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Viewing 10171 to 10200 of 10240
CURRENT
1941-03-01
Standard
AMS6337
No scope available.
CURRENT
1940-12-04
Standard
AMS6335
No scope available.
CURRENT
1940-12-01
Standard
AMS6332
No scope available.
HISTORICAL
1940-12-01
Standard
AMS2400
This specification covers the engineering requirements for electrodeposition of cadmium on metal parts and the properties of the deposit. Primarily to provide corrosion resistance to metal parts. For plating of high-strength steel parts, see AMS 2401.
HISTORICAL
1940-10-01
Standard
AMS5683
This specification covers a corrosion and heat resistant nickel alloy in the form of welding wire.
HISTORICAL
1940-10-01
Standard
AMS2620
This specification provides requirements and procedures for hydraulic-pressure leak testing of parts.
HISTORICAL
1940-10-01
Standard
AMS2625
This specification provides requirements and procedures for hydraulic-pressure leak testing of parts.
HISTORICAL
1940-10-01
Standard
AMS2503
This specification covers the engineering requirements for finishing aircraft parts and assemblies with a black enamel.
HISTORICAL
1940-10-01
Standard
AMS2616
This specification provides requirements and procedures for hydraulic-pressure leak testing of parts.
HISTORICAL
1940-10-01
Standard
AMS5665
This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1940-10-01
Standard
AMS2510
This specification covers the engineering requirements for finishng aircraft parts and assemblies with an engine gray enamel.
HISTORICAL
1940-06-13
Standard
AMS6252
No scope available.
HISTORICAL
1940-06-13
Standard
AMS6253
No scope available.
HISTORICAL
1940-06-01
Standard
AMS2601
This specification provides requirements and procedures for gas-pressure leak testing of parts.
HISTORICAL
1940-06-01
Standard
AMS3080
HISTORICAL
1940-06-01
Standard
AMS2606
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1940-06-01
Standard
AMS2800
This specification covers the requirements for identification of finished parts.
HISTORICAL
1940-06-01
Standard
AMS2808
This specification covers requirements for identification of forgings, including die forgings, hand forgings, and rolled rings.
HISTORICAL
1940-06-01
Standard
AMS2804
This specification covers requirements for identification of castings.
HISTORICAL
1940-03-13
Standard
AMS3410
This specification covers a silver-brazing flux in the form of a paste which contains not more than 35% water by weight.
HISTORICAL
1940-03-01
Standard
AMS5060
This specification covers a low-carbon steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1940-03-01
Standard
AMS7240
This specification covers plain helical lock washers fabricated from heat treated carbon steel.
HISTORICAL
1940-03-01
Standard
AMS3180
This specification covers, industrial-grade toluene in the form of a liquid.
HISTORICAL
1940-03-01
Standard
AMS2475
This specification establishes the requirements for chromate conversion coatings on magnesium alloys. This process has been used typically to improve corrosion resistance and adherence of organic finishes but usage is not limited to such applications. The dichromate treatment may not be suitable for alloys with high manganese content. The chrome pickle treatment has been used as touch-up for previously dichromate-treated surfaces and for improving corrosion protection temporarily, but usages are not limited to such applications.
HISTORICAL
1940-03-01
Standard
AMS5700
This specification covers a corrosion and heat-resistant steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1940-03-01
Standard
AMS5040
This specification covers a carbon steel in the form of sheet and strip.
HISTORICAL
1940-03-01
Standard
AMS5042
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.
HISTORICAL
1940-01-25
Standard
AMS6412
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
HISTORICAL
1940-01-23
Standard
AMS6415
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
Viewing 10171 to 10200 of 10240