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Viewing 20521 to 20550 of 20733
HISTORICAL
1942-03-01
Standard
AMS6250B
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
AMS6242B
HISTORICAL
1942-03-01
Standard
AMS6253B
No scope available.
HISTORICAL
1942-03-01
Standard
AMS6252B
HISTORICAL
1942-03-01
Standard
AMS6254B
No scope available.
HISTORICAL
1942-03-01
Standard
AMS6290B
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
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
AMS6315A
HISTORICAL
1942-03-01
Standard
AMS6312A
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
AMS6292B
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
1942-03-01
Standard
AMS6294B
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, and forging stock.
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
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
AMS3232A
HISTORICAL
1942-01-01
Standard
AMS4815
This specification covers bearings of low-carbon steel plated on one or both faces with silver.
HISTORICAL
1942-01-01
Standard
AMS3500
This specification covers leather tanned with chromium salts and retanned with vegetable tanning material.
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
AMS4140
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 materials which may have been widely used previously 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
1942-01-01
Standard
AMS4220
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of November 1995.
1942-01-01
Standard
AMS4076
1. ACKNOWLEDGMENT: A vendor shall mention this specification number and its revision letter in all quotations and when acknowledging purchase orders. 2. COM1POSITION: Silicon 45 to 65% of magnesium content Magnesium 1.10 - 1.40 Chromium 0.15 - 0.35 Iron 0.35 max Copper 0.10 max Titanium 0.10 max Manganese 0.10 max Zino 0.10 max Other Impurities, each 0.05 max Other Impurities, total 0.15 max Aluminum remainder
HISTORICAL
1942-01-01
Standard
AMS4088
This specification covers an aluminum alloy in the form of seamless, drawn tubing.
HISTORICAL
1942-01-01
Standard
AMS2607
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1942-01-01
Standard
AMS2602
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
AMS2606A
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
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
AMS4017
This specification covers an aluminum alloy in the form of sheet and plate.
HISTORICAL
1942-01-01
Standard
AMS3226
This specification covers a nitrile (NBR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes. Primarily for hose, packings, bushings, grommets, and seals in contact with hot, petroleum-base lubricating oils and glycol-type coolants from -40 degrees to +100 degrees C (-40 degrees to +212 degrees F).
Viewing 20521 to 20550 of 20733