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Viewing 36781 to 36810 of 42864
1967-11-01
Standard
AMS5805B
This specification covers a corrosion and heat resistant steel in the form of welding wire.
1967-11-01
Standard
AMS5804B
This specification covers a corrosion and heat-resistant steel in the form of welding wire.
1967-11-01
Standard
AMS5031A
This specification covers a low-carbon steel in the form of covered welding electrodes.
1967-11-01
Standard
AMS4974
This specification covers a titanium alloy in the form of bars, wire, forgings, and forging stock.
1967-11-01
Standard
AMS3634
This specification covers an irradiated, thermally-stabilized, modified- polyolefin plastic in the form of dual-wall tubing. This tubing has been used typically as a semi-rigid, electrical insulation tubing whose diameter can be reduced to a predetermined size by heating to 135 degrees C (275 degrees F) or higher, but usage is not limited to such applications. Tubing is not flame-retardant and will burn slowly. This tubing is stable for continuous exposure from -55 to +110 degrees C (-67 to +230 degrees F).
1967-11-01
Standard
AMS3638B
This specification covers an irradiated, thermally-stabilized, flame-retardant, modified polyolefin plastic in the form of thin-wall tubing. This tubing has been used typically as a semi-rigid, electrical insulation tubing whose diameter can be reduced to a predetermined size by heating to a temperature higher than 120 degrees C (248 degrees F), but usage is not limited to such applications.
1967-11-01
Standard
AMS3639B
This specification covers an irradiated, thermally-stabilized, modified polyolefin plastic in the form of semi-rigid, thin-wall, heat-shinkable tubing. This tubing has been used typically as a semi-rigid, electrical insulation tubing whose diameter can be reduced to a predetermined size by heating to 120 degrees C (250 degrees F) or higher, but usage is not limited to such applications.
1967-11-01
Standard
AMS4114D
This specification covers an aluminum alloy in the form of bars and rods.
1967-11-01
Standard
AMS4112A
This specification has been declared 'CANCELLED' by the Aerospace Materials Division, SAE, as of January 1996. Alloy: 2024-T6 UNS Number: A92024
1967-11-01
Standard
AMS4102C
This specification covers an aluminum alloy in the form of bars, rods, and wire. Primarily for parts requiring good formability and weldability in fabrications where strength is unimportant.
1967-11-01
Standard
AMS4168B
This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing. These products have been used typically for parts subject to excessive warpage during machining and for parts requiring high strength and whose fabrication does not involve welding or forming, but usage is not limited to such applications. Certain design and processing procedures may cause these extrusions to become susceptible to stress-corrosion cracking; SAE ARP 823 recommends practices to minimize such conditions.
1967-11-01
Standard
AMS4003D
This specification covers an aluminum alloy in the form of sheet and plate 1 .000 inch (25.40 mm) and under in nominal thickness.
1967-11-01
Standard
AMS4001D
This specification covers aluminum in the form of sheet and plate.
1967-11-01
Standard
AMS4000D
This specification covers aluminum in the form of sheet and plate.
1967-11-01
Standard
AMS4028C
This specification covers an aluminum alloy in the form of sheet and plate.
1967-11-01
Standard
AMS4006D
This specification covers an aluminum alloy in the form of sheet and plate.
1967-11-01
Standard
AMS4014A
SUPERSEDING SPECIFICATION: The requirements of this specification are embodied in the latest issue of AMS 4029, ALUMINUM ALLOY SHEET AND PLATE (2014; -T6 Sheet, -T651 Plate). The requirements of the latest issue of AMS 4029 shall be fulfilled whenever reference is made to this specification.
1967-11-01
Standard
AMS4036B
This specification covers an aluminum alloy in the form of sheet and plate clad on one side with a different aluminum alloy.
1967-11-01
Standard
AMS4046B
This specification covers an aluminum alloy in the form of sheet and plate.
1967-11-01
Standard
AMS4062E
This specification covers an aluminum alloy in the form of drawn seamless round tubing.
1967-11-01
Standard
AMS4065D
This specification covers an aluminum alloy in the form of drawn seamless tubing.
1967-11-01
Standard
AMS4067D
This specification covers an aluminum alloy in the form of seamless drawn tubing.
1967-11-01
Standard
AMS4077A
This specification covers an aluminum alloy in the form of sheet and plate. This product has been used typically for structural components, including machine tapered parts, but usage is not limited to such applications.
1967-11-01
Standard
AMS4501
This specification covers one type of copper in the form of sheet, strip, and plate
1967-11-01
Standard
AMS4602
This specification covers one type of copper in the form of bars, rods, and shapes.
1967-11-01
Standard
ARP998
This ARP is intended to make recommendations for flight crew and cabin attendant restraint systems in aircraft. A properly designed crew restraint system will avoid injury or debilitation during a survivable crash and enable post crash assistance to occupants and escape from the aircraft. Consideration is given to existing requirements of the FAA and to the recommendations of aircraft operators and those involved in the manufacture or use of restraining devices. Crew member safety is the primary objective, with appropriate provisions for crew comfort taken into consideration. The criteria established herein are designed to standardize restraining systems without hindering the development of new, improved systems.
1967-11-01
Standard
ARP982
Primarily to provide recommendations concerning minimizing stress corrosion cracking in wrought titanium alloy products.
1967-11-01
Standard
AMS7851A
This specification covers a columbium alloy in the form of foil, sheet, strip, or plate. This material has been used typically for parts requiring exposure at ultra-high temperatures, but usage is not limited to such applications. Applications in oxidizing atmospheres necessitate a protective coating.
1967-11-01
Standard
J318_196711
This SAE Recommended Practice is intended to provide a design, critical dimensions, performance requirements, and identification for gladhand-type air line couplers used to connect the brake systems of trucks, truck-tractors, and trailers when these vehicles are joined to operate as a combination unit. The purpose is to provide a coupler half for the service (control) and emergency (supply) brake lines on one vehicle that will be identified and compatible with the coupler halves on the service (control) and emergency (supply) brake lines of another vehicle.
1967-11-01
Standard
J321_196711
This SAE Standard establishes a criteria for a minimum zone of protection for the operator of the machine and establishes certain structural requirements for guards on pneumatic-tired earthmoving haulage machines capable of speeds in excess of 25 km/h. Earthmoving machines covered by this document are dumpers and tractor-scrapers as identified in SAE J/ISO 6165.