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Standard

Identification Carbon and Low-Alloy Steels, Corrosion- and Heat-Resistant Steels and Alloys Sheet, Strip, Plate, and Aircraft Tubing

2024-05-17

CURRENT

AMS2807C

This specification covers procedures for identifying carbon and low-alloy steels, corrosion- and heat-resistant steels and alloys, maraging and other highly alloyed steels, and iron alloy sheet, strip, and plate, and aircraft tubing.

Standard

Nickel Alloy, Corrosion- and Heat-Resistant, Seamless Tubing, 72Ni - 15.5Cr - 0.95Cb (Nb) - 2.5Ti - 0.70Al - 7.0Fe (X750), Vacuum Melted, Solution Heat Treated, Precipitation Hardenable to 170 ksi (1172 MPa) Tensile Strength

2024-05-17

CURRENT

AMS5583G

This specification covers a precipitation hardenable corrosion- and heat-resistant nickel alloy in the form of seamless tubing.

Standard

Nickel Alloy, Corrosion- and Heat-Resistant, Welding Wire 57Ni - 19.5Cr - 13.5Co - 4.2Mo - 3.1Ti - 1.4Al - 0.006B Vacuum Induction Melted, Solution Heat Treated

2024-05-17

CURRENT

AMS5828H

This specification covers a corrosion- and heat-resistant nickel alloy in the form of welding wire.

Standard

Aluminum Alloy, Extrusions 6.2Zn - 2.3Cu - 2.2Mg - 0.12Zr (7050-T76511) Solution Heat Treated, Stress Relieved, Straightened, and Overaged

2024-05-17

CURRENT

AMS4340H

This specification covers an aluminum alloy in the form of extruded bars, rods, wire, profiles, and tubing up to 5.000 inches (127.00 mm), inclusive, in nominal diameter or least thickness (see 8.5).

Standard

Magnesium Alloy Welding Wire, 9.0Al - 2.0Zn (AZ92A)

2024-05-17

CURRENT

AMS4395G

This specification covers a magnesium alloy in the form of welding wire (see 8.5).

Standard

Steel, Corrosion-Resistant, Sheet, Strip, and Plate 17Cr - 7.1Ni - 1.1Al (Alloy 17-7) Solution Heat Treated, Precipitation Hardenable

2024-05-17

CURRENT

AMS5528K

This specification covers a corrosion-resistant steel in the form of sheet, strip, and plate 0.005 to 1.000 inches (0.13 to 25.40 mm) in nominal thickness in the solution heat-treated condition.

Standard

Aluminum Alloy, Plate (7140-T7651) 6.6Zn - 1.8Cu - 2.0Mg - 0.10Zr Solution Heat Treated, Stress Relieved, and Overaged

2024-05-17

CURRENT

AMS4408B

This specification covers an aluminum alloy in the form of plate 4.000 to 10.000 inches (101.6 to 254.0 mm), inclusive, in nominal thickness (see 8.5).

Standard

Vacuum Gauge Calibration

2024-05-17

CURRENT

ARP7446A

This SAE Aerospace Recommended Practice (ARP) addresses the general procedure for the best practices for minimizing uncertainty when calibrating thermal conductivity and cold cathode vacuum gauges, which includes the vacuum sensor(s) and accompanying electronics necessary for a pressure measurement to be made. It also includes the best practices for an in-process verification where limitations make it impossible to follow the best practices for minimizing uncertainty. Verifying the accuracy and operation of vacuum gauges is critical to ensure the maintenance of processes while under vacuum.

Standard

Laser Beam Machining

2024-05-16

WIP

B24AA

This specification covers the engineering requirements for laser beam machining such as cutting and drilling.

Standard

Sheet and Strip Surface Finish Nomenclature

2024-05-16

CURRENT

AS4194B

This SAE Aerospace Standard (AS) defines the nomenclature for surface finishes commonly used for sheet and strip in aerospace material specifications. It is applicable to steel and to iron, nickel, cobalt, and titanium base alloys.

Standard

Reaffirm E 2024 - spring

2024-05-13

WIP

REFIRM-E-S2024

The following document were been proposed by the sponsor or by committee E for Reaffirmation at the Spring meeting 2024.

Standard

Reaffirmation Ballot - F 2024 Spring

2024-05-13

WIP

REFIRM-F-S2024

The following document has been proposed by the sponsor or by committee F for Reaffirmation at the Spring meeting 2024.

Standard

Peening Media, Conditioned Carbon Steel Cut Wire Shot, Regular Hardness (45 to 52 HRC)

2024-05-13

WIP

AMS2431/3F

The complete requirements for procuring the product shall consist of this document and the latest issue of the basic specification, AMS2431.

Standard

Peening Media, Conditioned Stainless Steel Cut Wire Shot (AWS)

2024-05-13

WIP

AMS2431/4E

The complete requirements for procuring the product shall consist of this document and the latest issue of the basic specification, AMS2431.

Standard

Peening Media, Conditioned Carbon Steel Cut Wire Shot, High Hardness (55 to 62 HRC) (AWCH)

2024-05-13

WIP

AMS2431/8D

This specification, in conjunction with the general requirements for peening media covered in AMS2431, establishes the requirements for the procurement of conditioned carbon steel cut wire shot with a hardness of 55 to 62 HRC.

Standard

GAF24AF (GAE24AF) Tensile Test Strain Rate Implementation

2024-05-09

WIP

GAF24AF

Update of when to implement a specific strain rate into tensile testing.

Standard

Nickel Alloy, Corrosion- and Heat-Resistant Seamless Tubing, 72Ni - 15.5Cr - 0.95Cb (Nb) - 2.5Ti - 0.70Al - 7.0Fe (X750), Solution Heat Treated, Precipitation Hardenable

2024-05-09

CURRENT

AMS5582H

This specification covers a precipitation hardenable, corrosion- and heat-resistant nickel alloy in the form of seamless tubing 0.125 inch (3.18 mm) and over in nominal OD and 0.015 inch (0.38 mm) and over in nominal wall thickness.

Standard

Dendrite Arm Spacing of Structural Aircraft Quality D357 Aluminum Alloy Castings, Determination and Acceptance of

2024-05-09

CURRENT

ARP1947D

This document covers the recommended practice for determining the acceptability of the dendrite arm spacing (DAS) of D357-T6 aluminum alloy castings required to have tensile strength not lower than 50 ksi (345 MPa).

Standard

Nuts, Self-Locking, Steel, Corrosion and Heat Resistant High Strength, All Metal 1200 °F Use, UN Thread Form

2024-05-09

CURRENT

AS7250E

This document covers all metal, self-locking wrenching nuts, plate nuts, shank nuts, and gang channel nuts made from a corrosion and heat resistant steel of the type identified under the Unified Numbering System as UNS S66286 and of 160 ksi tensile strength at room temperature, with maximum test temperature of parts at 1200 °F.

Standard

Nuts, Self-Locking, UNS N07001 730 °C, 1100 MPa, and 1210 MPa Procurement Specification for, Metric

2024-05-09

CURRENT

MA1943C

This procurement specification covers aircraft quality self-locking nuts for wrenching (hex, spline) and anchor (plate, gang channel, shank) types of nuts made from a corrosion and heat-resistant nickel-base alloy of the type identified under the Unified Numbering System as UNS N07001. Tension height nuts having overall length of threaded portion not less than 1.2 times the nominal thread diameter have 1210 MPa minimum tensile strength at room temperature. Shear height nuts having shorter threaded portion have 1100 MPa minimum tensile strength at room temperature. Maximum test temperature of parts is 730 °C.