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2015-07-21
WIP Standard
J2654
Hardness measurements are used as a quality control check of the consistency of formulation and processing of brake linings. This hardness method is nondestructive. NOTE-This method is not a measure of friction level. The hardness and the range of hardness are characteristic of each formulation; therefore, the acceptable values and ranges must be established for each formulation and may be affected by processing. NOTE-The hardness of sintered powder metal lining is usually determined with Rockwell superficial hardness equipment. (See ASTM B 347)
2015-07-21
WIP Standard
J2724
This procedure describes a method for measuring the fraction of underlayer (also referred to as backing layer) existing at any given height above the a disc brake friction materials shoe plate. Measuring underlayer distribution is useful for computing useable lining thickness and for friction material quality management.
2015-07-20
WIP Standard
AS4108/1A
SCOPE IS UNAVAILABLE.
2015-07-20
WIP Standard
J1704
This SAE Standard covers motor vehicle brake fluids of the nonpetroleum type, based upon glycols, glycol ethers, and borates of glycolethers, and appropriate inhibitors, for use in the braking system of any motor vehicle such as a passenger car, truck, bus, or trailer. These fluids are not intended for use under arctic conditions. These fluids are designed for use in braking systems fitted with rubber cups and seals made from styrene-butadiene rubber (SBR), or a terpolymer of ethylene, propylene, and a diene (EPDM).
2015-07-20
WIP Standard
AS4108/3A
SCOPE IS UNAVAILABLE.
2015-07-20
WIP Standard
AS4108/2A
SCOPE IS UNAVAILABLE.
2015-07-20
WIP Standard
J1703
This SAE Standard covers motor vehicle brake fluids of the nonpetroleum type, based upon glycols, glycolethers and appropriate inhibitors, for use in the braking system of any motor vehicle such as a passenger car, truck, bus, or trailer. These fluids are not intended for use under arctic conditions. These fluids are designed for use in braking systems fitted with rubber cups and seals made from styrene-butadiene rubber (SBR), or a terpolymer of ethylene, propylene, and a diene (EPDM).
2015-07-20
Standard
MA3393A
SCOPE IS UNAVAILABLE.
2015-07-20
Standard
MA3428A
SCOPE IS UNAVAILABLE.
2015-07-20
Standard
MA3394A
SCOPE IS UNAVAILABLE.
2015-07-17
Standard
AIR6441
This SAE Aerospace Information Report (AIR) provides information on the parking brake system design for a variety of aircraft including part 23, 25, 27, and 29. The document includes a discussion of key technical issues with parking brakes. This document does NOT provide recommended practices for parking brake system design.
2015-07-17
Standard
ARP5526D
This SAE Aerospace Recommended Practice (ARP) documents a common understanding of terms, compliance issues and design criteria to facilitate certification of seat installations specific to Part 25 aircraft. This ARP provides general guidance for seats to be installed in Part 23 aircraft and Parts 27 and 29 rotorcraft and does not specify specific designs or design methods for such certification.
2015-07-17
Standard
AS1284B
The test procedure and related limit value are intended to apply to fixed and mobile ground pressure fuel dispensing sytems and to aerial refueling tankers.
2015-07-17
Standard
AS50151C
This specification covers circular threaded electrical connectors with solder or removable crimp contacts (both front and rear release). These connectors are for use in electronic, electrical power, and control circuits (see 6.1).
2015-07-17
WIP Standard
AMS2430U
This specification covers the requirements for automatic shot peening of surfaces of parts by impingement of media, including metallic, glass, or ceramic shot.
2015-07-16
Standard
AMS5580L
This specification covers a corrosion and heat-resistant nickel alloy in the form of seamless tubing.
2015-07-16
Standard
AMS6901B
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) inclusive, in nominal diameter or least distance between parallel sides, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size.
2015-07-16
Standard
AMS6921B
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) in nominal diameter or least distance between parallel sides, inclusive, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (See 8.6).
2015-07-16
Standard
AMS6920C
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) in nominal diameter or least distance between parallel sides, inclusive, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (See 8.6).
2015-07-16
Standard
AMS6925B
This specification covers a titanium alloy in the form of bars up through 7.000 inches (177.80 mm) inclusive, in nominal diameter or least distance between parallel sides, forgings of thickness up through 7.000 inches (177.80 mm), inclusive, and stock for forging of any size.
2015-07-16
Standard
AMS6926B
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) inclusive, in nominal diameter or least distance between parallel sides, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, and stock for forging of any size (See 8.6).
2015-07-16
Standard
AMS6936B
This specification covers a titanium alloy in the form of bars up through 4.000 inches (101.60 mm) in nominal diameter or least distance between parallel sides, inclusive, forgings of thickness up through 4.000 inches (101.60 mm), inclusive, with bars and forgings having a maximum cross-sectional area of 32 square inches (204.5 cm2), and stock for forging of any size (See 8.6).
2015-07-15
WIP Standard
AMSQQA225/5A
This specification covers the specific requirements for 2017 aluminum alloy bar, rod and wire produced by rolling, drawing or cold finishing.
2015-07-15
WIP Standard
AMSQQA225/2B
This specification covers the specific requirements for 3003 aluminum alloy bar, rod, and wire produced by rolling, drawing, or cold finishing.
2015-07-15
WIP Standard
AMSQQA225/4A
This specification covers the specific requirements for 2014 aluminum alloy bar, rod, wire and special shapes produced by rolling, drawing or cold finishing.
2015-07-15
Standard
J1351_201507
This test applies to various materials used for insulation and other applications.
2015-07-15
Standard
J182_201507
This SAE Recommended Practice describes a procedure for locating the three-dimensional reference system on a motor vehicle as built.
2015-07-13
Standard
AMS4333D
This specification covers an aluminum alloy in the form of die forgings 4.000 inches (102 mm) and under in nominal thickness and of forging stock of any size.
2015-07-13
Standard
AMS6947A
This specification covers a titanium alloy in the form of bars, wire, forgings, flash welded rings, drawn shapes 4.000 inches (101.60 mm) and under, and stock for forging, heading, or flash welded rings of any size.
2015-07-13
Standard
ARP1796B
This SAE Aerospace Recommended Practice (ARP) discusses design philosophy, system and equipment requirements, installation environment and design considerations for military and commercial aircraft systems within the Air Transport Association (ATA) ATA 100 specification, Chapter 36, Pneumatic. This ATA system/chapter covers equipment used to deliver compressed air from a power source to connecting points for other systems such as air conditioning, pressurization, ice protection, cross-engine starting, air turbine motors, air driven hydraulic pumps, on board oxygen generating systems (OBOGS), on board inert gas generating systems (OBIGGS), and other pneumatic demands.
Viewing 31 to 60 of 38414