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Viewing 1 to 30 of 159
2007-11-09
WIP Standard
AMS3603B
This specification covers adhesive-backed protective film, pigmented or clear, for aircraft exterior applications. This film is used typically as a replacement for polyurethane paint topcoats on military and commercial exterior aircraft surfaces. The film has been designed to meet air pollution regulations with zero emission of volatile organic compounds (VOC)/organic hazardous air pollutants (HAP).
2016-10-01
WIP Standard
AMS3604A
This specification establishes requirements for a heat resistant aluminized organic coating with sufficient corrosion and erosion resistance for the finished substrate.
2007-04-17
WIP Standard
AMS3146A
This specification covers interior aircraft cabin coatings, which when tested under specified conditions exhibit low heat release and smoke release properties.
2009-09-02
WIP Standard
AMS3116B
This specification covers two types of two-component, epoxy, chemical and solvent resistant primer coatings formulated primarily for spray application. Coatings shall be compatible with epoxy and polyurethane topcoats.
2008-01-23
WIP Standard
AMS1659A
This specification covers a barrier coating in the form of a ready-to-be applied liquid with a consistency suitable for brush, spray, or dip application to exterior surfaces of aircraft. Primarily as a temporary protective coating for painted and unpainted exterior surfaces of aircraft to ease soil removal from difficult-to-clean areas and to increase paint durability.
2015-07-28
WIP Standard
AMSC83231B
This specification covers the requirements for two classes and two types of rain erosion resistant coatings. This specification has been prepared as a direct replacement for the Military Specification MIL-C-83231A Notice 1. These products have been used for protecting glass fabric reinforced plastic laminates and other plastic parts used for exterior surfaces of aircraft and missiles, but usage is not limited to such applications.
2011-02-28
WIP Standard
G811AA
The specification would establish requirements for the application of heavy-duty, super pentrating, water displacing corrosion inhibiting compound that can be applied by conventional airless or air-operated spray equipment and after drying form a firm transparent discernible protective coating with a low film weight.
2015-09-08
WIP Standard
G815AA
The clear coating is an interior decorative coating used on metal substrates to enhance decorative value and for wear protection. Certain metal might tarnish if it doesn’t have a coating applied it to protect against scratches, and the clear coating allows you to protect the surface as well as bring up the gloss.
HISTORICAL
1952-02-01
Standard
AMS3132A
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
HISTORICAL
1952-06-01
Standard
AMS3132B
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
HISTORICAL
1976-01-01
Standard
AMS3132D
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
HISTORICAL
1966-09-01
Standard
AMS3132C
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
HISTORICAL
1959-06-01
Standard
AMS3135
This specification covers an unpigmented silicone-resin-base coating material. Primarily for use on chemically or electrochemically treated magnesium and aluminum alloy surface to improve the high temperature corrosion and abrasion resistance and the air flow characteristics. The coating may also be used on steel for improvement of corrosion resistance.
HISTORICAL
1976-01-01
Standard
AMS3135B
This specification covers an unpigmented silicone-resin-base coating material. Primarily for use on chemically or electrochemically treated magnesium and aluminum alloy surface to improve the high temperature corrosion and abrasion resistance and the air flow characteristics. The coating may also be used on steel for improvement of corrosion resistance.
HISTORICAL
1966-09-01
Standard
AMS3135A
This specification covers an unpigmented silicone-resin-base coating material. Primarily for use on chemically or electrochemically treated magnesium and aluminum alloy surface to improve the high temperature corrosion and abrasion resistance and the air flow characteristics. The coating may also be used on steel for improvement of corrosion resistance.
HISTORICAL
1978-10-01
Standard
AMS3135C
This specification covers an unpigmented silicone-resin-base coating material. Primarily for use on chemically or electrochemically treated magnesium and aluminum alloy surface to improve the high temperature corrosion and abrasion resistance and the air flow characteristics. The coating may also be used on steel for improvement of corrosion resistance.
HISTORICAL
1970-11-01
Standard
AMS3145
This specification covers two-component colored systems composed of a resin and a miscible hardener supplied in kit form. Primarily for identification marking of parts and equipment exposed to temperatures from -55 to +150 degrees C (-65 to +300 degrees F) where various colors are needed. Systems produce tile-like compounds with good hardness, moisture and solvent resistance, and adhesion to metallic surfaces when properly cured.
HISTORICAL
1978-04-01
Standard
AMS3145A
This specification covers two-component colored systems composed of a resin and a miscible hardener supplied in kit form. Primarily for identification marking of parts and equipment exposed to temperatures from -55 to +150 degrees C (-65 to +300 degrees F) where various colors are needed. Systems produce tile-like compounds with good hardness, moisture and solvent resistance, and adhesion to metallic surfaces when properly cured.
HISTORICAL
1978-04-01
Standard
AMS3126A
This specification covers a corrosion and heat resistant aluminum coating material supplied as a liquid of suitable consistency for coating parts after being thoroughly mixed.
HISTORICAL
1971-05-01
Standard
AMS3126
This specification covers a corrosion and heat resistant aluminum coating material supplied as a liquid of suitable consistency for coating parts after being thoroughly mixed.
HISTORICAL
1945-10-01
Standard
AMS3130
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
HISTORICAL
1948-05-01
Standard
AMS3132
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
HISTORICAL
1968-05-01
Standard
AMS3130C
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
HISTORICAL
1978-01-15
Standard
AMS3130D
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
HISTORICAL
1952-02-15
Standard
AMS3130A
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
HISTORICAL
1954-11-01
Standard
AMS3130B
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
HISTORICAL
1951-12-01
Standard
AMS3108A
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
HISTORICAL
1948-07-01
Standard
AMS3108
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
HISTORICAL
1978-01-01
Standard
AMS3108C
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
HISTORICAL
1968-05-01
Standard
AMS3108B
This specification has been declared “CANCELLED” by the Aerospace Materials Division, SAE, as of June 2009. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications indicating that it has been “CANCELLED”. Cancelled specifications are available from SAE.
Viewing 1 to 30 of 159