Standards - SAE Mobilus

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Items (50,804)

FITTING ASSEMBLY, 45° ELBOW, EXTERNAL SWAGE TO FEMALE FLARELESS, HYDRAULIC

AS6468A (Current)

9/11/2026

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

FITTING ASSEMBLY, TEE, FEMALE FLARELESS TO EXTERNAL SWAGE ON RUN, EXTERNAL SWAGE ON BRANCH, HYDRAULIC

AS6471A (Current)

9/11/2026

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

FITTING ASSEMBLY, 90° ELBOW, EXTERNAL SWAGE TO FEMALE FLARELESS, HYDRAULIC

AS6475A (Current)

9/11/2026

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

FITTING ASSEMBLY, TEE, EXTERNAL SWAGE ON RUN, FEMALE FLARELESS ON BRANCH, HYDRAULIC

AS6489A (Current)

9/11/2026

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

Oxygen Considerations for High Elevation Airport Operations (HEAO)

AIR6829A (Current)

9/11/2026

This document covers information concerning the use of oxygen when flying into and out of high elevation airports for both pressurized and non-pressurized aircraft. Oxygen requirements for pressurized aircraft operating at high altitudes have for decades emphasized the potential failures that could lead to a loss of cabin pressurization coupled with the potential severe hypoxic hazard that decompressions represent. This document is intended to address the case where the relationship between cabin and ambient pressures are complicated by operations at high terrestrial altitudes. Operators who fly into these high-altitude airports should address the issues related to this environment because it carries the potential for insidious hypoxia and other conditions which can affect safety. It provides information to consider in developing operational procedures to address hypoxia concerns consistent with regulatory mandates. In some sections, procedures are discussed that may mitigate the deleterious effects of hypoxia in a non-flight regime yet still have the potential to represent risk factors associated with flight operations. All the information is provided as a framework for potential oxygen management and other procedures to facilitate responsible practices and facilitate compliance with existing regulatory requirements. This document cannot address every type of aircraft pressurization system, oxygen system, or operational condition the flight may encounter. Any threat or hazard not discussed in AIR6829 should be brought to the attention of the OEM, the regulatory authority, and the flight operations department for proper guidance.

A-10 Aircraft Oxygen Equipment Committee

FITTING, TEE, MALE FLARELESS TO EXTERNAL SWAGE ON RUN, FEMALE FLARELESS ON BRANCH, HYDRAULIC

AS8575A (Current)

9/11/2026

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

Preconditioned Air (PCA) Unit Air Quality, Humidity Management, and Cabin Connection

ARP6986 (Current)

9/11/2026

The provisions of this SAE Aerospace Recommended Practice (ARP) cover minimum performance requirements and design parameters for preconditioned air (PCA) devices supplying air to the aircraft cabin. It identifies the need for interim and future performance improvement for ground equipment delivery systems, to meet industry requirements for reducing airborne compounds or particulates (“source types”) in the aircraft cabin and flight deck. This ARP will guide SAE, IATA, airline operators, and airframe and PCA manufacturers to meet new requirements. This ARP defines: Minimum performance and maintenance requirements for filtration, hose assemblies, operations, and maintenance. Level of humidity supplied by the ground equipment to the aircraft cabin. Minimum performance and maintenance requirements for digital communication of cabin parameters between the cabin and the PCA. Installation of the sensor unit within the aircraft cabin. The data collected by these sensors is not intended to assess impacts on aircraft occupant health and shall not be used to make a finding of airworthiness.

AGE-3 Aircraft Ground Support Equipment Committee

Definition of Pressure Surge Test and Measurement Methods for Receiver Aircraft

ARP1665B (Current)

9/11/2026

The test procedure applies to the refueling manifold system connecting the receiver aircraft fuel tanks to the refueling source fuel pump(s) for both ground and aerial refueling. The test procedure is intended to verify that the limit value for surge pressure specified for the receiver fuel system is not exceeded when refueling from a refueling source which meets the requirements of AS1284 (reference 2). This recommended practice is not directly applicable to surge pressure developed during operation of an aircraft fuel system, such as initiating or stopping engine fuel feed or fuel transfer within an aircraft, or the pressure surge produced when the fuel pumps are first started to fill an empty fuel manifold.

AE-5A Aerospace Fuel, Inerting and Lubrication Sys Committee

Steel, Bars, Forgings, Mechanical Tubing, and Forging Stock, 1.45Cr (0.93 - 1.05C) (SAE 52100), Aircraft Quality For Bearing Applications

AMS6440U (Current)

9/10/2026

This specification covers a low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.

