SAE AMS 2478 SAE AMS 2825 SAE AMS 3020-1978 SAE AMS 3021 SAE AMS 3821 SAE AM

被代替标准

SAE AMS 3694A-1983

适用范围

This document has been declared "Stabilized" and will no longer be subjected to periodic reviews for currency. Users are responsible for verifying references and continued suitability or technical requirements. New technology may exist. This specification covers a two-component air-curing resin-base material in the form of a paste or putty, suitable for application by spatula or putty knife. Primarily to fill aircraft skin depressions to a maximum depth of 0.250 in. (6.25 mm) and be capable of being painted with subsequent specified coatings. These materials are meant for filling small holes, crevices, and gaps or for smoothing areas requiring thin layers of flexible material to produce the required smoothness on aerodynamic surfaces. Suitable for maintaining adhesion to surfaces subject to service temperatures from -55 degrees to +130 degrees C (-65 degrees to +270 degrees F).