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Viewing 7261 to 7279 of 7279
HISTORICAL
1944-08-01
Standard
AMS2640A
This specification has been declared 'CANCELLED' by the Aerospace Materials Division SAE, as of April 1996. and has been superseded ASTM E 1444.
HISTORICAL
1944-05-01
Standard
AS84A
This SAE Aerospace Standard (AS) defines an involute with a 30? pressure angle and a full radius at the roots thus reducing the stress concentration in the area of the root.
HISTORICAL
1943-11-01
Standard
ARP159
HISTORICAL
1943-11-01
Standard
ARP85A
This specification is written to cover heating and ventilating equipment under four main classifications, namely; A. HEATING AND VENTILATING EQUIPMENT - GENERAL - Dealing with features applicable to all makes and uses. B. HEATING AND VENTILATING EQUIPMENT - MILITARY - Dealing with features applicable only to military aircraft. C. HEATING AND VENTILATING EQUIPMENT - COMMERCIAL - Dealing with features applicable only to commercial aircraft. D. DESIRABLE DESIGN FEATURES - General information for use of those concerned in meeting requirements contained herein.
HISTORICAL
1943-10-01
Standard
AMS5032
This specification covers a low-carbon steel in the form of wire supplied as coils of wire or, when specified, as straight lengths.
HISTORICAL
1943-03-01
Standard
AS130
HISTORICAL
1943-01-01
Standard
ARP85
HISTORICAL
1942-12-01
Standard
AMS6352A
This specification covers an aircraft quality, low alloy steel in the form of sheet, strip, and plate. These products have been used typically for heat treated parts and structures that may require welding during fabrication, but usage is not limited to such applications. It may be through-hardened to a minimum tensile strength of 180 ksi (1241 MPa) in sections 0.125 inch (3.18 mm) and under in nominal thickness and proportionately lower strength in heavier section thicknesses.
HISTORICAL
1942-06-01
Standard
AMS6362
This specification covers an aircraft-quality, low-alloy steel in the form of round, seamless tubing having a wall thickness not greater than 0.188 inch (4.78 mm). This tubing has been used typically for general use where a minimum tensile strength of 150 ksi (1034 MPa) is required, but usage is not limited to such applications.
HISTORICAL
1942-03-01
Standard
AS84
This SAE Aerospace Standard (AS) defines an involute with a 30? pressure angle and a full radius at the roots thus reducing the stress concentration in the area of the root.
HISTORICAL
1942-01-01
Standard
AMS2601A
This specification provides requirements and procedures for gas-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
AMS2605
This specification provides requirements and procedures for air-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
AMS2606A
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1940-06-13
Standard
AMS2640
This specification has been declared 'CANCELLED' by the Aerospace Materials Division SAE, as of April 1996. and has been superseded ASTM E 1444.
HISTORICAL
1940-06-01
Standard
AMS2601
This specification provides requirements and procedures for gas-pressure leak testing of parts.
HISTORICAL
1940-06-01
Standard
AMS2606
This specification provides requirements and procedures for air-pressure leak testing of parts.
HISTORICAL
1939-12-04
Standard
AMS6352
This specification covers an aircraft quality, low alloy steel in the form of sheet, strip, and plate. These products have been used typically for heat treated parts and structures that may require welding during fabrication, but usage is not limited to such applications. It may be through-hardened to a minimum tensile strength of 180 ksi (1241 MPa) in sections 0.125 inch (3.18 mm) and under in nominal thickness and proportionately lower strength in heavier section thicknesses.
Viewing 7261 to 7279 of 7279