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Viewing 9781 to 9810 of 9893
HISTORICAL
1942-03-01
Standard
AMS6455A
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
HISTORICAL
1942-03-01
Standard
AMS3070
This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE as of January 1990.
HISTORICAL
1942-03-01
Standard
AMS6382A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1942-03-01
Standard
AMS2470A
This specification establishes the requirements for anodic coatings on aluminum alloys.
HISTORICAL
1942-03-01
Standard
AMS6330A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1942-03-01
Standard
AMS6317A
This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings.
HISTORICAL
1942-03-01
Standard
AMS6370A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.
HISTORICAL
1942-03-01
Standard
AMS5010A
This specification covers a free-machining carbon steel in the form of bars.
HISTORICAL
1942-01-01
Standard
AMS2450
This specification covers the procedure to be used for spraying metallic parts with aluminum and the properties of the coating.
HISTORICAL
1942-01-01
Standard
AMS2602
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1942-01-01
Standard
AMS2605
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1942-01-01
Standard
AMS2601A
This specification provides requirements and procedures for gas-pressure leak testing of parts.
HISTORICAL
1942-01-01
Standard
AMS2607
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1942-01-01
Standard
AMS5705
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of September, 2002. Alloy: CNS UNS Number: S63005
HISTORICAL
1942-01-01
Standard
AMS5710
This specification covers a corrosion and heat resistant steel in the form of bars, forgings, and forging stock.
HISTORICAL
1942-01-01
Standard
AMS2606A
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1942-01-01
Standard
AMS3500
This specification covers leather tanned with chromium salts and retanned with vegetable tanning material.
HISTORICAL
1941-11-01
Standard
AMS5515
This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate.
HISTORICAL
1941-11-01
Standard
AMS6254A
No scope available.
HISTORICAL
1941-11-01
Standard
AMS6252A
HISTORICAL
1941-11-01
Standard
AMS6253A
No scope available.
HISTORICAL
1941-11-01
Standard
AMS5540A
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, and plate.
HISTORICAL
1941-11-01
Standard
AMS5575
This specification covers a corrosion and heat-resistant steel in the form of welded tubing.
HISTORICAL
1941-11-01
Standard
AMS7310
This specification covers piston rings fabricated from cast iron.
HISTORICAL
1941-11-01
Standard
AMS6240A
HISTORICAL
1941-11-01
Standard
AMS6250A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1941-11-01
Standard
AMS6290A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. These products have been used typically for carburized parts which require low minimum core hardness and allow a wide hardness range in sections 0.375 in. (9.50 mm) and under in nominal thickness, but usage is not limited to such applications. The core may or may not be machinable after hardening.
HISTORICAL
1941-11-01
Standard
AMS6292A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock. Primarily for carburized parts which require intermediate minimum core hardness and allow wide hardness range in sections 0.25 in. (6 mm) and under in nominal thickness. The core may or may not be machinable after hardening. Alloy: 4617 UNS Number: G46170
HISTORICAL
1941-11-01
Standard
AMS6294A
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
HISTORICAL
1941-11-01
Standard
AMS5570A
This specification covers a corrosion and heat resistant steel in the form of seamless tubing. This tubing has been used typically for parts requiring both corrosion and heat resistance, especially when such parts are welded during fabrication, and also for parts requiring oxidation resistance up to 1500 degrees F (816 degrees C) but useful at that temperature only when stresses are low; usage is not limited to such applications.
Viewing 9781 to 9810 of 9893