Criteria

Text:
Content:
Display:

Results

Viewing 43651 to 43680 of 44329
CURRENT
1942-09-15
Standard
AS2174-7
No scope available.
CURRENT
1942-09-15
Standard
AS2225-10
No scope available.
CURRENT
1942-09-15
Standard
AS2220-5
No scope available.
CURRENT
1942-09-10
Standard
AGS1182-3
No scope available.
HISTORICAL
1942-09-01
Standard
AMS6260
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1942-09-01
Standard
AMS6280
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
1942-09-01
Standard
AMS6263
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1942-09-01
Standard
AMS6262
HISTORICAL
1942-09-01
Standard
AMS6272
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1942-09-01
Standard
AMS6274
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1942-09-01
Standard
AMS6270
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
HISTORICAL
1942-09-01
Standard
AMS6320
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
1942-09-01
Standard
AMS6325
This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings.
HISTORICAL
1942-09-01
Standard
AMS6322
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
1942-09-01
Standard
AMS6327
This specification covers an aircraft-quality, low-alloy steel in the form of bars and forgings.
HISTORICAL
1942-09-01
Standard
AMS6357
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate.
HISTORICAL
1942-09-01
Standard
AMS6355
This specification covers an aircraft-quality, low-alloy steel in the form of sheet, strip, and plate. Primarily for use where welding and moderate mechanical properties are required. Sheet and strip are extensively used where minimum tensile strength of 160,000 psi (1105 MPa) is required in sections up to 0.125 in. (3.12 mm) thick and proportionately lower strength in heavier thicknesses.
HISTORICAL
1942-09-01
Standard
AMS6535
Primarily for use where welding and moderate tensile properties are required. May be used where minimum tensile strength up to 180,000 psi (1240 MPa) is required for wall thicknesses up to 0.125 in. (3 mm) and proportionately lower strength is required in heavier thicknesses. This specification has been declared "Noncurrent" by the Aerospace Materials Division, SAE, as of 19 April 1988. It is recommended, therefore, that this specification not be specified for new designs.
HISTORICAL
1942-09-01
Standard
AMS6530
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of February 1995. The requirements of this specification are embodied in the laths issue of AMS 6360.
CURRENT
1942-08-22
Standard
AGS157-13
No scope available.
HISTORICAL
1942-08-01
Standard
AMS4130A
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
1942-08-01
Standard
AMS4140A
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
1942-08-01
Standard
AMS4145A
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of September 1996. Alloy: 4032-T6 UNS Number: A94032
HISTORICAL
1942-08-01
Standard
AMS3232B
HISTORICAL
1942-08-01
Standard
AMS4015A
This specification covers an aluminum alloy in the form of sheet and plate.
HISTORICAL
1942-08-01
Standard
AMS4231
This specification covers an aluminum alloy in the form of sand castings.
HISTORICAL
1942-08-01
Standard
AMS4037A
This specification covers an aluminum alloy in the form of sheet and plate. These products have been typically used for formed structural parts of good strength. Plate is also suitable for structural machined parts where warpage, during maching, due to residual stresses must be minimized, but usage is not limited to such application. Certain design and processing procedures may cause these products to become susceptible to stress-corrosion cracking; SAE ARP 823 recommends practices to minimize such conditions.
HISTORICAL
1942-08-01
Standard
AMS4035A
This specification covers an aluminum alloy in the form of sheet and plate. These products have been used typically for formed structural parts which will be subsequently heat treated, but usage is not limited to such applications. Certain design and processing procedures may cause these products to be susceptible to stress-corrosion cracking after heat treatment; SAE ARP 823 recommends practices to minimize such conditions.