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1951-06-01
Standard
AMS3004A
This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those specifications which have previously been widely used and which may be required on some existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. “NONCURRENT” specifications are available from SAE upon request.
1951-06-01
Standard
AMS3006A
This specification covers mixtures of methyl alcohol and/or ethyl alcohol with water in the form of liquids.
1951-06-01
Standard
AMS6412D
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
1951-06-01
Standard
AMS6442B
This specification covers a low-alloy steel in the form of bars, forgings, and forging stock. Primarily for parts of small cross-section, such as needle bearings, requiring a through-hardening steel usually with hardness of approximately 60 HRC and subject to very rigid inspection standards.
1951-06-01
Standard
AMS7240A
This specification covers plain helical lock washers fabricated from heat treated carbon steel.
1951-06-01
Standard
AMS7304A
This specification covers coiled springs fabricated from carbon-steel wire.
1951-06-01
Standard
AMS7301B
This specification has been declared “NONCURRENT” by the Aerospace Materials Division, SAE, as of August 2009. It is recommended, therefore, that this specification not be specified for new designs. “NONCURRENT” refers to those specifications which have previously been widely used and which may be required for production or processing of existing designs in the future. The Aerospace Materials Division, however, does not recommend these specifications for future use in new designs. “NONCURRENT” specifications are available from SAE upon request.
1951-06-01
Standard
AMS5785A
This specification covers a corrosion and heat resistant steel in the form of covered welding electrodes.
1951-06-01
Standard
AMS5783A
This specification covers a corrosion and heat resistant steel in the form of covered welding electrodes.
1951-06-01
Standard
AMS5794A
This specification covers a corrosion and heat-resistant iron alloy in the form of welding wire.
1951-06-01
Standard
AMS5795A
This specification covers a corrosion and heat resistant iron alloy in the form of covered welding electrodes.
1951-06-01
Standard
AMS5626A
This specification has been 'Cancelled' by the Aerospace Materials Division, SAE, as of January 1997. Alloy: T1 UNS Number: T12001
1951-06-01
Standard
AMS6264C
This specification covers an aircraft quality, low alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
1951-06-01
Standard
AMS6266A
This specification covers an aircraft-Quality, Low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
1951-06-01
Standard
AMS6270F
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
1951-06-01
Standard
AMS6272D
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
1951-06-01
Standard
AMS6324A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts, 0.750 inch (19.05 mm) and under in section thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 50 HRC when properly hardened and tempered and also parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.
1951-06-01
Standard
AMS6328B
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
1951-06-01
Standard
AMS6342B
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
1951-06-01
Standard
AMS5392C
This specification covers a moderate corrosion and heat resistant alloy iron in the form of sand castings.
1951-06-01
Standard
AMS5389A
This specification covers a corrosion and heat resistant nickel alloy in the form of sand castings.
1951-06-01
Standard
AMS5683B
This specification covers a corrosion and heat resistant nickel alloy in the form of welding wire.
1951-06-01
Standard
AMS5681A
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of September 1996, and has been superseded by AWS A5.4 E347. Alloy: 30347 UNS Number: W34710
1951-06-01
Standard
AMS5684A
This specification covers a corrosion and heat resistant nickel alloy in the form of covered welding electrodes. Primarily for shielded metal arc welding of corrosion and heat resistant steels and alloys. Alloy: Inconel WE 132 UNS Number: W86132
1951-06-01
Standard
AMS5695A
This specification covers a corrosion and heat resistant steel in the form of covered welding electrodes.
1951-06-01
Standard
AMS5691A
This specification covers a corrosion and heat resistant steel in the form of covered welding electrodes. Primarily for shielded-metal-arc welding of parts fabricated from steels of similar composition, particularly when the weld zone is required to have strength and corrosion-resistance comparable to those of the parent metal.
1951-06-01
Standard
AMS5053A
ABSTRACT
1951-06-01
Standard
AMS5061A
This specification has been declared "NONCURRENT " by the Aerospace Materials Division, SAE, as of February 2009. It is recommended, therefore, that this specification not be specified for new designs.
1951-06-01
Standard
AMS5310B
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of November 1994. It is recommended, therefore, that this specification not be specified for new designs.
1951-06-01
Standard
AMS5365A
This specification has been declared "NONCURRENT" by the Aerospace Materials Division, SAE, as of January 1995. It is recommended, therefore, that this specification not be specified for new designs.
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