AMS E Carbon and Low Alloy Steels Committee

Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing, Part 1 - General Requirements

AMS3970/1B (Current)

9/10/2026

AMS3970/1 gives information about the technical requirements and qualification procedure for carbon fiber fabric epoxy prepreg and a companion non-structural glass prepreg used for repair of carbon fiber reinforced epoxy structures. The prepreg system may include a film adhesive to be applied in a co-curing process with the prepreg for joint and sandwich bonding. The need for a film adhesive shall be established during screening tests.

AMS CACRC Commercial Aircraft Composite Repair Committee

Steel, Corrosion- and Heat-Resistant, Bars, Wire, Forgings, Mechanical Tubing, Rings, and Forging Stock, 18Cr - 10Ni - 0.40Ti (SAE 321), Solution Heat Treated

AMS5645U (Current)

9/10/2026

This specification covers a corrosion- and heat-resistant steel in the form of forgings, wire, bars, mechanical tubing, flash-welded rings, and stock of any size for forging or flash-welded rings.

AMS F Corrosion and Heat Resistant Alloys Committee

Heat Treatment, Martensitic Corrosion-Resistant Steel Parts

AMS2759/5G (Current)

9/10/2026

This specification, in conjunction with the general requirements for steel heat treatment covered in AMS2759, establishes the requirements for heat treatment of martensitic corrosion-resistant steel parts. Parts are defined in AMS2759. General ordering instructions are specified in AMS2759.

AMS F Corrosion and Heat Resistant Alloys Committee

Steel, Corrosion-Resistant, Bars, Wire, Forging, and Forging Stock, 13Cr (0.30-0.40C) (420), Annealed

AMS5621J (Current)

9/10/2026

This specification covers a corrosion-resistant steel in the form of bars, wire, forgings, and forging stock.

AMS F Corrosion and Heat Resistant Alloys Committee

Titanium Alloy Bars and Forging Stock, 8Al - 1Mo - 1V, Duplex Annealed

AMS6910E (Current)

9/10/2026

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, and stock for forging of any size (see 8.7).

AMS G Titanium and Refractory Metals Committee

Steel, Corrosion-Resistant, Investment Castings, 15Cr - 4.6Ni - 0.22Cb - 2.8Cu (15–5 PH®), Solution and Precipitation Heat Treated (H935), 170 ksi (1172 MPa) Tensile Strength

AMS5400E (Current)

9/10/2026

This specification covers a corrosion-resistant steel in the form of investment castings solution and precipitation heat treated to 170 ksi (1172 MPa) tensile strength.

AMS F Corrosion and Heat Resistant Alloys Committee

Titanium Alloy, Bars, Wire, Forgings, and Rings, 6Al - 6V - 2Sn, Annealed, Heat Treatable

AMS4971N (Current)

9/10/2026

This specification covers a titanium alloy in the form of bars, wire, forgings, and flash-welded rings 4.000 inches (101.60 mm) and under in diameter or least distance between parallel sides and stock for forging or flash-welded rings of any size (see 8.6).

AMS G Titanium and Refractory Metals Committee

Nickel Alloy, Corrosion- and Heat-Resistant, Investment Castings, 61Ni - 16Cr - 8.5Co - 1.8Mo - 2.6W - 0.85Cb, (Nb) - 3.4Ti - 1.8Ta - 3.4Al - 0.010B - 0.05Zr (738), Vacuum Melted, Vacuum Cast, As Cast, or Solution Treated, or Solution and Precipitation Hardened

AMS5410D (Current)

9/10/2026

This specification covers a corrosion- and heat-resistant vacuum melted nickel alloy in the form of investment castings.

AMS F Corrosion and Heat Resistant Alloys Committee

Steel Bars, Forgings, Mechanical Tubing and Forging Stock 1.75Cr - 4.0Ni - 0.5Mo - (0.35 - 0.40C) Premium Aircraft Quality Consumable Electrode Vacuum Remelted

AMS6551B (Current)

9/10/2026

This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.

AMS E Carbon and Low Alloy Steels Committee

Steel Bars, Forgings, Mechanical Tubing and Forging Stock, 1.0Cr - 3.2Ni - 0.2Mo (0.12 - 0.17C) (ISO 14NiCrMo1304), Premium Aircraft-Quality, Double Vacuum Melted

AMS6549B (Current)

9/10/2026

This specification covers a premium aircraft-quality, low-alloy steel in the form of bars, forgings, mechanical tubing, and forging stock.

