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2014-12-06
WIP Standard
AS9589A
No scope available.
2014-12-06
WIP Standard
AS9806A
No scope available.
2014-12-06
WIP Standard
AS9788A
No scope available.
2014-12-06
WIP Standard
AS7456C
This procurement specification covers aircraft quality studs made from a low alloy steel of the type identified under the Unified Numbering System as UNS G87400, and of a series of room temperature tensile strengths ranging from 125 000 psi to 185 000 psi. Primarily for aerospace propulsion system applications in light alloys where good strength is required and the part is protected against corrosion.
2014-12-06
WIP Standard
AS7458B
This procurement specification covers aircraft quality studs made from a low alloy, heat resistant steel of the type identified under the Unified Numbering System as UNS K14675.

AS 7458 135 000 psi ultimate tensile strength at room temperature

AS 7458-1 135 000 psi ultimate tensile strength at room temperature, nickel-cadium plated.>Primarily for aerospace propulsion system applications where good strength temperatures up to approximately 900 °F is required and the part is protected against corrosion.

2014-12-06
WIP Standard
AS7455B
This procurement specification covers aircraft quality bolts and screws made from a low alloy, heat resistant steel of the type identified under the Unified Numbering System as UNS K14675. The following specification designations and their properities are covered: AS7455 ~ 140 000 to 195 000 psi ultimate tensile strength at room temperture; AS7455-1 ~ 140 000 to 195 000 psi ultimate tensile strength at room temperature, nickel-cadmium plated.

Primarily for aerospace propulsion system applications where high strength at temperatures up to approximately 900 °F is required and the part is protected against corrosion.

2014-12-06
WIP Standard
AS7228A
This procurement specification covers aircraft quality solid rivets and tubular end rivets made from a corrosion resistant steel of the type identified under the Unified Numbering System as UNS S30200.

Primarily for joining corrosion resistant steel parts requiring corrosion, heat, and oxidation resistance up to approximately 800 degrees F but not requiring high shear strength.

2014-12-05
Standard
MA3384A
SCOPE IS UNAVAILABLE.
2014-12-05
WIP Standard
AS3397A
No scope available.
2014-12-05
WIP Standard
AS4723A
This procurement specification covers inserts made from A286 alloy of the type identified under the Unified Numbering System as UNS S66286, solid film lubricated with a plastic self locking device, integrated locking keys to positively secure the insert against rotation when properly installed in threaded holes.
2014-12-05
Standard
AS3307A
SCOPE IS UNAVAILABLE.
2014-12-05
Standard
MA3385A
SCOPE IS UNAVAILABLE.
2014-12-05
Standard
MA3383A
SCOPE IS UNAVAILABLE.
2014-12-05
Standard
MA3387A
SCOPE IS UNAVAILABLE.
2014-12-05
Standard
MA3386A
SCOPE IS UNAVAILABLE.
2014-12-05
Standard
MA3389A
SCOPE IS UNAVAILABLE.
2014-12-05
Standard
MA3392A
SCOPE IS UNAVAILABLE.
2014-12-05
Standard
AS5230C
SCOPE IS UNAVAILABLE.
2014-12-05
WIP Standard
AS20253B
Scope is unavailable.
2014-12-03
WIP Standard
J1453/3
The three parts of SAE J1453 cover material, dimensional, and performance requirements of steel O-ring face seal (ORFS) connectors for tubing and the O-ring face seal interface and nut portion of hose stem assemblies for nominal tube diameters of 6 mm through 50 mm. SAE J1453-3 covers the requirements for O-ring face seal connectors to inch stud ends along with the associated adapters, bulkhead and union connectors. Inch hex dimensions of parts will be moved from the main document to an informative annex after 2013.
2014-11-26
Standard
J1605_201411
This SAE Standard covers performance requirements and methods of test for master cylinder reservoir diaphragm gaskets that will provide a functional seal and protection from outside dirt and water.
2014-11-25
WIP Standard
AIR5464A
Over the past decade several metal clad fibers and fabrics have been developed to provide aerospace vehicle designers with a conductive, lighter weight alternative to coated copper or steel for shielding and harness overbraids of electrical cables. Several of these candidates have been unable to provide the strength or thermal stability necessary for the aerospace environment. However, the aramid-based products have shown remarkable resistance to the rigorous environment of aerospace vehicles. Concurrent with these fiber developments, there have been changes in the structures of aerospace vehicles involving greater use of nonmetallic outer surfaces. This has resulted in a need for increased shielding of electrical cables which adds substantial weight to the vehicle. Thus, a lighter weight shielding material has become more critical to meet the performance requirements of the vehicle.
2014-11-25
Standard
AS3308A
Scope is unavailable.
Viewing 271 to 300 of 15611

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