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Viewing 43651 to 43680 of 44832
HISTORICAL
1945-08-01
Standard
AMS2223
This specification covers established inch/pound manufacturing tolerances applicable to copper and copper alloy seamless tubing ordered to inch/pound dimensions. These tolerances apply to all conditions, unless otherwise noted. The term "exclusive" is used to apply only to the higher figure of a specified range.
HISTORICAL
1945-08-01
Standard
AMS6415B
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
CURRENT
1945-07-15
Standard
AS167A
CURRENT
1945-07-13
Standard
AGS1764-4
No scope available.
CURRENT
1945-07-13
Standard
AGS1763-4
No scope available.
CURRENT
1945-07-13
Standard
AGS1762-4
No scope available.
CURRENT
1945-07-04
Standard
AS1162-2
No scope available.
CURRENT
1945-07-04
Standard
AS1163-2
No scope available.
HISTORICAL
1945-07-01
Standard
AMS2211
HISTORICAL
1945-07-01
Standard
AMS2212
HISTORICAL
1945-07-01
Standard
AMS6365A
This specification covers an aircraft-quality, low-alloy steel in the form of seamless tubing. This tubing has been used typically for thin wall-thickness sections where minimum tensile strength up to 160 ksi (1103 MPa) is required and where parts may be welded during fabrication, but usage is not limited to such applications.
HISTORICAL
1945-07-01
Standard
AMS6535B
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
1945-07-01
Standard
AMS6530B
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of February 1995.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.
HISTORICAL
1945-07-01
Standard
AMS6550B
Primarily for general use is light wall-thickness sections where minimum tensile strength up to 160,000 psi (1105 MPa) is required and parts may be welded during fabrication. This specification has been declared "Noncurrent" by the Aerospace Materials Division, SAE, as of April 19, 1988. It is recommended, therefore, that this specification not be specified for new designs.
CURRENT
1945-07-01
Standard
AMS6510A
HISTORICAL
1945-07-01
Standard
AMS6325B
This specification covers an aircraft-quality, low-alloy steel in the form of heat treated bars and forgings.
HISTORICAL
1945-07-01
Standard
AMS5045
This specification covers a carbon steel in the form of sheet and strip.
HISTORICAL
1945-07-01
Standard
AMS3228B
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of September 1996.
HISTORICAL
1945-07-01
Standard
AMS3226B
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).
HISTORICAL
1945-07-01
Standard
AMS3229B
This specification covers a nitrile (NBR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
HISTORICAL
1945-07-01
Standard
AMS4280B
This specification covers an aluminum alloy in the form of permanent mold castings.
HISTORICAL
1945-07-01
Standard
AMS4290B
This specification covers an aluminum alloy in the form of die castings.
HISTORICAL
1945-07-01
Standard
AMS4281
This specification covers an aluminum alloy in the form of permanent mold castings.
1945-07-01
Standard
AMS4282B
1. ACKNOWLEDGMENT: A vendor must mention this specification number in all quotations and when acknowledging purchase orders. 2. COMPOSITION: Copper 4.0 - 5.0 Silioon 2.0 - 3.0 Iron 1.2 max Manganese 0.3 max Zinc 0.2 max Titanium 0.2 max Magnesium 0.05 max Other Impurities, each 0.05 max Other Impurities, total 0.15 max Aluminum remainder
HISTORICAL
1945-07-01
Standard
AMS4507
This specification covers a copper-zinc alloy (brass) in the form of sheet, strip, and plate.
HISTORICAL
1945-07-01
Standard
AMS4713
This specification covers one type of brass in the form of wire. This brass wire has been used typically for cold-headed parts such as pins and rivets, but usage is not limited to such applications.
HISTORICAL
1945-07-01
Standard
AMS2203
This specification has been declared "SUPERSEDED" by the Aerospace Materials Division, SAE, as of September 1994. The requirements of this specification are embodied in the latest issue of ANSI H35.2, Dimensional Tolerances for Aluminum Mill Products.
HISTORICAL
1945-07-01
Standard
AMS2232
This specification covers established inch/pound manufacturing tolerances applicable to carbon steel sheet, strip, and plate ordered to inch/pound dimensions. These tolerances apply to all conditions unless otherwise noted. The term 'excl' is used to apply only to the higher figure of the specified range. Tolerances for products sizes not listed herein shall be as agreed upon by purchaser and vendor.