AMS E Carbon and Low Alloy Steels Committee

Cobalt Alloy, Corrosion- and Heat-Resistant, Investment Castings, 60Co - 29Cr - 4.5W (Stellite® 6), As Cast

AMS5387G (Current)

9/10/2026

This specification covers a corrosion- and heat-resistant cobalt alloy in the form of investment castings.

AMS F Corrosion and Heat Resistant Alloys Committee

Manganese Bronze, Sand and Centrifugal Castings, 58Cu - 39Zn - 1.2Fe - 1.0Al - 0.80Mn, As Cast

AMS4860G (Current)

9/10/2026

This specification covers a manganese bronze alloy in the form of sand and centrifugal castings (see 8.5).

AMS D Nonferrous Alloys Committee

Leaded Red Brass, Sand and Centrifugal Castings, 85Cu - 5.0Sn - 5.0Pb - 5.0Zn, As Cast

AMS4855H (Current)

9/10/2026

This specification covers a leaded red brass alloy in the form of sand and centrifugal castings (see 8.5).

AMS D Nonferrous Alloys Committee

Steel, Corrosion- and Heat-Resistant, Bars, Wire, Forgings, Forging and Ring Stock, Mechanical Tubing, and Rings, 12Cr (410 MOD), Ferrite Controlled, Annealed, Consumable Electrode Melted

AMS5611H (Current)

9/10/2026

This specification covers a premium aircraft-quality, corrosion- and heat-resistant steel in the form of bars, wire, forgings, mechanical tubing, flash-welded rings, and stock for forging or flash-welded rings.

AMS F Corrosion and Heat Resistant Alloys Committee

Aluminum Alloy, Sheet and Plate, 4.4Cu - 1.5Mg - 0.60Mn (2024; -T3 Flat Sheet, -T351 Plate), Solution Heat Treated

AMS4037S (Current)

9/10/2026

This specification covers an aluminum alloy in the form of sheet and plate from 0.008 to 4.000 inches (0.20 to 101.60 mm) in thickness, inclusive (see 8.5).

AMS D Nonferrous Alloys Committee

BEARING, BALL, AIRFRAME, ANTIFRICTION, HEAVY DUTY

AS27640F (Current)

9/9/2026

ACBG Rolling Element Bearing Committee

CRIMPING TOOL AND ACCESSORIES, HAND OPERATED, DIE TYPE, WIRE SIZES 8 TO 0000 UN-INSULATED AND INSULATED CRIMP BARRELS

AS5259/3C (Current)

9/9/2026

AE-8C2 Terminating Devices and Tooling Committee

FITTING, TEE, SWIVEL NUT TO MALE FLARELESS ON RUN, EXTERNAL SWAGE ON SIDE

AS6494A (Current)

9/9/2026

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

Rolling Element Bearing No-Load Torque Test

ARP5483/1B (Current)

9/9/2026

This test method outlines the recommended procedure for performing the no-load rotational starting torque test on airframe rolling bearings. Bearings covered by this test method shall be antifriction ball bearings and spherical roller bearings.

ACBG Rolling Element Bearing Committee

Method of Testing Resistance to Scuffing of Trim Materials

J365_202609 (Current)

9/9/2026

This test can be used to determine the resistance to scuffing of test specimens such as fiberboards, fabrics, vinyl-coated fabrics, leathers, and similar trim materials.

Textile and Flexible Plastics Committee

Compound, Corrosion-Preventive, Thin Film, Fingerprint Removing

AMS3065J (Current)

9/9/2026

This specification covers corrosion-preventive organic substances dissolved or emulsified in a volatile solvent and supplied in the form of a ready-to-use liquid.

AMS B Finishes Processes and Fluids Committee

Titanium Alloy, Investment Castings 6Al - 4V, 130 UTS, 120 YS,6% EL, Hot Isostatically Pressed, Anneal Optional or When Specified

AMS4985F (Current)

9/9/2026

This specification covers a titanium alloy in the form of investment castings (see 8.6).

AMS G Titanium and Refractory Metals Committee

Copper-Nickel-Tin Alloy, Bars and Rods, 77Cu - 15Ni - 8Sn, Solution Annealed, Cold Finished, and Spinodal Hardened (TX TS)

AMS4597B (Current)

9/9/2026

This specification covers a copper-nickel-tin alloy in the form of bars and rods up to 3.25 inches (83 mm) in nominal thickness (see 8.7).

