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Viewing 36781 to 36810 of 37351
Standard
1945-05-01
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock. These products have been used typically for parts, 0.750 inch (19.05 mm) and under in section thickness at time of heat treatment, requiring a through-hardening steel capable of developing hardness as high as 50 HRC when properly hardened and tempered and also parts of greater thickness but requiring proportionately lower hardness, but usage is not limited to such applications.
Standard
1945-05-01
This specification establishes the requirements for chromate conversion coatings on magnesium alloys. This process has been used typically to improve corrosion resistance and adherence of organic finishes but usage is not limited to such applications. The dichromate treatment may not be suitable for alloys with high manganese content. The chrome pickle treatment has been used as touch-up for previously dichromate-treated surfaces and for improving corrosion protection temporarily, but usages are not limited to such applications.
Standard
1945-05-01
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
Standard
1945-05-01
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
Standard
1945-05-01
This specification covers an aluminum bronze alloy in the form of bars, rods, shapes, tubes, forgings, and forging stock.
Standard
1944-11-01
This specification provides requirements and procedures for air-pressure leak testing of parts.
Standard
1944-11-01
This specification provides requirements and procedures for air-pressure leak testing of parts.
Standard
1944-11-01
This specification covers a synthetic rubber and cork composition in the form of sheet, strip, and molded shapes.
Standard
1944-11-01
This specification covers silica gel dehydrating agent in the form of a granular powder in either plain or indicator grades. Indicator grades shall be impregnated with cobalt chloride.
Standard
1944-11-01
This specification has been "CANCELLED" by the Aerospace Materials Division, SAE, as of October 1996.
Standard
1944-11-01
This specification covers a carbon steel in the form of seamless tubing.
Standard
1944-11-01
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.
Standard
1944-11-01
This specification covers a chloroprene (CR) rubber sponge in the form of sheet, strip, molded shapes, or other forms, as ordered. These products have been used typically for general applications requiring the use of open-cell, soft rubber sponge pads and seals operating from -40 to +176 °F (-40 to +80 °C), but usage is not limited to such applications.
Standard
1944-11-01
This specification covers a corrosion-resistant steel in the form of welded tubing.
Standard
1944-11-01
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.
Standard
1944-11-01
This specification covers an aircraft-quality, low-alloy steel in the form of mechanical tubing.
Standard
1944-11-01
This specification covers an aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.
Standard
1944-11-01
This specification covers a zinc alloy in the form of die castings.
Standard
1944-11-01
This specification covers a nitrile (NBR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes.
Standard
1944-11-01
This specification has been 'CANCELLED' by the Aerospace Materials Division, SAE, as of September 1996. Alloy: 4032-T6 UNS Number: A94032
Standard
1944-11-01
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.
Standard
1944-11-01
This specification provides requirements and procedures for air-pressure leak testing of parts.
Standard
1944-11-01
This specification covers a low-carbon steel in the form of seamless tubing. This tubing has been used typically for oil lines and other parts requiring high-quality tubing suitable for severe forming and for welding or brazing, but usage is not limited to such applications.
Standard
1944-11-01
This specification covers a chloroprene (CR) rubber in the form of sheet, strip, tubing, extrusions, and molded shapes. These products have been used typically for parts, such as window channels, bumper pads, chafing strips, and seals, requiring resistance to weather and for use from -40 to +100 degrees C (-40 to +212 degrees F), but usage is not limited to such applications.
Standard
1944-11-01
This specification covers the engineering requirements for finishng aircraft parts and assemblies with an engine gray enamel.