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Viewing 151 to 180 of 20733
2017-11-13
WIP Standard
AS1895/7F
SCOPE IS UNAVAILABLE.
2017-11-10
WIP Standard
AMS6567/1
AMS6567 The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is designed specifically for vacuum-bag-only cure, with an initial low temperature cure followed by a higher temperature post-cure. This material is intended for use in laminate applications with a service temperature up to 250 °F. They are typically used in structural applications requiring high strength and stiffness.
2017-11-10
WIP Standard
AMS6567/2
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is designed specifically for vacuum-bag-only cure, with an initial low temperature cure followed by a higher temperature post-cure. This material is intended for use in laminate applications with a service temperature up to 250 °F. They are typically used in structural applications requiring high strength and stiffness.
2017-11-10
WIP Standard
AMS6569/1
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. These materials are designed specifically for vacuum bag autoclave cure. These materials are intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness.
2017-11-10
WIP Standard
AMS6569/2
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. These materials are designed specifically for vacuum bag autoclave cure. These materials are intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness.
2017-11-10
WIP Standard
AMS6568/3
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness.
2017-11-10
WIP Standard
AMS6568/2
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness.
2017-11-10
WIP Standard
AMS6568/1
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness. This is the base specification and it will have three slash/detail specs.
2017-11-10
WIP Standard
AMS6566/1
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness. This is the base specification and it will have one slash/detail specs.
CURRENT
2017-11-09
Standard
AS81582C
This specification covers environment-resisting, quick disconnect, EMI/RFI shielded and non-shielded umbilical, electric connectors and adapter assemblies with removable crimp or nonremovable solder-type contacts and accessories. Connectors are rated for operation from -55 °C (-67 °F) to 200 °C (392 °F). Adapter assemblies are rated for operation from -55 °C (-67 °F) to 125 °C (257 °F). The upper temperature is the maximum internal hot spot temperature resulting from any combination of electrical load and ambient temperature.
2017-11-09
WIP Standard
AMS6562/2
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 250 °F. The composite may be used for the manufacture of primary and secondary aircraft structure. This is the second detail spec.
2017-11-09
WIP Standard
AMS6562/1
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 250 °F. The composite may be used for the manufacture of primary and secondary aircraft structure. This is the first slash/detail spec.
2017-11-09
WIP Standard
AMS6562/3
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 250 °F. The composite may be used for the manufacture of primary and secondary aircraft structure. This is the third detail spec.
CURRENT
2017-11-09
Standard
AMS5442B
This specification covers a corrosion and heat-resistant nickel alloy in the form of bars, forgings, and flash welded rings up to 5.0 inches (127mm) in least nominal cross-sectional dimension having a cross-sectional area not greater than 50 in2 (323 cm2), and stock of any size for forging or flash welded rings (see 8.5).
CURRENT
2017-11-09
Standard
AMS2451/12A
This specification covers the engineering requirements and process for brush plating of tin by electrodeposition. It shall be used, in conjunction with AMS2451, for general purpose tin deposits.
CURRENT
2017-11-09
Standard
AMS2451/13A
This specification covers the engineering requirements and process for brush plating of silver by electrodeposition. It shall be used, in conjunction with AMS2451, for silver deposits.
CURRENT
2017-11-09
Standard
AMS5596M
This specification covers a corrosion and heat-resistant nickel alloy in the form of sheet, strip, foil, and plate 1.00 inch (25.4 mm) and under in thickness (see 8.5).
CURRENT
2017-11-08
Standard
AMS4403A
This specification covers an aluminum alloy in the form of die forgings 1.000 to 12.000 inches inclusive (25 to 305 mm) in nominal thickness at the time of heat treatment and of forging stock (see 8.4).
2017-11-08
WIP Standard
AMS6569
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. These materials are designed specifically for vacuum bag autoclave cure. These materials are intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness. This is the base specification and it will have two slash/detail specs.
2017-11-08
WIP Standard
AMS6567
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is designed specifically for vacuum-bag-only cure, with an initial low temperature cure followed by a higher temperature post-cure. This material is intended for use in laminate applications with a service temperature up to 250 °F. They are typically used in structural applications requiring high strength and stiffness. This is the base specification and it will have two slash/detail specs.
2017-11-08
WIP Standard
AMS6565
Establish a new AMS for dry carbon fabric for Hexcel SGP196P IM7 plain weave fabric.
2017-11-08
WIP Standard
AMS6562
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 250 °F. The composite may be used for the manufacture of primary and secondary aircraft structure. This is the basic spec and it will have three slash/detail specs.
2017-11-08
WIP Standard
AMS6568
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness. This is the base specification and it will have three slash/detail specs.
2017-11-08
WIP Standard
AMS6566
The purpose of this specification is to allow procurement of a defined material corresponding to statistically derived material properties published in CMH-17. This material is intended for use in laminate applications with a service temperature up to 180 °F. They are typically used in structural applications requiring high strength and stiffness. This is the base specification and it will have one slash/detail specs.
2017-11-08
WIP Standard
AS7471H
This procurement specification covers bolts and screws made from a corrosion and heat resistant, age hardenable nickel base alloy of the type identified under the Unified Numbering System as UNS N07001. The following specification designations and their properties are covered:
AS7471 165 ksi minimum ultimate tensile strength at room temperature. 75 ksi stress-rupture strength at 1350 °F.
AS7471-1 165 ksi minimum ultimate tensile strength at room temperature. 99 ksi minimum ultimate shear strength at room temperature.

CURRENT
2017-11-08
Standard
AS85485B
This specification covers the requirements for radio frequency absorptive component wires and finished cables which function electrically as distributed low-pass filters. Materials and construction details are specified in the detail specification.
CURRENT
2017-11-08
Standard
AMS6516B
This specification covers a premium aircraft quality alloy steel in the form of bars and forgings 189 in2 (1219 cm2) and under in cross-sectional area and forging stock of any size.
CURRENT
2017-11-08
Standard
AMS2434E
This specification covers the requirements for electrodeposited tin-zinc alloy plating.
Viewing 151 to 180 of 20733