AMS D Nonferrous Alloys Committee

J3335_202609 (Current)

9/9/2026

This document provides a recommended test guideline for secondary sodium-ion cells used for propulsion of electric vehicles including battery electric vehicles (BEV), hybrid electric vehicles (HEV), and other similar propulsion applications (e.g., forklift trucks). The objective of this document is to define common test procedures covering electrical performance, mechanical safety performance, thermal safety performance, and electrical safety performance. The results of these procedures can be used for comparative purposes. Requirements for pass/fail criteria are not defined in this document but are to be defined by the users of the document.

Battery Standards Testing Committee

Laser Peening

AMS2546B (Current)

9/9/2026

This specification covers the requirements for computer-controlled laser peening of metal part surfaces to induce residual compressive stresses at and beneath the surface.

AMS B Finishes Processes and Fluids Committee

Application Layer - Diagnostics

J1939-73_202609 (Current)

9/9/2026

SAE J1939-73 defines the SAE J1939 messages to accomplish diagnostic services and identifies the diagnostic connector to be used for the vehicle service tool interface. Diagnostic messages (DMs) provide the utility needed when the vehicle is being repaired. Diagnostic messages are also used during vehicle operation by the networked ECUs to allow them to report diagnostic information and self-compensate as appropriate, based on information received. Diagnostic messages include services such as periodically broadcasting active diagnostic trouble codes, identifying operator diagnostic lamp status, reading or clearing diagnostic trouble codes, reading or writing ECU memory, providing a security function, stopping/starting message broadcasts, reporting diagnostic readiness, monitoring engine parametric data, etc. California-, EPA-, or EU-regulated OBD requirements are satisfied with a subset of the specified connector and the defined messages.

Truck and Bus Control and Communications Network Committee

Coolant Filter Test Procedure

J2709_202609 (Current)

9/4/2026

This SAE Recommended Practice is applicable to coolant filters installed on mobile or stationary equipment. It describes a body of tests used to characterize the stuctural integrity and filtration performance of coolant filters.

Filter Test Methods Standards Committee

INSTALLING AND REMOVAL TOOLS, CONNECTOR, ELECTRICAL CONTACT, TYPE III, CLASS 1, COMPOSITION B

AS81969/16B (Current)

9/4/2026

AE-8C2 Terminating Devices and Tooling Committee

FITTING, ELBOW, 90 DEGREE, INTEGRAL WELD RING, 3000 PSI

AS1584F (Current)

9/3/2026

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

TUBE END, WELD DESIGN STANDARD

AS1577C (Current)

9/3/2026

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

FITTING, TEE, INTEGRAL WELD RING, 3000 PSI

AS1583F (Current)

9/3/2026

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

RING, WELD 3000 PSI, TITANIUM

AS1580F (Current)

9/3/2026

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

COVER ASSEMBLY, ELECTRICAL, FOR MS27212 TERMINAL BOARD ASSEMBLY

AS18029F (Current)

8/31/2026

AE-8C2 Terminating Devices and Tooling Committee

INSTALLING AND REMOVAL TOOLS, CONNECTOR ELECTRICAL CONTACT, TYPE I, CLASS 1, COMPOSITION C

AS81969/17B (Current)

8/31/2026

AE-8C2 Terminating Devices and Tooling Committee

INSTALLING AND REMOVAL TOOLS, CONNECTOR, ELECTRICAL CONTACT, TYPE III, CLASS 2, COMPOSITION A

AS81969/12B (Current)

8/31/2026

AE-8C2 Terminating Devices and Tooling Committee

FITTING, REDUCER, INTEGRAL WELD RING, 3000 PSI

AS1585G (Current)

8/27/2026

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

SLEEVE, TUBE END, ACORN TO WELD, SHORT FLARELESS

AS4695D (Current)

8/27/2026

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

RING, WELD 3000 PSI, CRES

AS1893F (Current)

8/27/2026

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

UNION, TUBE END, EXTERNAL THREAD TO WELD, SHORT FLARELESS

AS4693E (Current)

8/27/2026

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

Axially Swaged Fittings, Installation and Inspection Procedure

AS5959C (Current)

8/25/2026

This procedure establishes the instructions to prepare tube ends and install and inspect axially swaged permanent tube fittings qualified to AS5958. This procedure is applicable when specified on the engineering drawing or in the procurement document.

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

NUT, HEXAGON, DRILLED, BOSS CONNECTION, ALUMINUM - UNS A92024

AS90991D (Current)

8/25/2026

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies

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